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AD/B767/4 Amdt 1 - Horizontal Stabiliser Pivot Fitting - Outer Pivot Pin Inspection and Inner Pin Replacement
Boeing 767 Series AeroplanesBoeing 767 Series Aeroplanes
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Boeing 767 Series Aeroplanes
| AD/B767/4 Amdt 1 | Horizontal Stabiliser Pivot Fitting - Outer Pivot Pin Inspection and Inner Pin Replacement | 2/2005 |
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| Applicability: | Applicable to all aircraft listed by customer code and variable number in the requirement document. |
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| Requirement: | Boeing S.B. No. 767-55-0005 Rev 01 or latter FAA approved revision.Note: FAA AD 85-09-02, Amdt 39-5057 refers. |
| Compliance: | As detailed in the requirement document. |
| This Amendment becomes effective on 17 February 2005. | |
| Background: | The failure of a pivot fitting pin on the B767 major fatigue test article was attributed to improper manufacture. This directive is prompted by the discovery that a number of these parts were improperly manufactured.This amendment is issued to update the requirement document revision status.The original issue of this AD became effective on 31 July 1985. |
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David Villiers
Delegate of the Civil Aviation Safety Authority
14 December 2004
The above AD is notified in the Commonwealth of Australia Gazette on 26 January 2005.