IN-- FLIGHT CHECKS
Table of Contents
Vol. 2
IN-- FLIGHT CHECKS
Table of Contents
09--00--1
REV 56, Jan 31/03
CHAPTER 9 - IN-FLIGHT CHECKS
CHAPTER 9 - IN-FLIGHT CHECKS
TABLE OF CONTENTS
TABLE OF CONTENTS
09--00--1
Vol. 2
REV 56, Jan 31/03
Page
TABLE OF CONTENTS
09 -- 00 -- 1
TABLE OF CONTENTS
09 -- 00 -- 1
09 -- 01 -- 1
AIR - DRIVEN GENERATOR CHECKS
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INTRODUCTION
General
General
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INTRODUCTION
Page
09 -- 01 -- 1
AIR - DRIVEN GENERATOR CHECKS
09 -- 02 -- 1
General
09 -- 02 -- 1
Manual Deployment Operational Check
Before Flight
After Starting Engines (Before Test Flight)
In-Flight Procedures
09 -- 02 -- 1
09---02---1
09---02---2
09---02---3
Manual Deployment Operational Check
Before Flight
After Starting Engines (Before Test Flight)
In-Flight Procedures
09 -- 02 -- 1
09---02---1
09---02---2
09---02---3
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General
Flight Crew Operating Manual
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Flight Crew Operating Manual
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Vol. 2
IN--FLIGHT CHECKS
Table of Contents
09--00--2
REV 56, Jan 31/03
Vol. 2
09--00--2
REV 56, Jan 31/03
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IN-- FLIGHT CHECKS
Table of Contents
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Flight Crew Operating Manual
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IN-- FLIGHT CHECKS
Introduction
IN-- FLIGHT CHECKS
Introduction
09--01--1
REV 56, Jan 31/03
GENERAL
1.
REV 56, Jan 31/03
GENERAL
In-flight checks are special operating procedures not routinely performed every flight and are
accomplished when certain airplane systems are to be tested for proper operation in flight.
The following recommended procedures must be adhered to, in order to ensure the safe
conduct of the functional test to be performed.
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In-flight checks are special operating procedures not routinely performed every flight and are
accomplished when certain airplane systems are to be tested for proper operation in flight.
The following recommended procedures must be adhered to, in order to ensure the safe
conduct of the functional test to be performed.
09--01--1
Vol. 2
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1.
Vol. 2
Flight Crew Operating Manual
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Flight Crew Operating Manual
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Vol. 2
IN--FLIGHT CHECKS
Introduction
09--01--2
REV 56, Jan 31/03
Vol. 2
09--01--2
REV 56, Jan 31/03
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IN-- FLIGHT CHECKS
Introduction
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Flight Crew Operating Manual
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IN-- FLIGHT CHECKS
Air--Driven Generator Checks
Vol. 2
IN-- FLIGHT CHECKS
Air--Driven Generator Checks
09--02--1
REV 58, Oct 31/05
09--02--1
Vol. 2
REV 58, Oct 31/05
GENERAL
The following procedures are recommended to operationally check the air-driven generator (ADG)
in flight using the manual deployment system.
The following procedures are recommended to operationally check the air-driven generator (ADG)
in flight using the manual deployment system.
The ADG check shall be carried out in Visual Meteorological Conditions (VMC). Ensure that the ADG
check is not carried out in icing conditions.
The ADG check shall be carried out in Visual Meteorological Conditions (VMC). Ensure that the ADG
check is not carried out in icing conditions.
CAUTION
CAUTION
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1. The presence of foreign objects in the ADG bay could
cause damage to the ADG blades during deployment.
Before flight, the ADG bay must be inspected to ensure
that foreign objects are not present.
1. The presence of foreign objects in the ADG bay could
cause damage to the ADG blades during deployment.
Before flight, the ADG bay must be inspected to ensure
that foreign objects are not present.
Airplanes 7002 through 7304:
Airplanes 7002 through 7304:
2. When deployed, the ADG is maintained in position by
an ejection spring and airloads. After landing, high
deceleration could cause the ADG to swing forward
with resulting damage to the ADG blades and adjacent
fuselage panels. When landing with the ADG deployed,
plan to use maximum landing roll-out available to
minimize deceleration.
