Page 393 - (KU)01-75GAJ-1.5 - Change 1

INTRO

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

1.11.4 UTILITY HYDRAULIC SYSTEM FAILURE
ACAWS
Systems lost:

‡ Normal landing gear extension and retraction. GROUND
Refer to the Landing Gear subpart of this section.

‡ Nose wheel steering. TAKEOFF
Refer to the Landing Emergency subpart of this section.

FIRE/SMK
‡ Normal brake supply.
NORM Refer to Hydraulics subpart of this section.
PRES/OXY
‡ 1RUPDO ÀDS H[WHQVLRQ DQG UHWUDFWLRQ
Refer to Flap System Failure subpart of this section.
ENG/PROP
‡ +DOI RI WKH K\GUDXOLF SRZHU VXSSOLHG WR WKH ÀLJKW FRQWUROV
Refer to Flight/Airframe Controls System Failure subpart of FUEL
this section.

‡ Normal Aerial Refueling operations; however, the aux system AAR
must be used to operate the reels.

SPEC NOT FOR FLIGHT ELEC
NOTE

With either utility or booster hydraulic system inoperative,
V MCA FDQ EH VLJQL¿FDQWO\ KLJKHU WKDQ WKH FKDUWHG YDOXHV HYD
in (KU)01-75GAJ-1.1.

(End of Procedure) FLT CTRL

1.11.5 BOOSTER HYDRAULIC SYSTEM FAILURE GEAR

Systems lost:
DOR/RMP
PERF ‡ +DOI RI WKH K\GUDXOLF SRZHU VXSSOLHG WR WKH ÀLJKW FRQWUROV

Refer to Flight/Airframe Controls System Failure subpart of JETTISON
this section.

LANDING
NOTE

With either utility or booster hydraulic system inoperative, DITCHING
V MCA FDQ EH VLJQL¿FDQWO\ KLJKHU WKDQ WKH FKDUWHG YDOXHV
in the Performance Manual.

(End of Procedure) BAILOUT

OPER FAULT LG

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