9.2
9.2
Continued from previous page
----------------------------DEFERRED ITEMS ------------------------------
==> LANDING
ENGINE START switches . . . . . . . . . . . . . . . . . . . . . . . . CONT
Speedbrake. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ARMED
Landing gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .DOWN
Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .UP, no lights
FASTEN BELTS switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
Condition: The AUTO SLAT FAIL light illuminated indicates
failure of the auto slat system.
No crew action required in flight.
Condition: The FEEL DIFF PRESS light illuminated indicates
significant differential pressure in the elevator feel
computer.
No crew action required in flight.
Condition: The FLAP LOAD RELIEF light illuminated indicates
the flap load relief system has been activated and
flaps are retracting from 40 to 30 due to excessive
airspeed.
Check flap position and maintain appropriate airspeed.
AUTO SLAT FAIL
FEEL DIFFERENTIAL PRESSURE
FLAP LOAD RELIEF
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
9.3
9.3
Condition: A FLT CONTROL LOW PRESSURE light illuminated
indicates the related hydraulic system pressure to
ailerons, elevators and rudder is low or the rudder
pressure reducer has failed in the low pressure mode.
FLIGHT CONTROL SWITCH . . . . . . . . . . . . . . . . . . STBY RUD
FLIGHT CONTROL LOW PRESSURE
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
9.4
9.4
Condition: Movement of the elevator, aileron/spoiler or rudder is
restricted.
AUTOPILOT (if engaged) . . . . . . . . . . . . . . . . . . . .DISENGAGE
AUTOTHROTTLE (if engaged) . . . . . . . . . . . . . . .DISENGAGE
Verify thrust is symmetrical.
If rudder is jammed or restricted and STBY RUD ON light is
not installed on the overhead Flight Control panel or is
placarded INOP:
Accomplish the UNCOMMANDED RUDDER/YAW OR
ROLL Non-Normal checklist.
JAMMED or RESTRICTED system . . . . . . . . . . . . . Overpower
Use maximum force, including a combined effort of both
pilots, if required. A maximum two-pilot effort on the
controls will not cause a cable or system failure.
Do not turn off any flight control switches.
If controls are normal:
Accomplish the normal DESCENT, APPROACH and
LANDING checklists.
Continued on next page
JAMMED OR RESTRICTED
FLIGHT CONTROLS
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
9.5
9.5
Continued from previous page
If controls are not normal:
Use stabilizer or rudder trim to offload control forces.
If electric stabilizer trim is desired, position the Stabilizer
Trim Override switch to OVERRIDE.
Do not make abrupt thrust changes. Extend or retract
speedbrake slowly and smoothly.
Limit bank angle to 15°.
Plan to land at the nearest suitable airport.
Plan a flaps 15 landing.
Set VREF 15 + 5 knots.
------------------------DEFERRED ITEMS ------------------------------
==> DESCENT
Recall . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Checked
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 + 5 knots, Minimums ___
Approach briefing . . . . . . . . . . . . . . . . . . . . . . . . Completed
Go-around procedure . . . . . . . . . . . . . . . . . . . . . . . . Review
Accomplish normal go-around procedure. Advance
thrust to go-around smoothly and slowly to avoid
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