AD/AC/62 - Forward and Aft Inboard Wing Spar Cap Rivets - Inspection and Replacement

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

Legislation au F2006B02121 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

 


Twin Commander (Gulfstream/Rockwell/ Aerocommander 500, 600 and 700) Series Aeroplanes

 

AD/AC/62 Forward and Aft Inboard Wing Spar Cap

Rivets - Inspection and Replacement


4/77

 

Applicability: All models 690, 690A and 690B with S/Nos. 11000 to 11366, 11368, 11369, 11370

and 11371.

 

Document: 1. Rockwell International SB No. 163; or 2. FAA AD 77-03-01 Amend 39-2823.

Compliance: 1. Initially inspect before further flight, unless accomplished in the preceding 25 hours time in service, and thereafter at intervals not exceeding 25 hours time in service until replaced.

 

2. Replace rivets not later than next major inspection after 30 April 1977.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.