T.O. 1B-52H-34-2-8
AIRCREW WEAPONS DELIVERY MANUAL
(NONNUCLEAR)
B-52/AGM-158 JASSM
USAF
SERIES
B-52/AGM-158 JASSM
AIRCRAFT
WEAPONS
THE BOEING COMPANY
F34601-98-C-0002
F34601-03-D-0066
This manual contains unverified procedures. Refer to the validation/verification status page(s) prior to performing any operation or maintenance procedure.
THIS PUBLICATION IS INCOMPLETE WITHOUT CLASSIFIED SUPPLEMENT T.O. 1B-52H-34-2-8-1.
SEE T.O. 0-1-CD-1 FOR CURRENT STATUS OF FLIGHT MANUALS, SAFETY SUPPLEMENTS, OPERATIONAL SUPPLEMENTS, AND
FLIGHT CREW CHECKLISTS.
COMMANDERS ARE RESPONSIBLE FOR BRINGING THIS PUBLICATION TO THE ATTENTION OF ALL AIR FORCE PERSONNEL
CLEARED FOR OPERATION OF SUBJECT AIRCRAFT.
DISTRIBUTION STATEMENT E – Distribution authorized to the Department of Defense Components only, due to Direct Military Support, 29
October 1996. Other requests shall be referred to 327 BMSG/EN, Tinker AFB, OK 73145-3021.
WARNING –This document contains technical data whose export is restricted by the Arms Export Control Act (Title 22, U.S.C., Sec 2751, et seq.)
or the Export Administration Act of 1979, as amended, Title 50, U.S.C., App. 2401 et seq. Violations of these export laws are subject to severe
criminal penalties. Disseminate in accordance with provisions of DoD Directive 5230.25.
HANDLING AND DESTRUCTION NOTICE – Comply with distribution statement and destroy by any method that will prevent disclosure of
contents or reconstruction of the document. Demil code D.
PUBLISHED UNDER AUTHORITY OF THE SECRETARY OF THE AIR FORCE
1 DECEMBER 2003
CHANGE 3 – 1 JUNE 2006
T.O. 1B-52H-34-2-8
Technical orders are normally distributed promptly after printing. Date(s) shown on the title page (lower right corner) are for identification only. These
are not distribution dates. Processing time sometimes causes distribution to only appear to have been delayed.
INSERT LATEST CHANGED PAGES. DESTROY SUPERSEDED PAGES.
LIST OF EFFECTIVE PAGES
NOTE:
The portion of the text affected by the changes is indicated by a
vertical line in the outer margins of the page.
Dates of issue for original and changed pages are:
Original
0
1 Dec 03
Change
1
1 Dec 04
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2
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CURRENT ABBREVIATED CHECKLIST
AGM-158 JASSM
Abbreviated Flight Crew Checklist
T.O. 1B-52H-34-2-8CL-1
1 Dec 03
Change 3 - 1 Jun 06
Upon receipt of the second and subsequent changes to this technical order, personnel responsible for maintaining this publication in current
status will ascertain that all previous changes have been received and incorporated. Action should be taken promptly if the publication is
incomplete.
*The asterisk indicates pages changed, added, or deleted by the current change.
ADDITIONAL COPIES OF THIS PUBLICATION MAY BE OBTAINED BY USAF ACTIVITIES IN ACCORDANCE WITH T.O. 00-5-1.
A
Change 3
USAF
WARNING
This manual contains unverified procedures. Unverified procedures shall only be performed during verification, in accordance with TOs 00-5-1 and 00-5-3. Performance of unverified procedures may result in injury to personnel or damage to
equipment.
TECHNICAL ORDER VALIDATION/VERIFICATION STATUS PAGE
CHANGE NO. – DATE
PTO CHANGE NO. – DATE
1 DEC 03
CHANGE 2 - 1 JUL 2005
AMI
DATA ELEMENT
DATE
VALIDATED
(B)
(A)
TCTO Listings (P, PG iv)
Offensive Avionics System (OAS)
Interface (P, PG 1-11 )
Weapon Control Panel
Interface (P, PG 1-11 )
Missile Data Flow (Typical)
(F: 1-4, PG 1-13)
Weapon Control Panel
(F: 1-5, 2 /2, PG 1-15)
JASSM IKB Commands
(F: 1-9, 1/2, PG 1-19)
JASSM IKB Commands
(F: 1-9, 2/2, PG 1-20)
Weapon Jettison
(P, PG 1-22)
AJCP Commanded Jettison
(P, PG 1-22)
Pilot’s Bmb Bay & Missile Jett Contrl
Switch Commanded Jett (P, PG1-25)
JASSM SMO Software
(P, PG 1-27)
SMO MFD Displays
(P, PG 1-27 – 1-28)
Prime Mission Data
(P, PG 1-28)
Weapon Supervision Menu (CF-5)
(P, PG 1-30)
PART SIM Mode Command (CF-51)
(P, PG 1-30)
FULL SIM Mode Command (CF-52)
(P, PG 1-30)
JASSM Supervision Menu (CF-57)
(P, PG 1-30A)
JASSM Control Function (CF)
Commands (F: 1-16, PG 1-30B)
CF Menu
(F: 1-17, 1/2, PG 1-30C)
CF Menu
(F: 1-17, 2/2, PG 1-30D)
Weapon Supervision Menu (CF-5)
(F: 1-18, 1/2, PG 1-30E)
1 Mar 04
A
1 Mar 04
A
1 Mar 04
A
1 Mar 04
A
1 Mar 04
A
1 Mar 04
A
1 Mar 04
A
1 Mar 04
A
1 Mar 04
A
1 Mar 04
A
1 Mar 04
A
1 Mar 04
A
1 Mar 04
A
1 Dec 04
A
1 Dec 04
A
1 Dec 04
A
1 Mar 04
A
1 Mar 04
A
15 Mar 04
A
15 Mar 04
A
15 Mar 04
A
DATE
VERIFIED
VERIFICATION
METHOD
BASIC DATE
T.O. 1B-52H-34-2-8
VALIDATION
METHOD
T.O. NO.
REMARKS
(B)
LEGEND:
(A) DATA ELEMENT:
(S) = SECTION, (PG) = PAGE, (P) = PARAGRAPH, (F) = FIGURE, (T) = TABLE
(B) VALIDATION OR VERIFICATION METHOD:
(P) = PERFORMANCE, (S) = SIMULATION, (A) = ANALYSIS (TABLE-TOP)
V/VS-1
WARNING
This manual contains unverified procedures. Unverified procedures shall only be performed during verification, in accordance with TOs 00-5-1 and 00-5-3. Performance of unverified procedures may result in injury to personnel or damage to
equipment.
TECHNICAL ORDER VALIDATION/VERIFICATION STATUS PAGE
CHANGE NO. – DATE
PTO CHANGE NO. – DATE
1 DEC 03
CHANGE 2 - 1 JUL 2005
AMI
DATA ELEMENT
DATE
VALIDATED
(B)
(A)
Weapon Supervision Menu (CF-5)
(F: 1-18, 2/2, PG 1-30F)
15 Mar 04
Classified Data Erase Command
(CF-575) (P, PG 1-31)
1 Mar 04
JASSM Auto Targeting Mode
(CF-580) (P, PG 1-31)
1 Mar 04
Missile Tgt Assign(Manual Targeting)
Display (CF-586) (P, PG 1-31)
1 Mar 04
JASSM Supervision Menu (CF-57)
(F: 1-18, 1/2, PG 1-32)
15 Mar 04
JASSM Supervision Menu CF-57
(F: 1-18, 2/2, PG 1-33)
1 Mar 04
JASSM Targeting Menu (CF-58)
(F: 1-20, 1/2, PG 1-34)
1 Mar 04
JASSM Targeting Menu (CF-58)
(F: 1-20, 2/2, PG 1-35)
1 Mar 04
Missile Target Assignment Display
(CF-586) (F: 1-21, 1/3, PG 1-36)
1 Mar 04
Missile Target Assignment Display
(CF-586) (F: 1-18, 2/3, PG 1-37)
1 Mar 04
Missile Target Assignment Display
(CF-586) (F: 1-18, 3/3, PG 1-38)
1 Mar 04
Direct Target Definition Display
(CF-588,n) (P, PG 1-39)
1 Mar 04
Retarget-All Command (CF589)
(P, PG 1-41)
1 Mar 04
Direct Tgt Definition Disp (CF-588,n)
(P, 1-22, 2/4, PG 1-43)
1 Mar 04
CF-62 SMO Menu
(P, PG 1-46)
1 Mar 04
CF-65 Data Record
(P, PG 1-46)
1 Mar 04
CF-67 Shutdown
(P, PG 1-47)
1 Mar 04
CF-68 ECU Power Override
(P, PG 1-47)
1 Mar 04
CF-69A & CF-69B ACU Shutdown
(P, PG 1-47)
1 Mar 04
FCP Supervision Menu (CF-6)
(F: 1-23, 1/2, PG 1-48)
1 Mar 04
FCP Supervision Menu (CF-6)
(F: 1-23, 2/2, PG 1-49)
1 Mar 04
DATE
VERIFIED
VERIFICATION
METHOD
BASIC DATE
T.O. 1B-52H-34-2-8
VALIDATION
METHOD
T.O. NO.
REMARKS
(B)
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
LEGEND:
(A) DATA ELEMENT:
(S) = SECTION, (PG) = PAGE, (P) = PARAGRAPH, (F) = FIGURE, (T) = TABLE
(B) VALIDATION OR VERIFICATION METHOD:
V/VS-2
(P) = PERFORMANCE, (S) = SIMULATION, (A) = ANALYSIS (TABLE-TOP)
WARNING
This manual contains unverified procedures. Unverified procedures shall only be performed during verification, in accordance with TOs 00-5-1 and 00-5-3. Performance of unverified procedures may result in injury to personnel or damage to
equipment.
TECHNICAL ORDER VALIDATION/VERIFICATION STATUS PAGE
CHANGE NO. – DATE
PTO CHANGE NO. – DATE
1 DEC 03
CHANGE 2 - 1 JUL 2005
AMI
DATA ELEMENT
DATE
VALIDATED
(B)
(A)
SMO Load Menu (CF-62)
(F: 1-24, PG 1-50)
1 Mar 04
Mission Supervision Menu
(P, PG 1-51)
15 Mar 04
B-52 Mission Data Load Command
(P, PG 1-51)
1 Dec 04
Weapon Group Load Display
(CF-82A, CF-82C)(P, PG 1-52)
1 Mar 04
Mission Supervision Menu
(F: 1-25, 1/2, PG 1-52A)
15 Mar 04
Mission Supervision Menu
(F: 1-25, 2 /2, PG 1-52B)
15 Mar 04
B-52 Mission Data Load Display
(CF-81)(F: 25A, 1/2, PG 1-52C)
15 Mar 04
B-52 Mission Data Load Display
(CF-81)(F: 25A, 2/2, PG 1-52D)
1 Mar 04
Wpn Grp Load Menu
(F: 1-25B, 1/2, PG 1-52E)
1 Mar 04
Wpn Grp Load Menu
(F: 1-25B, 2/2, PG 1-52F)
1 Mar 04
Targeting Completion Command
(CF-DD) (P, PG 1-52G)
1 Mar 04
Direct Target Copy Command (CF-Dn)
(P, PG 1-52G)
1 Mar 04
Format (FRMT) Displays
(P, PG 1-56)
1 Mar 04
JASSM Status & Inventory Display
(FRMT-7)(P, PG 1-56)
1 Mar 04
JASSM Status & Invent Disp w/ Sel
Sta Status (FRMT-7xy)(P, PG 1-57)
1 Mar 04
Weapon Assignment Data Display
(P, PG 1-57)
1 Mar 04
Stores Inventory Summary Display
(FRMT-77)(P, PG 1-57)
1 Mar 04
JASSM Format Commands
(F: 1-28, PG 1-57)
1 Mar 04
JASSM FRMT (Format) Menu
(F: 1-29, 1/2, PG 1-58)
1 Mar 04
JASSM FRMT (Format) Menu
(F: 1-29, 2/2, PG 1-59)
1 Mar 04
PME Status Display (FRMT-6)
(F: 1-30, 1/2, PG 1-60)
1 Mar 04
DATE
VERIFIED
VERIFICATION
METHOD
BASIC DATE
T.O. 1B-52H-34-2-8
VALIDATION
METHOD
T.O. NO.
REMARKS
(B)
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
LEGEND:
(A) DATA ELEMENT:
(S) = SECTION, (PG) = PAGE, (P) = PARAGRAPH, (F) = FIGURE, (T) = TABLE
(B) VALIDATION OR VERIFICATION METHOD:
(P) = PERFORMANCE, (S) = SIMULATION, (A) = ANALYSIS (TABLE-TOP)
V/VS-3
WARNING
This manual contains unverified procedures. Unverified procedures shall only be performed during verification, in accordance with TOs 00-5-1 and 00-5-3. Performance of unverified procedures may result in injury to personnel or damage to
equipment.
TECHNICAL ORDER VALIDATION/VERIFICATION STATUS PAGE
CHANGE NO. – DATE
PTO CHANGE NO. – DATE
1 DEC 03
CHANGE 2 - 1 JUL 2005
AMI
DATA ELEMENT
DATE
VALIDATED
(B)
(A)
PME Status Display (FRMT-6)
(F: 1-30, 2/2, PG 1-61)
JASSM Status & Inventory Display
(FRMT-7)(F: 1-31, 1/6, PG 1-62)
JASSM Status & Inventory Display
(FRMT-7)(F: 1-31, 2/6, PG 1-62A)
JASSM Status & Inventory Display
(FRMT-7)(F: 1-31, 3/6, PG 1-62B)
JASSM Status & Inventory Display
(FRMT-7)(F: 1-31, 4/6, PG 1-62C)
JASSM Status & Inventory Display
(FRMT-7)(F: 1-31, 5/6, PG 1-62D)
JASSM Status & Inventory Display
(FRMT-7)(F: 1-31, 6/6, PG 1-63)
JASSM Stat & Invent Disp w/ Sel Sta
Status (F: 1-32, 2/5, PG 1-65)
JASSM Stat & Invent Disp w/ Sel Sta
Status (F: 1-32, 3/5, PG 1-66)
JASSM Stat & Invent Disp w/ Sel Sta
Status (F: 1-32, 4/5, PG 1-67)
JASSM Stat & Invent Disp w/ Sel Sta
Status (F: 1-32, 5/5, PG 1-68)
Weapon Assignment Data Display
(F: 1-32A, 1/2, PG 1-68A)
Weapon Assignment Data Display
(F: 1-32A, 2/2, PG 1-68B)
Stores Inventory Display
(F: 1-32B, Sheet 1/2, PG 1-68C)
Stores Inventory Display
(F: 1-32B, Sheet 2/2, PG 1-68D)
Weapon Summary Display
(P, PG 1-70)
Weapon Summary Display
(F: 1-34, 1/3, PG 1-71)
Weapon Summary Display
(F: 1-34, 2/3, PG 1-72)
Weapon Summary Display
(F: 1-34, 3/3, PG 1-73)
Program Display (PRGM)
(F: 1-36, 3/6, PG 1-77)
Program Display (PRGM)
(F: 1-36, 4/6, PG 1-78)
1 Mar 04
A
1 Mar 04
A
1 Mar 04
A
1 Mar 04
A
1 Mar 04
A
1 Mar 04
A
1 Mar 04
A
1 Mar 04
A
1 Mar 04
A
1 Mar 04
A
1 Mar 04
A
1 Mar 04
A
1 Mar 04
A
1 Mar 04
A
1 Mar 04
A
1 Mar 04
A
1 Mar 04
A
1 Mar 04
A
1 Mar 04
A
1 Mar 04
A
1 Mar 04
A
DATE
VERIFIED
VERIFICATION
METHOD
BASIC DATE
T.O. 1B-52H-34-2-8
VALIDATION
METHOD
T.O. NO.
REMARKS
(B)
LEGEND:
(A) DATA ELEMENT:
(S) = SECTION, (PG) = PAGE, (P) = PARAGRAPH, (F) = FIGURE, (T) = TABLE
(B) VALIDATION OR VERIFICATION METHOD:
V/VS-4
(P) = PERFORMANCE, (S) = SIMULATION, (A) = ANALYSIS (TABLE-TOP)
WARNING
This manual contains unverified procedures. Unverified procedures shall only be performed during verification, in accordance with TOs 00-5-1 and 00-5-3. Performance of unverified procedures may result in injury to personnel or damage to
equipment.
TECHNICAL ORDER VALIDATION/VERIFICATION STATUS PAGE
CHANGE NO. – DATE
PTO CHANGE NO. – DATE
1 DEC 03
CHANGE 2 - 1 JUL 2005
AMI
DATA ELEMENT
DATE
VALIDATED
(B)
(A)
General (Procedures)
(P, PG 2-3)
1 Mar 04
After Engine Start
(P, PG 2-7)
1 Mar 04
MIssile Power Application
(P, PG 2-9 - 2-10)
1 Mar 04
Post Strike/ Abort Procedures
(P, PG 2-22)
1 Mar 04
Selective Jettison Using WCP/SMO
(P, PG 3-3)
1 Mar 04
Selective Jettison Using AJCP
(P, PG 3-4)
1 Mar 04
Emergency Jettison
(P, PG 3-5)
1 Mar 04
Telemetry Power Off Command
(CF-57B) (Test Only)(P, PG 4-3)
1 Mar 04
MIssion Planning Considerations
(P, PG 6-7)
1 Mar 04
OAS/JASSM Operation
(P, PG 7-3)
1 Mar 04
WCE Power Application
(P, PG 7-7)
1 Mar 04
Missile Power Application
(P, PG 7-8)
1 Mar 04
Missile and Ejector Status
(P, PG 7-10 - 7-11)
1 Mar 04
Launch Point Target Number
(P, PG 7-12)
1 Mar 04
Missile GPS Alignment Quality
(P, PG 7-12)
1 Mar 04
JASSM Status & Inventory Display
(FRMT-7)(F: 7-4, PG 7-14)
1 Mar 04
Missile Mission Data and Targeting
(P, PG 7-17)
1 Mar 04
Missile Targeting Methods
(P, PG 7-17)
1 Mar 04
Automatic Targeting
(P, PG 7-17)
1 Mar 04
JASSM Tgt Assign (Manual Targeting)
Disp(CF-586)(F: 7-6, 1/2, PG 7-19)
1 Dec 04
Direct Target Definition Disp(CF-586)
(F: 7-7, 2/2, PG 7-20A)
1 Dec 04
DATE
VERIFIED
VERIFICATION
METHOD
BASIC DATE
T.O. 1B-52H-34-2-8
VALIDATION
METHOD
T.O. NO.
REMARKS
(B)
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
A
LEGEND:
(A) DATA ELEMENT:
(S) = SECTION, (PG) = PAGE, (P) = PARAGRAPH, (F) = FIGURE, (T) = TABLE
(B) VALIDATION OR VERIFICATION METHOD:
(P) = PERFORMANCE, (S) = SIMULATION, (A) = ANALYSIS (TABLE-TOP)
V/VS-5
WARNING
This manual contains unverified procedures. Unverified procedures shall only be performed during verification, in accordance with TOs 00-5-1 and 00-5-3. Performance of unverified procedures may result in injury to personnel or damage to
equipment.
TECHNICAL ORDER VALIDATION/VERIFICATION STATUS PAGE
CHANGE NO. – DATE
PTO CHANGE NO. – DATE
1 DEC 03
CHANGE 2 - 1 JUL 2005
AMI
DATA ELEMENT
DATE
VALIDATED
(B)
(A)
Missile/Tgt Assign (Man Targeting)
Data Entry Proced (P, PG 7-23)
Automatic Launch Determination
(P, PG 7-46)
Missile Jettison
(P, PG 7-50)
Simulation Capabilities
(P, PG 7-51)
Simulated Missile Loadout
(P, PG 7-51)
Simulated Targeting Operations
(P, PG 7-51)
Simulated WCE Responses
(P, PG 7-51)
Simulated Ranging
(P, PG 7-51)
SMO Termination
(P, PG 7-52)
SMO Restart
(P, PG 7-52)
JASSM Master Faults
(F: 7-19, 1/17, PG 7-53)
JASSM Master Faults
(F: 7-19, 2/17, PG 7-54)
JASSM Master Faults
(F: 7-19, 3/17, PG 7-55)
JASSM Master Faults
(F: 7-19, 4/17, PG 7-56)
JASSM Master Faults
(F: 7-19, 5/17, PG 7-57)
JASSM Master Faults
(F: 7-19, 6/17, PG 7-58)
JASSM Master Faults
(F: 7-19, 7/17, PG 7-59)
JASSM Master Faults
(F: 7-19, 8/17, PG 7-60)
JASSM Master Faults
(F: 7-19, 9/17, PG 7-61)
JASSM Master Faults
(F: 7-19, 10/17, PG 7-62)
JASSM Master Faults
(F: 7-19, 11/17, PG 7-63)
1 Mar 04
A
1 Mar 04
A
1 Mar 04
A
1 Mar 04
A
1 Mar 04
A
1 Mar 04
A
1 Mar 04
A
1 Mar 04
A
1 Mar 04
A
1 Mar 04
A
1 Dec 04
A
1 Mar 04
A
1 Mar 04
A
1 Dec 04
A
1 Mar 04
A
1 Dec 04
A
1 Mar 04
A
1 Dec 04
A
1 Dec 04
A
1 Mar 04
A
1 Dec 04
A
DATE
VERIFIED
VERIFICATION
METHOD
BASIC DATE
T.O. 1B-52H-34-2-8
VALIDATION
METHOD
T.O. NO.
REMARKS
(B)
LEGEND:
(A) DATA ELEMENT:
(S) = SECTION, (PG) = PAGE, (P) = PARAGRAPH, (F) = FIGURE, (T) = TABLE
(B) VALIDATION OR VERIFICATION METHOD:
V/VS-6
(P) = PERFORMANCE, (S) = SIMULATION, (A) = ANALYSIS (TABLE-TOP)
WARNING
This manual contains unverified procedures. Unverified procedures shall only be performed during verification, in accordance with TOs 00-5-1 and 00-5-3. Performance of unverified procedures may result in injury to personnel or damage to
equipment.
TECHNICAL ORDER VALIDATION/VERIFICATION STATUS PAGE
CHANGE NO. – DATE
PTO CHANGE NO. – DATE
1 DEC 03
CHANGE 2 - 1 JUL 2005
AMI
DATA ELEMENT
DATE
VALIDATED
(B)
(A)
JASSM Master Faults
(F: 7-19, 12/17, PG 7-64)
JASSM Master Faults
(F: 7-19, 13/17, PG 7-65)
JASSM Master Faults
(F: 7-19, 14/17, PG 7-66)
JASSM Master Faults
(F: 7-19, 15/17, PG 7-67)
JASSM Master Faults
(F: 7-19, 16/17, PG 7-68)
JASSM Master Faults
(F: 7-19, 17/17, PG 7-68A)
JASSM Advisories
(F: 7-20, 2/3, PG 7-68C)
JASSM Advisories
(F: 7-20, 3/3, PG 7-68D)
JASSM Status Messages
(F: 7-21, PG 7639)
Safe Release Advisories
(F: 7-22, PG 7-69)
1 Dec 04
A
1 Dec 04
A
1 Mar 04
A
1 Mar 04
A
1 Dec 04
A
1 Dec 04
A
1 Dec 04
A
1 Dec 04
A
1 Mar 04
A
1 Mar 04
A
DATE
VERIFIED
VERIFICATION
METHOD
BASIC DATE
T.O. 1B-52H-34-2-8
VALIDATION
METHOD
T.O. NO.
REMARKS
(B)
LEGEND:
(A) DATA ELEMENT:
(S) = SECTION, (PG) = PAGE, (P) = PARAGRAPH, (F) = FIGURE, (T) = TABLE
(B) VALIDATION OR VERIFICATION METHOD:
(P) = PERFORMANCE, (S) = SIMULATION, (A) = ANALYSIS (TABLE-TOP)
V/VS-7/(V/VS-8 blank)
BLA
T.O. 1B-52H-34-2-8
STATUS OF SAFETY AND OPERATIONAL SUPPLEMENTS
This supplement status page is based on information available to the manual editor as of the date of
this publication. The information may not be current as it must be updated by any subsequent supplement status pages and by reference to T.O. 0-1-CD-1.
SUPPLEMENTS IN THIS CHANGE
Number
Date
Short Title
Section Affected
OUTSTANDING SUPPLEMENTS
Number
Date
Short Title
Section Affected
SS-1(I)
30 September 03
Recycle Weapon Power After Targeting
II, VII
SS-4(I)
27 January 06
JASSM Launch Criteria
II, V, VI
Change 3
Flyleaf-1/(Flyleaf-2 blank)
BLA
T.O. 1B-52H-34-2-8
Table of Contents
SECTION I
DESCRIPTION
1-1
SECTION II
NORMAL AIRCREW PROCEDURES
2-1
SECTION III EMERGENCY AIRCREW PROCEDURES
3-1
SECTION IV SUPPLEMENTARY DATA
4-1
SECTION V
5-1
OPERATING LIMITATIONS
SECTION VI MISSION PLANNING
6-1
SECTION VII SYSTEMS OPERATION
7-1
GLOSSARY
ALPHABETICAL INDEX
GLOSSARY 1
INDEX 1
i
T.O. 1B-52H-34-2-8
INTRODUCTION
SCOPE. This manual provides aircrews with descriptive and procedural information required
for delivery of the AGM-158 Joint Air-To-Surface Standoff Missile (JASSM) from B-52H aircraft modified with Integrated Conventional Stores Management System (ICSMS), and the
Standoff Weapon Stores Management Overlay loaded.
CHECKLISTS. Abbreviated checklists for the procedures given in this manual are contained in
a stand alone Weapon Delivery Checklist. This checklist is identified by a T.O. number that is
identical to that of the applicable weapon delivery manual except for the addition of the letters CL (checklist).
ARRANGEMENT. This manual is divided into seven sections as follows:
Section I, DESCRIPTION – Locates, identifies, and functionally describes the weapon
and aircraft components which directly concern the aircrew in the control and delivery of the JASSM.
Section II, NORMAL AIRCREW PROCEDURES – Contains partially illustrated amplified checklists for performance of normal aircrew weapon delivery procedures from
preflight through after landing and procedures applicable in the event a mission is
aborted.
Section III, EMERGENCY AIRCREW PROCEDURES – Contains weapon jettison
procedures. No attempt is made to regulate or define conditions under which the mission will be aborted.
Section IV, SUPPLEMENTARY DATA – Contains information on operational test systems.
Section V, OPERATING LIMITATIONS – Contains important weapon and weapon
system limitations that must be taken into account during planning and accomplishment of a mission.
Section VI, MISSION PLANNING – Contains information on transportation of dangerous material, inflight emergency notification, and inflight mission data changes
that can be accomplished by the flightcrew.
Section VII, SYSTEMS OPERATION – Contains additional material regarding the
operation of the aircraft, JASSM systems. Theory of guidance system operation, guidance performance, and malfunction analysis are included.
PRECEDENCE. Compliance with procedures herein is mandatory. In all instances, only those
operations which are within the scope of the current applicable safety rules may be performed.
SAFETY POLICIES. The procedures in this manual reflect the latest applicable rules and poli-
cies. Aircrew compliance with these procedures and policies is mandatory.
Mission planning shall provide maximum protection to friendly and neutral areas consistent
with operational requirements. Selection of launch point and type of maneuver shall be
guided by the possible effect upon friendly or neutral areas of a missile guidance or control
system failure. Since launch point and type of maneuver are sufficiently flexible to allow for
inflight decisions, aircrews shall be briefed concerning the potential disaster hazard to
friendly or neutral areas.
ii
Change 2
T.O. 1B-52H-34-2-8
REFERENCES. The following publications, available to using commands, should be used to
gain more comprehensive information on subjects referred to in this technical order:
1B-52H-1
Flight Manual
1B-52H-1-1
Flight Manual - Appendix 1, Performance Data
1B-52H-1-12
Radar Navigator’s/Navigator’s Manual
1B-52H-1-13
Electronic Warfare Officer’s Manual
1B-52H-2-31GA-1 General Aircraft/Bomb Release System B-52H
1B-52H-33-2-1
Nonnuclear Munitions Loading Procedures
1B-52H-34-2-1
Aircrew Weapon Delivery Manual (Nonnuclear) B-52
1B-52H-34-2-7
Aircrew Weapon Delivery Manual (Nonnuclear) B-52/AGM-154 JSOW
1B-52H-34-2-8-1 B-52H/AGM-158 Aircrew Weapons Delivery Manual
Classified Supplement
1B-52H-34-2-9
Aircrew Weapon Delivery Manual (Nonnuclear) B-52/AGM-86C/D
1B-52H-5
Basic Weight Checklist and Loading Data B-52H
1-1M-34
Aircrew Weapons Delivery Manual (Nonnuclear)
JMEM
Joint Munition Employment Manual
SAFETY AND OPERATIONAL SUPPLEMENTS. Information involving flightcrew safety and di-
rectly pertaining to the information contained herein will be promptly forwarded to you by
Safety Supplements issued against this manual. Safety Supplements covering loss of life will
get to you in 48 hours by message (called Interim Safety Supplements) and those concerning
serious damage to equipment within 15 days by mail (in a formal printed form). Operational
information not involving safety but of an urgent nature will be forwarded to you by Operational Supplements issued against this manual. These will be forwarded by message (interim) or by mail (formal), depending on the urgency of the information. Interim supplements
are normally replaced by formal printed supplements at an early date. Formal printed supplements are identified by red letters “SS” for safety supplements and black letters “OS” for
operational supplements printed around the borders of the pages. The currency of safety and
operational supplements affecting your manual can be determined by referring to the Weekly
Index of Bomber Aircraft Safety Supplements (T.O. 0-1-CD-1). The title block of each supplement and the title page of this manual should also be checked to determine the effect they
may have on existing supplements. You must remain constantly aware of the status of all
supplements – current supplements must be complied with, but there is no point in restricting your operation by complying with a replaced or rescinded supplement. As a further aid a
supplement summary is included in this manual, following the A pages, for both safety and
operational supplements: however, this summary can only be as current as this manual.
Safety and operational supplements will be filed in accordance with Section VI of the Air
Force Technical Order System, T.O. 00-5-1.
WARNINGS, CAUTIONS, AND NOTES. The following definitions apply to “Warnings,” “Cautions,”
and “Notes” found throughout the manual.
Operating procedures, techniques, etc, which could result in personal injury or loss
of life if not carefully followed.
Operating procedures, techniques, etc, which could result in damage to equipment
if not carefully followed.
NOTE
An operating procedure, technique, etc, which is considered essential to emphasize.
Change 2
iii
T.O. 1B-52H-34-2-8
SHALL, WILL, SHOULD, and MAY. The following definitions apply to the words:
SHALL or WILL
The instructions or procedures prefaced by “shall” or “will” are
mandatory.
SHOULD
Normally used to indicate a preferred but nonmandatory
method of accomplishment.
MAY
An acceptable or suggested means of accomplishment.
CHANGE SYMBOLS. Changes to existing material and addition of new material are indicated
by one of three types of symbols determined by the nature of the material affected. Text material utilized a vertical line in the margin adjacent to the affected area. New illustrations
(figures) utilize a vertical line in the outer margin of the page. Line drawings use a miniature
pointing hand to highlight the affected area. Change symbols are not used for blank space
resulting from deletions, indexes, and tabular data where changes cannot be identified, relocation of material, or correction of minor inaccuracies unless such correction changes the
meaning.
RESPONSIBLE AGENCY. Every effort is made to keep this manual current. Review conferences
with operating personnel and a constant review of reports assure inclusion of the latest data
in this manual. Comments, corrections, and questions regarding this manual should be submitted on AF Form 847 through the local standardization/evaluation unit and routed to 327
BMSG/EN, 3001 Staff Drive Suite 2AF193A, Tinker AFB, Oklahoma 73145-3021.
RETROFIT CODING. The following code symbols along with the word ‘‘Less’’ are used to
distinguish information related to aircraft that have the described retrofit change
incorporated from that which is applicable to aircraft not yet retrofitted. This list contains
only TCTO’s currently active. Those known to be completed are not included.
SYMBOL
CS
[AMI]
iv
Change 3
T.O. NO.
⎧1B-52H-753
⎨
⎩1B-52H-756
1B-52H-830
TITLE
Installation of Global Positioning System (GPS) on B-52H
Aircraft (ECP 0109)
Installation of Integrated Conventional Stores Management System (ICSMS)
on B-52H Aircraft (ECP 0109)
Replacement of Ballistics Computer Set AN/AYQ-10 and Inertial Navigation
System AN/ASN-136 on B-52H Aircraft.
T.O. 1B-52H-34-2-8
Description
table of contents
PART 1 – B-52/AGM-158 JASSM SYSTEM DESCRIPTION
section I
page
1-3
B-52/JASSM WEAPON SYSTEM
1-3
B-52 CARRIER EQUIPMENT
1-3
JOINT AIR-TO-SURFACE STANDOFF MISSILE (JASSM)
1-3
JASSM SUSPENSION SYSTEM
1-7
JASSM COVER
1-7
PART 2 – OFFENSIVE AVIONICS SYSTEM
OFFENSIVE AVIONICS SYSTEM (OAS) INTERFACE
OAS/WEAPON SYSTEM RELATED CONTROLS AND DISPLAYS
WEAPON JETTISON
PART 3 – JASSM SMO SOFTWARE
SMO MFD DISPLAYS
1-11
1-11
1-11
1-22
1-27
1-27
RELEASE ADVISORY DISPLAY
1-27
PRIME MISSION DATA
1-29
CONTROL FUNCTION (CF) DISPLAYS
1-29
FORMAT (FRMT) DISPLAYS
1-56
PROGRAM (PRGM) DISPLAYS
1-74
1-1/(1-2 blank)
BLA
T.O. 1B-52H-34-2-8
PART 1 - B-52/AGM-158 JASSM SYSTEM DESCRIPTION
B-52/JASSM WEAPON SYSTEM
The B-52 Joint Air to Surface Standoff Missile
(JASSM) weapon system consists of a Conventional
Enhancement Modification (CEM) modified B-52
with OAS, and the JASSM. The B-52 aircraft has
the capability of releasing 12 JASSM missiles, six
from each Heavy Stores Adapter Beam (HSAB)
mounted on an Integrated Conventional Stores
Management System (ICSMS) external pylon.
B-52 CARRIER EQUIPMENT
The offensive avionics system (OAS) controls power
application, programming, and launch of missiles.
The OAS also provides signal processing, storage
avionics, control and display panels, missile supervision, regulated dc power conversion, and monitors
environmental control equipment in the aircraft.
The OAS interfaces with the carrier electrical
sources, and panel lighting. Primary missile control
and monitor is provided through the OAS weapon
control panel (WCP), integrated keyboard (IKB)
and the multifunction displays (MFD).
The B-52, when configured for JASSM carriage and
release, is equipped with the following equipment:
OAS Hardware; OAS Software, including the Joint
Air-To-Surface Standoff Missile Stores Management Overlay (JASSM SMO); and Less [AMI] the
pilots’ moving map display, which depicts both the
In-Range and In-Zone Launch Acceptability Regions (LARs) for the JASSM. For information on
the pilots’ moving map display see GPS IU/TACAN
EMULATION in T.O. 1B-52H-1.
anti-jam capability is also provided to ensure robust
performance. The no-seeker mission option provides
excellent performance against soft targets using
GPS/Inertial guidance to target impact. The seeker
is employed against targets requiring high impact
precision. The no-seeker mission option can be used
in a GPS/Inertial terminal guidance mode.
The JASSM is trapezoidal in cross section. The fuselage is constructed from composite shells of a
sandwiched foam core construction. An internal
hardback assembly and several bulkheads provide
structural strength. A pair of folding lugs with 30
inch spacing is provided for mating to the ejector
rack. Flight surfaces (wings) are stowed in a folded
location under the fuselage and are pyrotechnically
deployed after launch. A single vertical tail surface
assists in steering control. The vertical tail surface
is stowed in a folded position and is also pyrotechnically deployed after launch. Electrical connection to
the B-52 is made via a MIL-STD-1760 cable interface through the missile umbilical connector just aft
of the rear launch lug. After release, pyrotechnics
are fired to deploy both the flight surfaces and the
vertical tail. Propulsion is provided by a liquid
fueled (JP-10) Teledyne 370 series turbojet engine.
JASSM uses a 1000-pound class WDU-42/B warhead with a FMU-156B fuze. The aircraft MILSTD-1760 cable connection to the missile umbilical
is the only electrical connection to the missile. All
missile arming and flight transition actions are
electronically controlled within the missile after
missile release. No other lanyards or release devices are required between the host aircraft and the
JASSM.
JOINT AIR-TO-SURFACE STANDOFF MISSILE
(JASSM)
JASSM physical characteristics are as follows:
The AGM-158A JASSM, figure 1-1, is an airlaunched, medium range autonomous cruise missile. JASSM is designed as a launch and leave
weapon system, in that once launched, the missile
will navigate to and engage its planned target with
no further control communication from the launching aircraft or other command agency. The use of
the Infrared (IR) seeker in the nose of the missile is
optional based on target requirements. The missile
uses a tightly coupled Global Positioning System
(GPS) aided Inertial Navigation System (INS) for
mid-course and terminal area navigation. A GPS
Length
Width
Height
Lug Spacing
Wing Span (fully deployed)
Engine
Weight
Seeker
Guidance
Warhead
168 inches
24.9 Inches
20.4 Inches
30 inches
120 inches
Teledyne 370 series
Turbojet
2250 pounds
Infrared
GPS/Inertial
WDU-042
One Thousand
Pound Class
Change 3
1-3
T.O. 1B-52H-34-2-8
Joint Air to Surface Standoff Missile (JASSM)
Figure 1-1
1-4
T.O. 1B-52H-34-2-8
FUSELAGE
VERTICAL TAIL
The fuselage has a pointed nose with a trapezoidal
cross section. Two covers close out the bottom of the
fuselage. The forward cover encloses the IR seeker,
Inertial Measuring Unit (IMU), Missile Control
Unit (MCU), warhead and the wing section, while
fitting around the forward inlet lips; the aft cover
encloses the propulsion section and aft fuel tank
and test instrumentation kit areas.
The vertical tail is constructed similar to the wings.
Prior to launch the tail is folded over 135 degrees
and held in place by a mechanical latch. After
launch a pyrotechnic actuator located in the folded
tail fires to erect and latch the tail. The entire vertical tail pivots on a metallic shaft for yaw control.
The electro-mechanical rotary yaw actuator is located inside the aft fuselage. The Bomb Impact Assessment (BIA) antenna is located in the vertical
fin.
The fabricated skins are constructed of stiffened
foam cores contained between composite panels.
The bulkheads consist of a superframe assembly
and 2 conventional frames. The superframe assembly supports the launch lug, ejector and sway brace
loads, and missile retention. The aft lower bridge
encloses the warhead below the aft lug. The main
superframe and the wing carry-through are fabricated from stainless steel. The superframe assembly is split horizontally to allow the installation of
the warhead late in the assembly process. The composite forward frame provides stiffness. The engine/
tail frame secures the engine to the upper fuselage,
the vertical fin actuator and the vertical fin root.
WINGS
The missile has two deployable wings. The wings
have a constant chord and thickness except at the
wing fuselage intersection where the upper wing
surface transitions to a flat surface for the wing
pivot integration. Mechanical latches hold the
wings next to the missile fuselage until launch to
prevent flutter during captive carriage. The wings
are deployed in a two step process, using a twostage pyrotechnic actuator. The wings are commanded to extend to 75 degrees when clear of the
launch aircraft. This first deployment position increases pitch stability to aid separation from the
host aircraft. The wings move from 75 degrees to a
45 degree sweep position for cruise when initial
pitch stability is achieved. The 45 degree sweep
position aids longitudinal stability and contributes
a large dihedral effect. The wing deployment mechanism connects both the left and right wings to ensure symmetrical deployment.
An elevon located on the outer portion of each wing
provides pitch and roll control. The elevons are not
effective until the wings are deployed to 45 degrees.
Roll control is provided by differential elevon deflections and pitch control by symmetrical deflection.
Electro-mechanical actuators mounted inside the
wing spars drive the elevons.
BLOW OFF WEDGES
Two expendable wedges are located on the underside of each aft strake and held in place by pyrotechnic retention pins. The wedges insure the missile makes a clean separation from the aircraft and
are jettisoned from the missile after a fixed delay
following launch. Wedge separation occurs after
wings are deployed.
WARHEAD
The WDU-42/B warhead provides the hard target
penetration, detonation, and blast/fragmentation
damage capabilities for the JASSM. The warhead
consists of the loaded case, containing PBX(AF)-757
insensitive munition fill, and an FMU-156/B fuze.
The warhead is capable of penetrating and defeating hardened underground facilities as well as destroying soft targets. Arming power is provided only
from the JASSM engine alternator. The FMU-156/B
is a programmable fuze. The fuze is installed in the
aft well of the warhead case and secured with a retaining ring. The FMU-156/B modes of operation
are BIT, arm, impact fire and command fire. The
command fire delay times are instantaneous, 10, 15
20, 30, 40, 50 and 120 milliseconds. Fuze settings
are established during mission planning and can be
changed in flight.
FUEL SYSTEM
Fuel (JP-10) is carried in four fuselage fuel tanks
made of aluminum. The fuel system distributes fuel
from the tanks to the engine, transfers fuel between
tanks, and vents the tanks during filling. The fuel
tanks are pressurized by engine bleed air during
missile powered flight. Fuel from the tanks is fed to
the fuel pump where pressure is boosted to the
pressure level required by the engine for engine
start.
1-5
T.O. 1B-52H-34-2-8
ENGINE
IR Seeker Assembly
A Teledyne turbojet powers the vehicle. The flush
lower surface mounted inlet has full line of sight
blockage. The nozzle also provides for an ejector
flow to aid engine compartment cooling. A pyrotechnic cartridge starts the engine. The engine has a
variable throttle for optimal cruise or airspeed control to meet the time on target requirement.
The IR seeker assembly consists of a dual axis lineof-sight gimbal assembly, a sensor assembly; optics,
reference wheel assembly; a squib activated gas
bottle for cooling the sensor to cryogenic temperatures; and an Inertial Measurement Unit (IMU).
The IMU is attached to the seeker assembly to ensure dynamic alignment.
AIR DATA SYSTEM
JASSM Anti-Jam Global Positioning System Receiver
(JAGR) and JAGR-S Selective Availability Anti-Spoofing
Module (SAASM)
The air data system is composed of an Air Data
Probe (ADP), one Flush Static Port (FSP), and related sensor cards as part of the avionics package.
The air data system is equipped with anti-ice heaters on both the ADP and FSP. Weapon (115VAC)
power for missile loaded locations applies warmup
power to these heaters. Warm-up time may take up
to 13 minutes depending on ambient temperature.
The heaters remain on as long as 115 VAC power is
applied. Temperatures for these heaters can reach
250 degrees F. Heaters are on during any WIU operations.
Without proper warm-up time, icing can degrade the missile pitot-static system such
that mission failure could occur. Ensure the
JASSM heater power is applied (WIU ON)
at least 15 minutes prior to launch. If icing
conditions are encountered prior to 15 minutes of heater operation, then a minimum
warm-up time of 30 minutes is required
prior to launch.
AVIONICS
The JASSM Avionics consists of the Missile Control
Unit (MCU), Seeker Assembly, JASSM Anti-jam
Global Positioning System Receiver (JAGR or JAGRS), and associated antennas. The seeker assembly
consists of the gimbaled IR imaging sensor and IMU.
Missile Control Unit (MCU)
The MCU provides electrical power distribution
along with centralized communication, timing, control and processing for the operation of the missile,
and generates telemetry data. Its functional elements consist of a squib and power distribution
CCA, a system interface and processing CCA, and
actuator control CCA; and air data transducer assembly; a BIA transmitter; and an Electromagnetic
Interference (EMI) filter assembly.
1-6
Change 1
The JAGR provides the MCU with GPS measurement data computed from GPS satellite data collected in a jamming environment. Critical functions
performed by the JAGR include: acceptance of initialization data, acceptance of inertial aiding data
from the MCU, receiving GPS satellite and jammer
signals from the antenna, minimization of the jammer to GPS signal ratios, satellite selection, GPS
receiver control, computation of GPS data, and BIT.
The JASSM Anti-Jam GPS Receiver-SAASM (JAGRS) is a high fidelity Anti-Jam GPS receiver. It
achieves its Anti-Jam performance through the integration of a multi-channel analog RF Front End,
the implementation of Space-Time Adaptive signal
processing algorithms in digital nuller/front beamformer electronics and GPS measurement algorithms
in a digital receiver back-end. The JAGR-Ss critical
task is to provide GPS satellite line-of-sight (LOS)
Range and Delta-range measurements to the Navigation functions algorithms in the MCU. In order to
provide these measurements, the JAGR-S receives
Position, Time and Velocity Initialization data and inertial aiding data from the MCU and tracks GPS satellite signals from the GPS satellite through a Controllable Radiation Pattern (CRPA) antenna. In the
case of operation in a jamming environment, the digital beamformer/nuller adaptively and dynamically
nulls signals in the direction of the jammers while simultaneously steering multiple higher gain producing signal reception beams in the known directions of
the GPS satellites. This provides interference-free
LOS measurements to the MCU’s navigation function.
Bomb Impact Assessment (BIA) System
The BIA system’s primary function is to transmit
missile terminal engagement status and missile
health data just prior to target impact. The transmitter provides 25 watts of output power and is capable of transmitting data at 2400 Bps rate to a
line-of-sight airborne platform such as the RC-135
(RIVET JOINT) aircraft. The BIA transmitter is
connected to an antenna mounted in the tail for tactical operation. The BIA begins sending repeated
messages approximately 10 seconds prior to impact.
T.O. 1B-52H-34-2-8
JASSM SUSPENSION SYSTEM
JASSMs are carried externally on CEM modified
wing pylon weapon suspension assemblies which
are attached to the wing pylon adapter. Up to 6
JASSMs can be carried on each B-52 wing pylon.
Figure 1-2 illustrates the JASSM suspension system.
Each suspension assembly consists of the following:
Stub Pylon (Modified Wing Pylons)
Heavy Stores Adapter Beam (HSAB)
MAU-12 Ejector Racks (6 JASSM)
The HSAB is attached to the stub pylon on each wing
and houses the wire harnesses for missile control and
release. The adapter beam has provisions for carrying
6 JASSMs on stations 1, 2, 3, and 6, 7, 8.
The MAU-12 ejector rack (figure 1-3) is used to suspend and release the missiles. Each rack is
equipped with two hooks and four sway braces
which hold and support the missile. Two ejector
feet, one near each hook between each pair of sway
braces, ejects the missile when release is commanded. The rack has provisions for a ground safety
lockpin and an inflight safety lock. An extension
has been added to the rack which contains the umbilical restraint. This restraint is a cable which
holds the umbilical cable in position to help ensure
a clean missile separation when the missile is released. Electrical circuits to the inflight safety lock
are available but not used. Therefore, a bolt with
nut is installed in the inflight safety lockout pin
hole of each MAU-12 rack. The ground safety lockpin is used to prevent operation of the racks while
on the ground.
JASSM COVER
The missile is covered with an environmental cover,
whenever it is outside the shipping and storage container, which includes when loaded on external
stores stations for ground alert and other “extended
periods”. The environmental cover serves to protect
air data probe ports, static ports, and engine openings from dirt, debris and any other hazards that
may be the result of poor environmental conditions.
The environmental cover is required, due to warranty considerations.
The effects of environmental contamination
on weapon reliability and accuracy are unknown.
1-7
T.O. 1B-52H-34-2-8
Heavy Stores Adapter Beam JASSM Configuration
Figure 1-2
1-8
T.O. 1B-52H-34-2-8
MAU-12 Ejector Rack With Extension
1
2
3
4
5
6
INFLIGHT SAFETY LOCKOUT PIN
QUICK RELEASE PIN
LANYARD CHANNEL
QUICK RELEASE PIN
UMBILICAL RESTRAINT A HOLE
UMBILICAL RESTRAINT B HOLE
7
8
9
10
11
12
UMBILICAL RESTRAINT C HOLE
CAMLOCK FASTENER
LEFT PLATE ASSEMBLY
FORWARD CABLE LANYARD
UMBILICAL CABLE LANYARD
CENTER CHANNEL ASSEMBLY
Figure 1-3
1-9/(1-10 blank)
BLA
T.O. 1B-52H-34-2-8
PART 2 - OFFENSIVE AVIONICS SYSTEM
OFFENSIVE AVIONICS SYSTEM (OAS)
INTERFACE
Less [AMI] The B-52 Integrated Conventional
Stores Management System (ICSMS) provides OAS
control for release of JASSM. The ICSMS operational computer program consists of a Ground
Maintenance Computer Program (GMCP) and
Flight Computer Program (FCP). The GMCP is not
discussed. The FCP consists of the Flight Management System (FMS) and JASSM Stores Management Overlay (JASSM SMO). For further information regarding ICSMS and basic SMO functions, refer to INTEGRATED CONVENTIONAL STORES
MANAGEMENT SYSTEM, T.O. 1B-52H-1-12.
Less [AMI] The JASSM SMO software controls
JASSM functions. The Navigation and Weapon Delivery (NAWD) ACU executes the navigation and
weapon delivery functions for the SMO. The Controls and Displays (CAD) ACU executes the controls
and displays function along with a majority of the
BIT (Built In Test) processing.
[AMI] The B-52 OAS provides control for programming and release of JASSM. The operational computer program consists of a Ground Maintenance
Computer Program (GMCP) and Flight Computer
Program (FCP). The GMCP is not discussed. The
FCP consists of the Flight Management System
(FMS), Common Stores Processing (CSP), and
JASSM Stores Management Overlay (JASSM
SMO). For further information regarding OAS and
basic SMO functions, refer to T.O. 1B-52H-1-12.
[AMI] The OAS provides the capability for controlling and monitoring more than one type of weapon
system at a time. This is accomplished by the CSP
and loading multiple weapon SMOs. Currently, only
the CALCM SMO may be loaded with the JASSM
SMO. With the CALCM and JASSM SMOs loaded,
MIU/WIU power, environmental conditioning and
monitor capabilities are available to all the CALCM
and JASSM weapons. However, all other weapon
functions are available only to those weapons controlled by the Primary SMO.
• [AMI] If the JASSM SMO is not the Prima-
ry SMO, only WIU power, heating and monitoring functions (FRMT 7A, 7C and 77) are
available for the missiles.
• [AMI] If the JASSM SMO is not the Prima-
ry SMO and a mission planned JASSM
launch point is 30 minutes away, a JASSM
EVENT advisory message will be displayed.
• [AMI] If the JASSM SMO is not the Prima-
ry SMO and a mission planned JASSM
launch point is 25 minutes away, a JASSM
EVENT master fault will be displayed.
OAS/WEAPON SYSTEM RELATED CONTROLS AND
DISPLAYS
Operator controls and displays for weapon release
system control are located at the pilots’ and navigators’ stations. The munitions consent panel is located at the pilots’ station. The Weapon Control
Panel (WCP), OAS Power Control Panel (OAS
PCP), keyboards, MFD, and computer control panel
are located at the navigators’ station. See figure 1-4
for OAS/weapon data flow.
Weapon Control Panel
The Weapon Control Panel (WCP) (figure 1-5), located on the navigator’s front panel, provides controls for missile power application, missile power
removal, missile jettison, or missile abort. Missiles
are selected with the LOCATION (LP and RP) and
STATION (1, 2, 3, 6, 7, 8, and ALL) switches. The
WCP station switches are enabled only when one or
both pylon locations have been selected. If no location is selected when either the ALL station switch
or an individual station switch has been selected,
the advisory message LOCATION?? will be displayed on each MFD. If the bay location is selected
the advisory B: LOCATION will be displayed on
each MFD. If an invalid station (4 or 5) is selected,
the advisory Less [AMI] STATION??, [AMI]
JASSM STATION?? will be displayed on each MFD.
NOTE
• [AMI] With JASSM designated as the Pri-
mary SMO (CF-62x), all JASSM weapon
functions are available. The JASSM can be
powered, aligned, monitored, targeted,
ranged, launched and jettisoned (through
OAS).
Change 2
1-11
T.O. 1B-52H-34-2-8
WEAPON CONTROL PANEL ABNORMAL
PROCEDURES
An advisory WCP on the MFD indicates malfunction on the WCP. The operator will use CF-E (figure
1-26) to back up actions accomplished on the WCP.
This will allow the operator to work around certain
failures of the WCP and OAS PCP.
NOTE
With a total WCP failure prior to accomplishing hardwired function, (LOCK-UNLOCK) missile release is not possible.
CF-E may be used in conjunction with an operational WCP and OAS PCP to operate the system.
The operators may use keyboard entries to perform
functions mechanized on these panels at any time
regardless of the panels go/no-go status. The OAS
will treat the keyboard command as if it had originated from the WCP or OAS PCP. The lock-unlock
function is not available on the CF-E backup. The
display is laid out in basically the same arrangement as the panel. To accomplish a backup action
for the malfunctioning panel switch, the operator
enters CF-E and the symbols associated with the
switch on the keyboard in the same sequence that
normal switch operation would occur. See CF-E this
section for further discussion of the CF-E functions.
and will remain latched if the WIU loses power or is
shut down by the OAS. The light in the switch is
software controlled and will go out when WIU
power is removed regardless of switch position. To
reapply power to the WIU when they have been
shut down by other than the operator, the switch
must be pressed and released to reset the switch
and then pressed a second time to reapply WIU
power. If PCP switches malfunction, the navigator
or radar navigator can select CF-E which provides
a display of the PCP switches.
Keyboard
The keyboards (figure 1-8) located at the navigator’s and radar navigator’s stations, provide interface with the control of the OAS and weapon system. The keyboard and MFD provide operator interface with the missiles through the selection of
format (FRMT), control function (CF), program
(PRGM), and modify (MDFY) commands. The selection of FRMT results in the display of a specific
OAS and missile data presentation on the selected
MFD. Control function selection results in display
of a specific OAS data display or initiates the entry
into a specific operating mode. If WCP switches
malfunction, the navigator or radar navigator can
select CF-E which provides a display of the WCP
switches and the MIU power switches.
IKB commands associated with the JASSM are
listed in figure 1-9.
Pilot’s Munitions Consent Panel
MULTIFUNCTION DISPLAYS
The pilot’s munitions consent panel (figure 1-6) contains the PREARM-OFF and LOCK-UNLOCK
switches. The panel provides unlock consent for
powering the weapon ejectors. The PREARM function of the pilot’s switch is not used with JASSM.
The LOCK-UNLOCK switch is guarded in the
LOCK position.
The multifunction display (MFD) (figure 1-10) is a
CRT display unit. The MFD displays scan converted radar video, electro-optical viewing system
(EVS) video, and alphanumeric mission data. Two
MFDs are located at the navigator’s station and two
at the radar navigator’s station.
OAS Power Control Panel
MFD DISPLAY FIGURES
The OAS Power Control Panel (PCP) (figure 1-7) located on the navigators’ front panel provides power
control for the OAS and the WIU (Weapon Interface
Unit). All legends are backlighted green when
power is on. The MIU switches which command
power to the WIU are alternate action pushbuttons
In the MFD display figures in this T.O., the items
modifiable by the operator or the SMO are represented in the display explanations as lower case
(non-capital) letters. The labels which are not modifiable are presented in all capital letters.
1-12
Change 2
T.O. 1B-52H-34-2-8
Missile Data Flow (Typical)
Figure 1-4
Change 2
1-13
T.O. 1B-52H-34-2-8
Weapon Control Panel
NAVIGATOR’S FRONT PANEL
Figure 1-5 (Sheet 1 of 2)
1-14
T.O. 1B-52H-34-2-8
NO.
CONTROL/INDICATOR
FUNCTION
1
WPN JETTISON SEL (Weapon Jettison Select) Switch
Spring-loaded to NORM (off) position. Used with unlock consent from pilot’s
weapon consent panel and WCP NUCLEAR LOCK-UNLOCK switch.
SEL – Jettisons missiles selected on location and station switches.
2
STATION Switches
Used with location switches to select individual pylon weapon stations 1 thru
8 (4 and 5 not used) or all (ALL) stations at the selected location for missile operational functions
3
WPN PWR (Weapon Power)
Switch
Three position, spring-loaded to neutral (N).
ON – Commands power be applied to the missiles selected by the location and
station switches on the WCP.
OFF – Commands power be removed from the missiles selected by the WCP.
4
LAMP TEST Switch
When pressed all panel lights will come on.
5
MSTR (Master FAULT
Light
Indicates a fault has occurred. More information is available on the MFD.
Pressing acknowledges receipt of message, turns light off, and erases message.
6
MISSILE MAN LNCH (Manual
Launch) Switch
In manual launch mode, pressing the switch commands launch of the selected
JASSM at the current JASSM launch point or the currently selected direct target. If no launch point/direct target is selected or the selected missile is not
ready for launch the command is ignored. The light in the switch comes on
when the command is accepted and goes out on completion of the launch sequence.
NOTE
For JASSM, deselecting the MISSILE MAN LAUNCH during
manual launch sequence will result in an abort.
7
MISSILE LNCH MODE
(AUTO/MAN) Switch
The switch selects Automatic (AUTO) or Manual (MAN) missile launch mode.
The system is initialized in MAN.
NOTE
Switching the MISSILE LAUNCH MODE switch from AUTO to
MAN during the launch countdown may result in an abort.
8
LOCATION Switches
Used with station select switches to select missiles for missile operation
functions.
LP (Left Pylon) – Selects left pylon missiles.
RP (Right Pylon) – Selects right pylon missiles.
BAY (Bay) – Non functional with JASSM.
9
NUCLEAR LOCK-UNLOCK
Switch
Guarded two position switch used with pilot’s consent to apply power to weapon interface unit to allow operation of the ejectors for release or jettison.
NOTE
In SIM Mode a momentary UNLOCK CONSENT message will be
displayed each time the NUCLEAR LOCK-UNLOCK switch is
positioned. The message will clear automatically.
Figure 1-5 (Sheet 2 of 2)
Change 2
1-15
T.O. 1B-52H-34-2-8
Pilot’s Munition Consent Panel
PILOT’S SIDE PANEL
Figure 1-6
1-16
T.O. 1B-52H-34-2-8
OAS Power Control Panel
NAVIGATOR’S FRONT PANEL
NO.
CONTROL/INDICATOR
1
LAMP TEST Switch
2
Weapon
Interface
Switches (3)
3
MASTER POWER Switch
FUNCTION
Tests all lights on the Power Control Panel.
Unit
MIU/LP – Commands power to the left pylon weapon interface unit.
