In emergency mode, landing gear is actuated only by hydraulic power. Similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on a product, part or appliance not affected by this AD, can be reported to the EU aviation safety reporting system. F2000EX EASY 02-32-05 CODDE 1 PAGE 3 / 4 DGT94085 ATA 32 LANDING GEAR AND BRAKING SYSTEM GENERAL ISSUE 3 DASSAULT AVIATION Proprietary Data SOURCES In normal operation, landing gear is electrically controlled from the pilot station and hydraulically actuated. Item 32-01: Added requirement for approach minimums. Information about any failures, malfunctions, defects or other occurrences, which may be 31.3 31.3 31.3 31.3 35.5 35.5 32.6 32.6 32.6. ata 30 ice and rain protection Item 21-01: Revised to reflect all RR have CN-AA25656 incorporated. Enquiries regarding this AD should be referred to the EASA Safety Information Section,Ĭertification Directorate. We supply over 6 billion new, old, and obsolete inventory including but not limited to 32, Landing Gear or parts pertaining to Piston. No comments were received during the consultation period.ģ. Type In a part number, manufacturer or ATA number, and you can find specifications on what you need. This AD was posted on 08 October 2021 as PAD 21-143 for consultation until 05 NovemberĢ021.
If requested and appropriately substantiated, EASA can approve Alternative Methods ofĢ. The use of later approved revisions of the above-mentioned documents is acceptable forĬompliance with the requirements of this AD.ġ. KG WOI MD10-WOI-32-001 original issue dated 11 March 2021, or Rev. KG SB-MD10-007 original issue dated 11 March 2021, or Rev.