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AD/JETSTREAM/108 - Flap Torque Shaft Assembly
British Aerospace BAe 3100 (Jetstream) SBritish Aerospace BAe 3100 (Jetstream) Series Aeroplanes
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British Aerospace BAe 3100 (Jetstream) Series Aeroplanes
| AD/JETSTREAM/108 | Flap Torque Shaft Assembly | 22/2010 |
|---|
| Applicability: | All HP137 Mk 1, Jetstream Series 200 and Jetstream Series 3100 aircraft. |
|---|---|
| Requirement: | Retire flap torque shaft assemblies in accordance with Jetstream Service Bulletin27-JA840421 or later revision.Note: UK CAA AD 009-02-86 refers. |
| Compliance: | Before exceeding 18,000 landings or equivalent as specified in the Requirement document. |
| This Airworthiness Directive becomes effective on 19 November 2010. | |
| Background: | Continued testing of the fatigue test airframe has shown the need to limit thein-service life of the flap torque shaft assembly to 18,000 landings or its equivalent. |
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Mike Higgins
Delegate of the Civil Aviation Safety Authority
26 October 2010