AircraftDirectives
MembershipSign inCreate free account
Menu
Airworthiness Directive

AD 2024-06-02 89 FR 21196 Superseded

Federal Aviation Administration · 14 CFR part 39

Requires a one-time detailed visual inspection of the compressor case pad welds for any crack, and replacement of the compressor case if necessary, as specified in a European Union Aviation Safety Agency (EASA) AD, which is…

Superseded by AD 2025-18-08Federal Register (opens in a new tab)FAA DRS (opens in a new tab)

FR document
2024-06430
Amendment
39-22707
Published
2024-03-27
Effective
2024-04-11
Models covered
1

Last live check: 2026-08-19

Printed from https://aircraftdirectives.com/ad/2024-06-02 · AircraftDirectives restates official FAA and manufacturer records; the official sources named on this sheet control. Not an airworthiness determination.

This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.

Opens your browser's print dialog. Choose “Save as PDF” to export a file. Keyboard: Ctrl+P or Cmd+P.

AD

2024-06-02

FR doc 2024-06430 · 89 FR 21196

AD 2024-06-02Published 2024-03-27Effective 2024-04-11

Superseded by 2025-18-08

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 a one-time detailed visual inspection of the compressor case pad welds for any crack, and replacement of the compressor case if necessary, as specified in a European Union Aviation Safety Agency (EASA) AD, which is incorporated by reference (IBR).

Full official abstract

The FAA is adopting a new airworthiness directive (AD) 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 M601D-11, M601E-11, M601E-11A, M601E-11AS, M601E-11S, and M601F engines. This AD was prompted by a report of a crack on the centrifugal compressor case mount pad weld area, caused by a non-conforming welding (lack of welding penetration). This AD requires a one-time detailed visual inspection of the compressor case pad welds for any crack, and replacement of the compressor case if necessary, 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 2024-03-05 Airworthiness Directives; GE Aviation Czech s.r.o. (Type Certificate Pre... Effective 2024-04-17
  3. AD 2024-02-04 Airworthiness Directives; GE Aviation Czech s.r.o. (Type Certificate Pre... Effective 2024-03-28
  4. AD 2024-01-03 Airworthiness Directives; GE Aviation Czech s.r.o. (Type Certificate Pre... Effective 2024-02-27
  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

View on Federal Register (opens in a new tab) View this AD in FAA DRS (opens in a new tab) Print AD packet (opens the full Federal Register document in a new tab)

Applies to 1 model in our index