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AD/B737/281 Amdt 1 - Fuselage Stringer 14 Lap Joint at Body Station 727
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Boeing 737 Series Aeroplanes
| AD/B737/281 Amdt 1 | Fuselage Stringer 14 Lap Jointat Body Station 727 | 7/2006 |
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| Applicability: | Model 737-100, -200 and -200C series aircraft, line numbers 1 through 920, with more than 40,000 total landings. |
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| Requirement: | Action in accordance with the technical requirements of FAA AD 89-22-04 Amdt39-6355.Accomplishment of Boeing Alert S/B 737-53A1135 Revision 2 or later revision approved by the FAA as an Alternative Means of Compliance (AMOC) is an acceptable Alternative Means of Compliance for the requirements of this AD. |
| Compliance: | In accordance with the requirement document, unless already accomplished. |
| This Amendment becomes effective on 6 July 2006. | |
| Background: | This Directive requires inspection of the fuselage stringer 14 lap joint, left and right, at Body station 727 and aft. The actions required by this directive are intended to prevent fuselage structural failure.Amendment 1 is issued to allow the use of an FAA approved Alternate Means of Compliance. |
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David Villiers
Delegate of the Civil Aviation Safety Authority
23 May 2006