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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 -
3.12
Tail Rotor Gearbox In-
Cracks
001
ner/Outer Split Cones
4.2
Airframe Skin, Panels,
Cracks
003
Doors, Covers, and
Fairings - Metal
4.3
Honeycomb and
Voids
005
Composite Structures
4.4
Fluid in Honeycomb
Fluid
006
Core Panels and
Structures
4.5
Vibration Absorber
Cracks
002
Springs
4.6
Vibration Absorber
Cracks
003
Structural Fittings
4.7
Roll Vibration Absorber
Cracks
001
4.8
Aluminum Structural
Cracks
003
Beams and Frames
4.9
Pilot/Copilot Seat
Cracks
002
Midframe Support
4.10
Troop/Cargo Door
Cracks
003
Upper Track
4.11
Gunner's Window
Cracks
003
Lower Track
4.12
Gunner's Window
Cracks
003
Upper Track
4.13
Troop/Cargo Door
Cracks
003
Lower Track
4.14
Oil Cooler Compartment
Cracks
001
Access Door
4.15
Tail Pylon Attach Fitting
Cracks
003
4.16
Tail Rotor Pylon Skin,
Cracks
003
Station 200
4.17
Tail Rotor Pylon
Cracks
001
Attaching Hardware
4.18
Tail Pylon Lower Step
Cracks
003
4
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