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AD 2024-15808

Published 2024-07-18 · 3 models · 804 US-registered tails affected · Federal Register

Airworthiness Directives; Bell Textron Canada Limited Helicopters Federal Register ↗

Abstract

The FAA is adopting a new airworthiness directive (AD) for certain Bell Textron Canada Limited Model 407 helicopters. This AD was prompted by a report that a certain part-numbered fuel system standpipe assembly (standpipe) may have sharp edges at the interval weld joints due to a quality escape during the manufacturing process. This AD requires inspecting certain fuel system parts and, depending on the inspection results, taking corrective actions and performing a fuel quantity gauging system calibration. Depending on the results of the fuel quantity gauging system calibration, this AD requires performing additional corrective actions and repeating the fuel quantity gauging system calibration. The FAA is issuing this AD to address the unsafe condition on these products.

Applicability · by US fleet size

  • BELL HELICOPTER TEXTRON CANADA 407 418 tails
  • BELL 407 371 tails
  • BELL 222 15 tails

Federal Register text

Verbatim; the Federal Register publication is the legally binding document. Cite: 89 FR 58260. View on Federal Register ↗

[Federal Register Volume 89, Number 138 (Thursday, July 18, 2024)] [Rules and Regulations] [Pages 58260-58262] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR Doc No: 2024-15808]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2024-0232; Project Identifier MCAI-2023-00353-R; Amendment 39-22758; AD 2024-10-12] RIN 2120-AA64

Airworthiness Directives; Bell Textron Canada Limited Helicopters

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

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SUMMARY: The FAA is adopting a new airworthiness directive (AD) for certain Bell Textron Canada Limited Model 407 helicopters. This AD was prompted by a report that a certain part-numbered fuel system standpipe assembly (standpipe) may have sharp edges at the interval weld joints due to a quality escape during the manufacturing process. This AD requires inspecting certain fuel system parts and, depending on the inspection results, taking corrective actions and performing a fuel quantity gauging system calibration. Depending on the results of the fuel quantity gauging system calibration, this AD requires performing additional corrective actions and repeating the fuel quantity gauging system calibration. The FAA is issuing this AD to address the unsafe condition on these products.

DATES: This AD is effective August 22, 2024. The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of August 22, 2024.