TM 1–1520–238–T–2
(2–123 blank)/2–124
Change 5
Table 2–1.
Master Failure Symptom Index (cont)
Failure Symptom
Reference
MOC
NITROGEN INERT CIRCUIT BREAKER (CB94)
DOES NOT STAY CLOSED
TM 1–1520–238–T–7
NITROGEN
INERTING SYSTEM
NITROGEN INERT MONITOR INDICATOR IS
NOT BLACK
TM 1–1520–238–T–7
NITROGEN
INERTING SYSTEM
NITROGEN INERT MONITOR INDICATOR IS
NOT BLACK AND WHITE (FAIL) (NITROGEN
INERT MONITOR INDICATOR: PRESS TO
TEST SWITCH PRESSED FOR 10 SECONDS)
TM 1–1520–238–T–7
NITROGEN
INERTING SYSTEM
NIU IS NOT OPERATING (UTILITY RECEPTACLE
CIRCUIT BREAKER BOX: NITROGEN INERT
CIRCUIT BREAKER CLOSED)
TM 1–1520–238–T–7
NITROGEN
INERTING SYSTEM
NO DTC MESSAGE REMAINS WITH DTC
INSTALLED (ADD)
TM 1–1520–238–T–3
DTU (ADD)
NOE/APRCH SWITCH DISENGAGES OR STAB
INDICATORS DO NOT INDICATE 25 2
TM 1–1520–238–T–7
STABILATOR
NO–GO INDICATOR LIGHTS AT THE END OF
THE BITE TEST (PILOT INSTRUMENT PANEL:
JAM/TEST/GO/NO–GO INDICATOR
MOMENTARILY PRESSED AND RELEASED)
TM 11–1520–238–23–2
RADAR JAMMER
SYSTEM
AN/ALQ–136
NP FLUCTUATES (PILOT POWER QUADRANT:
ENGINE NO 1 PWR LEVER SET TO
LOCKOUT THEN MOVED BETWEEN FLY AND
IDLE)
TM 1–1520–238–T–4
POWER PLANTS
(ENGINE 1)
NP FLUCTUATES (PILOT POWER QUADRANT:
ENGINE NO 2 PWR LEVER SET TO
LOCKOUT THEN MOVED BETWEEN FLY AND
IDLE)
TM 1–1520–238–T–4
POWER PLANTS
(ENGINE 2)
NR RPM% DIGITAL READOUT 2 DOES NOT
STABILIZE AT 22% MINIMUM (PILOT POWER
QUADRANT: ENG START NO 1 SWITCH SET
TO IGN OVRD)
TM 1–1520–238–T–5
PRESSURIZED AIR
SYSTEM
