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(8) L and R BOOST PUMPs ...................................................... OFF
(9) APU (if not essential).............................................. SHUTDOWN
At 500 feet (Radio Altitude):
(10) PA.....................................................................................ALERT
Forced landing imminent.
(11) Radio ......................................................................... TRANSMIT
final position.
(12) BRACE FOR IMPACT.....................................................ORDER
“BRACE – BRACE – BRACE”.
(13) EMER LTS ............................................................................. ON
(14) LANDING LTS........................................................................ ON
JUST BEFORE CONTACT
(1) Thrust levers...............................................................SHUT OFF
EMER 7-5
REV 66, Feb 01/07
▼
QUICK REFERENCE HANDBOOK
PSP 604-15 DITCHING
Forced Landing (Cont’d)
(2) APU, LH and RH ENG FIRE ..............................................PUSH
(3) Terrain ........................................................................ CONTACT
with minimum forward speed, but not less than stick shaker
speed, and at minimum sink rate.
AFTER CONTACT
When the airplane has stopped:
(1) ENG and APU fire bottles....................................... DISCHARGE
(2) Door and overwing exit...................................................... OPEN
(3) Evacuation.....................................................................INITIATE
(4) BATT MASTER .................................................................... OFF
to prevent CVR erasure.
(5) Airplane ......................................................................ABANDON
with survival equipment.
END
EMER 7-6
REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15 DITCHING
CONTENTS PAGE
• Passenger Evacuation ................................................... EMER 8−2
EMER 8-1
REV 66, Feb 01/07
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PSP 604-15 EMERGENCY EVACUATION
Passenger Evacuation
Procedure initiated for a condition potentially endangering life or
physical well being of passengers and crew.
Pilot:
(1) PARKING BRAKE .................................................................SET
(2) EVACUATION...........................................................COMMAND
(3) GND SPOILERS ............................................................DISARM
(4) FLIGHT SPOILER lever ..............................................RETRACT
(5) Thrust levers...............................................................SHUT OFF
(6) Evacuation.....................................................................INITIATE
using PA system.
(7) APU, LH and RH ENG FIRE ..............................................PUSH
(8) BATT MASTER .................................................................... OFF
to prevent CVR erasure.
Copilot: On EVACUATION command
(9) ATC ................................................................................ NOTIFY
of condition and intention to evacuate.
(10) PACKs.................................................................................. OFF
(11) EMER DEPRESS................................................................... ON
(12) Exits................................................................................... OPEN
(13) Passenger evacuation.....................................................ASSIST
and direct passengers away from airplane.
(14) Airplane ......................................................................ABANDON
by any suitable exit.
END
EMER 8-2
REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15 EMERGENCY EVACUATION
CONTENTS PAGE
• EMER PWR ONLY ........................................................ EMER 9−2
EMER 9-1
REV 66, Feb 01/07
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PSP 604-15 ELECTRICAL EMERGENCY
EMER PWR ONLY
EMER PWR ONLY
(1) ADG manual deploy handle ................................................PULL
for at least 1 second, then stow.
(2) AC ESS BUS............................................... CHECK POWERED
When ADG power is established:
(3) STAB TRIM .........................................................ENGAGE CH 2
(4) Engine Instruments .........................................................VERIFY
N1, N2, & ITT.
Both engines confirmed failed:
Yes
(5) Double Engine Failure
Procedure .....................................................ACCOMPLISH
(See Page EMER 1–4)
− END −
　
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