CTHIn ForceLegislation
AD/AMD 10/22 Amdt 1 - Overwing Emergency Exit
AMD Falcon 10 Series AeroplanesAMD Falcon 10 Series Aeroplanes
Start here
Get a plain-English read of AMD Falcon 10 Series Aeroplanes
Turn the raw legal text into a practical explanation grounded in AD/AMD 10/22 Amdt 1 - Overwing Emergency Exit.
AMD Falcon 10 Series Aeroplanes
| AD/AMD 10/22 Amdt 1 | Overwing Emergency Exit | 8/2006 |
|---|
| Applicability: | All Falcon 10 aircraft for which the Aircraft Maintenance Manual (AMM) Airworthiness Limitation Section, Chapter 5-40, is not at Revision 08 or above. |
|---|---|
| Requirement: | Insert a copy of EASA AD 2006-0147 into Chapter 5-40 of the Aircraft Maintenance Manual.Note: Updating Chapter 5-40 with Revision 08 terminates the requirement of this Directive, upon which the copy of this Directive may then be removed from the AMM. |
| Compliance: | Within 30 days after 3 August 2006. |
| This Amendment becomes effective on 3 August 2006. | |
| Background: | During an attempted operation of a Falcon 50 emergency exit, interference was reported between interior trim and the exit.Amendment 1 is issued in response to a new EASA AD, which supersedes DGAC AD 1999-211-023(B) (the original issue of this Directive), and extends the repetitive overwing emergency exit opening test interval to 24 months. |
Image unavailable in extracted text
David Villiers
Delegate of the Civil Aviation Safety Authority
23 June 2006