Airworthiness Directive

AD 2003-02-06 68 FR 3379 Active

Federal Aviation Administration · 14 CFR part 39

FR document
03-1304
Amendment
39-13023
Published
2003-01-24
Effective
2003-02-10
Models covered
1
Last live check
2026-09-30
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AD

2003-02-06

FR doc 03-1304 · 68 FR 3379

AD 2003-02-06Published 2003-01-24Effective 2003-02-10

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 certain tailboom gearbox support castings (castings) for cracks and replacing the tailboom assembly if a crack is found.

Full official abstract

This amendment adopts a new airworthiness directive (AD) for Bell Helicopter Textron Canada Limited (Bell) Model 407 helicopters. This action requires visually inspecting certain tailboom gearbox support castings (castings) for cracks and replacing the tailboom assembly if a crack is found. This amendment is prompted by an incident in which a crack was discovered on the casting that holds the tail rotor gearbox and vertical fin. The actions specified in this AD are intended to detect a crack in the casting and prevent failure of the casting, loss of the vertical fin and tail rotor, 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 2026-07-17
  2. AD 2026-10-04 Airworthiness Directives; Bell Textron Canada Limited Helicopters 2026-05-21
  3. AD 2025-13-01 Airworthiness Directives; Bell Textron Canada Limited Helicopters 2025-06-23
  4. AD 2024-10-12 Airworthiness Directives; Bell Textron Canada Limited Helicopters 2024-07-18
  5. AD 2023-17-51 Airworthiness Directives; Bell Textron Canada Limited Helicopters 2023-09-06

All Bell 407 directives

Applies to 1 model in our index