AD/BELL 212/66 - Main Rotor Grip

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


AIRWORTHINESS DIRECTIVE


For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.1 (1) of CAR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.

 

Bell Helicopter Textron 212 Series Helicopters

 

 

AD/BELL 212/66

Main Rotor Grip

3/2003

DM

Applicability: Model

 

212

Main Rotor Grip Part Number 204-011-121-009, or -121.

 

 

Requirement: Action in accordance with the technical requirements of FAA AD 2003-01-04 Amdt 39-13015.

Note 1: Bell Helicopter Textron Non-Destructive Inspection Procedures, Log No. 00- 340 Revision E, dated 9 April 2002, refers.

 

Note 2: FAA AD 2003-01-04 can be found on the FAA website www.airweb.faa.gov/rgl.

 

Compliance: As specified in the Requirement document, with compliance times to count from the effective date of this Directive.

 

This Airworthiness Directive becomes effective on 29 January 2003.

 

Background: The FAA received reports of three in- flight main rotor grip failures and two recent incidents of cracked grips discovered during a 1,200- hour inspection and on a scheduled 2,400-hour overhaul, which brings the total to thirteen grips that have cracked in the lower tang. Cracking for all of the grips has been attributed to mechanical damage from improper blade bolt bushing installation, improper rework of the buffer pad tang surface, or subsurface fatigue damage.


David Alan Villiers

Delegate of the Civil Aviation Safety Authority 24 January 2003

 

 


The above AD is notified in the Commonwealth of Australia Gazette on 29 January 2003.

 

 


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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.