MIU/BAY – Not used for JASSM
MIU/RP – Commands power to the right pylon weapon interface unit.
ON (light on) – Sends master power to:
• OAS
• WEAPON CONTROL PANEL
• ARMAMENT INTERFACE UNIT (AIU)
• Enable MIU POWER switches
For all other functions, refer to the applicable flight manual.
Figure 1-7
1-17
T.O. 1B-52H-34-2-8
Integrated Keyboard (IKB)
MISSILE RELATED KEYS AND SWITCHES
NO.
CONTROL/INDICATOR
FUNCTION
1
0 – 9 Keys
Enter the respective number in the data/command to be transferred. When
used in conjunction with upper corner key, gives N, S, E, W, +, –, and comma
(,).
2
ENTER Key
Completes the operator sequence. When pressed, data/commands will be
transferred to OAS and displayed on MFD.
3
Message (MSG) Switch
Acknowledges an existing message after being displayed on all four MFDs.
4
A – F Keys
Enter respective letter in data/command to be transferred.
5
Return (RTN) Key
Places the MFD cursor to the first operator-changeable position in the row designated.
6
Backspace (←) and Advance
(→) Keys
Keys move the cursor on the MFD to the left and right respectively.
7
Upper Corner (UC) Key
When pressed, the number keys enter the symbols in the upper left corner of
the key.
8
Display Select Keys (4)
PRGM displays current event program or selected event program.
CF displays OAS mode supervision menu or initiates entry into specific OAS
mode.
MDFY initiates operator changes to MFD displayed data.
FRMT displays video and/or data.
9
L MFD and R MFD Selection
Switches
Select either MFD for display of data inputs from the keyboard.
Figure 1-8
1-18
T.O. 1B-52H-34-2-8
JASSM IKB Commands
COMMAND
DESCRIPTION
ADVISORY ACKNOWLEDGMENT
MSG
Control Function Menu Request
COMMAND MENU DISPLAY REQUESTS
CF-
Control Function Menu Request
CF-5
Weapon Supervision Menu Request
CF-5A [AMI]
JASSM Supervision Menu (CF-57) Request for Left Pylon (All JASSM SMO Controlled Locations)
CF-5C [AMI]
JASSM Supervision Menu (CF-57) Request for Right Pylon (All JASSM SMO Controlled Locations)
CF-57
JASSM Supervision Menu Request
CF-58
JASSM Targeting Menu Request
CF-6
FCP Supervision Menu Request
CF-62
SMO Load Menu Request
CF-8
Mission Supervision Menu Request
CF-82 [AMI]
Weapons Load Menu Request
CF-82A [AMI]
Weapon Group Load Menu (Left Pylon)
CF-82C [AMI]
Weapon Group Load Menu (Right Pylon)
CF-E
Weapon Control Panel Backup Display Command
FRMT-
Format Menu Request
SYSTEM STATUS DISPLAY REQUESTS
CF-DB [AMI]
Display Previous Weapon Assignment Data (from FRMT-7, 7A, or 7C)
CF-DF [AMI]
Display Next Weapon Assignment Data (from FRMT-7, 7A, or 7C)
FRMT-6
PME Status Display Request
FRMT-7
JASSM Status and Inventory Display Request
FRMT-7A [AMI]
JASSM Status and Inventory Display Request (Left Pylon - All JASSM SMO Controlled Locations)
FRMT-7C [AMI]
JASSM Status and Inventory Display Request (Right Pylon - All JASSM SMO Controlled Locations)
FRMT-7xy
JASSM Status and Inventory with Selected Station xy Display Request
FRMT-77 [AMI]
Stores Summary Display Request
PRGM-
Program Display Request
PRGM-nn
Destination View Command for Destination nn
PRGM-Dn
Direct Target Selection Command for Direct Target n
DESTINATION AND TARGETING DISPLAY REQUESTS
CF-586
Missile/Target Assignment Request (Manual Targeting)
CF-588,n
Direct Target Definition Display Request For Direct Target n
CF-Dn
Copy Current Direct Target to Direct Target n
CF-DB
Display Previous Weapon Summary (FRMT-12)
CF-DF
Display Next Weapon Summary (FRMT-12)
FRMT-12
Display Weapon Summary
FRMT-10,nn
Destination Table Display Request
FRMT-12,nn
Missile Summary Display Request for Launch Point nn
FRMT-12,Dn
Direct Target Missile Summary Display Request for Direct Target n
Figure 1-9 (Sheet 1 of 2)
Change 2
1-19
T.O. 1B-52H-34-2-8
JASSM IKB Commands (Cont)
COMMAND
DESCRIPTION
SENSOR DATA REQUESTS
FRMT-1
Radar Display Data Request
FRMT-2
Radar with PMD Display Data Request
FRMT-4
EVS Display Data Request
FRMT-5
EVS Full Display Data Request
SYSTEM CONTROL COMMANDS
CF-50
STRIKE Mode Command
CF-51 [AMI]
PART SIM Mode Command
CF-52
FULL SIM Mode Command
CF-57A
Telemetry ON Command for Selected Missile(s) (Flight Test Only)
CF-57B
Telemetry OFF Command for Selected Missile(s) (Flight Test Only)
CF-57C,xy
Flight Termination System (FTS) Enable/Disable Command for Missile xy (Flight Test Only)
CF-57D
FTS Power Source Command (Flight Test Only)
CF-57E,xy
TXA (Transfer Alignment) Halt Command for Missile xy (Flight Test Only)
CF-57F,xy
TXA (Transfer Alignment) Re-Initialize Command for Missile xy (Flight Test Only)
CF-571
Go/No-Go Test Command (Maintenance Only)
CF-572
SIT Command (Maintenance Only)
CF-575
Classified Data Erase Command For Selected Missiles
CF-580 [AMI]
Auto Target Enable/Disable
CF-589
Retarget-all Command
CF-62,n Less [AMI]
SMO Load Menu
CF-62x [AMI]
Primary SMO Selection by Location x
CF-65
SMO Mission Event Recording Command
CF-66
Clear PME Faults Command
CF-67
OAS Shutdown Command
CF-68
ECU Fault Override Command
CF-81,n
Read B-52 Sortie Mission Data Command
CF-82,nn [AMI]
CF-82,n [AMI]
Select Weapon Group
TARGETING PROCESS COMPLETION COMMANDS
PRGM-Dn
Target Selection Command for Direct Target n
CLR-D
Selected Weapon Event Deselection Command
TARGETING PROCESS COMPLETION COMMANDS
CF-DD
Download Data to Selected Missiles for Targeting
CF-DE
Exit Without Downloading Data
MODIFY DATA COMMANDS
MDFY-n
Modify Line Identified by Number n
Figure 1-9 (Sheet 2 of 2)
1-20
Change 2
T.O. 1B-52H-34-2-8
Multifunction Displays
TYPICAL MFD RADAR NAVIGATOR’S AND NAVIGATOR’S FRONT PANELS
PRIME MISSION DATA (PMD)
CRITICAL DESIGNATION/RELEASE EVENT DATA
OR
OAS SUPERVISORY MENUS, MISSION DATA TABLES,
AND WEAPON/PME STATUS
OAS ADVISORY DATA AREA
KEYBOARD DATA INPUTS
MASTER FAULT MESSAGES
NUCLEAR CAUTION MESSAGE
PME FAULT MESSAGES
QUESTIONS REQUIRING YES – NO RESPONSE
OAS ADVISORY MESSAGES AND SELECTED WEAPON STATION STATUS
GENERAL DISPLAY ARRANGEMENT
Figure 1-10
1-21
T.O. 1B-52H-34-2-8
WEAPON JETTISON
between weapons and between weapons
and aircraft cannot be ensured.
Weapon jettison for JASSM SMO controlled weapons is accomplished by one of three methods: the
navigator’s weapon jettison select switch on the
WCP, the Alternate Jettison Control Panel (AJCP)
at the navigator’s station or the pilots’ Bomb Bay
and Missile Jettison Control switch. All methods require unlock consent.
• The JASSM SMO has no interlocks prevent-
Less [AMI] The OAS must be operational with the
JASSM SMO loaded and WIU power must be on for
jettison of JASSMs when using the WCP or the pilots’
switch.
diode in the jettison system fails, the Radar
Navigator ’s Bomb Bay Jettison Control
switch will function in the same manner as
the pilot’s Bomb Bay & Missile jettison
switch. Normally, the radar navigator ’s
Bomb Bay Jettison Control switch is excluded
from operation with the SMO. A blocking
diode prevents signal travel between the radar navigator’s switch and the OAS. If the
diode fails, the signal will be sent through the
OAS to both internal and external weapons.
The only method to determine if this diode
has failed is to perform a jettison test using
the radar navigators switch and monitoring
the weapon stations for a jettison signal.
[AMI] The OAS must be operational with the
JASSM SMO loaded and selected as the Primary
SMO and WIU power must be on for jettison of
JASSMs when using the WCP or the pilots’ switch.
Only weapons for the SMO loaded will be jettisoned. (i.e. if JASSMs are being carried externally,
and CALCMs on the CSRL internal, only the weapons of the loaded SMO will be jettisoned). This does
not apply to jettison mixed loads with 1760 and
GWD SMO weapons, as GWD SMO weapon releases/jettisons are not WIU/SMO controlled.
Less [AMI] With OAS or WIU off, or a SMO other
than the JASSM SMO loaded, jettison of JASSMs
can only be accomplished using the AJCP.
[AMI] With OAS or WIU off, or a SMO other than
the JASSM SMO loaded as the Primary SMO, jettison of JASSMs can only be accomplished using the
AJCP.
The pilots’ Bomb Bay and Missile jettison switch
has the same effect as if all locations and all stations were selected on the WCP and then the WPN
JETTISON switch was selected.
ing jettison on the ground. With unlock consent, and power applied to the OAS and the
WIU, actuation of jettison switches while on
the ground will result in weapon jettison.
• For OAS controlled weapons, if the blocking
• If an OAS reconfiguration occurs during
JASSM jettison, the jettison command will be
retained and the jettison will continue after
reconfiguration.
• If there is a retained/HUNG center station
store, launching/jettisoning an adjacent
shoulder station may result in a Store-toStore contact. When a center station store
is retained/HUNG, operators will retain the
adjacent shoulder station stores.
OAS Commanded Jettison
Circuit breakers applicable to weapons jettison are
contained in figures 1-11 and 1-12.
The preferred method of jettison for SMO controlled
weapons uses the OAS and the JASSM SMO through
the LOCATION/STATION switches and the WEAPON JETTISON SEL switch on the Weapon Control
Panel (figure 1-5) to selectively jettison weapons.
CF-E Weapon Control Panel Backup display (Figure
1-26) can also be used for selective jettison.
• The pilots’ Bomb Bay & Missile Jettison
AJCP Commanded Jettison
Control switch jettisons all GWD and active/primary SMO controlled weapons
loaded on the aircraft and will only be used
as a backup to jettison by the Radar Navigator. If jettison is commanded using the pilots’ Bomb Bay & Missile Jettison Control
switch, all GWD weapons and, with OAS
operating and MIUs/WIUs powered, all active/primary SMO controlled weapons will
be jettisoned. Proper separation clearance
1-22
Change 3
The second method of jettison for JASSMs uses the
Alternate Jettison Control Panel (AJCP) located at
the navigator’s station, figure 1-13. The AJCP allows
selective jettison of JASSMs without the OAS operational, when a SMO other than the JASSM SMO is
loaded ([AMI] as the Primary SMO), or when WCP
jettison is not possible. The AJCP will selectively jettison the missiles, one at a time.
T.O. 1B-52H-34-2-8
NOTE
The OAS SMOs cannot detect AJCP jettison
commands and interprets the commands as
uncommanded EED power available faults.
Therefore if the AJCP is used for jettison
with the SMO loaded, the SMO will interpret the command as a fault and remove
WIU power at the affected station.
The AJCP has no interlocks preventing jettison on the ground. With unlock consent
and power applied to the aircraft, actuation
of AJCP switches while on the ground will
result in weapon jettison.
Circuit Breaker Panels
RIGHT FORWARD BNS CIRCUIT BREAKER PANEL
Figure 1-11
Circuit Protection
CIRCUIT
WEAPONS
JETTISON
BREAKER
NOMENCLATURE
AMPERE
RATING
JETTISON POWER
JETTISON CONTROL
LOCATION
TYPE
FUNCTION
15
Right fwd BNS
overhead CB
panel
DC
Pilot’s jettison
switch power
10
Right fwd BNS
overhead CB
panel
DC
Pilot’s jettison
switch power
Figure 1-12
1-23
T.O. 1B-52H-34-2-8
Alternate Jettison Control Panel
The AJCP has no interlocks preventing jettison on the ground. With unlock consent, actuation of AJCP switches while on the ground with power applied to the
aircraft will result in weapon jettison.
NO.
1
CONTROL/INDICATOR
POWER and STORES
Jettison Light
FUNCTION
Two part light:
PWR – Comes on when the pylon power (No. 2) switch is placed to either LEFT
or RIGHT indicating power is applied to the AJCP.
JET – Comes on when any jettison switch (No. 3) is placed up to command
jettison.
2
PYLON POWER Switch
Applies Jettison power to the selected pylon.
3
JETTISON Switch (8)
Switches 1 thru 8 command jettison at the respective HSAB ejector location.
Figure 1-13
1-24
T.O. 1B-52H-34-2-8
PILOTS’ BOMB BAY & MISSILE JETTISON CONTROL
SWITCH COMMANDED JETTISON
Jettison using the pilots’ Bomb Bay and Missile jettison switch (figure 1-14) should be used only if jettison by the other methods is not possible. Pressing
the pilots’ Bomb Bay & Missile jettison control
switch jettisons all weapons on the aircraft. For
OAS SMO controlled weapons the OAS must be up
and running ([AMI] with the JASSM SMO loaded
as the primary SMO) with the WIU powered for jettison of JASSM with this switch. The JETTISON
POWER and JETTISON CONTROL circuit breakers on the Right Forward BNS circuit breaker panel
must be in for the pilots’ jettison switch to function.
• The pilots’ Bomb Bay & Missile Jettison
Control switch jettisons all GWD and active/primary SMO controlled weapons
loaded on the aircraft and will only be used
as a backup to jettison by the Radar Navi-
gator. If jettison is commanded using the pilots’ Bomb Bay & Missile Jettison Control
switch, all GWD weapons and, with OAS
operating and MIUs/WIUs powered, all active/primary SMO controlled weapons will
be jettisoned. Proper separation clearance
between weapons and between weapons
and aircraft cannot be ensured.
• The JASSM SMO has no interlocks pre-
venting jettison on the ground. With unlock
consent, and power applied to the OAS and
the WIU and ([AMI] with the JASSM SMO
loaded as the primary SMO), actuation of
the pilots’ Bomb Bay & Missile jettison control switch while on the ground will result
in weapon jettison.
• If there is a retained/HUNG center station
store, launching/jettisoning an adjacent
shoulder station my result in a Store-toStore contact. When a center station store
is retained/HUNG, operators will retain the
adjacent shoulder station stores.
Jettison Control Switches
Figure 1-14 (Sheet 1 of 2)
Change 3
1-25
T.O. 1B-52H-34-2-8
Jettison Control Switches (Cont)
NO.
CONTROL/INDICATOR
FUNCTION
RADAR NAVIGATOR’S BOMB BAY JETTISON CONTROL (Cont)
1
BOMB BAY Jettison Control
Switch
The jettison switch is a button type with unmarked jettison and off positions with
the depressed position being jettison. The switch is spring-loaded to OFF position and is recessed in the panel to discourage inadvertent actuation. Momentary actuation of the switch to RELEASE position for non OAS Controlled
weapons will energize the jettison circuits.
Power is supplied by means of aft battery power through circuit breakers
marked JETTISON CONTR and JETTISON PWR on the right forward BNS
circuit breaker panel. When the jettison circuits are energized, the bomb door
open circuits will be energized and if unlock consent is present, all the weapons (internal and external) will be released in a safe configuration. The bomb
doors will be held open while the jettison circuits are energized.
For OAS controlled weapons (nuclear and SMO controlled) the switch will not
function. If the blocking diode in the switch’s jettison circuits has failed, the
switch will send a jettison signal to the OAS. If OAS receives this signal, with
OAS and WIU power on, all weapons at powered locations will be jettisoned.
2
INTERNAL STORES
RELEASE Light
Store jettisoned lights come on while the jettison circuit is energized. Power
source for the lights is the same as for the jettison switches.
PILOTS’ BOMB BAY & MISSILE JETTISON CONTROL
3
BOMB BAY & MISSILE
Jettison Control Switch
The jettison control switch is a button type with unmarked jettison and off positions with the depressed position being jettison. The switch is spring-loaded
to off position and is recessed in the panel to discourage inadvertent actuation.
Momentary depression of the switch for non OAS controlled weapons will jettison weapons at all locations.
For OAS controlled weapons the switch will send a jettison command to OAS.
If OAS is operating, OAS will respond to the jettison command by sending a
jettison all command to those locations with powered WIUs.
Figure 1-14 (Sheet 2 of 2)
1-26
T.O. 1B-52H-34-2-8
PART 3 - JASSM SMO SOFTWARE
The OAS controls the programming and launch or
release of JASSMs using the flight computer program (FCP). The FCP consists of the flight management system (FMS) and stores management overlay (SMO) and [AMI] Common Stores Processing
(CSP). The FMS controls navigation, radar, controls
and displays, and supports the JASSM SMO. The
JASSM SMO contains all weapon control delivery
functions required with JASSMs. [AMI] The CSP
incorporates common stores/weapon capabilities
and provides multi-SMO operation. The SMO menu
can be displayed to allow the operator to select the
appropriate SMO. Up to 10 SMOs can be listed on
control function CF-62, the SMO Load Menu.
Functions performed by the SMO include weapon
control processing, simulation processing, and controls and displays processing. To perform its required functions, the SMO interfaces with existing
aircraft weapon system components, the OAS
sources of navigation, steering, controls and displays processing, mission data, and with the global
positioning system (GPS) hardware.
• [AMI] With JASSM designated as the Primary
SMO (CF-62x), all JASSM weapon functions are
available. The JASSM can be powered, aligned, monitored, targeted, ranged, launched and jettisoned.
• [AMI] When the CALCM and the JASSM SMOs
are loaded at the same time, CALCM will be automatically selected as the primary SMO by the OAS.
• [AMI] If the JASSM SMO is not the Primary
SMO, only WIU power, heating and monitoring
functions are available for the missiles.
• [AMI] If the missiles are targeted with the
JASSM SMO primary, the missiles will retain the
targeting information while the JASSM SMO is secondary.
• [AMI] If the JASSM SMO is primary, setting
the JASSM SMO to secondary will be inhibited if
weapon power is on or if any process is active that
cannot be accomplished in the secondary SMO
mode.
SMO MFD DISPLAYS
Displays can be requested on each Multifunction
Display (MFD) which contain SMO data and are
used to interface with the operator for JASSM operations. Several of the displays are defined and
updated primarily by the FCP for which the SMO
provides additional data for display. Some of the
displays are completely unique to the SMO operation for which it provides all of the data.
The display commands ending in xy (i.e. CF-57Cxy,
FRMT-7xy, etc.) require an xy entry representing
the location and station of the applicable weapon.
The x represents the location and is entered as A
for the left pylon and C for the right pylon. The y
represents the station and is entered as 1,2,3,6,7, or
8 for the respective JASSM Launch station.
In this manual, discussion of display items/keyboard
entries has been standardized. If numbers or capital
letters are shown on a display, they are as actually
displayed on the MFD. Lower case (small) letters indicate variable entries. An a is an alphabetical entry,
an n is a number, mm:ss are minutes and seconds, dd
are degrees, xy is station/location, etc.
The following displays are affected wholly or in part
by the SMO:
• All Displays
• CF
• CF-5
• CF-5A
• CF-5C
• CF-57
• CF-58
• CF-586
• CF-588,n
• CF-6
• CF-62
• CF-8
• CF-82
• CF-82A
• CF-82C
• CF-E
• CF-DB/DF
• FRMT• FRMT-1
• FRMT-2
• FRMT-4
• FRMT-5
• FRMT-6
• FRMT-7
Release Advisory Display.
Control Function.
Weapon Supervision Menu.
[AMI] Weapon Supervision
Menu (Left Pylon).
[AMI] Weapon Supervision
Menu (Right Pylon).
JASSM Supervision Menu.
JASSM Targeting Menu.
Weapon/Target Assignment
(manual targeting) Display
Direct Target Definition
Display for Target n.
FCP Supervision Menu.
SMO Load Menu.
Mission Supervision Menu.
[AMI] Weapons Load Menu.
[AMI] Weapons Group Load
Menu (Left Pylon).
[AMI] Weapons Group Load
Menu (Right Pylon).
WCP Backup Display.
[AMI] With FRMT-7, 7A, 7C
Displays Previous/Next Weapon
Assignment Data (LP-RP).
Format Menu.
Radar Display Data.
Radar Display Data with PMD.
EVS Display Data.
EVS Full Display Data.
PME Status Display.
JASSM Status and Inventory
Display.
Change 2
1-27
T.O. 1B-52H-34-2-8
• FRMT-7A
• FRMT-7C
• FRMT-7xy
• FRMT-77
• FRMT-10,nn
• FRMT-12,nn
• PRGM
• PRGM-Dn
• PRGM-nn
[AMI] JASSM Status and
Inventory Display - Left Pylon
(All JASSM SMO Controlled
Locations).
[AMI] JASSM Status and
Inventory Display - Right Pylon
(All JASSM SMO Controlled
Locations).
JASSM Status and Inventory
Display with Selected Station
Status.
[AMI] Stores Summary Display.
Destination Table Display.
Weapon Summary Display.
Program Display.
Program Display
Selection for Direct Target n.
Program Display for
Destination nn.
RELEASE ADVISORY DISPLAY
When weapons are declared launched, jettisoned,
aborted, or hung, the Location/Station number and
the appropriate status of each affected weapon will
be shown as a Weapon Release advisory as indicated in figure 1-15. The Weapon Release Advisory
display will be shown on all MFDs that do not currently have data displayed on the bottom of the
MFD. Release advisories can be displayed for up to
4 weapons. When more than 4 advisories are displayed, release advisory window locations will be
updated from left to right with subsequent weapons
release advisories. There is no operator command to
1-28
Change 2
cause the Weapon Release advisory to be displayed.
The data will remain on the MFDs for five seconds
after the release or attempted release of the last
weapon in the sequence.
PRIME MISSION DATA
Less [AMI] The prime mission data (PMD) is displayed anytime a MFD is displaying FRMT-2,
FRMT-4, FRMT-5, FRMT-6, FRMT-8, FRMT-9,
FRMT-10, or a PRGM display. PMD is displayed
any time an MFD is displaying CF, CF-E, CF-1
through CF-8, CF-61, CF-62, CF-67, FRMT,
FRMT-0, or FRMT-7xy display, provided PMD was
previously displayed. PMD is not displayed when a
MFD is displaying CF-57, CF-58, CF-586, CF-588,
FRMT-1 (time to go current destination only),
FRMT-3, or FRMT-12 display. The SMO provides
the destination label for the current destination
when the destination is a JASSM initial point.
[AMI] The prime mission data (PMD) is displayed
anytime a MFD is displaying FRMT-2, FRMT-4,
FRMT-5, FRMT-6, FRMT-8, FRMT-9, FRMT-10, or
a PRGM display. PMD is displayed any time an
MFD is displaying CF, CF-E, CF-1 through CF-8,
CF-57, CF-58, CF-61, CF-67, FRMT or FRMT-0 display, provided PMD was previously displayed. PMD
is not displayed when a MFD is displaying CF-586,
CF-588, CF-62, CF-81, CF-82, FRMT-1 (time to go
current destination only), FRMT-3, or FRMT-12 display. FMS provides the destination label for the
current destination. FRMT-7xy will display only the
first line of the PMD.
T.O. 1B-52H-34-2-8
Release Advisory Display
WINDOW
1
2
DISPLAY
FUNCTION
Location/Station
Identifier
Location and station of each weapon launched.
xy
x = L for left pylon stations and R for right pylon stations.
y = Station number 1, 2, 3, 6, 7 or 8.
The location and station of each weapon launched will be displayed in the next
available window 1 from left to right in preferred launch sequence. If release advisories exist for more than 4 weapons, the first 4 advisories will appear in windows
1 and 2 for 5 seconds, then go to the next four weapons. The remaining advisories
will appear after the windows will be updated from left to right with the release
advisories.
Weapon Release
Status
ABORT
AWAY_
HUNG_
JETT_
A weapon release abort occurred.
The weapon was successfully launched.
The weapon umbilical and/or ejector status indicate that the weapon was not
released.
The weapon was successfully jettisoned.
Figure 1-15
Change 2
1-29
T.O. 1B-52H-34-2-8
CONTROL FUNCTION (CF) DISPLAYS
Less [AMI] SIM Mode Command (CF-52)
Pressing the CF key on the IKB will display the CF
MENU display (figure 1-17). The JASSM related
selections from this menu are; CF-5 which commands display of the JASSM supervision menu,
CF-6 which commands display of the FCP supervision display, CF-8 MSN SUPV which commands
display of the mission supervision menu, and CF-E
which commands display of the weapon control
panel backup display. The JASSM CF commands
are listed in figure 1-16.
Operator entry of CF-52 will command the SMO
from STRIKE mode into SIM mode. If the command
is entered while the SMO is in SIM mode, it will be
ignored. The SMO will reject a CF-52 command and
display the command in reverse video if any of the
following conditions exist:
WEAPON SUPERVISION MENU (CF-5)
The Weapon Supervision Menu, commanded by
CF-5, is shown in figure 1-18, and is available in all
SMOs and provides four common SMO functions.
The common functions are:
• Displays current SMO mode status (i.e.,
STRIKE, FULL SIM and [AMI] PART SIM).
• Identifies operator commands to change
between STRIKE (CF-50), FULL SIM (CF-52)
and [AMI] PART SIM (CF-51) modes.
• Identifies the operator command to request
the JASSM Supervision Menu (CF-57).
• Identifies the operator command to request
the JASSM Targeting Menu (CF-58).
• [AMI] Displays the twenty-four character
SMO identifier next to the assigned location
(LP, Bay and RP).
When the Weapon Supervision Menu is displayed,
the current SMO mode (i.e., STRIKE, FULL SIM
[AMI] or PART SIM), followed by the loaded mission
type (i.e., WAR, TLI, OTL, FERRY or CC) is displayed, similar to the Control Function Menu (CF-).
STRIKE Mode Command (CF-50)
Operator entry of CF-50 will command the SMO
from SIM mode into STRIKE mode. If the command
is entered while the SMO is in STRIKE mode, it
will be ignored. The SMO will reject a CF-50 command and display it in reverse video if simulated
power is applied to either WIU, Go/No-Go test
option is active, or SIT is active.
NOTE
After SIM mode is exited by commanding
STRIKE mode, the B-52 mission data and
the SMO must be reloaded to guarantee
proper operation of the system.
• Power is applied to either WIU.
• B-52 mission data is for an operational (WAR)
mission.
• B-52 mission data is for a timeline integration
(TLI) mission.
• Actual Go/No-Go test mode is active.
• Actual SIT test mode is active.
• 28 VDC T/R power discrepancy fault exists.
• AIU Communications fault (cyclic status message exists).
[AMI] PART SIM Mode Command (CF-51)
Operator entry of CF-51 will command the SMO
from STRIKE mode into PART SIM mode. If the
command is entered while the SMO is in PART SIM
mode, it will be ignored. The CF-51 command will
be rejected and displayed it in reverse video if one
or more of the following conditions are true:
• The system is in FULL SIM mode.
• Mission data is for an operational (strike/war)
•
•
•
•
•
mission or a timeline integration (TLI) mission.
Power is applied to either MIU or to any
weapon.
Actual Go/No-Go test mode is active.
Actual System Integrity Test (SIT) test mode
is active.
28 VDC T/R Power Discrepancy fault exists.
AIU (cyclic status message 5C23) Communication fault exists.
[AMI] FULL SIM Mode Command (CF-52)
Operator entry of CF-52 will command the the weapon system from STRIKE mode into FULL SIM mode.
If the command is entered while the SMO is in FULL
SIM mode, it will be ignored. The CF-52 command
will be rejected and displayed it in reverse video if one
or more of the following conditions are true
• The system is in PART SIM mode.
• Mission data is for an operational (strike/war)
mission or a timeline integration (TLI) mission.
• Power is applied to either MIU or to any
weapon.
• Actual Go/No-Go test mode is active.
• Actual System Integrity Test (SIT) test mode
is active.
• 28 VDC T/R Power Discrepancy fault exists.
• AIU (cyclic status message 5C23) Communication fault exists.
1-30
Change 2
T.O. 1B-52H-34-2-8
JASSM Supervision Menu (CF-57)
The JASSM Supervision Menu, commanded by
CF-57, is shown in figure 1-19.
When the JASSM Supervision Menu is displayed,
the current OAS mode and current mission type
and the IKB commands which can be used to monitor and control the weapons are displayed just as on
the Control Function Menu (CF-) and the Weapon
Supervision Menu (CF-5).
[AMI] Although designated for weapons on the left
and right pylons, respectively, CF-5A and CF-5C
provide the same display as CF-57 for all JASSM
SMO controlled weapons. That is, if carrying
JASSM and CALCM and the CALCM SMO is
prime, CF-57 is selectable, but will not be displayed
on the CF-5 menu. However, CF-5A and CF-5C are
selectable options and will display the JASSM Supervision Menu no matter which SMO is prime. Although the JASSM Supervision Menu is selectable
when the JASSM SMO is not prime, none of options
on the menu are available.
The control function commands that are unique to
the SMO are of the form CF-57x, where x represents any of several alphanumeric characters that
may or may not be followed by a comma and additional alphanumeric characters. The JASSM Supervision Menu displays the control function commands of this form that are accepted by the SMO
and the function commanded by each. [AMI] The
control function commands are not unique to the
JASSM SMO and thus these commands will only be
acted upon if JASSM is the primary SMO.
In addition to identifying the CF-57X commands,
the JASSM Supervision Menu (CF-57) also identifies other SMO commands, not identified on other
JASSM displays.
Telemetry Power ON Command (CF-57A), Telemetry Power OFF Command (CF-57B), FTS Enable/
Disable Command (CF-57C,xy), FTS Power Source
Command (CF-57D), Transfer Alignment (TXA)
Halt Command (CF-57E,xy), and Transfer Alignment (TXA) Re-Init Command (CF-57F,xy) are test
only commands and are discussed in Section IV.
Change 2
1-30A
T.O. 1B-52H-34-2-8
JASSM Control Function (CF) Commands
COMMAND
DESCRIPTION
CF
Control Function Menu Request
CF-5
Weapon Supervision Menu Request
CF-5A [AMI]
JASSM Supervision Menu (CF-57) Request for LP (All JASSM SMO Controlled Locations)
CF-5C [AMI]
JASSM Supervision Menu (CF-57) Request for RP (All JASSM SMO Controlled Locations)
CF-50
STRIKE Mode Command
CF-51 [AMI]
PART SIM Mode Command
CF-52
FULL SIM Mode Command
CF-57
JASSM Supervision Menu Request
CF-57A
Telemetry ON Command for selected weapon(s) (Test Only)
CF-57B
Telemetry OFF Command for selected weapon(s) (Test Only)
CF-57C,xy
Flight Termination System (FTS) Enable/Disable Command for Weapon xy (Test Only)
CF-57D
FTS Power Source Command (Test Only)
CF-57E,xy
TXA (Transfer Alignment) Halt Command for Weapon xy (Test Only)
CF-57F,xy
TXA (Transfer Alignment) Re-Initialize Command for Weapon xy (Test Only)
CF-571
Go/No-Go Test Command (Maintenance Only)
CF-572
SIT Command (Maintenance Only)
CF-575
Classified Data Erase Command For Selected Weapons
CF-58
JASSM Targeting Menu Request
CF-580 [AMI]
Auto Target Enable/Disable
CF-586
Weapon/Target Assignment Request (Manual Targeting)
CF-588,n
Direct Target Definition Display Request For Direct Target n
CF-589
Retarget-all Command
CF-6
FCP Supervision Menu Request
CF-62,n Less [AMI]
SMO Load Menu
CF-62x [AMI]
Primary SMO Selection
CF-65
SMO Mission Event Recording Command
CF-66
Clear PME Faults Command
CF-67
OAS Shutdown Command
CF-68
ECU Fault Override Command
CF-8
Mission Supervision Menu Request
CF-81,n
Read B-52 Sortie Mission Data Command
CF-82 [AMI]
Weapons Load Menu Request
CF-82A [AMI]
Weapons Group Load Menu (LP)
CF-82C [AMI]
Weapons Group Load Menu (RP)
CF-82,n [AMI]
CF-82,nn [AMI]
Select Weapon Group
CF-DB
Display Previous Weapon Summary (FRMT-12, [AMI] FRMT-7, 7A and 7C)
CF-DD
Download Data to Selected Weapons for Targeting
CF-DE
Exit Without Downloading Data
CF-Dn
Copy Current Direct Target to Direct Target n
CF-DF
Display Next Weapon Summary (FRMT-12, [AMI] FRMT-7, 7A and 7C)
CF-E
Weapon Control Panel Backup Display Command
CLR-D
Selected Weapon Event Deselection Command
Figure 1-16
1-30B
Change 2
T.O. 1B-52H-34-2-8
Control Function (CF) Menu
Less [AMI]
[AMI]
Figure 1-17 (Sheet 1 of 2)
Change 2
1-30C
T.O. 1B-52H-34-2-8
Control Function (CF) Menu (Cont)
WINDOW
1
2
DISPLAY
Operational Mode
MODIFIABLE
FUNCTION
NO
FULL SIM (Bright
Video)
Operational mode is full simulation of the WIU and weapons.
[AMI] PART SIM
(Bright Video)
Operational mode is partial simulation of the WIU and weapons.
STRIKE (Bright Video)
Operational mode is STRIKE.
Loaded B-52 Mission
Type
NO
WAR
JASSM War mission is loaded.
OTL
JASSM Operational Test Launch (OTL) mission is loaded.
CC
JASSM Captive Carry (CC) mission is loaded.
FERRY
JASSM Ferry mission is loaded.
TLI
JASSM Timeline Integration (TLI) mission is loaded.
(blank)
No mission is loaded, or the current mission is not recognized by the
JASSM SMO.
Figure 1-17 (Sheet 2 of 2)
1-30D
Change 2
T.O. 1B-52H-34-2-8
Weapon Supervision Menu (CF-5)
Less [AMI]
[AMI]
PMD
5 WPN SUP V
5 0 S TR I K E
5 1 P AR T S I M
5 2 F UL L S I M
1
2
57
J ASSM SUP V
58
59
5A
5B
5C
J ASSM T ARGE T I NG
B AY DOORS
3
L P WPN SUP V
B AY WPN SUP V
RP WPN SUP V
4
4
4
− − − −CF - 5
B40808
Figure 1-18 (Sheet 1 of 2)
Change 2
1-30E
T.O. 1B-52H-34-2-8
Weapon Supervision Menu (CF-5) (Cont)
WINDOW
1
2
3
4
DISPLAY
Operational Mode
MODIFIABLE
FUNCTION
NO
PART SIM [AMI]
(Bright Video)
Operational mode is simulation of the WIU and weapons.
FULL SIM (Bright
Video)
Operational mode is simulation of the WIU and weapons.
STRIKE (Bright Video)
Operational mode is STRIKE.
Loaded B-52 Mission
Type
NO
WAR
JASSM War mission is loaded.
OTL
JASSM Operational Test Launch (OTL) mission is loaded.
CC
JASSM Captive Carry (CC) mission is loaded.
FERRY
JASSM Ferry mission is loaded.
TLI
JASSM Timeline Integration (TLI) mission is loaded.
(blank)
No mission is loaded, or the current mission is not recognized by the
JASSM SMO.
Bomb Bay Door Status
NO
OPEN
The bomb bay doors are open.
CLSD
The bomb bay doors are closed.
[AMI] SMO ID
NO
28 Character ID of SMO assigned to specified location (LP, Bay, RP)
Figure 1-18 (Sheet 2 of 2)
1-30F
Change 2
T.O. 1B-52H-34-2-8
Classified Data Erase Command (CF-575)
JASSM Targeting Menu (CF-58)
Operator entry of CF-575 commands the SMO to
perform a classified data erase for the selected missiles. When a classified data erase is performed, the
following data is erased from missile memory:
The JASSM Targeting menu commanded by CF-58 is
shown in figure 1-20. The JASSM Targeting menu
displays targeting options that are available. Options available are Missile/Target Assignment
(manual targeting), Direct Target definition, and Retarget-all.
• Target Data Set.
• GPS Crypto Keys.
• Less [AMI] Missile Assignments.
Prior to initiating classified data erase, the SMO
seeks confirmation by displaying the confirmation
prompt CLSF DATA ERASE? (YES/NO). A YES response will result in classified data erase being initiated, while a NO response will terminate the request. After Less [AMI] 60 seconds, [AMI] 120 seconds, the default response of NO will be assumed.
After the classified data erase is performed, the
missile is powered off, unassigned and untargeted.
Reloading B-52 mission data, performing a Manual
Targeting operation, or commanding Retarget All
can restore missile assignments. However, power
must be applied to the missiles for targeting to be
initiated.
NOTE
• A classified data erase initiated by the SMO
due to a permanent fatal fault (rather than
the operator) results in missile assignments
being maintained. However, the missile will
be untargeted.
• Do not initiate classified data erase until IN
status is achieved.
• Do not initiate classified data erase while a
targeting operation is in progress (prior to
CF-DD).
The SMO will reject a CF-575 command and display the advisory LOC/STA?? ([AMI] JASSM LOC/
STA??) if no Location(s)/Station(s) have been selected on the WCP or PCP/WCP backup. The
CF-575 command will be displayed in reverse video
when it is rejected. The SMO will also reject a
CF-575 command, if another confirmation prompt
is displayed.
If a CF-575 command is accepted, but the selected
weapon(s) cannot be accessed (weapon not present,
weapon powered off, etc.), the advisory LOC/STA??
([AMI] JASSM LOC/STA??) will be displayed. A description of each failure and the corresponding corrective action is listed in figure 7-20.
[AMI] JASSM Auto Targeting Mode (CF-580)
Operator entry of CF-580 toggles between commanding the Auto Targeting mode ON and OFF.
The current status of the Auto Target mode is displayed on the JASSM Targeting Menu (CF-58). The
default state for Auto Targeting is ON.
Missile/Target Assignment (Manual Targeting) Display
(CF-586)
The Missile/Target Assignment Display commanded by CF-586 is shown in figure 1-21. The Missile/
Target Assignment (Manual Targeting) display allows the operator to download pre-planned targeting data to selected missile(s). The operator will select a missile launch point along with a corresponding mission group. If the mission group field is left
blank, mission group A will be assumed. After a
launch point and mission group have been identified, the operator will then select the desired missile to receive targeting data.
The SMO will reject a CF-586 command and display the command in reverse video if any of the following conditions are true:
• Targeting is active.
• A direct targeting operation is in progress.
• Less [AMI] A missile mission DTUC is not
available.
• B-52 mission data is in the process of being
loaded.
• Less [AMI] CAD processor reconfiguration is
in progress.
Manual targeting (CF-586), requires data item entry/
modification by the operator initiated by MDFY-n,
where n represents the MFD line number associated
with the data to be entered/modified. Several data
items are common to the CF-586 Manual Targeting
and CF-588 Direct Target Definition displays (See
Target Data Items). The operator will use the same
missile selection process for manual targeting and direct target assignment. If the operator enters an invalid command through the IKB, the command will
be displayed in reverse video. If the operator enters
invalid data values, the affected data fields will be
displayed in reverse video.
CDE COMPLT ([AMI] JASSM CDE COMPLT) will
be displayed when classified data erase has been completed for all selected missiles.
Change 2
1-31
T.O. 1B-52H-34-2-8
JASSM Supervision Menu (CF-57)
([AMI] CF-57, CF-5A, CF-5C)
WINDOW
1
2
DISPLAY
Operational Mode
MODIFIABLE
FUNCTION
NO
[AMI] PART SIM
(Bright Video)
Operational mode is partial simulation of the WIU and missiles.
FULL SIM (Bright
Video)
Operational mode is full simulation of the WIU and missiles.
STRIKE (Bright Video)
Operational mode is STRIKE.
Loaded B-52 Mission
Type
NO
WAR
JASSM War mission is loaded.
OTL
JASSM Operational Test Launch (OTL) mission is loaded.
CC
JASSM Captive Carry (CC) mission is loaded.
FERRY
JASSM Ferry mission is loaded.
TLI
JASSM Timeline Integration (TLI) mission is loaded.
(blank)
No mission is loaded, or the current mission is not recognized by the JASSM
SMO.
Figure 1-19 (Sheet 1 of 2)
1-32
Change 2
T.O. 1B-52H-34-2-8
WINDOW
3
4
5
6
DISPLAY
GO/NOGO Test
Status
MODIFIABLE
FUNCTION
NO
OFF (Bright Video)
Go-NoGo quick test mode is not active.
ON (Bright Video)
Go-NoGo quick test mode to determine proper umbilical connection is active.
ON (Reverse Video)
Go-NoGo quick test mode was in progress, but was terminated due to an
invalid condition (aircraft is airborne).
SIT Test Status
NO
OFF (Bright Video)
SIT is not commanded.
ON (Bright Video)
SIT mode is active.
ON (Reverse Video)
SIT mode was in progress, but was terminated due to an invalid condition
(aircraft is airborne).
FTS Power Enable/
Disable Identifier
(Test Only)
NO
xy
Location/station of the missile with FTS enabled/disabled.
x = L for left pylon stations and R for right pylon stations.
y = Station number 1, 2, 3, 6, 7 or 8.
xy (Reverse Video)
FTS enable/disable is commanded and an activate FTS fault exists.
(blank)
No missile has FTS enabled.
FTS Power Transfer
Power Source
(Test Only)
NO
CARR (Bright Video)
Aircraft is commanded as the power source to missile FTS (initial value
when FTS is enabled).
CARR (Reverse Video)
Aircraft is commanded as the power source to missile FTS and an activate
FTS fault exists.
MSL (Bright Video)
Missile battery is source of FTS power.
MSL (Reverse Video)
Missile battery is commanded as the source of FTS power and an activate
FTS fault exists.
(blank)
FTS is not enabled.
Figure 1-19 (Sheet 2 of 2)
Change 2
1-33
T.O. 1B-52H-34-2-8
JASSM Targeting Menu (CF-58)
Less [AMI]
Figure 1-20 (Sheet 1 of 2)
1-34
Change 2
T.O. 1B-52H-34-2-8
[AMI]
PMD
58
J ASSM T ARGE T I NG
586
WPN / TGT ASSGN
588 , N
D I R TGT
N= 1 − 6
589
RE TGT A L L
580
AUTO TGT
− − − −CF - 5 8
1
B40811
WINDOW
DISPLAY
MODIFIABLE
1
[AMI] Auto Targeting
Status
NO
FUNCTION
Auto targeting status.
ON (Bright Video)
Auto targeting is enabled.
OFF (Bright Video)
Auto targeting is disabled.
Figure 1-20 (Sheet 2 of 2)
Change 2
1-35
T.O. 1B-52H-34-2-8
Missile/Target Assignment Display (CF-586)
Less [AMI]
Figure 1-21 (Sheet 1 of 3)
1-36
Change 3
T.O. 1B-52H-34-2-8
[AMI]
WINDOW
1
2
DISPLAY
Targeting Data
Loading Status
MODIFIABLE
NO
COMPLT
Data has been successfully downloaded to the missile.
COMPLT
(Reverse Video)
Failure to download data.
LOADING
(Bright-Blinking Video)
Waiting for data to be downloaded to the missile.
(Blank)
Targeting operation is not active or transfer of data to the missile(s) has
not been initiated via a CF-DD command.
JASSM Launch Point
Number
nn
YES
JASSM launch point number where nn = _1 to 99 and is a valid target.
(blank)
3
3A
FUNCTION
Prior to operator entry or targeting operation is not active.
Mission Group
Identifier
a
YES
[AMI] JASSM Weapon
Group
NO
Mission group identifier where a = A to F.
28 Character Label
Selected Weapon Group for specified location.
(Blank)
No Weapon Group selected for specified location.
Figure 1-21 (Sheet 2 of 3)
Change 2
1-37
T.O. 1B-52H-34-2-8
Missile/Target Assignment Display (CF-586) (Cont)
WINDOW
4
5
DISPLAY
Location/Station
Selection Status
E
MODIFIABLE
FUNCTION
YES
The corresponding location or station is currently selected.
0
The corresponding location or station is not selected.
(blank)
The corresponding missile is not present or is unavailable for assignment due to a permanent fatal fault.
Location/Station
Identifier
xy
NO
Location/station of each missile present on the aircraft and available for
selection that is not currently assigned and targeted to any target.
xy (Bright
Underlined Video)
Location/station of each missile present on the aircraft and available for
selection that is currently assigned and targeted to this target or to
another target.
xy (Normal
Blinking Video)
Location/station of each missile that does not have power applied and
is available for selection.
xy (Reverse Video)
Location/station of each missile that was not successfully targeted after
a CF-DD command.
(blank)
The corresponding missile is not present or is unavailable for selection
due to a permanent fatal fault.
x = L for left pylon stations and R for right pylon stations.
y = Station number 1, 2, 3, 6, 7 or 8.
Each location and station that is displayed will be displayed in a dedicated screen location for that missile. The positions are assigned from
left to right across the screen in the preferred launch sequence.
6
7
Missiles Selected
NO
__n
Remaining missiles to be selected. n = 0 or 1.
–nn (Reverse Video)
More missiles are selected than are required for the mission.
nn = 1 to 11.
(blank)
When any of the following conditions is true:
•Targeting operation is not active.
•When manual targeting is active, prior to selection of JASSM launch
point destination and mission group identifier.
Missiles Required
NO
_n
Quantity of required missiles. _n = 1.
(blank)
When manual targeting is active, prior to selection of JASSM launch
point destination and mission group identifier or targeting operation is
not active.
Figure 1-21 (Sheet 3 of 3)
1-38
Change 2
T.O. 1B-52H-34-2-8
Direct Target Definition Display (CF-588,n)
Target Data Items
The Direct Target Definition display, commanded
by CF-588,n is shown in figure 1-22. The Direct
Target Definition display allows the operator to define targets that are not contained Less [AMI] on
the missile mission DTUC, [AMI] in the weapon
group on the DTC.
Manual Targeting (CF-586) and Direct Targeting
(CF-588) require data item entry/modification by
the operator. The following are the Target Data
items.
Operator entry of CF-588,n, where n is an operatordefined direct target, commands the Direct Target
Definition display for that direct target. The SMO
will reject a CF-588,n command and display the
command in reverse video if any of the following
conditions is true:
In order to manually target a missile, the operator
must select the launch point number associated
with the target. The launch point number is entered on the Manual Targeting display (CF-586)
(figure 1-21). The input is numeric and ranges from
01 to 99. Only the JASSM launch points defined by
the loaded B-52 mission are valid.
• n is not a valid direct target identifier.
• [AMI] Targeting is active.
• Any of the following targeting operations are ac-
•
tive:
a. Manual targeting.
b. Retarget-all.
c. Automatic targeting.
d. Direct targeting operation is in progress for
another direct target other than the one being
requested.
B-52 mission data is in the process of being
loaded.
The SMO will accept operator entry of CF-588 (excluding ,n) to command the Direct Target Definition
display to be displayed only when the direct target
operation is in progress. Otherwise, the SMO will
reject the CF-588 command and display the command in reverse video.
Direct target definition (CF-588) requires data item
entry/modification by the operator initiated by
MDFY-n, where n represents the MFD line number
associated with the data to be entered/modified.
Several data items are common to the CF-586
Manual Targeting and CF-588 Direct Target Definition displays. The operator will use the same missile selection process for manual targeting and direct target assignment. If the operator enters an invalid command through the IKB, the command will
be displayed in reverse video. If the operator enters
invalid data values, the affected data fields will be
displayed in reverse video.
LAUNCH POINT NUMBER
MISSION GROUP IDENTIFIER
Along with the selected launch point, the mission
group identifier associated with that launch point is
entered on the Manual Targeting display (CF-586)
(figure 1-21). Valid IKB input entries for window 3
are A, B, C, D, E, F, or it may be left blank. If it is
left blank, the default mission group A will be assumed. The range of valid alpha characters (A-F) is
dependent on the quantity of mission groups associated with the launch point and missile type currently loaded.
TARGET LOCATION
The target location is the geographical position and
elevation which a missile is to strike. The target
location data fields appear on the Direct Target
Definition screen (CF-588) (figure 1-22). The position entry key fields are:
• Target point reference latitude in degrees,
minutes, and ten-thousandths of a minute.
• Target point reference longitude in degrees,
minutes, and ten-thousandths of a minute.
• Target point reference elevation in feet (MSL).
• Target point reference elevation ([AMI] MSL;
Less [AMI] MSL or HAE) in feet.
• Less [AMI] Target point elevation reference
(HAE or MSL).
Change 3
1-39
T.O. 1B-52H-34-2-8
BEARING TO TARGET
The bearing to target specifies the weapon’s terminal ground track to the target. The bearing to target is entered on the Direct Target screen (CF-588)
(figure 1-22). The valid input values are from 0 to
360 degrees (0 is North), and 999, which indicates
the missile will determine bearing to target as an
angle from the aircraft to the target at point of release. The default value for this field is 999.
TARGET IMPACT ANGLE
The target impact angle specifies the angle in degrees, relative to local level plane at the target. The
impact angle is entered on the Direct Target Definition display, (CF-588) (figure 1-22). The default impact angle is 60 degrees. Valid input values are
from 0 (level) to 90 (vertical) degrees, however, the
missile will only use an impact angle ranging from
20 to 70 degrees.
NOTE
If less than 20 degrees is entered on
CF-588, the missile will use a built-in minimum impact angle value of 20 degrees. If
more than 70 degrees is entered on CF-588,
the missile will use a built-in maximum value of 70 degrees. FRMT-12 displays the impact angle actually being used by the missile. While in SIM mode, the FRMT-12 impact angle displayed is the same as the
CF-588 value input.
CRUISE ALTITUDE
The cruise altitude indicator on the JASSM Direct
Targeting display (CF-588) (figure 1-22) is used to
specify a cruise altitude (MSL) for the JASSM. Valid entries for this field range from 0 to 45000 feet
and 99999, the default value, displayed prior to operator entry. The default cruise altitude is 15,000
feet and, although the field range is 0 to 45,000
feet, the maximum altitude the missile will fly is
approximately 22,000.
FUZE MODE
The fuze mode indicator on the JASSM Direct Targeting display (CF-588) (figure 1-22) is used to specify a fuze mode of either soft impact referenced to
Crush Switch, or hard impact referenced to G-force
Sensor. The operator can select a fuze mode of Soft
1-40
Change 1
by entering 1 or a fuze mode of Hard by entering 2.
The text SOFT or HARD will be displayed, depending on the fuze mode selected. A default value of 1
(Soft) will be displayed prior to operator entry.
FUZE DELAY
Fuze delay milliseconds can be specified by entering a corresponding delay entry on the JASSM Direct Targeting display (CF-588) (figure 1-22). A fuze
delay will delay detonation from the time of impact
by the specified time value. Valid entries for this
field and their corresponding time values are listed
in the following table. A default value of 0 will be
displayed prior to operator entry.
FUZE DELAYS
VALID ENTRIES
MILLISECOND DELAY
0
0
1
10
2
15
3
20
4
30
5
40
6
50
7
120
MISSILE SELECTION INDICATOR
The missile selection indicator appears above the
location/station identifier for each available missile
on the JASSM Direct Targeting display (CF-588)
(figure 1-22). The missile selection identifier is used
when selecting missiles during a manual targeting
or direct target definition operation. Valid entries
are E and 0 (zero), where E indicates that the corresponding missile is selected for targeting and 0 indicates the missile is not selected. The missile selection indicator window will be blank when any of the
following conditions are true:
• The missile is not present.
• The missile is not selected and is unavailable
for selection due to a permanent fatal fault
prior to a CF-DD command.
• The missile is not present or is unavailable
for selection due to a permanent fatal fault
following a CF-DD command and is not a
selected missile.
T.O. 1B-52H-34-2-8
Retarget-all Command (CF-589)
• B-52 mission data is in the process of being
loaded.
Operator entry of CF-589 (figure 1-20) will result in
the targeting of missiles as directed by the B-52
mission that is loaded. Once CF-589 is accepted, all
missiles will become unassigned. The SMO will
then restore the missile assignment data to the
original values of the B-52 mission that is loaded.
This will result in the loss of modified targeting
data previously transferred to the missiles. All missiles not assigned to a JASSM Launch Point by the
B-52 mission that is loaded will remain unassigned
and considered untargeted by the SMO.
NOTE
A retarget-all command requires approximately 2 minutes per JASSM.
The SMO will reject a CF-589 command and display the command in reverse video if any of the following conditions exist:
• Less [AMI] Another confirmation prompt is
active.
• Less [AMI] A missile mission DTUC is not accessible.
Prior to initiating targeting of all missiles, the SMO
will seek confirmation by displaying the confirmation prompt RETARGET ALL? (YES/NO). A YES
response will result in the halting of any targeting
in progress, and proceed with the untargeting of all
missiles, while a NO response will terminate the request. After Less [AMI] 60 seconds, [AMI] 120 seconds, the default response of NO will be assumed.
When a valid CF-589 command is entered any of
the following targeting operations will be terminated, if active:
• Manual targeting.
• Direct targeting.
• Automatic targeting.
Change 2
1-41
T.O. 1B-52H-34-2-8
Direct Target Definition Display (CF-588,n)
Less [AMI]
Figure 1-22 (Sheet 1 of 4)
1-42
Change 3
T.O. 1B-52H-34-2-8
[AMI]
1
D I RECT TGT
2
L AT
3
1 TGT P T
9
5 F UZ E DE L AY
CF - DD =DONE
o
7
3 BRNG TO TGT
11
’
o
8
I MP ACT ANGL E
10
AL T
5
’
6
2 CRU I SE AL T
4 F UZE MODE
L ONG
4
1 − SOF T 2 −HARD
( 0−7 )
CF - DE = E SC
CF - DN =COP Y TO D I R TGT ( D 1 −D 6 )
6
13 13 13 13 13 13
13 13 13 13 13
13
12
(ALL TOP BOXES)
WPNS TO SE L ECT
1 4 OF 1 5
− − − −CF - 5 8 8 n
’
ENTER
E
TO
SE L ECT OR
0
TO DE L E TE
A75613
WINDOW
DISPLAY
MODIFIABLE
1
Direct Target Number
n
NO
Defined Direct Target. n = 1 to 6.
(blank)
2
3
Data Loading Status
FUNCTION
Targeting operation is not active.
NO
COMPLT
Data has been successfully downloaded to the missile.
COMPLT (Reverse
Video)
Failure to download data.
LOADING (BrightBlinking Video)
Assigned mission data is downloading to the missile.
(Blank)
Targeting operation is not active or transfer of data to the missile(s) has
not been initiated via a CF-DD command.
Direct Target Latitude
YES
add°mm.mmmm
Target point latitude in degrees, minutes and ten-thousandths of a minute.
a = N for north and S for south.
Limits are S90.00.0000 through N90.00.0000.
ITEM
VALID INPUT RANGE
Degrees (d)
S90 to N90
Minutes (m)
00.0000 to 59.9999
(blank)
Targeting operation is not active.
Figure 1-22 (Sheet 2 of 4)
Change 2
1-43
T.O. 1B-52H-34-2-8
Direct Target Definition Display (CF-588,n) (Cont)
WINDOW
DISPLAY
MODIFIABLE
4
Direct Target Longitude
YES
5
6
7
8
9
FUNCTION
addd°mm.mmmm
Target point longitude in degrees, minutes and ten-thousandths of a minute.
a = E for east and W for west.
Limits are W 180.00.0000 through E 179.59.9999
VALID INPUT RANGE
ITEM
Degrees (d)
W180 to E179
Minutes (m)
00.0000 to 59.9999
(blank)
Targeting operation is not active.
Direct Target Altitude
YES
fffff
Target point altitude (MSL): –328 to 32810 in feet.
(blank)
Targeting operation is not active.
Direct Target Missile
Cruise Altitude
YES
nnnnn
Cruise altitude for JASSM Direct Targets where nnnnn = 0 to 45000’ MSL
or 99999, the default value, displayed prior to operator entry. Although values up to 45000 are valid, the missile’s actual maximum cruise altitude is
approximately 22,000 feet MSL. The missile uses 15,000 feet MSL as the
default altitude (99999).
(blank)
Targeting operation is not active.
Direct Target Missile
Bearing to Target
YES
bbb
Bearing to target where bbb = 0 to 360 (0 being true north) or 999 where missile will determine BTT from A/C to target at time of launch.
A 999 is displayed prior to operator entry.
(blank)
Targeting operation is not active.
Direct Target Missile
Impact Angle
YES
dd
Target impact angle (0 - level to 90 - vertical) degrees relative to local level
horizontal plane at target impact. 60 is displayed on CF-588 prior to operator
entry.
(blank)
Targeting operation is not active.
Fuze Mode
YES
n
Fuze mode selector where n is used to specify whether to reference the
delay time from a crush switch (soft target) or g-force sensor (hard target).
A 1 is displayed prior to operator entry.
VALID INPUT
1
2
(blank)
10
Fuze Target Type
HARD
TARGET TYPE
Soft Impact
Hard Impact
Direct targeting is not active.
NO
SOFT
Selected Fuze Mode is function on impact referenced to G-Force Sensor
(Hard target).
Selected Fuze Mode is function on impact referenced to Crush Switch
(Soft target). SOFT is displayed prior to operator entry, or if Fuze Mode invalid.
(blank)
Direct targeting is not active.
Figure 1-22 (Sheet 3 of 4)
1-44
Change 2
T.O. 1B-52H-34-2-8
WINDOW
DISPLAY
MODIFIABLE
11
Fuze Function Delay
YES
12
13
FUNCTION
m
Fuze function delay setting where m = 0 to 7. A 0 is displayed prior to operator entry, or if Fuze Mode invalid.
(blank)
Direct targeting is not active.
Location/Station
Selection Status
YES
E
The corresponding location or station is currently selected.
0
The corresponding location or station is not selected.
(blank)
The corresponding missile is not present or is unavailable for assignment
due to a permanent fatal fault.
Location/Station
Identifier
NO
xy
Location/station of each missile present on the aircraft and available for
assignment that is not currently assigned and targeted to any target.
x = L for left pylon stations and R for right pylon stations.
y = Station number 1, 2, 3, 6, 7 or 8.
