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TB 1-1520-237-23-1
Table 1. Approved Nondestructive Test Inspection Components/Assemblies.
(1)
(2)
(3)
(4)
(5)
(6)
PROCEDURE
COMPONENT/ASSEMBLY
INSPECT
MAINTENANCE CATEGORY
INSPECTION
REMARKS
NUMBER
FOR
EQUIPMENT
AVUM
AVIM
DEPOT
REQUIRE
MENTS -
6.14
Pilot Collective Stick
Cracks
003
Backup
Bellcrank
001
6.15
Ferrous Connecting
Cracks
002
Links, Rod Ends,
Clevises, Levers, and
Attaching Parts
6.16
Nonferrous Connecting
Cracks
003
Links, Rod Ends,
Clevises, Levers, and
Attaching Parts
6.17
Swashplate Links
Cracks
002
6.18
Walking Beam
Cracks
002
6.19
Forward Bellcrank
Cracks
002
6.20
Lateral Bellcrank
Cracks
002
6.21
Aft Bellcrank
Cracks
002
6.22
Hydraulic/Pneumatic
Cracks
001
System Components
6.23
Ferrous Bolts Contained
Cracks
002
Within the Flight Control
System
6.24
Nonferrous Bolts Con-
Cracks
001
tained Within the Flight
Control System
5.
Points of Contact.
a.
Technical point of contact for this TB is Mr. Wayne Suchman, AGSE-PM, AMSAT-D-WAG, DSN 693-1924
or commercial (314)263-1924, e-mail: wsuchman@emh4.wsmd.stl.army.mil.
b.
Nondestructive Test Inspection technical point of contact for this TB is Mr. Scott Huddleston, DSN 693-1923
or commercial (314)263-1923, e-mail: shuddles@emh4.wsmd.stl.army.mil.
6.
Reporting of Errors and Recommending Improvements . You can help improve this TB. If you find any
mistakes or if you know of a way to improve these procedures, please let us know. Mail your letter or DA Form 2028
(Recommended Changes to Publications and Blank Forms) directly to: Commander, US Army Aviation and Troop
Command, ATTN: AMSAT-I-MP, 4300 Goodfellow Blvd., St. Louis, MO 63120-1798. A reply will be furnished to you.
You may also submit your recommended changes by E-mail directly to <mpmt%avma28@st-louis-emh7.army.mil>. A
reply will be furnished directly to you. Instructions for sending an electronic 2028 may be found at the back of this
manual.
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