Special Conditions: GE Aviation CT7-2E1 Turboshaft Engine Model
other · Rule · Final special conditions. · Published 2013-03-12 · Effective 2013-04-11 · 78 FR 15597
Document
Document number
2013-05676
Federal Register citation
78 FR 15597
Type
Rule
Action
Final special conditions.
Category
other
Publication date
2013-03-12
Effective date
2013-04-11
FAA docket
Docket No. FAA-2012-0745
Abstract
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.