Each location and station that is displayed will be displayed in a dedicated
screen location for that missile. The positions are assigned from left to right
across the screen in the preferred launch sequence.
14
15
16
xy (Bright
Underlined Video)
Location/station of each missile present on the aircraft and available for
assignment that is currently assigned and targeted to this target or to
another target.
xy (Normal Blinking
Video)
Location/station of each missile that does not have power applied and is
available for assignment.
xy (Reverse Video)
Location/station of each missile that was not successfully targeted after
a CF-DD command.
(blank)
The corresponding missile is not present or is unavailable for selection
due to a permanent fatal fault.
Weapons Remaining
NO
__n
Remaining missiles to be selected. n = 0 or 1.
–nn (Reverse Video)
More missiles are selected than are required for the mission.
nn = 1 to 11.
(blank)
When any of the following conditions is true:
•Targeting operation is not active.
•When manual targeting is active, prior to selection of JASSM launch
point destination and mission group identifier.
Weapons Required
NO
_n
Quantity of required missiles. _n = 1.
(blank)
When manual targeting is active, prior to selection of JASSM launch point
destination and mission group identifier or targeting operation is not active.
Direct Target Elevation
Reference Less [AMI]
YES
Target elevation reference in MSL or HAE.
n
Valid Input
n= 0
n= 1
Elevation Measurement
Mean Sea Level
Height Above Ellipsoid
(blank)
Targeting operation is not active.
Figure 1-22 (Sheet 4 of 4)
Change 3
1-45
T.O. 1B-52H-34-2-8
FCP SUPERVISION MENU (CF-6)
• DTS input/output is complete if a DTC is
installed.
The FCP Supervision Menu, commanded by CF-6,
is shown in figure 1-23. Much of the data displayed
on the FCP Supervision Menu is related to the FMS
and is contained in T.O. 1B-52H-1-12.
With the CF-62 menu displayed the operator will
enter MDFY-11 to copy the following text to the bottom of the MFD for modification:
CF-61 Startup
11 SMO LOAD LP__ BAY__ RP__
CF-61 commands OAS startup. The procedure for
starting up the OAS is the same as for any other
OAS startup and is contained in T.O. 1B-52H-1-12.
The operator will then enter the number of the desired SMO number into the field that corresponds
to the location that the SMO is to control and press
the ENTER key. The location: LP (left pylon), BAY
not used with JASSM), or RP (right pylon) is defined by the cursor which can be moved using the
arrow keys on the IKB. The primary SMO will be
the first SMO loaded until a primary is chosen.
Less [AMI] CF-62 SMO Menu
Operator entry of CF-62 will result in an FMS display of the SMOs available on the OCP DTUC (Figure 1-24). Operator entry of CF-62,n will result in
the FMS loading the SMO indicated by n. A number followed by the text AGM-158 XXXXXXX, identifies the number to be entered to load the SMO.
XXXXXXX is the version information extracted
from the CPIN number. While the SMO is active,
the SMO will delay a CF-62,n command to have the
FMS load a new SMO until the following conditions
have been met:
• All WIU and missile power removal complete.
• Classified data erase (CF-575) is completed.
• DTU input/output is complete if a Fault Data
Recorder Cartridge (FDRC) DTUC is installed.
The SMO is automatically initialized and begins
execution immediately upon loading the SMO into
the ACUs. The procedure for loading the SMO into
the ACUs is equivalent to loading any other CWI
SMO. The JASSM SMO, if it exists on the OCP
DTUC, is identified on the CF-62 menu. The status
message SMO LOAD CMPLT will be displayed on
each MFD following completion of a SMO load. The
procedure for loading the SMO, (the same as for
loading any other SMO) is contained in T.O.
1B-52H-1-12.
To select a SMO as the primary SMO, the operator
will enter CF-62x where x is either A, B or C to select the SMO that controls the left pylon, bay or
right pylon, respectively.
The procedure for loading SMOs is contained in
T.O. 1B-52H-1-12.
CF-64 CLSF Memory Erase
CF-64 commands the erasure of OAS classified memory. The procedure for classified memory erase is
the same as contained in T.O. 1B-52H-1-12.
CF-65 Data Record
CF-65 DATA RECORD indicates a CF-65 command
can be used to record mission event data. When a
SMO is loaded, the missile modes, safe conditions
and pertinent information are recorded along with
FMS mission event data. Operator entry of CF-65
will result in a DTUC/DTC recording of navigation
and mission parameters, missile mode switches,
time to go, and LAR status.
[AMI] CF-62 SMO Menu
CF-66 Erase PME Faults
SMO Load Menu (CF-62) (figure 1-24) allows the
operator to select and load a SMO for left pylon, bay
(not used with JASSM), or right pylon. The primary
SMO is selected from the SMO’s loaded on left pylon, bay, or right pylon.
CF-66 ERASE PME FAULTS indicates a CF-66
command can be used to erase fault indications
that are no longer valid from the PME Status Display (FRMT-6). The SMO will indicate to the FMS
which of its fault indications should be erased. Operator entry of CF-66 will result in erasure of all
past fault indications shown on the PME Status
Display (FRMT-6, figure 1-33). Any WIU communication faults and ECU faults will be cleared. Any
existing faults will cause a fault recording and the
fault indication will continue to be displayed in
reverse video.
While the SMO is active, the SMO will inhibit loading
a new SMO until the following conditions have been
met:
• All WIU and missile power removal complete.
• Classified data erase is completed (software
initiated).
1-46
Change 2
T.O. 1B-52H-34-2-8
CF-67 Shutdown
CF-67 SHUTDOWN indicates a CF-67 command
can be used to shutdown FMS and SMO processing
in the ACUs. Operator entry of CF-67 will result in
the shutdown of the FMS and SMO. The SMO will
delay compliance of the shutdown request until all
outstanding SMO faults have been recorded (Less
[AMI] if an FDRC is installed) and until power
down of all WCE and missiles is complete. The procedure for shuting down the OAS with the SMO
loaded is the same as for any other shutdown and is
contained in T.O. 1B-52H-1-12.
CF-68 ECU Power Override
Less [AMI] CF-68 ECU PWR ORIDE indicates a
CF-68 command can be used to override faults associated with non-availability of Environmental Control Unit (ECU) power. The current state of the
override is displayed (ON or OFF). The SMO will
not reject a CF-68 command.
[AMI] CF-68 ECU PWR ORIDE serves as an ONOFF toggle switch for overriding faults associated
with non-availability of Environmental Control
Unit (ECU) power. The current state of the override
is displayed (ON or OFF) on CF-6. The SMO will
not reject a CF-68 command.
During WIU power on and initialization, the ECU,
which supplies cooling air to the WIUs, is commanded on. If aircraft status indicates ECU power
is not available when commanded, the WIU power
on process is terminated. Additionally, if an Environmental No-Go fault is detected from the ECU
after ECU power has been applied for 2 minutes,
power will be removed from all missiles and both
WIUs unless the operator activates the ECU power
override option.
Less [AMI] Operator entry of CF-68 will command
the OAS to activate the ECU power override option
and ignore any ECU faults. If an Environmental
No-Go fault is detected, an ECU master fault will
be displayed. If the CF-68 command is entered
within 1 minute of the time that the fault is
detected, missile and WIU power will remain on,
otherwise missile and WIU power will be removed.
If WIU and/or missile power is removed because of
a fault, the CF-68 command can be entered prior to
re-applying WIU power and the ECU fault will be
ignored.
[AMI] Operator entry of CF-68 will command the
OAS to activate the ECU power override option and
ignore any ECU faults. If an ECU AC Discrepancy
fault is detected, ECU PWR will be displayed, and
ECU will be displayed on the Weapon Status and
Inventory Display (FRMT-7) and an X will be displayed next to ECU text on the PME Status Display (FRMT-6). If an ECU Environmental No-Go
fault is detected, X will be displayed by CSP next to
ECU text on the PME Status Display (FRMT-6) and
ECU will be displayed on the Weapon Status And
Inventory Display (FRMT-7). If an Environmental
No-Go fault is detected, an ECU master fault will
be displayed. If the CF-68 command is entered
within 1 minute of the time that the fault is
detected, missile and WIU power will remain on,
otherwise missile and WIU power will be removed.
If WIU and/or missile power is removed because of
a fault, the CF-68 command can be entered prior to
re-applying WIU power and the ECU fault will be
ignored.
While in ECU power override, the WIU may be operated using a 30 minute on, 15 minute off, 30 minute on cycle.
With an ECU fault present, damage to
equipment may occur if WIU power remains on continuously as a result of selecting ECU Power Override.
Less [AMI] The ECU power override option will
become inactive only if the SMO is reloaded or if a
logoff is commanded and the system is restarted.
The current status of the ECU power override
option, whether it is active or inactive, is displayed
on the FCP Supervision Menu (CF-6).
[AMI] The ECU power override option will become
inactive only if CF-68 is commanded when the ECU
power override is active. The operator will be given
1 minute from the time the CF-68 command was
entered to reenter the CF-68 command if an ECU
fault is still in effect otherwise weapon and WIU
power will be removed. A system logoff and restart
of the system will also deactivate the ECU override.
The current status of the ECU power override option, whether it is active or inactive, is displayed on
the FCP Supervision Menu (CF–6).
[AMI] CF-69A and CF-69B ACU Shutdown Commands
Primary ACU shutdown is initiated by entering a
CF-69A command and secondary ACU shutdown is
initiated by entering a CF-69B command. When the
primary ACU is shutdown, the secondary ACU will
be reconfigured to become the primary ACU if it is
operational. The ACU shutdown process is described in T.O. 1B-52H-1-12.
Change 3
1-47
T.O. 1B-52H-34-2-8
FCP Supervision Menu (CF-6)
Less [AMI]
PMD
6 F CP SUPV
6 1 S T AR TUP
6 2 SMO MENU
64
65
66
67
68
CL SF MEM ERASE
DA T A RECORD
ERASE PME F AUL T S
SHUTDOWN
2
ECU PWR OR I DE
CF - 6
B40814
[AMI]
PMD
6 F CP SUP V
PR I MARY SMO :
6 1 S T AR TUP
6 2 SMO MENU
1
F CP APP L I CA T I ONS
6 4 C L S F MEM E RASE
6 5 D A T A R E COR D
6 6 E R A S E PME F AUL T S
6 7 S H U T DOWN
6 8 E CU PWR OR I D E
2
6 9 A SHUTDOWN PR I MARY ACU
6 9B SHUTDOWN SECONDA RY A CU
− − − −CF - 6
B40815
Figure 1-23 (Sheet 1 of 2)
1-48
Change 2
T.O. 1B-52H-34-2-8
WINDOW
1
DISPLAY
Primary SMO Title
MODIFIABLE
NO
24 Character Label
2
ECU Power Override
FUNCTION
Primary SMO title.
NO
OFF
ECU power override is not commanded.
ON
ECU power override is commanded.
Figure 1-23 (Sheet 2 of 2)
Change 2
1-49
T.O. 1B-52H-34-2-8
SMO Load Menu (CF-62)
Less [AMI]
[AMI]
Figure 1-24
1-50
Change 2
T.O. 1B-52H-34-2-8
Less [AMI] MISSION SUPERVISION MENU (CF-8)
The Mission Supervision Menu, commanded by
CF-8, is shown in Figure 1-25. Much of the data
displayed on the Mission Supervision Menu is
related to the flight management system and is
contained in T.O. 1B-52H-1-12. The SMO operation
items include the current B-52 mission type (i.e.,
WAR, TLI, OTL, FERRY or CC) and the missile
group ID from the loaded missile DTUC.
Less [AMI] Read B-52 Sortie Mission Data Command
(CF-81,n)
Operator entry of CF-81,n will initiate reading of
B-52 mission n data. The SMO will inhibit loading of
the mission data and the command displayed in reverse video if any of the following conditions exist:
• The B-52 sortie mission file format is not in
conventional (ICSMS) format.
• There is a missile in launch countdown.
• Jettison is in progress for any missile.
• SIT is active.
• Go-NoGo test is active.
• The SMO is operating in SIM mode.
If the mission type of the loaded sortie mission is
not a conventional mission, the nonfatal master
fault MSN DATA?? will be displayed.
The JASSM SMO and a sortie mission must be
loaded in order to successfully apply power to the
WIUs. If a B-52 sortie mission is not loaded WIU
power application will be inhibited and the nonfatal
master fault MSN DATA ?? will be displayed.
If the sortie mission data that is loaded does not
identify a WIU as the Stores Management Interface
Unit (SMIU) at a location where power is applied,
power will be removed from that WIU and all missiles at that location, and the nonfatal master fault
MSN DATA?? will be displayed.
Once the WIU is powered on, weapons may be powered. Weapons are automatically assigned launch
points if the sortie mission has JASSM launch
points. When the weapons are powered on, weapon
types are verified and valid weapons are targeted to
the assigned launch points. When sortie mission
data is changed, valid weapons that are not direct
targeted are automatically targeted.
Weapon store mismatches with sortie mission data
can be discerned by observing the FRMT-7 Missile
type window in combination with a fault such as
XY:STORE ID or XY:WPN PRSNT.
If the missile type identified by mission data is not
the same as that identified by the previously loaded
mission and subsequently power is applied to the
missile(s), a xy:STORE ID transient fatal master
fault will be displayed.
If the missile type identified by mission data is not the
same as that identified by the previously loaded mission and if either WIU is operational, power will be removed from each WIU that is powered and a MSN
DATA?? master fault will be displayed. However, if
the missile type identified by the previous mission
was a JASSM, the power will not be removed.
NOTE
Manual Targeting, Direct Targeting, or Automatic Targeting, if active, will be terminated
when a valid CF-81,n command is entered.
For an in-depth discussion of mission data operations see MISSION DATA in Section VII.
[AMI] MISSION SUPERVISION MENU (CF-8)
The Mission Supervision Menu, commanded by
CF-8, is shown in Figure 1-25. Much of the data
displayed on the Mission Supervision Menu is
related to the flight management system and is
contained in T.O. 1B-52H-1-12. The screen displays
the sortie, mission type (i.e., WAR, TLI, OTL,
FERRY or CC), and weapon group for the left pylon, bay and right pylon loaded in the OAS.
[AMI] B-52 Mission Data Load Command (CF-81)
The B-52 Mission Data Load Display (CF-81), figure 1-25A, displays the primary SMO, loaded sortie, mission and primary SMO weapon group, number of sorties available on the DTC, and a list of
missions available for each sortie. The display also
provides the capability of selecting the sortie and
displaying the command to load a mission.
NOTE
The resident sortie and mission windows at
the top of the CF-81 display will remain blank
or display the previously loaded sortie and
mission identifiers until a mission/new mission is loaded.
The operator can select a sortie from one of three
ways, Either CF-DF to select the next sortie, CFDB to select the previous sortie, or MDFY-1, enter
the desired sortie number and press the ENTER
key. The selected sortie number will be displayed
along with the sortie title and the associated missions will be listed below them.
Change 2
1-51
T.O. 1B-52H-34-2-8
Operator entry of CF-81,n will initiate reading of
B-52 mission n data. The JASSM SMO will inhibit
loading of the mission data and the command displayed in reverse video if any of the following conditions exist:
If the weapon type identified by B-52 sortie mission
data is a JASSM and the weapon identifies itself as
a JASSM and subsequently a B-52 sortie mission is
loaded that does not identify JASSMs the master
fault JASSM MSN DATA?? will be displayed
• The B-52 sortie mission file format is not in
NOTE
•
•
•
•
•
•
conventional format.
There is a missile in launch countdown.
Jettison is in progress for any missile.
SIT is active.
Go-NoGo test is active.
The SMO is operating in SIM mode.
The B-52 sortie mission file currently loaded
is a captive carry mission and one or both
WIUs have power applied.
If the mission type of the loaded sortie mission is
not a conventional mission, the nonfatal master
fault JASSM MSN DATA?? will be displayed.
A sortie mission must be loaded in order to successfully apply power to the WIUs. If a B-52 sortie mission is not loaded WIU power application will be inhibited and the nonfatal master fault JASSM MSN
DATA ?? will be displayed.
If the sortie mission data that is loaded does not
identify a WIU as the Stores Management Interface
Unit (SMIU) at a location where power is applied,
power will be removed from that WIU and all missiles at that location, and the nonfatal master fault
JASSM MSN DATA?? will be displayed.
Once the WIU is powered on, weapons may be powered. Weapons are automatically assigned launch
points if the sortie mission has JASSM launch
points. When the weapons are powered on, weapon
types are verified and valid weapons are targeted to
the assigned launch points. When sortie mission
data is changed, valid weapons that are not direct
targeted are automatically retargeted when auto
targeting is not enabled.
Weapon store mismatches with sortie mission data
can be discerned by observing the FRMT-7 Missile
type window in combination with a fault such as
xy:STORE ID or xy:WPN PRSNT.
If the weapon type identified by mission data is a
JASSM and subsequently power is applied to the
weapon(s), and the weapon indicates it is not a
JASSM the transient fatal master fault XY:STORE
ID will be displayed and power will be removed
from the weapon.
1-52
Change 2
Any of the following targeting operations
will be terminated, if active, when a valid
CF-81,n command is entered.
• Manual Targeting
• Direct Targeting
• Automatic Targeting
For an in-depth discussion of mission data operations see MISSION DATA in Section VII.
[AMI] Weapon Group Load Display (CF-82A, CF-82C)
The JASSM Weapon Group Load Display (CF-82A
and CF-82C), figure 1-25B, shows the sortie, mission
and weapon group (for the pylons) that are loaded
into the OAS. The display also depicts the number
available and a listing of the JASSM weapon groups.
There can be up to 30 JASSM weapon groups on a
DTC. The CF-82A and CF-82C displays can show a
maximum of nine weapon groups at a time. CF-DF
and CF-DB commands are used to page forward or
back to the page containing the desired weapon
group.
The operator can select and load a weapon group
into the OAS with a CF-82,nn or CF-82,n command, where nn or n represents the weapon group
number as shown on the CF-82A or CF-82C display.
NOTE
• Although depicted as LP and RP WPN
GROUPs, CF-82A and CF-82C represent all
the JASSM SMO controlled weapons. A
CF-82,nn or CF-82,n command from either
the CF-82A or CF-82C display will load the
selected (nn or n) weapon group for all the
JASSMs.
• The CF-82,nn and CF-82,n commands will
be ignored, if CF-82A or CF-82C is not displayed on the current MFD.
T.O. 1B-52H-34-2-8
Mission Supervision Menu (CF-8)
Less [AMI]
[AMI]
PMD
8 MSN SUP V
81
B 5 2 DA T A
RE S I D ENT SOR T I E
RE S I D ENT B − 5 2 DATA
8 2 A L P WPN GRP
8 2 B B AY WPN GRP
8 2 C RP WPN GRP
1
3
4
SE L ECT ED WEAPON GROUP
5
5
- - - - CF - 8
B52478
Figure 1-25 (Sheet 1 of 2)
Change 2
1-52A
T.O. 1B-52H-34-2-8
Mission Supervision Menu (CF-8) (Cont)
WINDOW
DISPLAY
MODIFIABLE
1
Loaded B-52 Mission
Type
NO
2
3
4
5
FUNCTION
WAR
JASSM War mission is loaded.
OTL
JASSM Operational Test Launch (OTL) mission is loaded.
CC
JASSM Captive Carry (CC) mission is loaded.
FERRY
JASSM Ferry mission is loaded.
TLI
JASSM Timeline Integration (TLI) mission is loaded.
(blank)
No mission is loaded, or the current mission is not recognized by the JASSM
SMO.
Less [AMI] Missile
Mission Data Tape
NO
28 Character ASCII
Title
Missile mission data tape label.
(blank)
When no missile DTUC is installed; title on mission data tape contains all
blanks.
[AMI] Sortie Title
NO
28 Characters
Title of the sortie loaded into the ACU.
(Blank)
No mission is loaded into the ACU or mission data load is in progress.
[AMI] Mission Title
NO
28 Characters
Title of the mission loaded into the ACU.
(Blank)
No mission is loaded into the ACU or mission data load is in progress.
[AMI] Weapon Group
Title
28 Characters
NO
Title of the weapon group assigned to the associated location.
Figure 1-25 (Sheet 2 of 2)
1-52B
Change 2
T.O. 1B-52H-34-2-8
B-52 Mission Data Load Display (CF-81)
[AMI]
WINDOW
1
DISPLAY
Primary SMO Title
MODIFIABLE
NO
24 Character Label
2
3
4
Sortie Title
Primary SMO title.
NO
28 Character Label
Title of the sortie loaded into the ACU.
(Blank)
No mission is loaded into the ACU or mission data load is in progress.
Mission Title
NO
28 Character Label
Title of the mission loaded into the ACU.
(Blank)
No mission is loaded into the ACU or mission data load is in progress.
PRIMARY SMO
GROUP
(Bright Underlined
Video)
NO
(Blank)
5
FUNCTION
Primary SMO Weapon
Group
The text, PRIMARY SMO GROUP, will appear when a weapon group has
been loaded for the primary SMO.
No weapon group has been loaded for the primary SMO.
NO
28 Character Label
Title of the weapon group loaded for the primary SMO.
(Blank)
No weapon group has been loaded for the primary SMO.
Figure 1-25A (Sheet 1 of 2)
Change 2
1-52C
T.O. 1B-52H-34-2-8
B-52 Mission Data Load Display (CF-81) (Cont)
WINDOW
6
DISPLAY
MODIFIABLE
Sortie No. Select
YES
n
6A
7
8
Loaded B-52 Mission
Type
Selected sortie number (1 - 8).
NO
WAR
JASSM War mission is loaded.
OTL
JASSM Operational Test Launch (OTL) mission is loaded.
CC
JASSM Captive Carry (CC) mission is loaded.
FERRY
JASSM Ferry mission is loaded.
TLI
JASSM Timeline Integration (TLI) mission is loaded.
(blank)
No mission is loaded, or the current mission is not recognized by the JASSM
SMO.
DTC Sortie Count
NO
0
No DTC is installed or no sorties are resident on the DTC.
n
Number of sorties resident on the DTC.
Selected Sortie No.
NO
n
9
10
FUNCTION
Selected Sortie Title
Selected sortie number (1 - 8).
NO
28 Character Label
Title of selected sortie on the DTC.
(Blank)
No DTC is available.
DTC Mission Title
NO
28 Character Label
Title of each mission data file in the DTC for the selected sortie.
(Blank)
No DTC is available.
Figure 1-25A (Sheet 2 of 2)
1-52D
Change 2
T.O. 1B-52H-34-2-8
Weapon Group Load Menu (CF-82A, CF-82C)
[AMI]
Figure 1-25B (Sheet 1 of 2)
Change 2
1-52E
T.O. 1B-52H-34-2-8
Weapon Group Load Menu (CF-82A, CF-82C) (Cont)
WINDOW
DISPLAY
MODIFIABLE
1
Selected Sortie Title
NO
2
3
4
28 Character Label
Title of the sortie resident in the ACU.
(Blank)
No mission is loaded into the ACU or mission data load is in progress.
Selected Mission Title
NO
28 Character Label
Title of the mission resident in the ACU.
(Blank)
No mission is loaded into the ACU or mission data load is in progress.
Selected Weapon
Group
NO
28 Character Label
Title of the weapon group loaded into the ACU for the selected location.
(Blank)
No weapon group loaded into the ACU for the selected location.
Number of Weapon
Groups Available
NO
n or nn
5
Weapon Group
Number
Number of JASSM weapon groups available to load.
NO
n or nn
6
FUNCTION
Weapon Group
Title
28 Character Label
JASSM weapon group number.
NO
JASSM weapon group title.
Figure 1-25B (Sheet 2 of 2)
1-52F
Change 2
T.O. 1B-52H-34-2-8
TARGETING PROCESS CONTROL (CF-DD AND CF-DE)
DIRECT TARGET COPY COMMAND (CF-Dn)
There are two commands (CF-DD and CF-DE) that
allow an operator to control the completion process
when one of the following requests is active:
Operator entry of CF-Dn, will result in the direct
target data currently displayed being copied to direct target n. n represents the number of the direct
target to receive the copied direct target data. A
confirmation prompt, OVERWRITE DATA? (YES/
NO) will be displayed requesting confirmation to
overwrite the existing direct target data for direct
target n with the current direct target data. A YES
response to the confirmation prompt will result in
overwriting the target data for direct target n and
missiles previously assigned/targeted to direct target n will be unassigned/untargeted. A NO response
to the confirmation prompt will result in abandoning the CF-Dn command, leaving the direct target n
data and missile assignment and targeted states
unchanged. If the confirmation prompt is unanswered after Less [AMI] 60 seconds, [AMI] 120
seconds the default answer of NO will be assumed.
• Manual Targeting (CF-586).
• Direct Target Definition (CF-588).
The targeting process completion command, CFDD, initiates the downloading of target data to the
selected missile(s). The other command used to control the targeting process is the CF-DE command,
and is used to exit targeting process without downloading data to the missile(s).
Targeting Completion Command (CF-DD)
Operator entry of CF-DD will conclude the current
targeting request. If either the manual targeting or
direct targeting operation is being performed and if
missiles are selected, transfer of targeting data to
the selected missiles will be initiated. The current
targeting process will then be concluded if Direct
Targeting is active.
The SMO will reject a CF-DD command and display
it in reverse video if any of the following conditions
exist:
• The manual targeting or direct target definition operation is not active.
• The display associated with the active targeting operation is not present on the selected MFD.
• The data items required have not been entered for the active targeting operation.
• Less [AMI] Manual targeting operation is active and a missile mission DTUC is not available.
• [AMI] Manual targeting operation is active
and a weapon mission group is not available.
Exit Targeting Process Command (CF-DE)
Operator entry of CF-DE command will exit the request without initiating the transfer of targeting
data or saving direct target that has been changed.
The SMO will reject a CF-DE command and display
it in reverse video if any of the following conditions
exist:
• The manual targeting or direct target operation is not active.
• The display associated with the active targeting operation is not present on the selected MFD.
The SMO will reject a CF-Dn command and display
it in reverse highlight if any of the following conditions exist:
• Direct Target operation is not currently active.
• Direct target n is the same as the currently
displayed direct target.
• n is not a valid direct target number.
• There is another confirmation prompt pending.
• Direct Target display is not displayed on the
same MFD on which the copy command was entered.
MISSILE CONTROL PANEL BACKUP DISPLAY (CF-E)
CF-E, shown in figure 1-26, can be used by the operator to enter missile commands in lieu of entering
the commands via the WCP. The CF-E commands
associated with the JASSM SMO are contained in
figure 1-27. Input of commands using CF-E is contained in Section III of T.O. 1B-52H-1-12.
SELECTED DIRECT TARGET DESELECTION COMMAND (CLR-D)
If a direct target has been selected via PRGM-Dn,
operator entry of CLR-D will command the SMO to
deselect that direct target for launch. If a direct target is not currently selected for launch, CLR-D will
be rejected and displayed in reverse video. The selected direct target will also be exited if auto launch
mode is selected or a fly-to command is entered.
Change 2
1-52G/(1-52H blank)
BLA
T.O. 1B-52H-34-2-8
Missile Control Panel Backup Display (CF-E)
PMD
W I U PWR
L P 1 / 2 =E 9A
WPN J E T T
SE L = EE 1
4
RP 1 / 2 = E 9 C
EN HW SWCH= E 9D
L AUNCH
/ 5
MODE = E 7
= ECD
6
ENTER
WPN PWR
ON = E 6 A
OF F = E 6 B
3
=E 1 1
’ E 3 ’ THEN ENTER
L OCA T I ON
+
7
8
’A’
9
TO SE L ECT OR ’ 0 ’ TO CL E AR
S T A T I ON
= E3
1 2 3
6 7 8
CF E
10
11
WINDOW
1
2
3
4
DISPLAY
WIU Power Status
11
11
11
MODIFIABLE
NO
WIU power is off.
ON (Bright Underlined
Video)
WIU power is on.
NO
OFF
WIU power is on.
OFF (Bright Underlined Video)
WIU power is off.
Master Fault Status
NO
MSTR
FAULT
A master fault is not displayed.
MSTR
FAULT (Bright
Underlined Video)
A master fault is displayed.
AUTO Launch Mode
Status
A67182
FUNCTION
ON
WIU Power Status
11
NO
AUTO
Launch mode is manual.
AUTO (Bright
Underlined Video)
Launch mode is automatic.
Figure 1-26 (Sheet 1 of 2)
1-53
T.O. 1B-52H-34-2-8
Missile Control Panel Backup Display (CF-E) (Cont)
WINDOW
5
6
7
8
9
10
11
DISPLAY
MAN Launch Mode
Status
MODIFIABLE
FUNCTION
NO
MAN
Launch mode is automatic.
MAN (Bright
Underlined Video)
Launch mode is manual.
MAN Launch
Command
NO
MAN LAUNCH
Manual launch has not been commanded or has completed.
MAN LAUNCH (Bright
Underlined Video)
Manual launch has been commanded and launch is in progress.
Location Identifier
NO
LP
Left pylon is not selected.
LP (Bright Underlined
Video)
Left pylon is selected.
Location Identifier
NO
RP
Right pylon is not selected.
RP (Bright Underlined
Video)
Right pylon is selected.
Station Identifier
NO
ALL
ALL station switch is not selected.
ALL (Bright Underlined
Video)
ALL station switch is selected.
Station Identifier
NO
Station Number
1 Thru 8
Station is not selected (Stations 4 and 5 are not used).
Station Number
1 Thru 8 (Bright
Underlined Video)
Station is selected (Stations 4 and 5 are not used).
CF-E3 Status
YES
A
CF-E3 was the last command entered and the corresponding location or station is currently selected. When ‘A’ is displayed, the location/station identifier
above it will be displayed in Bright Underline Video.
0
CF-E3 was the last command entered and the corresponding location or station is not selected. When ‘0’ is displayed, the location/station identifier
above it will be displayed in Normal Video.
(blank)
CF-E3 was not the last command entered or corresponding location or station is not currently selected.
Figure 1-26 (Sheet 2 of 2)
1-54
T.O. 1B-52H-34-2-8
Commands for OAS Power Control Panel and Missile
Control Panel (CF-E)
OAS PCP/WCP SWITCH
CF-E COMMAND
PURPOSE
WPN JETT SEL
CF-EE1
Jettisons Selected missile(s)
WPN LNCH MODE
CF-E7
Switches AUTO/MAN Launch Function
MIU/LP
CF-E9A
Power ON/OFF for Left Pylon WIU
MIU/RP
CF-E9C
Power ON/OFF for Right Pylon WIU
EN HW SWCH
CF-E9D
Enable Commands to be Entered Via PCP/WCP subsequent to
CF-E9A or CF-E9C Commands
MAN LNCH
CF-ECD
Command Manual missile Launch
MSTR FAULT
CF-E11
Acknowledge Master Faults
Locations:
L PYLN
R PYLN
CF-E3
Allows Selection of Location(s) and Station(s)
WPN PWR ON
CF-E6A
Power ON for Selected missile(s)
WPN PWR OFF
CF-E6B
Power OFF for Selected missile(s)
Stations:
1, 2, 3, 6, 7, 8, and ALL
Figure 1-27
1-55
T.O. 1B-52H-34-2-8
FORMAT (FRMT) DISPLAYS
The FRMT display displays the format menu shown
in figure 1-29. FRMT-6 PME Status, FRMT-7 missile
Data, ([AMI] FRMT-7A LP Weapon Data, FRMT-7C
RP Weapon Data and FRMT-77 Stores Summary)
FRMT-10 DEST/OAP table, and FRMT-12 Weapon
Summary displays are applicable to JASSM operations. Operator entry of FRMT will cause the Format
Menu to be displayed on the selected MFD at the station where the command was entered. The format
commands are shown in figure 1-28.
tion Status displayed in the advisory area. The
Weapon Status and Inventory display without the
Selected Station Status is requested on the selected
MFD at an operator station by entering a FRMT-7
command when the JASSM SMO is the primary
SMO. The Weapon Status and Inventory display
can also be requested when the JASSM SMO is secondary SMO by entering a FRMT-7A command
when the JASSM SMO is assigned to the left pylon
or a FRMT-7C command when the JASSM SMO is
assigned to the right pylon.
NOTE
Radar/Electro-Optical Viewing System (EVS) Displays
Discussion of the Radar and EVS displays, commanded by FRMT-1, FRMT-2, FRMT-4, or FRMT-5,
is contained in T.O. 1B-52H-1-12. The SMO will
provide the destination label for these displays
when the destination is a JASSM launch point.
PME Status Display (FRMT-6)
Figure 1-30 shows FRMT-6, the PME Status display. Much of the data displayed on the PME Status
display is common OAS equipment and is contained
in T.O. 1B-52H-1-12.
The operator can review the operational status of
the AIU, ECU, left WIU and right WIU via the
PME Status display. The PME Status display
shows AIU and WIU A bus and C bus communication status and AIU, ECU and WIU failure status.
AIU will be displayed in reverse video, if the AIU
has failed; ECU will be displayed in reverse video,
if the ECU has failed; and WIU will be displayed in
reverse video for the left or right WIU respectively,
if either the WIU communication or the WIU have
failed. The AIU, ECU or WIU failure status is also
displayed on the JASSM Status and Inventory display (FRMT-7). Each failure display on FRMT-7 will
be removed if the associated failure status clears
[AMI] The CF-DF = PAGE FWD, CF–DB =
PAGE BACK label is in the advisory area
and will be overwritten if FRMT-7XY is
entered and when release advisories are
displayed.
The items which can be reviewed on the JASSM
Status and Inventory Display are contained in the
following list:
• Armament Interface Unit (AIU) fault indication.
• ECU fault indication.
• Left and right WIU, GPS receiver, IU, and
DTU/DTR fault indications.
• Missile identification type and sub-type.
• Missile power state.
• Missile faults.
• Ejector status (on selected station status only).
• Missile targeting status.
• Missile alignment status.
• Missile GPS data transfer status.
• Telemetry status (on selected station status
only).
• Manual launch required status (on selected
station status only).
• Crypto key presence indicators.
• Missile power on/off countup timer (on selected station status only).
Operator entry of FRMT-6 will cause the PME Status Display to be displayed on the selected MFD at
the station where the command was entered.
• Store missile type (on selected station status
JASSM Status and Inventory Display (FRMT-7)
• Carrier navigation mode status.
• In-Range/In-Zone status.
Less [AMI] The JASSM Status and Inventory display, commanded by FRMT-7, is shown in Figure
1-31. This display is used to view WCE and missile
status data.
[AMI] The Weapon Status and Inventory display
can be requested with or without the Selected Sta-
1-56
Change 2
only).
• Configuration ID (on selected station status
only).
Operator entry of FRMT-7 will cause the JASSM Status and Inventory Display to be displayed on the
selected MFD at the station where the command was
entered.
T.O. 1B-52H-34-2-8
JASSM Status and Inventory Display Request with Selected Station Status (FRMT-7xy)
Operator entry of FRMT-7xy, where xy represents a
single valid location and station selection, will
cause the JASSM Status and Inventory display
with selected station status display, figure 1-32, to
be displayed on the selected MFD along with status
from the selected location and station. A single valid location and station is selected on an IKB by entering ‘A’ or ‘C’ followed by a number 1, 2, 3, 6, 7, or
8. Numbers 4 and 5 are invalid stations for JASSM.
The characters ‘A’ and ‘C’ represent the left or right
pylon location respectively. The numbers represent
the selected station on the identified pylon. As an
example, a FRMT-7A3 command would request the
FRMT-7 display to appear with detailed station status for left pylon station 3 being displayed on the
bottom of the selected MFD at the station where
the command was entered.
[AMI] Weapon Assignment Data Display
(CF-DF or CF-DB From FRMT-7, 7A, 7C or 7xy)
The JASSM Weapon Assignment Data display (figure 1-32A), is requested by paging forward (CF-DF)
or backward (CF-DB) from the Weapon Status and
Inventory displays (FRMT-7, 7A, 7C or 7xy). In addition to common FRMT-7 data, such as station number, weapon type/subtype, and the launch point/target identifier, the Weapon Assignment Data display
provides the weapon group id, selected sortie, and
selected B-52 mission. Paging forward from FRMT-7
7A, 7C or 7xy, the Weapon Assignment Data dis-
plays are presented in the order of assigned JASSM
locations; Left Pylon, Right Pylon and back to the
starting FRMT-7,7A, 7C or 7xy display. Paging backward from the FRMT-7, 7A, 7C or 7xy will present
the Weapon Assignment Data displays in the reverse sequence.
NOTE
Although not displayed (overwritten with
JASSM xy data), CF-DF and CF-DB commands are available on the FRMT-7xy display, allowing the operator to request the
Weapon Assignment Data displays.
[AMI] Stores Inventory Summary Display (FRMT-77)
Operator entry of FRMT-77 displays the Stores Inventory Summary (figure 1-32B). The Stores Inventory Summary display provides generic store/weapon information for all locations. All data on this display is controlled by the CSP and none of the data
fields are modifiable.
Destination Table Display (FRMT-10,nn)
The Destination Table display, commanded by FMS
command FRMT-10,nn is shown in figure 1-33. The
SMO will provide the destination label, JASSM LP,
for each destination in figure 1-33 when the respective destination is a JASSM launch point. The SMO
will not allow modification of a turn short indication,
latitude, longitude, and altitude for a JASSM LP.
JASSM Format Commands
COMMAND
DESCRIPTION
FRMT
Format Menu Request.
FRMT-6
PME Status Display Request.
FRMT-7
JASSM Status and Inventory Display Request.
FRMT-7A [AMI]
JASSM Status and Inventory Display Request.
FRMT-7C [AMI]
JASSM Status and Inventory Display Request.
FRMT-7xy
JASSM Status and Inventory Display Request with Selected Station xy.
FRMT-77 [AMI]
Stores Inventory Summary Display
FRMT-10,nn
Destination Table Display. nn = current or selected destination.
FRMT-12,nn
Weapon Summary Display. nn = direct target (Dn) or launch point (nn).
CF-DF or CF-DB From
FRMT-7, 7A, 7C or 7xy [AMI]
JASSM Weapon Assignment Data Display Request.
Figure 1-28
Change 2
1-57
T.O. 1B-52H-34-2-8
JASSM FRMT (Format) Menu
Less [AMI]
PMD
1
2
3
4
5
6
7
8
9
10
FRMT MENU
RDR
RDR + PMD
E VS
E VS + PMD
E VS F UL L
PME S T A TUS
WPN DA T A (XY )
EMERG DA T A
F XP T TB L
DE S T / OAP TB L
(XY = L OC / S T A )
1 2 WE APON SUMMARY ( NN )
+ XH POS I T I ON
NN= J ASS M L AUNCH PO I NT ( 1 − 9 9 ) OR D I R TGT ( D 1 −D 6 )
− − FRMT -
A67183
[AMI]
PMD
1
2
3
4
5
6
7
8
9
10
7A
7B
7C
FRMT MENU
RDR
RDR + PMD
E VS
E VS + PMD
E VS F UL L
PME S T A TUS
PR I MARY WE APON DA T A
EMERG DA T A
F XP T TB L
DE S T / OAP TB L
L P WPN DA T A
B AY WPN DA T A
RP WPN DA T A
+ XH POS I T I ON
7 7 ST OR ES SUMMARY
1 2 WE APON SUMMARY ( NN )
NN = J ASSML AUNCH P T ( 1 − 9 9 ) OR
D I R TGT ( D 1 −D 6 )
1
1
− − FRMT -
B40819
Figure 1-29 (Sheet 1 of 2)
1-58
Change 2
T.O. 1B-52H-34-2-8
WINDOW
1
DISPLAY
SMO ID
MODIFIABLE
FUNCTION
NO
24 Character ASCII ID
ID of SMO assigned to specified location.
24 Character ASCII ID
(Bright Underline Video)
ID of SMO assigned to specified location and SMO is primary.
(blank)
No SMO assigned to location.
Figure 1-29 (Sheet 2 of 2)
Change 2
1-59
T.O. 1B-52H-34-2-8
PME Status Display (FRMT-6)
Less [AMI]
PMD
BUS PME
FL T
ACU A
ACU B
ACU C
D TU
D TU
D TU
D TU
1
2
3
4
I ME 1
I ME 2
DVS
EIU
BUS PME
FL T
BUS PME F L T
DEU
RSC
RVR
RNK B
NK B
B U S PME F L T
RIU
AHRS
RDR
IU
GP S
S AU
RPK B
NPK B
CD I U
CSCP
RNMP
WCP
1
3
2 AIU
RA
DOOR
3
ECU
1
1
2 L WI U 3
2 R WI U 3
- - F RM T - 6
A47310
[AMI]
Figure 1-30 Sheet (1 of 2)
1-60
Change 2
T.O. 1B-52H-34-2-8
WINDOW
1
2
3
DISPLAY
Device A Bus Test
MODIFIABLE
FUNCTION
NO
A
The corresponding device has failed the A Bus test since the last time
faults were cleared (CF-66), but is currently passing the A Bus test.
A (Reverse Video)
The corresponding device is currently failing A Bus test.
(Blank)
The corresponding device has not failed the A Bus test since the last time
faults were cleared.
Device C Bus Test
NO
C
The corresponding device has failed the C Bus test since the last time
faults were cleared (CF-66), but is currently passing the C Bus test.
C (Reverse Video)
The corresponding device is currently failing the C bus test.
(Blank)
The corresponding device has not failed the C Bus test since the last
time faults were cleared.
Device Fault
NO
X
The corresponding device has failed since the last time faults were
cleared (CF-66), but is currently not faulted.
X (Reverse Video)
The corresponding device is currently faulted.
(Blank)
The corresponding device has not failed since the last time faults were
cleared.
Figure 1-30 Sheet (2 of 2)
Change 2
1-61
T.O. 1B-52H-34-2-8
JASSM Status and Inventory Display (FRMT-7)
(FRMT-7, FRMT-7A, FRMT-7C)
Less [AMI]
SAMPLE
PMD
1
2 M 1 −GO / 1 0 C
0 1 / MG
1 2 − 3 / 4 5
6 / 7
8
2
R I GHT 2
Z
1
3
L EF T
3
3
R I GHT 1
R I GHT 3
9
7
7
L EF T
6
7
R I GHT 7
8
L EF T
10
− − FRMT − 7
6
6
L EF T
11
12
8
8
R I GHT 6
13
14
R I GHT 8
15
16
17
A75616
•
•
NOTE
Details of the LEFT 1 station inventory defined in the following table, LEFT 2 display is shown as a sample. The other station data displays are identical.
Stations 4 and 5 are not used with JASSMs.
Figure 1-31 (Sheet 1 of 6)
1-62
Change 3
T.O. 1B-52H-34-2-8
[AMI]
SAMPLE
PMD
R I GHT 2
1
3
1 2 − 3 / 4 5
6 / 7
8
9
2
1
2 M 1 −GO / 10 C
0 1 / MG
Z
L EF T
3
3
R I GHT 1
7
7
L EF T
6
7
R I GHT 7
8
L EF T
10
− − FRMT - 7
R I GHT 3
6
6
L EF T
11
12
C F - DF = P AGE FWD
8
8
R I GHT 6
13
14
R I GHT 8
15
16
17
C F - DB = P AGE B ACK
B41366
•
•
WINDOW
1
2
NOTE
Details of the LEFT 1 station inventory defined in the following table, LEFT 2 display is shown as a sample. The other station data displays are identical.
Stations 4 and 5 are not used with JASSMs.
DISPLAY
Crypto Key Status
MODIFIABLE
FUNCTION
NO
NO KEYS
(Reverse Video)
Crypto keys are not available.
(blank)
Crypto keys are available.
Missile Type
M1
NO
Weapon power is off and mission data indicates weapon is an
AGM-158A.
Weapon power is on and both weapon and mission data agree weapon is
an AGM-158A.
M1 (Reverse Video)
Weapon is on and indicates that the weapon is an AGM-158A. Mission data
disagrees. Not a JASSM mission.
Figure 1-31 (Sheet 2 of 6)
Change 2
1-62A
T.O. 1B-52H-34-2-8
JASSM Status and Inventory Display (FRMT-7)
(FRMT-7, FRMT-7A, FRMT-7C) (Cont)
WINDOW
2 (Cont)
DISPLAY
M
MODIFIABLE
NO
FUNCTION
Weapon is on and indicating it is a variant.
Weapon is off and mission data indicates weapon is a variant.
A carrier mission is not loaded and the weapon is a JASSM. (SIT and Go/NoGo test only)
3
M (Reverse Video)
Weapon power is on and indicating it is a variant, and mission data is in
disagreement.
P
Weapon is present, but it is of unknown type. JASSM MSN data indicates
empty station. (WPN PRSNT master fault)
P (Reverse Video)
Non-JASSM weapon (displayed after power on attempt)
(blank)
WIU power is off for the location, or a missile is not present at the station.
Weapon Status
NO
CL
Captive Carry missile launched (simulated launch).
GO
Mission capable: Safe to Release with launchable alignment state. Manual
launch required.
GO (Bright Underline
Video)
Fully Mission capable: All Up Round ready with launchable alignment state.
NG (Reverse Video)
Permanent fatal fault has occurred for this missile. Missile power is
inhibited.
OF
WIU power is on for this pylon and missile power is off for this missile.
ON
Missile power is on for this missile.
X
Missile is not present and no missile presence discrepancy exists.
X (Reverse Video)
Missile is not present and a missile presence discrepancy exists.
(blank)
WIU power for this pylon is off.
Figure 1-31 (Sheet 3 of 6)
1-62B
Change 3
T.O. 1B-52H-34-2-8
WINDOW
4
5
6
DISPLAY
Target Data
MODIFIABLE
FUNCTION
NO
Dn
Direct target has been assigned to missile where n = 1 to 6, or the missile
has been launched against the target.
Dn (Bright Video)
Direct target has been assigned to the missile and targeting is in progress,
or the weapon has been powered off after targeting. n = 1 to 6.
Dn (Bright Underline
Video)
Direct target has been assigned to the missile, targeting data has been assigned, loaded, and verified.
Dn (Reverse Video)
Targeting failure.
nn
Launch point number has been assigned to the missile, or the missile has
been launched against the target. nn = 1 to 99.
nn (Bright Video)
Launch point number has been assigned to the missile and targeting is in
progress, or the weapon has been powered off after targeting. nn = 1 to 99.
nn (Bright Underline
Video)
Launch point has been assigned to the missile, targeting data has been assigned, loaded and verified.
nn (Reverse Video)
Targeting failure.
(blank)
Missile is not assigned, WIU power is not applied, or the missile has been
jettisoned.
Mission Group
NO
a
Mission group associated with the launch point that has been assigned to the
missile, or the missile has been launched against the target.
a = A to F.
a (Bright Video)
Mission group associated with the launch point that has been assigned to
the missile and targeting is in progress. a = A to F.
a (Bright Underline
Video)
Mission group associated with the launch point that has been assigned to the
missile, targeting data has been assigned, loaded and verified. a = A to F.
a (Reverse Video)
Targeting failure for mission group associated with the launch point.
a = A to F.
(blank)
WIU power is off, the missile is not assigned, the missile is assigned to a direct target prior to targeting or missile has been jettisoned.
Transfer Alignment
Quality
NO
nn
Transfer alignment quality. nn= 1 to 10.
nn (Reverse Video)
Transfer alignment quality. nn= 10. Reverse video indicates a failure has
Less [AMI] occurred; [AMI] persisted for a minimum of 10 minutes.
(blank)
WIU or missile power off, missile is not present, or transfer alignment not initiated.
Figure 1-31 (Sheet 4 of 6)
Change 3
1-62C
T.O. 1B-52H-34-2-8
JASSM Status and Inventory Display (FRMT-7)
(FRMT-7, FRMT-7A, FRMT-7C) (Cont)
WINDOW
7
DISPLAY
Missile Status
MODIFIABLE
FUNCTION
NO
BT
Missile is in IBIT.
ER
Mission data successfully erased.
ER (Normal Blinking
Video)
Mission data erase in progress.
ER (Reverse Video)
Mission data erase failure.
IN
Missile is in GPS Initialization.
NOTE
IN can also indicate the combined loss of crypto keys, AUR ready,
and minimum GPS.
8
IN (Reverse Video)
Missile is in GPS initialization and Time Received fault has occurred.
MG
Missile has received minimum GPS data to acquire GPS after launch.
MG (Reverse Video)
Missile has received minimum GPS data and Ephemeris Received fault occurred.
TK
Missile is tracking at least 4 satellites (test launch only).
WU
Missile is in Warmup. Prior to missile power application, indicates heater
power is applied (115 VAC). Subsequent to missile power application,
indicates missile is in warm-up.
WU (Reverse Video)
Heater power fault has occurred (while missile power on or off) or warm up
fault has occurred (while missile power on).
(blank)
WIU is off, or missile 115 VAC and 28 VDC #1 is off.
Ranging/In-Zone
NO
R
In-Range.
[AMI] R (Reverse
Video)
In-Range with launch inhibited.
Z
In-Zone.
[AMI] Z (Reverse
Video)
In-Zone with launch inhibited.
(blank)
WIU or missile power is off, or neither In-Range nor In-Zone.
9
Missile Fault Display
NO
10
L WIU Fault Indicator
NO
When a missile fault exists, the fault text is displayed.
(See FRMT-7 missile Faults in Section VII).
WIU (Reverse Video)
A WIU fault indication has been received which may preclude missile launch
from the left pylon or communication with the left WIU has failed.
(blank)
No fault is present for the left WIU.
Figure 1-31 (Sheet 5 of 6)
1-62D
Change 3
T.O. 1B-52H-34-2-8
WINDOW
11
DISPLAY
Carrier Nav Mode
NO
Carrier nav mode is DPLR/AHRS. ([AMI] Over land only)
DPLR-NAV
Carrier nav mode is DPLR-NAV.
GPS/AHRS
(Reverse Video)
Carrier nav mode is GPS/AHRS.
GPS-NAV
Carrier nav mode is GPS-NAV.
NAV
Carrier nav mode is NAV.
NAV INVALD
(Reverse Video)
Invalid nav mode.
(blank)
No prime nav mode data available.
Fault/Status Indicators
12
[AMI] DTC (Blinking
Video)
NO
The I/O with the missile Mission DTUC/DTC failed (GPS initialization or missile Mission Data attempt).
(blank)
No fault is present or [AMI] SMO is not accessing the DTC.
IU (Reverse Video)
NO
GPS (Reverse Video)
ECU (Reverse Video)
NO
AIU (Reverse Video)
NO
R WIU Fault Indicator
An ECU fault indication has been received from the AIU.
No fault is present.
NO
(blank)
17
The IU has faulted the GPS receiver.
No fault is present.
(blank)
16
The I/O with the Interface Unit failed (GPS Almanac or Crypto Keys Access
attempt).
No fault is present.
(blank)
15
SMO is accessing DTC.
DTU ([AMI] DTC)
(Reverse Video)
(blank)
14
FUNCTION
DPLR/AHRS
(Reverse Video)
12-16
13
MODIFIABLE
An AIU fault indication has been received which may preclude missile
launch or communication with the AIU has failed.
No fault is present.
NO
WIU (Reverse Video)
A WIU fault indication has been received which may preclude missile launch
from the right pylon or communication with the right WIU has failed.
(blank)
No fault is present.
Figure 1-31 (Sheet 6 of 6)
Change 2
1-63
T.O. 1B-52H-34-2-8
JASSM Status and Inventory Display with Selected
Station Status (FRMT-7xy)
SAMPLE
PMD
2 M 1 −GO / 1 0 C
0 1 / MG
Z
1
2
R I GHT 2
3
L EF T
1
2
L EF T
3
7
R I GHT 3
7
L EF T
6
7
R I GHT 7
8
L EF T
3
R I GHT 2
6
6
L EF T
8
8
R I GHT 6
R I GHT 8
− − FRMT − 7 XY
12
3
11
8
T LMY
7
EJ
1 5 T I ME
4 / 5 6
12 / 13
9
10
16
14
A75617
NOTE
Stations 4 and 5 are not used with JASSMs.
WINDOW
1
DISPLAY
Selected Location
MODIFIABLE
FUNCTION
NO
x (Bright Video)
x = Pylon Location L or R.
L = Left pylon location of missile selected.
R= Right pylon location of missile selected.
2
Selected Station
y (Bright Video)
NO
y = Station number of missile selected; 1, 2, 3, 6, 7 or 8.
Figure 1-32 (Sheet 1 of 5)
1-64
T.O. 1B-52H-34-2-8
WINDOW
3
4
5
DISPLAY
Missile Type ID
possible:
MODIFIABLE
NO
FUNCTION
Store Identification for selected station.
AGM-158A
An AGM-158A JASSM is present.
(blank)
WIU is off; power has never been applied to the weapon; or weapon is
not present.
JASSM Status
NO
CL
Captive Carry missile launched (simulated launch).
GO
Mission capable: Safe to Release with launchable alignment state. Manual launch required.
GO (Bright Underline
Video)
Fully Mission capable: All Up Round ready with launchable alignment
state.
NG (Reverse Video)
Permanent fatal fault has occurred for this missile. Missile power is inhibited.
OF
WIU power is on for this pylon and missile power is off for this missile.
ON
Missile power is on for this missile.
X
Missile is not present and no missile presence discrepancy exists.
X (Reverse Video)
Missile is not present and a missile presence discrepancy exists.
(blank)
WIU power for this pylon is off.
Direct Target/Launch
Point Number
NO
Dn
Direct target has been assigned to missile where n = 1 to 6, or the missile
has been launched against the target.
Dn (Bright Video)
Direct target has been assigned to the missile and targeting is in progress,
or the weapon has been powered off after targeting. n = 1 to 6.
Dn (Bright Underline
Video)
Direct target has been assigned to the missile, targeting data has been
loaded and verified.
Dn (Reverse Video)
Targeting failure.
nn
Launch point number has been assigned to the missile, or the missile has
been launched against the target. nn = _1 to 99.
nn (Bright Video)
Launch point number has been assigned to the missile and targeting is in
progress, or the weapon has been powered off after targeting. nn = 1 to 99.
nn (Bright Underline
Video)
Launch point or target number has been assigned to the missile,
loaded and verified.
nn (Reverse Video)
Targeting failure.
(blank)
Missile is not assigned; WIU power is not applied; or the missile has been
jettisoned.
Figure 1-32 (Sheet 2 of 5)
Change 3
1-65
T.O. 1B-52H-34-2-8
JASSM Status and Inventory Display with Selected
Station Status (FRMT-7xy) (Cont)
WINDOW
6
DISPLAY
Mission Group
MODIFIABLE
NO
a
Mission group associated with the launch point that has been assigned to
the missile, or the missile has been launched against the target. a = A to F.
a (Bright Video)
Mission group associated with the launch point that has been assigned to
the missile and targeting is in progress. a = A to F.
a (Bright Underline
Video)
Mission group associated with the launch point that has been assigned to
the missile, targeting data has been assigned, loaded and verified. a = A
to F.
a (Reverse Video)
Targeting failure for mission group associated with the launch point. a = A
to F.
(blank)
WIU power is off, the missile is not assigned, the missile is assigned to a
direct target prior to targeting or missile has been jettisoned.
7
Missile Fault Display
NO
8
Telemetry Power Status
(Flight Test Only)
NO
9
10
11
FUNCTION
When a missile fault exists, the fault text is displayed.
(See FRMT-7 missile Faults in Section VII).
OFF
Telemetry is commanded off.
ON
Telemetry is commanded on.
(blank) Less [AMI]
WIU power is off.
Manual Launch
Required Indication
NO
MAN LNCH REQ
(Reverse Video)
Missile requires manual launch and missile power is on.
(blank)
Weapon power is on with no fault requiring manual launch existing or weapon power is off.
For Test Only:
In addition to the MAN LNCH REQ the window will display the following:
TXA HALT
Missile transfer alignment halt test is commanded (test only).
TXA HLT/REIN
Missile transfer alignment halt and reinitialization tests are both commanded (test only).
TXA REINIT
Missile transfer alignment reinitialization test is commanded (test only).
(blank)
Missile power is off and TXA halt is not commanded, or missile is not
present.
Ejector Status
NO
NOT UNLKD (Reverse
Video)
Illegal ejector status is detected.
UNLOCKD
Ejector is unlocked.
(blank)
Missile is not present or WIU power for this pylon is off.
Missile Configuration ID
NO
xxxxxx
Missile Configuration ID.
(blank)
Less [AMI] WIU power off. [AMI] Power has never been applied to either
the WIU or the weapon, or weapon is not present.
Figure 1-32 (Sheet 3 of 5)
1-66
Change 2
T.O. 1B-52H-34-2-8
WINDOW
12
13
DISPLAY
Transfer Alignment
Quality
MODIFIABLE
FUNCTION
NO
nn
Transfer alignment quality. nn= 1 or 10 (1 = Aligned;10 = NOT Aligned).
nn (Reverse Video)
Transfer alignment quality. nn= 10. Reverse video indicates a failure has
Less [AMI] occurred; [AMI] persisted for a minimum of 10 minutes.
(blank)
WIU or missile power off, missile is not present, or transfer alignment not initiated.
Weapon Data/GPS
Status
NO
BT
Missile is in IBIT.
ER
Mission data successfully erased.
ER (Normal Blinking
Video)
Mission data erase in progress.
ER (Reverse Video)
Mission data erase failure.
IN
Missile is in GPS Initialization.
NOTE
IN can also indicate the combined loss of crypto keys, AUR ready,
and minimum GPS.
14
IN (Reverse Video)
Missile is in GPS Initialization and Time Received fault has occurred.
MG
Missile has received minimum GPS data to acquire GPS after launch.
MG (Reverse Video)
Missile has received minimum GPS data and Ephemeris Received fault occurred.
TK
Missile is tracking at least 4 satellites (test launch only).
WU
Missile is in Warmup. Prior to missile power application, indicates heater
power is applied (115 VAC). Subsequent to missile power application,
indicates missile is in warm-up.
WU (Reverse Video)
Heater power fault has occurred (while missile power on or off) or warm up
fault has occurred (while missile power on).
(blank)
WIU is off, or missile 115 VAC and 28 VDC #1 is off.
Crypto Key Status
NO
K
Status received from the missile indicates crypto-keys are present. This indication will remain displayed even if missile subsequently fails to indicate
keys present.
K (Reverse Video)
Missile indicates crypto-keys are in error or have not been received.
(blank)
Missile is powered off or prior to download.
Figure 1-32 (Sheet 4 of 5)
Change 3
1-67
T.O. 1B-52H-34-2-8
WINDOW
15
DISPLAY
Missile Power/
Overheat Status
MODIFIABLE
FUNCTION
NO
The effects of weapon overheat on weapon reliability and accuracy are unknown.
16
HOT (Reverse Video)
Label indicating that Overheat Caution has been issued for missile that
has power applied.
