Commonwealth legislation

AD/750XL/13 - Aileron Inboard Hinge Attachment

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

4/10 complexity

Requires owners/operators of specified Pacific Aerospace 750XL aircraft (particular serial numbers, excluding those with modification PAC/XL/0285) to remove both ailerons and inspect and modify the aileron spar at the inboard hinge in accordance with Pacific Aerospace Service Bulletin PACSB/XL/027. Compliance is required within 150 flight hours or six months after 5 July 2007. The directive follows the New Zealand CAA's recommendation to prevent cracks developing adjacent to the inboard hinge.

JSON API

Deep dive

Want the full deep dive?

Zoe can write the in-depth analysis on top of the summary above: how it works, who it affects and what each part actually does.

Current sections

Direct links to the current provisions in AD/750XL/13 - Aileron Inboard Hinge Attachment.

Pacific Aerospace 750XL Series Aeroplane

Pacific Aerospace 750XL Series Aeroplanes

AD/750XL/13	Aileron Inboard Hinge Attachment	7/2007

Applicability:	Model 750XL aircraft, serial numbers 101, 102, 104 through 120, and 122 through 129; except aircraft with modification PAC/XL/0285 incorporated.
Requirement:	Remove both ailerons, then inspect and modify the aileron spar at the inboard hinge attachment point in accordance with Pacific Aerospace Ltd Service Bulletin PACSB/XL/027.Note 1: Aileron removal, installation and rigging procedures are detailed in PAC 750XL Maintenance Manual Chapter 27-10-00.Note 2: NZ CAA AD DCA/750XL/13 refers.
Compliance:	Within 150 hours time in service or 6 months after 5 July 2007, whichever occurs first.
	This Airworthiness Directive becomes effective on 5 July 2007.
Background:	The NZ CAA requires certain actions to prevent cracks developing in the aileron spar adjacent to the inboard hinge attachment.

View image in the official source
David Punshon
Delegate of the Civil Aviation Safety Authority

16 May 2007

AD/750XL/13

Aileron Inboard Hinge Attachment

7/2007

Source text

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

Pacific Aerospace 750XL Series Aeroplane Pacific Aerospace 750XL Series Aeroplanes

Pacific Aerospace 750XL Series Aeroplanes

AD/750XL/13	Aileron Inboard Hinge Attachment	7/2007

Applicability:	Model 750XL aircraft, serial numbers 101, 102, 104 through 120, and 122 through 129; except aircraft with modification PAC/XL/0285 incorporated.
Requirement:	Remove both ailerons, then inspect and modify the aileron spar at the inboard hinge attachment point in accordance with Pacific Aerospace Ltd Service Bulletin PACSB/XL/027.Note 1: Aileron removal, installation and rigging procedures are detailed in PAC 750XL Maintenance Manual Chapter 27-10-00.Note 2: NZ CAA AD DCA/750XL/13 refers.
Compliance:	Within 150 hours time in service or 6 months after 5 July 2007, whichever occurs first.
	This Airworthiness Directive becomes effective on 5 July 2007.
Background:	The NZ CAA requires certain actions to prevent cracks developing in the aileron spar adjacent to the inboard hinge attachment.

AD/750XL/13 - Aileron Inboard Hinge Attachment

Plain English Summary

Deep dive

Current sections

Pacific Aerospace 750XL Series Aeroplanes

Pacific Aerospace 750XL Series Aeroplanes

AD/750XL/13

AD/750XL/13

Aileron Inboard Hinge Attachment

Aileron Inboard Hinge Attachment

7/2007

7/2007

Source text

Pacific Aerospace 750XL Series Aeroplane Pacific Aerospace 750XL Series Aeroplanes

Pacific Aerospace 750XL Series Aeroplanes

AD/750XL/13 AD/750XL/13

AD/750XL/13

Aileron Inboard Hinge Attachment Aileron Inboard Hinge Attachment

Aileron Inboard Hinge Attachment

7/2007 7/2007

7/2007