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AD/DO 328/1 - Fuel Tank Safety Requirements
Dornier 328 Series AeroplanesDornier 328 Series Aeroplanes
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Dornier 328 Series Aeroplanes
| AD/DO 328/1 | Fuel Tank Safety Requirements | 13/2005 |
|---|
| Applicability: | Model 328-100 series aeroplanes. |
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| Requirement: | If not previously accomplished, carry out the following actions in accordance with AvCraft Aerospace GmbH Dornier 328 Service Bulletin SB-328-00-445 dated23 August 2004: |
| a. Modification of the electrical wiring of LH and RH fuel pump. | |
| b. Thermal insulation of Cross Bleed Valve, Flow Control and Shut Off Valves bodies and ECS heat exchanger and temperature control valve body. | |
| c. Installation of markings at fuel wiring harness. | |
| d. Amendment of Airworthiness Limitations Document (ALD). | |
| Note: LBA AD D-2005-001 (EASA Approval 2005-910) refers. | |
| Compliance: | Before 31 July 2006. |
| This Airworthiness Directive becomes effective on 22 December 2005. | |
| Background: | This Directive requires product improvement to meet the fuel tank safety requirements according to United States Special Federal Aviation Regulation (SFAR) 88 and European Joint Aviation Authorities Interim Policy INT/POL/25/12. The product improvements are designed to decrease the likelihood of ignition sources within the fuel tank and the possibility of an in-tank fire or explosion. |
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James Coyne
Delegate of the Civil Aviation Safety Authority
11 November 2005