BHT-212-MM-1
5-00-00
Page 194 Rev. 14 26 JUN 2013
Export Classification C, ECCN EAR99
(8) Tail rotor gearbox
(9) Tail rotor driveshafts
(10) Tail rotor driveshaft hangers
(11) Swashplate and support assembly
(12) Scissors and sleeve assembly and collective
levers
(13) Stabilizer bar assembly
(14) Helicopter structure directly supporting damaged
components identified in previous inspections
c. Check all cowling and doors for proper fit and
alignment. Remove cowling and inspect all attachment fittings.
If significant damage has been found in any area of
airframe, inspection shall be expanded in those
areas until it extends beyond zone of damage.
d. Make a complete inspection, using a 10X magnifying
glass, of pylon support structure for loose or sheared rivets,
cracked brackets, buckled or cracked support angles and webs.
Pay particular attention to pylon mounts attaching points.
e. Make a complete inspection of lift link, lift link
attachment fittings, and lift beam for cracks and other evidence
of damage. Remove lift link and replace with like serviceable
item, if damaged.
f. Remove both pylon dampers, disassemble and check
for internal yielding. Assemble dampers and install if no
evidence of damage exists. Replace with like serviceable item if
any damage is found.
g. Install serviceable mast, transmission assembly, and
main driveshaft assembly. Install removed pylon control
components.
5-50. AFTER HARD LANDING (CONT)
DATA REFERENCE INSPECTION TASK DESCRIPTION
INITIAL
MECH OTHER
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