96-590011-25_0911.fm Page 1 Monday, August 29, 2011 4:06 PM
LOG OF SUPPLEMENTS
Baron 95-B55 and 95-B55A
Pilot’s Operating Handbook
and
FAA Approved Airplane Flight Manual
P/N 96-590011-25
September, 2011
FAA Supplement must be in the airplane for all flight
operations when subject equipment is installed.
PART
NUMBER
SUBJECT
REV
NO.
DATE
130598
Landing Gear Safety System
3
1/83
*131262
Operation In The United Kingdom
1
8/03
131391
Manual Cowl Flaps (Kit 55-9017)
6/80
55-590000-51
Goodyear Electrothermal Propeller Deice
10/78
58-590000-49
Inside Cabin Door Handle With
Open/Closed Placard
12/90
95-590014-47
Goodrich Reservoir Type Pneumatic Deicing System
10/78
96-590000-1
Auxiliary Fuel Tank Annunciator
Light
(Kit 96-9001-1)
11/93
96-590010-19
King KN-74 Area Navigation
96-590010-21
Nickel-Cadmium Battery and
Charge Current Detector
10/76
SA126CE
Hartzell Propellers
4/1/69
1
2/79
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96-590011-25_0911.fm Page 2 Monday, August 29, 2011 4:06 PM
Log Of Supplements (Cont’d)
96-590011-25
September, 2011
PART
NUMBER
SA795CE
SUBJECT
Hartzell Propellers
REV
NO.
DATE
2
2/13/76
NOTE: Supplements applicable to equipment other than that
installed may, at the discretion of the owner/operator, be
removed from the manual.
* Supplements marked with an asterisk will not be supplied
with handbooks sold through Authorized Raytheon Outlets
due to their limited applicability. If a document is required for
your airplane, please order the document through normal
channels.
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2 of 2
BEECHCRAFT LANDPLANES
MODEL 9 5 - 5 5 SERIES
PILOT'S OPERATING HANDBOOK AND
FAA APPROVED AIRPLANE FLIGHT MANUAL
SUPPLEMENT
for the
GOODYEAR ELECTROTHERMAL
PROPELLER DEICE
GENERAL
The information in this supplement is FAA approved material and must be attached to the Pilot's Operating Handbook and FAA Approved Airplane Flight Manual when the
airplane is equipped with a Goodyear Electrothermal Propeller Deice System that has been installed in accordance
with BEECHCRAFT FAA approved data.
This document supersedes or adds to the Pilot's Operating
Handbook and FAA Approved Airplane Flight Manual only
where covered in the items contained herein.
LIMITATIONS
Do not operate the system unless engine is operating.
Airplanes equipped with approved emergency static air
source, surface deicing systems, pitot heat, heated stall
warning, windshield defogging or storm windows, and external antenna mast capable of withstanding ice load are
considered to be equipped for flight into icing conditions as
governed by operational practices of Bureau of Flight
Standards Release No. 434. When not equipped accordingly a placard as shown must be installed.
FAA Approved
Revised: October, 1 9 7 8
P/N 5 5 - 5 9 0 0 0 0 - 5 1
PLACARDS
On Instrument Panel:
WARNING
THIS AIRCRAFT IS NOT FULLY EQUIPPED
FOR FLIGHT I N ICING CONDITIONS
EMERGENCY PROCEDURES
1. Loss of one generator, off-load unnecessary electrical
equipment. Turn off the propeller deice system while
operating the cabin heater blower or the landing gear
motor. Monitor electrical loads so as not to exceed
generator capacity.
2 . Abnormal Reading on Propeller Deice Ammeter
a. Zero Amps
Check propeller deice switch. If the circuit breaker
in the switch has tripped, a wait of approximately
30 seconds is necessary before resetting the
switch to the ON position. If ammeter reads 0 and
switch has not tripped or if ammeter still reads 0
after the switch has been reset, turn the switch off
and consider t h e propeller deice system
inoperative.
b. Zero to 7 Amps
If propeller deice system ammeter occasionally or
regularly indicates less than 7 amps, operation of
the propeller deice system can continue unless
serious propeller imbalance results from irregular
ice throw-offs.
FAA Approved
Revised: October, 1 9 7 8
P/N 55-590000-51
c.
1 1 to 1 5 Amps
If propeller deice system ammeter occasionally or
regularly indicates 1 1 to 1 5 amps, operation of the
propeller deice system can continue unless
serious propeller imbalance results from irregular
ice throw-offs.
d.
More than 15 Amps
If the propeller deice system ammeter occasionally
or regularly indicates more than 1 5 amps, the
system should not be operated unless the need for
propeller deice is urgent.
NORMAL PROCEDURES
WARNING
To minimize slip ring pitting, do not operate the
system w i t h engines inoperative.
PREFLIGHT
1 . W i t h engines operating, place propeller deice switch i n
the ON position.
2. Check propeller deice system ammeter for reading of 7
to I 1 amperes.
