Commonwealth legislation

AD/F406/12 - Rudder Pulley Bracket

RepealedCTH

This Act has been repealed and is no longer in force. It is retained for historical reference.

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

A Civil Aviation Safety Authority Airworthiness Directive requires owners/operators of certain Reims Aviation F406 aircraft to inspect a rudder pulley bracket (P/N 6015511-1) for cracking and repair or replace it per REIMS AVIATION Service Bulletin No. F406-58 (3 May 2005 or later approved).

It affects specific serial-numbered F406s and became mandatory on 7 July 2005 to prevent rudder failure and loss of control.

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Current sections

Direct links to the current provisions in AD/F406/12 - Rudder Pulley Bracket.

Reims Aviation F406 Series Aeroplanes

AD/F406/12	Rudder Pulley Bracket	7/2005

Applicability:	Model F406 aircraft, serial numbers 0002, 0003, 0004, 0006, 0008, 0009, 0010, 0012, 0013, 0017, 0024, 0025, 0039, 0042, 0044, 0045, 0066, 0070, 0073, 0074, 0075, 0077, 0080 through 0090, and 0092.
Requirement:	Action in accordance with REIMS AVIATION Service Bulletin No. F406-58, dated 3 May 2005 or later DGAC approved revision.Note: DGAC AD UF-2005-080 refers.
Compliance:	As specified in the Requirement document.
	This Airworthiness Directive becomes effective on 7 July 2005.
Background:	The DGAC received several reports of cracked rudder pulley brackets part number 6015511-1. Such cracking, if undetected, could result in failure of the rudder pulley bracket and consequent loss of rudder control.

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David Villiers
Delegate of the Civil Aviation Safety Authority

11 May 2005

AD/F406/12

Rudder Pulley Bracket

7/2005

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.

Reims Aviation F406 Series Aeroplanes Reims Aviation F406 Series Aeroplanes

Reims Aviation F406 Series Aeroplanes

AD/F406/12	Rudder Pulley Bracket	7/2005

Applicability:	Model F406 aircraft, serial numbers 0002, 0003, 0004, 0006, 0008, 0009, 0010, 0012, 0013, 0017, 0024, 0025, 0039, 0042, 0044, 0045, 0066, 0070, 0073, 0074, 0075, 0077, 0080 through 0090, and 0092.
Requirement:	Action in accordance with REIMS AVIATION Service Bulletin No. F406-58, dated 3 May 2005 or later DGAC approved revision.Note: DGAC AD UF-2005-080 refers.
Compliance:	As specified in the Requirement document.
	This Airworthiness Directive becomes effective on 7 July 2005.
Background:	The DGAC received several reports of cracked rudder pulley brackets part number 6015511-1. Such cracking, if undetected, could result in failure of the rudder pulley bracket and consequent loss of rudder control.

AD/F406/12 - Rudder Pulley Bracket

Plain English Summary

Deep dive

Current sections

Reims Aviation F406 Series Aeroplanes

Reims Aviation F406 Series Aeroplanes

AD/F406/12

AD/F406/12

Rudder Pulley Bracket

Rudder Pulley Bracket

7/2005

7/2005

Source text

Reims Aviation F406 Series Aeroplanes Reims Aviation F406 Series Aeroplanes

Reims Aviation F406 Series Aeroplanes

AD/F406/12 AD/F406/12

AD/F406/12

Rudder Pulley Bracket Rudder Pulley Bracket

Rudder Pulley Bracket

7/2005 7/2005

7/2005