ARMY
TM 5-6115-612-34
MARINE CORPS TM 6115-34/8
AIR FORCE
TO 35C2-3-471-2
NAVY
AG-320BO-MME-OOO
8-2.
COMBUSTION CHAMBER CASE ASSEMBLY.
(cont)
Table 8-3.
Nondestructive Test Inspection Data - Continued
Type of
Method
*Acceptable
Part Name
Inspection
defects
Retainer,
Flourescent
30 minutes penetration
None
Seal
penetrant
Gear,
Magnetic
8-1500
None
Starter
particle
E-500
(Matched Set)
Gear,
Magnetic
B-1000
None
Pinion Spur
particle
C-500
(base of gear teeth)
Shaft,
Flourescent
30 minutes pentration
None
Generator
penetrant
Shouldered
Wheel,
Fluorescent
30 minutes penetration
None
Compressor
penetrant
Wheel,
Fluorescent
30 minutes penetration
None
Turbine
penetrant
(Recommended penetrant is MIL-I-25135, Type I Method B.)
*Interpret defects in accordance with MIL-I-6866 amd MIL-I-6868.
8-13
