737 FLIGHT MANUAL 737飞行手册1(27)

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determine the severity of the incident, it will be considered a LEVEL 4
SECURITY INCIDENT.
If the HARD LOCK mode is not engaged, it presumes that all pilots are
incapacitated, and after 30-seconds the alert warning will stop and the door will
be unlocked for only 5 seconds to allow opening. If the door is not opened
during this time, it will relock and the process will have to be repeated.
* * * *
IMMEDIATE ACTION
Flight Deck Door HARD LOCK Switch .................................................PUSH
AIRPLANE GENERAL
Sec. 2.1 Page 14
Rev. 11/15/02 #41
Continental
737
Flight Manual
FLIGHT DECK DOOR UNLKD
Condition: There is a fault in the door control system, status lights, or lock
mechanism and the security of the door is unknown.
Flight Deck Door Mechanical Lock ................................................ENGAGE
Insert the mechanical lock pin located on the door, into the hole on the latch
to mechanically lock the door.
Note: Use of the mechanical lock will not allow the door to be opened
by the FLIGHT DECK DOOR EMERGENCY ENTRANCE system. A flight
attendant, working crewmember, or other authorized ACM /
jumpseat rider must remain on the flight deck to engage /
disengage the mechanical lock anytime there is only one pilot on
the flight deck. This is to ensure access to the flight deck in the
event the one pilot becomes incapacitated.
HARD LOCK Switch...................................................................................... PUSH
If the UNLKD light and FLIGHT DECK DOOR lights are illuminated (indicating a
system fault), pushing the HARD LOCK switch will:
- extinguish the UNLKD light
- extinguish the FLIGHT DECK DOOR light
- not engage HARD LOCK mode
- not illuminate HARD LOCK light
- not ensure the door is locked
* * * *
737
Flight Manual
Continental
AIR SYSTEMS
Sec. 2.2 TOC-1
Rev. 11/15/02 #41
2.2 – AIR SYSTEMS
TABLE OF CONTENTS
AIR CONDITIONING SMOKE / FUMES................................................ 1
AUTO FAIL OR UNSCHEDULED PRESSURIZATION CHANGE ....... 3
AUTOMATIC PRESSURIZATION CONTROL
LANDING AIRPORT ELEVATION ABOVE 6000 FEET................. 4
BLEED TRIP DURING NO ENGINE BLEED TAKEOFF....................... 5
BLEED TRIP OFF................................................................................... 6
CABIN ALTITUDE WARNING OR RAPID DECOMPRESSION /
EMERGENCY DESCENT ............................................................... 7
>>@ CABIN DIFFERENTIAL PRESSURE CHART ................... 11
DUAL BLEED LIGHT............................................................................ 11
>>@B DUCT OVERHEAT ....................................................... 12
EMERGENCY DESCENT PROCEDURE ........................................... 13
Manual Flight.................................................................................. 14
Use Of The Autopilot...................................................................... 14
During Descent............................................................................... 15
After Level Off ................................................................................ 15
EQUIPMENT COOLING OFF .............................................................. 17
MANUAL MODE OPERATION............................................................. 18
OFF-SCHEDULE DESCENT ............................................................... 19
B PACK TRIP OFF / CD PACK.................................................. 20
>>@ PACK TRIP OFF.................................................................. 22
PASSENGER OXYGEN ON................................................................. 22
STANDBY / ALTN OPERATION.......................................................... 23
UNPRESSURIZED LANDING PROCEDURE –
DIGITAL AND NON-DIGITAL ........................................................ 24
UNPRESSURIZED TAKEOFF PROCEDURE –
DIGITAL AND NON-DIGITAL ........................................................ 25
WING-BODY OVERHEAT.................................................................... 26
CD ZONE TEMP ............................................................................ 27
AIR SYSTEMS
Sec. 2.2 TOC-2
Rev. 11/15/02 #41
Continental 737
Flight Manual
INTENTIONALLY LEFT BLANK
737
Flight Manual
Continental
AIR SYSTEMS
Sec. 2.2 Page 1
Rev. 11/15/02 #41
AIR SYSTEMS
AIR CONDITIONING SMOKE / FUMES
Air conditioning smoke / fumes can be detected by material entering the
passenger cabin and/or flight deck from the air conditioning system.
　
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