AD/BELL 47/84 - Frame Stiffening Assembly 660-2001-1 - Inspection

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

Legislation au F2006B04706 Not in force Legislative Instrument

Legislation content

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Bell Helicopter Textron 47 (All Variants) Series Helicopters

 

AD/BELL 47/84 Frame Stiffening Assembly 660-2001-1 - Inspection

Applicability: All models 47G equipped with Soloy turbine conversion. Document:  Soloy Conversions Limited SB 12-660.

Compliance: Within 100 hours time in service after 31 March 1981.


3/81

 

Background:  There is a possibility that the tubes comprising the stiffener assembly may not have received interior treatment.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Interactions

Authorises

All Versions

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.