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AD/F2000/5 - Engine Nacelle Firewalls
Dassault Aviation Falcon 2000 Series AerDassault Aviation Falcon 2000 Series Aeroplanes
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Dassault Aviation Falcon 2000 Series Aeroplanes
| AD/F2000/5 | Engine Nacelle Firewalls | 3/2006 |
|---|
| Applicability: | Model 2000 aircraft; except for aircraft with Dassault Aviation Service BulletinNo. F2000-248 incorporated in service or Dassault Aviation modification M2111 incorporated in production. |
|---|---|
| Requirement: | Action in accordance with DGAC AD 2002-413(B).Note: Dassault Aviation Service Bulletin F2000-248 refers. |
| Compliance: | Before 31 March 2006, unless already accomplished. |
| This Airworthiness Directive becomes effective on 16 March 2006. | |
| Background: | The manufacturer has determined that two manufacturing holes have not been plugged in the left and right engine masts firewalls. In the case of significant fuel leakage at the fuselage-nacelle connection, fuel could drain to a hot zone area. |
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David Villiers
Delegate of the Civil Aviation Safety Authority
2 February 2006