TM 1-2840-252-23-3
SECTION IV
REMARKS
REFERENCE
CODE
REMARKS/NOTES
A
Functional Test at AVUM - Engine in Airframe
B
Functional Test at AVIM - Engine in METS/FEDS
C
Repairs at AVUM includes minor repair of the engine and minor
repair/replacement of components and accessories
D
Blend Repair
E
Corrosion Control, Pitting
F
Magnetic-Particle Inspection
G
Nicks, Dents, Burrs, Cracks & Distortion
H
Adjust, Engine in Airframe
I
Bleed Band, Ground Idle, Maximum Power, Engine in Airframe
J
O-Rings, Drive Shaft Seal, Solenoid Valve
K
Seals and O-Rings
L
Torque Sensor, Output Shaft, and Signal Conditio er Unit are individually
n
replaceable, but the Output Shaft calibration must be set into the Signal
Conditioner Unit (Refer to TM 1-1520-252-23).
M
Repair is limited to Blend Repair and Seal/O-Ring Replacement
B-20