2. When deployed, the ADG is maintained in position by
an ejection spring and airloads. After landing, high
deceleration could cause the ADG to swing forward
with resulting damage to the ADG blades and adjacent
fuselage panels. When landing with the ADG deployed,
plan to use maximum landing roll-out available to
minimize deceleration.
NOTE
NOTE
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1. Once deployed, the ADG cannot be stowed during
flight. Therefore, this check should be performed at the
end of a test flight. Normal electrical power must be
restored before final landing approach is commenced.
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2. If icing conditions are encountered while the ADG is the
only source of electrical power, the WING anti-ice
system must be operated only in the standby (STBY)
mode.
MANUAL DEPLOYMENT OPERATIONAL CHECK
2. If icing conditions are encountered while the ADG is the
only source of electrical power, the WING anti-ice
system must be operated only in the standby (STBY)
mode.
Before Flight:
ADG bay . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check
(1)
S Clear of foreign objects.
(2)
1. Once deployed, the ADG cannot be stowed during
flight. Therefore, this check should be performed at the
end of a test flight. Normal electrical power must be
restored before final landing approach is commenced.
MANUAL DEPLOYMENT OPERATIONAL CHECK
Before Flight:
(1)
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GENERAL
Aft electrical bay . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check
(2)
S Verify that ADG AUTO and MAN circuit breakers (5B10 and 5B11) are
Aft electrical bay . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check
S Verify that ADG AUTO and MAN circuit breakers (5B10 and 5B11) are
closed.
Flight Crew Operating Manual
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ADG bay . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check
S Clear of foreign objects.
closed.
MASTER
Flight Crew Operating Manual
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MASTER
IN-- FLIGHT CHECKS
Air--Driven Generator Checks
Vol. 2
IN--FLIGHT CHECKS
Air--Driven Generator Checks
09--02--2
REV 57, Apr 05/04
Vol. 2
09--02--2
REV 57, Apr 05/04
After Starting Engines (Before Test Flight):
After Starting Engines (Before Test Flight):
Effectivity:
S Airplanes 7003 through 7027 not incorporating Canadair Service Bulletin:
S Airplanes 7003 through 7027 not incorporating Canadair Service Bulletin:
S SB 601R--24--010, Electrical Power, Air Driven Generator (ADG) --
S SB 601R--24--010, Electrical Power, Air Driven Generator (ADG) --
to UNIT.
Check the following:
(1) Centre pedestal, ADG AUTO DEPLOY
CONTROL switch . . . . . . . . . . . . . . . . . . . . . . Select
S TEST light ON for
S TEST light ON for
2 seconds then out.
After Starting Engines (Before Test Flight):
to UNIT.
Check the following:
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(1) Centre pedestal, ADG AUTO DEPLOY
CONTROL switch . . . . . . . . . . . . . . . . . . . . . . Select
Installation of a New Generator Control Unit (GCU).
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Installation of a New Generator Control Unit (GCU).
Effectivity:
2 seconds then out.
After Starting Engines (Before Test Flight):
Effectivity:
Effectivity:
S Airplanes 7003 through 7027 not incorporating Canadair Service Bulletin:
S Airplanes 7003 through 7027 not incorporating Canadair Service Bulletin:
S SB 601R--24--010, Electrical Power, Air Driven Generator (ADG) --
S SB 601R--24--010, Electrical Power, Air Driven Generator (ADG) --
S Airplanes 7125 and subsequent; and
S Airplanes 7125 and subsequent; and
S Airplanes 7003 through 7124 incorporating Canadair Service Bulletin:
S Airplanes 7003 through 7124 incorporating Canadair Service Bulletin:
S SB 601R--24--054, Electrical Power, Air Driven Generator (ADG) --
S SB 601R--24--054, Electrical Power, Air Driven Generator (ADG) --
Installation of a New Generator Control Unit (GCU); and
(1) Centre pedestal, ADG AUTO DEPLOY
CONTROL switch . . . . . . . . . . . . . . . . . . . . . . Select
to UNIT.
Check the following:
S TEST light ON after a time
delay of 1 second and
remains on for 1 second.
Flight Crew Operating Manual
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MASTER
Installation of a Time Delay Circuit to Prevent ADG Overvoltage During ADG
Deployment.
