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- FAA-2026-09574
FAA-2026-09574
Airworthiness Directives; Diamond Aircraft Industries Inc. Airplanes
Resumo Rápido
- Número AD
- FAA-2026-09574
- Autoridade
- FAA
- Data de emissão
- 13/05/2026
- Data efetiva
- —
- Criticidade
- routine
Autoridade
Federal Aviation Administration (EUA)
Data de Publicação
13 de maio de 2026
Data Efetiva
Não informada
Prazo de Cumprimento
Antes do próximo voo
Resumo da Diretiva
A FAA propõe adotar uma nova diretriz de aeronavegabilidade (AD) para todos os aviões Diamond Aircraft Industries Inc. (DAI) modelo DA 40, DA 40 F e DA 40 NG. Esta AD proposta foi motivada por diversos relatos de separação da porta de passageiro durante o voo. Esta AD proposta exigiria revisar o manual de voo do avião (AFM) existente para fornecer à tripulação de voo limitações operacionais revisadas, procedimentos de emergência e procedimentos operacionais normais; inspecionar as áreas do mecanismo de travamento da porta de passageiro e do mecanismo de gancho de segurança e executar ação corretiva, conforme aplicável; inspecionar o gancho de segurança, parafusos de travamento, blocos guia frontal e traseiro da porta, luz de aviso de claraboia e porta de passageiro, dobradiças de carbono, mola de tensão, bloco de retenção, botão de pressão do gancho de segurança, mola do mecanismo de travamento, mola a gás e moldura da porta; medir a força de acionamento da maçaneta da porta de passageiro; modificar o avião com placas de identificação; substituir a mola a gás; e substituir o conjunto de gancho, bloco de retenção, blocos guia da porta e vedação da porta, se necessário. A FAA propõe esta AD para resolver a condição insegura nestes produtos.
The FAA proposes to adopt a new airworthiness directive (AD) for all Diamond Aircraft Industries Inc. (DAI) Model DA 40, DA 40 F, and DA 40 NG airplanes. This proposed AD was prompted by several reports of passenger door separation during flight. This proposed AD would require revising the existing airplane flight manual (AFM) to provide the flight crew with revised operating limitations, emergency procedures, and normal operating procedures; inspecting the passenger door latching mechanism and safety hook mechanism areas and performing corrective action, as applicable; inspecting the safety hook, latching bolts, front and rear door guide blocks, canopy and passenger door warning light, carbon hinges, tension spring, retaining block, safety hook push button, latching mechanism spring, gas spring, and door frame; measuring the passenger door handle actuation force; modifying the airplane with placards; replacing the gas spring; and replacing the hook assembly, retaining block, door guide blocks, and door sealant if necessary. The FAA is proposing this AD to address the unsafe condition on these products.Texto Completo da Diretiva
Expandir texto completo (Federal Register)Texto completo (Federal Register)
Document Headings Document headings vary by document type but may contain the following: • the agency or agencies that issued and signed a document • the number of the CFR title and the number of each part the document amends, proposes to amend, or is directly related to • the agency docket number / agency internal file number • the RIN which identifies each regulatory action listed in the Unified Agenda of Federal Regulatory and Deregulatory Actions See the Document Drafting Handbook for more details. Department of Transportation Federal Aviation Administration • 14 CFR Part 39 • [Docket No. FAA-2026-4633; Project Identifier MCAI-2025-01173-A] • RIN 2120-AA64 AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM). SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD) for all Diamond Aircraft Industries Inc. (DAI) Model DA 40, DA 40 F, and DA 40 NG airplanes. This proposed AD was prompted by several reports of passenger door separation during flight. This proposed AD would require revising the existing airplane flight manual (AFM) to provide the flight crew with revised operating limitations, emergency procedures, and normal operating procedures; inspecting the passenger door latching mechanism and safety hook mechanism areas and performing corrective action, as applicable; inspecting the safety hook, latching bolts, front and rear door guide blocks, canopy and passenger door warning light, carbon hinges, tension spring, retaining block, safety hook push button, latching mechanism spring, gas spring, and door frame; measuring the passenger door handle actuation force; modifying the airplane with placards; replacing the gas spring; and replacing the hook assembly, retaining block, door guide blocks, and door sealant if necessary. The FAA is proposing this AD to address the unsafe condition on these products. DATES: The FAA must receive comments on this NPRM by June 29, 2026. ADDRESSES: You may send comments, using the procedures found in 14 CFR 11.43 and 11.45, by any of the following methods: • Federal eRulemaking Portal: Go to regulations.gov. Follow the instructions for submitting comments. • Fax: (202) 493-2251. • Mail: U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE, Washington, DC 20590. • Hand Delivery: Deliver to Mail address above between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA-2026-4633; or in person at Docket Operations between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this NPRM, the mandatory continuing airworthiness information (MCAI), any comments received, and other information. The street address for Docket Operations is listed above. Material Incorporated by Reference: • For Diamond Aircraft Industries material identified in this proposed AD, contact DAI, 1560 Crumlin Sideroad, London, Ontario, Canada, N5V 1S2; phone: (519) 457-4041; email:support-canada@diamondaircraft.com; website: diamondaircraft.com. • You may view this material at the FAA, Airworthiness Products Section, Operational Safety Branch, 901 Locust, Kansas City, MO 64106. For information on the availability of this material at the FAA, call (817) 222-5110. FOR FURTHER INFORMATION CONTACT: Fatin Saumik, Aviation Safety Enginee…
Fonte: Federal Register (federalregister.gov). Texto original em inglês. Conteúdo sanitizado por segurança.
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