733QRH快速检查单(19)

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737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
 1.5
1.5
Condition: The NOT ARMED light illuminated indicates the EMER
EXIT LIGHTS switch is not in the ARMED position.
If the EMER EXIT LIGHTS switch is ON, individual
emergency exit light batteries will provide a minimum of 10
minutes of lighting.
If the EMER EXIT LIGHTS switch is OFF, emergency lighting
is not available.
Condition: The flight deck door LOCK FAIL light illuminated
indicates the flight deck door lock has failed or the
Flight Deck Access System switch is OFF.
Conditions permitting:
Flight Deck Access System Switch . . . . . . . . . . . . . . . .OFF
[Removes electrical power to prevent possible lock overheat.]
Note: The door can be locked with the dead bolt.
Condition: The PASS OXY ON light illuminated indicates the
passenger oxygen system is activated.
EMERGENCY EXIT LIGHTS NOT ARMED
LOCK FAIL
PASSENGER OXYGEN ON
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.

1.6
1.6
Condition: Airplane tail has contacted the ground during takeoff.
CAUTION: Do not pressurize airplane due to possible
structural damage.
PRESSURIZATION MODE SELECTOR . . . . . . . . . . . . . . . MAN
OUTFLOW VALVE SWITCH . . . . . . . . . . . . . . . . . . . . . . . OPEN
Hold outflow valve switch in the OPEN position until
outflow VALVE position indicator shows valve full open.
Condition: Arcing, delamination, shattered or cracked condition
of any flight deck window is observed.
WINDOW HEAT SWITCH (affected window) . . . . . . . . . . .OFF
• Limit maximum airspeed to 250 knots below 10,000 feet.
• Use crew and passenger oxygen, if required.
Continued on next page
TAILSTRIKE ON TAKEOFF
WINDOW DAMAGE - DCPCS AIRPLANES
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
 1.7
1.7
Continued from previous page
If window 1, 2, 4 or 5 is affected:
LAND ALT. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10,000 FT
Reduce pressure differential by limiting flight altitude as
indicated in the following tables.
Note: For MEA between 15,000 and 20,000 feet select a
higher LAND ALT to maintain 2 psi differential.
Above 20,000 feet, select MAN and maintain 2 psi
differential.
Window 1, 2, or 5:
Window 4: A failed middle pane usually appears
shattered and transparency is virtually lost.
If window 3 is affected:
LAND ALT. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13,000 FT
Reduce pressure differential by limiting flight altitude as
indicated in the following table.
CRACKED
PANE
MAX DIFF
PRESSURE
APPROX
FLT ALT
Outer –– No Restriction ––
Inner 5 PSI 26,000 FT
Both 2 PSI 15,000 FT
CRACKED
PANE
MAX DIFF
PRESSURE
APPROX
FLT ALT
Outer –– No Restriction ––
Middle 5 PSI 26,000 FT
Both 2 PSI 15,000 FT
CRACKED
PANE
MAX DIFF
PRESSURE
APPROX
FLT ALT
Outer –– No Restriction ––
Inner –– No Restriction ––
Both 0 PSI 13,000 FT
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.

1.8
1.8
Condition: Arcing, delamination, shattered or cracked condition
of any flight deck window is observed.
WINDOW HEAT SWITCH (affected window) . . . . . . . . . . .OFF
• Limit maximum airspeed to 250 knots below 10,000 feet.
• Use crew and passenger oxygen, if required.
If window 1, 2, 4 or 5 is affected:
CABIN ALTITUDE INDICATOR . . . . . . . . . . . . . . . 10,000 FT
PRESSURIZATION MODE SELECTOR . . . . . . . . . . . .STBY
Reduce pressure differential by limiting flight altitude as
indicated in the following tables.
Note: For MEA between 15,000 and 20,000 feet select a
higher cabin altitude to maintain 2 psi differential.
Above 20,000 feet, select MAN and maintain 2 psi
differential.
Airplanes with heated window 3:
Window 1, 2, 3 or 5:
Airplanes without heated window 3:
Window 1, 2 or 5:
Continued on next page
WINDOW DAMAGE - CPCS AIRPLANES
CRACKED
PANE
MAX DIFF
PRESSURE
APPROX
FLT ALT
Outer –– No Restriction ––
Inner 5 PSI 26,000 FT
Both 2 PSI 15,000 FT
CRACKED
PANE
　
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