AD 2025-02187
Published 2025-02-04 · 12 models · 40 US-registered tails affected · Federal Register
Airworthiness Directives; Britten-Norman Aerospace Ltd. Airplanes Federal Register ↗
Abstract
The FAA is adopting a new airworthiness directive (AD) for certain Britten-Norman Aerospace Ltd. Model BN-2, BN-2A, BN-2A-2, BN- 2A-3, BN-2A-6, BN-2A-8, BN-2A-9, BN-2A-20, BN-2A-21, BN-2A-26, BN-2A- 27, BN-2B-20, BN-2B-21, BN-2B-26, BN-2B-27, BN-2T, BN2T-4R, and BN2T-4S airplanes; and certain Model BN2A MK. III, BN2A MK. III-2, and BN2A MK. III-3 airplanes. This AD was prompted by the determination that, in order to ensure the continued structural integrity of certain landing gear and associated components, it is necessary to require removal of these components from service prior to exceeding established fatigue lives. This AD requires determining the number of landings on affected main landing gears (MLGs), nose landing gears (NLGs), and associated components; removing from service any part that has reached or exceeded the established fatigue life and installing a replacement part; and prohibiting the installation of any affected part unless the number of landings for that part is below the established fatigue life. The FAA is issuing this AD to address the unsafe condition on these products.
Applicability · by US fleet size
- BRITTEN-NORMAN BN-2A TCDS A17EU 8 tails
- BRITTEN-NORMAN BN-2A-8 TCDS A17EU 8 tails
- BRITTEN-NORMAN BN-2A-27 TCDS A17EU 5 tails
- BRITTEN-NORMAN BN-2B-26 TCDS A17EU 4 tails
- BRITTEN-NORMAN BN-2A-9 TCDS A17EU 4 tails
- BRITTEN-NORMAN BN-2A-20 TCDS A17EU 3 tails
- BRITTEN-NORMAN BN-2A-21 TCDS A17EU 2 tails
- BRITTEN NORMAN LTD. BN-2B-20 TCDS A17EU 2 tails
- BRITTEN-NORMAN BN-2A-6 TCDS A17EU 1 tails
- UNKNOWN UNKNOWN 1 tails
- BRITTEN-NORMAN BN-2B-21 TCDS A17EU 1 tails
- BRITTEN-NORMAN LTD BN-2A-26 TCDS A17EU 1 tails
Federal Register text
Verbatim; the Federal Register publication is the legally binding document. Cite: 90 FR 8870. View on Federal Register ↗
[Federal Register Volume 90, Number 22 (Tuesday, February 4, 2025)] [Rules and Regulations] [Pages 8870-8874] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR Doc No: 2025-02187]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2024-1299; Project Identifier MCAI-2023-00237-A; Amendment 39-22925; AD 2025-01-01] RIN 2120-AA64
Airworthiness Directives; Britten-Norman Aerospace Ltd. Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for certain Britten-Norman Aerospace Ltd. Model BN-2, BN-2A, BN-2A-2, BN- 2A-3, BN-2A-6, BN-2A-8, BN-2A-9, BN-2A-20, BN-2A-21, BN-2A-26, BN-2A- 27, BN-2B-20, BN-2B-21, BN-2B-26, BN-2B-27, BN-2T, BN2T-4R, and BN2T-4S airplanes; and certain Model BN2A MK. III, BN2A MK. III-2, and BN2A MK. III-3 airplanes. This AD was prompted by the determination that, in order to ensure the continued structural integrity of certain landing gear and associated components, it is necessary to require removal of these components from service prior to exceeding established fatigue lives. This AD
[[Page 8871]]
requires determining the number of landings on affected main landing gears (MLGs), nose landing gears (NLGs), and associated components; removing from service any part that has reached or exceeded the established fatigue life and installing a replacement part; and prohibiting the installation of any affected part unless the number of landings for that part is below the established fatigue life. The FAA is issuing this AD to address the unsafe condition on these products.
DATES: This AD is effective March 11, 2025. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of March 11, 2025.