HOT (Reverse Blinking
Video)
Label indicating that Overheat Warning has been issued for missile that
has power applied.
OFF (Bright Video)
Label indicating that missile is powered OFF.
ON (Bright Video)
Label indicating that missile is powered ON and neither an Overheat
Warning nor an Overheat Caution exist.
(blank)
Less [AMI] WIU power is off, or missile not present, or power has never
been applied to missile. [AMI] Power has never been applied to either
the WIU or the weapon, or the weapon is not present.
Missile Overheat
Monitor Time
NO
hh:mm
Time in hours and minutes that missile has been powered ON, powered
OFF, or had either an Overheat Warning or an Overheat Caution issued
while powered on. Time pertains to status displayed in Missile Power/
Overheat Status window.
Range 00:00 – 99:59 (Hours:Minutes).
(blank)
Less [AMI] WIU power is off, or missile not present, or power has never
been applied to missile. [AMI] Power has never been applied to either
the WIU or the weapon, or the weapon is not present.
Figure 1-32 (Sheet 5 of 5)
1-68
Change 2
T.O. 1B-52H-34-2-8
Weapon Assignment Data Display
(CF-DF or CF-DB From FRMT-7, 7A, 7C or 7xy)
[AMI]
WINDOW
1
2
3
DISPLAY
MODIFIABLE
JASSM Location
LP
(Bright Underlined)
RP
(Bright Underlined)
NO
Selected Sortie Title
28 Character Label
(blank)
NO
Selected Mission Title
28 Character Label
NO
Displayed weapon assignment data is for the left pylon.
Displayed weapon assignment data is for the right pylon.
ID of sortie loaded into ACU.
No sortie is loaded into ACU.
ID of B-52 mission loaded into ACU.
(blank)
4
Missile Type
M1
FUNCTION
No B-52 mission is loaded in ACU.
NO
Weapon power is off and mission data indicates weapon is an
AGM-158A.
Weapon power is on and both weapon and mission data agree weapon is
an AGM-158A.
M1 (Reverse Video)
Weapon is on and indicates that the weapon is an AGM-158A. Mission data
disagrees. Not a JASSM mission.
Figure 1-32A (Sheet 1 of 2)
Change 2
1-68A
T.O. 1B-52H-34-2-8
Weapon Assignment Data Display
(CF-DF or CF-DB From FRMT-7, 7A, 7C or 7xy)
(Cont)
WINDOW
4 (Cont)
DISPLAY
MODIFIABLE
M
FUNCTION
Weapon is on and indicating it is a variant.
Weapon is off and mission data indicates weapon is a variant.
A carrier mission is not loaded and the weapon is a JASSM. (SIT and Go/NoGo test only)
5
6
M (Reverse Video)
Weapon power is on and indicating it is a variant, and mission data is in
disagreement.
P
Weapon is present, but it is of unknown type. JASSM MSN data indicates
empty station. (WPN PRSNT master fault)
P (Reverse Video)
Non-JASSM weapon (displayed after power on attempt)
(blank)
WIU power is off for the location, or a missile is not present at the station.
Target Data
NO
Dn
Direct target has been assigned to missile where n = 1 to 6, or the missile
has been launched against the target.
Dn (Bright Video)
Direct target has been assigned to the missile and targeting is in progress.
n = 1 to 6.
Dn (Bright Underline
Video)
Direct target has been assigned to the missile, targeting data has been assigned, loaded, and verified.
Dn (Reverse Video)
Targeting failure.
nn
Launch point number has been assigned to the missile, or the missile has
been launched against the target. nn = 1 to 99.
nn (Bright Video)
Launch point number has been assigned to the missile and targeting is in
progress. nn = 1 to 99.
nn (Bright Underline
Video)
Launch point has been assigned to the missile, targeting data has been assigned, loaded and verified.
nn (Reverse Video)
Targeting failure.
(blank)
Missile is not assigned, WIU power is not applied, or the missile has been
jettisoned.
Selected Weapon
Group
NO
28 Character Label
(Bright Underlined)
ID of weapon group, loaded into ACU and used for targeting data.
(blank)
No targeting data is currently assigned to the weapon.
Figure 1-32A (Sheet 2 of 2)
1-68B
Change 2
T.O. 1B-52H-34-2-8
Stores Inventory Summary Display
(FRMT-77)
[AMI]
PMD
1
1 2 3 4
5
1
1 2 3 4
5
1
1 2 3 4
5
2 2 3 4
5
2 2 3 4
5
2 2 3 4
5
3 2 3 4
5
3 2 3 4
5
3 2 3 4
5
4 2 3 4
5
4 2 3 4
5
4 2 3 4
5
5 2 3 4
5
5 2 3 4
5
5 2 3 4
5
6 2 3 4
5
6 2 3 4
5
6 2 3 4
5
7 2 3 4
5
7 2 3 4
5
7 2 3 4
5
8 2 3 4
− − FRMT - 7 7
5
8 2 3 4
5
8 2 3 4
5
B42831
WINDOW
1
2
DISPLAY
SMO Title
MODIFIABLE
FUNCTION
NO
17 Characters
SMO title assigned to the location (truncated to 17 characters).
17 Characters (Bright
Underlined Video)
Primary SMO title (truncated to 17 characters).
(blank)
No SMO assigned to the location.
Weapon Type
NO
aa
Weapon type as provided by the loaded aircraft mission data (No SMO
loaded at the location or the SMO cannot confirm the actual store type.)
aa = JA (JASSM) or CL (CALCM)
aa (Bright Underlined
Video)
Weapon type as provided by the loaded aircraft mission data, that has
been confirmed by the weapon.
aa (Reverse Video)
The SMO has confirmed that the weapon type as provided by the loaded
aircraft mission data does not match the actual weapon type.
(blank)
No SMO is assigned to the location and there is no mission loaded.
(Blank) (Reverse
Video)
No store indicated by mission data but weapon is present.
Figure 1-32B (Sheet 1 of 2)
Change 2
1-68C
T.O. 1B-52H-34-2-8
Stores Inventory Summary Display
(FRMT-77) (Cont)
WINDOW
3
4
5
DISPLAY
Weapon Status
MODIFIABLE
FUNCTION
NO
CL
Captive Carry missile launched (simulated launch).
GO
Mission capable: Safe to Release with launchable alignment state.
Manual launch required.
GO (Bright Underline
Video)
Fully Mission capable: All Up Round ready with launchable alignment
state.
NG (Reverse Video)
Permanent fatal fault has occurred for this missile. Missile power is
inhibited.
OF
WIU power is on for this pylon and missile power is off for this missile.
ON
Missile power is on for this missile.
X
Missile is not present and no missile presence discrepancy exists.
X (Reverse Video)
Missile is not present and a missile presence discrepancy exists.
(blank)
WIU power for this pylon is off.
Target Data
NO
Dn
Direct target has been assigned to missile where n = 1 to 6, or the missile
has been launched against the target.
Dn (Bright Video)
Direct target has been assigned to the missile and targeting is in progress,
or the weapon has been powered off after targeting. n = 1 to 6.
Dn (Bright Underline
Video)
Direct target has been assigned to the missile, targeting data has been
assigned, loaded, and verified.
Dn (Reverse Video)
Targeting failure.
nn
Launch point number has been assigned to the missile, or the missile has
been launched against the target. nn = 1 to 99.
nn (Bright Video)
Launch point number has been assigned to the missile and targeting is
in progress, or the weapon has been powered off after targeting. nn = 1
to 99.
nn (Bright Underline
Video)
Launch point has been assigned to the missile, targeting data has been
assigned, loaded and verified.
nn (Reverse Video)
Targeting failure.
(blank)
Missile is not assigned, WIU power is not applied, or the missile has been
jettisoned.
Time To In-Range
NO
mm:ss
The time in minutes and seconds required for the aircraft to reach a point
that is within range of the target if the aircraft continues flying at the current
GS, altitude and ground track. This condition is termed “time-to-go (TTG)
to in-range”. Maximum value is 59:59 if greater than one hour.
mm:ss (Reverse Video)
Weapon unable to provide valid in-range data, launch is inhibited, or aircraft is inside Min range circle. Number indicated is based on the last valid
data or 59:59 if greater than one hour.
00:00
Aircraft is in-range.
(blank)
In-range is unachievable, or no selected weapon event.
(blank) (Reverse Video)
Not ranging and weapon unable to provide valid in-range data.
Figure 1-32B (Sheet 2 of 2)
1-68D
Change 2
T.O. 1B-52H-34-2-8
Destination Table Display (FRMT-10,nn)
PMD
1
1 OAP − 1
2
−2
3
−3
4
−4
1
1
2
3
4
−1
−2
−3
−4
− − FRMT − 1 0
’
nn
A75618
WINDOW
1
DISPLAY
Destination ID
JASSM LP
MODIFIABLE
FUNCTION
NO
Destination is a JASSM Launch Point (LP).
Figure 1-33
1-69
T.O. 1B-52H-34-2-8
Weapon Summary Display (FRMT-12, FRMT-12,nn or
FRMT-12,Dn)
The Weapon Summary display, commanded by
FRMT-12, FRMT-12,nn or FRMT-12,Dn is shown in
figure 1-34. The FRMT-12 display provides a sorted
summary of targeting data for up to 12 missiles. A
maximum of 4 missiles will be shown on one display, requiring scrolling to view targeting data for
other missiles. CF-DB and CF-DF will allow the operator to scroll backwards and forwards between
missiles in groups of four. The sorted targeting data
will be displayed in the order of: JASSM stores targeted to launch points, followed by stores targeted
to direct targets, and ending with the status of missiles not targeted or having no assignment.
The FRMT-12 command will sort the targeting data
and request the Weapon Summary display starting
with the first missile identified by the sort. The
FRMT-12,nn command will sort the targeting data
and request the Weapon Summary display beginning with the missile assigned to JASSM launch
point nn. JASSM launch point nn can be a number
from _1 to 99. The FRMT-12,Dn command will sort
the targeting data and request the Weapon Summary display beginning with the missile assigned to
JASSM direct target D1. JASSM launch point Dn
can be a direct target from D1 to D6. The sort is executed once upon entry of the FRMT-12,nn or
FRMT-12,DN command. If a missile assignment
change occurs while the FRMT-12 screen is displayed, all location/stations will be displayed in reverse video in the location/station window. This provides an indication to the operator that the targeting data displayed may not be accurate. Therefore,
re-entry of the FRMT-12,nn command is required
after targeting is complete to resort and refresh displayed targeting data. The following four conditions
will cause a FRMT-12 command to be rejected and
displayed in reverse video.
• A FRMT-12,nn command was entered and nn
is not a valid JASSM launch point.
• A FRMT-12,Dn command was entered and n
is not a valid JASSM Direct target.
• No missile is assigned to the requested
JASSM launch point.
• A FRMT-12,nn command was entered and the
applicable carrier mission is not loaded.
1-70
Change 2
NOTE
Discrepancies can occur between an impact
angle displayed on FRMT-12 display and
CF-588 Direct Targeting display. The Missile will use a built in minimum impact
angle of 20 if less than 20 is entered. The
missile will use a built in maximum impact
angle value of 70 if a value greater than 70
is entered. Therefore, while in strike mode
the impact angle displayed on FRMT-12
represents the missile’s value. While in SIM
mode the impact angle displayed is the
same as the value input.
DISPLAY PREVIOUS WEAPON SUMMARY
(CF-DB)
Entry of CF-DB while the Weapon Summary display is active will cause the targeting data for the
four previous missiles to be displayed in the preferred launch sequence. The SMO will reject a CFDB command and display the command in reverse
video if the Weapon Summary Display is not active
on the selected MFD or if there are no previous missile targets points to be displayed.
NOTE
CF-DB will not display targeting data previous to missile target nn if FRMT-12,nn
was entered, or previous to missile target
Dn if FRMT-12,Dn was entered.
DISPLAY NEXT WEAPON SUMMARY (CF-DF)
Entry of CF-DF while the Weapon Summary display is active will cause the targeting data for up to
four missiles to be displayed in the preferred
launch sequence. The SMO will reject a CF-DF
command and display the command in reverse video if the Weapon Summary display is not active on
the selected MFD or if there are no more missile
targets to be displayed.
T.O. 1B-52H-34-2-8
WEAPON SUMMARY DISPLAY
(FRMT-12,nn/FRMT-12,Dn)
Less [AMI]
[AMI]
PMD
J ASSM WE APON SUMMARY
ID/
LS
L AT
L ONG
2
1
3
P TOF
8
9
10
CRU I SE
BRG
I MP
EL EV
AL T
TGT
ANG
5
4
6 o 7 o
’
’
F UZ E MODE
DE L AY
11
1
8
’
F UZ E MODE
11
L7
1
8
9
2
P TOF
3
10
4
5
11
’
6 o
DE L AY
7 o
N4 1 o 3 4 . 5 6 7 8
W1 1 8 o 3 4 . 5 6 7 8
10 7 4 9 ’
99999 ’
270 o 30 o
SKR
P TOF 1 0 0 : 2 5
F UZ E MODE SOF T
DE L AY 3
9
2
P TOF
3
10
4
’
F UZ E MODE
5
11
’
6 o
DE L AY
12
12
7 o
12
− − FRMT - 1 2 , NN
CF - DF = P AGE FWD
CF - DB = P AGE B ACK
A86436
Figure 1-34 (Sheet 1 of 3)
Change 2
1-71
T.O. 1B-52H-34-2-8
WEAPON SUMMARY DISPLAY
(FRMT-12,nn/FRMT-12,Dn) (Cont)
WINDOW
1
2
DISPLAY
Current Event No.
MODIFIABLE
NO
nn
JASSM launch point. nn = _1 to 99.
Dn
Direct Target. n = 1 to 6.
0
Missile displayed in window is not assigned to any launch point or direct target.
Latitude
NO
add°mm.mmmm
3
Longitude
Target point latitude in degrees, minutes and ten-thousandths of a minute.
a = N for north and S for south.
Limits are S90.00.0000 through N90.00.0000.
VALID INPUT RANGE
ITEM
Degrees (d)
S90 to N90
Minutes (m)
00.0000 to 59.9999
NO
addd°mm.mmmm
4
5
6
Target point longitude in degrees, minutes and ten-thousandths of a minute.
a = E for east and W for west.
Limits are W 180.00.0000 through E 179.59.9999
VALID INPUT RANGE
ITEM
Degrees (d)
W180 to E179
Minutes (m)
00.0000 to 59.9999
Target Point Elevation
fffff
NO
Missile Cruise Altitude
nnnnn
NO
Missile Impact Azimuth
NO
Target elevation (MSL or HAE, as designated in mission planning, for preplanned targets; MSL for direct targets): –328 to 32810 in feet. Displayed
MSL can vary up to 10 feet due to HAE conversion in mission planning systems.
Missile Cruise Altitude for Direct Targets. nnnnn = 0 to 45000 (MSL) or
99999. A 99999 is displayed prior to operator entry of a value.
bbb
7
FUNCTION
Missile Impact Angle
dd
Bearing to Target (Impact Azimuth) in degrees true. bbb = 0 to 360 (0 =
North); bbb = 999 where the missile will determine BTT from aircraft to target
at time of launch. A 999 is displayed prior to operator entry of a value.
NO
Target Impact Angle in degrees relative to local level horizontal plane at
target impact. dd = 0 (level) to 90 (vertical) degrees. A value of 60 is displayed prior to operator entry of a value.
NOTE
Discrepancies can occur between an impact angle displayed on
FRMT-12 display and CF-588 Direct Targeting display. The Missile will use a built in minimum impact angle of 20 if less than 20
is entered. The missile will use a built in maximum impact angle
value of 70 if a value greater than 70 is entered. Therefore, while
in strike mode the impact angle displayed on FRMT-12 represents
the missile’s value. While in SIM mode the impact angle displayed
is the same as the value input.
(blank)
Targeting operation is not active.
Figure 1-34 (Sheet 2 of 3)
1-72
Change 2
T.O. 1B-52H-34-2-8
WINDOW
8
DISPLAY
Location/Station
Identifier
MODIFIABLE
FUNCTION
NO
xy
Location and Station of each missile.
xy (Reverse Video)
Target data displayed for this location/station may not be accurate.
Re-entry of Weapon Summary Display FRMT-12 command is recommended.
x = L for left pylon stations and R for right pylon stations.
y = Station number 1, 2, 3, 6, 7 or 8.
Each location and station that is displayed will be displayed in a dedicated
screen location for that missile.
9
10
11
12
Seeker Requirement
NO
SKR
Seeker is required for the target.
(blank)
Seeker is not required for the target.
Missile Planned Time
Of Flight (PTOF)
NO
mmm:ss
JASSM Planned Time Of Flight (PTOF) when a missile Time on Target
(TOT) is required. mmm:ss = Minutes and Seconds 00:00 to 143:10.
(blank)
The missile time on target is not required.
Fuze Target Type
NO
SOFT (Bright
Underlined Video)
Selected Fuze Mode is function on impact referenced to Crush Switch
(Soft target). SOFT is displayed prior to operator entry, [AMI] or if fuze
mode invalid.
HARD (Bright
Underlined Video)
Selected Fuze Mode is function on impact referenced to G-Force Sensor
(Hard target).
Fuze Function Delay
NO
m
Fuze function delay setting where m = 0 to 7. A 0 is displayed prior to
operator entry.
0
0 = Fuze mode is invalid.
Figure 1-34 (Sheet 3 of 3)
Change 2
1-73
T.O. 1B-52H-34-2-8
PROGRAM (PRGM) DISPLAYS
NOTE
The Program Display, commanded by the FMS command PRGM-, is shown in figure 1-36. This command allows the operator to review certain mission
parameters prior to and during launch. In addition,
the Program display also shows pertinent launch,
ranging, and missile status data in preparation for
launch. The data displayed at the top and bottom of
the Program display is common OAS navigation
and B-52 mission data and is contained in T.O.
1B-52H-1-12. However, the items contained in the
middle of the screen, commonly designated as
Group III data, relate to JASSM launch events. The
items regarding JASSM operation are:
Safe launch advisories and ranging times on
the Program display are calculated by the aircraft. In-Range and In-Zone indications on
the display are independently calculated by
the weapon. Because of the independent calculation and data latency, it is possible for the
safe launch advisories and aircraft calculated
ranging indications to differ from the InRange and In-Zone indications. The InRange and In-Zone indications describe the
status of the weapon, and will be honored by
the weapon when launched.
• Current launch point identifier.
• In-Zone indication for current launch point.
• In Range indication for current launch point.
• Time to Go (TTG) to In-Range for current
Operator entry of PRGM will cause the Program
Display (Figure 1-36) for the current destination to
be displayed on the selected MFD at the station
where the command was entered. There are several
PRGM commands which will specify a certain
launch point to be displayed.
launch point.
• In-Range time remaining for current launch
point.
• TTG to In-Zone for current launch point.
• In-Zone time remaining for current missile
•
•
•
•
•
•
•
•
event.
Steering cue to In-Range for current missile
event.
Steering cue to In-Zone for current missile
event.
Missile Time on Target (TOT).
Seeker retained indicator.
Safe launch advisories.
Manual launch required, or LCD status.
Identification and launch status of missile(s)
associated with current launch point.
SMO identified mission event indicator.
Selected Destination Program Display (PRGM-nn)
Operator entry of PRGM-nn, where nn represents
destination nn, will cause the Program Display for
the specified carrier destination to be displayed on
the selected MFD.
Direct Target Program Display (PRGM-Dn)
Operator entry of PRGM-Dn, where n represents a
direct target number n, will cause the Program Display for the specified direct target to be displayed
on the selected MFD This will initiate ranging on
missile Dn. The SMO will reject a PRGM-Dn command and display it in reverse highlight if any of
the following conditions exist:
• n is not a valid direct target number.
• No missiles are assigned to the designated direct target.
JASSM SMO Program Commands
COMMAND
DESCRIPTION
PRGM
Program Display Request
PRGM-nn
Target Selection Command for JASSM Target nn
PRGM-Dn
Target Selection Command for Direct Target n
Figure 1-35
1-74
T.O. 1B-52H-34-2-8
PROGRAM DISPLAY (PRGM)
[AMI]
PMD
1 CP A
D
2
2
2
2
4
10
2
3
5
11
2
1
PTA
6
12
7
13
14
16
D
8
9
15
D
E TE
1
PTA
− − PRGM−
A75619
Less [AMI]
Figure 1-36 (Sheet 1 of 6)
Change 3
1-75
T.O. 1B-52H-34-2-8
PROGRAM DISPLAY (PRGM) (Cont)
WINDOW
1
DISPLAY
Destination Type
MODIFIABLE
NO
JASSM LP
2
3
4
Direct Target
Number
FUNCTION
SMO identified destination type. Current or next destination is a JASSM
Launch Point.
NO
Dn
A missile is assigned to the direct target n, it has not been released and
the direct target is not in range. n = 1 to 6.
Dn (BrightUnderlined Video)
A missile is assigned to the direct target n, it has not been released and
the direct target is in range.
(blank)
No missile is assigned to the direct target n or the assigned missile has
been released.
Current Event
Number
NO
LPnn
Current event is JASSM launch point number. nn = _1 to 99.
Dn__
Current event is JASSM Direct Target point number. Dn = D1 to D6.
(blank)
No launch point or direct target selected.
Location/Station
NO
xy
Location and station of each missile (displayed in preferred launch sequence) assigned to the current launch point that is targeted and ready for
launch.
x = L for left pylon stations and R for right pylon stations.
y = Station number 1, 2, 3, 6, 7 or 8.
5
xy (Normal Blinking
Video)
Location and station of each missile assigned to the current launch point that
cannot be launched because power is not applied or targeting has not been
completed.
xy (Bright Underlined
Video)
Location and station of each missile assigned to the current launch point that
is ready for launch and is In-Range.
xy (Reverse
Video)
Location and station of each missile assigned to the current launch point that
cannot be launched due to a WIU, AIU, or missile fault.
(blank) (Reverse
Video)
Displayed once for each missile that is required for the selected target by
mission data, but no missile is assigned.
(blank) (Normal Video)
The missile that was displayed in this MFD area was launched or missile not
assigned to this launch point or direct target.
In-Range Status
NO
RANGE (Bright
Underlined Video)
The missile currently indicates In-Range.
TTG-R
The missile currently indicates not In-Range but is achievable.
TTG-R (Reverse
Video)
The missile currently indicates not In-Range and In-Range not
achievable, or is not targeted.
(blank)
No selected launch point.
Figure 1-36 (Sheet 2 of 6)
1-76
Change 3
T.O. 1B-52H-34-2-8
WINDOW
DISPLAY
MODIFIABLE
6
Time-to-Go to In-Range
NO
7
8
9
FUNCTION
mm:ss
Time-to-Go (TTG) to In-Range. The time in minutes and seconds required
for the aircraft to reach a point that is within range of the target if the aircraft
maintains current ground speed, altitude, and ground track. Maximum value
is 59:59 if greater than 1 hour.
mm:ss (Reverse
Video)
The missile is unable to provide valid In-Range data, [AMI] launch is inhibited or aircraft is inside min range circle. Number displayed is based on the
last valid data, or 59:59 if greater than 1 hour.
00:00
Aircraft is In-Range.
(blank)
In-Range is not achievable, or no selected launch point.
(blank) (Reverse
Video)
Invalid data. [AMI] Not ranging and weapon not able to provide in-range
data.
In-Range Remaining
Time
NO
mm:ss
Remaining In-Range time in minutes and seconds if the aircraft maintains
current ground speed, altitude, and ground track. Maximum value is 59:59
if greater than 1 hour.
mm:ss (Reverse
Video)
The missile is unable to provide valid In-Range data, [AMI] launch is inhibited or aircraft is inside min range circle. Number displayed is based on the
last valid data, or 59:59 if greater than 1 hour.
(blank)
In-Range is not achievable, or no selected launch point.
(blank) (Reverse
Video)
Invalid data. [AMI] Not ranging and weapon not able to provide in-range
data.
TOT Label
NO
TOT
The TOT label is displayed when JASSM ranging is active.
TOT (Bright, Underlined Video)
Mission requires Time on Target.
(blank)
Ranging is not active or Less [AMI] no missile time of flight is being received from the missile.
Missile Time on Target
NO
hh:mm:ss
Missile Time on Target (TOT) determined by adding the current UTC and
the time of flight data from the weapon (00:00:00 to 23:59:59).
hh:mm:ss
(Reverse Video)
Missile unable to provide valid Time of Flight data or [AMI] or launch is
inhibited. The number displayed is based on the last valid data.
(blank)
No missile time of flight is being received from the missile.
Figure 1-36 (Sheet 3 of 6)
Change 2
1-77
T.O. 1B-52H-34-2-8
PROGRAM DISPLAY (PRGM) (Cont)
WINDOW
10
11
12
13
DISPLAY
In-Range Track
Indicator
MODIFIABLE
FUNCTION
NO
→
The aircraft is not on track and needs to steer to the right in order to
achieve In-Range for the selected direct target.
←
The aircraft is not on track and needs to steer to the left in order to
achieve In-Range for the selected direct target.
(blank)
The aircraft is on track to achieve In-Range or the aircraft is past the
point of closest approach for In-Range or no selected direct target event.
In-Zone Status
NO
TTG-Z
The missile currently indicates not In-Zone but is achievable.
TTG-Z (Reverse
Video)
The missile currently indicates not In-Zone and In-Zone unachievable, or
the missile is not targeted.
ZONE (Bright
Underlined Video)
The missile currently indicates In-Zone.
(blank)
No selected launch point, (Less [AMI] launch point has no waypoints) or
direct target is active event.
Time-to-Go to In-Zone
NO
mm:ss
The time in minutes and seconds required for the aircraft to reach a point
that is within zone of the first waypoint if the aircraft continues flying
towards the first waypoint at the current ground speed, altitude, and
ground track. This condition is termed Time-to-Go (TTG) to In-Zone.
Maximum value is 59:59 if greater than 1 hour.
mm:ss (Reverse
Video)
The missile is unable to provide valid In-Zone data. Number indicated is
based on the last valid data or 59:59 if greater than 1 hour.
00:00
Aircraft is In-Zone.
(blank)
In-Zone is not achievable, or no selected launch point.
(blank) (Reverse
Video)
Invalid data. [AMI] Not ranging and weapon unable to provide valid in-zone
data.
In-Zone Remaining
Time
NO
mm:ss
Remaining In-Zone time in minutes and seconds if the aircraft maintains
current ground speed, altitude, and ground track. Maximum value is
59:59 if greater than 1 hour.
mm:ss (Reverse
Video)
The missile is unable to provide valid In-Zone data. Number displayed is
the last valid time or 59:59 if greater than 1 hour.
(blank)
In-Zone is not achievable, or no selected launch point.
(blank) (Reverse
Video)
Invalid data. [AMI] Not ranging and weapon unable to provide valid in-zone
data.
Figure 1-36 (Sheet 4 of 6)
1-78
Change 2
T.O. 1B-52H-34-2-8
WINDOW
14
DISPLAY
Safe Release and
Weapon Launch
Advisories
MODIFIABLE
FUNCTION
NO
Safe release and weapon launch advisories are shown below in the order of
highest priority.
Weapon Launch
Advisories:
CLIMB (Blinking, Bright
Underlined Video)
Aircraft altitude is at, below, or within 500 feet of the minimum altitude for
release. Applicable when the aircraft is In-Zone or In-Zone is achievable.
ACCEL (Blinking, Bright
Underlined Video)
Aircraft speed is at, below, or within 0.02 Mach of the minimum Mach for
release. Applicable when the aircraft is In-Zone or In-Zone is achievable.
DIVE (Blinking, Bright
Underlined Video)
Aircraft altitude is at, above, or within 500 feet of the maximum altitude for
release. Applicable when the aircraft is In-Zone or In-Zone is achievable.
DECEL (Blinking, Bright
Underlined Video)
Aircraft speed is at, above, or within 0.02 Mach of the maximum Mach for
release. Applicable when the aircraft is In-Zone or In-Zone is achievable.
HDG TOL
(Blinking Video)
Current aircraft heading is within 6° to 9° of heading tolerance limits.
Applicable when the aircraft is not In-Zone, but In-Zone is achievable.
HDG TOL (Blinking,
Bright Video)
Current aircraft heading is within 3° to 6° of heading tolerance limits.
Applicable when the aircraft is not In-Zone, but In-Zone is achievable.
HDG TOL (Blinking,
Bright Underlined
Video)
Current aircraft heading is within 3° or outside of heading tolerance limits.
Applicable when the aircraft is not In-Zone, but In-Zone is achievable.
TRN LEFT
(Blinking Video)
Aircraft heading is within 6° to 9° of the right heading tolerance limit for release. (Turn LEFT to correct.) Applicable when the aircraft is In-Zone only.
TRN LEFT
(Blinking, Bright Video)
Aircraft heading is within 3° to 6° of the right heading tolerance limit for release. (Turn LEFT to correct.) Applicable when the aircraft is In-Zone only.
TRN LEFT (Blinking,
Bright Underlined
Video)
Aircraft heading is within 3° or outside of the right heading tolerance limit
for release. (Turn LEFT to correct.) Applicable when the aircraft is In-Zone
only.
TRN RIGHT
(Blinking Video)
Aircraft heading is within 6° to 9° of the left heading tolerance limit for release. (Turn RIGHT to correct.) Applicable when the aircraft is In-Zone only.
TRN RIGHT
(Blinking, Bright Video)
Aircraft heading is within 3° to 6° of the left heading tolerance limit for release. (Turn RIGHT to correct.) Applicable when the aircraft is In-Zone only.
TRN RIGHT (Blinking,
Bright Underlined
Video)
Aircraft heading is within 3° or outside of the left heading tolerance limit for
release. (Turn RIGHT to correct.) Applicable when the aircraft is In-Zone
only.
(blank)
No weapon launch advisories exist or no selected launch point.
Safe Release
Advisories:
Safe release advisories do not inhibit launch. Possible collision
between weapons and between weapon and aircraft can occur
if weapon is launched with a release advisory displayed.
ROLL
Aircraft roll angle and/or roll rate is too high for safe launch.
PITCH
Aircraft pitch angle and/or pitch rate is too high for safe launch.
LEVL_OFF
Aircraft vertical velocity and/or vertical acceleration is too high for safe
launch.
YAW
Aircraft yaw rate is too high for safe launch.
(blank)
No safe release advisories exist or no selected launch point.
Figure 1-36 (Sheet 5 of 6)
1-79
T.O. 1B-52H-34-2-8
PROGRAM DISPLAY (PRGM) (Cont)
WINDOW
15
16
17
DISPLAY
Seeker Status
MODIFIABLE
FUNCTION
NO
SKR (Reverse
Video)
The missile mission requires seeker and either a terminal guidance fault exists or the missile has no seeker.
(blank)
The missile has seeker guidance capability.
Countdown/Manual
Launch Indicator
NO
MAN LNCH REQ
(Bright Video)
Manual launch required for missile assigned to current launch point.
COUNTDOWN n
(Bright Video)
In LCD. n = TTG to launch ranging from 2 down to 0.
(blank)
Not in LCD and not in manual launch mode or no selected launch point.
CLR-D=EXIT DIR TGT
MODE Less [AMI]
NO
Displayed when Direct Target mode selected.
Figure 1-36 (Sheet 6 of 6)
1-80
Change 3
T.O. 1B-52H-34-2-8
Normal Aircrew Procedures
table of contents
section II
page
GENERAL
2-3
PREFLIGHT PROCEDURES
2-3
BEFORE EXTERIOR INSPECTION (POWER OFF) (RN/N)
2-3
EXTERIOR INSPECTION (POWER OFF) (RN/N)
2-3
AFTER ENGINE START (AIRCRAFT POWER AND COOLING AIR AVAILABLE)
MISSILE CHECK (RN/N)
INFLIGHT PROCEDURES
2-7
2-7
2-9
AFTER TAKEOFF (RN/N)
2-9
MISSILE POWER APPLICATION (N)
2-9
MISSILE TARGETING PROCEDURES (RN-N)
2-10
MISSILE/TARGET ASSIGNMENT (MANUAL TARGETING) PROCEDURES
2-10
DIRECT TARGETING DEFINITION DATA ENTRY PROCEDURES
2-13
LAUNCH PROCEDURES
2-17
MISSILE PREPARATION FOR LAUNCH (RN-N)
2-17
MISSILE LAUNCH PROCEDURES
2-18
BEFORE LAUNCH CHECK (RN)
2-18
AUTOMATIC MISSILE LAUNCH CHECKLIST (RN-N)
2-19
MANUAL MISSILE LAUNCH CHECKLIST (RN-N)
2-20
POST STRIKE/ABORT PROCEDURES
2-22
POST STRIKE/ABORT (RN/N)
2-22
AFTER LANDING PROCEDURES
2-23
GROUND SAFEING PROCEDURES (RN-N)
2-23
2-1/(2-2 blank)
BLA
T.O. 1B-52H-34-2-8
GENERAL
Detailed normal operating procedures for the
AGM-158 JASSM are contained in this section. The
procedural checklists are grouped in PREFLIGHT
PROCEDURES, AFTER ENGINE START (Power
and Cooling Air Available), INFLIGHT PROCEDURES, and AFTER LANDING PROCEDURES
subsections.
The step procedures are the call-response type in
which code letters appear after each response to indicate which member of the crew is to accomplish
that step. Identification symbols are used after each
response, except when the entire checklist is accomplished by a single crewmember, such as pilot or
navigator. Code letters are as follows: (P) pilot, (CP)
copilot, (N) navigator, and (RN) radar navigator.
NOTE
[AMI] On missions with mixed weapons loads, the JASSM SMO must be
loaded and selected as the primary SMO in order to power, align, target,
range and launch JASSMs.
PREFLIGHT PROCEDURES
BEFORE EXTERIOR INSPECTION (POWER OFF) (RN/N)
1. Jettison Power & Jettison Control Circuit Breakers – Out
2. Pilot’s Munitions Consent Panel: (RN)
a. LOCK-UNLOCK Switch – Guard closed
3. Weapon Control Panel: (N)
a. WPN JETTISON Switch – Guard closed
b. NUCLEAR LOCK-UNLOCK Switch – Guard closed
4. Alternate Jettison Control Panel: (N)
a. PYLON POWER Switch – OFF, Guard closed
b. POWER Light – Off
5. Proceed to aircraft EXTERIOR INSPECTION (POWER OFF) checklist (RN/N)
EXTERIOR INSPECTION (POWER OFF) (RN/N)
NOTE
• If any discrepancies are found, notify munitions personnel.
• Accomplish step 1 for each loaded HSAB, step 2 for each loaded
MAU-12, and step 3 for each missile.
1. External Heavy Stores Adapter Beam & Pylon General Condition – Checked
Check the general condition of the pylon for surface damage. Check pylon and HSAB fairings are
installed, the relay access door is fastened, and the pylon is configured for ICSMS.
Change 2
2-3
T.O. 1B-52H-34-2-8
EXTERIOR INSPECTION (POWER OFF) (RN/N) (Cont)
2. MAU-12 (Each missile Loaded Station):1.
a. Inflight Safety Lockout Pin Hole – Bolt and nut installed
b. Sway Braces & Ejector Feet – Seated and locked
Check sway brace lockout is tight and both ejector feet are against the missile.
c.
Ground Safety Lock Pin(s) – Removed, counted, and stowed
There should be one pin per missile.
If undue resistance is encountered when removing a lockpin, cease further action and call munitions personnel.
d. Sensing Switch Plunger – Checked
MAU-12 EJECTOR RACK
3. JASSM Missiles Checked :
The following steps should be accomplished for each missile. 2.3.
a. Leading Edge of Wings – Undamaged
b. Missile Skin – Smooth and undamaged
c. Missile Outer Coating – Undamaged
Accept or reject based on mission requirements.
d. Exhaust Nozzle – Undamaged and unobstructed
2-4
T.O. 1B-52H-34-2-8
e. Tail Fin Assembly – Undamaged and secure
f. IR Window – Checked
No visible scratches, cracks, or dirt.
g. Air Data Probe & Static Port Plate – Checked
No dents or obstructions.
h. Missile 1760 Umbilical Connector – Connected between pylon and missile
i. Umbilical Restraint – Closed, Cam lock fastener secure.
j. Umbilical Lanyard – Quick release pin inserted in B hole
2-5
T.O. 1B-52H-34-2-8
EXTERIOR INSPECTION (POWER OFF) (RN/N) (Cont)
With WIU power applied, extremely high
temperatures exist on the air data probe
and static port plate.
2-6
T.O. 1B-52H-34-2-8
AFTER ENGINE START (Aircraft Power and Cooling Air Available)
MISSILE CHECK (RN/N)
NOTE
For proper operation, the JASSM requires GPS almanac data to be less than two
weeks old to be considered valid. Since the primary source of almanac data for
the missile is the B-52 GPS Interface Unit, which retrieves the data from the GPS
receiver’s non-volatile memory, the crew should ensure that the GPS receiver
contains the current almanac data prior to applying missile power (28 vdc #1)
to any JASSM missile. If the GPS almanac data age is unknown, or the GPS IU
has not been operated within the last two weeks, the crew should accomplish
steps 1 through 4.
1. GPS Power – On (if required) (N)
Apply power to the GPS and GPS IU in accordance with GPS Power Turn-on in OAS, EVS, and
RADAR TURN-ON CHECKLIST of T.O. 1B-52H-1-12.
Wait a minimum of 12.5 minutes after the receiver indicates tracking of satellites. This allows the receiver to complete the initialization process and store current almanac data in its non-volatile memory.
2. GPS Power – Cycle (if required per Note above) (N)
Cycle GPS IU power. This causes the IU to retrieve the almanac data from the GPS receiver.
3. GPS Crypto Keys – Load (if required) (N)
Load weekly crypto keys into the IU in accordance with GPS Initialization OAS, EVS, AND RADAR
TURN-ON CHECKLIST of T.O. 1B-52H-1-12.
4. Less [AMI] JASSM SMO – Reload (CF-62,n) (if required) (N)
4. [AMI] JASSM SMO – Reload (CF-62) (if required) and checked primary (N)
5. PKB KEYS Indication – KEYS PRESENT (N)
Ensure keys are validated by observing the PRESENT indication on the PKB.
6. Simulation Mode (CF-52 or [AMI] CF-51) – Entered (if applicable) (N)
The system must be in STRIKE (CF-50) mode to enter simulation mode.
7. MISSILE LNCH MODE Switch – As briefed (N)
8. FRMT-7 – Entered
Change 2
2-7
T.O. 1B-52H-34-2-8
MISSILE CHECK (RN/N) (CONT)
9. OAS Power Control Panel MIU/LP & MIU/RP Power Switches – ON
Apply WIU power to missile loaded locations.
• Due to overheating of the Non-Interruptible Direct Current (NDC) power sup-
ply, WIU operation on the ground without cooling air being supplied directly to
the right wing root is limited to 2 minutes.
• To reapply WIU power on the ground without cooling air being supplied to
the right wing root, a minimum cool down period (power off) of 20 minutes
is required between power applications.
Status windows for each missile will be blank before WIU power is turned ON and, while WIU
power is ON, will show weapon type as M1 and status of OF (off).
10. WCP Location/Station (Missile Loaded Stations) – Selected
11. WCP Weapon Power Switch – ON
12. Missile Type – Checked (all missiles)
13. WIU & Ejector Faults Not Present – Checked
14. WCP Location/Station (Missile Loaded Stations) – Selected
15. WCP Weapon Power Switch – OFF
16. OAS Power Control Panel MIU/LP & MIU/RP Power Switches – Off
2-8
T.O. 1B-52H-34-2-8
INFLIGHT PROCEDURES
AFTER TAKEOFF (RN/N)
1. OAS Power Control Panel MIU/LP & MIU/RP Power Switches – ON (if required)
Applying WIU power (without JASSM weapon power) with the JASSM SMO loaded provides 115
VAC anti-ice heater power to the JASSM.
Without proper warm-up time, icing can degrade the missile pitot-static system such that mission failure could occur. Ensure the JASSM heater power is
applied (WIU ON) at least 15 minutes prior to launch. If icing conditions are
encountered prior to 15 minutes of heater operation, then a minimum warmup time of 30 minutes is required prior to launch.
MISSILE POWER APPLICATION (N)
1. [AMI] JASSM SMO – Primary (CF-62x), if not previously accomplished.
NOTE
The prime OAS navigation mode must be GPS-aided inertial, Doppler-aided
inertial, or free inertial prior to missile power application. If the alternate
navigation model is commanded as prime during missile alignment, JASSM
missile alignment is interrupted, weapon power is removed and a corresponding xy:COMM NOGO JASSM master fault is displayed for each missile.
2. Missile Status Check: (N)
a. FRMT-7 – Entered
NO KEYS, in reverse video, is displayed in the Crypto Key Status until validated during initialization.
b. OAS Power Control Panel MIU/LP & MIU/RP Power Switches – ON
Ensure WIU power is available to missile loaded locations.
c.
Missile Type – Checked (all missiles)
Status windows for each missile will be blank before WIU power is turned ON and, while WIU
power is ON, will show WEAPON TYPE as M1 and WEAPON STATUS of OF (off).
d. WIU & Missile Faults Not Present – Checked
Check for missile related faults; transient faults are possible.
Change 2
2-9
T.O. 1B-52H-34-2-8
MISSILE POWER APPLICATION (Cont)
3. Weapon Control Panel:
a. Desired Location(s) – Selected
b. Desired Station(s) – Selected
c.
WPN PWR Switch – ON
The WEAPON TYPE on FRMT-7 shows M1 for the missile and the WEAPON STATUS changes
from OF to ON. The WEAPON/GPS STATUS changes from WU to BT (IBIT) to IN and then to
MG. It may take up to 13.5 minutes after WIU power application for warmup to complete. IBIT
will not begin until warmup is complete. See Section VII for warmup and IBIT times. Following
IBIT, WEAPON STATUS changes from ON to GO.
NOTE
Exposure of the JASSM to ambient skin temperatures below –49° F (–45° C)
may result in weapon BIT [FAIL] indications and/or missile failures. Refer to
JASSM LOW TEMPERATURE OPERATIONS, Section VI.
4. Missile Auto Targeting – Checked
a. [AMI] AUTO TGT (CF-58) – Checked ON
b. FRMT-7 – Entered
When a missile has been assigned to a launch point number and targeting has been initiated, the
status changes from blank to nn (nn = JASSM launch point number 1 to 99), and is displayed in bright
video. Once targeting data has been loaded and verified nn changes to bright underlined video. Mission group number changes from blank to a (where a = A to F).
MISSILE TARGETING PROCEDURES (RN-N)
NOTE
• Upon completion of missile warm up, the automatic targeting process can
take up to 24 minutes (2 minutes per missile) and cannot be interrupted.
• An in depth discussion of missile targeting procedures is contained in Section VII.
MISSILE/TARGET ASSIGNMENT (MANUAL TARGETING) PROCEDURES
NOTE
• A CF-DE command can be entered to abandon the manual targeting operation
at any time. When a CF-DE command is entered, the manual targeting operation
is terminated, and all associated targeting displays will remain displayed and
updated. Data modification will be inhibited. The targeting availability status
for each location/station will continue to be displayed. All remaining windows
will be blank.
• The manual targeting operation is active from the time that a valid CF-586 com-
mand is entered until a CF-DE command is entered or until the manual targeting
display is replaced by another display on all MFDs where the manual targeting
display is selected. A CF-DD command will not terminate the manual targeting
operation. When the selected missiles have been targeted following a CF-DD
command, another or the same launch point can be selected for manual targeting
by entering a MDFY-1 command and repeating this process.
• Only one manual targeting process may be active at a time. Use caution when
modifying the same manual target on multiple screens, as data input by one operator can be overwritten by the other operator.
2-10
Change 3
T.O. 1B-52H-34-2-8
1. MISSILE LNCH MODE Switch – MAN
2. CF-586 – Entered
Upon entry of a valid CF-586 command, the CF-586 display will be presented on the selected MFD.
The location and station of each missile that is present will be displayed on MFD. The column
locations are assigned from left to right across the screen in the preferred launch sequence (figure
2-1). The video mode of the field indicates the missile’s targeting availability status. This status is
continually updated while the manual targeting display is present on an MFD.
3. MDFY-1 – Entered
Enter MDFY-1 to copy line 1 to the MFD command line for modification.
The information contained on line 1 will be copied to the MFD command line as:
1 LAUNCH POINT (1 - 99) nn MISSION GROUP (A–F) a
NOTE
Modifiable fields are shown in boldface for convenience, but are highlighted
as defined when displayed on the MFD.
4. Desired JASSM Launch Point Number, nn, & Desired Mission Group Identifier, a – Entered
Key in JASSM Launch Point Number, nn (nn = 01 to 99), and Mission Group identifier, a (a = A to F).
After the desired data is keyed in, press the ENTER key.
5. MDFY-6 – Entered
6. Location/Station of Missile to be Retargeted – E or 0 entered (as required)
Location/Station Selection Status on Missile/Target Assignment Display indicates an E to reflect
missile selected and an 0 to reflect missiles not selected.
Entry of CF-586 and selection of a JASSM does not prevent that missile from
being launched at the target to which it was previously assigned if the missile
is in LAR prior to a CF-DD command.
NOTE
If more than one weapon is selected, all selected weapons will have ranging
inhibited, until corrected by the operator. The operator should either correct
the desired missile entry, using CF-DE, or leave the CF-586 screen to remove
the inhibit.
7. CF-DD – Entered
If the missile selected is the missile to be targeted enter CF-DD to initiate the transfer of the targeting data to the selected missiles.
8. FRMT-12 – Entered
Determine if the selected missiles are to receive the targeting data associated with the designated
missile launch point and mission group. This is done by viewing each location/station displayed in
combination with the corresponding missile selection indicator. The possible display combinations
and the Select/Deselect process are described in Section VII.
9. FRMT-7 – Entered
When a missile has been assigned to a JASSM launch point number and retargeting has been initiated, the status changes from blank to nn (nn = JASSM launch point number 1 to 99), and is displayed in bright video. Once retargeting data has been loaded and verified, nn changes to bright
underlined video. Mission group identifier a (where a = A to F) changes to bright video.
2-11
T.O. 1B-52H-34-2-8
Missile Preferred Launch Sequence
If there is a retained/HUNG center station store, launching/jettisoning an adjacent shoulder station may result in a Store-to-Store Contact. When a center
station store is retained/HUNG, operators will retain the adjacent shoulder
station stores.
Figure 2-1
2-12
T.O. 1B-52H-34-2-8
DIRECT TARGETING DATA ENTRY PROCEDURES
NOTE
• To perform the direct targeting operation, the Direct Target Definition Display (CF-588,n) must be displayed on the selected MFD.
• Only one direct target may be modified at a time. Use caution when modifying
the same direct target on multiple screens, as data input by one operator can be
overwritten by the other operator.
• A CF-DE command can be entered to exit the direct target definition opera-
tion without downloading data to the missile at any time prior to entry of a
CF-DD command. When a CF-DE command is entered, the direct target definition operation is terminated, data modification is inhibited, and the specified direct target number will remain displayed on the top of the MFD. The
targeting availability status for each location/station will continue to be statused. All remaining windows are blanked. The direct target data will not be
saved if a CF-DE command is entered. The previous direct target data is
maintained.
• Performing direct targeting for an already targeted weapon while CDE is in
progress will result in a misleading FRMT-7 display. Allow the CDE to complete, then recommand the desired targeting operation after re-powering on
the weapon.
1. MISSILE LNCH MODE Switch – MAN
2. CF-588,n – Entered
n (1 to 6) is the number of the direct target to be defined.
3. MDFY-1 – Entered
The information contained on line 1 is copied to the MFD command line as follows:
1 TGT PT addomm.mmmm adddomm.mmmm fffff’ Less [AMI] r
NOTE
Modifiable fields are shown in boldface for convenience, but are highlighted
as defined when displayed on the MFD.
4. Desired Target Point Latitude, Longitude, Elevation, Less [AMI] and Elevation Reference – Entered
addomm.mmmm is the target latitude in degrees, minutes, and ten-thousandths of a minute. a =
N for North and S for South. dd = degrees from 0 to 90. mm.mmmm = minutes from 00 to 59 and
ten-thousandths of a minute from 0000 to 9999.
adddomm.mmmm is the target longitude in degrees, minutes, and ten-thousandths of a minute. a
= E for East and W for West. ddd = degrees from West 180 to East 179. mm.mmmm = minutes from
00 to 59 and ten-thousandths of a minute from 0000 to 9999.
fffff is the target point elevation in feet (MSL Less [AMI] or HAE). Input ranges from –328 to 32810
feet.
Less [AMI] r is the target elevation reference. Valid input is 0 or 1. 0 represents a measurement
of MSL for the target point elevation while 1 indicates HAE.
The entered latitude, longitude, elevation, and Less [AMI] target elevation reference will be displayed on line 1.
Change 3
2-13
T.O. 1B-52H-34-2-8
DIRECT TARGETING DATA ENTRY PROCEDURES (Cont)
5. MDFY-2 – Entered
The information contained on line 2 is copied to the MFD command line as:
2 CRUISE ALT fffff’
6. Desired Cruise Altitude – Entered
fffff is the desired cruise altitude in feet MSL. Valid input range is from 0 to 45000 ft. Prior to
operator entry the default value of 99999 (representing 15000 ft) is displayed.
The entered cruise altitude is displayed on line 2.
7. MDFY-3 – Entered
The information contained on line 3 is copied to the MFD command line as:
3 BRNG TO TGT bbb° IMPACT ANGLE dd°
8. Desired BRNG TO TGT & Impact Angle – Entered
bbb° is the missile’s Bearing to Target in degrees. Valid input range is from 0 to 360 degrees true
(0 = North) or 999. The default value of 999 is displayed prior to operator entry. The default value
indicates the missile will determine it’s bearing to target from the aircraft to the target at time of
launch.
NOTE
If 360 is entered by the operator, the resulting display will be 0.
dd° is the desired impact angle for the missile. Valid input range is from 0 (level) to 90 (vertical)
degrees, however, the missile will only use an impact angle ranging from 20 to 70 degrees. The
default angle of 60° is displayed prior to operator input.
NOTE
If less than 20 degrees is entered on CF-588, the missile will use a built-in
minimum impact angle value of 20 degrees. The missile will use a built-in
maximum value of 70 degrees, if more than 70 degrees is entered on CF-588.
FRMT-12 displays the impact angle actually being used by the missile. While
in SIM mode, the FRMT-12 impact angle displayed is the same as the CF-588
value input.
The entered Range on Bearing and Bearing to Target is displayed on line 2.
9. MDFY-4 – Entered
The information contained on line 4 is copied to the MFD command line as:
4 FUZE MODE n XXXX
10. Desired Fuze Mode Identifier – Entered
n is the missile’s fuze impact setting. Valid inputs for fuze mode are 1 (Soft Impact) and 2 (Hard
Impact). The default value of 1 will be displayed prior to operator entry.
The entered fuze mode will be displayed on line 4. The corresponding fuze mode of SOFT or HARD
will also be displayed.
2-14
T.O. 1B-52H-34-2-8
DIRECT TARGETING DATA ENTRY PROCEDURES (Cont)
11. MDFY-5 – Entered
The information contained on line 5 is copied to the MFD command line as:
5 FUZE DELAY n (0-7)
12. Desired Fuze Delay – Entered
n is a single digit that corresponds to the
missile’s fuze delay in milliseconds. Valid
input values for fuze delay are 0 through 7.
The millisecond delay corresponding to the
number is listed in the figure to the right.
VALID ENTRIES
MILLISECOND DELAY
0
0
1
10
2
15
3
20
4
30
5
40
6
50
7
120
Select/Deselect Missile(s) to be assigned to the designated target as follows:
13. MDFY-6 – Entered
The information contained on line 6 is copied to the MFD command line.
14. Missiles – Selected
For each missile that is to be selected, overwrite the 0 with an E. For each missile that is to be
deselected, overwrite the E with a 0. Selected missiles are not assigned to a direct target until a
CF-DD command is entered.
NOTE
If more than one weapon is selected, all selected weapons will have ranging
inhibited, until corrected by the operator. The operator should either correct
the desired missile entry, using CF-DE, or leave the CF-586 screen to remove
the inhibit.
If more than one missile is selected, the difference is displayed in the Missiles Selected window as
a negative number in reverse video. If fewer missiles were selected than required, the difference is
displayed in normal video. The contents of the display will be updated to show which missiles are
assigned.
If more missiles are selected than required, the least preferred missiles will be deselected by the SMO
to reduce the number of missiles selected to the number of missiles required for the designated target
when a CF-DD command is entered. The data is updated with a 0 displayed in normal video, and will
then be updated to show which missiles are assigned.
2-15
T.O. 1B-52H-34-2-8
DIRECT TARGETING DATA ENTRY PROCEDURES (Cont)
15. CF-Dn Direct Target Copy – Entered (if required)
Copy direct target information to direct target, as required.
16. CF-DD – Entered
If no other missile is to be selected, enter CF-DD to save the direct target data and initiate the
downloading of the targeting data to the selected missile.
NOTE
If no missiles are selected and a CF-DD command is entered, the data for the
designated direct target is saved, but the direct target will not be defined.
Selected missile is set as untargeted.
NOTE
Selected missile will no longer be targeted to its previous target.
The SMO will initiate the transfer of the targeting data to the selected missile. Selected missiles
that do not have power applied are assigned but not targeted. The order of selected missiles is based
on the preferred launch sequence.
Data modification is inhibited and associated targeting displays will remain displayed and updated
as follows:
LOADING is displayed in bright blinking video while the data is being downloaded to a missile.
The specified direct target number will remain displayed, The targeting availability status for each
location/station window will continue to be statused. All remaining windows are blanked out.
17. FRMT-7 – Entered, if desired
The targeting process of each selected missile can be monitored on the FRMT-7 display. The CF-588
display is updated as follows:
If the transfer of targeting data to all selected missiles completes successfully:
If direct targeting data is subsequently modified. an * will be displayed to the right of the
Mission Group Identifier.
COMPLT is displayed in normal video. The location/station of assigned missiles is displayed
in bright underline video in the appropriate window. All modifiable windows and the WPNS
TO SELECT window will be blank.
If the transfer of targeting data to any of the selected missiles completes unsuccessfully:
COMPLT is displayed in reverse video and a corresponding advisory/master fault message
is displayed to indicate which failure occurred. The location/station of each missile that was
not successfully targeted is displayed in reverse video in the appropriate window. Data will
remain displayed in all modifiable windows and in the WPNS TO SELECT windows. The
missile will retain the previously selected targeting data.
2-16
T.O. 1B-52H-34-2-8
LAUNCH PROCEDURES
MISSILE PREPARATION FOR LAUNCH (RN-N)
NOTE
• These checklists should be completed prior to the HEW, IP (high altitude
launch), or descent (low altitude launch).
• A transfer alignment maneuver is not required for JASSM operation.
1. Cabin Pressurization – COMBAT (if applicable) (CP)
2. Personal Locator Beacon Lanyards – Set as briefed (All)
3. Exterior Lights – As briefed (P)
4. Jettison Power & Jettison Control Circuit Breakers – In (RN)
5. Missile Status Check: (N)
a. FRMT-7 – Entered
b. Missile Targeting - Checked
A missile has been assigned to a launch point number and targeting has occurred, the status
displays nn or Dn (nn = JASSM launch point number 1 to 99, Dn = JASSM direct target number
D1 to D6), in bright underlined video. Mission group number displays an a (where a = A to F)
in bright video.
c.
Missile Status - Checked
The missile should be powered on and should indicate a GO status.
2-17
T.O. 1B-52H-34-2-8
MISSILE LAUNCH PROCEDURES
BEFORE LAUNCH CHECK (RN)
1. Fuel Transfer – Accomplished (if required) (RN, CP)
2. HAC/LAC – Cross checked
B-52 Operators must be aware that the Inertial/GPS aided munitions
use the transfer alignment data (latitude, longitude, altitude, etc.) of
the aircraft prime navigation model. Buffers are not incorporated/
transferred to the Inertial/GPS aided munitions. This navigation transfer applies to a prime navigation model with, or without, GPS aiding.
Failure to recognize this condition may result in weapons impacting
other than the intended target or failing to release due to LAR considerations. Refer to MAJCOM or Theater specific guidance for degraded
weapon release ROE.
3. Circuit Breakers – Checked (RN-N)
Check all lower deck circuit breakers. Ensure all release associated circuit breakers are in the proper
configuration for the planned launch.
4. Prime NAV Mode – Selected (RN)
5. MISSILE LNCH MODE Switch – MAN
6. Missile Launch – Review (All)
Review number of missiles and data for each missile including missile location, total time to launch
missile, run in heading, turn direction, altitude, airspeed, launch mode, and egress maneuver, if
applicable.
If there is a retained/HUNG center station store, launching/jettisoning an adjacent shoulder station may result in a Store-to-Store Contact. When a center
station store is retained/HUNG, operators will retain the adjacent shoulder
station stores.
NOTE
During In-Zone JASSM launch operations, it is highly recommended that
crews use the AUTO launch feature. The JASSM SMO incorporates an 8 second “look back” feature to preclude the system from falling into In-Range (i.e.,
a heading tolerance problem) just prior to launch. If the aircraft was In- Zone
during the 8 seconds prior to the at or abeam launch point, the weapon will
fly the planned In-Zone mission. If the missile was to fly an In-Range profile,
all preplanned autorouting data would be lost, as the missile determines it’s
own profile.
2-18
Change 1
T.O. 1B-52H-34-2-8
AUTOMATIC MISSILE LAUNCH CHECKLIST (RN-N)
1. Pilot’s Munitions Consent Panel LOCK/UNLOCK Switch – UNLOCK (P)
2. Master Fault Light – ON (RN)
3. WCP LOCK/UNLOCK Switch – UNLOCK (RN)
4. Master Fault Light – OFF (RN)
5. FLY-TO nn – Entered (as required)
6. Missile Status – GO (N)
7. PRGM – Entered (N)
a. Ranging – Monitor
Ranging is being performed for the current JASSM launch point.
b. TTG-Z – Monitor
TTG-Z (Time-To-Go to In-Zone) decreases to zero and changes to ZONE 00:00 in bright underlined video to indicate the missile is in zone. The time remaining In-Zone will be displayed in
the window immediately to the right of the ZONE 00:00, and will begin to decrease. In the
Automatic launch mode, the JASSM will begin launch countdown to launch at, or the closest
point of approach to, the planned launch point.
8. MISSILE LNCH MODE Switch – AUTO
• During a weapon launch, do not enter PRGM-Dn or CLR-D until the weapon
AWAY advisory has been displayed or the launch may be aborted.
• Switching the MISSILE LNCH MODE switch from AUTO to MAN during the
launch countdown may result in an ABORT.
9. Launch Countdown – Monitored (N)
NOTE
Launch will take 3.5 seconds maximum from countdown entry to AWAY.
