0.28
0.28
Condition: Airplane tail has contacted the ground during takeoff.
CAUTION: Do not pressurize airplane due to possible
structural damage.
PRESSURIZATION MODE SELECTOR . . . . . . . . . . . . . . . MAN
OUTFLOW VALVE SWITCH . . . . . . . . . . . . . . . . . . . . . . . OPEN
Hold outflow valve switch in the OPEN position until
outflow VALVE position indicator shows valve full open.
TAILSTRIKE ON TAKEOFF
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
0.29
0.29
Intentionally
Blank
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
0.30
0.30
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.
Continued on next page
UNCOMMANDED RUDDER/YAW OR ROLL
AUTOPILOT (if engaged) . . . . . . . . . . . . . . . . . . . .DISENGAGE
Maintain control of the airplane with all available flight
controls. If roll is uncontrollable, immediately reduce
pitch/angle of attack and increase airspeed. Do not attempt
to maintain altitude until control is recovered.
AUTOTHROTTLE (if engaged) . . . . . . . . . . . . . . .DISENGAGE
Verify thrust is symmetrical.
June 3, 2005
737 Flight Crew Operations Manual
Copyright © The Boeing Company. See title page for details.
0.31
0.31
Continued from previous page
If STBY RUD ON light is not installed on the overhead Flight
Control panel or is placarded INOP:
YAW DAMPER . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .OFF
If the yaw or roll stops:
AUTOPILOT . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ENGAGE
AUTOTHROTTLE . . . . . . . . . . . . . . . . . . . . . . . .ENGAGE
Accomplish the normal DESCENT, APPROACH and
LANDING checklists.
If yaw or roll is the result of uncommanded rudder
displacement or pedal kicks:
Rudder trim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Center
Rudder pedals . . . . . . . . . . . . . . . . . . . . . . . Free & center
Use maximum force including a combined effort of
both pilots, if required, to free and center the rudder
pedals.
If rudder pedal position and/or movement are normal:
YAW DAMPER. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ON
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：733QRH快速檢查單(15)