(1) Centre pedestal, ADG AUTO DEPLOY
CONTROL switch . . . . . . . . . . . . . . . . . . . . . . Select
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Installation of a Time Delay Circuit to Prevent ADG Overvoltage During ADG
Deployment.
to UNIT.
Check the following:
S TEST light ON after a time
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Installation of a New Generator Control Unit (GCU); and
delay of 1 second and
remains on for 1 second.
Flight Crew Operating Manual
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MASTER
IN-- FLIGHT CHECKS
Air--Driven Generator Checks
IN-- FLIGHT CHECKS
Air--Driven Generator Checks
09--02--3
Vol. 2
REV 58, Oct 31/05
In-Flight Procedures:
BATTERY MASTER . . . . . . . . . . . . . . . . . . . . . . . . . Check ON
(1)
BATTERY MASTER . . . . . . . . . . . . . . . . . . . . . . . . . Check ON
(2)
APU . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Start
(2)
APU . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Start
(3)
APU GEN . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
(3)
APU GEN . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
(4)
VHF Comm, VHF Nav, ADF and transponder . . Set to no. 1
(4)
VHF Comm, VHF Nav, ADF and transponder . . Set to no. 1
NOTE
The no. 2 VHF Comm, VHF Nav, ADF and transponder
become inoperative when the main generators (GEN 1
and GEN 2) are turned off in the steps to follow.
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NOTE
The no. 2 VHF Comm, VHF Nav, ADF and transponder
become inoperative when the main generators (GEN 1
and GEN 2) are turned off in the steps to follow.
(5)
HYDRAULIC, 1 and 2 switches . . . . . . . . . . . . . . . . . . . . . . . ON
(5)
HYDRAULIC, 1 and 2 switches . . . . . . . . . . . . . . . . . . . . . . . ON
(6)
Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . Maintain 180 KIAS
(6)
Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . Maintain 180 KIAS
(7)
Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Set to 20_
(7)
Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Set to 20_
(8)
Altitude . . . . . . . . . . . . . . . . . . . . Maintain 10,000 feet or below
(8)
Altitude . . . . . . . . . . . . . . . . . . . . Maintain 10,000 feet or below
(9)
ADG DEPLOY CONT - AUTO
circuit breaker (2N6) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Open
(9)
ADG DEPLOY CONT - AUTO
circuit breaker (2N6) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Open
(10)
LDG GEAR lever . . . . . . . . . . . . . . . . . . . . . . . . . . Select to DN
(10)
LDG GEAR lever . . . . . . . . . . . . . . . . . . . . . . . . . . Select to DN
(11)
HYDRAULIC, 3A and 3B switches . . . . . . . . . . . . . . . . . . . OFF
S Bleed off No. 3 system pressure and check that HYD 3 LO PRESS caution
message comes on.
(11)
AC ELECTRICAL synoptic page . . . . . . . . . . . . . . . . . . . Select
(12)
HYDRAULIC, 3A and 3B switches . . . . . . . . . . . . . . . . . . . OFF
S Bleed off No. 3 system pressure and check that HYD 3 LO PRESS caution
message comes on.
NOTE
Do not push the PWR TXFR OVERRIDE switch prior to
manual deployment. This could prevent the ADG from
coming on line if the handle is stowed.
AC ELECTRICAL synoptic page . . . . . . . . . . . . . . . . . . . Select
NOTE
Do not push the PWR TXFR OVERRIDE switch prior to
manual deployment. This could prevent the ADG from
coming on line if the handle is stowed.
ADG manual deploy handle . . . . Pull for 1 second then stow,
then pull the handle again.
(13)
S Pulling the handle for one (1) second ensures proper opening of the uplock.
S Pulling the handle for one (1) second ensures proper opening of the uplock.
Effectivity:
Fo
Effectivity:
ADG manual deploy handle . . . . Pull for 1 second then stow,
then pull the handle again.
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(13)
REV 58, Oct 31/05
In-Flight Procedures:
(1)
(12)
09--02--3
Vol. 2
S Airplanes 7125 and subsequent; and
S Airplanes 7003 through 7124 incorporating Canadair Service Bulletin:
S SB 601R--24--054, Electrical Power, Air Driven Generator (ADG) --
Installation of a Time Delay Circuit to Prevent ADG Overvoltage During ADG
Deployment.
