Airworthiness Directive

AD 2006-08-07 71 FR 19624 Active

Federal Aviation Administration · 14 CFR part 39

Requires certain inspections and measurements of the upper tail rotor vertical gearbox (gearbox), vertical shaft (shaft) and shaft housing (housing) and their associated parts; and of the intermediate gear box bushing (bushing).

FR document
06-3536
Amendment
39-14562
Published
2006-04-17
Effective
2006-05-02
Models covered
1

Last live check: 2026-10-04

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AD

2006-08-07

FR doc 06-3536 · 71 FR 19624

AD 2006-08-07Published 2006-04-17Effective 2006-05-02

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 certain inspections and measurements of the upper tail rotor vertical gearbox (gearbox), vertical shaft (shaft) and shaft housing (housing) and their associated parts; and of the intermediate gear box bushing (bushing).

Full official abstract

This amendment adopts a new airworthiness directive (AD) for the specified Brantly International, Inc. (Brantly) model helicopters. This action requires certain inspections and measurements of the upper tail rotor vertical gearbox (gearbox), vertical shaft (shaft) and shaft housing (housing) and their associated parts; and of the intermediate gear box bushing (bushing). This amendment is prompted by an accident and an incident report of fatigue cracking of a shaft. The actions specified in this AD are intended to prevent fatigue cracking of a shaft, failure of a shaft, and subsequent loss of control of the helicopter.

More directives for Brantly B-2 / 305

  1. AD 2021-26-09 Airworthiness Directives; Brantly Helicopters Industries U.S.A. Co., Ltd... Effective 2022-01-19
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All Brantly B-2 / 305 directives

Applies to 1 model in our index