BHT-212-MM-1
5-00-00
Export Classification C, ECCN EAR99
CONDITIONAL INSPECTIONS
5-49. CONDITION INSPECTION
1. Perform applicable conditional inspection of
helicopter after hard landing, after blade strike or other
rotating system torque spike, overspeed, overtorque,
compressor stall or surge, lightning strikes, and after
reduction (combining) gearbox clutch
nonengagement, misengagement, or in-flight slippage
(paragraph 5-50 through paragraph 5-56).
2. If overhaul evaluation is specified, complete both
the conditional inspection and normal inspection
procedures (as applicable) for that component listed in
BHT-212-CR&O manual.
3. If applicable conditional inspection does not
provide complete information on a specific type of
incident or if any doubt exists as to the serviceability of
the helicopter of related components, contact:
Product Support Engineering
12800 rue de l’Avenir
Mirabel, Quebec J7J 1R4
Fax: (450) 433-0272
Tel: (450) 437-6201or
800-363-8028 (U.S./Canada)
E-mail: psemedium@bh.com
26 JUN 2013 Rev. 14 Page 189/190
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