Airworthiness Directive

AD 2000-20-18 65 FR 62275 Active

Federal Aviation Administration · 14 CFR part 39

FR document
00-26236
Amendment
39-11930
Published
2000-10-18
Effective
2000-11-22
Models covered
1
Last live check
2026-10-03
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AD

2000-20-18

FR doc 00-26236 · 65 FR 62275

AD 2000-20-18Published 2000-10-18Effective 2000-11-22

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 inspecting the brackets that attach each horizontal stabilizer slat (slat) to the stabilizer for a crack and replacing the slat assembly if a crack is found.

Full official abstract

This amendment adopts a new airworthiness directive (AD) for Bell Helicopter Textron Canada (BHTC) Model 407 helicopters. This AD requires inspecting the brackets that attach each horizontal stabilizer slat (slat) to the stabilizer for a crack and replacing the slat assembly if a crack is found. Installing airworthy segmented slat assemblies would be required prior to flight after December 31, 2000 and would constitute terminating action for the requirements of this AD. This amendment is prompted by an incident in which a slat separated from a helicopter. The actions specified by this AD are intended to prevent a slat from separating, impact with a main or tail rotor blade, 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