Airworthiness Directive

AD 2024-01-03 89 FR 4181 Active

Federal Aviation Administration · 14 CFR part 39

Requires revising the ALS of the existing EMM and the operator's existing approved engine maintenance or inspection program, as applicable, to incorporate new and more restrictive instructions and associated thresholds and…

FR document
2024-01218
Amendment
39-22654
Published
2024-01-23
Effective
2024-02-27
Models covered
1

Last live check: 2026-08-19

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AD

2024-01-03

FR doc 2024-01218 · 89 FR 4181

AD 2024-01-03Published 2024-01-23Effective 2024-02-27

Supersedes 2023-01-07

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 revising the ALS of the existing EMM and the operator's existing approved engine maintenance or inspection program, as applicable, to incorporate new and more restrictive instructions and associated thresholds and intervals for life-limited parts, as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference (IBR).

Full official abstract

The FAA is superseding Airworthiness Directive (AD) 2023-01- 07 for all GE Aviation Czech s.r.o. (GEAC) (type certificate previously held by WALTER Engines a.s., Walter a.s., and MOTORLET a.s.) Model H75- 100, H75-200, H80, H80-100, H80-200, H85-100, and H85-200 engines. AD 2023-01-07 required revising the airworthiness limitations section (ALS) of the existing engine maintenance manual (EMM) and the operator's existing approved maintenance or inspection program, as applicable, to incorporate updated coefficients and recalculate the cycles accumulated on critical parts. Since the FAA issued AD 2023-01- 07, the manufacturer revised the ALS of the EMM to introduce new and more restrictive airworthiness limitations and associated thresholds and intervals for life-limited parts, which prompted this AD action. This AD requires revising the ALS of the existing EMM and the operator's existing approved engine maintenance or inspection program, as applicable, to incorporate new and more restrictive instructions and associated thresholds and intervals for life-limited parts, as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference (IBR). The FAA is issuing this AD to address the unsafe condition on these products.

More directives for GE Aviation Czech M601/H80

  1. AD 2025-18-08 Airworthiness Directives; GE Aviation Czech s.r.o. (Type Certificate Pre... Effective 2025-10-21
  2. AD 2024-06-02 Airworthiness Directives; GE Aviation Czech s.r.o. (Type Certificate Pre... Effective 2024-04-11
  3. AD 2024-03-05 Airworthiness Directives; GE Aviation Czech s.r.o. (Type Certificate Pre... Effective 2024-04-17
  4. AD 2024-02-04 Airworthiness Directives; GE Aviation Czech s.r.o. (Type Certificate Pre... Effective 2024-03-28
  5. AD 2023-12-24 Airworthiness Directives; GE Aviation Czech s.r.o. (Type Certificate Pre... Effective 2023-08-15

All GE Aviation Czech M601/H80 directives

Applies to 1 model in our index