Page 364 - (KU)01-75GAJ-1.5 - Change 1

INTRO

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

1.10.7.7 R PNL DATA BUS FAIL*
ACAWS
Condition:

Both channels of the data bus have failed. Failure will be preceded by GROUND
an MC failure.

Associated ACAWS: TAKEOFF
‡ MC 1 (or 2) FAIL (C)

A. Potential Mission Impacts..................................................... Review FIRE/SMK
NORM ‡ Failed Components:

MC 1 (or 2) PRES/OXY
NOT FOR FLIGHT
CNBP
‡ The following copilot panels will be inoperative; use pilot panels ENG/PROP
as required:
AMU FUEL
REF/MODE
Mode Annunciator
HEADING COURSE AAR
‡ The following panels will be inoperative; control respective
SPEC system via CNI-MU soft panel selection: ELEC
AERIAL DELIVERY
AIR COND HYD
APU
COPILOT LIGHTING
ELECTRICAL FLT CTRL
ENGINE START 1 and 4
EXTERIOR LIGHTING GEAR
LANDING GEAR and LIGHTS
OIL COOLER
RADAR CONTROL DOR/RMP
PERF REFUEL CONTROL

‡ As-is Components (components which will continue to operate JETTISON
in their current state, but will not respond to control/switch panel
operation):
Copilot ICS CONTROL panel LANDING

Augmented Crew ICS CONTROL and MON panels
B. Fault Log............................................................................... Review DITCHING
MC 1 OR 2, ICS B

PANELS: BAILOUT
CP REF SET, CP HDG/CRS, CP LTS, CP AMU
OPER CP MODE ANNUN, CP ICS CNTL, ELECT, A/C FAULT LG

1 -324 Use, copying and/or disclosure is
governed by the statement on the
BACK title page of this document. CHARTS