TM 1–1520–238–T–2
2–5
Table 2–1.
Master Failure Symptom Index (cont)
Failure Symptom
Reference
MOC
AFT FUEL QTY INDICATOR DOES NOT
INDICATE E (REFUELING PANEL: FUEL QTY
SWITCH SET TO OFF)
TM 1–1520–238–T–7
GRAVITY
REFUELING/
DEFUELING
AFT FUEL QTY INDICATOR DOES NOT
INDICATE E (REFUELING PANEL: FUEL QTY
SWITCH SET TO OFF)
TM 1–1520–238–T–7
PRESSURE
REFUELING/
DEFUELING
AFT FUEL QTY INDICATOR DOES NOT
INDICATE SAME FUEL LOAD AS PILOT FUEL
QUANTITY INDICATOR AFT VERTICAL
DISPLAY (REFUELING PANEL: REFUEL
VALVE SWITCH SET TO OPEN)
TM 1–1520–238–T–7
PRESSURE
REFUELING/
DEFUELING
AFT FUEL QTY INDICATOR DOES NOT SHOW
INCREASE DURING PRESSURE REFUELING
TM 1–1520–238–T–7
PRESSURE
REFUELING/
DEFUELING
AFT VERTICAL DISPLAY SCALE ON PILOT
FUEL QUANTITY INDICATOR DOES NOT
SHOW INCREASE (PILOT FUEL PANEL: EXT
TK SWITCH SET TO ON)
TM 1–1520–238–T–7
AUXILIARY FUEL
SYSTEM
AIRCRAFT PHYSICAL DAMAGE IS EVIDENT
(APU OPERATING)
TM 1–1520–238–T–8
AUXILIARY POWER
UNIT
AIRCRAFT SYMBOL DOES NOT MOVE UP AND
DOWN ON FACE OF SAI GYROSPHERE
(PILOT SAI: PULL TO CAGE KNOB ROTATED
CLOCKWISE AND COUNTERCLOCKWISE)
TM 1–1520–238–T–5
ENGINE
INSTRUMENTS
AIR DATA AC OR AIR DATA DC CIRCUIT
BREAKERS DO NOT STAY CLOSED
TM 1–1520–238–T–7
STABILATOR
AIR DATA PROCESSOR NO–GO AFT AVIONICS
BAY APPEARS ON HOD
TM 1–1520–238–T–7
DASE
AIR DATA PROCESSOR NO–GO AFT AVIONICS
BAY APPEARS ON HOD
TM 9–1230–476–20–2
AIR DATA SYSTEM
AIR DOES NOT FLOW THROUGH VENT TUBE
DURING PRESSURE REFUELING
TM 1–1520–238–T–7
PRESSURE
REFUELING/
DEFUELING
