Document ID: chunk:federal_register_of_legislation:F2006B05006:body:0
Version: federal_register_of_legislation:F2006B05006
Segment Type: other
Provision Reference: 
Character Range: 0–927

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.