AD/F28/25 - Cargo Door Latch Fittings - Inspection and Modification

This AD mandates inspection and modification of cargo door latch fittings on affected Fokker F28 series aeroplanes, requiring operators and maintenance organisations to implement the procedures in Fokker SB F28/53-54.

Compliance is compulsory under the Civil Aviation Safety Authority’s Part 39 framework, must be completed before 1 January 1976, and places direct costs and scheduling burdens on operators while enforcement rests with the regulator.

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source Fokker F28 Series Aeroplanes

AD/F28/25 Cargo Door Latch Fittings - Inspection NK

and Modification

Applicability: As detailed in the requirement document. Document: Fokker SB F28/53-54.

Compliance: Before 1 January 1976.

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

Fokker F28 Series Aeroplanes

AD/F28/25 Cargo Door Latch Fittings - Inspection NK

and Modification

Applicability: As detailed in the requirement document. Document: Fokker SB F28/53-54.

Compliance: Before 1 January 1976.

AD/F28/25 - Cargo Door Latch Fittings - Inspection and Modification

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