Table 1. Approved Nondestructive Test Inspection Components/Assemblies. (CONT)

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 -

5.17

Engine Load Demand

Cracks

001

Control Cable Support

5.18

Engine Air Inlet "V"

Cracks

001

Band Clamp

5.19

Starter Flange

Cracks

003

5.20

Engine Shroud

Cracks

001

5.21

Engine Load Demand

Cracks

003

Spindle Bellcrank

Support

5.22

Engine Components

Cracks

001

6.2

Toe Pedal Actuator

Cracks

001

6.3

Toe Pedal Assembly

Cracks

003

Backup

001

6.4

Yaw Pedal Support

Cracks

002

Shaft

6.5

Yaw Pedal Brake

Cracks

003

Cylinder Supports

6.6

Pedal Adjuster Arms

Cracks

003

Backup

and Link

001

6.7

Pilot/Copilot Cyclic and

Cracks

003

Backup

Collective Stick Socket

001

6.8

Collective Boost and

Cracks

002

Yaw Boost Servo Input/

Output Piston Shafts

and Cylinders

6.9

Yaw/Pitch Coupling Link

Cracks

003

6.10

Ferrous Flight Control

Cracks

002

System Push-Pull Rods

6.11

Nonferrous Flight Con-

Cracks

003

trol System Push-Pull

Rods

6.12

Pilot Collective Stick

Cracks

003

Bellcrank Support

6.13

Pilot/Copilot Collective

Cracks

003

Backup

Stick Support

001