AD/CESSNA 177/11 Amdt 1 - Stabilator Attachment Angles

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

Legislation au F2006B05006 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

 


Cessna 177 Series Aeroplanes

 

AD/CESSNA 177/11

Amdt 1


Stabilator Attachment Angles 4/72

 

Applicability: Model 177 with S/Nos. 17700001 to 17701164 and Model 177A with S/Nos.

17701165 to 17701370 not fitted with Cessna Kit No. SK 177-11 (Ref. Cessna SB SE70-32).

 

Requirement: 1. Remove the fuselage tail stinger and inspect the stabilator attachment angles P/No.

1712108 for cracking using a dye- penetrant method.

 

2. Modify the stabilator attachments by fitting Cessna Kit No. SK 177-11.

 

Compliance: For para. 1 - Within 50 hours time in service after 29 January 1971 and thereafter at intervals not exceeding 50 hours time in service.

 

For para. 2 - Within 100 hours time in service after 28 April 1972.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.