9.24
9.24
Condition: The trailing edge flaps do not move when flaps 1 is
selected.
If no asymmetry exists:
Ensure the TRAILING EDGE FLAP DISAGREE checklist
has been accomplished.
If an asymmetry exists:
ALTERNATE FLAPS master
switch (230 knots maximum) . . . . . . . . . . . . . . . . . . . . ARM
ALTERNATE FLAPS position
switch . . . . . . . . . . . . . . . . . . . . . . . . . . . .Momentary DOWN
Verify leading edge devices annunciator indicates
FULL EXT.
Note: The LE FLAPS TRANSIT light will remain
illuminated.
If the leading edge devices annunciator does not indicate
FULL EXT:
Accomplish the ALL FLAPS UP LANDING checklist.
Burn off fuel to reduce touchdown speed.
Set VREF 40 + 40 knots.
Check the appropriate Non-Normal Configuration Landing
Distance table in the ADVISORY INFORMATION section of
the Performance-Inflight chapter.
Maintain 210 knots until on final.
Limit bank angle to 15° until reaching 210 knots.
Continued on next page
TRAILING EDGE FLAPS UP LANDING
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
9.25
9.25
Continued from previous page
----------------------------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 40 + 40 knots, Minimums ___
[A nuisance stick shaker may occur when slowing to VREF 40 + 40 at high
gross weights and/or bank angles greater than 15°.]
Approach briefing . . . . . . . . . . . . . . . . . . . . . . . . . . Completed
Go-around procedure . . . . . . . . . . . . . . . . . . . . . . . . . . Review
Accomplish normal go-around procedure except:
• Limit bank angle to 15 ° until reaching 210 knots.
• Accelerate to 210 knots.
• Do not exceed 230 knots with leading edge flaps
extended.
----------------------------DEFERRED ITEMS ------------------------------
==> APPROACH
Altimeters . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ___
Continued on next page
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
9.26
9.26
Continued from previous page
----------------------------DEFERRED ITEMS ------------------------------
==> LANDING
ENGINE START switches . . . . . . . . . . . . . . . . . . . . . . . . CONT
Speedbrake . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ARMED
Landing gear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .DOWN
Flaps . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . UP, amber light
[On speed tape equipped airplanes, operation within the lower yellow
airspeed band is normal for this condition.]
Note: Due to minimum speed reversion, V/S and VNAV PTH
modes may revert to LVL CHG mode.
FASTEN BELTS switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
9.27
9.27
Intentionally
Blank
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
9.28
9.28
Condition: Uncommanded rudder pedal displacement or pedal
kicks or uncommanded yaw or roll.
If trailing edge flaps are extended, with no flap asymmetry
and rudder pedals are normal. (May be accompanied by a
loud bang.)
FLAPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . Retract to flaps 1
on schedule
[Roll may be the result of trailing edge flap displacement due to a flap
spindle fracture.]
Consider accomplishing a go-around.
Plan a flaps 1 landing.
Set VREF 40 + 30.
Check the appropriate Non-Normal Configuration
Landing Distance table in the ADVISORY INFORMATION
section of the Performance-Inflight chapter.
Continue checklist at DEFERRED ITEMS, DESCENT.
If STBY RUD ON light is installed on the overhead Flight
Control panel and is not placarded INOP:
Accomplish the JAMMED OR RESTRICTED FLIGHT
CONTROLS Non-Normal Checklist.
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