Fairchild Industries, Inc. Airworthiness Directives

4 ADs indexed for Fairchild Industries, Inc. aircraft.

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90-08-10

final rule

Airworthiness Directives; FAIRCHILD INDUSTRIES, INC. Model F-27 and FH-227 Series Airplanes

Unsafe Condition: Reduced structural capability of the wing due to undetected fatigue cracks in the wing outer panel upper surface stringer splice fittings.

Effective: May 14, 1990 Category: aircraft Compliance: Within 25 hours time-in-service after August 21, 1989 (the effective date of AD 89-15-01, Amendme...

Why matched: Airworthiness Directives; FAIRCHILD INDUSTRIES, INC. Model F-27 and FH-227 Series Airplanes

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

46-40-01

final rule

Airworthiness Directives; Fairchild Model 24 Series Aircraft

Unsafe Condition: Engine failure due to air-lock in the fuel system when fuel is fed from more than one tank at a time.

Effective: Dec 31, 1946 Category: aircraft Compliance: immediately

Why matched: Airworthiness Directives; Fairchild Model 24 Series Aircraft

46-40-02

final rule

Airworthiness Directives; Fairchild Models 22 and 24 Series Aircraft

Unsafe Condition: Failure of the oleo tube reinforcement could result in structural failure of the oleo tube at the piston end, leading to loss of aircraft control.

Category: aircraft Compliance: next 100-hour inspection

Why matched: Airworthiness Directives; Fairchild Models 22 and 24 Series Aircraft

46-21-01

final rule

Airworthiness Directives; Fairchild Model 24 Series Aircraft

Unsafe Condition: Freezing of the upper and lower universal joints on the landing gear oleo shock struts.

Category: aircraft Compliance: next periodic inspection

Why matched: Airworthiness Directives; Fairchild Model 24 Series Aircraft

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

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