(13) ADG manual deploy handle . . . . . . . . . . . . . . . . . . . . . . . . Pull
Flight Crew Operating Manual
CSP A-- 013
S Airplanes 7125 and subsequent; and
S Airplanes 7003 through 7124 incorporating Canadair Service Bulletin:
S SB 601R--24--054, Electrical Power, Air Driven Generator (ADG) --
Installation of a Time Delay Circuit to Prevent ADG Overvoltage During ADG
Deployment.
(13) ADG manual deploy handle . . . . . . . . . . . . . . . . . . . . . . . . Pull
MASTER
Flight Crew Operating Manual
CSP A-- 013
MASTER
IN-- FLIGHT CHECKS
Air--Driven Generator Checks
Vol. 2
Vol. 2
09--02--4
REV 58, Oct 31/05
Airplanes 7002 through 7304:
AC ELECTRICAL synoptic page . . . . . . . . . . . . . . . . . . Check
(14)
S Verify that within six (6) seconds, the following indications occur:
S ADG voltage . . . . . . . . . . . . . . . . . . . . . . . . . . 115 ± 5 V AC
S Frequency . . . . . . . . . . . . . . . . . . . . . . . . . . . . 380 -- 420 Hz
S AC ESS BUS . . . . . . . . . . . . . . . . . . . . . . . . . Powered
S AC essential bus temporarily not powered (AC ESS BUS
AC ELECTRICAL synoptic page . . . . . . . . . . . . . . . . . . Check
S Verify that within six (6) seconds, the following indications occur:
S ADG voltage . . . . . . . . . . . . . . . . . . . . . . . . . . 115 ± 5 V AC
S Frequency . . . . . . . . . . . . . . . . . . . . . . . . . . . . 380 -- 420 Hz
S AC ESS BUS . . . . . . . . . . . . . . . . . . . . . . . . . Powered
S AC essential bus temporarily not powered (AC ESS BUS
caution message on EICAS comes on briefly, then out).
Airplanes 7305 and subsequent:
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caution message on EICAS comes on briefly, then out).
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Airplanes 7002 through 7304:
(14)
IN--FLIGHT CHECKS
Air--Driven Generator Checks
09--02--4
REV 58, Oct 31/05
Airplanes 7305 and subsequent:
(14) AC ELECTRICAL synoptic page . . . . . . . . . . . . . . . . . . . Check
S Verify that within six (6) seconds, the following indications occur:
(14) AC ELECTRICAL synoptic page . . . . . . . . . . . . . . . . . . . Check
S Verify that within six (6) seconds, the following indications occur:
S ADG voltage . . . . . . . . . . . . . . . . . . . . . . . . . . 115 ± 5 V AC
S Frequency . . . . . . . . . . . . . . . . . . . . . . . . . . . . 400 ± 40 Hz
S AC ESS BUS . . . . . . . . . . . . . . . . . . . . . . . . . Powered
S AC essential bus temporarily not powered (AC ESS BUS
S ADG voltage . . . . . . . . . . . . . . . . . . . . . . . . . . 115 ± 5 V AC
S Frequency . . . . . . . . . . . . . . . . . . . . . . . . . . . . 400 ± 40 Hz
S AC ESS BUS . . . . . . . . . . . . . . . . . . . . . . . . . Powered
S AC essential bus temporarily not powered (AC ESS BUS
caution message on EICAS comes on briefly, then out).
caution message on EICAS comes on briefly, then out).
S ADG output flow line (between the ADG parameter box and AC ESS BUS) on
EICAS turns green (AC ESS BUS powered by ADG).
Pending rectification:
S ADG output flow line (between the ADG parameter box and AC ESS BUS) on
EICAS turns green (AC ESS BUS powered by ADG).
Pending rectification:
NOTE
NOTE
The AC ESS BUS remains available, however AC ESS
BUS caution messages may be displayed
intermittently.
Fo
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The AC ESS BUS remains available, however AC ESS
BUS caution messages may be displayed
intermittently.
