CTHIn ForceLegislation
AD/AMD 50/43 - Rivets between Frames 9 and 10, and Stringer Reinforcements
AMD Falcon 50 and 900 Series AeroplanesAMD Falcon 50 and 900 Series Aeroplanes
Start here
Get a plain-English read of AMD Falcon 50 and 900 Series Aeroplanes
Turn the raw legal text into a practical explanation grounded in AD/AMD 50/43 - Rivets between Frames 9 and 10, and Stringer Reinforcements.
AMD Falcon 50 and 900 Series Aeroplanes
| AD/AMD 50/43 | Rivets between Frames 9 and 10, andStringer Reinforcements | 13/2007 |
|---|
| Applicability: | Model Falcon 900EX (version F900DX) aircraft, serial numbers 601 through 605. |
|---|---|
| Requirement: | Action in accordance with the requirements of EASA AD 2006-0320-E. |
| Compliance: | Before 31 December 2007. |
| This Airworthiness Directive becomes effective on 20 December 2007. | |
| Background: | The manufacturer has determined that some stringer reinforcements and some rivets are missing from the skin panels on each side of the fuselage between frames 9 and 10 on certain Falcon 900DX aircraft. |
Image unavailable in extracted text
David Villiers
Delegate of the Civil Aviation Safety Authority
7 November 2007