Airworthiness Directive

AD 2011-08-06 76 FR 20231 Active

Federal Aviation Administration · 14 CFR part 39

FR document
2011-8470
Amendment
39-16656
Published
2011-04-12
Effective
2011-05-17
Models covered
1
Last live check
2026-10-02
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AD

2011-08-06

FR doc 2011-8470 · 76 FR 20231

AD 2011-08-06Published 2011-04-12Effective 2011-05-17

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 removing certain power turbine rotors from service using a specific drawdown schedule.

Full official abstract

We are adopting a new airworthiness directive (AD) for the products listed above. This AD requires removing certain power turbine rotors from service using a specific drawdown schedule. This AD was prompted by reports of fatigue cracks in the airfoil of the power turbine blades. We are issuing this AD to prevent fracture of the power turbine blade airfoil, which could result in sudden loss of engine power and prevent continued safe flight or safe landing.

More directives for Honeywell LTP101

  1. AD 2009-24-12 Airworthiness Directives; Honeywell International Inc. LTS101 Series Tur... 2009-11-30
  2. AD 2002-03-09 R1 Airworthiness Directives; Honeywell International Inc. (formerly AlliedS... 2002-03-21
  3. AD 2002-03-09 Airworthiness Directives; Honeywell International Inc. (Formerly AlliedS... 2002-02-20
  4. AD 2001-25-04 Airworthiness Directives; Honeywell International Inc. Models LTS101-600... 2001-12-19
  5. AD 2001-22-07 Airworthiness Directives; Honeywell International, Inc. LTP 101 Series T... 2001-10-26

All Honeywell LTP101 directives

Applies to 1 model in our index