Airworthiness Directive

AD 2005-21-03 70 FR 60203 Active

Federal Aviation Administration · 14 CFR part 39

FR document
05-20677
Amendment
39-14341
Published
2005-10-17
Effective
2005-11-21
Models covered
1
Last live check
2026-10-03
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AD

2005-21-03

FR doc 05-20677 · 70 FR 60203

AD 2005-21-03Published 2005-10-17Effective 2005-11-21

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 replacing any affected serial-numbered blade with an airworthy blade.

Full official abstract

This amendment adopts a new airworthiness directive (AD) for the specified Bell Helicopter Textron Canada (BHTC) model helicopters that requires, before the first flight of each day, checking the tail rotor blade (blade) root doublers (doublers) for an edge void or de- bond on both sides of each blade, and if an edge void or de-bond is found, replacing the unairworthy blade with an airworthy blade. This AD also requires replacing any affected serial-numbered blade with an airworthy blade. This amendment is prompted by reports of de-bond of the doublers due to inadequate surface preparation resulting in poor adherence of the doublers. The actions specified by this AD are intended to prevent loss of a blade, loss of tail rotor control, and subsequent loss of control of the helicopter.

More directives for Bell 206 JetRanger / LongRanger

  1. AD 2023-06-05 Airworthiness Directives; Bell Textron Canada Limited Helicopters 2023-04-14
  2. AD 2022-22-08 Airworthiness Directives; Bell Textron Canada Limited (Type Certificate ... 2022-11-18
  3. AD 2022-20-04 Airworthiness Directives; Bell Textron Canada Limited Helicopters 2022-11-18
  4. AD 2021-26-08 Airworthiness Directives; Bell Textron Canada Limited Helicopters 2021-12-23
  5. AD 2021-24-15 Airworthiness Directives; Bell Textron Canada Limited Helicopters 2021-12-14

All Bell 206 JetRanger / LongRanger directives

Applies to 1 model in our index