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Table 1-7. Air Data Subsystem Interface continued.
Up
TM-9-1270-219-13-P Fire and Flight Air Data Subsystem Helicopter Armament: XM 143 PN 03-004-02 Manual
Next
Table 1-10. AVIM Tools and Test Equipment.
TM 9-1270-219-13&P
Table 1-8. Helicopter Installation Details continued.
Helicopter
Installation
Box No/
LRU/
Location
Connector
Cable
Control
Switch No.
AADS
Sensor Installation
Right Hand Side
18A2J1
18A2
18A2P1
of Cockpit
Pilots Panel
18A3P1
18A3J1
LAI
18A3
AADS
ECS Control
--
--
10S1
Heater
Panel
1-21. Special Tools and Equipment.
Table 1-9. AVUM Test Equipment.
Part Number
NSN
Nomenclature
Function
T o leak test ADS pitot-static plumbing after
4920-00-
MB-1A
Tester, Pitot
installation.
580-2303
S t a t i c Systems
Provides the necessary pitot static adapters
Kit,
Pneumatic
901488
to
accomplish
interface
between
either
the
EPU
or
AADS
and
the
CGSE
tester,
Pitot Static Systems.
Table 1-10. AVIM Tools and Test Equipment.
Function
NSN
Part Number
Nomenclature
4931-01-
95-112-02
Test Station, ADS
074-3322
(LRU)
Consisting of:
P e r f o r m a n c e verification of the ADS LRUs
Test Set, ADS
95-109-02
(1)
(LRU)
and isolating faults in the EPU to SRU Level.
1-31, 1-32
Provides a fixed datum and mechanical
Fixture,
AADS
99-265-02
(2)
reference to facilitate AADS angle resolver
(Checking)
o u t p u t alignment checks.
99-245-01
Connects EPU under test to Pressure Test
(3)
Pneumatic
Assembly
Set. Provides the necessary pitot static
adapters
to
accomplish
interface
between
either the EPU or AADS and the CGSE
Tester, Pitot Static Systems.
6625-00-
For current measurement.
AN/USM
223
999-7465

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