Flight Crew Operating Manual
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Flight Crew Operating Manual
CSP A-- 013
MASTER
IN-- FLIGHT CHECKS
Air--Driven Generator Checks
09--02--5
REV 58, Oct 31/05
DC ELECTRICAL synoptic page . . . . . . . . . . . . . . . . . . Check
(15)
(16)
S Verify the following indications:
S ESS TRU 1, DC ESS BUS
S ESS TRU 1, DC ESS BUS
and BATT BUS . . . . . . . . . . . . . . . . . . . . . . . . Powered
HYDRAULIC synoptic page . . . . . . . . . . . . . . . . . . . . . . . Check
(16)
S Verify that hydraulic system No. 3 pressure shows 3,000 ± 200 psi.
(17)
GEN 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
(17)
GEN 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
(18)
Primary display . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check
(19)
WARNING
If the ADG fails to deliver the required electrical power
after the GEN 1 and GEN 2 switches are set to OFF, the
GEN 1 and GEN 2 switches must be reset immediately
to ON and normal supply to the essential busses
restored by pressing the PWR TXFR OVERRIDE switch,
after confirming that the ADG manual deploy handle is
stowed.
If the ADG fails to deliver the required electrical power
after the GEN 1 and GEN 2 switches are set to OFF, the
GEN 1 and GEN 2 switches must be reset immediately
to ON and normal supply to the essential busses
restored by pressing the PWR TXFR OVERRIDE switch,
after confirming that the ADG manual deploy handle is
stowed.
NOTE
NOTE
Pilot’s, copilot’s and
third crewmember’s intercoms . . . . . . . . . . . . . . . . . . . . Check
Fo
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The 10th stage bleed air shutoff valves close when
power is removed from DC bus 1 and DC bus 2. Normal
control of the cabin pressurization system is therefore
lost and cabin altitude slowly increases.
STAB TRIM, CH 2 switch/light . . . . . . . . . . . . Check engaged
(21)
(20)
S STAB TRIM CH 1 INOP status message on.
(22)
Primary display . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Check
S Verify that EMER PWR ONLY warning message comes on,
S MACH TRIM caution message comes on, and
S All other indications are normal, except VIB=0.0 .
WARNING
(21)
GEN 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
S Check that GEN 2 OFF caution message comes on.
S Verify that EMER PWR ONLY warning message comes on,
S MACH TRIM caution message comes on, and
S All other indications are normal, except VIB=0.0 .
(20)
GEN 1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
S Check that GEN 1 OFF caution message comes on.
S Check that GEN 2 OFF caution message comes on.
(19)
HYDRAULIC synoptic page . . . . . . . . . . . . . . . . . . . . . . . Check
S Verify that hydraulic system No. 3 pressure shows 3,000 ± 200 psi.
S Check that GEN 1 OFF caution message comes on.
(18)
The 10th stage bleed air shutoff valves close when
power is removed from DC bus 1 and DC bus 2. Normal
control of the cabin pressurization system is therefore
lost and cabin altitude slowly increases.
Pilot’s, copilot’s and
third crewmember’s intercoms . . . . . . . . . . . . . . . . . . . . Check
STAB TRIM, CH 2 switch/light . . . . . . . . . . . . Check engaged
S STAB TRIM CH 1 INOP status message on.
YAW DAMPER, YD 1 switch/light . . . . . . . . . Check engaged
(22)
S YD 1 INOP status message out.
Flight Crew Operating Manual
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REV 58, Oct 31/05
DC ELECTRICAL synoptic page . . . . . . . . . . . . . . . . . . Check
S Verify the following indications:
and BATT BUS . . . . . . . . . . . . . . . . . . . . . . . . Powered
09--02--5
Vol. 2
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(15)
Vol. 2
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IN-- FLIGHT CHECKS
Air--Driven Generator Checks
YAW DAMPER, YD 1 switch/light . . . . . . . . . Check engaged
S YD 1 INOP status message out.
MASTER
Flight Crew Operating Manual
CSP A-- 013
MASTER
(23)
Vol. 2
IN--FLIGHT CHECKS
Air--Driven Generator Checks
09--02--6
REV 58, Oct 31/05
Pitch trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Operate
(23)
S To check that stabilizer trim operates normally.
(24)
09--02--6
REV 58, Oct 31/05
Pitch trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Operate
S To check that stabilizer trim operates normally.
