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Special conditions

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.