Airworthiness Directive

AD 2026-15-06 91 FR 47953 Active

Federal Aviation Administration · 14 CFR part 39

FR document
2026-15365
Amendment
39-23418
Published
2026-07-30
Effective
2026-09-03
Models covered
1

Last live check: 2026-08-19

This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.
AD

2026-15-06

FR doc 2026-15365 · 91 FR 47953

AD 2026-15-06Published 2026-07-30Effective 2026-09-03

Supersedes 2024-02-55

Supersedence is read from the Federal Register text of the newer AD — the FAA publishes no structured field for it — and names only ADs held in our index.

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Requires the inspection requirements of AD 2024-02- 55 and would limit the applicability to exclude certain serial numbered BTCL Model 505 helicopters with an improved design vertical stabilizer top end cap installed at production.

Full official abstract

The FAA is superseding Airworthiness Directive (AD) 2024-02- 55, which applies to certain Bell Textron Canada Limited (BTCL) Model 505 helicopters. AD 2024-02-55 required initial and recurring inspections of the vertical stabilizer top end cap assembly and corrective action if a crack is found. Since the FAA issued AD 2024-02- 55, the manufacturer introduced a new one- piece vertical stabilizer machined top end cap assembly, which is implemented during production, and designed a new replacement for the vertical stabilizer machined top end cap assembly currently in service. This AD continues to require the inspection requirements of AD 2024-02- 55 and would limit the applicability to exclude certain serial numbered BTCL Model 505 helicopters with an improved design vertical stabilizer top end cap installed at production. This AD also requires replacing the vertical stabilizer top end cap assembly with an improved design top end cap assembly, which constitutes a terminating action for the recurring detailed visual inspections. The FAA is issuing this AD to address the unsafe condition on these products.

More directives for Bell 505 Jet Ranger X

  1. AD 2026-18-10 Airworthiness Directives; Bell Textron Canada Limited Helicopters Effective 2026-10-22
  2. AD 2026-16-02 Airworthiness Directives; Bell Textron Canada Limited Helicopters Effective 2026-09-10
  3. AD 2026-05-51 Airworthiness Directives; Bell Textron Canada Limited Helicopters Effective 2026-04-16
  4. AD 2025-22-03 Airworthiness Directives; Bell Textron Canada Limited Helicopters Effective 2025-11-20
  5. AD 2025-18-10 Airworthiness Directives; Bell Textron Canada Limited Helicopters Effective 2025-09-25

All Bell 505 Jet Ranger X directives

Applies to 1 model in our index