AC and DC essential busses . . . . . . . . . . . . . . . . . . . . . . Check
(24)
S Verify that power is available on each bus. It is sufficient to confirm the
AC and DC essential busses . . . . . . . . . . . . . . . . . . . . . . Check
S Verify that power is available on each bus. It is sufficient to confirm the
normal operation of one of the services powered by the bus. The following is
a list of the essential busses and the services appropriate for this check:
normal operation of one of the services powered by the bus. The following is
a list of the essential busses and the services appropriate for this check:
DC Essential Bus:
S VHF Nav 1 operational,
DC Essential Bus:
S VHF Nav 1 operational,
S ADF 1 operational,
S Transponder 1 operational,
S Transponder 1 operational,
S Pilot’s MFD and PFD with complete displays,
S Pilot’s MFD and PFD with complete displays,
S Wing anti-ice, STBY (Check for ITT variation).
S Wing anti-ice, STBY (Check for ITT variation).
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S ADF 1 operational,
AC Essential Bus:
S ICE DET 1 FAIL status message out.
AC Essential Bus:
S ICE DET 1 FAIL status message out.
S ICE DET TEST: . . . . . . . . . . Press switch/light to test and verify that
S ICE DET TEST: . . . . . . . . . . Press switch/light to test and verify that
L AOA, L & STBY PITOT, L STATIC and L WINDOW HEAT
caution messages out; then
LH WSHLD switch . . . . . . . . RESET.
L AOA, L & STBY PITOT, L STATIC and L WINDOW HEAT
caution messages out; then
LH WSHLD switch . . . . . . . . RESET.
NOTE
L AOA HEAT, PITOT BASE HEAT, L PITOT HEAT and
STBY PITOT HEAT caution messages may come on
during ADG deployment. If this occurs, reset circuit
breaker 4A7.
NOTE
L AOA HEAT, PITOT BASE HEAT, L PITOT HEAT and
STBY PITOT HEAT caution messages may come on
during ADG deployment. If this occurs, reset circuit
breaker 4A7.
Battery Bus:
S RAM AIR SOV operational,
re
Battery Bus:
S RAM AIR SOV operational,
S Pilot’s clock operational,
Fo
S Pilot’s clock operational,
S Standby attitude indicator and altimeter/indicated airspeed
S Standby attitude indicator and altimeter/indicated airspeed
indicators operational,
indicators operational,
S INTEG instruments panel lights operational.
S INTEG instruments panel lights operational.
(25)
Hydraulic system No. 3 pressure . Monitor on synoptic page
(25)
(26)
LDG gear lever . . . . . . . . . . . . . . . . . . . . . . . Cycle UP then DN
(26)
S Check that hydraulic system No. 3 pressure does not go below 2,000 psi.
Flight Crew Operating Manual
CSP A-- 013
Vol. 2
ly
IN-- FLIGHT CHECKS
Air--Driven Generator Checks
MASTER
Hydraulic system No. 3 pressure . Monitor on synoptic page
LDG gear lever . . . . . . . . . . . . . . . . . . . . . . . Cycle UP then DN
S Check that hydraulic system No. 3 pressure does not go below 2,000 psi.
Flight Crew Operating Manual
CSP A-- 013
MASTER
IN−FLIGHT CHECKS
Air−Driven Generator Checks
Vol. 2
IN−FLIGHT CHECKS
Air−Driven Generator Checks
09−02−7
Vol. 2
REV 58, Oct 31/05
Airplanes 7002 through 7304:
(27)
09−02−7
REV 58, Oct 31/05
Airplanes 7002 through 7304:
Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Reduce
(27)
Slow down to 150 KIAS or slowest practical safe speed and confirm
Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Reduce
Slow down to 150 KIAS or slowest practical safe speed and confirm
the ADG output:
the ADG output:
ADG voltage . . . . . . . . . . . . . . . . . . . . . . . . . . 115 5 VAC
Frequency . . . . . . . . . . . . . . . . . . . . . . . . . . . . 380 Hz minimum
Airplanes 7305 and subsequent:
Airplanes 7305 and subsequent:
Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Reduce
(27)
Slow down to 150 KIAS or slowest practical safe speed and confirm
Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Reduce
Slow down to 150 KIAS or slowest practical safe speed and confirm
the ADG output:
ADG voltage . . . . . . . . . . . . . . . . . . . . . . . . . . 115 5 VAC
ADG voltage . . . . . . . . . . . . . . . . . . . . . . . . . . 115 5 VAC
the ADG output:
Frequency . . . . . . . . . . . . . . . . . . . . . . . . . . . . 360 Hz minimum
Frequency . . . . . . . . . . . . . . . . . . . . . . . . . . . . 360 Hz minimum
Pending rectification:
Pending rectification:
NOTE
NOTE
The AC ESS BUS remains available, however AC ESS
BUS caution messages may be displayed
intermittently.