10. Missile Status Indication – xy AWAY
xy AWAY is displayed for 5 seconds at the bottom of the MFDs.
11. Notify Crew – “Missile Away” (RN)
12. Egress Maneuver As Briefed – Called after release of the missile (N); Performed (P)
13. MISSILE LNCH MODE Switch – As required
2-19
T.O. 1B-52H-34-2-8
MANUAL MISSILE LAUNCH CHECKLIST (RN-N)
NOTE
Manual Launch is required if:
• The missile is targeted to a Direct Target.
• The missile has no waypoint data.
• The aircraft is beyond the closest point of approach and is still In-Zone.
1. Pilot’s Munitions Consent Panel LOCK/UNLOCK Switch – UNLOCK (P)
2. Master Fault Light – ON (RN)
3. WCP LOCK/UNLOCK Switch – UNLOCK (RN)
4. Master Fault Light – OFF (RN)
5. MISSILE LNCH MODE Switch – MAN
6. Missile Status – GO (N)
7. PRGM/PRGM Dn – Entered (N)
a. Ranging – Monitor
Ranging is being performed on the selected (PGRM or PGRM Dn) JASSM target event.
b. TTG-R – Monitor
TTG-R (Time-To-Go to In-Range) decreases to zero and changes to RANGE 00:00 in bright underlined video to indicate the missile is in range. The time remaining In Range will be displayed
in the window immediately to the right of the RANGE 00:00, and will begin to decrease. In the
Manual launch mode, JASSM launch of a GO missile can be commanded upon entering RANGE
00:00.
c.
TTG-Z – Monitor
TTG-Z (Time-To-Go to In-Zone) decreases to zero and changes to ZONE 00:00 in bright underlined video to indicate the missile is in zone. The time remaining In Zone will be displayed in
the window immediately to the right of the ZONE 00:00, and will begin to decrease. In the
Manual launch mode, JASSM launch of a GO missiles can be commanded upon entering ZONE
00:00.
Pressing the MAN LNCH switch more than once during step 8 may stop the
launch countdown and result in an ABORT.
8. MISSILE MAN LNCH Switch – Pressed
During a weapon launch, do not enter PRGM-Dn or CLR-D until the weapon
AWAY advisory has been displayed or the launch may be aborted.
9. Launch Countdown – Monitored (N)
NOTE
Launch will take 3.5 seconds maximum from countdown entry to AWAY.
2-20
T.O. 1B-52H-34-2-8
MANUAL MISSILE LAUNCH CHECKLIST (RN-N) (Cont)
10. Missile Status Indication – xy AWAY
xy AWAY is displayed for 5 seconds at the bottom of the MFDs.
11. Notify Crew – “Missile Away” (RN)
12. Egress Maneuver As Briefed – Called after release of missile (N); Performed (P)
2-21
T.O. 1B-52H-34-2-8
POST STRIKE/ABORT PROCEDURES
POST STRIKE/ABORT (RN/N)
NOTE
• Accomplish the following for mission abort when no further launches
are to be attempted.
• The MASTER CAUTION light will come on and remain on any time
there is a disagreement between the pilot and navigator unlock
switches.
1. Weapon Control Panel LOCK/UNLOCK Switch – LOCK (RN)
2. Master Fault Light – ON (RN)
3. Munitions Consent Panel LOCK/UNLOCK Switch – LOCK (P)
4. Master Fault Light – OFF (RN)
5. MISSILE LNCH MODE Switch – MAN
6. Jettison Power & Jettison Control Circuit Breakers – Out (RN)
7. FRMT-7 – Entered
8. LP & RP Location & ALL Station – Selected
9. Classified Data Erase (CF-575):
a. CF-575 – Entered
b. CLSF Data Erase Question – Answer YES
A CDE COMPLT ([AMI] JASSM CDE COMPLT) message will be displayed below each missile
on FRMT-7 and at the bottom of the MFD when classified data erase is complete. Missiles will
be automatically powered off.
10. Missile Status – Checked
Missile status should change to OF, alignment status and targeting status should be blank.
NOTE
If any JASSM remains aboard, but is not hung, delay step 11 until after landing.
11. MIU Power Switches – OFF
2-22
Change 2
T.O. 1B-52H-34-2-8
AFTER LANDING PROCEDURES
GROUND SAFEING PROCEDURES (RN-N)
Flight crew will notify ground crew personnel and will use caution regarding
potential hot spots on the missile at the air data probe and static plate. Contacting these hot spots with unprotected skin should be avoided. Required
cool down time is comparable to that for the aircraft pitot tubes.
NOTE
If missiles are retained on the aircraft and qualified maintenance personnel
are not available, missile release system safeing procedures must be accomplished by the navigator and radar navigator using the following checklist.
Do not apply power until ground safety lockpins are installed.
1. MAU-12 Ground Safety Lockpin(s) – Installed
2-23/(2-24 blank)
BLA
T.O. 1B-52H-34-2-8
Emergency Aircrew Procedures
section III
table of contents
page
INTRODUCTION
3-1
MISSILE JETTISON
3-2
SELECTIVE JETTISON USING THE WCP/SMO
3-3
SELECTIVE JETTISON USING THE AJCP
3-4
EMERGENCY JETTISON
3-5
NOTIFICATION PROCEDURES - DANGEROUS MATERIALS
3-6
FIREFIGHTING AND EVACUATION CRITERIA
3-7
INTRODUCTION
Emergency procedures listed in this section are specific to the JASSM. If a weapon malfunction or aircraft emergency occurs, contact a command authority, if necessary, and proceed as directed. If contact
cannot be made and jettison is required, see MISSILE
JETTISON checklists. The JASSM jettison envelope
is contained in Section V.
NOTE
When a JASSM is retained/HUNG it should
be monitored visually, if possible, until jettisoned or, if not jettisoned, it should be periodically monitored visually (when possible)
until after landing.
3-1
T.O. 1B-52H-34-2-8
MISSILE JETTISON
Missile Preferred Jettison Sequence
If there is a retained/HUNG center station store, launching/jettisoning an adjacent shoulder station may result in a Store-to-Store Contact. When a center
station store is retained/HUNG, operators will retain the adjacent shoulder
station stores.
Figure 3-1
3-2
T.O. 1B-52H-34-2-8
SELECTIVE JETTISON USING THE WCP/SMO
• The weapon SMO has no interlocks preventing jettison on the ground. With
unlock consent, and power applied to the OAS and the WIU, actuation of
Weapon Control Panel Jettison Select switch while the aircraft is on the
ground will result in jettison of the selected weapon(s).
• If there is a retained/HUNG center station store, launching/jettisoning an
adjacent shoulder station may result in a Store-to-Store Contact. When a
center station store is retained/HUNG, operators will retain the adjacent
shoulder station stores.
NOTE
Selective jettison using the WCP is the preferred method of jettison when
OAS is loaded and operating with the weapon SMO loaded [AMI] as the primary SMO.
1. Crew – Alerted (RN)
2. Command Authority – Contacted, if necessary (P)
3. Impact Area – Cleared (P-CP-RN)
Clear area visually and/or by radar to the maximum extent possible.
4. OAS Master Power – ON (N)
5. Processors – Loaded (N)
NOTE
The OAS and the JASSM SMO must be loaded ([AMI] as the primary SMO) and
operating to enable jettison.
6. [AMI] JASSM SMO – Primary (CF-62x) (N)
7. MIU Power Switches – ON (pylon location of weapon(s) to be jettisoned) (RN)
8. Pilot’s Munitions Consent Panel LOCK-UNLOCK Switch – UNLOCK (P)
9. Master Fault Light – ON (RN)
10. WCP Nuclear LOCK-UNLOCK Switch – UNLOCK (RN)
11. Master Fault Light – OFF (RN)
12. Location & Station Switches (Weapon(s) To Be Jettisoned) – Selected (RN)
13. Classified Data Erase (CF-575):
a. CF-575 – Entered
b. CLSF Question – Answer YES
A CDE COMPLT ([AMI] JASSM CDE COMPLT) message will be displayed below each weapon
on FRMT-7 and at the bottom of the MFD when classified data erase is complete. Missiles will
be automatically powered off.
14. Location & Station (Weapon(s) To Be Jettisoned) – Selected (RN)
15. WCP Jettison Select Switch – Select (1 second) (RN)
16. Jettison Monitored – Weapon(s) AWAY (RN)
17. WCP Nuclear LOCK-UNLOCK Switch – LOCK (RN)
18. Master Fault Light – ON (RN)
19. Pilot’s Munitions Consent Panel LOCK-UNLOCK Switch – LOCK (P)
20. Master Fault Light – OFF (RN)
Change 2
3-3
T.O. 1B-52H-34-2-8
SELECTIVE JETTISON USING THE AJCP
• The AJCP has no interlocks preventing jettison on the ground. With unlock
consent, and power applied to the aircraft, actuation of AJCP switches while
on the ground will result in weapon jettison.
• If there is a retained/HUNG center station store, launching/jettisoning an
adjacent shoulder station may result in a Store-to-Store Contact. When a
center station store is retained/HUNG, operators will retain the adjacent
shoulder station stores.
NOTE
• Selective jettison using the WCP is the preferred method of jettison if the
OAS is loaded and operating with the weapon SMO loaded [AMI] as the
primary SMO.
• If AJCP jettisons are commanded with OAS loaded and operating with the
weapon SMO loaded and the WIU(s) powered, the WIU will be powered off
by the OAS. An uncommanded EED power available fault will be displayed
by OAS.
1. Crew – Alerted (RN)
2. Command Authority – Contacted, if necessary (P)
3. Impact Area – Cleared (P-CP-RN)
Clear area visually and/or by radar to the maximum extent possible.
4. Pilot’s Munitions Consent Panel LOCK-UNLOCK Switch – UNLOCK (P)
5. Master Fault Light – ON (RN)
6. WCP Nuclear LOCK-UNLOCK Switch – UNLOCK (RN)
7. Master Fault Light – OFF (RN)
8. AJCP Pylon Power Switch (Location Of Weapon To Be Jettisoned) – LEFT or RIGHT selected (N)
POWER and STORES jettison light, PWR, will be on while the PYLON POWER Switch is in the
left or right position.
9. AJCP JETTISON Station Select Switch (Weapon To Be Jettisoned) – Actuated (N)
POWER and STORES jettison light, JET, will be on while the JETTISON Switch is in the left or
right position.
10. WCP Nuclear LOCK-UNLOCK Switch – LOCK (RN)
11. Master Fault Light – ON (RN)
12. Pilot’s Munitions Consent Panel LOCK-UNLOCK Switch – LOCK (P)
13. Master Fault Light – OFF (RN)
3-4
Change 2
T.O. 1B-52H-34-2-8
EMERGENCY JETTISON
• The pilots’ Bomb Bay & Missile Jettison Control switch jettisons all GWD and
active/primary SMO controlled weapons loaded on the aircraft and will only be
used as a backup to jettison by the Radar Navigator. If jettison is commanded
using the pilots’ Bomb Bay & Missile Jettison Control switch, all GWD weapons
and, with OAS operating and MIUs/WIUs powered, all active/primary SMO controlled weapons will be jettisoned. Proper separation clearance between weapons and between weapons and aircraft cannot be ensured.
• The JASSM SMO has no interlocks preventing jettison on the ground. With
unlock consent and power applied to the OAS and the WIU, actuation of the
pilots’ Bomb Bay & Missile jettison control switch while on the ground will
result in weapon jettison.
• If there is a retained/HUNG center station store, launching/jettisoning an
adjacent shoulder station may result in a Store-to-Store Contact. When a
center station store is retained/HUNG, operators will retain the adjacent
shoulder station stores.
1. Crew – Alerted (RN)
2. Command Authority – Contacted, if necessary (P)
3. Impact Area – Cleared (P-CP-RN)
Clear area visually and/or by radar to the maximum extent possible.
4. Jettison Control & Jettison Power Circuit Breakers (2) – In (RN/N)
5. OAS Master Power – ON (N)
6. Processors – Loaded (N)
NOTE
The OAS and the JASSM SMO must be loaded, [AMI] as the primary SMO, and
operating to enable jettison.
7. [AMI] JASSM SMO – Primary (CF-62x) (N)
8. MIU Power Switches – ON (pylon location of weapon(s) to be jettisoned) (RN)
9. Pilot’s Munitions Consent Panel LOCK-UNLOCK Switch – UNLOCK (P)
10. Master Fault Light – ON (RN)
11. WCP Nuclear LOCK-UNLOCK Switch – UNLOCK (RN)
12. Master Fault Light – OFF (RN)
13. Pilots’ Bomb Bay & Missile Jettison Switch - Pressed (momentarily) (P)
NOTE
After weapons have been released perform the following.
14. Jettison Monitored - Weapons AWAY (RN)
15. WCP Nuclear LOCK-UNLOCK Switch – LOCK (RN)
16. Master Fault Light – ON (RN)
17. Pilot’s Munitions Consent Panel LOCK-UNLOCK Switch – LOCK (P)
18. Master Fault Light – OFF (RN)
19. Jettison Control & Jettison Power Circuit Breakers (2) – Out (RN/N)
Change 3
3-5
T.O. 1B-52H-34-2-8
NOTIFICATION PROCEDURES –
DANGEROUS MATERIALS
Procedures for alerting the fire department and
other base support elements for aircraft carrying
dangerous materials are as follows:
DEFINITION OF TERMS
Definitions of some of the terms used in communications are as follows:
• Dangerous Materials: Any material that is
flammable, corrosive, an oxidizing agent, explosive,
toxic, radioactive, nuclear, unduly magnetic, or biologically infective or any other material that (because of its quantity, properties, or packaging) may
endanger human life or property.
• Firefighting Time: A period that begins when
the material becomes enveloped in flames and terminates when the material can be expected to detonate, deflagrate, or begin burning.
• Withdrawal Distance: The minimum permissible distance, between firefighters, rescue, and/or
nonessential personnel and the site of the accident
(fire/detonation), without protective barricades.
• Department of Transportation (DOT) Classifications: Classifications established by DOT for handling dangerous materials in transit. They define
classes of dangerous materials.
• Inert Devices: Devices containing no dangerous
material but closely resembling nuclear or explosive
items that are classified as dangerous.
• Net Explosive Weight (NEW): The actual (or
high explosive equivalent) weight of explosive substances contained within a munition/weapon to be
used when applying quantity – distance criteria or
other standards.
NORMAL NOTIFICATION PROCEDURES
It is the responsibility of the major command concerned to ensure that all required information is
transmitted to departure and destination (primary/
alternate) bases far enough in advance to ensure
adequate preparation before the departure/arrival
of aircraft carrying dangerous materials.
3-6
AIRCRAFT COMMANDER’S RESPONSIBILITIES
The aircraft commander must ensure that his crew
members thoroughly understand the operational
mission requirements and procedures governing the
dangerous materials to be airlifted. He will comply
with applicable backup and emergency inflight notification procedures, plan flight routes to avoid
overflight of heavily populated or otherwise critical
areas, and refuse to accept any ATC clearance that,
in the aircraft commander’s judgment, would interfere with operational necessity or flight safety. For
each flight ‘‘Dangerous Cargo,’’ ‘‘Inert Devices,’’ or
both (as appropriate) will be entered in the ‘‘Remarks’’ section of the DD Form 175 or ‘‘Other Information’’ section of the DD Form 1801 (ICAO Flight
Plan) unless prohibited by regulations governing
the area of operation.
BACKUP NOTIFICATION PROCEDURES
If the ETE is less than 1 hour or if other known circumstances will preclude timely receipt of information, the aircraft commander will contact the base
of intended landing by priority telephone and provide tactical call sign, ETA, DOT class of dangerous
material aboard, DOD quantity-distance class
(when applicable), NEW (total weight in pounds of
all DOT Class A and Class B explosives on board),
withdrawal distance and firefighting time (if assigned), request for special handling (if required),
inert devices (when applicable) and line numbers
and quantities (if applicable).
INFLIGHT NOTIFICATION PROCEDURES
At least 30 minutes (or as soon thereafter as practical) before the ETA, the aircraft commander will
contact the base operations dispatcher, control tower, approach control, or other agency specified in
the applicable FLIP announcing that he has dangerous material and to verify receipt of arrival notification. If advance notice has not been received, request that the information stated in backup notification procedures, be relayed to the military base
operations or civil airport manager to pass to appropriate base support elements (Example: ‘‘Bird 51,
ETA – 1200Z, DOT Class A explosives, DOD class
7, ‘‘NEW’’ four zero pounds, four zero zero zero feet,
3 minutes, request isolated parking, four each MXXX bombs in bomb bay. Please relay immediately
to fire department and other base support elements.’’)
T.O. 1B-52H-34-2-8
INFLIGHT EMERGENCY NOTIFICATION PROCEDURES
(WORLD WIDE)
FIREFIGHTING AND EVACUATION
CRITERIA
Under inflight emergency conditions or for unscheduled landings, the aircraft commander will inform the appropriate Air Traffic Control Facility of
the nature of the emergency, his intentions, and, as
practicable, the information as stated in backup notification procedures. (Example: ‘‘Bird 51, 60 miles
east of intended landing base – Nest AFB, No. 1
and 2 engines out; six personnel, forward section of
aircraft; have dangerous cargo in bomb bay of aircraft, four zero pounds of DOT class A explosives; if
explosives become enveloped in flames, detonation
may be expected after 3 minutes; withdrawal distance is 2000 feet; 10,000 gallons of fuel remaining,
apply emergency procedures accordingly.’’)
These emergency procedures consist of actions to
take if munitions are involved in a fire. The aircrew
should be thoroughly familiar with these instructions.
Aircraft fires involving conventional munitions cannot be definitized to any one set of circumstances
and environmental conditions. This precludes development of reliable standardized test criteria and
reliable specific item firefighting and withdrawal
times. The conclusion to be reached from available
data is that a munitions reaction to fire is a function of case thickness and type of explosive filler
which can be varied by environmental conditions.
Since the circumstances of a fire cannot be predicted, specific item by item firefighting and withdrawal times cannot be determined with any degree
of reliability.
Inert Devices
If inert devices are carried, the radio call will be
similar to inflight emergency notification procedures (world wide), identifying the devices as inert,
that they present no hazard, and including the
amount of fuel remaining. (Example: ‘‘Bird 51, 60
miles east of intended landing base – Next AFB,
No. 1 and 2 engines shut down, six personnel forward compartment, inert cargo in bomb bay of aircraft; no hazard; 10,000 gallons fuel remaining; apply emergency procedures accordingly.’’)
Normally, aircraft fire involving munitions occurs
under a set of circumstances wherein it is impossible to know immediately the specific missile, bomb,
or BLU model number. Such information is absolutely essential for specific firefighting and withdrawal times. Therefore, these times are presented
for family groups only; i.e., bombs, BLUs, missile,
etc.
• Bombs: See T.O. 1B-52H-34-2-1
• CBUs: See T.O. 1B-52H-34-2-1
• Missiles: Missiles normally react in a propul-
CONUS Civil Airports
When aircraft must land at a CONUS civil airport
which has no control tower, information in inflight
emergency notification procedures (world wide), as
applicable, will be furnished to the nearest FAA
Flight Service Station.
sion, detonation, or both between +45 seconds and
2 minutes. A propulsion hazard (missile flight) exists within 45 seconds and a major hazard to environment and firefighting capability exists after 1
minute. Approach the fire, if necessary, from the
side of the aircraft. See figure 3-2 for specific
AGM-158 data.
Aircraft Ditching/Abandonment
If the aircraft must be ditched or abandoned, record
the coordinates and descriptive location of abandoned cargo for later use by appropriate authorities.
The firefighting guidance provided in AFI 91-201
will be utilized in all instances. There is no specific
withdrawal time assigned to items which do not
align into one of the family groups mentioned
above.
Fire Fighting and Evacuation Criteria
NOMENCLATURE
WITHDRAWAL DISTANCE (FT) FIRE
NONESSENTIAL PERSONNEL
SYMBOL
AGM-158A
4000
1
Figure 3-2
3-7/(3-8 blank)
BLA
T.O. 1B-52H-34-2-8
Supplementary Data
section IV
table of contents
page
TEST INSTRUMENTATION KIT (TIK)
4-1
JASSM SMO FLIGHT TEST SOFTWARE COMMANDS
4-1
TEST INSTRUMENTATION KIT (TIK)
The TIK is a limited use package installed only for
use on designated flight test ranges. It provides telemetry of the missile in-flight data parameters and
provides for destructive flight termination in the
case of range footprint limitations being exceeded.
The TIK consists of the following major components:
• Telemetry package
• Transponder
• Flight Termination System (FTS)
(Destruct ring, safe & arms, receivers, logic
units, battery packs)
• Antennas
• Sensors
• Missile aft bottom cover (TIK cover assembly)
JASSM SMO FLIGHT TEST SOFTWARE
COMMANDS
NOTE
If it becomes necessary to reload the
JASSM SMO and mission data, reload the
SMO first.
TELEMETRY POWER ON COMMAND (CF-57A)
(TEST ONLY)
Operator entry of CF-57A will result in enabling
the Telemetry (TM) Radio Frequency (RF) transmitter for selected weapon(s). The SMO will reject a
CF-57A command to enable telemetry power, display the command in reverse video, and display the
advisory Less [AMI] LOC/STA??, [AMI] JASSM
LOC/STA??, if no location/station(s) have been selected on the WCP or PCP/WCP backup. The SMO
will ignore a CF-57A command to enable telemetry
power for each selected weapon where telemetry
power is already ON. The SMO will retain a valid
Telemetry Power On command for a selected weapon that does not have power applied. The command
will be processed for the selected weapon after the
weapon is powered on.
If a CF-57A command is accepted, but the selected
weapon(s) cannot be accessed (for example: weapon
not present), the advisory Less [AMI] LOC/STA??,
[AMI] JASSM LOC/STA??, will be displayed. A description of each failure and the corresponding corrective action is listed in figure 7-20.
JASSM SUPERVISION MENU (CF-57)
The JASSM Supervision Menu commanded by CF-57
is shown in Figure 1-18. When the JASSM Supervision Menu is displayed, the current SMO mode is displayed just as on the Control Function Menu (CF-)
and the Weapon Supervision Menu (CF-5).
Due to RF hazards when TM power is applied, ensure personnel avoid the TM antenna area by at least two feet.
NOTE
NOTE
The displayed status of CF-57 commands is
the commanded state in the OAS, not the
missiles status. The actual status of the
missile may or may not be the same.
If either TM or FTS is commanded on and
the missile has an uncommanded power
down, the TM and/or FTS may transition to
internal battery power. Re-applying missile
power will automatically power off the TM/
FTS battery.
The control function commands that are unique to
the SMO are of the form CF-57x, where x represents any of several alphanumeric characters that
may or may not be followed by a comma and additional alphanumeric characters. The JASSM Supervision Menu displays the control function commands of this form that are accepted by the SMO
and the function commanded by each. In addition to
identifying the CF-57x commands, the JASSM Supervision Menu (CF-57) also identifies other SMO
commands not identified on other JASSM displays.
Change 3
4-1
T.O. 1B-52H-34-2-8
JASSM Telemetry Antenna
Figure 4-1
4-2
T.O. 1B-52H-34-2-8
TELEMETRY POWER OFF COMMAND (CF-57B)
(TEST ONLY)
Operator entry of CF-57B will result in disabling
the TM RF transmitter for selected weapon(s). The
SMO will reject a CF-57B command to disable power, display the command in reverse video, and display the advisory Less [AMI] LOC/STA??, [AMI]
JASSM LOC/STA??, if no location/station has been
selected on the WCP or PCP/WCP backup. The
SMO will ignore a CF-57B command to disable telemetry power OFF for each selected weapon where
telemetry power is already OFF. The SMO will retain a valid Telemetry Power Off command for a selected weapon that does not have power applied.
The command will be processed for the selected
weapon after the weapon is powered on.
If a CF-57B command is accepted, but the selected
weapon(s) cannot be accessed (for example: weapon
not present), the advisory Less [AMI] LOC/STA??,
[AMI] JASSM LOC/STA??, will be displayed. A description of each failure and the corresponding corrective action is listed in figure 7-20.
FTS ENABLE/DISABLE COMMAND (CF-57C,xy)
(OTL ONLY)
Operator entry of CF-57C,xy, where xy represents a
valid location/station, will result in the Flight Termination System (FTS) being enabled/disabled for
the selected weapon. The FTS Enable is a test command that allows the operator to terminate a weapon
test flight if it is determined the weapon is posing a
safety risk. If the command is entered while FTS Enable is active for the selected weapon, FTS will become disabled for the selected weapon. A single valid
location and station is selected on an IKB by entering
A or C followed by a number 1, 2, 3, 6, 7 or 8. The characters “A” and “C” represent the left or right pylon
location respectively. The numbers represent the selected station on the identified pylon. The SMO will
reject a CF-57C,xy command to enable FTS and display the command in reverse video if any of the following conditions exist:
If a CF-57C,xy command is accepted, but the selected
weapon(s) cannot be accessed (for example: weapon
not present), the advisory LOC/STA?? will be displayed. A description of each failure and the corresponding corrective action is listed in figure 7-20.
The SMO will also reject a CF-57C,xy command to
disable FTS and display the command in reverse
video if any of the following conditions exist:
• Location entered is not A or C.
• Station number entered is not 1, 2, 3, 6, 7, or 8.
The FTS default state is disabled.
FTS POWER SOURCE COMMAND (CF-57D) (OTL ONLY)
Operator entry of CF-57D will result in FTS power
source being toggled between aircraft (carrier) power and the missile’s battery power for the missile
with FTS enabled. The SMO will reject a CF-57D
command and display the command in reverse video, if no location/station has FTS enabled.
The FTS default power source for an enabled weapon is aircraft power.
For Operational Test Launch (OTL) missions, the
JASSM SMO will automatically command TM and
FTS power off, including removal from internal battery power, prior to removing initialization power
from the weapon in all cases, except for a normal
launch sequence. However, it is recommended that
FTS power source be manually commanded to aircraft power, and TM and FTS be manually commanded off prior to weapon power down.
NOTE
If either TM or FTS is commanded on and
the missile has an uncommanded power
down, the TM and/or FTS may transition to
internal battery power. Re-applying missile
power will automatically power off the TM/
FTS battery.
• Location entered is other than A (left pylon)
or C (right pylon).
• Station number entered is not 1, 2, 3, 6, 7, or 8.
• Weapon is not present at selected station.
• Weapon is not operational selected station.
• Carrier mission is not live launch with Telemetry (TIK) package.
• Another weapon has FTS enabled.
Change 3
4-3
T.O. 1B-52H-34-2-8
TRANSFER ALIGNMENT (TXA) HALT COMMAND
(CF-57E,xy) (CAPTIVE CARRY ONLY)
TRANSFER ALIGNMENT (TXA) RE-INIT COMMAND
(CF-57F,xy) (CAPTIVE CARRY ONLY)
Operator entry of CF-57E,xy while Transfer Alignment (TXA) Halt is inactive, where xy represents a
valid location/station, will result in the weapon ignoring transfer alignment. If the command is entered while TXA Halt is active for the selected
weapon, TXA Halt will become inactive for the selected weapon. A single valid location and station is
selected by IKB entry. The letters A and C are used
on the IKB to enter the left or right pylon location
respectively. The numbers 1, 2, 3, 6, 7, or 8 are used
on the IKB to enter the selected station on the identified pylon. The SMO will reject a CF-57E,xy command to activate TXA Halt and display the command in reverse video if any of the following conditions exist:
Operator entry of CF-57F,xy, where xy represents a
single valid location/station, will result in the reinitialization of missile transfer alignment for that
location/station. A single valid location and station
is selected on an IKB by entering A or C followed by
a number 1, 2, 3, 6, 7 or 8. The characters A and C
represent the left or right pylon location respectively. The numbers represent the selected station on
the identified pylon.
• Location entered is other than A (left pylon)
• Station number entered is other than 1, 2, 3,
• Station number entered is not 1, 2, 3, 6, 7 or 8.
• Carrier mission is not captive carry.
• Weapon is not present at selected station.
• Weapon has a permanent fatal fault.
• Carrier mission is not captive carry.
• Weapon is not present at selected station.
• Weapon has a permanent fatal fault.
or C (right pylon).
The SMO will also reject a CF-57E,xy command to deactivate TXA Halt and display the command in reverse video if any of the following conditions exist:
• Location entered is other than A (left pylon)
or C (right pylon).
• Station number entered is other than 1, 2, 3,
6, 7 or 8.
The SMO will retain a valid TXA Halt command for
a selected weapon that does not have power applied. The command will be processed for the selected weapon after the weapon is powered on.
4-4
The SMO will reject a CF-57F,xy command to reinitialize TXA and display the command in reverse
video if any of the following conditions exist:
• Location entered is other than A (left pylon)
or C (right pylon).
6, 7 or 8.
The SMO will retain a valid TXA Re-Init command
for a selected weapon that does not have power applied. The command will be processed for the selected weapon after the weapon is powered on.
T.O. 1B-52H-34-2-8
Operating Limitations
table of contents
section V
page
WING FLUTTER AIRSPEED LIMITATIONS
5-1
JASSM ANTI-ICE OPERATION
5-1
JASSM JETTISON AND LAUNCH ENVELOPE
5-1
JASSM LAUNCH OR JETTISON WITH OPEN BAY DOORS
5-1
JASSM SAFE SEPARATION AND DECONFLICTION
5-2
WING FLUTTER AIRSPEED LIMITATIONS
JASSM JETTISON AND LAUNCH ENVELOPES
The wing flutter airspeed limitations when carrying
JASSMs are contained in T.O.1B-52H-1, Section V.
JASSM Jettison and Launch envelopes are shown
in figure 5-1.
JASSM ANTI-ICE OPERATION
JASSMs are equipped with anti-ice heaters on both
the air data probe and the flush static port. Power
to the anti-ice heaters is automatically applied
whenever the SMO is loaded and MIU power is on.
MIU power for missile heaters should be applied to
all missiles for a minimum of 15 minutes prior to
weapon release or entering icing conditions. MIU
power may be removed during flight when required,
however it should be re-applied as soon as practical.
When heater power is off, flight through icing
should be avoided.
If flight through icing conditions with MIU
power off is unavoidable, re-apply MIU
power for a minimum of 30 minutes prior
to release.
• Launch or jettison of an AGM-158 in excess
of the speeds shown in figure 5-1 may result
in collision between the JASSM and the aircraft.
• The JASSM jettison and launch envelope
limits, detailed in figure 5-1, reflect a variable relationship between altitude, mach
number, gross weight, and carriage position. Operators must be familiar with all aspects of the jettison and launch envelopes
and use care when operating near the perimeters of the envelope.
JASSM LAUNCH OR JETTISON WITH OPEN
BOMB BAY DOORS
In an emergency, launch or jettison of JASSM may be
attempted with the bomb bay doors open; however,
consideration should be given to possible aircraft
damage due to a weapon to aircraft impact. Planned
release of JASSM is not authorized with the bomb bay
doors open.
The pilot’s Bomb Bay & missile Jettison control
switch jettisons all weapons loaded on the aircraft.
If jettison is commanded using this switch, the
bomb bay doors will open and would likely result in
aircraft/JASSM collision during jettison.
Release of JASSM with the bomb bay doors
open may result in damage to the aircraft.
5-1
T.O. 1B-52H-34-2-8
JASSM SAFE SEPARATION AND
DECONFLICTION
The MAU-12 ejector rack imparts a safe separation
velocity to the JASSM to allow the weapon to meet
the following safe separation requirements:
• The JASSM normally maintains a minimum
of two inches clearance from adjacent stores/structure during all releases (launch or jettison).
If there is a retained/HUNG center station
store, launching/jettisoning an adjacent
shoulder station may result in a Store-toStore contact. When a center station store
is retained/HUNG, operators will retain the
adjacent shoulder station stores.
• The JASSM does not eject any items during
and after separation until the weapon has achieved
safe clearance from the aircraft.
• The JASSM has positive movement away from
the aircraft such that no portion of the weapon
penetrates a determined interference boundary of
the aircraft and/or remaining suspension systems
and stores. The interference boundary is defined as
a four foot envelope around the fuselage, wings, engines, and tail during launch and jettison.
To further ensure safe separation, launch advisories
will be issued when the required aircraft flight parameters are exceeded, refer to PGRM Weapon
Launch Advisories in Section VII.
Deconfliction reduces the possibility of an in-flight
collision between the JASSM and the aircraft during separation and the JASSM’s flight to the first
5-2
waypoint. At launch detection, weapon flight path
criteria are evaluated to determine if the direction
toward the first waypoint is within three degrees of
the horizontal flight path and if the altitude of the
first waypoint requires the weapon to climb
through the launch altitude. If this scenario does
not exist, then no special considerations are necessary to ensure the weapon does not penetrate the
keep out zone around the aircraft. However, when
such a scenario does exist, the following operations
take place:
• The latitude and longitude of the first
waypoint are adjusted to create an offset of 1400
feet (1000 feet requirement + 400 feet navigation
uncertainty) normal to the computed azimuth.
• The altitude command is set at least 500 feet
(100 feet requirement + 400 feet navigation uncertainty) below the launch altitude.
• The heading command is biased by three degrees.
Modification of waypoint information and desired
heading is necessary to avoid an impending flight
path conflict with the aircraft, which is assumed to
continue on its flight path at release.
To avoid conflict with the aircraft, the JASSM will:
• Achieve a minimum lateral separation of 1000
feet, to the right of the aircraft, before climbing
through the aircraft’s altitude at release.
• Achieve a minimum vertical separation of 100
feet below the aircraft’s altitude at release before
crossing the aircraft’s flight path.
• When crossing the aircraft’s flight path, maintain 100 feet minimum vertical separation below
the aircraft’s altitude at release until lateral separation of 1000 feet is reached.
T.O. 1B-52H-34-2-8
JASSM Jettison and Launch Envelopes
STATIONS L1 and R3
50
45,000 Ft.
40
KI
Lb
0
17
1
0,
00
0
Lb
20
ff e
t
30
0,
00
30
Bu
48
Lb
40
0 ,0
00
15
10
Jettison
Only
5
0
0.15
0.20
0.25
Lb
0.30
0.35
0.40
0.45 Indicated Mach Number
ow
A ll
x im
um
20
0
00
8,
Launch And
Jettison
ed
25
Ma
Pressure Altitude − 1000 Feet
AS
Top View
35
0.84 Indicated Mach N umber
45
0.81 Indicated Mach Num ber
Launch And
Jettison
Prohibited
0.45
0
34
K
I
Launch And
Jettison
Prohibited
AS
3
0.50 0.55 0.60 0.65
True Mach Number
0.70
90
KI
0.75
AS
0.80
0.85
0.90
0.95
1.00
B46518
Figure 5-1 (Sheet 1 of 4)
5-3
T.O. 1B-52H-34-2-8
JASSM Jettison and Launch Envelopes (Cont)
STATIONS L8 and R6
50
45
45,000 Ft.
0.84 Indicated Mach Number
Launch And
Jettison
Prohibited
40
KI
Lb
0
Lb
20
17
1
0,
00
0
35
ff e
t
30
0,
00
30
Bu
48
Lb
40
0 ,0
00
15
10
Jettison
Only
5
0
0.15
0.20
0.25
Lb
0.30
0.35
0.40
0.45 Indicated Mach Number
ow
A ll
x im
um
20
0
00
8,
Launch And
Jettison
ed
25
Ma
Pressure Altitude − 1000 Feet
AS
Top View
0.45
3
KI
AS
3
0.50 0.55 0.60 0.65
True Mach Number
Figure 5-1 (Sheet 2 of 4)
5-4
40
0.70
d
An
h on
c
u n ti s t e d
L a J et h ib i
o
Pr
90
KI
0.75
AS
0.80
0.85
0.90
0.95
1.00
B46517
T.O. 1B-52H-34-2-8
STATIONS L2, L3, L7 and R1, R2, R7
50
Launch And
Jettison
Prohibited
45,000 Ft.
0.84 Indicated Mach Number
45
40
KI
Lb
0
Lb
20
17
1
0,
00
0
35
0,
00
30
8,
Lb
Bu
ff e
t
30
48
0
00
Lb
40
0 ,0
00
15
10
Jettison
Only
5
0
0.15
0.20
0.25
0.30
0.35
0.40
0.45 Indicated Mach Number
ow
A ll
x im
um
20
M I = 0.81
Launch And
Jettison
ed
25
Ma
Pressure Altitude − 1000 Feet
AS
Top View
0.45
340 KIAS
Launch And
Jettison
Prohibited
39
0.50
0.55
0.60
0.65
0.70
0
KI
0.75
AS
0.80
0.85
0.90
0.95
1.00
True Mach Number
B46519
Figure 5-1 (Sheet 3 of 4)
5-5
T.O. 1B-52H-34-2-8
JASSM Jettison and Launch Envelopes (Cont)
STATIONS L6 and R8
50
45
45,000 Ft.
0.84 Indicated Mach Number
Launch And
Jettison
Prohibited
40
KI
Lb
0
Lb
20
17
1
0,
00
0
35
t
30
0,
00
30
Bu
ff e
48
Lb
40
0 ,0
00
5
10
Jettison
Only
5
0
0.15
0.20
0.25
Lb
0.30
0.35
0.40
0.45
36
3
KI
0.70
Launch And
Jettison
Prohibited
AS
3
0.50 0.55 0.60 0.65
True Mach Number
340 KIAS
M I = 0.81
0.45 Indicated Mach Number
ow
A ll
x im
um
20
0
00
8,
Launch And
Jettison
ed
25
Ma
Pressure Altitude − 1000 Feet
AS
Top View
90
KI
0.75
AS
0.80
0.85
0.90
0.95
1.00
B46520
Figure 5-1 (Sheet 4 of 4)
5-6
T.O. 1B-52H-34-2-8
Mission Planning
table of contents
section VI
page
GENERAL
6-1
MISSION PLANNING MODULES
6-3
REPF MISSION PLANNING
6-4
UNIT MISSION PLANNING INTEGRATION
6-4
MISSION PLANNING TIMELINES
6-4
MISSION PLANNING CONSIDERATIONS
6-7
GENERAL
Mission Planning is the key component in the effective operational use of a weapon system, especially
with the advent of launch and leave precision
guided munitions. These weapons require the mission planner to provide both the routing and targeting information used to autonomously guide the
weapon to the desired impact point with high precision.
The low-observable JASSM missile uses GPS-aided
inertial guidance, updated with an imaging infrared (IIR) terminal area seeker to provide high
precision terminal guidance to engage heavily defended and/or hardened targets requiring greater
impact point precision. The terminal seeker requires the mission planning system to provide the
terminal attack plan, including reference material
for locating and tracking the target, JASSM terminal trajectory, weapon fusing and Bomb Impact Assessment (BIA) data. Extended range weapons such
as JASSM also require a launch aircraft launch acceptability region (LAR), weapon route waypoints,
and time of flight information to achieve desired
time on target. JASSM simplifies missile route
planning by flying midcourse at high altitude,
avoiding terrain obstacles.
The JASSM mission begins with the Air Tasking
Order (ATO) defining specific targets, delivery air-
craft and mission details. JASSM planning is designed to conform to ATO planning cycle
constraints. During the ATO process, desired targets as well as desired effects are coordinated with
a JASSM Rear Echelon Production Facility (REPF).
The REPF is responsible for designing, building,
and maintaining the primary target database, the
primary element of which is:
• Target Area Model (TAM) – A wire frame rendering of a target complex, utilizing Digital
Point Position Database (DPPDB) as the principle source of reference imagery, selection of
weapon type data, and specification and evaluation of the attack trajectory and azimuth.
REPF planners use a Precision Targeting
Module (PTM) workstation online with current Intel sources to achieve the model. The
TAM provides the ability to utilize the JASSM
seeker, if desired. The TAM can also be manipulated if a DMPI adjust is desired.
The other key target database incorporated in
JASSM planning is:
• PGMTDB – A standard database for precise
target information. Using targets from this
data set does not allow for seeker use.
PGMTDB targets may also be manipulated to
achieve desired effects. Planners may manually enter desired DMPI information at the unit
level.
6-1
T.O. 1B-52H-34-2-8
Effects-based targeting then occurs, utilizing these
two formats, at the AOC, and, if the targets are not
readily available in a database, the desired target
models are requested from the REPF. Once the
TAM is built and verified, the REPF and/or the
AOC will pass the resulting appropriate target data
set (TDS) to the tasked unit with instructions.
Since the JASSM’s effectiveness lies mainly in high
value, fixed targets, it is highly desired that a current, coordinated baseline TAM database be available prior to deployment to minimize the time needed for target material generation during an ATO
cycle. Large-scale operations should utilize preplanned sortie data from operational plans conceived far in advance of hostilities.
Once target tasking is received, a JASSM mission
plan is assembled at the tasked unit level. This
mission consists of an enroute plan, release points,
Target Area Model (TAM) or Precision Guided
Munition Target Database (PGMTDB) target data
sets, and terminal engagement trajectory for the
desired weapon effect. DMPI manipulation may be
required at the unit level by a qualified JASSM
planner. Alternate missions may also be specified if
desired (up to 5 per launch point). The JASSM mission plans are then integrated with the delivery aircraft flight plan and transferred to the aircraft using a data transfer cartridge (DTC). The ability to
carry multiple JASSM missions on the aircraft
DTUC allows great flexibility in striking targets,
and appropriate strike planning should incorporate
procedures to use the various options.
USAF JASSM Mission Planning Module
Figure 6-1
The JASSM system mission planning is performed
within the existing or planned infrastructure and
using existing or planned data products, formats
and hardware. Design infrastructure includes the
REPF, and should be implemented with a
centralized management system, such as Theater
Battle Management Core System (TBMCS), or like
system located at the AOC, wing and units. Final
JASSM mission planning uses the tasked units’ Air
Force Mission Support System (AFMSS) Mission
Planning System (MPS) workstations for weapon
and aircraft routing.
6-2
Target materials used in terminal planning and
route planning include:
• Target descriptions (BE#, DMPI, TAM ID).
• Weapon data (Fuzing, Impact Angle, Azimuth).
• DMPI identification (Short written description, Imagery).
• Geopositional reference data (Latitude, Longitude, Elevation).
• Digital imagery with support data.
• Digital terrain elevation data (DTED, Terrain
Clobber Analysis).
• Threat information.
• Weather conditions.
T.O. 1B-52H-34-2-8
JASSM planning utilizes the skills of personnel
currently responsible for performing targeting and
route planning functions. The approach also meets
the targeting timeline where the target area, TAM
DMPI selection, and associated reference model
construction and terminal attack planning must be
performed in 15 minutes (average). DMPI review
and manipulation, and weapon routing must be
performed in 5 minutes (average). The approach
provides significant flexibility to the planners in the
use of existing data and the ability to plan/replan at
both the force and unit levels to meet a variety of
targeting circumstances, including emerging targets. The overall Mission Planning flow and partitioning to planning workstations is shown in figure
6-2.
MISSION PLANNING MODULES
The REPF planners use the Precision Targeting
Module to produce the Terminal Area Model, which
contains the terminal attack plan data (Seeker reference, DMPI and weapon data). The PTM supports
all functions of planning the terminal attack including designation of the DMPI and seeker aim point,
construction and evaluation of the seeker reference
model using national asset products, selection of
weapon type data, specification of the attack trajectory and azimuth and evaluation of the attack plan.
The PTM provides archiving and transfer of
JASSM TAM files with associated TAM ID to
AFMSS.
The tasked unit mission planners use the Weapon
Planning Module (WPM), which is an AFMSS A/
W/E hosted on the AFMSS workstation. The WPM
supports reading of archived JASSM TAM files, review and revision of DMPI’s and terminal attack
plans; weapon auto route and manual modification
planning, time-on-target planning, LAR deconfliction, association of a JASSM with the aircraft
route, AFMSS based multi-JASSM route deconfliction; and constraint checking, and transfer of required weapon data to the aircraft A/W/E for
download to the Data Transfer Device (DTD).
Mission Planning Flow and Partitioning
Target Data
TBMCS or DIWS
– DMPI coordinates
Stereo Work Station
– Imagery
Weapon selection
AFMSS or TAMPS
Work Station
(Unit Level)
(Force / Unit Level)
JASSM Target
Target Data
DTD
Material
Tasking
Terminal attack
planning
Launch A/C routing
Weapon Type
Threat data
Target Materials
Missile and A/C route
Weapon Materials
planning and loadout
– A/C routing
– Weapon routing
– Target area imagery
– Terminal data
– DMPI
(TOT, Fusing settings, etc)
– seeker reference
Precision
Aircraft / Weapon
– Seeker reference
– performance
Weapon
Planning
Module
Targeting
Module
Figure 6-2
6-3
T.O. 1B-52H-34-2-8
REPF MISSION PLANNING
To develop a TAM, the REPF mission planner views
the stereo data on the PTM to perform imagery
analyses. He/she can use the Digital Point Positioning Data Base (DPPDB) imagery as the principle
source of reference imagery and National Technical
Means (NTM) NITF 2.0 imagery to augment the
DPPDB data. A target nomination list is then accessed to identify target areas of interest via using
other Intel application and databases such as the
MIDB (modern integrated intelligence database) on
the TBMCS workstation. The planner can view existing JASSM target seeker reference database
models for review and refinement or build a new
model. If he/she chooses to build a new model, the
reference imagery is accessed either by loading a
tape or accessing a previously loaded DPPDB segment on his system. Once the imagery is displayed,
the three dimensional data is used to locate and
designate a DMPI. Once the Designated Mean
Point of Impact (DMPI) is chosen, building a seeker
reference model can begin. A 3D reference wireframe (WF) is constructed using the visible edges in
the reference imagery. While the building the WF,
the user can perform a reference evaluation process
that provides a quantitative assessment of the model. The completed model can be archived in a TAM
for future use, a feature useful in prewar planning.
The operator may also choose to select and use an
existing TAM. A TAM is selected from the database
and opened for review of the terminal planning
data. Then the existing reference model with its associated reference imagery can be viewed. The user
may update the original reference model by bringing in new NTM imagery to use with the original
reference imagery (DPPDB or other NTM imagery).
The operator can tie the DPPDB and NTM imagery
together in support of reference model update. He/
she can overlay the original wireframe on the NTM
image and update it as required. The reference
model update is performed using drawing tools to
construct wireframes of objects in the NTM image.
The modified reference wireframe can be evaluated
against the new, up to date, NTM imagery. Once
the update is complete, a DMPI can be added or
modified using a target location description corresponding to a viewable location in the update imagery.
Once the reference model is ready, terminal planning is performed. An attack trajectory and fuze
delay time is selected based on the target to be attacked. An attack azimuth range is selected by the
planner based on the attack trajectory, terminal
area imagery, and target characteristics. For each
azimuth selected the seeker reference model is com-
6-4
piled and performance effectiveness is evaluated for
the selected azimuth range and provided to the operator. The terminal planning could potentially be
performed at stereo capable Sun/UNIX workstations within the DODIIS CSE or TBMCS/DIICOE
environment.
The resulting attack plan including a reference stereo image pair and NTM imagery is exported as a
TAM and passed to the unit for use in the WPM on
an AFMSS workstation.
UNIT MISSION PLANNING INTEGRATION
The mission plan is then available to the unit level
planner along with the ATO for weapon routing.
The Weapon Route Planning functional flow is also
shown in figure 6-3. Using the JASSM A/W/E module on the AFMSS workstation, the planner readsin the JASSM TAM file. He/she reviews the attack
plan and can modify weapon data and DMPI’s on
the 3D reference model. The reference image is displayed to support DMPI review and adjustment.
With modified DMPI’s, the terminal attack plan
will be reevaluated to verify that the reference model supports the new DMPI. Missile information is
entered including BIA and TOT data when applicable. The operator also reviews and updates weapon fuze settings and impact angle and which of the
terminal profiles is to be used for the target.
The unit planner then builds the weapon route. The
operator displays or enters the DMPI coordinates.
He/she then, guided by JASSM range rings on the
AFMSS display, selects either a waypoint one (planning scenarios one and two) or an aircraft release
point (planning scenario three). He/she can then
display a LAR. He/she has now completed definition of a stick route. The operator then selects autorouting using the Common Low-observable Auto
Router (CLOAR) selection. Either a time-on-target
or non time-on-target (not time critical) flyout profile will be used by the auto-router. Once the autoroute has been performed, the operator may perform manual modifications of the route, if desired.
The resulting weapon data, weapon route, terminal
trajectory, seeker reference and BIA settings are accessed via calls to the JASSM A/W/E by the aircraft
A/W/E on the AFMSS system for download to the
Data Transfer Device.
MISSION PLANNING TIMELINES
The mission planning timelines are shown in figures
6-4 and 6-5 for the PTM and WPM respectively.
T.O. 1B-52H-34-2-8
Mission Planning Functional Flow
Precision Targeting Module
Target Materials
Nominations
– DTM
Designate DMPI’s
Modify / Generate
– MIDB
Reference Model
Evaluate
Reference
Model
Generate Terminal
Attack Plan and
Evaluate
IMINT
– DPPDB
– Updatel Imagery
Open
WF Model
Archive
WF Model
Archive / Transmit
JASSM Target
Materials
JASSM Weapon
– Seeker
Archive Plan
– Non–seeker
Weapon Planning Module
JASSM
Target Materials
Review terminal
Threat Data
DTED
attack plan and
modify DMPI’s
Weapon Route Plan
Determine A/C LAR
Evaluate Route
Wx
– Move DMPI’s
–Analyze attack
Repeat each weapon
Integrate A/C and
Weapon Mission
Plans (A/C AWE)
Download
Weapon Mission
Plan to DTD
Figure 6-3
6-5
T.O. 1B-52H-34-2-8
PTM Timeline Definition
Figure 6-4
WPM Timeline Definition
Figure 6-5
6-6
T.O. 1B-52H-34-2-8
MISSION PLANNING CONSIDERATIONS
Since JASSM requires the use of time sensitive materials, such as GPS crypto data, the planner must
ensure the most current data is used at all times to
maximize mission effectiveness. If B-52 mission
duration will extend across any crypto expiration
boundary, the following period’s data should be
loaded to ensure the JASSM receiver has sufficient
information. For example, a B-52 mission will start
at 2000 hrs GMT/ZULU and end at 0900 hrs. During the sortie there is a new GPS crypto issued. If
the GPS/IU keyboard has failed, or the crew does
not have the new keys available, the only other
source is the weapon or aircraft mission DTUC/
DTC.
• Divert and Staging base security – Appropri-
•
•
•
NOTE
The following steps may be used to correct
for GPS rollover:
• (RN-N) CF-61 entered.
• Correct date is input on the MFD, but not en-
•
tered into the system.
• (RN-N) Monitor for GPS date to rollover to incorrect date.
• Enter Key pressed to insert the correct date.
• A missile health status check occurs.
Other Items to Consider When Preparing to
Employ JASSM:
• JASSM MPS security/environment
• Height Above Ellipsoid (HAE) – JASSM uses
•
•
•
•
•
•
HAE for all altitude computations (launch,
cruise, target). This closely mirrors the OAS
HA altitude for launch operations, and should
be a consideration if determining deconfliction
from other platforms.
Coordinate format – JASSM uses DDMMSS.
SSS for higher fidelity. Planning on MPS can
be done in DDMM.MMMM, since data is converted in the MPS to give the missiles the correct format.
GPS Crypto Data Currency – Weekly keys required. Recommend that current and following week keys always be loaded on DTC.
AS/SV Data Currency
BIA Data – BIA frequencies used must be
coordinated with the AOC, Intel, and ELINT
platforms to assure missile health data is received and matched against the proper missile
mission, if desired.
GPS Almanac Data – Should be current, or at
least within 14 days of mission.
Intel feed – Coordinated with unit Intel section for current threat database and other
flight restrictions.
ate to support the highest levels security for
planning systems, communication nodes, and
the assets themselves. Foreign controlled
bases should be avoided and only used for
emergencies.
Divert and Staging base logistics support –
Load equipment, missile storage (including
environmental needs), and planning system
support should be examined as far in advance
as possible.
Direct targeting ROEs – Theater or Operational commanders must drive use, due to limited number of assets, cost, range, etc.
Integration with other JASSM platforms – A
centralized, coordinated plan for JASSM
strikes that includes all JASSM capable aircraft is highly recommended. Mass JASSM
launch scenarios will occupy copious amounts
of airspace, and the ATO must sanitize space
for missile launch(s).
LAR Tolerances – Must be thoroughly briefed to
ensure planned IN ZONE launches are achieved. Aircraft flying a pressure altitude, for example, could be off the HAE altitude enough to be
out of IN ZONE launch tolerances.
JASSM Operations Near the Poles
The JASSM SMO great circle distance equation is
approximate when operating close to or at the
poles. This will affect the times-to-go to enter and
exit ranging indications on the PRGM screen. This
will not affect the actual In-Range/In-Zone status
reported by the weapon. To minimize the distance
error when planning sortie destinations to either
pole, ensure the following:
• Aircraft route follows the same longitude as
•
the launch point destination, and
Center of range circle, center of zone arcs, and
launch point destination are on the same side
of the pole.
Planning for JASSM Safe Separation and Deconfliction
For planning of a low altitude or co-altitude launch,
it should be noted that the JASSM will require a
minimum 5 degree offset to the right of the aircraft
heading to avoid conflict with the aircraft. The missile will achieve a minimum lateral separation of
1000 feet to the right of the aircraft before climbing
through the aircraft altitude at release. The JASSM
will also achieve a minimum vertical separation of
100 feet below the aircraft altitude at release before
crossing the aircraft’s flight path. This combination
will assure the missile will maintain a minimum
vertical separation of 100 feet below the aircraft’s
altitude at release until lateral separation of 1000
feet is reached.
Change 2
6-7
T.O. 1B-52H-34-2-8
JASSM Low Temperature Flight Operations
The JASSM missile is designed for captive carriage
and free flight down to a minimum ambient skin
temperature (Ts) of –49 degrees F (–45 deg. C). Exposure of the JASSM missile to ambient skin temperatures below –49 degrees F could result in BIT
[FAIL] indications and or missile failures. Since
wind friction warming affects the JASSM skin during external carriage, low temperature exposure
should not be an operational concern unless the
JASSM is carried in the bomb bay or if loaded on
the aircraft for alert during extreme cold weather
6-8
conditions. JASSM missile skin temperature (Ts)
during external carriage is defined as:
External Carriage and Free Flight:
Ts = (OAT + 460)(1+0.18M2) – 460
Where Ts = Missile skin temperature (degrees F);
OAT = True ambient air temperature (degrees F);
M = True flight Mach number.
For example, a JASSM mission profile of FL 370 at
0.76 mach should produce JASSM skin temperatures of approximately –25 degrees F.
T.O. 1B-52H-34-2-8
Systems Operation
table of contents
OAS/JOINT AIR TO SURFACE STANDOFF MISSILE OPERATION
section VII
page
7-3
JASSM EMPLOYMENT OVERVIEW
7-3
MISSILE MISSION TYPES
7-3
WEAPON MONITOR AND POWER CONTROL
7-7
WEAPON CONTROL EQUIPMENT (WCE) STATUS
7-7
WCE POWER APPLICATION
7-7
WCE POWER REMOVAL
7-8
MISSILE POWER APPLICATION
7-8
MISSILE AND EJECTOR STATUS
7-10
MISSILE POWER REMOVAL
7-15
MISSILE MISSION DATA AND TARGETING
7-17
MISSILE TARGETING METHODS
7-17
TARGETING TECHNIQUES
7-22
TARGET RANGING
7-29
IN-RANGE LAR
7-31
IN-ZONE LAR
7-36
TARGET RANGING INDICATIONS
7-43
IN-RANGE/IN-ZONE INDICATION
7-43
WEAPON LAUNCH ADVISORIES
7-43
SAFE RELEASE ADVISORIES
7-44
MISSILE LAUNCH
7-45
MISSILE LAUNCH PROCESS
7-45
AUTOMATIC LAUNCH DETERMINATION
7-46
MANUAL LAUNCH DETERMINATION
7-47
MISSILE LAUNCH TERMINATION
7-47
PREFERRED LAUNCH/JETTISON SEQUENCE
7-48
MISSILE LAUNCH RESTRICTIONS
7-48
JASSM FREE FLIGHT SEQUENCE
7-48
7-1
T.O. 1B-52H-34-2-8
page
7-2
MISSILE JETTISON
7-50
SIMULATION CAPABILITIES
7-51
SIMULATED MISSILE LOADOUT
7-51
SIMULATED TARGETING OPERATIONS
7-51
SIMULATED WCE RESPONSES
7-51
SIMULATED RANGING
7-51
SMO TERMINATION
7-52
SMO RESTART
7-52
MESSAGES
7-52A
MASTER FAULTS
7-52A
ADVISORIES AND STATUS MESSAGES
7-52A
SAFE RELEASE AND WEAPON LAUNCH ADVISORIES
7-52A
FRMT-7 MISSILE FAULTS
7-52A
Change 2
T.O. 1B-52H-34-2-8
OAS/JOINT AIR TO SURFACE STANDOFF MISSILE OPERATION
The B-52 OAS provides the operator interface for
control, targeting, and release of JASSMs.
ence model which was developed using the JASSM
mission planning system.
Operation of the JASSM while carried by the B-52
is made up of six major functions. These functions
are:
The missile is designed to operate under adverse
weather conditions of 1500 ft. ceiling and 3 nautical
mile visibility. If weather conditions preclude the
seeker from acquiring the target, the system will
guide to the target using the inertial navigation
system and target coordinates it received via mission planning. During the terminal trajectory, a
Bomb Impact Assessment (BIA) subsystem transmits missile position and status information in an
unencrypted format to an airborne receiving platform.
• Missile Monitor and Power Control
• Mission Data and Targeting
• Transfer Alignment
• Target Ranging
• Missile Launch
• Missile Jettison
NOTE
[AMI] In order to accomplish any of the six
major functions listed above, the JASSM
SMO must be designated as the primary
SMO (CF-62x).
JASSM EMPLOYMENT OVERVIEW
At a specified time prior to arriving at the aircraft
missile launch point, initialization power is applied
to the missile, initiated BIT is run, mission data
and GPS Crypto keys are downloaded, and the selected missile mission number is designated by the
aircrew. When aircraft transfer alignment is complete, the missile is ready for launch at the specified release point.
After missile launch (autonomous missile flight),
missile navigation to the target is accomplished via
predetermined three-dimensional waypoints. Ingress is at an optimum altitude condition to achieve
the desired range and enhance survivability. At a
specified distance from the target the JASSM descends to a selected altitude above ground level for
final target ingress which will enable the missile to
achieve the desired terminal impact angle. The terminal profile depends on target orientation (vertical
or horizontal) and hardness. Impact velocity is
maintained to achieve the required penetration of
hard targets. The terminal dive starts approximately 3 km from the target with a pushover maneuver
to the desired impact angle. An imaging infrared
seeker is used to reduce terminal area guidance error for hardened targets requiring greater impact
point precision. When the seeker line-of-sight is
pointed at the target area, an algorithm which determines if the JASSM is above or below the cloud
ceiling is initiated.
