733QRH快速检查单(17)

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If engines have flamed out or stalled, or EGT rapidly
approaches or exceeds limit:
Accomplish the LOSS OF THRUST ON BOTH ENGINES
checklist.
Engines may accelerate to idle very slowly, especially at
high altitudes. Slow acceleration may be incorrectly
interpreted as a hung start or an engine malfunction. If N2 is
steadily increasing, and EGT remains within limits, the start
is progressing normally.
Plan to land at the nearest suitable airport.
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.

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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:
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.
Continued on next page
WINDOW DAMAGE - DCPCS 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
MAX DIFF
PRESSURE
APPROX
FLT ALT
Outer –– No Restriction ––
Middle 5 PSI 26,000 FT
Both 2 PSI 15,000 FT
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
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Continued from previous page
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 –– 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.

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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
MAX DIFF
PRESSURE
APPROX
FLT ALT
Outer –– No Restriction ––
Inner 5 PSI 26,000 FT
Both 2 PSI 15,000 FT
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
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Continued from previous page
If window 1, 2, 4 or 5 is affected: (continued)
Window 4: A failed middle pane usually appears
shattered and transparency is virtually lost.
Airplanes without heated window 3:
If window 3 is affected:
CABIN ALTITUDE INDICATOR . . . . . . . . . . . . . 13,000 FT
PRESSURIZATION MODE SELECTOR . . . . . . . . . .STBY
Reduce pressure differential by limiting flight altitude
as indicated in the following table.
CRACKED
PANE
MAX DIFF
PRESSURE
APPROX
FLT ALT
Outer –– No Restriction ––
　
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