2024-24365. Airworthiness Directives; Safran Helicopter Engines, S.A. (Type Certificate Previously Held by Turbomeca, S.A.) Engines
Estimated Costs
Action Labor cost Parts cost Cost per product Cost on U.S. operators Recalculate cycle lives 2 work-hours × $85 per hour = $170 $0 $170 $0 Replace axial wheel 1 8 work-hours × $85 per hour = $680 118,703 119,383 0 Replace axial wheel 2 8 work-hours × $85 per hour = $680 74,023 74,703 0 Replace axial wheel 3 8 work-hours × $85 per hour = $680 86,939 87,619 0 Replace centrifugal impeller 8 work-hours × $85 per hour = $680 164,583 165,263 0 Replace high-pressure turbine (HPT) disk 1 8 work-hours × $85 per hour = $680 97,800 98,480 0 Replace HPT disk 2 8 work-hours × $85 per hour = $680 92,284 92,964 0 Replace injection wheel 8 work-hours × $85 per hour = $680 76,799 77,479 0
Document Information
- Effective Date:
- 11/26/2024
- Published:
- 10/22/2024
- Department:
- Federal Aviation Administration
- Entry Type:
- Rule
- Action:
- Final rule.
- Document Number:
- 2024-24365
- Dates:
- This AD is effective November 26, 2024.
- Pages:
- 84272-84274 (3 pages)
- Docket Numbers:
- Docket No. FAA-2024-1691, Project Identifier MCAI-2023-01269-E, Amendment 39-22847, AD 2024-19-05
- RINs:
- 2120-AA64: Airworthiness Directives
- RIN Links:
- https://www.federalregister.gov/regulations/2120-AA64/airworthiness-directives
- Topics:
- Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety
- PDF File:
- 2024-24365.pdf
- Supporting Documents:
- » U.S. DOT/FAA - Supplemental AD Documents
- » U.S. DOT/FAA - Supplemental AD Documents
- CFR: (1)
- 14 CFR 39