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· Loss of A: #1 Thrust Reverser.
· Loss of B: L.E. devices and #2 thrust reverser.
* * * *
STANDBY HYDRAULIC LOW QUANTITY
The Standby Hydraulic LOW QUANTITY light illuminated indicates low fluid level
in the Standby Hydraulic System.
The Standby Hydraulic System may be inoperative.
* * * *
HYDRAULICS
Sec. 2.13 Page 10
Rev. 11/15/02 #41
Continental
737
Flight Manual
INTENTIONALLY LEFT BLANK
737
Flight Manual
Continental
LANDING GEAR
Sec. 2.14 TOC-1
Rev. 11/15/02 #41
2.14 – LANDING GEAR
TABLE OF CONTENTS
ANTI-SKID INOPERATIVE..................................................................... 1
AUTOBRAKE DISARM........................................................................... 1
BRAKE PRESSURE INDICATOR ZERO PSI ....................................... 2
EMERGENCY LANDING TECHNIQUES .............................................. 3
General............................................................................................. 3
Landing Runway............................................................................... 3
Landing Techniques......................................................................... 3
After Stop.......................................................................................... 5
FAILURE OF AIR/GROUND SENSING LOGIC .................................... 6
GEAR LEVER WILL NOT MOVE ABOVE OFF AFTER TAKEOFF ..... 7
MANUAL GEAR EXTENSION................................................................ 9
PARTIAL OR GEAR UP LANDING...................................................... 11
PARTIAL OR GEAR UP LANDING TECHNIQUES ............................ 13
> TIRE SCREEN................................................................................ 14
WHEEL WELL FIRE............................................................................. 14
LANDING GEAR
Sec. 2.14 TOC-2
Rev. 11/15/02 #41
Continental 737
Flight Manual
INTENTIONALLY LEFT BLANK
737
Flight Manual
Continental
LANDING GEAR
Sec. 2.14 Page 1
Rev. 11/15/02 #41
OR
OORR
LANDING GEAR
ANTI-SKID INOPERATIVE
The ANTI-SKID INOP light illuminated indicates a system fault is detected by
the automatic anti-skid monitoring system.
IF On The Ground:
Check MEL for restrictions. For takeoff, turn autobrake switch OFF.
* * * *
IF In Flight:
Autobrakes ...................................................................................OFF
Auto speedbrake is not available. Use manual speedbrakes on
landing.
Brake with caution.
Reference Actual Landing Distances (Unfactored) chart in
Section 5.
* * * *
AUTOBRAKE DISARM
IF On Ground:
Autobrakes ...................................................................................OFF
If the light remains illuminated, DO NOT attempt takeoff.
* * * *
IF In Flight:
Autobrakes ................................................OFF THEN RESELECT
IF The AUTOBRAKE DISARM Light Re-Illuminates:
Autobrakes............................................................................OFF
Use manual brakes.
* * * *
LANDING GEAR
Sec. 2.14 Page 2
Rev. 11/15/02 #41
Continental 737
Flight Manual
BRAKE PRESSURE INDICATOR ZERO PSI
This indicates the nitrogen precharge in the brake accumulator has leaked out,
and accumulator braking is not available.
With hydraulic systems indications normal, brake operation is unaffected.
There is no leak on the hydraulic side of the brakes.
* * * *
737
Flight Manual
Continental
LANDING GEAR
Sec. 2.14 Page 3
Rev. 11/15/02 #41
EMERGENCY 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
　
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