BHT-206A/B-SERIES-MM-1
5-00-00
30 APR 2013 Rev. 14 Page 37
Export Classification C, ECCN EAR99
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
In the event that cracks are found during inspection
of tailboom, contact Product Support Engineering.
1. Clean entire tailboom taking particular care to remove all
grime and dirt.
2. Remove tail rotor driveshaft and gearbox fairings. Inspect
for condition and attachment of fasteners.
Chapter 53 3. Examine entire tailboom for cracks, dents, deformation,
waviness, working rivets, and chafing between tailboom skin
and fairing. Pay particular attention to the left side upper
quadrant of the tailboom. Also pay particular attention to the
rivets attaching the tail rotor gearbox support to the tailboom.
BHT-206-SRM 4. Replace any loose or working rivets found.
To Next Page
Loading...
Need help?
General
