BHT-206A/B-SERIES-MM-1
5-00-00
Page 160 Rev. 14 30 APR 2013
Export Classification C, ECCN EAR99
15. If damage in any inspection requirements of step 9 through
step 13 is noted, the main rotor hub assembly must be
overhauled in accordance with the conditional inspection
criteria.
16. Inspect mast for indentions caused by static stop(s). If
mast is damaged from an excessively hard contact with main
rotor static stop, scrap mast pole and remove and overhaul the
following components to ensure airworthiness:
Chapter 62 a. Main rotor hub assembly in accordance with the
conditional inspection criteria.
Chapter 63 b. Transmission assembly
c. Main driveshaft assembly
d. Isolation mount
e. Remove main rotor blades and send to a Bell Helicopter
Textron approved blade repair facility for evaluation.
Chapter 53 17. Inspect engine mounts at fuselage attachment points for
cracks.
18. Inspect tailboom for contact with main rotor blades. If
damage is found, accomplish main rotor sudden stoppage
inspection.
Chapter 65 19. Inspect oil cooler blower shaft for straightness, and
impeller and shaft assembly for balance.
Chapter 64 20. Inspect tail rotor blades for damage. If damage is found,
accomplish tail rotor sudden stoppage inspection.
Chapter 32 and
Chapter 53
21. Inspect tail skid tube and mounting for damage. Inspect
tailboom internally and externally for cracks, distortion, and
sheared or loose rivets. Inspect the tailboom attachment points
for elongated bolt holes and damaged structure.
22. Inspect fuel and oil system for damage. During ground run,
check fuel and oil systems for leaks.
5-52. HARD LANDING (CONT)
DATA REFERENCE INSPECTION TASK DESCRIPTION
INITIAL
MECH OTHER
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