Commonwealth legislation

AD/A119/8 - Tail Rotor Pitch Control Link Assembly

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Commonwealth

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legislative instrument

Plain English Summary

3/10 complexity

This Airworthiness Directive requires operators to inspect or take the corrective action specified in Agusta Alert SB 119-15 (or later EASA-approved revisions) for tail rotor pitch control link assembly P/N 109-0130-05-117 with serial numbers MO001–MO773 on Agusta A119 helicopters, and forbids installing affected spare links, effective before the next flight. The AD follows a reported failure traced to a production defect and therefore affects A119 owners/operators and maintenance organisations, who must bear immediate inspection, grounding or replacement costs.

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Current sections

Direct links to the current provisions in AD/A119/8 - Tail Rotor Pitch Control Link Assembly.

Agusta A119 Series Helicopters

AD/A119/8	Tail Rotor Pitch Control Link Assembly	10/2006 TX

Applicability:	Agusta A119 helicopters fitted with tail rotor pitch control link assembly part number (P/N) 109-0130-05-117 with serial (S/N) from MO001 up to S/N MO773 (included).The AD does not apply to tail rotor pitch control link assembly P/N 109-0130-05-117 with S/N MOxxx and identified with the letter T” after the S/N.
Requirement:	Action in accordance with Agusta Alert SB 119-15 or later EASA approved revisions.Note: EASA Emergency AD 2006-0228-E dated 27 July 2006 refers.
Compliance:	Before further flight after the effective date of this AD.For links held as spares: Before installation on a helicopter after the effective date of this AD.
	This Airworthiness Directive becomes effective on 7 August 2006.
Background:	An A109E experienced a failure of the tail rotor pitch control link assembly P/N109-0130-05-117 with 10 FH. Preliminary investigation made by the TCH Agusta has revealed that the failure has been caused by a production defect.

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James Coyne
Delegate of the Civil Aviation Safety Authority

3 August 2006

AD/A119/8

Tail Rotor Pitch Control Link Assembly

10/2006 TX

Source text

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

Agusta A119 Series Helicopters Agusta A119 Series Helicopters

Agusta A119 Series Helicopters

AD/A119/8	Tail Rotor Pitch Control Link Assembly	10/2006 TX

Applicability:	Agusta A119 helicopters fitted with tail rotor pitch control link assembly part number (P/N) 109-0130-05-117 with serial (S/N) from MO001 up to S/N MO773 (included).The AD does not apply to tail rotor pitch control link assembly P/N 109-0130-05-117 with S/N MOxxx and identified with the letter T” after the S/N.
Requirement:	Action in accordance with Agusta Alert SB 119-15 or later EASA approved revisions.Note: EASA Emergency AD 2006-0228-E dated 27 July 2006 refers.
Compliance:	Before further flight after the effective date of this AD.For links held as spares: Before installation on a helicopter after the effective date of this AD.
	This Airworthiness Directive becomes effective on 7 August 2006.
Background:	An A109E experienced a failure of the tail rotor pitch control link assembly P/N109-0130-05-117 with 10 FH. Preliminary investigation made by the TCH Agusta has revealed that the failure has been caused by a production defect.

AD/A119/8 - Tail Rotor Pitch Control Link Assembly

Plain English Summary

Deep dive

Current sections

Agusta A119 Series Helicopters

Agusta A119 Series Helicopters

AD/A119/8

AD/A119/8

Tail Rotor Pitch Control Link Assembly

Tail Rotor Pitch Control Link Assembly

10/2006 TX

10/2006 TX

Source text

Agusta A119 Series Helicopters Agusta A119 Series Helicopters

Agusta A119 Series Helicopters

AD/A119/8 AD/A119/8

AD/A119/8

Tail Rotor Pitch Control Link Assembly Tail Rotor Pitch Control Link Assembly

Tail Rotor Pitch Control Link Assembly

10/2006 TX 10/2006 TX

10/2006 TX