Thompson Aircraft Sales Airworthiness Directives

2 ADs indexed for Thompson Aircraft Sales aircraft.

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61-05-05

final rule

Airworthiness Directives; North American Model T-28A Aircraft

Unsafe Condition: The R-1300-1A engines may experience failure modes requiring incorporation of Change 53 of T.O. 2R-R1300-5, fuel pump overhauls, hydraulic pump overhauls, propeller inspections and removal, and cyl...

Effective: Mar 4, 1961 Category: engine Compliance: Compliance required as indicated.

Why matched: Airworthiness Directives; North American Model T-28A Aircraft

58-22-02

final rule

Airworthiness Directives; North American Model T-28A Aircraft

Unsafe Condition: Fatigue cracks emanating from the bolt holes in the main landing gear trunnion shaft.

Category: aircraft Compliance: every 200 hours

Why matched: Airworthiness Directives; North American Model T-28A Aircraft

Technical illustration of an aircraft landing gear and wheel assembly
Problem area Landing gear

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