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46-14-02

final rule

Airworthiness Directives; FAIRCHILD Models M- 62A3 and M-62A4 Aircraft

Unsafe Condition: The aluminum alloy cockpit heat control valve box and valve may fail due to corrosion or structural weakness, leading to potential fire hazards or loss of cockpit heating functionality.

Category: aircraft Compliance: Compliance required immediately.

Why matched: Airworthiness Directives; FAIRCHILD Models M- 62A3 and M-62A4 Aircraft

47-07-06

final rule

Airworthiness Directives; Fairchild M-62 Series Aircraft

Unsafe Condition: The forward attachment of the vertical fin may fail due to insufficient reinforcement, leading to structural failure.

Category: aircraft Compliance: at next periodic inspection

Why matched: Airworthiness Directives; Fairchild M-62 Series Aircraft

46-14-01

final rule

Airworthiness Directives; Fairchild Model M- 62C Aircraft

Unsafe Condition: Failure of the engine crankshaft due to improper indexing of the fixed pitch wood propeller.

Category: aircraft

Why matched: Airworthiness Directives; Fairchild Model M- 62C Aircraft

47-07-05

final rule

Airworthiness Directives; Fairchild M-62 Series Aircraft

Unsafe Condition: Foreign objects entering the torque tube could cause failure of the elevator control system.

Category: aircraft Compliance: next periodic inspection

Why matched: Airworthiness Directives; Fairchild M-62 Series Aircraft

Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

43-07-01

final rule

Airworthiness Directives; Fairchild M-62 Series Aircraft

Unsafe Condition: Wood deterioration and weakened glue joints due to moisture accumulation in the wing center-section front and rear spars.

Category: aircraft Compliance: At each periodic inspection

Why matched: Airworthiness Directives; Fairchild M-62 Series Aircraft

48-45-01

final rule

Airworthiness Directives; Fairchild Model M-62 Series Aircraft

Unsafe Condition: Separation of plywood butt plates from wing spar ends and rot in wing spar webs and caps, which could lead to structural failure of the wing spar.

Category: aircraft Compliance: at each annual inspection

Why matched: Airworthiness Directives; Fairchild Model M-62 Series Aircraft

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

47-07-02

final rule

Airworthiness Directives; Fairchild M-62 Series Aircraft

Unsafe Condition: Looseness in elevator hinge attachments to the rear spar of the stabilizer could lead to structural failure of the elevator control system.

Category: aircraft Compliance: at each periodic inspection

Why matched: Airworthiness Directives; Fairchild M-62 Series Aircraft

Technical illustration of an aircraft flight control surface and actuator
Problem area Flight controls

47-07-04

final rule

Airworthiness Directives; Fairchild M-62 Series Aircraft

Unsafe Condition: The control sticks may become disengaged from the socket due to insufficient safetying of the AN393-51 clevis pin, leading to loss of control.

Category: aircraft Compliance: next periodic inspection

Why matched: Airworthiness Directives; Fairchild M-62 Series Aircraft

47-07-03

final rule

Airworthiness Directives; Fairchild M-62 Series Aircraft

Unsafe Condition: Cracks in the wing center section bottom surface extending into the spar flange area, loose strap hinge fittings, missing or improperly attached spar butt plates, checks or cracks in plywood spar w...

Category: aircraft Compliance: Prior to original certification and at each periodic inspection thereafter, and as otherwise noted.

Why matched: Airworthiness Directives; Fairchild M-62 Series Aircraft

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