Special Conditions: Pratt & Whitney Canada, Inc. (Formerly United Aircraft of Canada, Limited), Model PT6T-9 Turboshaft Engine
Special conditions are rules the FAA writes for one design when the standard certification rules do not cover something new about it. These were published December 26, 2000 for Pratt & Whitney Canada INC. System: engine.
What it applies to
- Applicant
- Pratt & Whitney Canada INC
- Makes
- Pratt & Whitney
- Models
- —
- Published
- December 26, 2000
- Effective
- December 26, 2000
- The FAA's document
- On the FAA's site
The FAA's summary their words, unchanged
Pratt & Whitney Canada, Inc. (PWC) has applied for an amendment to type certificate (TC) #E22EA, to add a new model PT6T-9 turboshaft engine. The FAA has determined that this new model engine should be viewed as a derivative to the PT6T-3 engine. On June 8, 1970, the FAA issued Special Conditions (SC) No. 33-23-EA-6 for the PT6T-3 turboshaft engine model, and later amended those SC in 1970 to clarify a potential ambiguity in the vibration test requirements. In addition to the requirements contained in SC No. 33-23-EA-6, as amended, these new special conditions provide for 30-second one-engine-inoperative (OEI), 2-minute OEI, and continuous OEI ratings to be included in the PT6T-9 turboshaft engine model power ratings. The special conditions will define the changes to the engine certification basis that are required to establish a level of safety equivalent to the current requirements of 14 CFR part 33, for the new PWC PT6T-9 turboshaft engine model.
Source: FAA special conditions (final) from the Dynamic Regulatory System; the Federal Register carries the same notices.
