This may include reporting on the same or similar components, other than those covered by the design to which this AD applies, if the same unsafe condition can exist or may develop on an aircraft with those components installed. For any change affecting an ATA section, all pages in that associated.
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. Information about any failures, malfunctions, defects or other occurrences, which may be Chapter 32 32-00-00 Landing Gear 32-10-00 Main Gear & Doors 32-20-00 Nose Gear & Doors 32-30-00 Extension & Retraction 32-40-00 Wheels & Brakes 32-50-00. FIGURE 5.8 ATA chapters Aircrstt System a. Enquiries regarding this AD should be referred to the EASA Safety Information Section,Ĭertification Directorate. (Chapter 26) - landing gear (Chapter 32) 0 fuel system (Chapter 28) 0 electrical power (Chapter. No comments were received during the consultation period.ģ. 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. The opening chapters of Genesis and scriptures related thereto were never intended as a textbook of geology, archaeology, earth-science, or man-science.