AD/B727/112 Amdt 1 - Fuselage Forward Lower Body Skin

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B02635 In force Legislative Instrument

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Boeing 727 Series Aeroplanes

 

AD/B727/112

Amdt 1


Fuselage Forward Lower Body Skin 7/90

 

Applicability: All Boeing 727-200.

 

Requirement: Action in accordance with Boeing Alert SB 727-53A0203 Rev 1.

 

Note: FAA AD 89-23-13 Amendment 39-6388 refers.

 

Compliance: Prior to 5 December 1989, unless previously accomplished within the last 6 months, and thereafter at intervals not exceeding 12 calendar months until preventive modification is carried out.

 

Background: Country of origin AD. Overseas aircraft found to have cracks 1200 mm long. Initial inspection has found cracks on one local aircraft. Amendment 1 references Revision 1 to the Requirement document. This requires repeat inspections until preventive modification is carried out, deletes specific line numbers and quotes FAA AD.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.