BHT-212-MM-1
5-00-00
26 JUN 2013 Rev. 14 Page 81
Export Classification C, ECCN EAR99
The following inspection (step c and step d) is for
helicopters equipped with escape panels which may
be identified by a rotating handle installed below the
passenger door windows. The handle is labeled
EMERGENCY RELEASE PULL COVER TURN
LEFT AND PUSH.
c. Inspect passenger door emergency egress panel pins
and mechanisms for wear, corrosion, operation, and security.
d. Perform operational check of passenger door escape
panels.
e. Passenger door window retainers and fillers (if
applicable) for damage.
f. Nose, electrical, and equipment compartment access
doors for corrosion, damage, distortion, and positive locking
mechanisms.
g. Inspect heated windshield, if installed, for condition and
proper operation.
Chapter 67 4. Collective flight control actuator.
a. Universal bearings for looseness.
b. Input lever bearings and bolts for wear and looseness.
c. Fasteners attaching cylinder lower supports to structure
for looseness.
d. Cylinder lower bearings for looseness.
e. Actuator assembly for damage and leakage.
f. Cylinder extension tube for condition and security.
g. Actuator linkage, balance spring, and bracket for wear
and security.
5-13. 300 HOURS — PART B (CONT)
DATA REFERENCE INSPECTION TASK DESCRIPTION
INITIAL
MECH OTHER
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