TM 1–1520–238–T–1
4–16
Change 5
4–2
DASE – INTERACTIVE FD/LS CHECK (cont)
4–2
FD/LS NO–GO
DISPLAY
CORRECTIVE ACTION
LONG ACTUATOR
NO–GO RH XMSN
BAY
Troubleshoot wiring to isolate
fault (TM 1-1520-238-T-7).
If troubleshooting does not
remove NO–GO, replace
longitudinal servoactuator
(TM 1-1520-238-23).
AIR DATA
PROCESSOR NO–GO
AFT AVIONICS BAY
Troubleshoot wiring to isolate
fault (TM 9-1230-476-20-2).
If troubleshooting does not
remove NO–GO, replace air
data processor
(TM 9-1230-476-20-1).
HARS ELECTRONIC
UNIT NO–GO AFT
AVIONICS BAY
Troubleshoot wiring to isolate
fault (TM 11-1520-238-23-2).
If troubleshooting does not
remove NO–GO, replace
HARS electronic unit
(TM 11-1520-238-23-1).
DASE COMPUTER
NO–GO AFT
AVIONICS BAY
Troubleshoot wiring to isolate
fault (TM 1-1520-238-T-7).
If troubleshooting does not
remove NO–GO, replace
DASE computer
(TM 1-1520-238-23).
ROTOR BRAKE
NO–GO PLT
COMPARTMENT
Perform UTILITY
HYDRAULIC SYSTEM –
OPERATIONAL CHECK
(TM 1-1520-238-T-6).
PILOT CYCLIC GRIP
NO–GO PLT
COMPARTMENT
Troubleshoot wiring to isolate
fault (TM 1-1520-238-T-7).
If troubleshooting does not
remove NO–GO, replace pilot
cyclic grip
(TM 1-1520-238-23).
PILOT COLL 2 DCPLR
NO–GO PLT
COMPARTMENT
Troubleshoot wiring to isolate
fault (TM 1-1520-238-T-7).
If troubleshooting does not
remove NO–GO, replace pilot
collective SPAD switch S2
(TM 1-1520-238-23).
