Page 420 - (KU)01-75GAJ-1.5 - Change 1

INTRO

EP'S (KU)01-75GAJ-1.5 FIGURES

1.13.1 GENERAL LANDING GEAR EMERGENCY
INFORMATION ACAWS

As a general rule for landing gear system malfunctions, if all landing
gear are down and locked, do not retract the landing gear unless a GROUND
greater emergency exists. Additionally, if there is known or suspected
damage to main landing gear structural components, it is recommended
that the crew secure the landing gear down, using the Main Landing TAKEOFF
Gear Tiedown procedures.

If any landing gear fails to extend after normal operation of the landing FIRE/SMK
NORM gear control lever, attempt to identify the malfunction before making

further attempts to lower the gear. Check circuit breakers, utility hydraulic
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NOT FOR FLIGHT
leaks or mechanical failures. The following is the general precedence
order for correcting landing gear malfunctions:
ENG/PROP
‡ Overriding the Landing Gear Selector Valve

‡ Main Landing Gear Manual Extension FUEL
‡ Nose Landing Gear Emergency Extension
‡ Nose Landing Gear Emergency Extension after Complete Loss AAR
of Hydraulic Pressure (Utility and Auxiliary)

SPEC ‡ Main Landing Gear Extension After Normal and Emergency ELEC
System Failure

WARNING HYD

If the soft panel is used to lower the landing gear, due to FLT CTRL
hard panel failure, do not turn the soft panel off until the
nose gear is pinned and all personnel are clear of the
nose wheel area. Selecting soft panel to VERIFY OFF GEAR
may send the last valid hard panel command of gear up
to the landing gear selector valve.
DOR/RMP

PERF CAUTION

JETTISON

Prior to landing with a main landing gear system and/ or
position indicator failure (actual or suspected), visually LANDING
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bumper stops. Depressurize the aircraft and remove the
main landing gear inspection windows (affected side) as DITCHING
required for visual access.

BAILOUT

OPER FAULT LG

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