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On airplanes 5301 to 5386 not incorporating SB
604−24−002:
• FMS 1
• Copilot’s PFD, MFD, navigation & communication systems
• R Pack
• Right probe heaters, AOA vane heater and ice detector
• Nose wheel steering system, anti-skid system
• Both windshield heaters, right window heater
• Copilot’s instrument lights, NAV lights, and L & R landing
lights
• SPS altitude compensation
At 10,000 feet MSL or lowest safe altitude:
(18) RAM-AIR ........................................................................... OPEN
(19) GPWS/FLAP OVRD (if installed)....................................... OVRD
(20) Approach start point .................................................ESTABLISH
at 5,000 feet AGL over landing area.
EMER 1-9
REV 76, Jul 17/09
▼
QUICK REFERENCE HANDBOOK
PSP 604-15
POWER PLANT
EMERGENCIES
Double Engine Failure (Cont’d)
(21) Turn (20° to 30° bank angle) ............................................START
over landing area.
(22) Target airspeed .......................................................... MAINTAIN
(23) Downwind leg ...........................................................ESTABLISH
at 2,500 feet AGL abeam landing area
and 180° from final approach heading.
(24) Landing flaps (if available)...................................................... 20°
(25) LDG GEAR............................................................................. DN
(26) Final approach..........................................................ESTABLISH
at 1,500 feet AGL.
(27) Final approach speed.............................................VREF + ΔVREF
for applicable flap setting.
(28) Actual landing distance ............................................. INCREASE
as applicable by factor given below:
Flaps
Setting
(Degrees)
Δ VREF
(KTS)
ALD Factor
APU generator
available
Emergency
power only
0 30 1.80 (80%) 3.60 (260%)
20 14 1.55 (55%) 3.20 (220%)
When time and conditions permit:
(29) Ditching and Forced Landing ........................................ REVIEW
(See Page EMER 7–2)
END
EMER 1-10
REV 76, Jul 17/09
QUICK REFERENCE HANDBOOK
PSP 604-15
POWER PLANT
EMERGENCIES
L (R) JETPIPE OVHT
L JETPIPE OVHT
or
R JETPIPE OVHT
“JETPIPE OVERHEAT”
(1) Affected thrust lever .............................CONFIRM and RETARD
slowly until message goes out.
L (R) JETPIPE OVHT message persists:
Yes
(2) In-Flight Engine
Failure/Shutdown..........................................ACCOMPLISH
(See Page ABNORM 1–2)
− END −
No
(2) No further action required.
END
Post-Shutdown Engine Tail Pipe Fire
........ Engine ITT exceeds 350°C and ITT is rising rapidly, or
........ Flame is reported at engine tail pipe.
Affected engine:
(1) Dry motor..............................................................ACCOMPLISH
until ITT is reduced below 150°C or starter limit.
NOTE
The APU or ground air source (if available) may be used to
dry motor the engine.
Tail pipe fire indications persist:
Yes
(2) ENG FIRE...................................................................PUSH
(3) Passenger Evacuation
Procedure ....................................................AS REQUIRED
(See Page EMER 8–2)
(4) Control tower .............................. INFORM OF CONDITION
and request fire-fighting assistance.
− END −
No
(2) No further action required.
END
EMER 1-11
REV 76, Jul 17/09
QUICK REFERENCE HANDBOOK
PSP 604-15
POWER PLANT
EMERGENCIES
L (R) REV UNLOCKED
L REV UNLOCKED
or
R REV UNLOCKED
Affected engine:
(1) Thrust lever .................................................CONFIRM and IDLE
(2) L (R) THRUST REVERSER .................................. EMER STOW
L (R) REV UNLOCKED caution message will remain on.
(3) Airspeed ....................................................................... 200 KIAS
maximum.
Anti-ice is on:
Yes
(4) WING ANTI-ICE ........................................................... OFF
(5) Affected COWL ANTI-ICE ............................................ OFF
No
Thrust reverser fails to stow:
Yes
Thrust lever locked at idle, and continued airplane buffet
and yaw:
(4) In-Flight Engine
Failure/Shutdown..........................................ACCOMPLISH
　
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