Airworthiness Directive

AD 2015-15-04 80 FR 43615 Active

Federal Aviation Administration · 14 CFR part 39

Requires removing a certain part-numbered main rotor (M/R) blade grip (grip) from service.

FR document
2015-17953
Amendment
39-18213
Published
2015-07-23
Effective
2015-08-07
Models covered
1

Last live check: 2026-10-04

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AD

2015-15-04

FR doc 2015-17953 · 80 FR 43615

AD 2015-15-04Published 2015-07-23Effective 2015-08-07

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 removing a certain part-numbered main rotor (M/R) blade grip (grip) from service.

Full official abstract

We are adopting a new airworthiness directive (AD) for certain Bell Helicopter Textron, Inc. (Bell), Model 204B, 205A, 205A-1, and 212 helicopters. This AD requires removing a certain part-numbered main rotor (M/R) blade grip (grip) from service. This AD is prompted by an error in a parts manufacturer approval (PMA) that incorrectly allows installation of the grips on the Bell Model 212. The actions specified in this AD are intended to prevent grip failure, separation of the M/R blade, and subsequent loss of control of the helicopter.

More directives for Bell 205 / 212

  1. AD 2024-16-19 Airworthiness Directives; Bell Textron Inc. Helicopters Effective 2024-11-08
  2. AD 2024-17-02 Airworthiness Directives; Bell Textron Inc. Helicopters Effective 2024-11-08
  3. AD 2024-19-17 Airworthiness Directives; Bell Textron Inc. and Various Restricted Categ... Effective 2024-10-11
  4. AD 2022-20-14 Airworthiness Directives; Bell Textron Inc., Helicopters and Various Res... Effective 2022-12-27
  5. AD 2022-22-12 Airworthiness Directives; Bell Textron Inc., Erickson 214 Holdings, LLC,... Effective 2022-11-22

All Bell 205 / 212 directives

Applies to 1 model in our index