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AD/DO 328/74 - Engine Controls - Power Lever Control Box
Dornier 328 Series AeroplanesDornier 328 Series Aeroplanes
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Dornier 328 Series Aeroplanes
| AD/DO 328/74 | Engine Controls - Power Lever Control Box | 12/2009 |
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| Applicability: | Dornier Luftfahrt GmbH; Fairchild-Dornier GmbH; AvCraft Aerospace GmbH Model 328-100 aeroplanes. |
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| Requirement: | 1. Inspect and modify the power lever control box in accordance with the accomplishment instructions of 328 Support Services GmbH Service Bulletin SB-328-76-486 dated 15 July 2009.2. If discrepancies are found during the inspection and installation as detailed in Requirement 1 of this AD, contact 328 Support Services GmbH for corrective actions and accomplish those actions accordingly.The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.Note: EASA AD 2009-0196 dated 4 September 2009 refers. |
| Compliance: | For Requirement 1 - Within the next 15 months after the effective date of this AD, unless previously accomplished.For Requirement 2 - Before further flight. |
| This Airworthiness Directive becomes effective on 19 November 2009. | |
| Background: | Several runway excursion incidents and a single accident have occurred in the past with Dornier 328-100 aeroplanes, where the power lever could not be operated as intended during the landing roll-out. This situation has resulted in a safety record below the desirable standard.Recurrence of such an event under similar conditions, if not corrected, could result in further cases of runway excursion, possibly resulting in damage to the aeroplane and injury to the occupants. |
| A modification to the power lever control box has been designed to prevent further power lever handling difficulties. |
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David Villiers
Delegate of the Civil Aviation Safety Authority
28 September 2009