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2006-12-07

final rule

Airworthiness Directives; Engine Components Inc. (ECi) Reciprocating Engine Cylinder Assemblies

Unsafe Condition: Cracks in the cylinder assemblies and possible engine failure caused by separation of a cylinder head.

Effective: Jul 11, 2006 Category: engine Compliance: Before further flight

Why matched: Airworthiness Directives; Engine Components Inc. (ECi) Reciprocating Engine Cylinder Assemblies

Technical illustration of an aircraft turbine engine assembly
Problem area Engine

79-07-02

final rule

Airworthiness Directives; ESB WISCO, INCORPORATED: Applies To Those Batteries Manufactured During December 1978, January and February 1979

Unsafe Condition: The Exide AC 78M and Willard W 78M batteries manufactured between December 1978 and February 1979, identified by N-8, A-9, or B-9 stamped on terminal posts, may fail due to internal short circuits ...

Effective: Apr 3, 1979 Category: appliance Compliance: before next flight

Why matched: Airworthiness Directives; ESB WISCO, INCORPORATED: Applies To Those Batteries Manufactured During December 1978, January and February 1979

78-20-06

final rule

Airworthiness Directives; Aircraft Parts and Development Corporation Models A-9, A-9A, and A-9B Airplanes

Unsafe Condition: Failure of the main carry-through tube, P/N 11013, due to corrosion from exposure to corrosive chemicals in airplanes equipped with the large hopper.

Effective: Dec 8, 1978 Category: aircraft Compliance: within the next 25 hours' time in service after the effective date of this AD except that aircraf...

Why matched: Airworthiness Directives; Aircraft Parts and Development Corporation Models A-9, A-9A, and A-9B Airplanes

73-22-02

final rule

Airworthiness Directives; Aircraft Parts and Development Corp Models A-9, A- 9A, and A-9B Aircraft

Unsafe Condition: Water accumulation in the wing lift struts due to insufficient 360-degree fillet welds on both sides of the struts at P/N 10671 eye fittings, leading to corrosion and structural deterioration.

Effective: Nov 20, 1973 Category: aircraft Compliance: within the next 100 hours' time in service after the effective date of this AD

Why matched: Airworthiness Directives; Aircraft Parts and Development Corp Models A-9, A- 9A, and A-9B Aircraft

64-02-03

final rule

Airworthiness Directives; Callair Models A-5 and A-6 Aircraft

Unsafe Condition: Failures of the front attaching tube of the horizontal stabilizer due to cracks in the area where the tube attaches to the fuselage carry through member and around the horizontal tail fixed handle ...

Effective: Jan 17, 1964 Category: aircraft Compliance: Within 25 hours' time in service after the effective date of this AD

Why matched: Airworthiness Directives; Callair Models A-5 and A-6 Aircraft

60-07-03

final rule

Airworthiness Directives; Callair Models A-4, A-5 , and A-6 Aircraft

Unsafe Condition: Cracks and separation of the lower diagonal brace member on the engine mount in the area of the gusset plates at the ends of the members.

Effective: May 15, 1960 Category: aircraft Compliance: Not later than May 15, 1960, and at each 50 hours' time in service thereafter.

Why matched: Airworthiness Directives; Callair Models A-4, A-5 , and A-6 Aircraft

Technical illustration of an aircraft turbine engine assembly
Problem area Engine