Airworthiness Directive

AD 2018-10-06 83 FR 23349 Active

Federal Aviation Administration · 14 CFR part 39

Requires repetitive inspections of the tail rotor (TR) driveshaft segment assemblies and a torque check of the TR adapter retention nuts.

FR document
2018-10491
Amendment
39-19281
Published
2018-05-21
Effective
2018-06-25
Models covered
1

Last live check: 2026-10-04

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AD

2018-10-06

FR doc 2018-10491 · 83 FR 23349

AD 2018-10-06Published 2018-05-21Effective 2018-06-25

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 repetitive inspections of the tail rotor (TR) driveshaft segment assemblies and a torque check of the TR adapter retention nuts.

Full official abstract

We are adopting a new airworthiness directive (AD) for Bell Model 407 helicopters. This AD requires repetitive inspections of the tail rotor (TR) driveshaft segment assemblies and a torque check of the TR adapter retention nuts. This AD was prompted by a report of an in- flight failure of the TR drive system. The actions of this AD are intended to detect and correct an unsafe condition on these products.

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All Bell 407 directives

Applies to 1 model in our index