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Federal Register · Final Rule

Special Conditions: Pratt and Whitney Canada, PW220A; Flat 30-Second and 2-Minute OEI Rating.

Final Rule Final · effective Published 2025-12-15 Effective 2026-01-14 90 FR 57896 View on federalregister.gov ↗
Affects · Manufacturers · 14 CFR 33

Abstract

These special conditions are issued for the Pratt and Whitney Canada (PWC) aircraft engine model PW220A. This engine will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for engines. This design feature is an additional one engine inoperative (OEI) power rating that combines the 30-second and 2-minute OEI power ratings into a single rating. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.

Full text

13 paragraphs · 227 words.

[Federal Register Volume 90, Number 238 (Monday, December 15, 2025)] [Rules and Regulations] [Pages 57896-57898] From the Federal Register Online via the Government Publishing Office [www.gpo.gov] [FR Doc No: 2025-22759]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 33

[Docket No. FAA-2025-0950; Special Conditions No. 33-029-SC]

Special Conditions: Pratt and Whitney Canada, PW220A; Flat 30- Second and 2-Minute OEI Rating.

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final special conditions.

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SUMMARY: These special conditions are issued for the Pratt and Whitney Canada (PWC) aircraft engine model PW220A. This engine will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for engines. This design feature is an additional one engine inoperative (OEI) power rating that combines the 30-second and 2-minute OEI power ratings into a single rating. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.

DATES: These special conditions are effective January 14, 2026.

FOR FURTHER INFORMATION CONTACT: Philip Haberlen, Engine and Propulsion Section, AIR-625, Technical Policy Branch, Policy and Standards Division, Aircraft Certification Service, Federal Aviation Administration, 1200 District Avenue, Burlington, MA 01803; telephone 781-238-7770; email [email protected].

Verbatim from the Federal Register. The agency's published document is the authoritative source. federalregister.gov ↗