Textron Bell 206A Series, Руководство по обслуживанию

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BHT-206A/B-SERIES-MM-1
5-00-00
30 APR 2013 Rev. 14 Page 51 Export Classification C, ECCN EAR99
PROGRESSIVE INSPECTIONS
5-21. 300-HOUR AIRFRAME PROGRESSIVE INSPECTION — EVENT NO. 1
DATA REFERENCE INSPECTION TASK DESCRIPTION
INITIAL
MECH OTHER
DATE: __________________W.O. _____________________
FACILITY: __________________________________________
HELICOPTER S/N: ___________________________________
REGISTRY NO.: ____________ _________________________
TOTAL TIME:_______________________________________
SIGNATURE:_______________ _________________________
ZONE 1 — MAIN ROTOR SYSTEM
Chapter 11 PLACARDS AND MARKINGS
1. Examine the placards, decals, and markings. Make sure
they are readable, correctly applied, and in agreement with the
applicable configuration of your helicopter.
Chapter 62 MAIN ROTOR SYSTEM
1. Verify main rotor flap restraint for freedom of movement,
condition, and security.
2. Examine static stops and mast for evidence of mast
bumping.
3. Remove main rotor blade leading edge erosion protection
tape, if installed.
4. Examine main rotor blades for cleanliness and overall
condition. Examine for cracks, corrosion, and de-bonding of
doublers.
5. Examine leading edge of blades for corrosion and erosion.
Restore contour as necessary.
6. Examine the tip weight cap for corrosion, cracks, erosion,
and deformation.