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to free and center the rudder pedals.
IF Rudder Pedal Position Or Movement Is Not Normal And The Condition Is
Not The Result Of Rudder Trim:
System B Flight Control Switch ............................................. STBY RUD
A slight rudder deflection may remain, but continued rudder pedal pressure
may help maintain an in-trim condition.
Sufficient directional control is available on landing using differential
braking and nose wheel steering.
Crosswind capability may be reduced.
Do not use autobrakes.
Consider checking rudder freedom of movement at a safe altitude using
slow rudder inputs while in the landing configuration and at approach
speed.
IF Condition Was The Result Of Rudder Trim Or Environmental Factors:
Yaw Damper Switch ...............................................................................ON
Accomplish the normal DESCENT – APPROACH and LANDING checklists.
* * * *
OR
FLIGHT CONTROLS
Sec. 2.9 Page 18
Rev. 11/15/02 #41
Continental 737
Flight Manual
YAW DAMPER
The yaw damper is a separate control and provides a limited rudder movement
in opposition of the yaw rate of the aircraft. Rudder (yaw damper) indicator
displacement indicates yaw damper operation. YAW DAMPER light illuminates
amber when the yaw damper is not engaged (Ref. A.D. 96-26-07).
Yaw Damper Switch.............................................................. OFF, THEN ON
IF Light Remains Illuminated:
Yaw Damper Switch ...........................................................................OFF
* * * *
737
Flight Manual
Continental
FLT INSTRMT, DSPLYS
Sec. 2.10 TOC-1
Rev. 11/15/02 #41
2.10 – FLIGHT INSTRUMENTS, DISPLAYS
TABLE OF CONTENTS
AIRSPEED UNRELIABLE ...................................................................... 1
BCD ALT DISAGREE................................................................. 1
BCD CDS FAULT ....................................................................... 2
BCD CDS MAINT........................................................................ 2
BCD DISPLAYS CONTROL PANEL ......................................... 3
BCD DSPLY SOURCE............................................................... 4
BCD DISPLAY UNIT FAILURE.................................................. 4
ERRONEOUS COMPASS HEADINGS ................................................. 5
FLIGHT RECORDER ............................................................................. 5
BCD IAS DISAGREE.................................................................. 5
INSTRUMENT SWITCHING .................................................................. 5
>@ SYMBOL GENERATOR FAIL.................................................. 6
FLT INSTRMT, DSPLYS
Sec. 2.10 TOC-2
Rev. 11/15/02 #41
Continental 737
Flight Manual
INTENTIONALLY LEFT BLANK
737
Flight Manual
Continental
FLT INSTRMT, DSPLYS
Sec. 2.10 Page 1
Rev. 11/15/02 #41
FLIGHT INSTRUMENTS, DISPLAYS
AIRSPEED UNRELIABLE
· Pitch attitude not consistent with existing phase of flight, altitude, thrust,
and weight, or noise and/or low frequency buffeting.
· Crosscheck ground speed and winds provided by the IRS and FMC to
determine airspeed accuracy if indicated airspeed is questionable.
· Reference FLIGHT WITHOUT RELIABLE AIRSPEED chart in section 5
or QRH.
Note: Erroneous or unreliable airspeed indications may be caused by blocked
or frozen pitot-static system(s), or a severely damaged or missing
radome.
Aircraft Attitude & Thrust ............................................................... ADJUST
Pitot / Probe Heat .........................................................................CHECK ON
Mach & Airspeed Indicators .............................................. CROSS CHECK
* * * *
BCD ALT DISAGREE
The ALT DISAGREE alert indicates the Captain’s and First Officer’s altitude
indications disagree by more than 200 feet for more than 5 continuous seconds.
Altimeter Barometric Settings...........................................................CHECK
Check all altimeters set to proper barometric setting for phase of flight.
IF ALT DISAGREE alert extinguishes after resetting barometric settings, operate
normally.
* * * *
IF ALT DISAGREE alert remains:
Flight not permitted in RVSM airspace.
Transponder altitude received by ATC may be unreliable.
Maintain visual conditions, if possible.
OR
(Continued)
FLT INSTRMT, DSPLYS
Sec. 2.10 Page 2
Rev. 11/15/02 #41
Continental
737
Flight Manual
　
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