TB 1-1670-260-12
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3.1.3.14 If Figure 3 is not incorporated then the following complete inspections must be
performed instead. It should be noted that these inspections would be more manpower
3.1.3.14.1 Hard Landing Inspection per TM 1-1520-238-23-1
3.1.3.14.2 The 10 hr /14 day PMS per TM 1-1520-238-PMS
3.1.3.15 Add the following to the non-flyable damage classification in Introduction,
paragraph 1.(1),:
3.1.3.15.1 Main rotor base.
3.1.3.15.2 Main rotor support truss legs.
3.1.3.15.3 Main rotor support truss leg attachments.
3.1.3.15.4 Frames at FS 176 and FS 230.
Figure 3. Post-recovery inspection list prior to
release for flight
Structure
Inspection Type
Criteria
Corrective action
Droop stop hardware
Visual
Bent or broken pieces
Replace
Hub lower shoe
Visual
Abrasion
Replace or repair per
DMWR 1-1615-312,
paragraph 4-17.5
Landing gear
Hard Landing
Hard landing evidence
Replace or repair per
DMWR 1-1620-248
Tailboom
Visual
Damage or abrasion
Repair per TM 1-1500-
204-23-10 Vol. 10
Tailboom
Internal Visual
Cracks in #4,6,&7
Repair per TM 1-1500-
(if tail sling is improperly
stringers between FS
204-23-10 Vol. 10
rigged)
436.5 and 450
Fuselage between and
Visual
Cracks or deformation.
Repair per TM 1-1500-
including frames at FS
Missing, sheared, or
204-23-10 Vol. 10
176 and FS 230 (include
loose fasteners
skin/stringers, deck and
struts
M/R blade (if recovered
Visual and
Damage, cracks,
Repair or replace per
w/blades on)
cheesecloth*
abrasion
DMWR 55-1615-313
Main Rotor blade
Visual
Damage, cracks,
Repair per TM 1-1500-
tiedown points
abrasion
5