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Landing Procedure............................................................................REVIEW
· Position fuel pump switches OFF just prior to flare. Fuel pressure to
the engines should be shut OFF prior to landing to reduce the
possibility of fire.
· Raise speed brake lever at touchdown if both main landing gears are
fully extended or if stopping distance is critical.
· After stop, accomplish the EMERGENCY EVACUATION (LAND)
CHECKLIST, if required.
* * * *
737
Flight Manual
Continental
LANDING GEAR
Sec. 2.14 Page 13
Rev. 11/15/02 #41
PARTIAL OR GEAR UP
LANDING TECHNIQUES
General
Consideration should be given to the best suitable airport with adequate firefighting
capability.
Coordinate with all ground emergency facilities. For example, the fire trucks
normally operate on a common VHF frequency with the aircraft and can advise
the crew of aircraft condition during landing.
Consideration should be given to landing with as many gear down as possible.
Circumstances will influence the pilot's decision as to whether a partial gear-up
landing should be made. If a choice of configuration is available, the decision
will be determined by the amount of landing gear available, the conditions at the
landing field, time of landing, available facilities, aircraft load distribution, and
controllability. In all cases, reduce weight as much as practicable by burning off
fuel to provide the slowest possible touchdown speed.
Fuel pressure to the engines should be shut off before the engines contact the
ground to reduce the possibility of fire. If the APU is running, it also should be
shut down prior to landing.
Landing Runway
Consideration should be given to the best suitable airport with adequate runway
and fire fighting capability. Foaming the runway is not recommended. Tests
have shown that foaming provides minimal benefit and it takes approximately
30 minutes to replenish the fire truck's foam supply.
Landing Techniques
Plan a normal approach, extending maximum (for configuration) flaps as for a
normal landing and normal rate of descent. Use the normal VREF speed plus
wind velocity and gust factor corrections.
The landing should be made with all available gear down and every effort
should be made to keep the aircraft on the hard surfaced runway. This will
minimize damage to the aircraft and facilitate passenger evacuation.
Deployment of speedbrakes at touchdown with one main landing gear retracted
is not recommended unless stopping distance is critical.
LANDING GEAR
Sec. 2.14 Page 14
Rev. 11/15/02 #41
Continental 737
Flight Manual
> TIRE SCREEN
The TIRE SCREEN light monitors the screen locking pins in the wheel well.
Caution: If the TIRE SCREEN light is illuminated and the cause is a tire
burst screen not secure, equipment damage could result when
the gear is retracted.
Note: The screens are not installed in A/C 329 and subsequent.
* * * *
WHEEL WELL FIRE
Landing Gear (270 Kts. Max) .............................................................DOWN
Do not retract landing gear until at least 20 minutes after WHEEL WELL fire
warning light extinguishes.
No fire extinguishing equipment is installed in the wheel wells. The primary
source of overheat or fire is in the wheel brake system. If a warning sound
should occur, the wheels may be extended removing the heat or fire from the
wheel wells.
IF The Landing Gear Must Be Retracted For Aircraft Performance:
Landing Gear (235 Kts. Max) ..............................................................UP
Do not retract landing gear until airspeed is reduced to retract limit of 235
knots.
Land At Nearest Suitable Airport.
* * * *
737
Flight Manual
Continental
WARNING SYSTEMS
Sec. 2.15 TOC-1
Rev. 11/15/02 #41
2.15 – WARNING SYSTEMS
TABLE OF CONTENTS
CONFIGURATION WARNING............................................................... 1
GROUND PROXIMITY ALERT .............................................................. 1
BCD PSEU.................................................................................... 2
WARNING SYSTEMS
Sec. 2.15 TOC-2
Rev. 11/15/02 #41
Continental 737
Flight Manual
INTENTIONALLY LEFT BLANK
737
Flight Manual
Continental
WARNING SYSTEMS
Sec. 2.15 Page 1
Rev. 11/15/02 #41
WARNING SYSTEMS
CONFIGURATION WARNING
Condition: An intermittent warning horn sounds when advancing thrust levers
to takeoff, or a steady warning horn sounds inflight.
Assure proper aircraft configuration.
　
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