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(See Page ABNORM 1–2)
CAUTION
Do not relight engine.
(5) Land at the nearest suitable airport.
Anti-ice is required:
Yes
(6) 14TH STAGE ISOL ............................................OPEN
(7) WING ANTI-ICE ................................................NORM
No
Prior to landing:
(6) Approach speed ...................................................VREF + 22
minimum.
EMER 1-12
REV 76, Jul 17/09
▼
QUICK REFERENCE HANDBOOK
PSP 604-15
POWER PLANT
EMERGENCIES
L (R) REV UNLOCKED (Cont’d)
(7) Actual landing distance...................................... INCREASE
by a factor of 1.70 (70%).
− END −
No
CAUTION
Limit airspeed to not more than 200 KIAS.
(4) Thrust levers........................................................AS REQUIRED
(5) THRUST REVERSERs ........................................................ OFF
CAUTION
Do not arm thrust reverser.
(6) Land at the nearest suitable airport.
Anti-ice is required:
Yes
(7) WING ANTI-ICE ........................................................NORM
(8) Affected COWL ANTI-ICE .............................................. ON
No
Prior to landing:
(7) GPWS/FLAP OVRD (if installed)....................................... OVRD
(8) Landing flaps .......................................................................... 20°
(9) Approach speed ...........................................................VREF + 22
minimum.
(10) Actual landing distance ............................................. INCREASE
by a factor of 1.70 (70%).
END
EMER 1-13
REV 76, Jul 17/09
QUICK REFERENCE HANDBOOK
PSP 604-15
POWER PLANT
EMERGENCIES
Engine Oil Pressure Low
L ENG OIL PRESS
or
R ENG OIL PRESS
“ENGINE OIL”
........ or left or right engine oil pressure is below 25 psi.
(1) Affected thrust lever ....................................CONFIRM and IDLE
(2) Affected engine oil pressure............................................CHECK
L (R) ENG OIL PRESS warning message is on:
Yes
Affected engine oil pressure is below 25 psi:
Yes
(3) Affected thrust lever ............................. CONFIRM and
SHUT OFF
(4) In-Flight Engine
Failure/Shutdown ................................. ACCOMPLISH
(See Page ABNORM 1–2)
− END −
No
(3) Affected thrust lever .......................................................ADJUST
as required.
(4) Engine instruments......................................................MONITOR
END
EMER 1-14
REV 76, Jul 17/09
QUICK REFERENCE HANDBOOK
PSP 604-15
POWER PLANT
EMERGENCIES
ENGINE
ENGINE
ENGINE OVERSPEED
N1 or N2 readout indicates engine limits being exceeded.
(1) Affected thrust lever .............................CONFIRM and RETARD
until engine responds.
Engine limits continue to be exceeded:
Yes
(2) In-Flight Engine
Failure/Shutdown..........................................ACCOMPLISH
(See Page ABNORM 1–2)
− END −
No
(2) Thrust levers (both) .......................................................RETARD
to below 79% N2.
(3) ENG SPEED (both) .............................................................. OFF
to prevent asymmetric thrust.
NOTE
The APR system is inoperative when the ENG SPEED
switches are selected OFF.
(4) Affected thrust lever ................................................... ADVANCE
NOTE
Thrust lever controls are more sensitive to changes.
Engine accelerates to desired power:
Yes
(5) Affected engine....................................................MONITOR
− END −
No
(5) In-Flight Engine Failure/Shutdown .......................ACCOMPLISH
(See Page ABNORM 1–2)
EMER 1-15
REV 76, Jul 17/09
▼
QUICK REFERENCE HANDBOOK
PSP 604-15
POWER PLANT
EMERGENCIES
ENGINE (Cont’d)
ENGINE OVERTEMPERATURE
ITT readout indicates engine limits being exceeded.
(1) Affected thrust lever .............................CONFIRM and RETARD
until ITT below limit range.
ITT limits continue to be exceeded:
Yes
(2) In-Flight Engine
Failure/Shutdown..........................................ACCOMPLISH
(See Page ABNORM 1–2)
− END −
No
(2) No further action required.
END
EMER 1-16
REV 76, Jul 17/09
QUICK REFERENCE HANDBOOK
PSP 604-15
POWER PLANT
EMERGENCIES
L (R) ENGINE START SOV
　
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