Weatherly Aircraft Company Airworthiness Directives

6 ADs indexed for Weatherly Aircraft Company aircraft.

Models

Recent ADs

2020-10-03 Recurring

final rule

Airworthiness Directives; Weatherly Aircraft Company

Unsafe Condition: fatigue cracking of the center wing and outer wing spar hinge brackets due to corrosion pitting

Effective: Jun 15, 2020 Category: aircraft Compliance: Within 5 years after the effective date of this AD, or within 5 years after the initial inspectio...

Why matched: Airworthiness Directives; Weatherly Aircraft Company

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

2016-07-11

final rule

Airworthiness Directives; Weatherly Aircraft Company Airplanes

Unsafe Condition: Fatigue cracks in the center wing front spar lower hinge fitting, which could lead to failure of the wing front spar lower hinge fittings and cause the wing to separate, resulting in loss of control.

Effective: Apr 15, 2016 Category: aircraft Compliance: Before further flight

Why matched: Airworthiness Directives; Weatherly Aircraft Company Airplanes

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

96-16-06

final rule

Airworthiness Directives; Weatherly Aviation Company, Inc., Models 620A and 620B Airplanes

Unsafe Condition: Failure of the wing hinge pin, part number 40852-001, at the main wing-to-center section attachment due to insufficient pin length, excessive threaded end depth, or misalignment, which could result...

Effective: Oct 6, 1996 Category: aircraft Compliance: Required prior to further flight after the effective date of this AD, unless already accomplished...

Why matched: Airworthiness Directives; Weatherly Aviation Company, Inc., Models 620A and 620B Airplanes

80-05-01

final rule

Airworthiness Directives; Weatherly Model 201C Series Airplanes

Unsafe Condition: Failure of the aft fuselage attach provisions due to cracking in the P/N 40352-9 and 40352-10 tail cone attach fittings, particularly in the bend radii and bend relief hole areas.

Effective: Mar 3, 1980 Category: aircraft Compliance: Within 50 hours' time in service from the effective date of this AD

Why matched: Airworthiness Directives; Weatherly Model 201C Series Airplanes

76-22-11

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Airworthiness Directives; WEATHERLY AVIATION COMPANY Model 201B and 201C Airplanes

Unsafe Condition: Inadvertent activation of the parking brakes and loss of airplane control during ground operation due to failure to move the parking brake levers to the fully off position.

Effective: Nov 15, 1976 Category: aircraft Compliance: Within the next 200 hours time in service after the effective date of this AD

Why matched: Airworthiness Directives; WEATHERLY AVIATION COMPANY Model 201B and 201C Airplanes

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

76-12-08

final rule

Airworthiness Directives; WEATHERLY AVIATION COMPANY Model 201 Aircraft

Unsafe Condition: Failure of the weld attachment of the landing gear ring P/N 40213-14 to the wrap plate P/N 40213-15 and tube P/N 40213-16, or use of improperly ground bolt heads of AN-5-10A bolts, which may result...

Effective: Jun 21, 1976 Category: aircraft Compliance: within the next 50 hours time in service after the effective date of this AD, unless already acco...

Why matched: Airworthiness Directives; WEATHERLY AVIATION COMPANY Model 201 Aircraft

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

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