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Table 2–1. Master Failure Symptom Index (cont) | Up
TM-1-1520-238-T-2 Army Model AH-64 Helicopter (NSN
1520-01-106-9519) (EIC: RHA) Master Failure Symptom Index Manual | Next
Table 2–1. Master Failure Symptom Index (cont) |
TM 1–1520–238–T–2
2–22
Table 2–1.
Master Failure Symptom Index (cont)
Failure Symptom
MOC
Reference
AUDIO WARNING TONE IS NOT PRESENT IN
EITHER HEADSET AND ENGINE 1 OUT AND
ENGINE 2 OUT INDICATORS ARE NOT
LIGHTED (PILOT CENTER CIRCUIT
BREAKER PANEL: ENG WARN CIRCUIT
BREAKER CYCLED OPEN AND CLOSED)
TM 11–1520–238–23–2
INTEGRATED AUDIO
WARNING SYSTEM
(IAWS)
AUDIO WARNING TONE IS NOT PRESENT IN
PILOT HEADSET (PILOT AFT CIRCUIT
BREAKER PANEL: STAB AUTO AC CIRCUIT
BREAKER CYCLED OPEN AND CLOSED)
TM 11–1520–238–23–2
INTEGRATED AUDIO
WARNING SYSTEM
(IAWS)
AUDIO WARNING TONE IS NOT PRESENT IN
PILOT HEADSET WITH ENGINE 1 OUT AND
ENGINE 2 OUT INDICATORS LIGHTED
(PILOT CENTER CIRCUIT BREAKER PANEL:
ENG WARN CIRCUIT BREAKER CYCLED
OPEN AND CLOSED)
TM 11–1520–238–23–2
INTEGRATED AUDIO
WARNING SYSTEM
(IAWS)
AUDIO WARNING TONE IS NOT SILENCED
(PILOT COLLECTIVE STICK: RESET SWITCH
PRESSED)
TM 11–1520–238–23–2
INTEGRATED AUDIO
WARNING SYSTEM
(IAWS)
AUX/ANTI–ICE PANEL EDGE–LIGHT DOES NOT
BRIGHTEN (CPG INTR LT PANEL: L CSL
CONTROL ROTATED TO BRT)
TM 1–1520–238–T–8
CANOPY DEFOG
AND ANTI–ICE
AUXILIARY FUEL TANK PRESSURE CONTROL
VALVE DOES NOT OPEN
TM 1–1520–238–T–7
AUXILIARY FUEL
SYSTEM
AUX PWR INDICATOR DOES NOT LIGHT (PILOT
DIM/TEST PANEL: DGT OFF/ NORM/TST
SWITCH HELD AT TST
TM 1–1520–238–T–5
ENGINE
INSTRUMENTS
AUX PWR INDICATOR DOES NOT LIGHT (PILOT
DIM/TEST PANEL: DGT OFF/ NORM/TST SET
TO NORM AND MANUAL DIM CONTROL SET
TO MIDPOSITION)
TM 1–1520–238–T–5
ENGINE
INSTRUMENTS
AUX PWR INDICATOR LIGHTS (PILOT
DIM/TEST PANEL: DGT OFF/ NORM/TST SET
TO NORM AND MANUAL DIM CONTROL SET
TO MIDPOSITION)
TM 1–1520–238–T–5
ENGINE
INSTRUMENTS
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