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Do not take off.
* * * *
OR
FLIGHT CONTROLS
Sec. 2.9 Page 12
Rev. 11/15/02 #41
Continental 737
Flight Manual
STAB OUT OF TRIM
The STAB OUT OF TRIM light illuminated, with the autopilot engaged, indicates
that the elevator position exceeds a certain value in relation to stabilizer
position.
Momentary illumination of the STAB OUT OF TRIM light during large changes in
trim requirements is normal.
IF The Stabilizer Is Not Trimming:
Control Column..............................................................HOLD FIRMLY
The control column should be held steady to prevent undesirable
aircraft pitching.
Autopilot...............................................................................DISENGAGE
The autopilot should be disengaged as soon as practical.
Stabilizer Trim.................................................................AS REQUIRED
Return to an in-trim condition.
* * * *
TRAILING EDGE FLAPS MALFUNCTION
Flap Position Indicator CB .........................................................CHECK
IF Flaps Are Asymmetric (Flap Position Needles Are Separated):
Caution: Do not attempt further movement of trailing edge flaps
with the alternate flaps switch as there is no asymmetry
protection.
Consider burning off fuel to reduce touchdown speed. Max tire speed
is 195 knots.
Flap Lever.........MOVE FLAP LEVER TO DETENT NEAREST
TO THE SMALLEST ACTUAL FLAP POSITION
Adjusted VREF computation (set VREF Bug as follows):
Flaps Less Than 1 ...........................................VREF 40 + 40 KNOTS
Flaps Between 1 & 15.....................................VREF 40 + 30 KNOTS
Flaps 15 Or More ..............................SET VREF FOR SMALLEST
ACTUAL FLAP POSITION
OR
~
(Continued)
737
Flight Manual
Continental
FLIGHT CONTROLS
Sec. 2.9 Page 13
Rev. 11/15/02 #41
BCD If using VREF 15 and If icing conditions have been
experienced or are anticipated prior to landing set VREF =VREF 15 +
10.
Use normal wind additive to VREF for establishing appropriate “target”
speed.
Target Speed ........... ADJUSTED VREF PLUS WIND ADDITIVE
· Stick shaker may occur at high gross weights and/or bank
angles greater than 15 degrees.
Flaps less than 1:
· Maintain VM Flaps 0 until on final.
· Limit bank angle to 15 degrees below VM Flaps 0 speed.
Flaps 1 or greater:
· Maintain at or above VM for smallest actual flap position until
on final.
· Limit bank angle to 15 degrees when below VM for smallest
actual flap position.
- - - - - PRIOR TO FINAL - - - - -
Ground Proximity Flap Inhibit Switch.............................INHIBIT
IF Leading Edge Devices Are Not In FULL EXT Position:
Alternate Flaps Master Switch......................................... ARM
This arms the alternate flaps switch and starts the standby
hydraulic pump for leading edge device extension.
Alternate Flaps Position
Switch (230 Knots Max) ...........MOMENTARILY DOWN
The flap asymmetry is not adversely affected by holding the switch
momentarily down. Verify LED annunciator panel (AFT
overhead) indicated FULL EXT.
Amber LE FLAPS TRANSIT light (center instrument panel) may
remain illuminated if flaps are less than 10 degrees.
Note: If leading edge devices remain retracted and trailing
edge devices are less than 1, refer to ALL FLAPS
UP LANDING procedure.
~
~ (Continued)
FLIGHT CONTROLS
Sec. 2.9 Page 14
Rev. 11/15/02 #41
Continental 737
Flight Manual
Go-Around Procedure ....................................................... REVIEW
Limit bank angle to 15 degrees when below VM for smallest actual
flap position.
Do not exceed leading edge or trailing edge flap limit speeds.
* * * *
IF Flaps Are Symmetric (Flap Position Indicator Needles Are Not
Separated):
Plan a flaps 15 landing using alternate flap extension.
A flaps 15 landing is recommended because of the time required to
retract flaps electrically in event of a go-around.
Flaps 15 configuration results in a higher than normal pitch attitude.
There is a tendency to push the nose down to obtain a normal visual
sight picture. Use caution to avoid going below the normal glide path.
REF Speed ...............................................................................VREF 15
BCD If using VREF 15 and if icing conditions have been
experienced or are anticipated prior to landing set VREF = VREF 15
+ 10.
Use normal wind additive to VREF for establishing appropriate
“target” speed.
　
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