re
The AC ESS BUS remains available, however AC ESS
BUS caution messages may be displayed
intermittently.
Fo
(27)
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on
ly
ADG voltage . . . . . . . . . . . . . . . . . . . . . . . . . . 115 5 VAC
Frequency . . . . . . . . . . . . . . . . . . . . . . . . . . . . 380 Hz minimum
Flight Crew Operating Manual
CSP A−013
MASTER
Flight Crew Operating Manual
CSP A−013
MASTER
Vol. 2
IN−FLIGHT CHECKS
Air−Driven Generator Checks
09−02−8
Vol. 2
TR RJ/ 271, Jan 11/12
Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . As required
(28)
Resume normal airspeed for phase of flight, in accordance with the operating
limitations as established in Chapter 1.
(29)
limitations as established in Chapter 1.
GEN 1 and GEN 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
(29)
Check that GEN 1 OFF and GEN 2 OFF caution messages go out;
Check that EMER PWR ONLY warning message goes out.
(30)
(31)
(33)
ADG manual deploy handle . . . . . . . . . . . . . . . . . . . . . . . STOW
(30)
ADG, PWR TXFR OVERRIDE switch . . . . . . . . . . . . . . . Press
(31)
ADG manual deploy handle . . . . . . . . . . . . . . . . . . . . . . . STOW
ADG, PWR TXFR OVERRIDE switch . . . . . . . . . . . . . . . Press
To restore normal power supply.
Check that all indications return to normal.
ADG DEPLOY CONT - AUTO
circuit breaker (2N6) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Close
(32)
HYDRAULIC, 3A and 3B switches . . . . . . . . . . . . As required
(33)
The hydraulic 3A and 3B switches are normally set to ON and AUTO,
ADG DEPLOY CONT - AUTO
circuit breaker (2N6) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Close
HYDRAULIC, 3A and 3B switches . . . . . . . . . . . . As required
The hydraulic 3A and 3B switches are normally set to ON and AUTO,
respectively.
respectively.
Ground Lift Dumping system . . . . . . . . . . . . . . . . . . . . . Re-arm
(34)
GND LIFT DUMPING switch . . . . . . . . . . . . Check at AUTO
L or R engine thrust . . . . . . . . . . . . . . . . . . . . Increase momentarily
To take-off N1.
GND LIFT DUMPING switch . . . . . . . . . . . . Check at AUTO
L or R engine thrust . . . . . . . . . . . . . . . . . . . . Increase momentarily
To take-off N1.
Airplanes 7002 through 7304:
Airplanes 7002 through 7304:
CAUTION
CAUTION
On landing, with the ADG deployed, use gentle
deceleration to preclude the ADG from swinging
forward and damaging the fuselage.
re
On landing, with the ADG deployed, use gentle
deceleration to preclude the ADG from swinging
forward and damaging the fuselage.
Flight Crew Operating Manual
CSP A−013
Ground Lift Dumping system . . . . . . . . . . . . . . . . . . . . . Re-arm
Fo
(34)
GEN 1 and GEN 2 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON
Check that GEN 1 OFF and GEN 2 OFF caution messages go out;
Check that EMER PWR ONLY warning message goes out.
To restore normal power supply.
Check that all indications return to normal.
(32)
Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . As required
Resume normal airspeed for phase of flight, in accordance with the operating
du
N cat
ot io
fo na
ru lp
se ur
in spo
fli se
gh s
t
on
(28)
09−02−8
TR RJ/ 271, Jan 11/12
ly
IN−FLIGHT CHECKS
Air−Driven Generator Checks
MASTER
Flight Crew Operating Manual
CSP A−013
MASTER