AD/BELL 205/37 - Main Rotor Hub Fitting Assemblies - Inspection

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

Legislation au F2006B04375 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 205 Series Helicopters

 

AD/BELL 205/37 Main Rotor Hub Fitting Assemblies - Inspection 3/77

Applicability: All models. Document: Bell SB No. 205-77-1.

Compliance: 1. For fittings which have achieved 1000 hours time in service, before 1 March 1977 and thereafter at intervals not exceeding 1000 hours time in service.

 

2. All other fittings, at intervals not exceeding 1000 hours time in service.

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.