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Special conditions · electric or hybrid design

Special Conditions: General Electric Aircraft Engines Models CT7-6D, 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 May 27, 1999 for General Electric Aircraft Engines. System: electric propulsion.

What it applies to

Applicant
General Electric Aircraft Engines
Makes
General Electric
Models
—
Published
May 27, 1999
Effective
May 20, 1999
The FAA's document
On the FAA's site

The FAA's summary their words, unchanged

These special conditions are issued for the General Electric Aircraft Engines (GEAE) Models CT7-6D, CT7-6E and CT7-8 turboshaft engines. These engines will have 30-second one-engine-inoperative (OEI) and 2-minute OEI ratings. The applicable airworthiness standards do not contain appropriate safety standards for engine overspeed test requirements for these engine ratings. This document contains the additional safety standards for the overspeed test for these ratings under Sec. 33.27 that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards. This document also specifies the mandatory post-flight engine inspection and maintenance requirements for these ratings in accordance with Sec. 33.4.

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