Textron Bell 212 - 50 Hours after Installation of Components

BHT-212-MM-1
5-00-00
Export Classification C, ECCN EAR99
SPECIAL INSPECTIONS
5-24. 50 HOURS AFTER INSTALLATION OF COMPONENTS
DATA REFERENCE INSPECTION TASK DESCRIPTION
INITIAL
MECH OTHER
DATE: __________________W.O. _____________________
FACILITY: __________________________________________
HELICOPTER S/N: ___________________________________
REGISTRY NO.: _____________________________________
TOTAL TIME:_______________________________________
SIGNATURE:________________________________________
NOTE
Accomplish 50 flight hours after installation of
components.
Chapter 53 TAILBOOM
Torque check anti-torque bellcrank support 212-001-706-001/
101 attachment nuts 75 to 95 inch-pounds (8.47 to 10.73 Nm).
Chapter 63 ROTOR BRAKE
1. Torque check brake assembly (caliper) attachment bolts 80
to 100 inch-pounds (9.04 to 11.30 Nm).
2. Torque check brake disc attachment bolts 50 to
70 inch-pounds (5.65 to 7.91 Nm).
26 JUN 2013 Rev. 14 Page 129/130