Once the seeker Line-of-Sight (LOS) is clear, an Automatic Target Correlator (ATC) algorithm provides
target aim point error corrections for terminal guidance. The ATC uses a preloaded target area refer-
MISSILE MISSION TYPES
There are two types of JASSM missions, preplanned missions and direct target missions (also
called Target of Opportunity missions by JASSM).
There are two types of preplanned missions, those
that require a Time on Target (TOT) and those that
do not require a TOT.
All preplanned missions are planned as In-Zone releases, but can be released In-Range, if the In-Zone
conditions cannot be achieved by the host aircraft.
All Target of Opportunity (TOO) missions are released In-Range, there is not an In–Zone region associated with a TOO.
Altitudes can be mission planned, aircrew defined
via cockpit controls or missile default.
Preplanned Missions
Preplanned missions require at least one waypoint
to define the route of flight and flight altitudes. The
requirement for TOT required missions is set by
mission planning and must be launched In-Zone.
Using missile throttle adjustments the missile flies
the planned route within ± 5 seconds of the Current
Time Of Flight (CTOF), giving it a TOT which is
also ± 5 seconds of planned TOT assuming the missile was launched on time and at the preplanned release point. If the TOT requirement is not set, the
missile flies the preplanned route without throttle
adjustments. If a TOT required missile is launched
In-Range, but not In-Zone, it deviates from the
planned route of flight and does not attempt to
make the required TOT, but still maintains all preplanned terminal conditions. See figure 7-1 for
Flight Profile Summary and figure 7-2 for JASSM
Flight Profiles.
Change 2
7-3
T.O. 1B-52H-34-2-8
JASSM Flight Profile Summary
MISSION TYPE
LAUNCH
WAYPOINTS
SEEKER
TOT
REQUIRED
PTOF
TOLERANCE
JASSM FLIES
TO
PREPLANNED
In-Zone
Yes
Used, If
Required
Yes
± 5 Seconds
Waypoint 1
PREPLANNED
In-Zone
Yes
Used, If
Required
No
Not Required
Waypoint 1
PREPLANNED
In-Range
No
Used, If
Required
Yes
Not Used
Target Azimuth
PREPLANNED
In-Range
No
Used, If
Required
No
Not Required
Target Azimuth
DIRECT TARGET
In-Range
No
Not Used
N/A
Not Required
Target Azimuth
Figure 7-1
PREPLANNED, LAUNCHED IN-ZONE
In-Zone launched missions use a static Launch Acceptability Region (LAR). This preplanned static
LAR defines the zone around the launch point from
which the missile will be able to intercept the missile mission at the first waypoint and fly the preplanned route (See Target Ranging this section).
In-Zone launches have the following parameters:
• Can be with or without seeker terminal guidance.
• Missile flies the preplanned route of flight (including all waypoints and altitudes).
• For non-TOT missions, the nominal cruise altitude is 22000 feet MSL, until transitioning
to the terminal area. During the mission planning process, the user can change the cruise
altitude ± 500 feet in 50 feet increments, relative to the nominal altitude. For example, acceptable mission planned entries are 21500,
21550, 21600, etc.
• For TOT missions, the nominal cruise altitude
is 12000 feet MSL until transitioning to the
terminal area. During the mission planning
process, the user can change the cruise altitude ± 500 feet in 50 feet increments, relative
to the nominal altitude. For example, acceptable mission planned entries are 11500,
11550, 11600, etc.
• Impacts the target under preplanned conditions.
• Preplanned data items cannot be changed.
PREPLANNED, LAUNCHED IN-RANGE
For preplanned missions launched In-Range, the
missile does not attempt to make the planned waypoints nor planned timing. Instead the missile will
7-4
fly directly to meet the target azimuth into the target.
In-Range launches have the following parameters:
• The missile will generate its own route to intercept target azimuth.
• Proceeds to 22,000 feet MSL and remains
there until descending to the terminal area.
• Since the route from the last waypoint to tar•
•
get did not change it can be with or without
seeker terminal guidance as planned.
Since the route from the last waypoint to target did not change it impacts the target under
preplanned conditions.
Preplanned data items cannot be changed.
Direct Targeted Missions/Target of Opportunity (TOO)
Direct target function allows the operator to specify
a target that is not included as a preplaned mission. TOO missiles can only be launched In-Range.
TOO launches have the following parameters:
• Waypoints cannot be specified for a direct target.
• A direct target can be assigned to a specific
missile.
• Target latitude, longitude, and elevation must
be entered.
• The missile will fly cruise altitude until transitioning to the terminal area. The cruise altitude can be specified from 0 to 22,000 feet
MSL (defaults to 15,000 feet MSL).
• Bearing to target and impact angle can be
specified.
• Fuze mode of soft impact or hard impact can
be specified. Defaults to soft.
• Fuze delay time can be specified.
T.O. 1B-52H-34-2-8
JASSM Flight Profiles
Figure 7-2
7-5/(7-6 blank)
BLA
T.O. 1B-52H-34-2-8
WEAPON MONITOR AND POWER CONTROL
The Weapon Control Equipment (WCE), which consists of the Armament Interface Unit (AIU), Environmental Control Unit (ECU) and Weapon Interface
Units (WIUs) must be powered on to enable the operator to power on, control, and release any missiles. The
AIUs supply power to the ECU and WIUs. The ECUs
supply cooling air to the WIUs. The WIUs enable power application to the missile(s), perform data transmissions with the missile(s), and provide ejector control. AIU power is supplied when OAS master power
is turned on. ECU and WIU power are supplied power
when WIUs are turned on.
Subsequent to applying power to the WIU on a pylon,
initialization power can be commanded on for any
missile(s) on that pylon via the WCP. Missile initialization power must be applied to enable the SMO to
verify the weapon type, missile operational and LAR
status, and to transmit missile initialization, GPS,
alignment, and targeting data to the missile(s) prior
to launch.
WEAPON CONTROL EQUIPMENT (WCE) STATUS
The operator can review the operational status of the
AIU, ECU, left WIU (L WIU) or right WIU (R WIU)
using the PME Status Display (FRMT-6). The SMO
communicates with these LRUs using OAS 1553 data
buses A and C. The PME Status Display (FRMT-6)
shows AIU and WIU A bus and C bus communication
status and AIU, ECU and WIU failure status. If a
WIU A bus communication failure has occurred, an A
will be displayed for the respective WIU. If a WIU C
bus communication failure has occurred, a C will be
displayed for the respective WIU. If an LRU failure
has occurred, an X will be displayed for the ECU or respective WIU. In a similar manner, FMS will display
an A or a C next to AIU if an AIU A bus or C bus communication failure has occurred and an X next to AIU
if an AIU failure has occurred. The format of the text
indicates whether or not the failure currently exists.
If the failure currently exists, the text (A, C, or X) will
be displayed in reverse video. If the failure does not
currently exist, the text (A, C, or X) will be displayed
in normal video.
To clear unwanted data from the PME Status Display
(FRMT-6), the operator can enter CF-66 Erase PME
Faults, to delete the display of all failures which no
longer exist. When the CF-66 command is entered, all
failure text displayed in normal video will be blanked
and any text displayed in reverse video will remain.
The AIU, ECU or WIU failure status is also displayed
on the JASSM Status and Inventory Display
(FRMT-7). AIU will be displayed in reverse video if
the AIU has failed. ECU will be displayed in reverse
video if the ECU has failed. WIU will be displayed in
reverse video for the left or right WIU respectively, if
either the WIU communication or the WIU have failed. Each failure displayed on FRMT-7 will be removed if the associated failure status clears.
WCE POWER APPLICATION
WIU power will be applied when the operator
presses the WIU power switch (MIU/LP or MIU/RP)
to the depressed (Power On) position. When the
switch is in the depressed position it illuminates after a short delay. If the switch was in the depressed
position when the SMO was loaded or restarted, the
switch must be cycled to command power to the
WIU. The MIU/BAY switch is not recognized by
JASSM SMO. If it is selected the advisory message
B: LOCATION will be displayed. Power will be applied to the WIU and then the WIU will be initialized for the selected location.
If the SMO is unable to complete the WIU power-on
sequence it will be terminated, the appropriate
fault will be displayed, and any power which has
been applied will be removed. However, for an ECU
fault, if ECU Power Override is currently active,
the SMO will continue with the power-on sequence.
The operator can verify completion of the WIU power on sequence by viewing FRMT-7.
When the sequence is complete, the following display changes will occur on FRMT-7 next to each
WIU station number (1, 2, 3, 6, 7, and 8)(4 and 5
are not recognized by the JASSM SMO):
• The weapon type window will indicate either
M1 to identify there is a weapon present at the station or blank to indicate that no weapon is present.
• The missile status window will change from
blank to OF, X, NG, or CL, to indicate missile state.
See FRMT-7 in Section I for a description of the
display options.
1. OF will be displayed to indicate that missile
initialization power is not applied at the
station.
2. X will be displayed if both the ejector and
umbilical status show no missile is present
at the station.
3. NG will be displayed in reverse video if a
permanent fatal fault has occurred for the
missile.
4. CL will be displayed if the missile is a captive carry launched (Flight Test Only).
Change 3
7-7
T.O. 1B-52H-34-2-8
• The missile fault display window will display a
fault indication if a missile is present and any faults
have been detected at the station. All faults are listed
and described at the end of this Section. If no missile
is present the fault window will remain blank.
• The JASSM launch point number (1 to 99) and
mission group (A to F) will be displayed as assigned
per B-52 mission data.
MISSILE POWER APPLICATION
Missile Warm-up
After applying power to the WIU on a pylon, power
application can be commanded for any missile(s) on
that pylon. Missile power must be applied in order
for the SMO to verify the weapon type, missile operational and LAR status, and to transmit missile
initialization, GPS Crypto Keys (weekly), GPS Almanac (less than 2 weeks old), alignment, and targeting data to the missile(s) prior to launch.
Upon application of power to the WIU, 115-volt ac
power is applied to the missiles to thermally condition the missiles air data systems (requires up to
13.5 minutes). When takeoff and climb-out through
icing conditions is anticipated, heater power should
be applied prior to take-off and remain on for a
minimum of 15 minutes or until clear of icing conditions, whichever occurs last. Flight through icing
conditions should be avoided.
Missile Initialization power (28-volt DC-1) power
will be applied when the operator depresses the desired Location (left and/or right) and Station (1, 2,
3, 6, 7, and/or 8 or ALL) switches on the WCP and
momentarily moves the WPN PWR switch to the
ON position. Missile power can also be applied using CF-E. Subsequently, the selected missile(s) will
be powered on and initialized. See figure 7-3 for an
initialization timeline.
The missile will set an Overtemperature Caution
indicating the probability of the missile overheating
before completing its mission, if the missile is not
launched in approximately ten minutes.
The OAS provides GPS data to the JASSM through
the WIU in order to prepare the weapon GPS receiver
to acquire satellites after separation from the aircraft. The GPS data provided includes: Almanac data,
Anti-Spoofing Status/Space Vehicle Configuration
(AS/AV) data, GPS Crypto Keys, Time data, Ephemeris. GPS data transfer occurs after warm up and
built in test. The JASSM must have weekly crypto
keys that are current for the duration of the mission.
The missile will set an Overtemperature Warning
indicating the probability of the missile overheating
before completing its mission if the missile is not
launched in approximately one minute.
If, as a result of an Overtemperature Caution or
Warning, the operator removes missile power no
damage will occur. If missile power is removed due
to an overtemperature condition, a cool down period
of approximately 45 minutes should be allowed before missile power is reapplied.
The crew should ensure that the weapon mission
DTUC/DTC contains GPS Almanac Data (less than 2
weeks old) and GPS Crypto Keys (weekly) sufficient
to support the mission since the B-52 SMO uses the
weapon mission DTUC/DTC as backup.
The effects of weapon overheat on weapon
reliability and accuracy are unknown.
The SMO can acquire crypto key data from either
the GPS interface unit (IU) or the weapon mission
DTUC. The primary source of crypto key data is the
GPS IU. If the GPS receiver validates the crypto
key data, the SMO loads the validated crypto data
anytime after SMO start-up. After power initialization is complete, the crypto key data is transferred
to any weapon requiring the data.
WCE POWER REMOVAL
WIU power will be removed from the selected location when the operator presses the desired WIU
power switch (MIU/LP or MIU/RP) and allows it to
return to the out (non-depressed) position. No
faults will be displayed during WIU power removal.
The operator can verify completion of the WIU power off sequence by viewing FRMT-7, CF-E and/or
the OAS Power Control Panel. When the sequence
is complete, the selected WIU power switch (LWIU
or RWIU) will no longer be lit and all data contained on FRMT-7 for each station at that WIU location
will be blanked within 3 seconds.
7-8
Change 2
If the GPS almanac data age is unknown, or the
GPS has not been operated within the last two
weeks, it should be updated in accordance with procedures in Section II of this T.O.
If the crypto key data in the IU is not validated or
not available, the data can be obtained from the
weapon mission DTUC/DTC. When weapon power
initialization is complete, the SMO retrieves the
crypto key data from the weapon mission DTUC/
DTC and transfers the data to the weapon(s).
T.O. 1B-52H-34-2-8
JASSM Initialization Timeline
Figure 7-3
7-9
T.O. 1B-52H-34-2-8
MISSILE AND EJECTOR STATUS
The operator can review the operational status of
each JASSM via the JASSM Status and Inventory
display (FRMT-7) figure 7-4 or FRMT-7xy figure
7-5. The JASSM Status and Inventory Display
shows missile presence, missile power, missile state
and missile fault status for each station (1, 2, 3, 6,
7, and 8) on each pylon (left and right). The station
status windows are grouped together for each station. The station number is displayed immediately
to the left of the weapon type window.
If the SMO is unable to complete any of the steps
for a missile, the missile power on sequence will be
terminated for that missile, the appropriate fault
will be displayed and any missile power which has
been applied to that missile will be removed. When
the power on sequence is complete, the following
display changes will occur within 2 seconds on
FRMT-7 or FRMT-7xy next to each selected WIU
station number (1, 2, 3, 6, 7, or 8) where power was
applied:
• Missile type will change from blanks to M1 when
the missile is determined to be a JASSM or it will
remain M1 if the missile has previously been determined to be a JASSM. P will be displayed if the
system detects a missile at the station but cannot
identify the type.
• Weapon Status will change from OF to ON, to
indicate missile initialization power is available at
the station. If the missile is a captive carry missile,
CL, will be displayed when the missile is launched.
• Missile Fault display will display a fault indication if any missile faults have been detected at the
station. All missile faults are listed and described
at the end of this section.
The following conditions must exist:
• The JASSM SMO must be the primary SMO.
• The associated WIU must have power applied
and be initialized.
• The missiles selected must be pylon stations 1, 2,
3, 6, 7, or 8; or ALL.
• The missiles selected must be present and powered off.
• Carrier mission stores table is loaded.
• The missiles selected must not have any permanent fatal faults. If a fatal fault exists for a missile,
NG will be displayed in reverse video.
In addition, the operator can review the operational
status of a selected station ejector and additional
7-10
Change 3
missile status via the JASSM Status and Inventory
with Selected Station Status display (FRMT-7xy).
See FRMT-7xy in Section I for a description of the
display windows and the data that will be displayed
at the bottom of the requesting MFD.
• Window 1 (figure 7-5), will display the location of
the selected missile with L signifying the Left pylon
or R signifying the Right pylon.
• Window 2 (figure 7-5), will display the station
(1-3, 6-8) of the selected missile.
• Window 3 (figure 7-5), indicates the missile type
(e.g. AGM-158A) of the selected missile.
• Window 8 (figure 7-5), will display ON or OFF to
indicate whether or not missile telemetry power has
been commanded.
NOTE
The telemetry command is initialized to off
and the command state is displayed anytime the display is requested, regardless of
WIU or missile power status.
• Window 9 (figure 7-5), will display MAN LNCH
REQ if the missile does not meet the requirements
for launching the missile in automatic launch mode.
A manual launch will be required if any of the following occurs:
1. Selected missile has a non-fatal fault requiring manual launch.
2. Selected missile does not indicate AUR
READY = TRUE (SAFE TO RELEASE =
TRUE).
3. Selected missile indicates In-Range LAR =
TRUE and In-Zone LAR = FALSE.
4. Selected missile indicates In-Range LAR =
TRUE and In-Zone LAR = TRUE and past
the closest point of approach.
• Window 10 (figure 7-5), will display station ejector status as either blank, UNLOCKD or
NOT_UNLKD to indicate the ejector status at the
station.
1. The field will be blank if no weapon is present or WIU power for this pylon is off.
2. UNLOCKD will appear if the ejector locked
status is false and unlocked status is true.
3. NOT_UNLKD will appear if an illegal ejector status is detected.
T.O. 1B-52H-34-2-8
• Window 11 (figure 7-5), displays the configuration
ID of the selected missile.
• Window 14 (figure 7-5), will display a K in normal video to indicate keys are present in the missile. If the missile fails to indicate Crypto Keys
Present subsequent to a successful Crypto Key
Present indication, the SMO will resend the keys
and the normal video K will remain displayed. The
K in reverse video indicates keys are in error or
have not been received. A blank window indicates
the missile is powered off or no targeting data has
been downloaded to the missile.
• Window 15 (figure 7-5), will display ON, OFF, or
HOT to indicate the missile timer status.
1. ON will be displayed, if the missile is currently powered on and neither an Overheat
Warning nor an Overheat Caution exist for
the missile.
2. OFF will be displayed, if the missile is currently powered off.
3. HOT will be displayed in reverse video, if
the missile is currently powered on and
there is an Overheat Caution issued for the
missile. This indicates the missile may overheat during its mission, if not released
within 10 minutes.
4. HOT will be displayed in blinking reverse
video, if the missile is currently powered on
and there is an Overheat Warning issued
for the missile. This indicates the missile
may overheat during its mission, if not released within 1 minute.
• Window 16 (figure 7-5), will indicate the hours
and minutes that the missile has been either ON
or OFF, or the elapsed time since either an Overheat Caution or an Overheat Warning was issued.
The text and associated indications for station status on the JASSM Status and Inventory display are
outlined in the following paragraphs. All of these
fields will be blank for a station if either the WIU is
not powered on for that pylon or if no missile is
present at the station.
Weapon Type
TEXT
VIDEO
INDICATION
M1
Normal
Prior to initial weapon power application, loaded sortie mission
identifies
missile
type
is
AGM-158A;
or
After initial weapon power application, both loaded sortie mission and
weapon identify the same missile
type as AGM-158A.
M1
Reverse
Sortie mission identifies an
AGM-158A but the missile at station is a different variant;
or
A non-JASSM sortie is loaded after
the missile type was identified as
an AGM-158A.
M
Normal
A sortie mission is not loaded and
after weapon power application,
the missile is a JASSM (SIT and
Go/No-Go test only);
or
A different JASSM variant sortie
mission is loaded prior to initial
weapon application;
or
A different JASSM variant sortie
mission is loaded and after weapon
power application, the weapon is
an AGM-158A.
M
Reverse
A non-JASSM sortie mission is
loaded and after initial weapon
power is applied, the weapon present is a JASSM;
or
An AGM-158A sortie mission is
loaded with no weapon identified
for this location and after initial
weapon power is applied, the
weapon present is a JASSM (WPN
PRSNT master fault).
P
Normal
Prior to initial weapon power application during SIT or Go/NoGo
testing with no sortie mission
loaded, a weapon is present, but is
of unknown type.
P
Reverse
Prior to initial weapon power application a non-JASSM sortie mission is loaded;
or
Prior to initial weapon power application JASSM mission data indicates an empty station (WPN
PRSNT master fault);
or
After weapon power application is
attempted a non-JASSM weapon
is present (STORE ID master
fault).
The weapon presence field, window 2, on FRMT-7
the JASSM Status and Inventory display (figure
7-4), indicates what the SMO identifies as present
at the umbilical based on the data available from
the ejector, WIU and missile.
Blank
Location WIU power Off or weapon
power Off.
7-11
T.O. 1B-52H-34-2-8
Missile Status
TEXT
The missile status field, window 3, on the FRMT-7,
JASSM Status and Inventory display (figure 7-4),
indicates the status of the missiles.
nn
Normal
The missile is assigned to launch
point nn (nn= _1 to 99) or the missile has been launched against the
target.
TEXT
nn
Bright
The missile is in the process of
being targeted to launch point nn.
nn
Bright/
Underline
The missile has been successfully
targeted to launch point nn
nn
Reverse
The missile has failed to target successfully.
OF
VIDEO
Normal
INDICATION
WIU Power for the Location is On
and missile power for specific missile is Off. (115-volt ac power is applied to the missile. 28-volt dc #1
power is off)
VIDEO
INDICATION
ON
Normal
Missile power is On for specific
missile. (Both 28-volt dc #1 and
115-volt ac power are applied to the
missile.)
Dn
Normal
The missile is assigned to Direct
target Dn (n= 1 to 6) or the missile
has been launched against the direct target.
NG
Reverse
Permanent Fatal Fault has occurred for this missile or abort has
been commanded prior to release
attempt. All power (both 28-volt dc
#1 and 115-volt ac power) has been
removed from the missile. Power
application is inhibited.
Dn
Bright
Direct target Dn has been assigned
to the missile and targeting has
been initiated.
Dn
Bright/
Underline
Direct target Dn has been assigned
to the missile and targeting has
been loaded and verified.
Mission capable missile. Safe to release with launchable alignment
status. Manual launch required.
(Both 28-volt dc #1 and 115-volt ac
power are applied to the missile.)
Dn
Reverse
The missile has failed to target successfully.
GO
GO
Normal
Bright/
Underline
Fully Mission capable missile. All
Up Round Ready with launchable
alignment status. (Both 28-volt dc
#1 and 115-volt ac power are applied to the missile.)
CL
Normal
Captive Carry missile launched
(simulated launch). (Both 28-volt
dc #1 and 115-volt ac power are applied to the missile.)
X_
Normal
Weapon not present and no presence discrepancy exists.
No power applied.
X_
Reverse
Weapon not present and Weapon
presence discrepancy exists.
No power applied.
Blank
Blank
The missile has not started the targeting process.
Missile GPS Alignment Quality
The missile alignment quality field, window 6, on
FRMT-7, the JASSM Status and Inventory display
(figure 7-4), indicates the quality of GPS data. The
missile transfer alignment quality field will display
1 or 10 indicating the quality of each missile’s alignment. Display of the transfer alignment quality in
reverse video indicates an alignment failure has occurred and [AMI] persisted for a minimum of 10
minutes.
NOTE
A transfer alignment quality of 1 is required for launch.
WIU Power for the Location is Off.
In conjunction with window 6, the FMS primary
navigation mode used to align the missile is displayed in window 11.
Launch Point/Target Number Indicator
The missile launch point/target number field, window 4, on the FRMT-7, JASSM Status and Inventory
display (figure 7-4), indicates the launch point or direct target number for the specified missile. In conjunction with windows 4 and 7, window 12 (DTU/
DTC) indicates the missile mission DTUC/DTC has
failed anytime a missile is operational when the SMO
requests GPS almanac, GPS AS status/SV configuration data, GPS crypto keys, or missile TDS.
7-12
Change 3
NOTE
In order to achieve good missile alignment
quality (1), an INS/INU must be selected as
the primary FMS navigation mode.
T.O. 1B-52H-34-2-8
Missile Data GPS Status
Missile Fault Status
The missile GPS status field, window 7, on
FRMT-7, the JASSM Status and Inventory display
(figure 7-4), indicates the status of missile GPS
data. If a missile has successfully completed a classified data erase ER is displayed in window 7. If the
classified data erase was unsuccessful, the ER will
be in reverse video. BT is displayed when the missile is in IBIT. If a missile indicates a combined loss
of crypto keys, AUR ready, and minimum GPS, the
text IN will be displayed in window 7. The missile
status indicators that may be displayed in window
7 are listed below.
The missile fault field, window 9 on FRMT-7,
JASSM Status and Inventory display (figure 7-4),
indicates any missile faults present. The highest
priority fault will be displayed in window 9 if more
than one fault exists. The missile faults, which may
be displayed in window 7 on FRMT-7xy, the JASSM
Status and Inventory display with Selected Station
Status (figure 7-5), and their description are provided in the Station Master Faults, this section.
TEXT
VIDEO
INDICATION
Missile In-Range/In-Zone Status
The missile In-Range/In-Zone status field, window
8, on FRMT-7, the JASSM Status and Inventory
display (figure 7-4), indicates the In-Range/In-Zone
status of the missiles.
BT
Normal
Missile is in IBIT.
ER
Normal
Missile Mission data is erased.
ER
Blinking
Missile Mission data erase in
progress.
R
Normal
Missile is In-Range.
Normal
Missile is In-Zone.
TEXT
ER
Reverse
Missile Mission data erase failure.
Z
IN
Normal
Missile is in Initialization.
Blank
IN
Reverse
Initialization fault has occurred.
MG
Normal
Missile has received minimum
GPS.
MG
Reverse
Minimum GPS received and
Ephemeris Received fault occurred.
TK
Normal
Missile is tracking at least 4
satellites.(Test launch only).
WU
Normal
Missile in Warm-up.
WU
Reverse
Warm-up fault or missile heater
power fault has occurred.
Blank
WIU or missile power has not been
applied.
VIDEO
INDICATION
Otherwise.
Ejector State
The ejector state field, window 10, on FRMT-7xy,
the JASSM Status and Inventory display with Selected Station Status (figure 7-5), indicates the
state of missile ejectors.
TEXT
VIDEO
INDICATION
UNLOCKD
Normal
Ejector locked status indicates
unlocked.
NOT
UNLKD
Reverse
Ejector status cannot be determined.
Blank
Missile is not present or WIU
power for the location is off.
In conjunction with window 7, window 13 (IU) indicates the IU has failed or there is no communication with the IU any time the WIU is operational
when the SMO requests GPS almanac, ephemeris,
GPS time mark, or crypto key data.
In conjunction with window 7, window 14 (GPS) indicates the GPS is faulted by the IU any time the
WIU is operational.
7-13
T.O. 1B-52H-34-2-8
JASSM Status and Inventory Display (FRMT-7)
Less [AMI]
SAMPLE
PMD
1
2 M 1 −GO / 1 0 C
0 1 / MG
1 2 − 3 / 4 5
6 / 7
8
2
R I GHT 2
Z
1
3
L EF T
3
3
R I GHT 1
R I GHT 3
9
7
7
L EF T
6
7
R I GHT 7
6
8
L EF T
6
L EF T
11
12
10
− − FRMT − 7
8
8
R I GHT 6
13
R I GHT 8
14
15
16
17
A75616
[AMI]
SAMPLE
PMD
R I GHT 2
1
3
1 2 − 3 / 4 5
6 / 7
8
9
2
1
2 M 1 −GO / 10 C
0 1 / MG
Z
L EF T
3
R I GHT 1
3
7
7
L EF T
6
7
R I GHT 7
6
8
L EF T
10
− − FRMT - 7
R I GHT 3
6
L EF T
11
12
8
8
R I GHT 6
13
C F - DF = P AGE FWD
14
R I GHT 8
15
16
17
C F - DB = P AGE B ACK
B41366
Figure 7-4
7-14
Change 2
T.O. 1B-52H-34-2-8
JASSM Status and Inventory Display with Selected
Station (FRMT-7,xy)
SAMPLE
PMD
2 M 1 −GO / 1 0 C
0 1 / MG
Z
1
2
R I GHT 2
3
L EF T
1
2
L EF T
3
3
R I GHT 2
7
7
L EF T
6
7
R I GHT 7
8
L EF T
R I GHT 3
6
6
L EF T
8
8
R I GHT 6
R I GHT 8
− − FRMT − 7 XY
12
3
11
8
T LMY
7
EJ
1 5 T I ME
4 / 5 6
12 / 13
14
9
10
16
A75617
Figure 7-5
MISSILE POWER REMOVAL
Missile initialization power will be removed when
the operator depresses the desired Location (left
and/or right) and Station (1, 2, 3, 6, 7 and/or 8 or
ALL) switches on the WCP and momentarily moves
the WPN PWR switch to the OFF position. Subsequently, the selected missile(s) will be powered off.
Missile heater power (115-volt ac) will remain on as
long as the respective WIU remains powered.
The operator can verify completion of the missile
initialization power off sequence by viewing
FRMT-7 or FRMT-7xy. When the sequence is complete, the following display changes will occur on
FRMT-7 or FRMT-7xy next to each selected WIU
station number within 2 seconds:
• The missile fault display window will continue to
display the highest priority fault indication if any
missile faults have been detected at the station. All
missile faults are listed and described at the end of
this Section.
The following limitations apply to missile power removal:
• The missiles selected cannot be pylon stations 4
or 5.
• A missile must be present at selected station.
• Missile power removal will not be performed for
any missile to which an Commit To Separate (CTS)
command has been issued.
• Missile CDE is not in progress.
• The missile status window will change to OF in-
dicating missile initialization power is not available
at the station.
Change 2
7-15/(7-16 blank)
BLA
T.O. 1B-52H-34-2-8
MISSILE MISSION DATA AND TARGETING
Automatic Targeting
Prior to launching a missile, targeting data must be
provided to the missiles. JASSM missions are preplaned and loaded onto a B-52 DTUC/DTC and Less
[AMI] associated missile DTUC(s). Subsequently the
missile targeting data is downloaded to the missiles
prior to launch. In addition, the operator may perform
direct targeting as required.
Each missile must be targeted prior to launch. Missile target data set is automatically transferred to a
missile when:
MISSILE TARGETING METHODS
This paragraph describes the types of missile targeting requests, targeting data items, and the processes
for entering, modifying, and reviewing missile targeting data. The SMO supports four types of missile targeting requests as described in the following paragraphs:
• Automatic targeting.
• Manual targeting (CF-586).
• Retarget-all (CF-589).
• Direct targeting (CF-588,n).
Only one targeting request is allowed to be in progress at any one time.
The following targeting operations will be terminated, if active, when a valid Retarget-all (CF-589) or
a Load B-52 Mission Data (CF-81,n) is entered.
• Manual targeting.
• Direct targeting.
• Automatic Targeting.
Less [AMI] Reconfiguration of the Hot Spare as the
Controls and Display (CAD) or Navigation and Weapon Delivery (NAWD) processor will terminate any active targeting operations and update any targeting
display associated with that targeting operation to indicate targeting did not complete. The operator is required to re-enter the appropriate command to restart the targeting operation. If a CF-DD command
was entered for a Direct Targeting operation, the target assignment will be removed from each missile
previously selected.
[AMI] Reconfiguration of the processor will terminate any active targeting operation and update any
targeting display associated with that targeting operation to indicate targeting did not complete. The operator is required to re-enter the appropriate command to restart the targeting operation. If a CF-DD
command was entered for a Direct Targeting operation, the target assignment will be removed from each
missile previously selected.
• Missile power application and initialization is
complete.
• A B-52 mission is loaded which contains
•
•
•
•
•
JASSM targets, the JASSM SMO is loaded,
and missiles are assigned to the appropriate
launch points.
Less [AMI] A missile mission DTUC associated with the B-52 mission is accessible.
[AMI] A weapon mission group associated
with the B-52 mission is accessible.
The missile is not currently targeted.
No other targeting operation is active.
Automatic Targeting is enabled on CF-58.
Less [AMI] If a missile mission DTUC is not accessible, automatic targeting will remain suspended
until a missile DTUC is accessible. If the missile
mission DTUC becomes unaccessible while automatic targeting is in progress, targeting will resume when the missile mission DTUC is accessible
again and no other targeting operations are active.
[AMI] If a weapon mission group is not accessible,
automatic targeting will remain suspended until a
weapon mission group is accessible. If the weapon
mission group becomes inaccessible while automatic targeting is in progress, targeting will resume
when the weapon mission group is accessible again
and no other targeting operations are active. If the
faults JASSM WPN DATA?? and xy:WPN NOGO
occur in conjunction, the operator must select
another weapon group.
If missiles have been targeted and a B-52 mission is
subsequently reloaded, all missiles that were
loaded with preplanned targeting data will be considered untargeted and automatic targeting will be
performed on those missiles. Missiles that have
been loaded with direct targeting data will not be
retargeted. A Retarget All command (CF-589) or
manual targeting Missile Target Assign (Manual
Targeting) command (CF-586) will be necessary to
retarget missiles that have been direct targeted.
NOTE
Targeting may take up to two minutes. A
weapon may fail if the OAS is transferring
data to the weapon. Attempt to retarget the
weapon.
Change 3
7-17
T.O. 1B-52H-34-2-8
The missiles are targeted with specific targeting
data as directed by the B-52 mission that is loaded.
After power is applied and initialization is complete
for a missile, targeting data will be transferred to
that missile. If power is applied to several missiles,
targeting data will be transferred to missiles as directed by the B-52 mission. While targeting data is
being transferred, the launch point or target number associated with the targeting data being transferred will be displayed bright video in window 4
for that missile on the FRMT-7 display (figure 7-4).
The mission group identifier will be displayed in
window 5. After the transfer of targeting data has
completed successfully, the launch point or target
number will be displayed in bright underline video
in window 4. Automatic retargeting of all missiles
can be initiated manually by entering a CF-589
command.
JASSM Target Assignment (CF-586) (Manual Targeting)
The manual targeting request allows the operator
to command the transfer of targeting data associated with specific launch points to selected missile(s).
This is initiated by operator entry of CF-586. The
Manual Targeting display as shown in figure 7-6,
will be displayed on the selected MFD. The operator
will then select a launch point and mission group
identifier of the targeting data to be transferred,
via a MDFY-1 command. Subsequently, the operator will choose the missile to receive the targeting
data via a MDFY-6 command. A CF-DD command
will initiate the transfer of designated targeting
7-18
Change 2
data to the selected missile. A CF-DE command will
exit the current targeting request without transferring targeting data to any missile. The active targeting operation may also be deactivated by removing the display associated with the current targeting request from all MFDs, prior to CF-DD.
Retarget All (CF-589)
The operator can initiate the transfer of preplanned targeting data to all missiles as directed by
the currently loaded B-52 mission by entering a
CF-589 command.
Once a CF-589 command is accepted, all missiles
will become untargeted and the SMO will halt any
targeting in progress. The SMO will then restore
the missile assignment data to the original values
of the B-52 mission that is loaded and initiate automatic targeting of all missiles assigned to a launch
point or target with the pre-planned targeting data.
This will result in the loss of targeting data previously transferred to the missiles. Targeting data
will not be transferred unless the same conditions
exist as for automatic targeting. Missiles that do
not have power applied or have not completed the
power-on sequence will be targeted when missile
power is applied.
NOTE
A retarget-all command requires approximately 2 minutes per JASSM on the aircraft.
T.O. 1B-52H-34-2-8
JASSM Target Assignment (Manual Targeting)
Display (CF-586)
[AMI]
Less [AMI]
Figure 7-6
Change 3
7-19
T.O. 1B-52H-34-2-8
Direct Targeting (CF-588,n)
Direct target definition and assignment allows the
operator to specify a target that is not included as a
preplaned mission. This process is initiated by the operator entering CF-588,n. The Direct Target screen,
figure 7-7, will be displayed on the selected MFD. A
missile assigned to a direct target will generate its
own route to intercept target azimuth. Waypoints
cannot be specified for a direct target. The direct target request allows the operator to specify a direct target to be assigned to a missile. The operator can enter
the target latitude, longitude, elevation, and Less
[AMI] target elevation reference, by entering a
MDFY-1 command. The missile’s cruise altitude can
be specified by entering a MDFY-2 command. The
MDFY-3 command allows the operator to enter a
bearing to target and impact angle. The fuze mode of
soft impact or hard impact can be specified by entering a MDFY-4 command. The fuze delay time can be
specified by entering a MDFY-5 command. By entering a MDFY-6 command, the operator can choose the
missile to receive the direct target data.
Operator entry of CF-Dn, where n represents the
number of the direct target to receive the copied direct
7-20
Change 3
target data, will result in the Direct Target currently
displayed being copied to direct target n. A confirmation prompt, OVERWRITE DATA? (YES/NO) will be
displayed requesting confirmation to overwrite the
existing direct target data for direct target n with the
current direct target data. A YES response to the confirmation prompt will result in overwriting the target
data for direct target n and any missiles previously
assigned/targeted to direct target n will be unassigned/untargeted. A NO response to the confirmation prompt will result in abandoning the CF-Dn command, leaving the direct target n data and missile assignment and targeted states unchanged. If the confirmation prompt is unanswered after 60 seconds, the
default answer of NO will be assumed.
A CF-DD command with missiles selected, will initiate the transfer of the direct target data to the selected missile. A CF-DD command without a missile
selected will save the data without transferring data
to any missile or changing the assignment status or
targeting status of any missile. A CF-DE command
will exit this targeting request and not transfer the
targeting data.
T.O. 1B-52H-34-2-8
Direct Target Definition Display (CF-588,n)
Less [AMI]
[AMI]
1
D I RECT TGT
2
L AT
3
1 TGT P T
6
2 CRU I SE AL T
7
3 BRNG TO TGT
4 F UZE MODE
5 F UZ E DE L AY
CF - DD =DONE
L ONG
4
9
11
’
’
o
o
8
I MP ACT ANGL E
10
AL T
5
1 − SOF T 2 −HARD
( 0−7 )
CF - DE = E SC
CF - DN =COP Y TO D I R TGT ( D 1 −D 6 )
6
13 13 13 13 13 13
13 13 13 13 13
13
12
(ALL TOP BOXES)
WPNS TO SE L ECT
1 4 OF 1 5
− − − −CF - 5 8 8 n
’
ENTER
E
TO
SE L ECT OR
0
TO DE L E TE
A75613
Figure 7-7
Change 3
7-20A
T.O. 1B-52H-34-2-8
Targeting Data Items
BEARING TO TARGET
Direct target definition (CF-588) and manual targeting (CF-586), require data item entry/modification by the operator initiated by MDFY-n, where n
represents the MFD line number associated with
the data to be entered/modified. Several data items
are common to the Manual Targeting and Direct
Target Definition displays. The operator will use
the same missile selection process for manual targeting and direct target assignment. If the operator
enters an invalid command through the IKB, the
command will be displayed in reverse video. If the
operator enters invalid data values, the affected
data fields will be displayed in reverse video.
The bearing to target specifies the weapon’s terminal ground track to the target (figure 7-8). The desired bearing to target is entered in window 7,
(figure 7-7) of the Direct Target screen (CF-588).
The valid input values are from 0 to 360 degrees (0
= North) and 999, the default value, which indicates the missile will use the angle from the aircraft
to the target at point of release, as the bearing to
target.
LAUNCH POINT NUMBER
In order to manually target a missile, the operator
must select the launch point number associated
with the target. The launch point number is entered in window 2, (figure 7-6) of the Manual Targeting display (CF-586). The input is numeric and
ranges from 1 to 99. Only the numbers of launch
points defined by the B-52 mission to be launch
points for the SMO that is loaded are valid.
MISSION GROUP IDENTIFIER
Along with the missile event selected in window 2,
(figure 7-6) the mission group identifier associated
with that launch point is entered in window 3 of the
Manual Targeting display, (figure 7-6). Valid IKB
input entries for window 3 are A, B, C, D, E, F, or it
may be left blank. If it is left blank, the currently
identified mission group will be assumed. If no mission group has been preplaned, a default mission
group A will be assumed. The range of valid alpha
characters (A-F) is dependent on the quantity of
mission groups associated with the launch point
and missile type currently loaded.
TARGET IMPACT ANGLE
The target impact angle specifies the angle in degrees, relative to local level plane at the target (figure 7-8). The impact angle is entered in window 8
of CF-588, the Direct Target screen (figure 7-7). The
valid input values are from 0 (level) to 90 (vertical)
degrees. The default impact angle is 60 degrees.
NOTE
If less than 20 is entered for an impact
angle, the missile will use a built in minimum value of 20. If more than 70 is entered
for an impact angle, the missile will use a
built in maximum value of 70.
CRUISE ALTITUDE
The cruise altitude indicator, window 6, is used to
specify a cruise altitude (MSL) for the JASSM on
CF-588, the JASSM Direct Targeting display (figure 7-7). Valid entries for this field range from 0 to
45000 feet (MSL) and 99999, the default value, displayed prior to operator entry. Although entries
from 0 to 45,000 feet are permitted, the missile will
not fly above 22,000 feet. The missile uses 15,000
feet as the default value (99999).
FUZE MODE
TARGET LOCATION
The target location is the geographical position and
elevation which a missile is to strike. The target
location data fields appear on the direct target definition screen (CF-588), figure 7-7. The position
entry key fields are:
• Target point reference latitude in degrees, minutes, and ten-thousandths of a minute.
• Target point reference longitude in degrees, minutes, and ten-thousandths of a minute.
• Target point reference elevation ([AMI] MSL;
Less [AMI] MSL or HAE) in feet.
• Less [AMI] Target point elevation reference
(HAE or MSL).
All data on pages 7-20C through 7-20D (Deleted).
7-20B Change 3
The fuze mode indicator, window 9, (figure 7-7), is
used to specify a fuze mode of either soft impact referenced to Crush Switch, or hard impact referenced
to G-force Sensor. On CF-588, the JASSM Direct
Targeting display. The operator can select a fuze
mode of Soft by entering 1 or a fuze mode of Hard
by entering 2. The text SOFT or HARD will be displayed in window 10, depending on the fuze mode
selected. A default value of 1 (Soft) is displayed
prior to operator entry.
T.O. 1B-52H-34-2-8
JASSM Target Definition
Figure 7-8
FUZE DELAY
MISSILE SELECTION INDICATOR
Fuze delay in milliseconds can be specified by entering a corresponding delay entry number in
window 11, of the JASSM Direct Targeting display
(CF-588) figure 7-7. Valid entries are shown in the
table below. A fuze delay will delay detonation from
the time of impact by the specified time value. A default value of 0 is displayed prior to operator entry.
The missile selection indicator, window 12, is used
when selecting missiles during a manual targeting
or direct target definition operation. Valid entries
are E and 0 (zero), where E indicates that the corresponding missile is selected for targeting and 0 indicates the missile is not selected. Window 12 will
be blank when any of the following conditions are
true:
VALID ENTRIES
MILLISECOND DELAY
0
0
1
10
2
15
3
20
4
30
5
40
6
50
7
120
• The missile is not present
• The missile is not selected and is unavailable for
selection due to a permanent fatal fault prior to
a CF-DD command.
• The missile is not present or is unavailable for
selection due to a permanent fatal fault following
a CF-DD command and is not a selected missile.
7-21
T.O. 1B-52H-34-2-8
TARGETING TECHNIQUES
NOTE
This section describes the methods and procedures
used when entering targeting data for the following
targeting operations:
• Manual targeting.
• Direct targeting.
When a targeting display is initially requested, the
associated targeting operation becomes active. Subsequently, the same targeting display can be requested on another MFD by entering the associated
targeting display request command while that targeting operation is active. This capability can be
used to allow the other operator to view targeting
data. Once the targeting display is requested on
another MFD, the targeting process control commands, CF-DD and CF-DE, can also be entered for
that MFD. By using this method, the operators will
be able to view and confirm data that is being entered or continue the targeting process if an IKB
failure occurs.
NOTE
If data is being entered by both operators,
data input by one operator can be overwritten by data input by the other operator.
Once a target data set modification or direct targeting operation has been completed via a CF-DD command, that targeting operation is no longer active.
The manual targeting operation will remain active
after a CF-DD command has been entered. Once a
manual targeting or direct targeting operation has
been exited using a CF-DE command, that targeting operation will no longer be active.
NOTE
An active targeting operation will also be
deactivated if the display associated with
the active targeting operation is removed
from all MFDs or a valid Retarget All command (CF-589) or Load B-52 Sortie Mission
Data (CF-81,n) command is entered.
If the operator enters an invalid command through
the IKB, the command is displayed in reverse video. If an invalid value is input in more than one
field, only the first field with an invalid value is
displayed in reverse video when the ENTER key is
pressed. If a valid value is input for that window,
the next window with an invalid value is displayed
in reverse video on MFD command line.
7-22
Do not initiate a manual targeting or direct
targeting operation to weapons that have
not achieved a GO status (FRMT-7, JASSM
Status).
Missile/Target Assignment (Manual Targeting)
Data Entry Process
To perform the manual targeting operation, the
Manual Targeting display (CF-586) must be displayed on the selected MFD. The Manual Targeting
display is shown in figure 7-6. The detailed data
entry process is described below.
A.
Enter CF-586.
NOTE
A CF-DE command can be entered to abandon the manual targeting operation at any
time. When a CF-DE command is entered,
the manual targeting operation is terminated, and all associated targeting displays
will remain displayed and updated. The targeting availability status for each location/
station, window 5, figure 7-6 will continue
to be statused. All remaining windows will
be blanked.
Upon entry of a valid CF-586 command:
CF-586 display will be presented on the selected
MFD as shown in figure 7-6.
The location and station of each missile that is
present and available for selection is displayed in
window 6. The locations are assigned from left to
right across the screen in the preferred launch sequence, figure 7-21. This status is continually updated while the manual targeting display is present
on the MFD.
Blanks are displayed in the column location reserved for each missile that is not present or not
available for selection due to a permanent fatal
fault.
• Targeting data loading status (window 1).
• Launch Point number (window 2).
• Mission group identifier (window 3).
• Missile selection status indicator (window 4).
• Number of missiles remaining to be selected
(window 6).
• Number of missiles required (window 7).
T.O. 1B-52H-34-2-8
B. Enter MDFY-1 to copy line 1 to the MFD command line for modification.
The information contained on line 1 is copied to the
MFD command line as:
1 LAUNCH POINT (1-99) nn MISSION GROUP
(A-F) a
NOTE
Modifiable fields are shown in boldface for
convenience, but are highlighted as defined
when displayed on the MFD.
C. Enter the desired launch point and mission
group identifier.
nn is the desired launch point number, where nn is
a valid JASSM launch point number from 01 to 99.
The remaining number of missiles to be selected, if
any, is displayed in window 6. JASSM targets require only one missile.
• The value in window 6 should be 1 when no
weapon is selected or 0 when one weapon is
selected. If more than one missile is selected,
the difference is displayed as a negative number in reverse video.
NOTE
If more than one missile is selected, all selected missiles will have ranging inhibited until corrected by the operator. CFDD, CF-DE, or leaving the CF-586 screen
are sufficient to remove the inhibit.
• If no missile is selected, a 1 is displayed in
normal video indicating that one missile remains to be selected.
a is the desired mission group identifier, where a is
any value from A to F. The mission group identifier
default is A.
The contents of window 4 will be updated to show
which missiles are assigned.
Upon entry of the launch point and mission group,
the missile assignment is indicated by an E in window 4. Missiles not assigned to the launch point
will be indicated with a 0 in window 4.
If more than one missile is selected, the least preferred missiles will be deselected by the SMO to reduce the number of missiles selected to one missile
required for the designated target when a CF-DD
command is entered. The contents of window 6 will
be updated with a 0 displayed in normal video. The
contents of window 4 will then be updated to show
which missile is assigned.
D. Enter MDFY-6 to copy line 6 to the MFD command line for modification
The information contained on line 6 is copied to the
MFD command line as:
6xxxxxxxxxxxx
The instruction ENTER E TO SELECT OR 0 TO
DELETE is displayed on the bottom of the MFD.
E. Key in the desired missile assignment indicator as follows:
G. Enter CF-DD to save the target data and initiate the downloading of the targeting data to the selected missiles.
NOTE
A CF-DD command will be accepted only after the missile launch point number and
mission group identifier have been input,
one missile required has been determined,
and the Less [AMI] missile mission DTC
([AMI] Weapon Group Data) is accessible.
x is the indicated missile assigned to the indicated
missile launch point or launch point and mission
group identifier. Input is either E to indicate the
missile has been selected, or 0 to indicate the missile is not selected.
The currently selected missile and the missile currently assigned will be set as untargeted.
NOTE
NOTE
Only one missile is required for assignment
to the designated launch point. If more than
one missile is selected, ranging will be inhibited for all selected missiles while manual targeting is active.
These missiles will no longer be targeted to
their previous missile launch point or direct
target.
F. Press the ENTER key. the missile selection
status for the desired missile location/station will
be updated and displayed on line 6.
Change 2
7-23
T.O. 1B-52H-34-2-8
Assignment of selected missiles and the transfer of
targeting data to selected missiles is initiated.
NOTE
Missile power must be applied to a selected
missile in order to be targeted. A selected
missile which does not have power applied
will not be targeted until power is applied
and the manual targeting operation is terminated by either entering CF-DE or by removing the manual targeting display from
all MFDs.
Data modification will be inhibited and associated
targeting displays will remain displayed and updated as follows:
• All line 1 and line 6 modifiable variables will
be blank.
• Windows 6 and 7 will be blank.
• LOADING will be displayed in window 15 in
bright blinking video while the data is being
downloaded to the missiles.
H. The targeting process of each selected missile
can be monitored on the FRMT-7 display. The
CF-586 display will be updated as follows:
If the transfer of targeting data to all selected missiles completes successfully:
• COMPLT is displayed in window 1 in normal
video.
• The location/station of assigned missiles will
•
be displayed in reverse video in the appropriate window 5.
Data will remain displayed in all modifiable
windows and windows 6 and 7.
If the transfer of targeting data to all selected missiles completes unsuccessfully:
• COMPLT is displayed in window 1 in reverse
video.
• The location/station of the unsuccessfully tar•
7-24
geted missile is displayed in reverse video in
the appropriate window 5.
Data will remain displayed in all modifiable
windows and windows 6 and 7.
Direct Targeting Data Entry Process
To perform the direct targeting operation, the Direct Target Definition Display (CF-588) (figure 7-7)
must be displayed on the selected MFD. The process is described in detail below.
A. Enter CF-588,n (figure 7-7) where n (1 to 6) is
the number of the direct target to be defined.
NOTE
A CF-DE command can be entered to exit
the direct target operation without downloading data to the missile at any time prior
to entry of a CF-DD command. When a CFDE command is entered, the direct target
operation is terminated, data modification
is inhibited, and the specified direct target
number will remain displayed on the top of
the MFD. The targeting availability status
for each location/station will continue to be
statused. All remaining windows are
blanked. The direct target data will not be
saved if a CF-DE command is entered. The
previous direct target data is maintained.
Upon entry of a valid CF-588,n command:
The CF-588 display is presented on the selected
MFD.
The identifier n (1, 2, 3, 4, 5, or 6) for the requested
direct target is displayed on the top of the MFD,
window 1. The targeting completion status, window
2 will be blank.
The location and station of each missile that is
present and does not have a permanent fatal fault
is displayed on the bottom of the MFD in a reserved
column location (window 13). The column locations
are assigned from left to right across the screen in
preferred launch sequence. The video mode of window 13 indicates each missile’s targeting availability status (figure 7-7). This status is updated while
the Direct Target Definition display is present on
the MFD.
T.O. 1B-52H-34-2-8
If the requested direct target data is requested for
the first time:
• The target point reference latitude (window 3),
longitude (window 4), and elevation (window 5)
with a default value of 0, Less [AMI] and target
elevation reference (window 6) with a default
value of 1 will be displayed.
• Cruise altitude (window 6) is displayed with
a default value of 99999 feet which indicates
the missile will use the default value of 15000
feet MSL.
• The Bearing to Target (window 7) will have a
default value of 999, which indicates the missile will determine the BTT at the point of
release. Impact angle (window 8) will have a
default value of 60 degrees.
• Fuze mode (window 9) will have a default value of 1, SOFT.
• Fuze delay (window 11) will have a default
value of 0.
If data for the requested direct target has been previously changed and saved, the targeting data for
the specified direct target n is displayed.
The following steps outline the data modification
process which is initiated by entering a MDFY-n
command where n is the line number of the data to
be copied to MFD command line. The steps below
are ordered from entry of a MDFY-1 through
MDFY-6. Data can be entered in any order and sequencing through the lines in order is not required.
B. Enter MDFY-1 to copy line 1 to the MFD command line for modification.
The information contained on line 1 is copied to the
MFD command line as follows:
1 TGT PT addomm.mmmm adddomm.mmmm
fffff’ Less [AMI] r
NOTE
Modifiable fields are shown in boldface for
convenience, but are highlighted as defined
when displayed on the MFD.
C. Key in the desired target latitude, longitude,
elevation, and Less [AMI] elevation reference using
the IKB.
addomm.mmmm is the target latitude (window 3) in
degrees, minutes, and ten-thousandths of a minute.
a = N for North and S for South. dd = degrees from 0
to 90. mm.mmmm = minutes from 00 to 59 and tenthousandths of a minute from 0000 to 9999.
adddomm.mmmm is the target longitude (window
4) in degrees, minutes, and ten-thousandths of a
minute. a = E for East and W for West. ddd = degrees from West 180 to East 179. mm.mmmm =
minutes from 00 to 59 and ten-thousandths of a
minute from 0000 to 9999.
fffff is the target point elevation (window 5) in feet
(MSL, Less [AMI] or HAE). Input ranges from
–328 to 32810 feet.
Less [AMI] r is the target elevation reference (window 6). Valid input is 0 or 1. 0 represents a measurement of MSL for the target point elevation
while 1 indicates HAE.
D.
Press the ENTER key.
The entered latitude, longitude, elevation, and Less
[AMI] target elevation reference will be displayed
on line 1, windows 3, 4, 5 and Less [AMI] 6.
E. Enter MDFY-2 to copy line 2 to the MFD command line for modification.
The information contained on line 2 is copied to the
MFD command line as:
2 CRUISE ALT fffff’
F. Key in the desired cruise altitude using the
IKB.
fffff’ is the desired cruise altitude in feet MSL
(window 6). Valid input range is from 0 to 45000
feet, however, the missile will not fly above 22,000
feet. A value of 99999 is displayed prior to operator
entry, indicating that the default value of 15,000
feet is being used.
G. Press the ENTER key.
H. Enter MDFY-3 to copy line 3 to the MFD command line for modification.
The information contained on line 3 will be copied
to the command line of the MFD as:
3 BRNG TO TGT bbb° IMPACT ANGLE dd°
I. Key in the desired Bearing to Target and Impact Angle using the IKB.
bbb° is the desired bearing to target in degrees
(window 7). Valid input range is from 0 to 360 degrees (0 = North) or 999. The default value of 999 is
displayed prior to operator entry. The default value
indicates that the missile will determine it’s bearing to target from the aircraft to the target at time
of launch.
dd° is the desired impact angle for the missile in
degrees (window 8).
The default impact angle is 60 degrees. Valid input
values are from 0 (level) to 90 (vertical) degrees,
however, the missile will only use an impact angle
ranging from 20 to 70 degrees.
J.
Press the ENTER key.
Change 3
7-25
T.O. 1B-52H-34-2-8
K. Enter MDFY-4 to copy line 4 to the MFD command line for modification.
The information contained on line 4 will be copied
to the command line of the MFD as:
4 FUZE MODE n XXXX
L. Key in the desired Fuze Mode Identifier using
the IKB.
n is the missile’s fuze impact setting. Valid inputs
for fuze mode are 1 (Soft Impact) and 2 (Hard Impact). The default value of 1 is displayed prior to
operator entry.
M. Press the ENTER key.
The entered fuze mode is displayed on line 4, window 9. The corresponding fuze mode of SOFT or
HARD is displayed in window 10.
N. Enter MDFY-5 to copy line 5 to the MFD command line for modification.
The information contained on line 5 will be copied
to the command line of the MFD as:
5 FUZE DELAY n (0-7)
O. Key in the desired Fuze Delay Identifier using
the IKB.
n is a single digit entry that identifies the millisecond fuze delay of the missile. Valid input entries for
fuze delay are 0 through 7.
P.
Press the ENTER key.
The entered fuze delay identifier is displayed in
window 11.
R.
Press the ENTER key.
The remaining number of missiles to be selected, if
any, is displayed in window 14. JASSM targets require only one missile.
• The value in window 6 should be 1 when no
weapon is selected or 0 when one weapon is
selected. If more than one missile is selected
the difference is displayed as a negative number in reverse video.
NOTE
If more than one missile is selected, all selected missiles will have ranging inhibited until corrected by the operator. CFDD, CF-DE, or leaving the CF-586 screen
are sufficient to remove the inhibit.
• If no missile is selected, a 1 is displayed in
normal video indicating that one missile remains to be selected.
The contents of window 12 will be updated to show
which missiles are selected.
If more than one missile is selected, the least preferred missiles will be deselected by the SMO to reduce the number of missiles selected to one missile
required for the designated target when a CF-DD
command is entered. The contents of window 6 will
be updated with a 0 displayed in normal video. The
contents of window 4 will then be updated to show
which missile is assigned.
S. If no other missiles are to be selected, enter
CF-DD to save the direct target data and initiate
the downloading of the targeting data to the selected missiles.
NOTE
Select/deselect missile(s) to be assigned to the designated target as follows:
Q, Enter MDFY-6 to copy line 6 to the MFD command line for modification.
If no missile is selected and a CF-DD command is entered, the data for the designated direct target will be saved.
The instruction ENTER ‘E’ TO SELECT OR ‘0’ TO
DELETE is displayed on the MFD.
Currently selected missiles and missiles currently
assigned will be set as untargeted.
NOTE
NOTE
Only one missile is required for assignment
to the designated direct target. If more than
one missile is selected, ranging will be inhibited for all selected missiles while direct
targeting is active.
These missiles will no longer be targeted to
their previous launch point or direct target.
7-26
T.O. 1B-52H-34-2-8
The SMO will compute the targeting data for each
selected missile and initiate the transfer of that
data to the missiles.
• A selected missile that does not have power
applied will be assigned but not targeted.
Data modification will be inhibited and associated
targeting displays will remain displayed and updated as follows:
• LOADING is displayed in window 2 in bright
•
•
•
blinking video while the data is being downloaded to the missiles.
The specified direct target number will remain displayed in window 1.
The targeting availability status for each location/station, window 13, will continue to be
statused.
All remaining windows will be blanked.
T. The targeting process of the selected missile
can be monitored on the FRMT-7 display.
The CF-588 display will be updated as follows:
1. If the transfer of targeting data to the selected
missile completes successfully:
• COMPLT is displayed in window 2 in normal
video.
• The location/station of assigned missiles is
•
displayed in bright underline video in the appropriate window 13.
All modifiable windows and windows 14 and
15 will be blank.
2. If the transfer of targeting data to the selected
missiles completes unsuccessfully:
• COMPLT is displayed in window 2 in reverse
video.
