TM 1-1520-238-23
2-46.2
Change 2
2.12.
CLASSIFICATION OF FUSELAGE DAMAGE AND TYPES OF REPAIR – continued
Category
Limits
Action
b. Tailboom fuselage skin.
C
Abrasion damage.
Repair by installing 0.032 INCH aluminum
alloy, QQ-A-205/4, T-3, doubler
(TM 1-1500-204-23).
FS370.00
APPROX
3.00
WL 145.5
= EXISTING RIVET
= NEW RIVET
APPROX
3.75
M04-4514-3
E
N
E
N
E
E
E
E
E
E
E
E
E
E
N
N
N
c. Tail Rotor Drive Shaft T355 Fairing Fasteners.
C
Abrasion exceeds 0.010 INCH deep.
Replace plate (para 2.21).
END OF TASK
