13.6
13.6
Continued from previous page
----------------------------DEFERRED ITEMS ------------------------------
==> LANDING
ENGINE START switches . . . . . . . . . . . . . . . . . . . . . . . . CONT
Speedbrake. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ARMED
Landing gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .DOWN
Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15, green light
December 5, 2003
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
13.7
13.7
Intentionally
Blank
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
13.8
13.8
Condition: Both system A & B hydraulic pump LOW PRESSURE
lights illuminated accompanied by low system A & B
pressure indicates loss of both system A & B. Other
indications include:
• system A & B flight control LOW PRESSURE lights illuminated.
SYSTEM A and B
FLIGHT CONTROL switches . . . . . . . . . . . . . . . . . . STBY RUD
SYSTEM A and B
HYDRAULIC PUMP switches . . . . . . . . . . . . . . . . . . . . . . .OFF
Note: Inoperative items:
• ground spoilers
• all flight spoilers
• nose wheel steering
• autopilot A & B
• yaw damper
Note: Thrust reversers and leading edge flaps and slats
have standby pressure. Trailing edge flaps have
alternate electrical power. Inboard and outboard
brakes have accumulator pressure only.
Plan for flaps 15 landing.
Set VREF 15.
Plan for manual gear extension.
Note: When the gear has been lowered manually, it cannot
be retracted. The drag penalty with gear extended
may make it impossible to reach an alternate field.
Plan to extend flaps to 15 using alternate flap extension.
Note: Alternate flap extension time to flaps 15 is
approximately 2 minutes.
Note: The drag penalty with the leading edge devices
extended may make it impossible to reach an
alternate field.
Note: The crosswind capability of the airplane is greatly
reduced.
Continued on next page
MANUAL REVERSION
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
13.9
13.9
Continued from previous page
On touchdown, apply steady brake pressure without
modulating the brakes.
Do not attempt to taxi the airplane after stopping.
----------------------------DEFERRED ITEMS ------------------------------
==> DESCENT
Recall. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Checked
Autobrake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
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 ___
Approach briefing . . . . . . . . . . . . . . . . . . . . . . . . . . Completed
Go-around procedure . . . . . . . . . . . . . . . . . . . . . . . . . . Review
Accomplish normal go-around procedure except:
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