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Special conditions · electric or hybrid design

Special Conditions: General Electric Aircraft Engines Model CT7-6E and CT7-8 Turboshaft Engines

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 August 9, 2000 for General Electric Aircraft Engines. System: electric propulsion.

What it applies to

Applicant
General Electric Aircraft Engines
Makes
General Electric
Models
—
Published
August 9, 2000
Effective
August 9, 2000
The FAA's document
On the FAA's site

The FAA's summary their words, unchanged

These special conditions are issued for General Electric Aircraft Engines (GEAE) models CT7-6E and CT7-8 turboshaft engines. These engines will have a novel or unusual rated 30-minute power that makes the issue of these special conditions necessary. The existing airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These special conditions contain the additional safety standards the Administrator considers to establish a level of safety equivalent to that established by existing airworthiness standards. The rated 30-minute power provides necessary increased rotorcraft hover time to enable operators to better perform critical, life-saving search and rescue missions. For this reason and because a delay would not be in the public interest, the FAA has determined that good cause exists for adopting these special conditions immediately upon publication.

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