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wheel provides roll control from the ailerons. The spoilers and the First
Officer’s control wheel are inoperative.
IF Controls Are Normal:
Accomplish normal IN RANGE, APPROACH and LANDING
checklists when appropriate.
IF Controls Are Not Normal:
Stabilizer Trim Override Switch .................................OVERRIDE
(Continued)
OR
737
Flight Manual
Continental
FLIGHT CONTROLS
Sec. 2.9 Page 5
Rev. 11/15/02 #41
Bank Angle Limit ........................................................15 DEGREES
Plan To Land At Nearest Suitable Airport.
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
BCD If icing conditions have been experienced or are
anticipated prior to landing set VREF = VREF 15 + 10.
Target Speed ....................................VREF PLUS WIND ADDITIVE
Ground Proximity Flap Inhibit Switch...............................INHIBIT
* * * *
FLIGHT CONTROLS
Sec. 2.9 Page 6
Rev. 11/15/02 #41
Continental 737
Flight Manual
JAMMED STABILIZER
This condition is recognized by failure of the stabilizer to respond to electric
trim inputs.
Manual Trim..........................................................................................APPLY
There is no limit on the amount of effort which the Pilots may exert on the
manual trim wheels when attempting to free a jammed stabilizer. Force applied
to the trim wheels causes a disconnect clutch to disengage. Approximately ½
turn of the stabilizer wheel is necessary to disengage the clutch before trimming
can take place. Steady pressure on the manual trim handles is required to
prevent engagement before the desired trim is attained.
IF Airload Causes Trim Wheel To Move When Released:
Stabilizer Trim Autopilot Cutout Switch .......................................CUTOUT
· Autopilot is not available.
· Maintain in-trim airspeed until start of approach. To reduce the force
required to move the stabilizer, use an airspeed which results in an in-trim
condition.
· 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
BCD 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.
· Establish landing configuration early.
· Anticipate higher than normal elevator force during approach and landing.
Ground Proximity Flap Inhibit Switch............................................INHIBIT
* * * *
737
Flight Manual
Continental
FLIGHT CONTROLS
Sec. 2.9 Page 7
Rev. 11/15/02 #41
LEADING EDGE FLAP TRANSIT LIGHT ON
The LE FLAPS TRANSIT amber light illuminated indicates an asymmetry, no
leading edge device(s), or leading edge devices not in programmed position
with respect to the trailing edge flaps. The leading edge devices
annunciator on the aft overhead panel confirms status of leading edge
devices.
Airspeed (Max).............................................................................230 KTS
Wing Anti-Ice (If TAT Below 10° C)..................................................ON
IF Roll Encountered Or During Flap Extension With No Roll:
Plan a flaps 15 landing.
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 additive to VREF for establishing 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.
* * * *
IF During Flap Retraction With No Roll Encountered:
LED Annunciator Panel (Aft Overhead) ..........................CHECK
Flap Handle (Pilot Option).............................................RECYCLE
　
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