CTHIn ForceLegislation
AD/BEECH 76/19 - Trailing Edge Flaps
Beechcraft 76 (Duchess) Series AeroplaneBeechcraft 76 (Duchess) Series Aeroplanes
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Beechcraft 76 (Duchess) Series Aeroplanes
| AD/BEECH 76/19 | Trailing Edge Flaps | 2/2005 |
|---|
| Applicability: | All Beechcraft 76 series. |
|---|---|
| Requirement: | Inspect flap internal structure at the flap hinge bracket attachment ribs for corrosion.This inspection will require leading edge skin removal or installation of inspection panels to a scheme approved by the Authority or a suitably authorised CAR 35 person. |
| Compliance: | Unless already accomplished, within 25 hours time in service after 17 February 2005 or 3 months, whichever occurs first and thereafter at intervals not exceeding 3 years. |
| This Airworthiness Directive becomes effective on 17 February 2005. | |
| Background: | Numerous Major Defect Reports have indicated that an advanced state of corrosion can exist without external indications. In some instances more than half of the hinge bracket was corroded away. |
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Neville Probert
Delegate of the Civil Aviation Safety Authority
21 December 2004
The above AD is notified in the Commonwealth of Australia Gazette on 26 January 2005.