Commonwealth legislation

AD/ATR 42/15 - Wing Inner Skin Surface at Rear Spar Junction

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

What this AD does: Requires owners/operators of ATR 42-300 and -320 aircraft (serial numbers 3–59) to have the wing rear-spar inner-skin fastener holes cold‑worked in line with DGAC AD 98-147-075(B). The work must be done before the aircraft reaches 33,000 flights and the AD took effect 30 August 2007. Operators pay for and schedule the maintenance; the rule enforces a technical fatigue‑mitigation action and cross‑references a foreign authority’s procedure.

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Current sections

Direct links to the current provisions in AD/ATR 42/15 - Wing Inner Skin Surface at Rear Spar Junction.

Avions de Transport Regional ATR 42 Seri

Avions de Transport Regional ATR 42 Series Aeroplanes

AD/ATR 42/15	Wing Inner Skin Surface at Rear Spar Junction	9/2007

Applicability:	Model ATR 42-300 and -320 aircraft, serial numbers 3 through 59.
Requirement:	Action in accordance with the requirements of DGAC AD 98-147-075(B).
Compliance:	Before the accumulation of 33,000 flights.
	This Airworthiness Directive becomes effective on 30 August 2007.
Background:	This Directive requires fastener hole cold-working in order to prevent the initiation and development of fatigue damage.

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David Villiers
Delegate of the Civil Aviation Safety Authority

10 July 2007

AD/ATR 42/15

Wing Inner Skin Surface at Rear Spar Jun

Wing Inner Skin Surface at Rear Spar Junction

9/2007

Source text

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

Avions de Transport Regional ATR 42 Seri Avions de Transport Regional ATR 42 Series Aeroplanes

Avions de Transport Regional ATR 42 Series Aeroplanes

AD/ATR 42/15	Wing Inner Skin Surface at Rear Spar Junction	9/2007

Applicability:	Model ATR 42-300 and -320 aircraft, serial numbers 3 through 59.
Requirement:	Action in accordance with the requirements of DGAC AD 98-147-075(B).
Compliance:	Before the accumulation of 33,000 flights.
	This Airworthiness Directive becomes effective on 30 August 2007.
Background:	This Directive requires fastener hole cold-working in order to prevent the initiation and development of fatigue damage.

David Villiers
Delegate of the Civil Aviation Safety Authority

10 July 2007

AD/ATR 42/15 - Wing Inner Skin Surface at Rear Spar Junction

Plain English Summary

Deep dive

Current sections

Avions de Transport Regional ATR 42 Series Aeroplanes

Avions de Transport Regional ATR 42 Series Aeroplanes

AD/ATR 42/15

AD/ATR 42/15

Wing Inner Skin Surface at Rear Spar Junction

Wing Inner Skin Surface at Rear Spar Junction

9/2007

9/2007

Source text

Avions de Transport Regional ATR 42 Seri Avions de Transport Regional ATR 42 Series Aeroplanes

Avions de Transport Regional ATR 42 Series Aeroplanes

AD/ATR 42/15 AD/ATR 42/15

AD/ATR 42/15

Wing Inner Skin Surface at Rear Spar Jun Wing Inner Skin Surface at Rear Spar Junction

Wing Inner Skin Surface at Rear Spar Junction

9/2007 9/2007

9/2007