Page 394 - (KU)01-75GAJ-1.5 - Change 1

INTRO

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

1.11.6 AUXILIARY HYDRAULIC SYSTEM FAILURE
ACAWS

WARNING
GROUND

Coming in contact with a pump that has been or is
cavitating, or the adjacent plumbing, may cause severe TAKEOFF
burns.

FIRE/SMK
NORM CAUTION

PRES/OXY
‡ NOT FOR FLIGHT
Allowing a cavitating pump to run will eventually cause
it to overheat.
ENG/PROP

NOTE
FUEL
Operation of the cargo door and ramp at altitude may
cause the auxiliary hydraulic pump to cavitate.
Failure of the electric motor-driven auxiliary hydraulic pump in the AAR
auxiliary hydraulic system results in the loss of hydraulic power for
SPEC normal operation of the following systems: ELEC

‡ Cargo door and ramp.
‡ Loss of electrically controlled emergency hydraulic power for: HYD
- Main landing gear brakes

- Extension of the nose landing gear FLT CTRL

NOTE GEAR

If the auxiliary hydraulic pump is inoperative, the auxiliary
hydraulic system hand pump may be used to supply DOR/RMP
PERF emergency pressure to these systems in the event of the
loss of electrically controlled hydraulic system pressure.
JETTISON
‡ If both utility and auxiliary pressure are lacking for
the brakes, stopping and taxiing control must be
accomplished with reverse thrust and differential power LANDING
application. Stop the aircraft as soon as possible.
Taxiing the aircraft under its own power without brakes
is not recommended. DITCHING

(End of Procedure)
BAILOUT

OPER FAULT LG

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