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![]() TM 9-1270-219-13&P 
insulation, 
broken 
wires, 
kinks, 
or 
sharp 
(6) Painted surfaces must be free of bare spots. 
bends. 
(7) Operating controls must function smoothly. 
Materiel must be free of burrs, particularly 
(3) 
those on functional surfaces. 
(8) Identification plates must be present and 
secure. 
(4) 
Parts must not be cracked, bent, distorted, 
or damaged, and must be free of detrimental 
components for 
improper 
wear. 
(9) 
Inspect 
electrical 
functions, 
physical 
damage, 
and 
missing 
parts. 
Rivets must be tight. 
(5) 
Section 
III. 
FUNCTIONAL 
TESTS 
F u n c t i o n a l tests as specified in this section will 
( 2 ) Functional Tests 
be performed on the AADS or LAI to confirm a fault 
Angular Outputs Accuracy Test 
reported 
by 
AVUM 
level 
and 
on 
the 
EPU 
as 
a 
final 
(a) 
inspection 
after 
troubleshooting. 
An 
EPU 
failing 
any 
test 
will be subjected to the troubleshooting procedure specified 
Heater Test 
(b) 
i n Section IV. An AADS or an LAI failing any test will be 
returned 
to 
Depot. 
Before 
starting 
the 
test 
procedure, 
(c) 
T e m p e r a t u r e Sensor Initial Check 
verify the performance of the tester, Pitot Static Systems, 
in accordance with TO 33D-2-6-9-11. 
(d) 
Static Pressure Leak Test 
(e) 
5-4. Testing of the Airspeed and Direction Sensor. 
Static Pressure-path Flow Test 
a. T e s t 
R e q u i r e m e n t s . To confirm a fault reported 
(f) 
Pitot Pressure Leak Test 
by AVUM the AADS will be subjected to the following 
t e s t s . Any AADS which fails any test will be returned to 
Pitot Pressure-path Flow Test 
(g) 
Depot for repair. 
Temperature Sensor Resistance Test 
(h) 
( 1 ) Preliminary Tests 
(a) Bonding Resistance Test 
b. T e s t E q u i p m e n t R e q u i r e d 
Nomenclature 
Part No. 
NSN 
Test Station ADS (LRU) 
95-112-02 
4931-01-074-3322 
MB-1A 
Tester, Pitot Static Systems 
Voltmeter, Digital 
1430-00-366-8753 
8125A 
AN/USM 
233 
Stopwatch 
CG-S-764-T1-C2 
60SK6240 
C a p a c i t y Tank 
(Local 
Manufacture) 
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