Airworthiness Directive

AD 2010-26-52 76 FR 67051 Active

Federal Aviation Administration · 14 CFR part 39

Prompted by another incident in which the blade tip weight separated from a blade during flight, causing vibration.

FR document
2011-27769
Amendment
39-16821
Published
2011-10-31
Effective
2011-11-15
Models covered
2

Last live check: 2026-10-04

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AD

2010-26-52

FR doc 2011-27769 · 76 FR 67051

AD 2010-26-52Published 2011-10-31Effective 2011-11-15

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.

Prompted by another incident in which the blade tip weight separated from a blade during flight, causing vibration.

Full official abstract

We are publishing in the Federal Register an amendment which was sent previously to all known U.S. owners and operators that supersedes an existing airworthiness directive (AD) for the specified Bell Helicopter Textron, Inc. (BHT) Model helicopters with certain tail rotor blades (blades). The superseded AD requires, before further flight, replacing certain blades with airworthy blades. This AD retains the requirements of the superseded AD but adds new blade part numbers (P/Ns) and serial numbers (S/Ns) to the applicability. This AD was prompted by another incident in which the blade tip weight separated from a blade during flight, causing vibration. This incident led to the determination that additional blades could be affected, and should be added to the applicability. We are issuing this AD to prevent loss of the blade tip weight, loss of a blade, and subsequent loss of control of the helicopter.

More directives for Bell 205 / 212

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All Bell 205 / 212 directives

Applies to 2 models in our index