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48-32-01

final rule

Airworthiness Directives; Timm Models N2T and PT-220-C Aircraft

Unsafe Condition: Throttle quadrants pulling off the fuselage skin to which they were glued and nailed during manufacture.

Category: aircraft Compliance: Reinforcements must be installed not later than January 1, 1949.

Why matched: Airworthiness Directives; Timm Models N2T and PT-220-C Aircraft

Technical illustration of a riveted aircraft structural panel and frame
Problem area Airframe structure
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