AD 2025-02027
Published 2025-01-31 · 7 models · 19 US-registered tails affected · Federal Register
Airworthiness Directives; Airbus Helicopters Federal Register ↗
Abstract
The FAA is adopting a new airworthiness directive (AD) certain Airbus Helicopters Model AS332C, AS332C1, AS332L, AS332L1, AS332L2, AS355E, AS355F, AS355F1, AS355F2, AS355N, AS355NP, AS-365N2, AS 365 N3, EC 155B, EC155B1, EC225LP, SA-365N, and SA-365N1 helicopters. This AD was prompted by a report of an unintentional activation of the hoist shear-button (shear-button) on the collective pitch handle during a night flight. This AD requires checking the operation of the shear- button safety-cap on each applicable collective pitch handle and prohibits installing certain part-numbered collective pitch handles or collective sticks with those part-numbered collective pitch handles installed unless certain requirements are met. The FAA is issuing this AD to address the unsafe condition on these products.
Applicability · by US fleet size
- AIRBUS HELICOPTERS EC225LP TCDS H4EU 7 tails
- AIRBUS HELICOPTERS EC155B1 TCDS H10EU 3 tails
- AIRBUS HELICOPTERS AS332L1 TCDS H4EU 3 tails
- AIRBUS HELICOPTERS AS355N TCDS H11EU 2 tails
- AIRBUS HELICOPTERS AS332L2 TCDS H4EU 2 tails
- AIRBUS HELICOPTERS AS355F2 TCDS H11EU 1 tails
- AIRBUS HELICOPTER AS355F1 TCDS H11EU 1 tails
Federal Register text
Verbatim; the Federal Register publication is the legally binding document. Cite: 90 FR 8656. View on Federal Register ↗
[Federal Register Volume 90, Number 20 (Friday, January 31, 2025)] [Rules and Regulations] [Pages 8656-8658] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR Doc No: 2025-02027]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2024-2332; Project Identifier MCAI-2022-01479-R; Amendment 39-22950; AD 2025-03-02] RIN 2120-AA64
Airworthiness Directives; Airbus Helicopters
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
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SUMMARY: The FAA is adopting a new airworthiness directive (AD) certain Airbus Helicopters Model AS332C, AS332C1, AS332L, AS332L1, AS332L2, AS355E, AS355F, AS355F1, AS355F2, AS355N, AS355NP, AS-365N2, AS 365 N3, EC 155B, EC155B1, EC225LP, SA-365N, and SA-365N1 helicopters. This AD was prompted by a report of an unintentional activation of the hoist shear-button (shear-button) on the collective pitch handle during a night flight. This AD requires checking the operation of the shear- button safety-cap on each applicable collective pitch handle and prohibits installing certain part-numbered collective pitch handles or collective sticks with those part-numbered collective pitch handles installed unless certain requirements are met. The FAA is issuing this AD to address the unsafe condition on these products.
DATES: This AD is effective March 7, 2025.
ADDRESSES: AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA-2024-2332; 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 final rule, the mandatory continuing airworthiness information (MCAI), any comments received, and other information. The address for Docket Operations is U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE, Washington, DC 20590.
FOR FURTHER INFORMATION CONTACT: Dan McCully, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: (404) 474-5548; email: [email protected].