AD/ENST 28/21 - Tail Rotor Blade Grip - Inspection and Modification

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

Legislation au F2006B09577 In force Legislative Instrument

Legislation content

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Enstrom F-28 Series Helicopters

 

AD/ENST 28/21 Tail Rotor Blade Grip - Inspection

and Modification


5/79

 

Applicability: All models F-28C and 280C with Tail Rotor Blade Grip P/N 28-150013-1 wide chord.

 

Document: Enstrom Service Directive Bulletin No. 0048. Compliance: As per requirement document.

The Preflight Inspections may be carried out by the pilot in command in which case certification is not required.

 

Background:  The manufacturer has received several field reports of crack indications being found in the wide chord tail rotor blade retentions grip.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.