Textron Bell 206L3, Maintenance Manual

Page: 65 / 230

BHT-206L3-MM-1
5-00-00
25 FEB 2011 Rev. 16 Page 33 ECCN EAR99
PROGRESSIVE INSPECTIONS
5-18. 100-HOUR AIRFRAME PROGRESSIVE INSPECTION — EVENT NO. 3
DATA REFERENCE INSPECTION TASK DESCRIPTION
INITIAL
MECH OTHER
DATE: __________________W.O. _____________________
FACILITY: __________________________________________
HELICOPTER S/N: ___________________________________
REGISTRY NO.: _____________________________________
TOTAL TIME:_______________________________________
SIGNATURE:_______________ _________________________
ZONE 6 — TAILBOOM
Chapter 11 PLACARDS AND MARKINGS
1. Examine the placards, decals and markings. Ensure they
are readable, correctly applied and in agreement with the
applicable configuration of your helicopter.
Chapter 53 TAILBOOM STRUCTURE
NOTE
In the event that cracks are found during inspection
of tailboom, contact Bell Helicopter Textron, Product
Support Engineering.
1. Examine tailbooms 206-033-004-045 and prior, modified in
accordance with ASB 206L-87-47 as follows:
a. Remove tail rotor driveshaft and gearbox fairings.
Inspect for condition and attachment of fasteners.
b. Remove a sufficient amount of anti-chafing tape to
permit inspection of tailboom skin adjacent to tail rotor driveshaft
cover retention clips aft of horizontal stabilizer, and in area of
double row of rivets attaching tail rotor gearbox support fitting to
tailboom (BS 174).