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ABNORM CONTENTS-3
REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15 ABNORMAL PROCEDURES
ABNORM CONTENTS-4
REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15 ABNORMAL PROCEDURES
THIS PAGE INTENTIONALLY LEFT BLANK
CONTENTS PAGE
ENGINE FAILURE PROCEDURES
• In-Flight Engine Failure/Shutdown............................ABNORM 1−2
• Cross Bleed Relight/Starter Assisted........................ABNORM 1−3
• Windmill Relight ........................................................ABNORM 1−5
• Single Engine............................................................ABNORM 1−7
THRUST REVERSER FAILURES
• L (R) REV UNSAFE .................................................ABNORM 1−8
ENGINE CONTROL FAILURES
• Thrust Lever Inoperative ...........................................ABNORM 1−8
• APR INOP ................................................................ABNORM 1−9
• APR CMD SET .........................................................ABNORM 1−9
• Uncommanded Deceleration or Abnormal
Engine Oscillation/Fluctuation.................................ABNORM 1−10
OTHER FAULTS
• N1 Fan Vibration......................................................ABNORM 1−11
• N2 Core Vibration ....................................................ABNORM 1−13
• L (R) ENG MISCOMP ............................................ABNORM 1−14
• High Oil Temperature..............................................ABNORM 1−14
• Fluctuating Oil Pressure..........................................ABNORM 1−15
• Hot Start ..................................................................ABNORM 1−16
• Interrupted Start ......................................................ABNORM 1−16
• No Lightoff...............................................................ABNORM 1−16
• Low Idling ................................................................ABNORM 1−16
• N2 Stagnation..........................................................ABNORM 1−17
NOTE
1. During single engine operations, APU-assisted air
start is not always possible. Priority is given to a
cross bleed start (i.e., highest bleed air pressure).
2. Use air turbine starter whenever possible.
ABNORM 1-1
REV 75, Feb 17/09
QUICK REFERENCE HANDBOOK
PSP 604-15
POWER PLANT
MALFUNCTIONS
In-Flight Engine Failure/Shutdown
Accomplish an engine shutdown only when flight conditions
permit.
(1) Affected engine, thrust lever........................CONFIRM and IDLE
(2) Affected engine, thrust lever..............CONFIRM and SHUT OFF
(3) TAIL TANK TRANSFER,
MANUAL OVRD................................................................... OFF
Anti-ice system is on:
Yes
(4) 14TH STAGE ISOL ................................................... OPEN
(5) Affected COWL ANTI-ICE ............................................ OFF
No
HYD 1 (2) HI TEMP caution message is out:
Yes
(4) Applicable HYDRAULIC pump ....................................... ON
If left engine shut down, turn 1B ON.
If right engine shut down, turn 2B ON.
No
(4) Affected PACK ..................................................................... OFF
(5) Affected 10TH STAGE bleed ........................................CLOSED
(6) Affected GEN ....................................................................... OFF
(7) APU (if available)..............................................................START
when at or below 20,000 feet.
On airplanes 5301 to 5630 without SB 604–49–006 or
604–49–009:
(7) APU (if available)..........................................................START
when at or below 15,000 feet.
On airplanes 5301 to 5630 without SB 604–49–006 or
604–49–009:
CAUTION
Use of the APU generator in flight
is not permitted unless both main
generators have failed or are
off-line.
(8) APU GEN ............................................................................... ON
(9) Fuel system .....................................................................CHECK
and monitor fuel quantity and balance.
ABNORM 1-2
REV 71, Oct 31/07
▼
QUICK REFERENCE HANDBOOK
PSP 604-15
POWER PLANT
MALFUNCTIONS
In-Flight Engine Failure/Shutdown (Cont’d)
(10) Leave icing conditions.
NOTE
Icing conditions exist in flight at a TAT of 10°C (50°F) or
below, and visible moisture in any form is encountered
　
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