AD/P68/21 - Horizontal Stabilator to Fuselage Frame Attachment - Check Torque

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Legislation au F2006B05349 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

 


Partenavia P68 Series Aeroplanes

 

AD/P68/21 Horizontal Stabilator to Fuselage Frame

Attachment - Check Torque


4/83

 

Applicability: All Partenavia P68, P68B, P68C, P68C-TC and P68 Observer aircraft with S/Nos. 1 to 289 except S/Nos. 234, 256, 259, 269 and 288.

 

Requirement: Check torque AN4-6A bolts securing the horizontal stabilator torque tube brackets to fuselage frame. If necessary retorque to correct torque value 78-83 LB inches.

 

Note: RAI AD 83-3 and Partenavia SB No. 57 refer.

 

Compliance: Before further flight.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.