Airworthiness Directive

AD 2002-11-09 67 FR 39844 Active

Federal Aviation Administration · 14 CFR part 39

Requires visually inspecting the forward hanger bearing bracket (bracket) for a crack.

FR document
02-14566
Amendment
39-12770
Published
2002-06-11
Effective
2002-07-16
Models covered
1

Last live check: 2026-10-04

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AD

2002-11-09

FR doc 02-14566 · 67 FR 39844

AD 2002-11-09Published 2002-06-11Effective 2002-07-16

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 visually inspecting the forward hanger bearing bracket (bracket) for a crack.

Full official abstract

This amendment adopts a new airworthiness directive (AD) for Bell Helicopter Textron Canada (BHTC) Model 407 helicopters that requires visually inspecting the forward hanger bearing bracket (bracket) for a crack. This amendment is prompted by reports of cracks in the bracket. The actions specified by this AD are intended to detect a crack in the bracket, to prevent loss of tail rotor drive or control and subsequent loss of control of the helicopter.

More directives for Bell 407

  1. AD 2026-14-07 Airworthiness Directives; Bell Textron Canada Limited Helicopters Effective 2026-08-21
  2. AD 2026-10-04 Airworthiness Directives; Bell Textron Canada Limited Helicopters Effective 2026-06-25
  3. AD 2025-13-01 Airworthiness Directives; Bell Textron Canada Limited Helicopters Effective 2025-07-08
  4. AD 2024-10-12 Airworthiness Directives; Bell Textron Canada Limited Helicopters Effective 2024-08-22
  5. AD 2023-17-51 Airworthiness Directives; Bell Textron Canada Limited Helicopters Effective 2023-09-21

All Bell 407 directives

Applies to 1 model in our index