Special Conditions; Cessna Model 208 Series Airplanes
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 June 26, 1983 for Cessna Aircraft Company. System: engine.
What it applies to
- Applicant
- Cessna Aircraft Company
- Makes
- Cessna
- Models
- —
- Published
- June 26, 1983
- Effective
- July 26, 1983
- The FAA's document
- On the FAA's site
The FAA's summary their words, unchanged
These Special Conditions are issued under 21.16 and 21.101(b) of the Federal Aviation Regulations (FAR) to the Cessna Aircraft Company (Cessna) for the Cessna Model 208 Series airplanes. The airplane will have novel and unusual design features associated with a turbine engine installation a single engine airplane for which the applicable airworthiness standards of Part 23 of the FAR do not contain adequate or appropriate safety standards. These Special Conditions contain the safety standards which the Administrator finds necessary to establish a level of safety equivalent to that provided in the regulations for reciprocating-engine-powered, single engine airplanes.
Source: FAA special conditions (final) from the Dynamic Regulatory System; the Federal Register carries the same notices.
