AD/B737/94 - Outboard Chords of BS 727 Frame and Stringer 18A

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

Legislation au F2006B02995 Not 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 737 Series Aeroplanes

 

AD/B737/94 Outboard Chords of BS 727 Frame and Stringer 18A 11/95

Applicability: Model 737-100 and 200 series aircraft with line numbers 1 through 999. Requirement:               Action in accordance with the technical requirements of FAA AD 95-12-17 Amdt 39-

9268.

 

Note: Boeing Service Bulletins 737-53-1088 and 737-53A1166 refer.

 

Compliance: As specified in the Requirement Document.

 

Background: The FAA received reports of fatigue cracks in the outboard chord of the frame at BS 727, and in the outboard chord of stringer 18A. This Directive requires on-going repetitive inspections, with terminating action required if cracking is detected.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.