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Special conditions · electric or hybrid design · engine

Special Conditions: GE Aviation CT7-2E1 Turboshaft Engine Model

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 March 11, 2013 for General Electric Aviation. System: electric propulsion.

What it applies to

Applicant
General Electric Aviation
Makes
General Electric Aviation
Models
—
Published
March 11, 2013
Effective
April 10, 2013
The FAA's document
On the FAA's site

The FAA's summary their words, unchanged

These final special conditions are issued for the General Electric Aviation (GE) CT7-2E1 engine model. This engine model will have a novel or unusual design feature, which is a combination of two existing ratings into a new rating called ``flat 30-second and 2-minute OEI'' rating. This rating is intended for the continuation of flight of a multi-engine rotorcraft after one engine becomes inoperative. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These final special conditions contain the additional safety standards the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.

Source: FAA special conditions (final) from the Dynamic Regulatory System; the Federal Register carries the same notices.