CTHRepealedLegislation
AD/B727/201 - Trailing Edge Flap Foreflap
Boeing 727 Series AeroplanesBoeing 727 Series Aeroplanes
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Boeing 727 Series Aeroplanes
| AD/B727/201 | Trailing Edge Flap Foreflap | 4/2006 |
|---|
| Applicability: | Model 727, 727C, 727-100, 727-100C, 727-200, and 727-200F series aircraft, as listed in Boeing Alert Service Bulletin 727-57A0135 Revision 3, or later FAA approved revision. |
|---|---|
| Requirement: | Action in accordance with the technical requirements of FAA AD 2005-14-07Amdt 39-14184.Note: Boeing Service Bulletin 727-27-133, and Boeing 727 Service Bulletins57-59 and 57-72; or later FAA approved revisions, refer. |
| Compliance: | As specified in the Requirement document, with a revised effective date of13 April 2006. |
| This Airworthiness Directive becomes effective on 13 April 2006. | |
| Background: | The FAA received reports of damaged or failed outboard foreflaps with a cracked or failed carriage attach fitting of the foreflap sequencing carriage. |
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David Punshon
Delegate of the Civil Aviation Safety Authority
1 March 2006