Airworthiness Directive

AD 2023-01-07 88 FR 2501 Active

Federal Aviation Administration · 14 CFR part 39

FR document
2023-00490
Amendment
39-22301
Published
2023-01-17
Effective
2023-02-21
Models covered
1
Last live check
2026-10-02
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AD

2023-01-07

FR doc 2023-00490 · 88 FR 2501

AD 2023-01-07Published 2023-01-17Effective 2023-02-21

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 revising the ALS of the existing EMM and the operator's existing approved maintenance or inspection program, as applicable, to incorporate the updated coefficients and recalculate the cycles accumulated on critical parts.

Full official abstract

The FAA is adopting a new airworthiness directive (AD) for all GE Aviation Czech s.r.o. (GEAC) H75-100, H75-200, H80, H80-100, H80- 200, H85-100, and H85-200 model turboprop engines. This AD is prompted by the manufacturer revising the airworthiness limitations section (ALS) of the existing engine maintenance manual (EMM) to introduce updated coefficients for the calculation of the cyclic life and safe life for the main shaft. This AD requires revising the ALS of the existing EMM and the operator's existing approved maintenance or inspection program, as applicable, to incorporate the updated coefficients and recalculate the cycles accumulated on critical parts. The FAA is issuing this AD to address the unsafe condition on these products.

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  3. AD 2024-03-05 Airworthiness Directives; GE Aviation Czech s.r.o. (Type Certificate Pre... 2024-03-13
  4. AD 2024-02-04 Airworthiness Directives; GE Aviation Czech s.r.o. (Type Certificate Pre... 2024-02-22
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All GE Aviation Czech M601/H80 directives

Applies to 1 model in our index