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AD/CL-600/73 - Main Landing Gear Main Fitting - 2
Bombardier (Canadair) CL-600 (ChallengerBombardier (Canadair) CL-600 (Challenger) Series Aeroplanes
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Bombardier (Canadair) CL-600 (Challenger) Series Aeroplanes
| AD/CL-600/73 | Main Landing Gear Main Fitting - 2 | 8/2007 |
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| Applicability: | Model CL-600-2B19 aircraft, equipped with main landing gear main fittings part number 601R85001-81 and 601R85001-82 (MDI part number 17064-105 and17064-106). |
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| Requirement: | Action in accordance with the requirements of Transport Canada AD CF-2003-09.Note: Bombardier Alert Service Bulletin A601R-32-088 original issue, or later Transport Canada approved revision, refers. |
| Compliance: | As specified in the Requirement document, with a revised effective date of2 August 2007. |
| This Airworthiness Directive becomes effective on 2 August 2007. | |
| Background: | To prevent the collapse of the main landing gear upon landing, this Directive requires repetitive detailed visual and eddy current inspection of the main landing gear main fittings, and repetitive inspection of the main landing gear shock strut, for nitrogen pressure and visible chrome dimensions. |
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David Villiers
Delegate of the Civil Aviation Safety Authority
22 June 2007