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Textron Bell 206A Series - Page 95

Textron Bell 206A Series
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BHT-206A/B-SERIES-MM-1
5-00-00
30 APR 2013 Rev. 14 Page 65
Export Classification C, ECCN EAR99
PROGRESSIVE INSPECTIONS
5-23. 300-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 4 — POWER PLANT
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.
AIRFRAME (POWER PLANT AREA)
Chapter 71 1. Examine firewalls for condition and security.
2. Examine engine cowlings and doors for condition and
security. Using a bright light and mirror, inspect exposed upper
and lower edges of the joints between aluminum longerons and
titanium engine pan. Edge of sealant coating should be visible.
No indications of corrosion or cracks are acceptable.
3. Examine engine pan area for evidence of loose fasteners
and damage. Restore cracked or missing sealant form engine
pan.
4. Examine engine pan drains. Make sure that they are not
clogged.
Chapter 28 5. Examine airframe fuel filter assembly for evidence of
leakage and security, if installed.

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