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OR
(Continued)
FLIGHT CONTROLS
Sec. 2.9 Page 8
Rev. 11/15/02 #41
Continental 737
Flight Manual
OR
IF LE FLAP TRANSIT Light Extinguishes:
Proceed normally.
* * * *
IF LE FLAP TRANSIT Light Remains Illuminated, Limit Airspeed As
Follows:
· If any light(s) for only one leading edge device is illuminated, do not
exceed 300 knots (280 kts for turbulent air penetration) or .65 Mach,
whichever is lowest.
· If any light(s) for more than one leading edge device is illuminated, do
not exceed to 230 knots.
- - - - - PRIOR TO LANDING - - - - -
Plan a flaps 15 landing. 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 PLUS 5 KNOTS
BCD VREF 15 PLUS 15 KNOTS
BCD VREF 15 PLUS 15 KNOTS additive above is adequate in
icing conditions, therefore no additional icing penalty is necessary.
Use normal wind additives to establish an appropriate “target” speed.
Bank Angle .......................................LIMIT TO 15 DEGREES WHEN
BELOW VM FLAPS 0 SPEED
Ground Proximity Flap Inhibit Switch ....................................INHIBIT
Note: If LE FLAPS TRANSIT light should extinguish during flap
extension, proceed with normal landing.
* * * *
737
Flight Manual
Continental
FLIGHT CONTROLS
Sec. 2.9 Page 9
Rev. 11/15/02 #41
MACH TRIM FAIL
The MACH TRIM FAIL light illuminated indicates the Mach Trim system has failed.
Limit airspeed to 280 KIAS or >>@ .74 or BCD .82 Mach,
whichever is lower.
* * * *
FLIGHT CONTROLS
Sec. 2.9 Page 10
Rev. 11/15/02 #41
Continental 737
Flight Manual
RUNAWAY STABILIZER
This condition is recognized by continuing rotation of the stabilizer trim wheel
in a manner not appropriate for flight conditions.
Maintain normal flight attitude by moving control column smoothly in opposite
direction to runaway. Stabilizer brake should engage.
Control Column.....................................................................HOLD FIRMLY
Autopilot (If Engaged) ...............................................................DISENGAGE
Do not re-engage the autopilot.
IF Runaway Continues:
Stabilizer Trim Cutout Switches ..............................................CUTOUT
Continued trimming opposite to an electric trim runaway may result in
overheating and/or stalling of the stabilizer trim motor. In the unlikely
event that both stabilizer brake systems have malfunctioned, placing
the stabilizer trim cutout switches to cutout will have no effect on the
runaway. Control column displacement with no trim input can cause
air loads to aggravate the runaway condition.
IF Runaway Continues:
Stabilizer Trim Wheel..........................................GRASP & HOLD
If positioning the stabilizer trim cutout switches to cutout does not
stop the runaway, stabilizer travel can be stopped by grabbing and
holding the stabilizer trim wheel.
Stabilizer ...........................................................TRIM MANUALLY
Anticipate trim requirements.
Complete IN RANGE, APPROACH, and LANDING
CHECKLISTS.
Establish proper airspeed and establish an in-trim airspeed early
on final approach.
* * * *
737
Flight Manual
Continental
FLIGHT CONTROLS
Sec. 2.9 Page 11
Rev. 11/15/02 #41
SPEED TRIM FAIL
The SPEED TRIM FAIL light illuminated indicates failure of the speed trim system.
No crew action required in flight.
* * * *
SPEEDBRAKE DO NOT ARM
The SPEEDBRAKE DO NOT ARM light illuminated indicates a fault in the automatic
speedbrake system.
Speedbrake Lever..............................................................FULL FORWARD
Manually deploy the speedbrakes immediately upon touchdown.
* * * *
BCD SPEEDBRAKES EXTENDED
The SPEEDBRAKES EXTENDED light illuminated in flight indicates the spoilers are
deployed and:
· Speed brake handle is beyond the ARMED position, and
· Trailing edge flaps extended more than 10°, or
· Radio altitude less than 800 feet.
The SPEEDBRAKES EXTENDED light illuminated on the ground indicates the speed
brake lever is in the DOWN detent and the ground spoilers are deployed.
Speed Brake Lever ..............................................ARMED/DOWN DETENT
IF Light Remains Illuminated After Speed Brake Lever Is Down:
Spoilers may be extended.
IF Light Is Illuminated On The Ground:
　
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