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时间:2010-10-11 23:27来源:蓝天飞行翻译 作者:admin
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(For airplanes SN 1000 thru 1155 with ASC 157 and airplanes
SN 1156 and subsequent.)
NOTE: As cabin altitude increases, cabin rate of climb can be
controlled by increasing available bleed pressure above 35 psi. Bleed
pressure can be increased by increasing power to maximum
continuous setting or by selecting cowl anti-ice ON at higher altitudes.
If unable to attain 35 psi or greater or if selecting cowl anti-ice ON
results in COOL TURB HOT message, descend to lower altitude until
cabin rate of climb is controllable. Select cowl anti-ice OFF if COOL
TURB HOT message persists.
9. After smoke / fumes dissipate, locate the source of the smoke /
fumes and extinguish / eliminate.
NOTE: If the source of the smoke / fumes cannot be eliminated,
consideration should be given to descending to 20,000 ft. along with
increasing cabin altitude to 20,000 ft. in attempt to starve the smoke /
fumes source. Proceed to nearest suitable airport and land if smoke /
fumes persist.
Continued on next page →
Quick Reference Handbook
REVISION 7 ABNORMAL / EMERGENCY PROCEDURES
May 30/02 Page ED - 15
Smoke In Baggage Compartment, Aft Galley, Lavatory or Right
Hand Avionics Bay, ctd… AFM 4-23-20
10. Cabin pressurization may be returned to normal by:
A. Baggage Door Handle .........RETURN TO NORMAL (CLOSED)
(For airplanes SN 1000 thru 1155 without ASC 157.)
B. Baggage Door Seal Selector Valve ....................NORMAL OPS
(For airplanes SN 1000 thru 1155 with ASC 157 and airplanes
SN 1156 and subsequent.)
END
Quick Reference Handbook
ABNORMAL / EMERGENCY PROCEDURES REVISION 7
Page ED - 16 May 30/02
Notes
Quick Reference Handbook
REVISION 7 ABNORMAL / EMERGENCY PROCEDURES
May 30/02 Page EE - 1
Flight Controls / Autoflight Index
Hydraulic System Diagram............................................................EE-2
General Guidance .......................................................................EE-3
Flight Controls Runaway To Hardover Position......................EE-3
Immovable Flight Controls.........................................................EE-3
Stall Barrier Malfunction ............................................................EE-4
Ground Spoiler Failure ...............................................................EE-4
Runaway Electric Pitch Trim .........................................................EE-5
Frozen Pitch Trim..........................................................................EE-5
Failure of Stabilizer / Flap Interconnect.........................................EE-6
Wing Flaps - Alternate Operation..................................................EE-7
Partial Flaps Landings...................................................................EE-8
Undesired Flap Movement ............................................................EE-8
Autopilot Malfunction.....................................................................EE-9
Autothrottle Malfunction ................................................................EE-9
AFGCS Failure............................................................................EE-10
Mach Trim Compensation Failure...............................................EE-10
Yaw Damper Failure ...................................................................EE-10
Quick Reference Handbook
ABNORMAL / EMERGENCY PROCEDURES REVISION 7
Page EE - 2 May 30/02
Hydraulic System Diagram
ACCUM
ACCUM
AUX
PUMP
FLT
COMB
AUX
AUX PUMP
OFF/ARM ON
NOT
ARM ON
ELECT CONT
MECH CONT
COMBINED
FLIGHT
AUX
COMB/UTIL
COMB/UTIL/AUX
LEFT
ENG
PUMP
RIGHT
ENG
PUMP
FIRE
HANDLE
DISCH
1 2  FIRE
HANDLE
DISCH
2 1 
UTILITY
PUMP MOTOR
UTILITY PUMP
OFF/ARM ON
NOT
ARM ON
GND SPLR SERVO
WING FLAPS
LANDING GEAR
BRAKES
STALL BARRIER
NOSEWHEEL STEERING
CARGO DOOR (ASC 213/354)
MAIN ENTRANCE DOOR
PARKING BRAKES
N2
ACCUM
BOOTSTRAP
BOOTSTRAP
STBY ELEC
ON
HMG
MOTOR
ELEVATORS ELEVATORS
RUDDER RUDDER / YAW DAMP
AILERONS AILERONS
FLIGHT SPOILERS/
SPEED BRAKES
FLIGHT SPOILERS/
SPEED BRAKES
GROUND SPOILERS
COMB OR UTIL OR AUX PRESS
SIGNAL REQ’D FOR FLT USE
GROUND SPOILERS
FLIGHT POWER
SHUT OFF
LEFT
REVERSER
RIGHT
REVERSER
NITROGEN
CHECK VALVE SHUTOFF VALVE
SHUTOFF VALVE (CAA CERT ONLY)
GROUND SERVICE VALVE
Quick Reference Handbook
 
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