• The location/station of each missile that was
•
not successfully targeted is displayed in reverse video in the appropriate window 13.
Data will remain displayed in all modifiable
windows and windows 14 and 15.
7-27/(7-28 blank)
BLA
T.O. 1B-52H-34-2-8
TARGET RANGING
The SMO will perform Safe Launch advisories and
LAR achievability/timing calculations for the associated target if any of the following conditions exist:
• A direct target mission has been downloaded into
a missile and that direct target has been selected
as the current weapon event with a PRGM-Dn command.
• The current B-52 mission destination has a
launch point associated with it and an associated
target mission has been downloaded into a missile.
NOTE
Ranging will be inhibited for all selected
missiles on which Manual or Direct Targeting is in progress.
JASSM uses a preplanned Static Launch Acceptability Region (LAR) to determine when a target is
In-Zone for launch. This LAR is determined during
missile mission planning, and used to determine
the B-52 route planning. Figure 7-9 illustrates an
In-Range and static In-Zone LAR.
There are two type of LARs, In-Range and In-Zone.
The In-Range LAR is the larger of the two. Launch
while In-Range, but not In-Zone will command the
missile to fly to the target, omitting all waypoints.
The missile will approach the target from the direction of the waypoint immediately prior to the target. As a result, an In-Range launch does not follow
the preplanned route of flight, and therefore cannot
fulfill a TOT requirement. The In-Zone LAR is
smaller than the In-Range LAR with tighter tolerances on location and heading, allowing a launch
that will follow the preplanned route. The automatic launch point, at the closest point of approach, is
explained further in the In-Zone LAR subsection
and in figure 7-13. If launched at the preplanned
time, the missile will arrive at the target within ±5
seconds of the planned TOT.
JASSM Static LAR
Figure 7-9
7-29
T.O. 1B-52H-34-2-8
The JASSM SMO computes In-Range and In-Zone
achievability, Time to Go (TTG) to the In-Range/InZone LARs, and Time to Go (TTG) out of In-Range/
In-Zone LARs for the ranging event. The SAIR parameters are computed as a function of the LAR
data provided by the missiles, mission data, and the
current aircraft flight conditions. The JASSM SMO
will establish a ranging cycle for polling a missile’s
ranging message and determine the current ranging event in order to provide ranging information
for operator display and launch processing.
The JASSM SMO polls the missile associated with
the current ranging event a minimum of once per
second. For missiles associated with other targets/
launch points (Direct Targets, Next Ranging
Event), the JASSM SMO polls at least one (1) missile every two (2) seconds. However, the JASSM
SMO will attempt a ranging cycle rate of one (1)
missile per pylon per major frame to accommodate
both of these requirements. The JASSM SMO provides the capability to interrupt the ranging cycle
with a higher priority (Current, next, and other direct targets) ranging request for its data.
The JASSM SMO only polls operational missiles
and starts the ranging cycle when the aircraft is
airborne and at least one missile is present and
powered on with Min TXA, Min TDS, and has been
targeted by the JASSM SMO.
All missile stations will be included in the ranging
cycle. If missile ranging cannot be performed because it failed to satisfy the above criteria, the
JASSM SMO marks the missile as not In-Range,
unachievable (clear any steering cues), and ensures
the In-Range TTG values are marked as invalid.
The cycle will continue with the next major frame
with the next missile in the cycle for the respective
pylon.
The JASSM SMO provides In-Range/In-Zone status
indications as follows:
• FRMT-7 Missile Status and Inventory for all
Current Ranging Event
The current ranging event will be determined from
the B-52 Mission data as it is flown by the aircraft
except when pre-empted by operator action. The
current ranging event will be one of the following
missile event types:
• Preplanned JASSM Launch Point.
• Operator created Direct Target.
The current ranging event is defined as the next
planned missile event on the Carrier Mission data
based on the current destination of the aircraft
(current mission leg only) when not pre-empted by
an operator selected missile event. The JASSM
SMO allows the operator to select the current ranging event for direct targets. The JASSM SMO also
allows the operator to select the current ranging
event when the selected destination is a JASSM
launch point. An operator selected ranging event
takes precedence over the next missile event indicated in the carrier mission data. The launch point
must have missiles assigned. Achievability, TTG to
Enter In-Range/In-Zone, TTG to Exit In-Range/InZone and safe launch verification is performed for
the current ranging event. The missile associated
with the current ranging event and the missile entered into launch countdown must be the same missile. During launch countdown, the JASSM SMO
continues the ranging calculations for the current
launch point using the last valid data from the missile prior to commanding Commit To Separate Store
(CTS).
The JASSM SMO terminates the current ranging
event when one of the following occurs:
• The missile event is disabled (missiles per target is less than 1).
• The missile is in the process of being powered
off, or has a power-off fault.
• For direct targets, the operator changes the
system to Automatic Launch mode.
• The current ranging event (non-operator se-
present missiles.
• PRGM Display (Launch and Ranging data) for
•
7-30
the current ranging event and all direct targets.
Missile event recording when there is a
change of status.
•
•
lected ranging event) is not the current (InRange or In-Zone LAR) destination identified
in the Carrier Mission data. (This may occur
due to destination sequencing.)
Operator deselection.
The mission data preplanned launch point is
behind the aircraft and the aircraft has exited
the In-Range LAR.
T.O. 1B-52H-34-2-8
The missile event following the terminated current
ranging event in the Carrier Mission data will become the current ranging event.
The JASSM SMO shall not range on a missile event
if any of the following conditions exist:
• The missile event is disabled (missiles per target is less than 1).
• The missile is not targeted, powered off, is in
•
•
the process of being powered off, or has a power-off fault.
The missile event (non-operator selected ranging event) is not the current (In-Range or InZone LAR) destination identified in the B-52
Mission data (This may occur due to destination sequencing).
Any preplanned launch point occurring prior
to the current destination of the aircraft.
IN-RANGE LAR
The missile provides the characteristics of the InRange LAR and the In-Range status to the JASSM
SMO. The JASSM SMO uses valid In-Range data
from the missile and aircraft prime data to determine In-Range Achievability, TTG to enter and exit
the In-Range LAR. The In-Range calculations are
only performed for the launch points and direct targets identified as the current/next ranging events.
In-Range Achievability
The JASSM SMO sets In-Range Achievable, if the
current aircraft ground track will intersect the InRange circle for the current ranging event. Figure
7-10 illustrates when JASSM is In-Range achievable.
The JASSM SMO processes data to determine if InRange is achievable (value of In-Range circle radius
is greater than the absolute value of Target crossrange) for a JASSM launch by computing the following:
• Range from aircraft prime position to Target
•
using the aircraft prime latitude and longitude from FMS and In-Range LAR latitude
and longitude.
Azimuth of Target with respect to aircraft
prime position relative to North, using the aircraft prime latitude and longitude from FMS
and In-Range LAR latitude and longitude.
• Azimuth of Target with respect to aircraft
•
prime position relative to the ground track
line through aircraft prime position, using the
aircraft prime ground track from FMS and
azimuth of Target with respect to aircraft
prime position relative to True North.
Target downrange and crossrange distance
from aircraft prime position with respect to
aircraft ground track, using the range from
aircraft to Target, azimuth of Target with respect to aircraft position relative to the
ground track line through aircraft position.
JASSM In-Range Unachievable
The geometry defining an unachievable In-Range
LAR is illustrated in figure 7-11. For direct targets
only, the JASSM SMO provides a directional arrow
that points to the target and blanks the TTG InRange, if unachievable, until passing the point of
closest point of approach (CPOA) to the direct target. After passing CPOA for a direct target, the
JASSM SMO will remove the directional arrow,
blank the TTG, and display the In-Range LAR label
in reverse video.
Time to Go to Enter/Exit In-Range
The JASSM SMO computes the TTG to the entry/
exit points of the In-Range LAR when the aircraft
is outside the In-Range circle and In-Range is
achievable. The JASSM SMO computes TTG using
distance to enter/exit In-Range (current prime aircraft position, closest intersection point of aircraft
ground track line with In-Range LAR circle, farthest intersection point of aircraft ground track line
with In-Range LAR circle) and current prime aircraft ground speed from FMS. The TTG displayed
may have an error of up to $5 seconds, however,
when In-Range, 0:00 will be displayed for TTG-R
entry time.
Once the aircraft is inside LAR, the TTG to exit
counts down to zero as the aircraft approaches the
exit point. The In-Range LAR exit point is the point
at which In-Range Achievable transitions from
achievable to unachievable. If TTG to exit is equal
or greater than one hour, the time displayed will be
59:59. The JASSM SMO blanks the TTG when InRange becomes unachievable.
7-31
T.O. 1B-52H-34-2-8
JASSM Achievable In-Range LAR
Figure 7-10 (Sheet 1 of 2)
7-32
T.O. 1B-52H-34-2-8
PMD
1 CPA
800 ’
150 0
D 1 NAV
D1
R2
493
D1
T TG−R 4 5 : 2 0 5 9 : 5 9 TOT
P TA 0 : 0 0 : 0 0
L 10 : 0 4 : 2 2
MAN L NCH REQ
150 0
D 1
D 2 NAV
355
E TE 1 : 2 6 : 5 8 P TA 0 : 1 5 : 2 0
L 1 1 : 16 : 0 0
− − PRGM - D 1
A. PRIOR TO ENTERING IN-RANGE
B40822
PMD
1 CPA
800 ’
150 0
D 2 − NAV
D1
D2
337
L7
P TA 0 : 1 5 : 2 3
L 10 : 3 0 : 5 3
D1
RANGE 0 : 0 0 5 9 : 5 9 TOT 1 4 : 1 5 : 2 5
MAN L NCH REQ
150 0
D 2
D 3 J ASSML P
7
E TE 1 : 0 9 : 5 5 P TA 0 : 1 6 : 5 1
L 1 1 : 3 9 : 14
− − PRGM - D 1
B. IN-RANGE
B40823
Figure 7-10 (Sheet 2 of 2)
7-33
T.O. 1B-52H-34-2-8
JASSM Unachievable In-Range LAR
PMD
1 CPA
800 ’
150 0
D 2 NAV
D1
D2
P TA 0 : 1 5 : 2 0
L 10 : 2 7 : 4 8
336
D2
R 7 T TG−R
TOT
MAN L NCH REQ
150 0
D 2
D 3 J ASSML P
080
E TE 1 : 0 9 : 0 6 P TA 0 : 1 6 : 5 1
L 11 : 36 : 27
− − PRGM - D 2
A. IN-RANGE UNACHIEVABLE ON LEFT
Figure 7-11 (Sheet 1 of 2)
7-34
B40824
T.O. 1B-52H-34-2-8
PMD
1 CPA
800 ’
150 0
D 2 − NAV
D1
D2
P TA 0 : 1 5 : 3 0
L 10 : 14 : 3 5
15 4
D1
L 7 T TG−R
TOT
MAN L NCH REQ
150 0
D 2
D 3 J ASSML P
070
E TE 0 : 5 4 : 3 6 P TA 0 : 1 6 : 5 1
L 1 1 : 0 6 : 12
− − PRGM - D 1
B. IN-RANGE UNACHIEVABLE ON RIGHT
B40825
Figure 7-11 (Sheet 2 of 2)
7-35
T.O. 1B-52H-34-2-8
IN-ZONE LAR
The definition of the In-Zone LAR is illustrated in figure 7-12. The missile provides the characteristics of
the In-Zone LAR and the In-Zone status to the
JASSM SMO. The JASSM SMO uses In-Zone data
from the missile which is marked valid by the missile
and aircraft prime data to determine In-Zone Achievability, TTG to enter and exit the In-Zone LAR. The
In-Zone parameters are displayed on the MFD. When
In-Zone data is invalid, the TTG for the current ranging event missile is displayed in reverse video.
HAE altitude. Speed must be within ± 0.1 True
Mach of preplanned release speed. Heading tolerance is selectable in the AFMSS setup, but is normally ± 20°. Releases should always be at level conditions. Release advisories are provided to the
RN/N in the Program Display to guide the crew to
the correct release conditions.
To achieve In-Zone LAR, the aircraft must be within tolerance of preplanned release conditions. Altitude must be within ± 3000 feet of the planned
Weapon release advisories do not inhibit
launch. Possible collision between weapons
and between weapon and aircraft can occur if
weapon is launched with a release advisory
displayed.
JASSM In-Zone LAR
Figure 7-12
7-36
T.O. 1B-52H-34-2-8
In-Zone Achievability
The JASSM SMO sets In-Zone Achievable to logic
one if the current aircraft ground track will intersect the In-Zone LAR area for the current event. Figure 7-13 illustrates an achievable In-Zone LAR.
The JASSM SMO processes data supplied by the
missile to determine if In-Zone is achievable for a
JASSM launch by computing the following:
• Latitude and longitude for the point of inter-
•
•
section of In-Zone Start Angle and In-Zone
Arc Min Radius, using In-Zone Arc Center latitude and longitude, In-Zone Arc Min Radius,
as the distance d, and In-Zone Start Angle.
Latitude and longitude for the point of intersection of In-Zone Start Angle and In-Zone
Arc Max Radius, using In-Zone Arc Center
latitude and longitude, In-Zone Arc Min Radius, as the distance d, and In-Zone Start
Angle.
Latitude and longitude for the point of intersection of In-Zone Stop Angle and In-Zone Arc
Min Radius, using In-Zone Arc Center lati-
•
•
•
•
tude and longitude, In-Zone Arc Max Radius,
as the distance d, and In-Zone Stop Angle.
Latitude and longitude for the point of intersection of In-Zone Stop Angle and In-Zone Arc
Max Radius, using In-Zone Arc Center latitude and longitude, In-Zone Arc Max Radius,
as the distance d, and In-Zone Stop Angle.
In-Zone approach azimuth with respect to the
point of intersection of In-Zone Stop Angle
and In-Zone Arc Min Radius relative to North.
Range from aircraft position to Waypoint #1
position, using the current aircraft prime latitude and longitude from FMS and In-Zone Arc
Center latitude and longitude.
Azimuth of Waypoint #1 with respect to aircraft position relative to aircraft ground track
line, using the current aircraft prime latitude
and longitude from FMS and In-Zone Arc
Center latitude and longitude.
JASSM In-Zone Unachievable
The geometry defining an unachievable In-Zone
LAR is illustrated in figure 7-14.
JASSM Achievable In-Zone LAR
Figure 7-13 (Sheet 1 of 3)
7-37
T.O. 1B-52H-34-2-8
JASSM Achievable In-Zone LAR (Cont)
PMD
1 CPA
800 ’
150 0
D 3 J ASSML P
15 4
LP03
L 2 T TG−R
T TG− Z
P TA 0 : 1 6 : 5 1
L 9 : 2 4 : 18
4 3 : 2 2 TOT
ROL L
MAN L NCH REQ
150 0
D 2
D 4 −NAV
080
E TE 0 : 0 2 : 4 9 P TA 0 : 1 9 : 3 0
L 9 : 24 : 25
− − PRGM -
A. RANGE CALCULATED, ZONE NOT CALCULATED
B40826
PMD
1 CPA
800 ’
150 0
D 3 J ASSML P
14 7
LP03
L 2 T TG−R
3 : 0 9 5 9 : 5 9 TOT
T TG− Z 2 2 : 5 8
1 : 26
P TA 0 : 1 6 : 5 1
L 9 : 24 : 20
150 0
D 3
D 4 − NAV
050
E TE 0 : 0 2 : 4 9 P TA 0 : 1 6 : 5 1
L 9 : 24 : 30
− −PRGM -
B. RANGE AND ZONE CALCULATED
Figure 7-13 (Sheet 2 of 3)
7-38
B40827
T.O. 1B-52H-34-2-8
PMD
1 CPA
800 ’
150 0
D 3 J ASSML P
D1
P TA 0 : 1 6 : 3 1
L 9 : 24 : 21
33
L2
LP03
RANGE
0 : 0 0 5 9 : 5 9 TOT 1 4 : 1 5 : 3 3
T TG− Z 1 3 : 1 6
1 : 59
MAN L NCH REQ
150 0
D 3
D 4 −NAV
051
E TE 0 : 0 2 : 4 9 P TA 0 : 1 6 : 5 1
L 9 : 24 : 22
− − PRGM -
C. IN-RANGE, NOT IN-ZONE
B40828
PMD
1 CPA
800 ’
150 0
D 3 J ASSML P
D1
D2
P TA 0 : 1 6 : 5 1
L 9 : 19 : 16
0 : 0 0 5 1 : 5 3 T OT 1 4 : 1 5 : 2 0
0 : 00
1 : 22
ROL L
2
LP03
L 2 RANGE
ZONE
150 0
D 3
D 4 NAV
052
E TE 1 : 2 6 : 5 8 P TA 0 : 1 6 : 5 1
L 9 : 19 : 2 6
− − PRGM -
D. IN-RANGE AND IN-ZONE
B40829
Figure 7-13 (Sheet 3 of 3)
7-39
T.O. 1B-52H-34-2-8
JASSM Unachievable In-Zone LAR
PMD
1 CPA
800 ’
150 0
D 3 J ASSML P
D1
P TA 0 : 1 6 : 5 1
L 8 : 43 : 03
0 : 0 0 5 9 : 5 9 TOT 1 4 : 1 5 : 2 0
15 4
LP03
L 2 RANGE
T TG− Z
MAN L NCH REQ
150 0
D 4 −NAV
D 3
052
E TE 0 : 0 2 : 4 9 P TA 0 : 1 9 : 3 0
L 8 : 4 3 : 19
− − PRGM -
B40830
Figure 7-14
7-40
T.O. 1B-52H-34-2-8
Time to Go to Enter/Exit In-Zone
The JASSM SMO computes the TTG to the entry/
exit point of the In-Zone LAR area when the aircraft is outside the In-Zone LAR area and In-Zone
Achievable is achievable. The TTG displayed may
have an error up to $5 seconds with TTG-Z entry
time displayed as 0:00, once In-Zone. When In-Zone
is achievable for a JASSM launch, the JASSM SMO
processes data to determine Time to Go to enter/
exit In-Zone by using the following parameters:
• Distance to go to In-Zone entry point (current
•
prime aircraft position, intersection point of
aircraft ground track line with In-Zone Arc
Max Radius) and current prime aircraft
ground speed.
Distance to go to In-Zone exit point (current
prime aircraft position, intersection point of
aircraft ground track line with In-Zone Arc
Min Radius) and current prime aircraft
ground speed.
Once the aircraft is inside In-Zone LAR, the time to
exit counts down to zero. The JASSM SMO blanks
TTG when In-Zone in unachievable.
Time on Target
The JASSM SMO displays the current Time on Target (TOT) on PRGM screen any time the missile in-
dicates an In-Range or In-Zone status for the current ranging event.
In-Zone Advisories
When In-Zone is achievable for a JASSM launch,
the JASSM SMO shall compute In-Zone advisories
for Altitude, Mach and Heading.
Preplanned Launch Point (Mission Data Preplanned
Missions Only)
The preplanned Launch Point latitude and longitude are identified in the missile Mission data. For
a JASSM Launch Point within the In-Zone LAR,
the JASSM SMO determines the closest point of approach (CPOA) for the preplanned launch point
(JASSM LP). If the closest point of approach is
within the In-Zone LAR, the JASSM SMO will allow an automatic launch at this point. If the closest
point of approach is not within the In-Zone LAR,
but In-Range LAR is achievable, the JASSM SMO
requires a manual launch. Figure 7-15 illustrates
CPOA geometry for a CPOA outside the In-Zone
LAR, but within the In-Range LAR.
For preplanned JASSM launch points which do not
have an In-Zone LAR defined, the JASSM SMO requires a manual launch.
JASSM Closest Point of Approach Outside In-Zone LAR
Figure 7-15 (Sheet 1 of 2)
7-41
T.O. 1B-52H-34-2-8
JASSM Closest Point of Approach Outside
In-Zone LAR (Cont)
PMD
1 CPA
800 ’
150 0
D 3 J ASSML P
D1
D2
P TA 0 : 1 6 : 5 1
L 9 : 53 : 36
0 : 0 0 5 5 : 1 9 TOT 1 4 : 1 5 : 1 7
1 : 59
0 : 12
HDG TOL
MAN L NCH REQ
16
LP03
L 2 RANGE
T TG− Z
150 0
D 3
D 4 − NAV
052
E TE 0 : 0 2 : 5 0 P TA 0 : 1 6 : 5 1
L 9 : 53 : 43
− − PRGM -
A. PRIOR TO IN-ZONE
B40831
PMD
1 CPA
800 ’
150 0
D 3 J ASSML P
D1
D2
P TA 0 : 1 6 : 5 1
L 9 : 53 : 36
0 : 0 0 5 5 : 1 9 TOT 1 4 : 1 5 : 1 2
0 : 00
1 : 23
TRN L EF T
5
LP03
L 2 RANGE
T TG− Z
150 0
D 3
D 4 − NAV
052
E TE 0 : 0 2 : 4 9 P TA 0 : 1 6 : 5 1
L 9 : 53 : 11
− − PRGM -
B. IN-ZONE, OUT OF HEADING TOLERANCE
Figure 7-15 (Sheet 2 of 2)
7-42
B40832
T.O. 1B-52H-34-2-8
TARGET RANGING INDICATIONS
Operator entry of PRGM displays the PRGM screen
(figure 7-16) that will contain ranging data if any of
the preceding conditions exist. Operator entry of
PRGM-Dn displays the PRGM screen with ranging
data for the defined direct target (n = 1 - 6). The following is a summary of the windows which provide
ranging data displayed on the PRGM screen.
• Window 3 displays the JASSM launch point
number or direct target identifier for which ranging
data is being provided.
• Window 4 displays the location/station of the missile assigned to the target. The launch ability and
ranging status of the missile is displayed in this
window.
• The In-Range status is displayed in window 5.
• Window 6 indicates the time to go (mm:ss) in order to achieve In-Range. If the time displayed is
00:00, the aircraft is already In-Range.
• Window 7 indicates the remaining In-Range time
in minutes and seconds if the aircraft continues flying
at the current ground speed, altitude, and ground
track.
• Window 8 displays TOT (Time on Target) label if
the missile is calculating the Time of Flight.
• Window 9 indicates the Weapon TOT which is
calculated by adding the Current Time of Flight
(CTOF) plus UTC when CTOF is returned from a
weapon ranging on a target. CTOF is the time from
release (Umbilical separation) to target impact
based on current aircraft position and heading. If
the aircraft is In-Zone, CTOF represents the estimated flight time from the current aircraft position
to the target along the preplanned flight path. If
the aircraft is In-Range and not In-Zone, CTOF represents the estimated flight time from the current
aircraft position to the target along the In-Range
flight path. TOT is accurate within ±5 seconds only
if the aircraft is In-Zone and the mission is planned
as Time on Target required.
• Window 10 displays an arrow as a steering cue
when the aircraft is not on track and needs to steer
either left ( ← ) or right ( → ) in order to achieve
In-Range. Preplaned targets will not use arrow
steering cues. Direct targets will have arrow steering cues for In-Range only. A blank in window 10
indicates the aircraft is on track to intersect InRange or the target is a preplaned target.
• The In-Zone status is displayed in window 11.
• Window 12 indicates the time to go (mm:ss) in
order to achieve In-Zone. If the time displayed is
00:00, the aircraft is already In-Zone.
• Window 13 indicates the remaining In-Zone time
for a launch point in minutes and seconds if the
aircraft continues flying at the current ground
speed, altitude, and ground track.
• Window 15 indicates seeker guidance capability.
A blank indicates missile has seeker guidance capability, the reverse video text SKR indicates the missile mission requires a seeker and either a terminal
guidance fault exists or a seeker is not available.
• Window 16 indicates launch method requirements. If a manual launch is required, MAN LNCH
REQ will be displayed in bold. If the window is
blank, an automatic launch is permitted.
IN-RANGE/IN-ZONE INDICATION
The In-Range/In-Zone status for missile launches is
provided in windows 5 (Range) and 11 (Zone) of the
PRGM Screen display, see figure 7-16. This status
is displayed in different video modes to indicate
whether the aircraft is approaching In-Range/InZone or is currently In-Range/In-Zone.
NOTE
Once the missile is launched, it will fly
waypoints, if it is In-Zone or was In-Zone in
the last 8 seconds. If the missile was launched
within 8 seconds of exiting In-Zone, In-Range
will be displayed upon launch, but the missile
will fly an In-Zone profile.
WEAPON LAUNCH ADVISORIES
Weapon launch advisories appear on the PRGM
screen display (figure 7-16, window 14) to alert the
aircrew that an action is required to ensure weapon
launch parameters are met. When multiple weapon
launch advisories exist, the highest applicable advisory message will be displayed on the PRGM display. The defined JASSM weapon launch advisories
and the corrective action are contained at the end of
this section in figure 7-23.
NOTE
Weapon launch advisories are calculated by
the aircraft. In-Range and In-Zone indications are independently calculated by the
weapon. Due to differences in these calculations, such as computing method and data
latency, it is possible there may be a difference in the timing of these indications. The
In-Range and In-Zone indications describe
the status of the weapon, and will be honored by the weapon when launched.
7-43
T.O. 1B-52H-34-2-8
safe release advisories and the corrective action are
contained at the end of this section in figure 7-22.
SAFE RELEASE ADVISORIES
The JASSM SMO does not have any safe launch restrictions which would prevent missile launch. The
safe release advisories, displayed on the PRGM
screen, inform the operators of a potentially unsafe
launch condition, however, launch can still be performed.
Safe release advisories do not inhibit launch.
Possible collision between weapons and between weapon and aircraft can occur if weapon is launched with a safe release advisory
displayed.
When multiple safe release advisories exist, the
highest applicable advisory message will be displayed on the PRGM Display. The defined JASSM
PRGM Display In-Range/In-Zone Indications
PMD
1 CP A
D
2
2
2
2
4
10
2
2
3
5
11
1
PTA
6
12
8
7
13
14
16
9
15
D
D
E TE
1
PTA
− − PRGM−
A75619
WINDOW
5
11
DISPLAY TEXT
VIDEO
INDICATION
TTG-R
Normal
Aircraft is approaching In-Range.
TTG-R
Reverse
Aircraft is not In-Range and In-Range is unachievable or
missile is not targeted.
RANGE
Bright Underline
Aircraft is currently In-Range.
TTG-Z
Normal
Aircraft is approaching In-Zone.
TTG-Z
Reverse
Aircraft is not In-Zone and In-Zone is unachievable or
missile is not targeted.
ZONE
Bright Underline
Aircraft is currently In-Zone.
NOTE
In-Range LAR is determined by the missile and retrieved by the SMO In-Range
status and Range distance messages.
Figure 7-16
7-44
T.O. 1B-52H-34-2-8
MISSILE LAUNCH
The missile launch process, including the means for
controlling, suspending, and stopping a missile
launch, as well as launch command restrictions are
described in the following paragraphs. Figure 7-17
shows a Launch Sequence Timeline.
If launch is commanded while either unlock consent
switch is in the lock position, the advisory message
NO CONSENT will be displayed on each MFD.
NOTE
Once the missile is launched, it will fly
waypoints, if it is In-Zone or was In-Zone in
the last 8 seconds. If the missile was launched
within 8 seconds of exiting In-Zone, In-Range
will be displayed upon launch, but the missile
will fly an In-Zone profile.
MISSILE LAUNCH PROCESS
The following provides a summary of the activities
which the SMO will command or control to launch a
missile:
• Apply 28-volt dc #2 power to the missile station.
If unsuccessful, a dc #2 power discrepancy master
fault will be declared as indicated by the text
xy:ACFT PWR displayed as a master fault.
• Issue a Preset-Verify-Execute (PVE) command
sequence to apply Release Consent to the missile.
If the PVE command sequence fails after two
successive issue attempts, a double critical verify
master fault will be issued and indicated by the
text X:CRIT VRFY displayed as a master fault and
WIU power will be removed. A release consent driver failure will be indicated by the master fault text
X:RC DRVR. If the selected station fails to verify on
two consecutive attempts, a double critical function
ejector master fault will be issued and indicated by
the text X:UNCMD PVE displayed as a master
fault and WIU power will be removed.
• Command a Commit to Separate (CTS) command.
• Remove the release consent.
• Verify that missile status indicates the missile
has Committed to Separate Store (CTSS). If unsuccessful, the master fault xy:ABORT will be displayed, the SMO will perform a normal shutdown
of the missile and inhibit reapplication of power to
the missile.
• Remove 28-volt dc #1 and 28-volt dc #2 power. If
unsuccessful in removing either power, WIU status
will indicate a dc power discrepancy master fault
which will be displayed as xy:ACFT PWR or
xy:28-volt dc #2 respectively. If missile communication fails after removal of 28-volt dc #1 and 28-volt
dc #2 power, indicating a battery failure, xy:CTSS
will be displayed as a permanent fatal master fault.
Reapplication of power to the missile is inhibited.
• Apply unregulated 38-volt dc EED power to the
selected location. If unsuccessful, a 38-volt dc EED
uncommanded low fault will be declared as indicated by the text X:EED PWR displayed as a master fault.
• Perform the Ejector Squib Fire PVE sequence. If
a failure exists after two attempts, a double critical
verify fault will be indicated by the text X:CRIT
VRFY displayed as a master fault. An ejector squib
fire driver failure will be indicated by the text
X:SQF DRVR displayed as a master fault. Two subsequent failures to verify the preset will result in
a double critical function ejector selection master
fault being issued as indicated by the text
X:UNCMD PVE being displayed as a master fault
and power being removed from the missile.
• Remove unregulated 38-volt dc EED power from
the selected location. If unsuccessful after two attempts, a 38-volt dc EED uncommanded high fault
will be declared, power will be removed from the
WIU and all missiles associated with the WIU, and
the text X:EED PWR will be displayed as a master
fault.
• Command Critical Terminate to the location.
• Perform missile scoring recording.
• The missile launch advisory will be displayed on
all MFDs. The missile launch advisory will remain
displayed for 5 seconds, then the missile launch advisory will be blanked. The SMO displays appropriate xy (x = L (left pylon) or R (right pylon), y = 1,
2, 3, 6, 7, or 8) for each launched missile in successive launch advisory locations from left to right on
the bottom of the MFD. The SMO determines if the
missile was successfully launched, aborted, or is
hung and will display either AWAY, ABORT, or
HUNG in normal video in the location immediately
following the launch advisory location for that missile.
• If the missile has become hung, HUNG will be
displayed in reverse video in window 9 of the
FRMT-7 display. xy:HUNG will be displayed as a
master fault. An unsuccessful launch sequence will
be indicated by the text xy:ABORT displayed as a
master fault.
• Power application to the missile will be inhibited.
7-45
T.O. 1B-52H-34-2-8
JASSM Launch Sequence Timeline (Typical)
Figure 7-17
AUTOMATIC LAUNCH DETERMINATION
The SMO will initiate automatic launch of a missile
when all the following conditions are true for that
missile:
• Automatic launch mode has been selected by the
operator.
Do not switch from automatic to manual
launch mode while the missile is in launch
countdown. This will abort the missile with
a permanent fatal fault.
NOTE
Selection of Automatic Launch mode is limited to missions where the preplanned JASSM
Launch Point (JASSM LP) is located at a distance of at least three seconds of flight inside
the planned In-Zone area. The reason for this
limitation is that, for auto launches, the SMO
calculates the start of the launch countdown
(LCD) to occur three seconds before the aircraft achieves the closest point of approach to
the preplanned JASSM LP. This allows release of the missile precisely at the JASSM
LP, or at the aircraft’s closest point of approach to the JASSM LP if the aircraft is deviating from the preplanned route. If at the
start of LCD the aircraft is not within the InZone area, the SMO displays an LCD ENTRY
7-46
Change 2
([AMI] JASSM LCD ENTRY) advisory and
waits until the aircraft is within the In-Zone
area to begin LCD. If the first In-Zone indication received from the missile occurs after the
aircraft has passed the closest point of approach to the JASSM LP, the SMO will inhibit
automatic launch and indicate manual
launch is required in addition to the LCD
ENTRY ([AMI] JASSM LCD ENTRY) advisory.
• The missile has power applied and is in an All
Up Round (AUR) Ready state:
• Weapon is Safe to Launch:
• There is no critical weapon hardware failure.
• Weapon has received minimum TXA data.
• Weapon has minimum targeting data.
• Timeline aborted has not been issued.
• Weapon is not in IBIT.
• TXA is good.
• Last BIT passed.
• Warm-up is complete.
• The pilot’s munitions consent switch and the navigator’s unlock consent switch are in the unlock
position.
• No missile jettison request is present and no jettison is in progress for any missile.
• No WIU faults are detected which would prevent
the launch of the missile.
• LAR conditions have been met for the missile.
The missile status must indicate In-Zone. The
JASSM will launch at the point of closest approach
to the JASSM launch point.
T.O. 1B-52H-34-2-8
MANUAL LAUNCH DETERMINATION
Manual launch mode is selected at the time the
SMO is loaded. The selection of manual launch
mode, either by the operator or default, will be indicated on the WCP launch select switch and on the
CF-E display. The following conditions must be true
in order for the operator to manually launch a missile:
• Manual launch mode is the current mode of op-
eration.
• The missile has had power applied.
• The pilot’s munitions consent switch and the navigator’s unlock consent switch are in the unlock
position.
• No missile jettison request is present and no jettison is in progress for any missile.
• No WIU faults are detected which would prevent
the launch of the missile.
• LAR conditions have been met for the missile.
Missile status indicates In-Range.
• Missile status indicates Safe to Launch:
• There is no critical weapon hardware failure.
• Weapon has received minimum TXA data.
• Weapon has minimum targeting data.
• Timeline aborted has not been issued.
• Weapon is not in IBIT.
Manual launch is required for the following:
• The missile is targeted to a direct target.
• The missile has a fault requiring manual launch.
• The point of closest approach is outside of the
zone.
• The seeker is required, but not functional.
• Invalid zone data.
• Target data set contains no valid waypoints.
Use care not to deselect (press again) the
manual launch switch while the weapon is
in launch countdown. This will abort the
weapon with a permanent fatal fault.
MISSILE LAUNCH TERMINATION
The missile launch process will be terminated before the selected missile has been launched if any of
the following conditions occur:
• Any WIU or missile fault occurs which requires
that power be removed from the WIU or missile.
• The WIU or missile has power removed.
• The missile is no longer targeted to the current
ranging event.
• An ACU reconfiguration occurs.
• A jettison is in progress for any missile on the
same pylon as the launch missile.
• Operator deselects the manual launch command.
• Operator switches from automatic to manual
launch mode.
• If either unlock consent is removed.
• CLR-D or PRGM-Dn is entered during a direct
launch.
NOTE
Prior to CTS, the SMO will declare a nonfatal LCD Abort fault. If the abort condition
occurs, past CTS and the carrier mission is
not captive carry, the SMO will issue a message to abort the missile and declare a permanent fatal LCD Abort fault.
7-47
T.O. 1B-52H-34-2-8
PREFERRED LAUNCH/JETTISON SEQUENCE
The JASSM preferred launch/jettison sequence is
shown in the figure 7-18 and the following table.
If there is a retained/HUNG center station
store, launching/jettisoning an adjacent
shoulder station may result in a Store-toStore contact. When a center station store
is retained/HUNG, operators will retain the
adjacent shoulder station stores.
LAUNCH
SEQUENCE
PYLON
POSITION
1
LP - 2
LP Forward Center
2
RP - 2
RP Forward Center
3
LP - 7
LP Aft Center
4
RP - 7
RP Aft Center
5
LP - 1
LP Forward Outboard
6
RP - 3
RP Forward Outboard
7
LP - 3
LP Forward Inboard
8
RP - 1
RP Forward Inboard
9
LP - 6
LP Aft Outboard
10
RP - 8
RP Aft Outboard
11
LP - 8
LP Aft Inboard
12
RP - 6
RP Aft Inboard
7-48
POSITION
MISSILE LAUNCH RESTRICTIONS
Currently there are no SMO launch inhibits to missile launch due to aircraft flight conditions. Safe release advisories and the corrective action are contained in figure 7-22.
Safe release advisories do not inhibit
launch. Possible collision between weapons
and between weapon and aircraft can occur
if weapon is launched with a release advisory displayed.
JASSM FREE FLIGHT SEQUENCE
Following separation from the aircraft, the JASSM:
• Detects separation.
• Deploys its wings to 75 degrees to aid pitch stability and separation from the aircraft.
• Deploys its tail to add yaw control and the lugs
retract.
• Deploys its wings to 45 degrees, when initial
pitch stability is achieved.
• Releases elevon brakes to make pitch and control
active.
• Activates fuel control and engine squib (3.0 sec
after separation), if in engine start envelope.
• Releases wedges on underside of stakes to insure
clean separation from the aircraft.
• Switches to alternator power, FUZE ARM (RPM
satisfied), FUZE safe separation timer – On.
• Engine achieves max thrust when at proper altitude.
• FUZE firing mode/delay time is set by mission
processor.
• GPS satellite acquisition occurs 90 seconds after
separation from the aircraft.
T.O. 1B-52H-34-2-8
JASSM Preferred Launch/Jettison Sequence
If there is a retained/HUNG center station store, launching/jettisoning an adjacent shoulder station may result in a Store-to-Store Contact. When a center
station store is retained/HUNG, operators will retain the adjacent shoulder
station stores.
Figure 7-18
7-49
T.O. 1B-52H-34-2-8
MISSILE JETTISON
The operator can command the SMO to jettison
missiles using either the WPN JETTISON switch
on the WCP or the pilots’ Bomb Bay & Missile jettison switch. The OAS must be operational with the
JASSM SMO loaded ([AMI] as primary SMO) and
WIU power must be on for jettison of JASSMs using the WCP or the Pilots’ switch. With OAS or
WIU off, or a SMO other than the JASSM SMO
loaded, jettison of JASSMs can only be accomplished using the Alternate Jettison Control Panel
(AJCP). All methods require unlock consent. The
Pilot Bomb Bay and Missile jettison switch has the
same effect as if all locations and all stations were
selected on the WCP and then the WPN JETTISON
switch was selected.
NOTE
The radar navigator’s jettison switch was
excluded from operation with the JASSM
SMO, however, a malfunction in the jettison
system (failed blocking diode) could enable
the switch, making it function in the same
manner as the pilots’ Jettison Control Bomb
Bay & Missile switch.
If the WCP JETTISON switch or Pilot Jettison ALL
switch is used, the jettison is controlled by the SMO
and the process is as follows:
• Operator selects Location and Station of missile(s) to be jettisoned on the WCP.
• Operator moves JETT switch to the JETT position.
1. Classified data erase will be commanded if missile power is on, but will not be statused for completion.
2. Missile power will be removed if missile power
is on.
3. The SMO commands ejector squib fire to the
ejector of the missile in the most preferred release
sequence order.
4. The SMO performs a scoring recording on the
flight DTUC/DTC for jettisoned missile.
5. The missile launch advisory is requested on all
MFDs. The missile launch advisory will remain displayed for 5 seconds. The advisory area of each
MFD where the missile launch advisory is displayed will be blanked. The SMO displays appropriate xy (x = L (left pylon) or R (right pylon); y = 1, 2,
3, 6, 7, or 8) for each jettisoned missile in successive
7-50
Change 2
launch advisory locations from left to right on the
bottom of the MFD.
6. The SMO determines if the missile has been
successfully jettisoned, is hung, or jettison is
aborted and displays either JETT, HUNG or
ABORT for the jettisoned missile in normal video in
the location immediately following the launch advisory location for that missile.
7. If the missile has become hung, HUNG will be
displayed in reverse video in window 9 of the
FRMT-7 display. The text xy:HUNG will be displayed as a master fault when the missile is hung.
8. If the jettison has been aborted, ABORT will be
displayed in reverse video in window 9 of the
FRMT-7 display. The text xy:ABORT will be displayed as a non-fatal master fault.
9. The SMO requests a video recording of the
launch advisory.
10. The SMO then inhibits power reapplication to
the selected station. (Power application is allowed if
jettison of missiles was aborted.)
11. The SMO repeats all steps 1 through 10 above
until all the desired missiles have been jettisoned.
When missiles are jettisoned using the Alternate Jettison Control Panel (AJCP) hard-wired switches,
EED power is applied independent of the WIU. However, if the WIU has power applied, the WIU will continue to monitor the state of the EED power.
NOTE
If missiles are jettisoned using the AJCP
hard-wired switches while the SMO is loaded
and the WIU is powered on, there is the probability that the WIU status retrieved by the
SMO will show that the EED power is on
when it has not been commanded on by the
SMO. If this occurs, WIU master fault will be
declared, x:EED PWR (x = L or R to indicate
left or right WIU) will be displayed, and the
WIU will be powered off by the SMO.
Also, a missile Present Discrepancy master fault
will be declared for each missile jettisoned via the
AJCP. This results in the display of xy:WPN
PRSNT for each missile. The text WPN PRSNT will
also be displayed in window 9 of the FRMT-7 display for each missile jettisoned via the AJCP.
If jettison is commanded while either unlock consent
switch is in the lock position, the advisory message
NO CONSENT will be displayed on each MFD.
T.O. 1B-52H-34-2-8
SIMULATION CAPABILITIES
SIMULATED TARGETING OPERATIONS
Less [AMI] This paragraph describes any differences in the SMO capabilities while in SIM mode.
SIM mode is commanded by entering CF-52. The
operator can verify the currently active SMO mode,
whether STRIKE or SIM, by observing window 1 on
either the CF- menu, the CF-5 menu or the CF-57
menu.
Manual Targeting can be commanded while a SIM
mode is active by operator entry of CF-586. Manual
Targeting while a SIM mode is active will operate
as described in Section I.
[AMI] This section describes any differences in the
SMO capabilities while in the FULL or PART SIM
mode. PART SIM mode is commanded by entering
CF-51. FULL SIM mode is commanded by entering
CF-52. The operator can verify the currently active
SMO mode, whether STRIKE, FULL SIM or PART
SIM, by observing either the CF- menu, the CF-5
menu or the CF-57 menu.
NOTE
[AMI] For JASSM there is no difference between the FULL and PART SIM modes.
SIMULATED MISSILE LOADOUT
Each time a SIM mode is commanded, only the missiles shown as present in the stores table will be
shown present. Subsequent to releases (launches or
jettisons) in a SIM mode, commanding STRIKE and
reentering SIM will reset only the missiles identified in the stores table as present.
On SIM mode entry, the assignments set while in
STRIKE mode are maintained. However, the missiles are marked as untargeted. FRMT-7 will display the target assignments in normal video. Less
[AMI] To prevent assignment carry over from
strike mode reload mission.
Less [AMI] On SIM mode exit, all missiles are
marked as unassigned and untargeted. FRMT-7
will display blanks (i.e. no targets assigned) for the
targeting status. The operator must either reload
the B-52 mission, accomplish a retarget all operation (CF-589), or accomplish a manual targeting operation (CF-586).
[AMI] On SIM mode exit, all missile assignments
that were set in STRIKE mode will be retained.
FRMT-7 will display target assignments as they
were before entry into a SIM mode.
Direct Targeting can be commanded while a SIM
mode is active by operator entry of CF-588,n. Direct
Targeting while a SIM mode is active will operate
as described in Section I.
SIMULATED WCE RESPONSES
While in a SIM mode, WCE and missile I/O is not
transmitted and actual WCE and missile status
and responses to commands are not available.
Therefore, while in a SIM mode, the following concepts are implemented by the SMO:
• No faults are declared for any WCE or missiles.
• WCE and missile responses are simulated
using the response times are shown below.
SIM Mode Response Times
DESIRED WCE/MISSILE
STATUS
WIU initialization
Missile IBIT completion
Missile battery activation
RESPONSE TIME
(SECONDS)
15.625
180.0
1.27
Power is not applied to the pilot’s munitions consent
switch when the SMO is operating in SIM mode and,
therefore, the switch position is not known to the
SMO. The pilot’s munitions consent switch input is
simulated as being the same as the navigator’s unlock
consent switch. Therefore, providing ejector unlock
consent from the navigator’s unlock consent switch is
the only ejector unlock consent that is necessary to allow the simulated release of missiles.
NOTE
After a SIM mode is exited by commanding
STRIKE mode, the B-52 mission data and
the SMO must be reloaded to guarantee
proper operation of the system.
SIMULATED RANGING
While in SIM mode, ranging is accomplished in the
same manner as in STRIKE. The SMO performs
ranging by using the TDS data from the missile mission data DTUC ([AMI] selected weapon group) for
each missile. The data along with the aircraft position and headings is used to estimate the parameters in the missile LAR message.
Change 2
7-51
T.O. 1B-52H-34-2-8
SMO TERMINATION
SMO RESTART
SMO execution can be terminated in two ways:
• Less [AMI] Another SMO can be loaded into
the ACUs, using a SMO load and initialization process similar to that used for initial SMO loading.
This process terminates execution of and overwrites
the SMO which is already loaded. With this
method, FMS will continue to be executed. The
SMO will delay compliance with the command to
terminate execution until the SMO has removed
power from the WIUs and until all outstanding
SMO faults have been recorded (if a Flight Data
Record tape is installed).
• Less [AMI] Also, CF-67 can be entered by the
operator. This command halts execution of all software loaded into the ACUs (FMS and any loaded
SMO). The SMO will delay compliance with the
shutdown request until all outstanding SMO faults
have been recorded and for as long as it takes the
SMO to remove power from all WCE and missiles
that have powered applied.
• [AMI] Loading another SMO or entering zero
at the location the JASSM SMO is loaded, terminates execution and unloads the SMO. With this
method, the FMS and CSP will continue to operate.
• [AMI] Alternatively, the operator can enter
CF-67 which halts execution of all software loaded
into the ACUs (FMS, CSP, and any loaded SMO).
The method of restarting the SMO is dependent
upon the method which terminated SMO execution.
The two methods are described below.
• Less [AMI] If SMO execution was terminated
by loading another SMO into the ACUs, or ACU
memory has been erased, the SMO must be reloaded into the ACUs.
• Less [AMI] If SMO execution was terminated
by entering CF-67, and ACU memory has not been
erased, FMS and the SMO can be restarted by depressing the PROC SYNC button on the computer
control panel.
• [AMI] If the SMO execution was terminated
by loading another SMO into the ACU, the SMO
must be reloaded into the ACUs.
• [AMI] If the SMO execution is terminated by
a CF-67 command, the FMS and the SMO can be
restarted by pressing the PROC SYNC button on
the computer control panel and logging on to the
OAS using the CF-61 command, then the SMO
must be reloaded.
7-52
Change 2
T.O. 1B-52H-34-2-8
MESSAGES
This paragraph defines all SMO messages, their indications and lists any corrective action which can be
taken by the operator to resolve the anomaly when
applicable.
MASTER FAULTS
The JASSM Master Faults are identified in figure
7-19. Master faults are an indication of WCE or
missile failures, or conditions which will preclude
the launch of missiles. Master faults are displayed
in reverse video at the bottom left hand end of the
MFD. When the faulted device is a WIU or a missile, the text that is displayed will be preceded by a
location or location and station identifier. The text
for WIU faults that are not associated with a specific station will be preceded by L or R. L will be
displayed to identify the faulted device location as
the left pylon and R will be displayed to identify the
faulted device location as the right pylon. Missile
faults and WIU faults that are associated with a
specific location will be preceded by a location and
station identifier of the form xy, where x will be L
or R to identify the left or right pylon, respectively,
and y will be the station number, 1, 2, 3, 6, 7 or 8.
Faults which are not applicable to this SMO are
identified with the text N/A in the corresponding
fault text and fault type columns of figure 7-19.
No corrective action can be taken by the operator for
WIU or missile faults, although power re-application
can be commanded by the operator when power is
removed from a faulted device. If the SMO has determined that power should not be re-applied because of
the failure, the SMO will not respond to the command
to apply power. The operator can override an ECU
NO-GO fault and an ECU AC POWER fault with a
CF-68 command to allow WIU power application.
Permanent fatal faults will initiate a CDE, leaving
the weapon assigned, but untargeted.
With an ECU fault present, damage to equipment may occur if WIU power remains on as
a result of selecting ECU power override.
The SMO expects the ejectors to be pinned in the
unlock position. If they are not pinned in the unlock
position at one or more stations, an uncommanded
ejector locked non-fatal master fault xy:UNCMD
LK will be generated for each of those stations.
navigator’s unlock consent switch are in the unlock
position. Even if the ejectors are pinned in the unlock
position, this fault will still prevent a normal release
sequence because this power is also used to fire the
squibs which eject the missile.
The types of master faults identified in figure 7-19,
the associated abbreviations and the actions taken
by the SMO as a result of the fault are as follows.
Safety Critical (SC)
Safety critical faults present a safety threat to personnel or to the aircraft. The SMO will remove
power from the faulted device and inhibit re-application of power by the operator. Power will be
removed from the affected missile when a missile or
station safety critical fault is detected. There are no
identified safety critical faults for the JASSM SMO.
Permanent Fatal (PF)
The SMO will perform a normal shutdown of the
faulted device and inhibit re-application of power by
the operator. Any weapon or station permanent fatal
fault that occurs after CTS has been commanded to
that weapon will be treated as a safety critical fault.
Transient Fatal (TF)
The SMO will perform a normal shutdown of the
faulted device. Re-application of power by the operator is allowed. Any missile or station transient
fatal fault which occurs after CTS has been commanded to that missile will be treated as a permanent fatal fault.
Non Fatal (NF)
The SMO will not remove power from the faulted
device.
ADVISORIES AND STATUS MESSAGES
The SMO Advisories are identified in figure 7-20. The
SMO Status Messages are identified in figure 7-21.
Advisories and Status Messages are displayed in
reverse video at the bottom right hand end of the
MFD.
SAFE RELEASE AND WEAPON LAUNCH ADVISORIES
The safe release advisories are identified in figure
7-22. The weapon launch advisories are identified
in figure 7-23. Safe release and launch advisories
are displayed, approximately, in the center of
PRGM display. See figures 7-22 and 7-23.
FRMT-7 WEAPON FAULTS
When both ejector unlock enable monitors for a WIU
indicate that ejector unlock enable is not present, the
text x:NO UE is displayed as a master fault for that
WIU. Unlock enable power is provided to each WIU
when the pilot’s munitions consent switch and the
The weapon faults displayed as part of the missile
status block on FRMT-7 and FRMT-7xy, and also at
the bottom of the FRMT-7xy display, are listed in
figure 7-24.
Change 2
7-52A/(7-52B blank)
BLA
T.O. 1B-52H-34-2-8
JASSM Master Faults
Fault Indication Coding:
• NF = NON-FATAL Fault
• PF = PERMANENT FATAL Fault
• SC = SAFETY CRITICAL Fault
• TF = TRANSIENT FATAL Fault
• x = L - LEFT PYLON OR R - RIGHT PYLON LOCATION
• y = 1, 2, 3, 6, 7, OR 8 STATION NUMBER
FAULT
INDICATION
FAULT
TYPE
POSSIBLE CAUSE
SYSTEM RESPONSE
OPERATOR ACTION
ARMAMENT INTERFACE UNIT MASTER FAULTS
AIU COMM
Less [AMI]
or
AIU [AMI]
NF
1. Armament Interface Unit
(AIU) communications failure.
2. AIU terminal failure.
3. Interruptible Direct Current
(IDC) power enable discrepancy (uncommanded power on or
off).
NOTE
Fault displayed and recorded every 30 minutes,
as long as the fault is
present.
This master fault may result in
any or all of the following:
1. Loss of Environmental Control Unit (ECU) power control.
2. Loss of WIU power control.
3. Weapons cannot be powered or launched.
4. Less [AMI] SMO controlled
jettison is not available.
5. RBS tone cutoff will not occur.
6. [AMI] Loss of Pylon jettison
capability.
7. [AMI] Loss of OAS control of
bay door operation.
1. Acknowledge message
2. Check Circuit Breakers
on the AUX BNS S/V FILTER BOX Circuit Breaker
Panel. Pull and reset, if required.
3. Verify status of weapon
and WIU power.
AIU 28 VDC
NF
STORE 28 VDC T/R
power discrepancy.
NOTE
Fault displayed and recorded every 30 minutes,
as long as the fault is
present.
This master fault may result in
any or all of the following:
1. May not be able to apply
WIU essential (ESS) power.
2. May not be able to apply
store 28 VDC #1 power.
1. Acknowledge message.
2. Check Circuit Breakers
on the AUX BNS S/V FILTER BOX Circuit Breaker
Panel. Pull and reset, if required.
3. [AMI] Check AIU circuit
breaker on the RIGHT S/V
FILTER BOX CIRCUIT
BREAKER PANEL. Pull
and reset, if required.
4. Verify status of weapon
and WIU power.
Figure 7-19 (Sheet 1 of 17)
Change 2
7-53
T.O. 1B-52H-34-2-8
JASSM Master Faults (Cont)
FAULT
INDICATION
FAULT
TYPE
POSSIBLE CAUSE
SYSTEM RESPONSE
OPERATOR ACTION
ENVIRONMENTAL CONTROL UNIT MASTER FAULTS
ECU
TF
ECU NO-GO and ECU orride
is off.
1. Environmental conditions
are out of limits.
2. Insufficient Airflow.
3. Low engine power settings.
4. Transient failure during
climb or descent.
5. ECU failure.
NOTE
• If an environment No-Go
fault is detected from the
ECU after power has been
applied for at least two
minutes, power will be removed from all weapons
and both WIUs one minute
from the time that the fault
is displayed.
• Fault displayed and re-
corded every 30 minutes,
as long as the fault is present.
This master fault may result in
any or all of the following:
1. Cooling air to the WIU is unavailable or inadequate.
2. Weapon temperature or airflow out of limits could cause
degraded weapon performance and weapon malfunctions.
3. If the fault remains for more
than 1 minute, weapon power
and WIU power are removed.
With an ECU fault present, damage to equipment may occur if WIU
power remains on continuously as a result of
selecting ECU power
override. While in ECU
power override, the WIU
may be operated using a
30 minute on, 15 minute
off, 30 minute on cycle.
1. Acknowledge message.
2. If the cause is low airflow, increase power on engines 3 and 4.
3. Close air outlet knobs
and decrease cabin temperature.
4. Verify pilot’s cabin master pressure switch is in
ECS.
5. In potential icing conditions check pilot’s anti-icing
is on.
6. Remove weapon power
and recycle WIU power.
7. If override is warranted,
operator entry of CF-68
commands the SMO to activate ECU power override.
NOTE
• If the CF-68 command
is entered within 1 minute of the fault indication, weapon and WIU
power will remain on,
otherwise, weapon and
WIU power are automatically removed.
• If WIU and/or weapon
power is removed because of a fault, the
CF-68 command must
be entered prior to reapplying WIU power.
Figure 7-19 (Sheet 2 of 17)
7-54
Change 3
T.O. 1B-52H-34-2-8
JASSM Master Faults (Cont)
FAULT
INDICATION
FAULT
TYPE
POSSIBLE CAUSE
SYSTEM RESPONSE
OPERATOR ACTION
ENVIRONMENTAL CONTROL UNIT MASTER FAULTS (Cont)
ECU PWR
TF
ECU AC power discrepancy
(uncommanded on or off) and
ECU orride is off.
NOTE
Loss of conditioned air to the
WIU.
• If an environment No-Go
fault is detected from the
ECU after power has been
applied for at least two
minutes, power will be removed from all weapons
and both WIUs one minute
from the time that the fault
is displayed.
• Displayed and recorded
every 30 minutes, as long
as the fault is present.
1. Before WIU power on – unable to power up WIU or weapons.
2. After WIU power on – WIU
and weapon power is removed.
With an ECU fault present, damage to equipment may occur if WIU
power remains on continuously as a result of
selecting ECU power
override. While in ECU
power override, the
WIU may be operated
using a 30 minute on, 15
minute off, 30 minute on
cycle.
1. Acknowledge message.
2. Remove weapon power
and recycle WIU power.
3. If override is warranted,
operator entry of CF-68
commands the SMO to activate ECU power override.
NOTE
• If the CF-68 command
is entered within 1 minute of the fault indication, weapon and WIU
power will remain on,
otherwise, weapon and
WIU power are automatically removed.
• If WIU and/or weapon
power is removed because of a fault, the
CF-68 command must
be entered prior to reapplying WIU power.
Figure 7-19 (Sheet 3 of 17)
Change 3
7-55
T.O. 1B-52H-34-2-8
JASSM Master Faults (Cont)
FAULT
INDICATION
FAULT
TYPE
POSSIBLE CAUSE
SYSTEM RESPONSE
OPERATOR ACTION
WEAPON INTERFACE UNIT MASTER FAULTS
x:CRIT VRFY
TF
Double critical verify Fault.
1. [AMI] Preset commanded
but response not verified.
2. [AMI] WIU CRITICAL COMMAND status not valid.
3 [AMI] Weapon address selected with no critical function
active.
1. WIU and weapon power are
removed.
2. JASSM heater power not
available.
3. Jettison or launch sequence
may be aborted.
1. Acknowledge message.
2. Re-apply WIU power.
3. If Fault persists, verify
WIU power is removed.
4. If Fault occurred post
CTS, accomplish POST
STRIKE/ABORT checklist.
x:EED PWR
TF
1. 38 VDC Electro-explosive
Devise (EED) power on when
not commanded on.
1. Weapon power and WIU
power will be removed.
2. Weapon heater power not
available.
1. Acknowledge message.
2. Re-apply WIU power.
3. If Fault occurred post
CTS, accomplish POST
STRIKE/ABORT checklist.
4. [AMI] If fault resulted
from AJCP jettison, continue.
NF
2. 38 VDC Electro-explosive
Devise (EED) off when not
commanded off.
1. If EED power is not present
when requested (i.e. during a
launch or jettison), a non-fatal
master fault will occur and the
WIU will remain on.
2. Jettison or launch sequence
may be aborted.
3. Weapon heater power not
available, if WIU powered off.
1. Acknowledge message.
2. Less [AMI] Remove
weapon and WIU power.
3. Less [AMI] Accomplish POST STRIKE/
ABORT checklist.
4. [AMI] If Fault occurred
post CTS, accomplish
POST
STRIKE/ABORT
checklist.
5. [AMI] If fault resulted
from AJCP jettison, continue.
Figure 7-19 (Sheet 4 of 17)
7-56
Change 2
T.O. 1B-52H-34-2-8
JASSM Master Faults (Cont)
FAULT
INDICATION
FAULT
TYPE
POSSIBLE CAUSE
SYSTEM RESPONSE
OPERATOR ACTION
WEAPON INTERFACE UNIT MASTER FAULTS
x:ESS PWR
x:NO UE
TF
1. 28 VDC Essential (ESS)
power off when not commanded off.
1. Essential power is not present when desired.
2. Weapon and WIU power will
be removed
3. JASSM heater power not
available.
1. Acknowledge message.
2. Check AIU circuit breaker on S/V FILTER BOX Circuit Breaker panels.
3. If WIU and weapon power are removed, re-apply
WIU power.
