Specific Location (Cont)

Area

Specific L ocation

FWD ROTOR and

Internal and external area of upper fuselage from STA 160.00

PYLON (Right Side)

forward and right of BL 0.0

NOTE

Check all areas and components accessed by the Daily Inspection for corrosion. If

corrosion is discovered, clean up the corroded area and inspect for pits and/or cracks. If

no pits or cracks are found, treat the area in accordance with TM 55-1500-344-23 or

other approved corrosion-preventive practices. If pits or cracks are discovered, contact

the local Field Maintenance Technician for corrective procedures.

NOTE

The terms damage or condition refer to but are not limited to: cracks, distortion, chafing,

abnormal wear, leaks, loose or missing rivets, torn or worn weather stripping and/or

door seals, voids, and missing or illegible stencils.

TM 55-1520-240-PMD