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Figure 4-3. LAI in Pilots Instrument Panel
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TM-9-1270-219-13-P Fire and Flight Air Data Subsystem Helicopter Armament: XM 143 PN 03-004-02 Manual
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Table 4-2 ADS Troubleshooting
TM
9-1270-219-13&P
Section
Il.
PREVENTIVE
MAINTENANCE
CHECKS
AND
SERVICES
(PMCS)
c. If your equipment fails to operate. Troubleshoot
as
4-10. General. Table 4-1 contains the procedures for PMCS.
d e s c r i b e d in Section III. Report any deficiencies
using the proper forms (see TM 38-750).
a. Before
operation. Perform
your
'before'
(B)
PMCS.
d. The Item No. column of Table 4-1 will be used as
source
of
item
numbers
for
the
´TM
Number´
c o l u m n on DA Form 2404, Equipment Inspection
b. A f t e r o p e r a t i o n . Be sure to perform your ´after´
and
Maintenance
Worksheet,
in
recording
the
(A) PMCS.
results of PMCS.
Table 4-1. Preventive Maintenance Checks and Services
A - After
B - Before
Equipment will be
Items to be
B
A
Item
Procedures
Reported not ready/
Inspected
No.
Available if:
AADS damaged
AADS
Inspect for any
1
sign of damage
S e n s o r Installation damaged
Sensor Installation
Inspect for any
2
sign of damage
AADS gimbal
Swivelling
rotation
Check that
3
restricted
swivelling
probe
r o t a t e s freely
Mounting bolts or
Check that
4
AADS mounting
s a f e t y wire damaged
bolts and securing
electrical and
safety wire
pressure
connectors
are undamaged
F r o n t panel components
EPU Front Panel
Check that
5
damaged
s w i t c h e s , lamps,
electrical and
pressure
c o n n e c t o r s are
undamaged
Front panel glass
Check that glass is
LAI Front Panel
6
damaged
undamaged
Section
Ill.
TROUBLESHOOTING
system is reported. For complete wiring interface refer
4-11. Air Data Subsystem Troubleshooting Procedure.
TM 55-1520-236-23 or TM 55-1520-239-23.
a. The ADS will be subjected to the troubleshooting
procedures listed in Table 4-2 whenever a fault in the

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