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Airworthiness Directive

AD 2022-26-01: Turbine Engine Combustion Section

Airworthiness Directives; GE Aviation Czech s.r.o. (Type Certificate Previously Held by WALTER Engines a.s., Walter a.s., and MOTORLET a.s.) Turboprop Engines

Effective
Jan 26, 2023
Published
Dec 22, 2022
Registered aircraft
18

Models this AD may apply to

AI-extracted — verify against original

Matched from the AD's applicability section. Applicability must be confirmed by a mechanic against the aircraft's records.

Engines

  • MOTORLET M601D-11
  • MOTORLET M601E-11
  • MOTORLET M601E-11A
  • MOTORLET M601E-11AS
  • MOTORLET M601E-11S
  • MOTORLET M601F
  • WALTER M601D-11
  • WALTER M601E-11
  • WALTER M601E-11A
  • WALTER M601E-11AS
  • WALTER M601E-11S
  • WALTER M601F
  • Only with: Engines installed on single-engine airplanes with combustion chamber outer liner P/N M601-229.3, M601-229.3A, M601-229.3B, M601-229.31A, or M601-229.31B installed.
  • Only with: Engines installed on single-engine airplanes with combustion chamber outer liner P/N M601-229.3, M601-229.3A, M601-229.3B, M601-229.31A, or M601-229.31B installed.

Applicability

From the AD text
This AD applies to GE Aviation Czech s.r.o. (GEAC) M601D-11, M601E-11, M601E-11A, M601E-11AS, M601E-11S, M601F, H75-100, H75-200, H80, H80-100, H80-200, H85-100, and H85-200 model turboprop engines installed on single-engine airplanes, with an installed combustion chamber outer liner having part numbers (P/Ns) M601-229.3, M601-229.3A, M601-229.3B, M601-229.31A, or M601-229.31B.

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