9.16
9.16
Condition: STBY RUD ON light is illuminated.
If the STBY RUD ON light is illuminated due to pilot manual
positioning of FLT CONTROL A or B Switch to STBY RUD or
in response to a hydraulic system non-normal situation:
No crew action required in flight.
If the STBY RUD ON light is illuminated with no other flight
deck indications:
Avoid large or abrupt rudder pedal inputs.
STANDBY RUDDER ON
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
9.17
9.17
Intentionally
Blank
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
9.18
9.18
Condition: An uncommanded roll occurs when a new flap
selection is made and/or a difference between the left
and right flap indication is observed.
FLAPS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Set
Move flap lever to the detent nearest the smallest
indicated flap position.
CAUTION: Do not attempt to move the trailing edge flaps
with the alternate flaps switch as there is no
asymmetry protection.
If flaps are 15 or more:
Set VREF for smallest flap position.
Note: VREF + wind additive must not exceed the flap
placard speed for the next larger flap setting.
Continue checklist at DEFERRED ITEMS, DESCENT.
If flaps are 1 or greater and less than 15:
Set VREF 40 + 30 knots.
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 flaps are less than 1:
Accomplish the TRAILING EDGE FLAPS UP LANDING
checklist.
Note: Do not use FMC fuel predictions with flaps
extended.
Continued on next page
TRAILING EDGE FLAP ASYMMETRY
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
9.19
9.19
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 ___, Minimums ___
Approach briefing . . . . . . . . . . . . . . . . . . . . . . . . . . Completed
----------------------------DEFERRED ITEMS ------------------------------
==> APPROACH
Altimeters . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ___
----------------------------DEFERRED ITEMS ------------------------------
==> LANDING
ENGINE START switches . . . . . . . . . . . . . . . . . . . . . . . . CONT
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