{"content":[{"text":"[Federal Register Volume 86, Number 136 (Tuesday, July 20, 2021)] \n [Rules and Regulations] \n [Pages 38212-38213] \n From the Federal Register Online via the Government Publishing Office [www.gpo.gov] \n [FR Doc No: 2021-15351]","bbox":{"left":0.1,"top":0.045741,"width":0.697118,"height":0.086476}},{"text":"––––––––––––––––––––––––––––––––––","bbox":{"left":0.1,"top":0.150589,"width":0.333333,"height":0.01677899999999999}},{"text":"DEPARTMENT OF TRANSPORTATION","bbox":{"left":0.1,"top":0.185437,"width":0.36161200000000004,"height":0.01677899999999999}},{"text":"Federal Aviation Administration","bbox":{"left":0.1,"top":0.220286,"width":0.27443399999999996,"height":0.01677899999999999}},{"text":"14 CFR Part 39","bbox":{"left":0.1,"top":0.255134,"width":0.130981,"height":0.01677899999999999}},{"text":"[Docket No. FAA-2021-0339; Project Identifier MCAI-2020-01605-T; Amendment 39-21636; \n AD 2021-14-09]","bbox":{"left":0.1,"top":0.289983,"width":0.7743730000000001,"height":0.03420299999999998}},{"text":"RIN 2120-AA64","bbox":{"left":0.1,"top":0.342256,"width":0.134313,"height":0.01677899999999999}},{"text":"Airworthiness Directives; Airbus Canada Limited Partnership (Type Certificate Previously \n Held by C Series Aircraft Limited Partnership (CSALP); Bombardier, Inc.) Airplanes","bbox":{"left":0.1,"top":0.377104,"width":0.764509,"height":0.03420299999999998}},{"text":"AGENCY: Federal Aviation Administration (FAA), DOT.","bbox":{"left":0.1,"top":0.429074,"width":0.464314,"height":0.01677899999999999}},{"text":"ACTION: Final rule.","bbox":{"left":0.1,"top":0.463922,"width":0.170196,"height":0.01677899999999999}},{"text":"––––––––––––––––––––––––––––––––––","bbox":{"left":0.1,"top":0.499074,"width":0.333333,"height":0.01677899999999999}},{"text":"SUMMARY: The FAA is adopting a new airworthiness directive (AD) for certain Airbus Canada \n Limited Partnership Model BD-500-1A10 and BD-500-1A11 airplanes. This AD was prompted by a \n design review that identified rib 0 of the center wing box (CWB) as an area where a single failure of \n a clamshell type refuel/defuel line coupling could lead to the accumulation of dangerous levels of \n electrostatic charges within the fuel tank. This AD requires replacing the clamshell type refuel/defuel \n line coupling in the CWB at rib 0 with a threaded type fuel coupling, and installing an additional \n support bracket and clamp in the CWB at rib 0, as specified in a Transport Canada Civil Aviation \n (TCCA) AD, which is incorporated by reference. The FAA is issuing this AD to address the unsafe \n condition on these products.","bbox":{"left":0.1,"top":0.533619,"width":0.7938769999999999,"height":0.156173}},{"text":"DATES: This AD is effective August 24, 2021. \n The Director of the Federal Register approved the incorporation by reference of a certain \n publication listed in this AD as of August 24, 2021.","bbox":{"left":0.1,"top":0.707861,"width":0.732549,"height":0.05162800000000001}},{"text":"ADDRESSES: For material incorporated by reference (IBR) in this AD, contact TCCA, Transport \n Canada National Aircraft Certification, 159 Cleopatra Drive, Nepean, Ontario K1A 0N5, Canada; \n telephone 888-663-3639; email AD-CN@tc.gc.ca; internet https://tc.canada.ca/en/aviation. You may \n view this IBR material at the FAA, Airworthiness Products Section, Operational Safety Branch, 2200 \n South 216th St., Des Moines, WA. For information on the availability of this material at the FAA, \n call 206-231-3195. It is also available in the AD docket on the internet at \n https://www.regulations.gov by searching for and locating Docket No. FAA-2021-0339.","bbox":{"left":0.1,"top":0.777558,"width":0.796079,"height":0.12132500000000002}},{"text":"1","bbox":{"left":0.495098,"top":0.96468,"width":0.00980399999999998,"height":0.01677899999999999}}],"images_bbox":[],"images_bbox_not_text_overlap":[]}