733QRH快速检查单(32)

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PACK SWITCH . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .-AUTO
Accomplish the ENGINE IN-FLIGHT START checklist to start
the other engine.
If neither IRS attitude display recovers after a generator bus
is restored:
IRS MODE SELECTOR SWITCHES . . . . . . . . . . . . . . . . ATT
Maintain straight and level, constant airspeed flight
until attitude displays recover (approximately 30
seconds).
MAGNETIC HEADING . . . . . . . . . . . . . . . . . . . . . . . . ENTER
APU . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED
Condition: The LOW IDLE light illuminated indicates the related
engine is below minimum required RPM.
AUTOTHROTTLE (if engaged) . . . . . . . . . . . . . . .DISENGAGE
[Allows thrust lever to remain where manually positioned.]
THRUST LEVERS . . . . . . . . . . . . ADVANCE THRUST LEVERS
UNTIL LIGHT EXTINGUISHES
LOW IDLE
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.

7.20
7.20
Condition: Landing must be accomplished with one engine
inoperative.
Plan a flaps 15 landing.
Set VREF 15.
Maintain VREF 15 + 5 knots minimum on final approach.
Apply normal wind correction but do not go below VREF 15
+ 5 knots to assure adequate speed for go-around.
----------------------------DEFERRED ITEMS ------------------------------
==> DESCENT
Recall . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Checked
Anti–ice . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ___
Use engine anti–ice on the operative engine only.
If additional go–around thrust is desired, below 10,000 feet
configure the pressurization system for a no engine bleed
landing:
ISOLATION valve switch . . . . . . . . . . . . . . . . . . . . . . CLOSE
Engine No. 1 BLEED air switch . . . . . . . . . . . . . . . . . . .OFF
APU BLEED air switch . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
Do not open the APU bleed valve if the engine fire
warning switch remains illuminated.
Left PACK switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTO
Engine No. 2 BLEED air switch . . . . . . . . . . . . . . . . . . .OFF
Autobrake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ___
GROUND PROXIMITY FLAP/GEAR
INHIBIT switch (as installed) . . . . . . . . . . FLAP/GEAR INHIBIT
GROUND PROXIMITY FLAP
INHIBIT switch (as installed) . . . . . . . . . . . . . . . .FLAP INHIBIT
Landing data . . . . . . . . . . . . . . . . . . . .VREF 15, Minimums ___
Continued on next page
ONE ENGINE INOPERATIVE LANDING
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
 7.21
7.21
Continued from previous page
Approach briefing . . . . . . . . . . . . . . . . . . . . . . . . . . Completed
Go–around procedure . . . . . . . . . . . . . . . . . . . . . . . . . . Review
Accomplish normal go–around procedure except:
• Use flaps 1
• Maintain VREF 15 + 5 knots to flap retraction altitude
• Limit bank angle to 15 degrees until reaching VREF 15
+ 15 knots or minimum maneuver speed
• Accelerate to flaps 1 maneuvering speed prior to flap
retraction.
----------------------------DEFERRED ITEMS ------------------------------
==> APPROACH
Altimeters . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ___
----------------------------DEFERRED ITEMS ------------------------------
==> LANDING
ENGINE START
switch (operating engine) . . . . . . . . . . . . . . . . . . . . . . . . CONT
Speedbrake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ARMED
Landing gear. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .DOWN
Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15, green light
Condition: The power management control INOP light
illuminated indicates the PMC is inoperative or OFF.
THRUST LEVERS (if required) . . . . . . . . . . . . . . . . . . ADJUST
Flight may continue with the autothrottle ON.
In manual operation, adjust the thrust levers as required.
Observe engine limits.
POWER MANAGEMENT CONTROL
(PMC) INOPERATIVE
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.

7.22
7.22
Condition: The REVERSER light illuminated indicates a fault is
detected in the related engine reverser system.
Note: Additional system failures may cause inflight
　
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