4. If fault persists, verify
WIU power is removed.
5. If Fault occurred post
CTS, accomplish POST
STRIKE/ABORT checklist.
NF
2. 28 VDC ESS power on
when not commanded on.
1. Less [AMI] Essential power
is present when not desired.
2. [AMI] If power is on when
commanded off, a non-fatal
master fault will occur and WIU
power will remain on.
3. JASSM heater power not
available, if WIU powered off.
1. Acknowledge message.
2. Check S/V FILTER BOX
Circuit Breaker panels.
3. If WIU and weapon power are removed, re-apply
WIU power.
4. If fault persists, verify
WIU power is removed.
5. If Fault occurred post
CTS, accomplish POST
STRIKE/ABORT checklist.
NF
Unlock enable not present
when commanded.
NOTE
Fault displayed and recorded every 30 minutes,
as long as the fault is
present.
1. Acknowledge message.
2. Set Pilot’s and WCP
consent switches to the
LOCK position.
3. Set Pilot’s and WCP
consent switches to the
UNLOCK position.
4. If Fault remains:
A. Set Pilot’s and WCP
consent switches to the
LOCK position.
B. Remove weapon
power and cycle WIU power.
C. Set Pilot’s and WCP
consent switches to the UNLOCK position.
5. If fault persists, accomplish POST STRIKE/
ABORT checklist, if applicable.
Launch or SMO controlled jettison unavailable.
Figure 7-19 (Sheet 5 of 17)
Change 2
7-57
T.O. 1B-52H-34-2-8
JASSM Master Faults (Cont)
FAULT
INDICATION
FAULT
TYPE
POSSIBLE CAUSE
SYSTEM RESPONSE
OPERATOR ACTION
WEAPON INTERFACE UNIT MASTER FAULTS (Cont)
x:RC DRVR
Less [AMI]
NF
Release
consent
uncommanded off.
driver
NOTE
A CTSS PF Fault will follow and the SMO will shut
down weapon power.
1. Acknowledge message.
2. Accomplish POST
STRIKE/ ABORT checklist,
if applicable.
May result in an aborted launch
or jettison sequence.
x:RC DRVR [AMI]
NF
Release
consent
uncommanded off.
driver
1. A pre-CTSS LCD abort and
release consent Fault will occur if the weapon is unable to
verify receipt of Release Consent. In this case, the SMO will
not remove weapon power.
2. May result in an aborted
launch or jettison sequence.
1. Acknowledge message.
2. Re-apply WIU power.
3. If fault persists, verify
WIU power is removed.
4. If fault occurred post
CTS, accomplish POST
STRIKE/ ABORT checklist.
x:UNCMD DRVR
TF
1. Double release consent
driver uncommanded on fault.
2. Less [AMI] Double ejector
squib fire driver status of true
when not commanded.
1. Weapon and WIU power will
be removed.
2. Jettison or launch sequence
may be aborted.
3. JASSM heater power not
available.
1. Acknowledge message.
2. Attempt re-applying
WIU and weapon power.
3. If fault persists, verify
WIU power is removed and
accomplish POST
STRIKE/ABORT checklist,
if applicable.
x:UNCMD PVE
TF
1. Double critical command
register status fault.
2. Double critical function ejector selection station fault.
1. WIU and weapon power are
removed.
2. JASSM heater power not
available.
1. Acknowledge message.
2. Attempt re-applying
WIU and weapon power.
3. If fault persists, verify
WIU, and weapon, power is
removed and accomplish POST STRIKE/
ABORT checklist, if applicable.
x:UNCMD UE
NF
Unlock enable (UE) power Hardware safeguard provided
available without Pilot’s and by Pilot’s and WCP unlock conWCP UNLOCK switches in the sent circuit is negated.
UNLOCK position (i.e., system
has consent without switches
set for consent).
1. Acknowledge message.
2. Cycle the Pilot’s and
WCP UNLOCK switches to
LOCK.
3. If fault remains, power
off weapons and cycle WIU
power.
2. Cycle the Pilot’s and
WCP UNLOCK switches to
LOCK.
4. Continue normal procedures, however, ejector
rack unlock enable is present. For non-combat missions leave WIU power off.
For combat missions do not
power WIUs over friendly
territory.
Figure 7-19 (Sheet 6 of 17)
7-58
Change 2
T.O. 1B-52H-34-2-8
JASSM Master Faults (Cont)
FAULT
INDICATION
FAULT
TYPE
POSSIBLE CAUSE
SYSTEM RESPONSE
OPERATOR ACTION
WEAPON INTERFACE UNIT MASTER FAULTS (Cont)
x:WIU
TF
WIU end around communica- 1. WIU power is removed.
tion test fault – data transmitted 2. JASSM heater power not
to the WIU does not match data available.
received from the WIU during
power on sequence.
1. Acknowledge message.
2. Cycle WIU power.
3. If fault persists, verify
WIU power is removed.
x:WIU COMM
TF
Double WIU communication
failure.
1. WIU and weapon power are
removed.
2. JASSM heater power not
available.
1. Acknowledge message.
2. Cycle WIU power.
3. If fault persists, verify
WIU power is removed.
x:WIU RESET
TF
1 WIU not reset.
2. WIU reset monitor active
fault.
1. WIU power is removed.
2. JASSM heater power not
available.
1. Acknowledge message.
2. Cycle WIU power.
3. If fault persists, verify
WIU power is removed.
Figure 7-19 (Sheet 7 of 17)
Change 2
7-59
T.O. 1B-52H-34-2-8
JASSM Master Faults (Cont)
FAULT
INDICATION
FAULT
TYPE
POSSIBLE CAUSE
SYSTEM RESPONSE
OPERATOR ACTION
STATION MASTER FAULTS
xy:28VDC2
TF
WIU status indicates 28 VDC
#2 uncommanded on.
1. Weapon batteries may be
squibbed inadvertently.
2. Weapon may be launched
or jettisoned with power still at
the umbilical.
3. [AMI] Weapon COMM NOGO and weapon power removal may follow failure.
1. Acknowledge message.
2. If weapon power is not
removed:
A. Remove weapon
power.
B. Cycle WIU power.
C. Re-apply weapon
power.
D. If fault persists, shut
down weapons and WIU,
and accomplish POST
STRIKE/ABORT checklist.
3. If weapon power was removed, shut down WIU and
accomplish POST
STRIKE/ABORT checklist.
xy:ABORT
PF
1. Launch countdown abort
fault after CTS.
2. CTSS Battery Failure.
(Non-Captive Carry missions).
1. Weapon power is removed.
2. SMO inhibits weapon power
re-application.
3. Weapon batteries may have
been squibbed.
1. Acknowledge message.
2. Verify weapon power removed.
3. Accomplish POST
STRIKE/ABORT checklist.
4. If fault occurred during
Captive Carry launch, remove weapon power and
do not attempt further
launches at that station.
xy:ACFT PWR
NF
1. 28 VDC #1 Power Fault
(Uncommanded on or off).
2. 28 VDC #2 Power Fault
(Uncommanded off). May occur due to the loss of AIU 28
VDC T/R power or WIU 28
VDC ESS power.
3. 3-Phase 115V AC Power
Fault (Uncommanded on).
1. Manual launch required.
2. Weapon may be jettisoned/
released, with power still applied at the umbilical.
1. Acknowledge message.
2. Remove weapon power.
3. Cycle WIU power.
4. Re-apply weapon power.
5. If the fault persists, remove weapon power.
xy:BIA Fail
NF
Bomb Impact Assessment
(BIA) Fault.
1.Manual launch required.
2. Weapon power not removed.
3. [AMI] Weapon will not transmit terminal targeting data.
4. [AMI] MDT may be corrupted.
1. Acknowledge message.
2. Cycle weapon power.
3. If BIA is required and
the fault persists, remove weapon power.
xy:BUS TEST
NF
MIL-STD-1553B Weapon Bus
Test Fault.
Loss of dual redundant 1553
weapon bus. Communication
retry will occur on second bus.
1. Acknowledge message.
2. Monitor for additional
bus faults.
Figure 7-19 (Sheet 8 of 17)
7-60
Change 2
T.O. 1B-52H-34-2-8
JASSM Master Faults (Cont)
FAULT
INDICATION
FAULT
TYPE
POSSIBLE CAUSE
SYSTEM RESPONSE
OPERATOR ACTION
STATION MASTER FAULTS (Cont)
xy:COMM NOGO
TF
1. Aircraft ID fault.
Weapon power is removed.
2. Weapon comm fault.
3. Almanac received fault.
4. GPS keys transfer fault.
5.Timeline abort fault.
6. Surface/Fin delay fault. Fin
deployment delay is less than
commanded.
7 Timeline integration fault.
8. Mass data transfer fault.
Weapon functions dependant
on data transferred by the SMO
may not have received the correct data.
9. Uncommanded timeline
abort fault.
10.Simulated launch countdown fault. (Captive Carry only)
11. Minimum TXA fault.
12. INS/INU no longer designated as prime OAS navigation
source with JASSMs powered.
13. [AMI] Possible hardware
problem located at the aircraft
station interface.
1. Acknowledge message.
2. If the fault occurred before CTS:
A. Ensure an INS/INU is
designated as the prime
navigation model.
B. Re-apply weapon
power.
C. If the fault persists,
verify weapon power is removed.
3. If the fault occurred after
CTS, accomplish POST
STRIKE/ABORT checklist.
xy:CTSS
PF
1. Uncommanded Commit to
Separate (CTSS) fault.
2. Uncommanded CTS fault.
1. LCD is terminated.
2. Weapon power is removed.
3. CDE is commanded.
4. Weapon batteries may be
active.
5. SMO inhibits weapon power
reapplication.
1. Acknowledge message.
2. Accomplish POST
STRIKE/ABORT checklist.
3. Verify weapon power is
removed.
xy:EJECTOR
NF
1. Ejector status discrepancy
fault.
2. Uncommanded ejector lock
fault.
NOTE
1. Ejector status indicates:
A. Both locked and unlocked.
B. Neither locked nor unlocked.
C. Locked
2. This fault may occur if:
A. The ejectors are not
physically pinned in the unlocked position.
B. The ICSMS pylon assembly is not correctly figured.
3. [AMI] Manual launch required.
1. Remove weapon and
WIU power.
2. Ensure the ejector inflight safety lock is in the
unlock position and the
lockout bolt is installed.
3. Ensure pylon is properly
configured.
4. Re-apply WIU power.
5. If fault persists, do not
attempt launch or jettison at
this station.
If pylon is improperly configured, there should also be a
WPN PRSNT fault and all
weapons on that pylon
should show the same pylon
related faults.
Figure 7-19 (Sheet 9 of 17)
Change 2
7-61
T.O. 1B-52H-34-2-8
JASSM Master Faults (Cont)
FAULT
INDICATION
FAULT
TYPE
POSSIBLE CAUSE
SYSTEM RESPONSE
OPERATOR ACTION
STATION MASTER FAULTS (Cont)
xy:ERASE FAIL
NF
1. Data erase fault.
2. Less [AMI] CDE fault.
Mission classified data erase
was not successful per weapon CDE.
1. Acknowledge message.
2. Recommand weapon
CDE (CF-575).
3. If Fault persists:
A. Verify weapon power
is removed.
B. Weapon must be handled as if it contains classified data.
xy:FTS
(Flight Test Only)
NF
Flight Termination System
(FTS) is not active when commanded or is active when not
commanded.
1. FTS may not be available.
2. Manual launch is required.
Test launch may not be achievable.
3. FTS battery may be active
and battery life is limited to 15
minutes.
1. Acknowledge message.
2. [AMI] If mission is an
OTL,
perform
POST
STRIKE/ABORT checklist.
3. If mission is captive
carry, cycle weapon power.
4. If fault persists, accomplish POST STRIKE/
ABORT checklist.
xy:GPS DATA
NF
1. Ephemeris received fault.
2. Time received fault.
1. Loss of Ephemeris data.
2. Loss of ability to accurately
acquire GPS satellites for
weapons.
3. May cause weapon failure
to validate crypto keys.
4. Manual launch required.
1. Acknowledge message.
2. Verify the Interface Unit
(IU) and GPS receiver are
powered on.
3. Verify INU is powered
and navigating.
4. Check the GPS DATA
validity on the PKB.
5. Check GPS system fault
on FRMT-6.
6. Determine weapon GPS
initialization status.
7. Perform weapon CDE.
8. Recycle weapon power.
NOTE
Auto retargeting is required, if targeting is desired.
9. If the fault persists, verify
weapon power is removed.
Figure 7-19 (Sheet 10 of 17)
7-62
Change 2
T.O. 1B-52H-34-2-8
JASSM Master Faults (Cont)
FAULT
INDICATION
FAULT
TYPE
POSSIBLE CAUSE
SYSTEM RESPONSE
OPERATOR ACTION
STATION MASTER FAULTS (Cont)
xy:GPS INIT
NF
AS Status/SV Configuration
fault.
1. Weapon may not track GPS.
2. Manual launch required.
3. GPS accuracy may be impaired.
NOTE
The B-52 GPS 3A receiver requires approximately 15 minutes to decipher the new daily key
after a Zulu day rollover.
A NO KEYS may be displayed for weapons that
have power cycled during this period.
1. Acknowledge message.
2. Verify the IU and GPS
receiver are on and tracking satellites.
3. Verify current date on
CF-61.
4. Verify KEY PRESENT
is displayed on the IU
PKB.
5. Verify initialization data,
including date, is sent via
the PKB.
6. Verify FLY-TO has been
commanded and the B-52
is navigating.
7. Command a weapon
CDE.
8. Zeroize GPS receiver.
9. If keys are available on
the B-52 mission DTUC/
DTC:
A. Ensure B-52 mission DTUC/DTC is
installed.
B. Cycle IU power.
10. If keys are not available on the B-52 mission
DTUC/DTC, manually input GPS keys data via the
IU IKB.
11. Cycle weapon power.
12. If the fault persists,
verify weapon power is removed.
Figure 7-19 (Sheet 11 of 17)
Change 2
7-63
T.O. 1B-52H-34-2-8
JASSM Master Faults (Cont)
FAULT
INDICATION
FAULT
TYPE
POSSIBLE CAUSE
SYSTEM RESPONSE
OPERATOR ACTION
STATION MASTER FAULTS (Cont)
xy:HTR PWR
NF
3 Phase 115 VAC Power Fault
(Uncommanded off)
1. Weapon power is removed
or not applied.
2. Weapon communication
No-Go may follow failure.
3. JASSM heater power not
available at that station.
4. Manual launch required.
5. [AMI] Launch or jettison sequence may be aborted.
1. Acknowledge message.
2. Remove weapon power.
3. Cycle WIU power.
4. Re-apply weapon power.
5. If fault persists, remove
weapon power.
xy:HUNG
PF
Hung store following a launch
or jettison attempt.
1. Weapon is hung at ejector.
2. Weapon battery may be active.
3. Weapon present status indicates a weapon is present after
ejectors squib fire command
has been issued.
4. Weapon power is removed.
5. SMO inhibits re-application
of weapon power.
6. [AMI] SMO issues an abort
command to the weapon.
1. Acknowledge message.
2. Obtain visual confirmation of hung store, if possible.
3. Accomplish POST
STRIKE/ABORT checklist.
NOTE
A JASSM should only be
considered to be a HUNG
store, if the xy:HUNG message is received.
xy:LCD FAIL
NF
LCD abort prior to CTS.
Less [AMI] CTSS battery failure (Captive Carry missions
only).
1. Weapon will not launch.
2, LCD is terminated.
3. [AMI] If abort occurs before
CTS weapon power will not be
removed nor re-application inhibited. Weapon batteries will
not have been squibbed.
1. Verify LAR, weapon and
unlock consent status.
2. Cycle missile power.
3. If fault persists, verify
weapon power is removed.
4. Accomplish POST
STRIKE/ABORT checklist,
if applicable.
xy:OVERTEMP
NF
1. Overtemp caution fault.
The missile will set an Overtemperature Caution based on
the probability of the missile
overheating before completing
its mission, if the missile is not
launched in approximately ten
minutes.
2. Overtemp warning fault
The missile will set an Overtemperature Warning based on
the probability of the missile
overheating before completing
its mission, if the missile is not
launched in approximately one
minute.
1. For overheat caution fault,
the weapon is in danger of
overheating in not less than ten
minutes. FRMT-7xy displays
HOT in reverse video.
1. Acknowledge message.
2. If launch is not imminent,
remove missile power and
allow missile to cool for
approximately 45 minutes.
3. Cycle weapon power.
4. If fault persists, remove
weapon power.
2. For overheat warning fault,
the weapon is in danger of
overheating in not less than
one minute. FRMT-7xy displays HOT in blinking, reverse
video.
3. [AMI] Manual launch is required.
Figure 7-19 (Sheet 12 of 17)
7-64
Change 2
T.O. 1B-52H-34-2-8
JASSM Master Faults (Cont)
FAULT
INDICATION
FAULT
TYPE
POSSIBLE CAUSE
SYSTEM RESPONSE
OPERATOR ACTION
STATION MASTER FAULTS (Cont)
xy:SEEKER
NF
Terminal Guidance fault.
1. Terminal guidance has
failed. Weapon may not hit target.
2. Manual launch required.
1. Acknowledge message.
2. If the seeker mission can
be accomplished without a
seeker, proceed with
launch. Otherwise, assign
the mission to weapon with
a good seeker.
3. Cycle weapon power.
4. If fault persists, remove
weapon power.
xy:SQUIB NOGO
PF
Squibs fault.
1. Weapon power is removed.
2. SMO inhibits re-application
of weapon power.
1. Acknowledge message.
2. Accomplish POST
STRIKE/ABORT checklist.
xy:STORE ID
TF
Weapon store description
transmitted from the weapon
does not match B-52 mission
data.
Weapon power is removed.
1. Acknowledge message.
2. Verify correct B-52 mission is loaded.
3. Re-apply weapon power.
4. If fault persists, verify
weapon power is removed.
xy:TGT NOGO
TF
Target data not loaded/invalid.
1. Weapon power removed.
2. Weapon not targeted with
planned mission.
1. Acknowledge message.
2. Verify correct weapon
mission DTUC/DTC is
installed.
3. Power off the WIUs.
4. Reload the SMO and
B-52 mission.
5. Re-apply WIU power.
6. Re-apply weapon power
and perform a weapon CDE
prior to completion of IBIT
(Within 20 seconds of
weapon power application).
7. Re-apply weapon power.
8. If fault persists, verify
weapon power is removed.
xy:TIK FAIL
Less [AMI]
(Flight Test Only)
NF
Test Instrumentation Kit (TIK)
fault.
1. Weapon telemetry not available.
2. Manual launch required.
1. Acknowledge message.
2. Verify correct weapon
mission is loaded.
3. Cycle weapon power.
4. Verify telemetry response with ground.
5. Cycle telemetry power,
as required, to match
FRMT-7 to telemetry signal.
6. If fault persists and functional TIK is required, abort
mission objective.
Figure 7-19 (Sheet 13 of 17)
Change 2
7-65
T.O. 1B-52H-34-2-8
JASSM Master Faults (Cont)
FAULT
INDICATION
FAULT
TYPE
POSSIBLE CAUSE
SYSTEM RESPONSE
OPERATOR ACTION
STATION MASTER FAULTS (CONT)
xy:TLMY
(Flight Test Only)
NF
Telemetry fault.
1. Telemetry may not be on
or off as requested.
2. Manual launch required.
1. Acknowledge message.
2. Verify telemetry response
with ground.
3. Cycle telemetry power, as
required, to match FRMT-7 to
telemetry signal.
4. Remove weapon and WIU
power.
5. Reload SMO and re-apply
WIU and weapon power.
6. Command weapon telemetry on.
7. If fault persists and functional telemetry is required,
abort mission objective.
xy:WARM UP
NF
Weapon thermal conditioning 1. Weapon will not enter IBIT
and testing is not complete ten and therefore, will not align.
minutes after standby power is 2. Manual launch is required.
applied.
1. Acknowledge message.
2. Cycle weapon power.
3. If fault persists, verify
weapon power is removed.
xy:WPN DATA
NF
Weapon mission data fault.
Approximate waypoint data,
release data, target engagement data, or target data is not
valid after mass data transfer
or completion of primary target
message.
1. Acknowledge message.
2. Less [AMI] Verify the correct weapon mission DTUC
is installed.
2. [AMI] Verify DTC is correctly installed and cycle
weapon power.
3. Command auto targeting.
4. Power off the WIUs and
reload the SMO and B-52
mission.
5. Re-apply WIU power.
6. Re-apply weapon power
and perform a weapon
CDE.
7. ]Re-attempt auto-targeting.
8. Attempt manual targeting.
9. If fault persists, remove
weapon power.
Weapon may not have received correct targeting data.
Figure 7-19 (Sheet 14 of 17)
7-66
Change 2
T.O. 1B-52H-34-2-8
JASSM Master Faults (Cont)
FAULT
INDICATION
FAULT
TYPE
POSSIBLE CAUSE
SYSTEM RESPONSE
OPERATOR ACTION
STATION MASTER FAULTS (CONT)
xy:WPN NOGO
TF
1. Weapon BIT report No-Go
(CS fault, Processor fault, GPS
BIT fault, PS Fault, Engine Controls fault, PF fault, IMU fault).
2. Critical hardware fault.
3. Uncommanded data erase
fault.
4. Activate IBIT fault.
5. Release consent uncommanded fault.
6. Uncommanded weapon test
fault.
7. Reset power dropout fault.
8. [AMI] Uncommanded IBIT
fault.
1. Weapon power is removed.
2. LCD is terminated (if active).
1. Acknowledge message.
2. If fault occurred post
CTS, accomplish POST
STRIKE/ABORT checklist.
3. If fault occurred pre CTS
cycle weapon power.
4. If fault persists, remove
weapon power.
NOTE
Less [AMI] If this fault occurs in conjunction with a
WPN DTUC?? master
fault, the operator must
cycle DTUC mount power
or remove and re-insert
the
weapon
mission
DTUC in order to recover
use of the weapon mission
DTUC.
xy:WPN PRSNT
NF
1. Ejector Weapon present
monitor status and umbilical
weapon present status disagree
on weapon presence.
2. Stores table disagrees with
ejector weapon present monitor
status and umbilical weapon
present status.
3. ICSMS pylon assembly is not
configured correctly.
4. [AMI] Ejector weapon present monitor or umbilical weapon
present monitor changes status
after a hung store fault.
NOTE
1. No weapon present or at incorrect station.
2. Weapon presence cannot
be determined.
3. Incorrect mission load.
4. Manual launch required.
1. Acknowledge message.
2. Verify correct weapon
mission is loaded (CF-81).
3. Less [AMI] Verify correct
mission DTUC is installed
and the DTUC retainer knob
is in the proper position.
4. Cycle WIU power.
5. If on the ground, ensure
the pylon is properly configured.
If pylon is improperly configured, there should also be an
EJECTOR fault and all weapons on that pylon should show
the same pylon related faults.
Figure 7-19 (Sheet 15 of 17)
Change 2
7-67
T.O. 1B-52H-34-2-8
JASSM Master Faults (Cont)
FAULT
INDICATION
FAULT
TYPE
JASSM EVENT
[AMI]
NF
JASSM MSN
DATA?? [AMI]
NF
JASSM WPN
DATA?? [AMI]
NF
MSN DATA??
Less [AMI]
NF
NO CONSENT
NF
POSSIBLE CAUSE
SYSTEM RESPONSE
OTHER MASTER FAULTS
JASSM SMO is secondary and Weapon for mission planned
mission planned JASSM launch launch is not targeted.
point is within 25 minutes.
1. Mission data discrepancy.
2. Invalid or no Classified Parameters loaded.
3. Launch commanded while in
Strike Mode with a Ferry mission
loaded.
1. The JASSM SMO has detected a discrepancy with the
availability of Weapon Group
data on the DTC.
2. GPS Crypto Keys or or Almanac Data are unavailable from
the DTC and the IU upon weapon power on or after processor
reconfiguration prior to JASSM
weapon power on.
Change 2
1. Acknowledge message.
2. Make JASSM SMO primary, then power missiles.
Carrier mission data not
available or incorrect.
1. Acknowledge message.
2. Verify DTC correctly
installed, then reload mission data.
1. Weapon mission data not
available or incorrect for
available weapon.
2. Improper crypto keys
loaded. Crypto keys not valid
for current date.
3. SIM mode ranging is not
available without CLAPAR
data.
NOTE
The GPS receiver requires
approximately 15 minutes
to decipher the new daily
key after a Zulu day rollover. a NO KEYS or KEY
RECV may be displayed
while this condition exists.
1. Acknowledge message.
2. Verify DTC installed correctly.
3. Verify GPS/IU is on and
tracking satellites.
4. Verify Key Present is
displayed on the IU PKB.
5. Verify FLY-TO has been
commanded and B-52 is
navigating.
6. If keys available on the
DTC, verify current date on
CF-61.
7. Verify/deselect key
override in IU PKB.
8. Command a weapon
CDE.
9. Zeroize GPS receiver.
10. Cycle GPS/IU power.
11. If keys are not available
on the mission DTC, input
GPS keys via the IU PKB or
Crypto Fill port.
12. Cycle weapon power.
13. If fault persists, remove
weapon power.
1. Mission data discrepancy.
Carrier mission data not
available or incorrect.
Launch or jettison was commanded and either the pilot’s or
navigator’s unlock consent
switch or both are not in the unlock position.
Weapon will not launch/jettison.
1. Acknowledge message.
2. Reload B-52 mission.
3. Determine DTUC status
from FRMT-6 and if necessary, re-install DTUC into a
different DTU cavity.
1. Acknowledge message.
2. Ensure both unlock consent switches are in the unlock position.
3. Re-attempt release.
Figure 7-19 (Sheet 16 of 17)
7-68
OPERATOR ACTION
T.O. 1B-52H-34-2-8
JASSM Master Faults (Cont)
FAULT
INDICATION
FAULT
TYPE
POSSIBLE CAUSE
SYSTEM RESPONSE
OPERATOR ACTION
OTHER MASTER FAULTS
UNLOCK CONSENT
NF
The Navigator’s unlock consent
switch and the Pilot’s weapon
consent switch are in opposite
positions.
No unlock consent enable
and ejector squib fire is not
possible.
NOTE
[AMI] PMCP Unlock Consent Switch position monitor is not available to the
SMO unless WIU power is
applied. Default is LOCK.
WPN DTUC??
Less [AMI]
NF
1. Weapon DTUC access failure
has occurred. The JASSM SMO
has detected a discrepancy with
the availability of data on the
weapon mission DTUC.
2. Weapon mission DTUC is not
available when access is needed.
3. Improper crypto keys loaded
or crypto keys are not valid for
the current date.
1. SIM mode ranging is not
available without CLAPAR
data.
1. Acknowledge message.
2. Place both unlock consent switches in the unlock
position.
3. If the fault persists, set
both switches to the lock
position.
4. If fault persists, remove
weapon power and cycle
WIU power.
1. Acknowledge message.
2. Verify correct mission
DTUC is installed and the
DTUC retainer knob is in
the proper position.
3. Confirm DTU status on
FRMT-6.
4. Remove/reseat weapon
mission DTUC.
5. Re-install the mission
DTUC into a different DTU
cavity.
6. Verify the correct date
was entered on CF-61.
7. If available, input current
crypto keys through the IU
PKB.
NOTE
If this fault occurs in conjunction with a xy:WPN
NOGO master fault, remove and re-insert the
weapon mission DTUC.
Figure 7-19 (Sheet 17 of 17)
Change 2
7-68A
T.O. 1B-52H-34-2-8
JASSM Advisories
Less [AMI]
Fault Indication Coding:
• x = L - LEFT PYLON OR R - RIGHT PYLON LOCATION
• y = 1, 2, 3, 6, 7, OR 8 STATION NUMBER
FAULT
INDICATION
POSSIBLE CAUSE
OPERATOR ACTION
ALIGN FAIL
(Reverse Video)
Missile alignment failure.
Check OAS Nav Mode is INS AIDED
NAV. Recycle missile power.
B: LOCATION
(Reverse Video)
The BAY location select switch was selected.
B (bay) is not a selectable location,
do not select bay location switch,
and verify selection.
LCD ENTRY
(Reverse Video)
No JASSM launch point/direct target is selected or no weapon is
ready to be launched when the manual launch switch is momentarily
depressed while in manual launch mode.
1. Ensure current destination is a
JASSM launch point/direct target.
2. Ensure the associated weapon is
operational and targeted.
LOCATION??
(Reverse Video)
A station switch was selected with no location selected or an operation was attempted without designating a Location on the
WCP.
Select a location before selecting a
station.
LOC/STA??
(Reverse Video)
1. A weapon is not present at one or more of the selected stations
when weapon power on, jettison, CDE, or TM on/off is commanded.
Select only stations that have a
weapon present.
2. No location/station is selected when weapon power on/off, jettison, CDE, or TM on/off is commanded.
Select location(s) and station(s) prior
to placing weapon jettison switch in
SEL position.
3. A weapon, which has a permanent fatal Fault, was selected individually when weapon power on/off, CDE, or TM on/off was commanded.
Select only stations that do not have
a weapon with a permanent fatal
Fault.
4. An unpowered weapon was selected when CDE was commanded.
Select only weapons that have power applied.
5. A weapon, where CTS has been commanded, was selected when
CDE, TM on/off, FTS enable, jettison, weapon power on was commanded.
Do not command power off to a
weapon that has received the CTS
command.
STATION??
(Reverse Video)
An invalid station select switch (4 or 5) was selected.
Select a valid station (1-3, 6-8).
WPN GPS DATA
(Reverse Video)
Input/Output with the Interface Unit (IU) failed (GPS Almanac,
Ephermeris, AS/SV Configuration data, or Time Mark Data access
attempt).
Verify the correct weapon DTUC is
installed and powered, and the IU
and aircraft GPS receiver are operational.
xy:LCD ENTRY
(Reverse Video)
Entry into Launch Countdown (LCD) was attempted but was unsuccessful due to LCD entry check failure.
Review FRMT-7 and Master Faults
displayed and re-attempt launch.
Figure 7-20 Sheet (1 of 3)
7-68B
Change 2
T.O. 1B-52H-34-2-8
JASSM Advisories (Cont)
[AMI]
Fault Indication Coding:
• x = L - LEFT PYLON OR R - RIGHT PYLON LOCATION
• y = 1, 2, 3, 6, 7, OR 8 STATION NUMBER
FAULT
INDICATION
POSSIBLE CAUSE
OPERATOR ACTION
B: LOCATION
(Reverse Video)
The BAY location select switch was selected.
B (bay) is not a selectable JASSM
location, do not select bay location
switch, and verify selection.
JASSM ALIGN FAIL
(Reverse Video)
Missile alignment failure.
1. Check OAS Nav Mode is INS
AIDED NAV.
2. Recycle missile power.
JASSM EVENT
(Reverse Video)
The JASSM SMO is secondary and a mission planned
JASSM launch point is within 30 minutes.
1. Proceed with mission profile.
2. If required, make JASSM SMO
prime, then power and align missiles.
JASSM GPS DATA
(Reverse Video)
I/O with the IU failed.
1. Verify that the GPS Initialization
file exists on the DTC and the aircraft
IU and GPS receiver are operational.
JASSM LCD ENTRY
(Reverse Video)
No JASSM launch point/direct target is selected or no weapon is ready to be launched when the manual switch is momentarily depressed while in manual launch mode.
1. Entry into LCD was expected but unsuccessful.
2. LCD is not initiated for the current release event.
3. A weapon is not selected for launch and:
A. If in automatic launch mode, aircraft is within the InZone LAR and will be at the point of closest approach when
LCD is complete.
B. If in manual launch mode, a manual launch command
is present. SMO will reset the manual launch command if
launch entry requirements are not met.
1. Ensure current destination is a
JASSM launch point/direct target.
2. Ensure the associated weapon is
operational and targeted before
pressing the manual launch switch
while in manual launch mode.
JASSM LOC/STA??
(Reverse Video)
1. A weapon is not present at one or more of the selected stations when weapon power on, jettison, CDE, or TM on/off is
commanded.
2. No location/station is selected when weapon power on/
off, jettison, CDE, or TM on/off is commanded.
3. A weapon with a permanent fatal fault was selected individually when weapon power on/off, CDE, or TM on/off commanded.
4. A weapon, which is not powered and not permanently fatal
faulted, was selected when CDE was commanded.
5. A weapon, where CTS has been commanded, was selected when CDE, TM on/off, FTS enable, jettison, weapon
power on was commanded.
1. Select appropriate location(s) and
station(s) with weapon(s) present.
1. PCP Left Pylon switch was selected but there is no SMO
assigned to the LP location.
2. WCP LOCATION L PYLON switch was selected but there
is no SMO assigned to the LP location.
3. WCP LOCATION LEFT PYLON switch was selected subsequent to selection of the Bay location and/or the Right Pylon location and the SMO assigned to the LP location is not
the same as the SMO assigned to the previously selected
location.
1. Deselect the PCP LP switch and
assign a SMO to the Left Pylon location, if required.
2. Assign a SMO to the Left Pylon
location before selecting the WCP
LOCATION L PYLON switch, if required.
L: LOCATION??
(Reverse Video)
2. Select location(s) and station(s)
prior to entering the command.
3. Do not select a station having a
weapon with a permanent fatal fault.
4. Select only weapons that have
power applied.
5. Do not enter a command to a
weapon that has received the CTS
command.
Figure 7-20 (Sheet 2 of 3)
Change 2
7-68C
T.O. 1B-52H-34-2-8
JASSM Advisories (Cont)
[AMI]
Fault Indication Coding:
• x = L - LEFT PYLON OR R - RIGHT PYLON LOCATION
• y = 1, 2, 3, 6, 7, OR 8 STATION NUMBER
FAULT
INDICATION
POSSIBLE CAUSE
OPERATOR ACTION
LOCATION??
(Reverse Video)
WCP station switch was selected with no location selected.
Select a location on the WCP.
LOC/STA??
(Reverse Video)
No location and station selected when weapon power on/off
or jettison is commanded.
Select location(s) and station(s) prior
to entering the command.
R: LOCATION??
(Reverse Video)
1. PCP Right Pylon switch was selected but there is no SMO
assigned to the RP location.
2. WCP LOCATION R PYLON switch was selected but there
is no SMO assigned to the RP location.
3. WCP LOCATION RIGHT PYLON switch was selected
subsequent to selection of the Bay location and/or the Left
Pylon location and the SMO assigned to the RP location is
not the same as the SMO assigned to the previously selected
location.
1. Deselect the PCP RP switch and
assign a SMO to the Right Pylon
location, if required.
2. Assign a SMO to the Right Pylon
location before selecting the WCP
LOCATION R PYLON switch, if required.
STATION??
(Reverse Video)
1. An invalid station select switch (4 or 5) was selected.
2. Individual WCP station switch was selected with multiple
locations selected and the SMO has inhibited such.
1. Select a valid station (1-3, 6-8).
2. Select the ALL station switch or
have only one location selected.
STORES DATA FAIL
(Reverse Video)
A failure occurred during stores data loading from the DTC.
1. Ensure the DTC is properly inserted.
2. Reattempt mission data load.
3. Determine DTR status from
FRMT-6.
4. Reinstall DTC to different DTR
and reload mission.
x:JETT INHIB
(Reverse Video)
Either a WCP selective jettison or a BMJCP Jettison All has
been commanded for a location for which there is no SMO
assigned.
1. For a WCP selective jettison, select the location(s) for which the primary SMO is assigned.
2. For a BMJCP Jettison All, change
the primary SMO and reissue the Jettison All request.
xy:LCD ENTRY
(Reverse Video)
Entry into Launch Countdown (LCD) was attempted but was
unsuccessful due to LCD entry check failure.
Review FRMT-7 and Master Faults
displayed and re-attempt launch.
Figure 7-20 (Sheet 3 of 3)
7-68D
Change 2
T.O. 1B-52H-34-2-8
JASSM Status Messages
MESSAGE TEXT
STATUS INDICATED
GO/NOGO COMPLT (Normal Video)
The Go/No-Go Test has been completed for all weapons that
have had power applied.
SIT COMPLT (Normal Video)
The System Integrity Test has been completed for all weapons
that have had power applied.
CDE COMPLT (Normal Video)
Less [AMI]
JASSM CDE COMPLT (Normal Video)
[AMI]
Classified data erase has been completed for all selected
weapons.
Figure 7-21
Safe Release Advisories
Safe release advisories do not inhibit launch. Possible collision between weapons and between weapon and aircraft can occur if weapon is launched with a
release advisory displayed.
NOTE
In order of priority, safe release advisories follow weapon launch advisories in
the following order:
RELEASE ADVISORY
INDICATION
CORRECTIVE ACTION
ROLL
Maximum roll angle (10°) or maximum
roll rate (5°/second) violated.
Decrease aircraft roll angle or
maximum roll rate.
PITCH
Maximum pitch angle (10°) or maximum pitch rate (5°/second) violated.
Decrease aircraft pitch angle or
maximum pitch rate.
LEVL_OFF
Vertical velocity or vertical acceleration
(< –0.5 G or >2.0 G) is too high.
Decrease altitude rate of change.
YAW
Maximum yaw rate (1°/second) violated.
Decrease aircraft yaw rate.
(blank)
No release advisory exists.
None.
Figure 7-22
Change 2
7-69
T.O. 1B-52H-34-2-8
Weapon Launch Advisories
NOTE
• Weapon launch advisories are displayed when crew actions are required, to
obtain an effective JASSM launch.
• The weapon launch advisories are shown below in the order of highest priority.
LAUNCH ADVISORY
INDICATION
CORRECTIVE ACTION
CLIMB (Blinking, Bright
Underlined Video)
Aircraft altitude is at, below or within 500
feet of the minimum altitude for release.
Applicable when the aircraft is In-Zone
or In-Zone is achievable.
Increase aircraft altitude rate of
change.
ACCEL (Blinking, Bright
Underlined Video)
Aircraft speed is at, below or within 0.02
Mach of the minimum Mach for release.
Applicable when the aircraft is In-Zone
or In-Zone is achievable.
Increase aircraft airspeed.
DIVE (Blinking, Bright
Underlined Video)
Aircraft altitude is at, above or within 500
feet of the maximum altitude for release.
Applicable when the aircraft is In-Zone
or In-Zone is achievable.
Decrease altitude rate of change.
DECEL (Blinking, Bright
Underlined Video)
Aircraft speed is at, above, or within 0.02
Mach of the maximum Mach for release.
Applicable when the aircraft is In-Zone
or In-Zone is achievable.
Decrease aircraft airspeed.
HDG TOL
(Blinking Video)
Current aircraft heading is within 6° to 9°
of heading tolerance limits.
Applicable when the aircraft is not InZone, but In-Zone is achievable.
Put the aircraft back on preplanned
path or wait until the aircraft is InZone for the TRN LEFT or TRN
RIGHT indication.
HDG TOL
(Blinking, Bright Video)
Current aircraft heading is within 3° to 6°
of heading tolerance limits.
Applicable when the aircraft is not InZone, but In-Zone is achievable.
Put the aircraft back on preplanned
path or wait until the aircraft is InZone for the TRN LEFT or TRN
RIGHT indication.
HDG TOL (Blinking,
Bright Underlined Video)
Current aircraft heading is within 3° or
outside of heading tolerance limits.
Applicable when the aircraft is not InZone, but In-Zone is achievable.
Put the aircraft back on preplanned
path or wait until the aircraft is InZone for the TRN LEFT or TRN
RIGHT indication.
Figure 7-23 (Sheet 1 of 2)
7-70
T.O. 1B-52H-34-2-8
LAUNCH ADVISORY
INDICATION
CORRECTIVE ACTION
TRN LEFT
(Blinking Video)
Aircraft heading is within 6° to 9° of the
right heading tolerance limit for release.
(Turn LEFT to correct.) Applicable when
the aircraft is In-Zone only.
Turn aircraft to the left until within
tolerance for release.
TRN LEFT
(Blinking, Bright Video)
Aircraft heading is within 3° to 6° of the
right heading tolerance limit for release.
(Turn LEFT to correct.) Applicable when
the aircraft is In-Zone only.
Turn aircraft to the left until within
tolerance for release.
TRN LEFT (Blinking,
Bright Underlined Video)
Aircraft heading is within 3° or outside of
the right heading tolerance limit for release. (Turn LEFT to correct.) Applicable when the aircraft is In-Zone only.
Turn aircraft to the left until within
tolerance for release.
TRN RIGHT
(Blinking Video)
Aircraft heading is within 6° to 9° of the
left heading tolerance limit for release.
(Turn RIGHT to correct.) Applicable
when the aircraft is In-Zone only.
Turn aircraft to the right until within
tolerance for release.
TRN RIGHT
(Blinking, Bright Video)
Aircraft heading is within 3° to 6° of the
left heading tolerance limit for release.
(Turn RIGHT to correct.) Applicable
when the aircraft is In-Zone only.
Turn aircraft to the right until within
tolerance for release.
TRN RIGHT (Blinking,
Bright Underlined Video)
Aircraft heading is within 3° or outside of
the left heading tolerance limit for release. (Turn RIGHT to correct.) Applicable when the aircraft is In-Zone only.
Turn aircraft to the right until within
tolerance for release.
(blank)
No launch advisory exists.
None.
Figure 7-23 (Sheet 2 of 2)
7-71
T.O. 1B-52H-34-2-8
FRMT-7 Weapon Faults
FRMT-7 MESSAGE
VIDEO
HIGHLIGHT
CAUSE
ABORT
R
ACFT PWR
R
LCD abort after CTS.
CTSS Battery Failure.
3-Phase 115V AC power Fault (uncommanded on).
28 VDC #1 Power Fault.
28 VDC #2 Power Fault (uncommanded off).
BIA FAIL
R
BIA Fault.
BUS TEST
R
Weapon Bus Test Fault.
COMM NOGO
R
Weapon communication Fault.
Aircraft ID Fault.
Surface/Fin Delay Fault.
Almanac Received Fault.
GPS Keys Transfer Fault.
Mass Data Transfer Protocol Fault.
Simulated Launch Fault.
Timeline Abort Fault.
Timeline Integration Fault.
Uncommanded Timeline Abort.
Min TXA Received Fault.
CTSS
R
Uncommanded CTS Fault.
Uncommanded CTSS Fault.
EJECTOR
R
Ejector status discrepancy Fault.
Uncommanded Ejector Lock.
ERASE FAIL
R
Data Erase Failure Fault.
FTS
R
Activate FTS Fault.
GPS DATA
R
Ephemeris Received Fault.
Time Received Fault.
GPS INIT
R
AS/SV Received Failure.
HTR PWR
R
3-Phase 115 VAC Power Fault (uncommanded off).
HUNG
R
Hung store.
LCD FAIL
R
OVERTEMP
R
LCD abort prior to CTS.
CTSS Battery Failure.
Over Temperature Caution Fault.
R/Blinking
Over Temperature Warning Fault.
SEEKER
R
Terminal Guidance Fault.
Figure 7-24 (Sheet 1 of 2)
7-72
T.O. 1B-52H-34-2-8
FRMT-7 MESSAGE
VIDEO
HIGHLIGHT
SQUIB NOGO
R
Squibs Fault.
STORE ID
R
Store description Fault.
TGT NOGO
R
Targeting Fault.
TIK FAIL
R
TIK Fault.
TLMY
R
Telemetry Fault.
WARM-UP
R
Warm-up Complete Fault.
WPN DATA
R
Weapon Mission Data Fault.
WPN NOGO
R
WPN PRSNT
R
Reset Power Dropout Fault.
Current Weapon State Fault.
BIT report Fault.
(CS Fault, Engine Control Fault, GPS Fault, IMU Fault,
PF Fault, Processor Fault, PS Fault).
Critical hardware Fault.
Uncommanded Data Erase Fault.
Activate IBIT Fault.
Uncommanded IBIT Fault.
Release Consent Uncommanded High Fault.
Reset Power Dropout Fault.
Uncommanded Weapon Test Fault.
Weapon present status discrepancy.
XXX-YYYZ
N
Store ID when Go/NoGo Test or SIT is active and no
weapon Faults exist.
28VDC2
R
28 VDC #2 Power Fault (uncommanded on).
LCD Abort after CTS.
(blank)
N
Weapon is not present or no Fault exists for this weapon or WIU power for this pylon is off.
CAUSE
Figure 7-24 (Sheet 2 of 2)
7-73/(7-74 blank)
BLA
T.O. 1B-52H-34-2-8
Glossary
ACU
Avionics Control Units
EED
Electroexplosive Device
ADP
Air Data Probe
EMI
Electromagnetic Interference
Air Force Mission Support System
FCP
Flight Computer Program
AFMSS
AIU
Armament Interface Unit
FDRC
Fault Data Recorder Cartridge
AJCP
Alternate Jettison Control Panel
FMS
Flight Management System
AOC
Air Operations Center
FSP
Flush Static Port
AS/SV
Anti-Spoofing/Satellite Vehicle
FTS
Flight Termination System
ATC
Automatic Target Correlator
GMCP
ATL
Above Target Level
GPI
Global Position Indicator
ATO
Air Tasking Order
GPS
Global Positioning System
AUR
All Upround Ready
GWD
Gravity Weapon Delivery
Aircraft/Weapon/Electronic software
HSAB
Heavy Stores Adapter Beam
A/W/E
BIA
Bomb Impact Assesment
BIT
Built In Test
BTT
Bearing To Target
C&D
Controls and Displays
CAD
Controls And Displays processor
CCA
Circuit Card Assembly
CDE
Classified Data Erase
CEM
Conventional Enhancement Modification
CEP
Circular Error Probable
CPOA
Closest Point of Approach
CTOF
Current Time Of Flight
CTS
CTSS
Commit to Separate (synonymous to ITL)
Commit to Store Separation
CWI
Conventional Weapons Integration
DMPI
Desired Mean Point of Impact
DPPDB
Digital Point Position Database
DTC
DTCU
Data Transfer Cartridge
Data Transfer Controller Unit
DTD
Digital Transfer Device
DTED
Digital Terrain Elevation Data
DTG
Distance To Go
DTU
Data Transfer Unit
DTUC
E
ECU
Data Transfer Unit Cartridge
East
Environmental Control Unit
IBIT
ICSMS
Ground Maintenance Computer Program
Initiated Built-in-Test
Integrated Conventional Stores
Management System
IKB
Integrated Keyboard
IMU
Inertial Measurement Unit
IMV
Instrumented Measurement Vehicle
INS
Inertial Navigation System
IR
Infrared
IIR
Imaging and Infrared
ITL
Intent to Launch (synonymous to CTS)
IUS
Interface Unit Software
IZ
In-Zone
JAGR
JASSM Anti-Jam GPS Receiver
JASSM
Joint Air-to-Surface Standoff Missile
LAR
Launch Acceptability Region
LCD
Launch Countdown
LOS
Line of Sight
LP
Launch Point
LRU
Line Replaceable Unit
MCU
Missile Control Unit
MF
Master Fault
MFD
Multifunction Display
MIDB
Modern Integrated Intelligence Database
MIU
Missile Interface Unit
MPS
Mission Planning System
Glossary 1
T.O. 1B-52H-34-2-8
MSG
N
Advisory message acknowledgment switch
SIT
System Integrity Test
North
SMIU
Stores Management Interface Unit
NAWD
Navigation and Weapon Delivery Processor
SMO
Stores Management Overlay
NEW
Net Explosive Weight
NF
Non Fatal
TACT Ferry
Tactical Ferry Flight
TAM
Target Area Module
NTM
National Technical Means
N/A
Not Applicable
TF
Transient Fatal
OAS
Offensive Avionics System
T/R
Transformer/Rectifier
OCP
Operational Computer Program
TAL
Transfer Alignment Maneuver
OML
Outer Mold Line
TDS
Target Data Set
PCP
Power Control Panel
TIK
Test Instrumentation Kit
PDU
Power Distribution Unit
TLI
Timeline Integration
PMD
Prime Mission Data
TM
Telemetry
PF
Permanent Fatal
TOF
Time of Flight
Precision Guided Munition Target Database
TOT
Time on Target
PME
Prime Mission Equipment
TTG
Time to Go
PTM
Precision Targeting Module
TXA
Transfer Alignment
PTOF
Planned Time Of Flight
UC
Upper Corner
PVE
Preset–Verify–Execute
UTC
Universal Time Coordinated
REPF
Rear Echelon Production Facility
VAC
Volts Alternating Current
RF
Radio Frequency
VDC
Volts Direct Current
ROB
Range On Bearing
W
PGMTDB
S
SC
SAASM
TBMCS
Theater Battle Management Core System
West
South
WCE
Weapon Control Equipment
Safety Critical
WCP
Weapon Control Panel
Selective Availability Anti-Spoofing Module
WF
Wire Frame
SA
Situation Awareness
WGS-84
SAU
Splitter Amplifer Unit
WIU
Weapon Interface Unit
SAIR
Safe and In–Range
WPM
Weapon Planning Module
Glossary 2
World Geodetic System 1984
T.O. 1B-52H-34-2-8
Alphabetical Index
*DENOTES ILLUSTRATION
Page
A
E
Advisories and Status Messages
7-52A
After Engine Start (Aircraft Power and Cooling
Air Available)
2-7
After Landing Procedures
2-23
After Takeoff (RN/N)
2-9
Aircraft Commander’s Responsibilities
3-6
Air Data System
1-6
Alternate Jettison Control Panel
1-24*
Automatic Launch Determination
7-46
Automatic Missile Launch Checklist (RN-N)
2-19
Avionics
1-6
B
B-52 Carrier Equipment
1-3
B-52/JASSM Weapon System
1-3
B-52 Mission Data Load Display (CF-81
1-52C*
Backup Notification Procedures
3-6
Before Exterior Inspection (Power Off) (RN/N) 2-3
Before Launch Check (RN)
2-18
Blow Off Wedges
1-5
C
Circuit Breaker Panels
Circuit Protection
Commands for OAS Power Control Panel
and Missile Control Panel (CF-E)
Control Function (CF) Displays
Control Function (CF) Menu
Page
1-23*
1-23*
1-55*
1-30
1-30C*
D
Definition of Terms
3-6
Destination Table Display (FRMT-10,nn)
1-69*
Direct Target Copy Command (CF-Dn)
1-52G
Direct Targeting Data Entry Procedures
2-13
Direct Target Definition
Display (CF-588,n)
1-42*,7-20A*
Emergency Aircrew Procedures
Emergency Jettison
Engine
Exterior Inspection (Power Off) (RN/N)
3-1
3-5
1-6
2-3
F
FCP Supervision Menu (CF-6)
1-46, 1-48*
Firefighting and Evacuation Criteria
3-7, 3-7*
Format (FRMT) Displays
1-56
FRMT-7 Missile Faults
7-52A
FRMT-7 Weapon Faults
7-52A, 7-72*
FTS Enable/Disable Command (CF-57C,xy)
(OTL Only)
4-3
FTS Power Source Command (CF-57D)
(OTL Only)
4-3
Fuselage
1-5
Fuel System
1-5
G
General Procedures
Ground Safeing Procedures (RN-N)
2-3
2-23
H
Heavy Stores Adapter Beam JASSM
Configuration
1-8*
I
Inflight Emergency Notification Procedures
(World Wide)
Inflight Notification Procedures
Inflight Procedures
In-Range LAR
In-Range/In-Zone Indication
Integrated Keyboard (IKB)
In-Zone LAR
Change 2
3-7
3-6
2-9
7-31
7-43
1-18*
7-36
Index-1
T.O. 1B-52H-34-2-8
Page
Page
J, K
JASSM Achievable In-Range LAR
7-32*
JASSM Achievable In-Zone LAR
7-37*
JASSM Advisories
7-68B*
JASSM Anti-Ice Operation
5-1
JASSM Closest Point of Approach Outside
In-Zone LAR
7-41*
JASSM Control Function (CF) Commands 1-30B*
JASSM Control Switches
1-25*
JASSM Cover
1-7
JASSM Employment Overview
7-3
JASSM Flight Profile Summary
7-4*
JASSM Flight Profiles
7-5*
JASSM Format Commands
1-57*
JASSM Free Flight Sequence
7-48
JASSM FRMT (Format) Menu
1-58*
JASSM IKB Commands
1-19*
JASSM Initialization Timeline
7-9*
JASSM In-Zone LAR
7-36*
JASSM Jettison and Launch Envelopes
5-1, 5-3*
JASSM Launch Or Jettison
With Open Bomb Bay Doors
5-1
JASSM Launch Sequence Timeline (Typical) 7-46*
JASSM Master Faults
7-53*
JASSM Preferred Launch/Jettison Sequence 7-49*
JASSM Program Commands
1-74*
JASSM Safe Separation and Deconfliction
5-2
JASSM SMO Flight Test Software Commands 4-1
JASSM SMO Software
1-27
JASSM Static LAR
7-29*
JASSM Status and Inventory
Display (FRMT-7)
1-62*, 7-14*
JASSM Status and Inventory Display with
Selected Station (FRMT-7xy)
1-64*, 7-15*
JASSM Status Messages
7-69*
JASSM Supervision Menu (CF-57)
1-32*, 4-1
JASSM Suspension System
1-7
JASSM Target Assignment (Manual Targeting)
Display (CF-586)
7-19*
JASSM Target Definition
7-21*
JASSM Targeting Menu (CF-58)
1-34*
JASSM Telemetry Antenna
4-2*
JASSM Unachievable In-Range LAR
7-34*
JASSM Unachievable In-Zone LAR
7-40*
Jettison Control Switches
1-25*
Joint Air-to-Surface Standoff Missile
(JASSM)
1-3, 1-4*
Index-2
Change 2
L
Launch Procedures
2-17
M
Manual Launch Determination
7-47
Manual Missile Launch Checklist (RN-N)
2-20
Master Faults
7-52A
MAU-12 Ejector Rack With Extension
1-9*
Messages
7-52A
MFD Display Figures
1-12
Missile and Ejector Status
7-10
Missile Check (RN/N)
2-7
Missile Control Panel Backup
Display (CF-E)
1-52G, 1-53*
Missile Data Flow (Typical)
1-13*
Missile Jettison
3-2, 7-50
Missile Launch
7-45
Missile Launch Procedures
2-18
Missile Launch Process
7-45
Missile Launch Restrictions
7-48
Missile Launch Termination
7-47
Missile Mission Data and Targeting
7-17
Missile Mission Types
7-3
Missile Power Application
7-8
Missile Power Application (N)
2-9
Missile Power Removal
7-15
Missile Preferred Launch Sequence
2-12*
Missile Preferred Jettison Sequence
3-2*
Missile Preparation For Launch (RN-N)
2-17
Missile/Target Assignment Display (CF-586) 1-36*
Missile/Target Assignment (Manual
Targeting Procedures
2-10
Missile Targeting Methods
7-17
Missile Targeting Procedures (RN-N)
2-10
Mission Data Load Display (CF-81)
1-52C*
Mission Planning
6-1
Mission Planning Flow and Partitioning
6-3*
Mission Planning Functional Flow
6-5*
Mission Planning Modules
6-3
Mission Planning Considerations
6-7
Mission Planning Timelines
6-4
Mission Supervision Menu (CF-8)
1-51, 1-52A*
Multifunction Displays
1-12, 1-21*
T.O. 1B-52H-34-2-8
Page
N
Notification Procedures – Dangerous Materials 3-6
Normal Notification Procedures
3-6
O
OAS Power Control Panel
OAS/Joint Air to Surface Standoff
Missile Operation
OAS/Weapon System Related Controls and
Displays
Offensive Avionics System (OAS)
Interface
Operating Limitations
1-17*
7-3
1-11
1-11
5-1
P, Q
Pilots’ Bomb Bay & Missile Jettison Control
Switch Commanded Jettison
1-25
Pilot’s Munition Consent Panel
1-16*
PME Status Display (FRMT-6)
1-60*
Post Strike/Abort Procedures
2-22
Post Strike/Abort (RN/N)
2-22
Preferred Launch/Jettison Sequence
7-48
Preflight Procedures
2-3
PRGM Display In-Range/In-Zone Indications 7-44*
Prime Mission Data
1-28
Program Displays (PRGM)
1-74, 1-75*
PTM Timeline Definition
6-6*
R
Release Advisory Display
REPF Mission Planning
Page
SMO Load Menu (CF-62)
SMO MFD Displays
SMO Restart
SMO Termination
Stores Inventory Summary
Display (FRMT-77)
Supplementary Data
1-50*
1-27
7-52
7-52
7-68B*
4-1
T
Targeting Process Control (CF-DD and
CF-DE)
1-52G
Target Ranging
7-29
Target Ranging Indications
7-43
Targeting Techniques
7-22
Telemetry Power OFF Command (CF-57B)
(Test Only)
4-3
Telemetry Power ON Command (CF-57A)
(Test Only)
4-1
Test Instrumentation Kit (TIK)
4-1
Transfer Alignment (TXA) Halt Command
(CF-57E,xy) (Captive Carry Only)
4-4
Transfer Alignment (TXA) Re-Init Command
(CF-57F,xy) (Captive Carry Only)
4-4
U
Unit Mission Planning Integration
USAF JASSM Mission Planning Module
V
Vertical Tail
1-28, 1-29*
6-4
S
Safe Release Advisories
7-44, 7-69*
Safe Release and Weapon Launch Advisories 7-52A
Selective Jettison Using the AJCP
3-4
Selective Jettison Using the WCP/SMO
3-3
Selected Direct Target Deselection
Command (CLR-D)
1-52G
SIM Mode Response Times
7-51*
Simulated Missile Loadout
7-51
Simulated Ranging
7-51
Simulated Targeting Operations
7-51
Simulated WCE Responses
7-51
Simulation Capabilities
7-51
SMO Control Function (CF) Commands
1-30*
SMO Format Commands
1-57*
SMO FRMT (Format) Menu
1-58*
6-4
6-2
1-5
W, X, Y, Z
Warhead
1-5
WCE Power Application
7-7
WCE Power Removal
7-8
Weapon Assignment Data Display (CF-DF or
CF-DB from FRMT-7, 7A, 7C or 7xy)
1-68A*
Weapon Control Equipment (WCE) Status
7-7
Weapon Control Panel
1-14*
Weapon Group Load Menu
(CF-82A, CF-82C)
1-52E*
Weapon Jettison
1-22
Weapon Launch Advisories
7-43, 7-70*
Weapon Monitor and Power Control
7-7
Weapon Summary Display
(FRMT-12,nn/FRMT-12,Dn)
1-71*
Weapon Supervision Menu (CF-5)
1-30, 1-30E*
Wing Flutter Airspeed Limitations
5-1
Wings
1-5
WPM Timeline Definition
6-6*
Change 2
Index-3/(Index-4 blank)
BLA