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Rule. "Airworthiness Directives; DAHER (Type Certificate Previously Held by SOCATA) Airplanes" Federal Register 89, no. 204 (October 22, 2024): 84277-84280. https://www.govinfo.gov/app/details/FR-2024-10-22/2024-24368.
Office of the Federal Register, National Archives and Records Administration. (). 89 FR 84277 - Airworthiness Directives; DAHER (Type Certificate Previously Held by SOCATA) Airplanes. [Government]. Office of the Federal Register, National Archives and Records Administration. https://www.govinfo.gov/app/details/FR-2024-10-22/2024-24368
Office of the Federal Register, National Archives and Records Administration. 89 FR 84277 - Airworthiness Directives; DAHER (Type Certificate Previously Held by SOCATA) Airplanes. Office of the Federal Register, National Archives and Records Administration, , https://www.govinfo.gov/app/details/FR-2024-10-22/2024-24368
Office of the Federal Register, National Archives and Records Administration, Airworthiness Directives; DAHER (Type Certificate Previously Held by SOCATA) Airplanes, govinfo, (October 22, 2024), https://www.govinfo.gov/app/details/FR-2024-10-22/2024-24368.
Close xFederal Register Volume 89, Issue 204 (October 22, 2024)
Regulatory Information
Federal Register
AE 2.7:
GS 4.107:
AE 2.106:
Office of the Federal Register, National Archives and Records Administration
Rules and Regulations
Final rule.
This AD is effective November 26, 2024.
Fred Guerin, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: (206) 231-2346; email: fred.guerin@faa.gov.
The FAA is superseding Airworthiness Directive (AD) 2016-08-08 for all SOCATA (type certificate now held by DAHER) Model MS 880B, MS 885, MS 892A-150, MS 892E-150, MS 893A, MS 893E, MS 894A, MS 894E, Rallye 100S, Rallye 150ST, Rallye 150T, Rallye 235C, and Rallye 235E airplanes. AD 2016-08-08 required doing repetitive detailed visual inspections of the intersection between the axle radius and the nose landing gear (NLG) fork area for chafing; doing repetitive dye penetrant inspections on the NLG wheel axle for cracks, distortion, and nicks or wear; doing corrective actions if necessary; and replacing the NLG wheel axle attachment screws with new screws. This AD is prompted by the introduction of a new inspection method and a new design for the affected NLG wheel axle that provides terminating action for the repetitive inspections, as specified in updated service information published by the manufacturer. This AD requires preparing, inspecting, replacing, reconditioning the NLG wheel axle, and prohibiting affected parts. The FAA is issuing this AD to address the unsafe condition on these products.
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
84277-84280
89 FR 84277
2120-AA64
14 CFR 39
Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety
Docket No. FAA-2024-1480, Project Identifier MCAI-2023-00930-A, Amendment 39-22851, AD 2024-19-09
2024-24368