Airworthiness Directive

AD 2016-08-17 81 FR 24010 Active

Federal Aviation Administration · 14 CFR part 39

FR document
2016-09236
Amendment
39-18494
Published
2016-04-25
Effective
2016-05-31
Models covered
3
Last live check
2026-09-30
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AD

2016-08-17

FR doc 2016-09236 · 81 FR 24010

AD 2016-08-17Published 2016-04-25Effective 2016-05-31

Supersedes 2010-19-51

Supersedence is read from the Federal Register text of the newer AD — the FAA publishes no structured field for it — and names only ADs held in our index.

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 installing a servo actuator with a new stainless steel piston rod.

Full official abstract

We are superseding Airworthiness Directive (AD) 2010-19-51 for Bell Helicopter Textron Canada (Bell) Model 222, 222B, 222U, 230, and 430 helicopters. AD 2010-19-51 required inspecting parts of the main rotor hydraulic servo actuator (servo actuator) for certain conditions and replacing any unairworthy parts before further flight. This new AD requires installing a servo actuator with a new stainless steel piston rod. This AD was prompted by a collective servo actuator malfunction. We are issuing this AD to detect corrosion on a piston rod, which could result in failure of the servo actuator and consequent loss of helicopter control.

More directives for Bell 222

  1. AD 2026-17-51 Airworthiness Directives; Bell Textron Canada Limited Helicopters 2026-08-28
  2. AD 2021-19-01 Airworthiness Directives; Bell Textron Canada Limited Helicopters 2021-09-08
  3. AD 2013-18-06 Airworthiness Directives; Bell Helicopter Textron Canada Limited (Bell) ... 2013-09-12
  4. AD 2010-26-51 Airworthiness Directives; Bell Helicopter Textron Canada Limited (BHTC) ... 2011-03-10
  5. AD 2010-19-51 Airworthiness Directives; Bell Helicopter Textron Canada Model 222, 222B... 2010-11-24

All Bell 222 directives

Applies to 3 models in our index