AD/CESSNA 170/30 - Wing Flap Actuator Ball Nut Assemblies

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Legislation au F2006B04962 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 170, 172, F172, FR172 and 175 Series Aeroplanes

 

AD/CESSNA 170/30 Wing Flap Actuator Ball Nut Assemblies 1/77

Applicability: Model 172 and R172 with S/Nos. as detailed in Cessna Service Letter SE76-25. Requirement:               1. Inspect P/N C301002-0101 wing flap actuator for date stamp code as detailed in

Cessna SL SE76-25.

 

2.    If the date stamp code on the actuator is OH, HH, WH or ZH, install a placard near the flap control which reads:

 

“FLAP EXTENSION PROHIBITED”.

 

Note: This placard may be removed when the Paragraph 3 requirement is satisfied.

 

3.    Replace affected wing flap actuator ball nut assemblies in accordance with Cessna SL SE76-25.

 

Compliance: Paragraphs 1 and 2 - Before further flight after 28 January 1977.

 

Paragraph 3 - Within 100 hours time in service after 28 January 1977.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Federal Register of Legislative Instruments F2006B04962

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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.