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Textron Bell 212 - 5-46. EACH 24 MONTHS OF FLIGHT CONTROL SYSTEM BOLT OPERATION

Textron Bell 212
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BHT-212-MM-1
5-00-00
26 JUN 2013 Rev. 14 Page 177
Export Classification C, ECCN EAR99
5-46. EACH 24 MONTHS OF FLIGHT CONTROL SYSTEM BOLT OPERATION
DATA REFERENCE INSPECTION TASK DESCRIPTION
INITIAL
MECH OTHER
DATE: __________________W.O. _____________________
FACILITY: __________________________________________
HELICOPTER S/N: ___________________________________
REGISTRY NO.: _____________________________________
TOTAL TIME:_______________________________________
SIGNATURE:________________________________________
NOTE
Accomplish each 24 months of flight control system
bolt operation.
Chapter 67 FLIGHT CONTROL SYSTEM BOLTS
NOTE
Refer to Chapter 4 for retirement life of flight control
system bolts.
— Inspect
1. Remove the following flight control bolts:
a. Two fixed swashplate to right and left cyclic boost tube
bolts P/N 20-057-5-24D.
b. One collective lever to collective boost tube bolt P/N
20-057-5-24D.
c. Three boost tube universal bolts P/N 20-057-24D.
d. Three universal to hydraulic cylinder tube bolts P/N
20-057-5-24D.
e. Two mixing lever to scissors tubes bolts P/N
20-057-5-27D.

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