3. A small momentary deflection of the needle may be
noticed approximately every 30 seconds: This is due to
the switching action of the timer and is an indication of
normal operation of the system.
F A A Approved
Revised: October, 1978
P / N 55-590000-51
IN FLIGHT
1. To place the system i n operation, move propeller deice
switch to the ON position. The system may be operated continuously i n flight and w i l l function automatically until the switch is turned off.
2. Propeller imbalance may be relieved by varying rpm.
Increase rpm briefly and return to desired setting, repeating if necessary.
PERFORMANCE - No change
Approved:
&J
I
Chester A. Rembleske
Beech Aircraft Corporation
DOA CE-2
FAA Approved
Revised: October, 1978
P/N 55-590000-51
BEECHCRAFT BARON LANDPLANES
PILOT'S OPERATING HANDBOOK
AND FAA APPROVED
AIRPLANE FLIGHT MANUAL SUPPLEMENT
FOR THE
AUXILIARY FUEL TANK ANNUNCIATOR LIGHT
(BEECH KIT NO. 96-9001-1)
PILOT'S OPERA TING HANDBOOKS AFFECTED:
Baron 95-55195-A55
(TC-1 thru TC-501 except TC-350 and TC-371)
. . . . . . . . . . . . . . . . . . . . . . . . . PIN 55-590000-65
Baron 95-855195-B55A
(TC-371 and TC-502 thru TC-1607)
. . . . . . . . . . . . . . . . . . . . . . . . . . PIN 96-590011-25
Baron 95-C55195-C55A, D551D55A. E55lE55A
(TC-350 and TE-1 thru TE-942 except TE-938)
. . . . . . . . . . . . . . . . . . . . . . . . . PIN 96-590010-29
Airplane Serial Number:
Airplane Registration Number:
DOA CE-2
FAA Approved
Issued: November, 1993
P/N 96-590000-1
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CONTENTS
GENERAL . . . . . . . . . . . . . . . . . . . . . . . . . .Page 2
LIMITATIONS . . . . . . . . . . . . . . . . . . . . . . . .Page 3
EMERGENCY PROCEDURES . . . . . . . . . . . . .Page 3
NORMAL PROCEDURES . . . . . . . . . . . . . . . .Page 4
PERFORMANCE . . . . . . . . . . . . . . . . . . . . . .Page 4
WEIGHT & BALANCE . . . . . . . . . . . . . . . . . .Page 4
SYSTEMS DESCRIPTION . . . . . . . . . . . . . . .Page 5
HANDLING, SERVICING, AND
MAINTENANCE . . . . . . . . . . . . . . . . . .Page 5
GENERAL
This document must be attached to the Pilot's Operating
Handbook and FAA Approved Airplane Flight Manual
when the airplane has been modified by the installation of
the Auxiliary Fuel Tank Annunciator Light in accordance
with Beech Kit 96-9001-1.
The information in this supplement supersedes or adds to
the basic Pilot's Operating Handbook and FAA Approved
Airplane Flight Manual only as set forth within this document. Users of this manual are advised always to refer to
the supplement for possibly superseding information and
placarding applicable to the operation of the airplane.
FAA Approved
Issued: November, 1993
P/N 96-590000-1
LIMITATIONS
PLACARDS
On instrument Panel:
ANNUNCIATOR
LIGHT
I
WARNING
TAKEOFF AND LANDING PROHIBITED
EMERGENCY PROCEDURES
No Change.
FAA Approved
Issued: November, 1993
P/N 96-590000-1
NORMAL PROCEDURES
BEFORE STARTING
-
Battery Switch and Generator Switches- ON (If
external power is used, Generator Switches 0FF)
-
Fuel Selector Valves - CHECK OPERATION.
THEN SET TO MAIN TANKS
Left Aux Tank Selected - AUX TANK SELECTED annunciator light CHECK ILLUMINATED
Left Main Tank Selected - AUX TANK SELECTED annunciator light CHECK EXTINGUISHED
Right Aux Tank Selected - AUX TANK SELECTED annunciator light CHECK ILLUMINATED
Right Main Tank Selected - AUX TANK
SELECTED annunciator light CHECK U(TlNGUlSHED
PERFORMANCE
No Change.
WEIGHT & BALANCE
No Change.
FAA Approved
Issued: November, 1993
P/N 96-590000-1
SYSTEMS DESCRIPTION
FUEL SYSTEM
AUXILIARY FUEL TANK ANNUNCIATOR LIGHT
When BEECH Kit 96-9001-1 is installed, a red auxiliary
fuel tank annunciator light will illuminate if either one of
the auxiliary fuel tanks is selected when the landing gear
is extended. Auxiliary fuel tanks are to be used during level flight only and not during takeoff or landing.
HANDLING, SERVICING, AND MAINTENANCE
No Change.
FAA Approved
Issued: November, 1993
P/N 96-590000-1