TM 1–1520–238–T–2
Change 7
2–141
Table 2–1.
Master Failure Symptom Index (cont)
Failure Symptom
MOC
Reference
PILOT HIGH RPM ROTOR INDICATOR DOES
NOT LIGHT AT 104% NR (ACV) (IN FLIGHT
AUTOROTATION)
TM 1–1520–238–T–4
DRIVE SYSTEM
VIBRATION
PILOT HIGH RPM ROTOR INDICATOR DOES
NOT LIGHT AT 108% NR (ACW) (IN FLIGHT
AUTOROTATION)
TM 1–1520–238–T–4
DRIVE SYSTEM
VIBRATION
PILOT LAT 1 DCPLR NO–GO PLT
COMPARTMENT APPEARS ON HOD
TM 1–1520–238–T–7
DASE
PILOT LAT 2 DCPLR NO–GO PLT
COMPARTMENT APPEARS ON HOD
TM 1–1520–238–T–7
DASE
PILOT LAT LVDT NO–GO PLT COMPARTMENT
APPEARS ON HOD
TM 1–1520–238–T–7
DASE
PILOT LEFT BRAKE IS NOT FIRM OR WHEEL
ASSEMBLY ROTATES (PRESSURE APPLIED)
TM 1–1520–238–T–4
MAIN LANDING
GEAR
PILOT LEFT SSU NO–GO PILOT
COMPARTMENT APPEARS ON HOD
TM 9–1270–221–23
IHADSS
PILOT LONG 1 DCPLR NO–GO PLT
COMPARTMENT APPEARS ON HOD
TM 1–1520–238–T–7
DASE
PILOT LONG 2 DCPLR NO–GO PLT
COMPARTMENT APPEARS ON HOD
TM 1–1520–238–T–7
DASE
PILOT LONG LVDT DCPLR NO–GO PLT
COMPARTMENT APPEARS ON HOD
TM 1–1520–238–T–7
DASE
PILOT LOW RPM ROTOR INDICATOR DOES
NOT LIGHT AT 93% OR LESS (ENGINES 1
AND 2 OPERATING) (PILOT ENG–RTR RPM%
INDICATOR: NP BETWEEN 80% TO 85%)
TM 1–1520–238–T–4
DRIVE SYSTEM
VIBRATION
PILOT LSR DET CIRCUIT BREAKER – DOES
NOT STAY CLOSED (ADP)
TM 11–1520–238–23–2
LASER DETECTING
SET AN/AVR–2A(V)1
(ADP)
PILOT MAGNETIC COMPASS LAMP DOES NOT
LIGHT (PILOT EXT LT/INTR LT PANEL: INST
CONTROL ROTATED TO BRT)
TM 1–1520–238–T–5
FLIGHT
INSTRUMENTS
PILOT MASTER CAUTION/WARNING
INDICATORS ARE LIGHTED (HELICOPTER
SAFED AND BATTERY CONNECTED)
TM 1–1520–238–T–6
BATTERY
