Page 421 - (KU)01-75GAJ-1.5 - Change 1

INTRO

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

NOTE
ACAWS
‡ Pressure-sealed doors are provided in the wheel well
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two gearbox and hydraulic brake assemblies, and the
vertical torque shafts in the event of a malfunction of GROUND
the MLG system. A NLG inspection window is provided
in the nose wheel well aft bulkhead to permit visual
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doors and on the NLG inspection window. Depressurize
the aircraft before removing the pressure-sealed doors FIRE/SMK
NORM or window.

‡ If hydraulic pressure is lost when placing the landing
gear handle DOWN, place the landing gear handle UP PRES/OXY
NOT FOR FLIGHT
prior to losing all hydraulic pressure.
1.13.2 MAIN AND NOSE GEAR FAIL TO EXTEND ENG/PROP
NORMALLY

If the main and nose landing gear fail to extend normally, attempt to FUEL
identify the malfunction by checking ECBs, hydraulic pressures and
quantity, and for evidence of leaks. If a hydraulic leak is the cause of
the malfunction, further attempts to extend the gear hydraulically may AAR
only serve to deplete the utility hydraulic system.

SPEC If the main and nose landing gear fail to extend normally, proceed as ELEC
follows:

IS A LEAK FOUND OR IS PRESSURE LOST HYD
Q1
WHEN PLACING THE GEAR DOWN?

NO FLT CTRL
A. GEAR................................................................... UP (CP)
Q2 B. Hydraulic System Lo/Loss/Leak procedure....................... GEAR
........................................................ Accomplish (as required)

C. Manual Gear Extension procedure.................. Accomplish
DOR/RMP
PERF (End of Procedure)

JETTISON
Q2 IS THERE A MECHANICAL MALFUNCTION?

NO LANDING
D. Manual Gear Extension procedure................. Accomplish

E (End of Procedure)
DITCHING

E. ECBs.............................................................................. Check (CP)
BAILOUT
F. ECBs....................................................... RESET (as required) (CP)

OPER FAULT LG

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