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Special conditions

Special Conditions; Fairchild Model SA227 Series Airplanes to Type Certificate \nNo. A8SW

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 February 7, 1985 for Fairchild Aircraft. System: engine.

What it applies to

Applicant
Fairchild Aircraft
Makes
Fairchild Aircraft
Models
—
Published
February 7, 1985
Effective
March 10, 1985
The FAA's document
On the FAA's site

The FAA's summary their words, unchanged

This special conditions amendment is issued to become part of the type certification basis for new Fairchild Aircraft Corporation (FAC) Model SA227-PC airplanes to be added to Type Certificate No. A8SW. These airplanes will have novel or unusual design features associated with turbopropeller engine installations incorporating Automatic Power Reserve (APR) Systems for which the applicable airworthiness regulations do not contain adequate or appropriate safely standards. This amendment contains the additional safety standards which the Administrator finds necessary to establish a level of safety equivalent to that established in the regulation applicable to the SA227-PC airplane. A Notice of Proposed Special Conditions, Notice No. 23-ACE-6, was published in the Federal Register on September 6, 1984 (49 FR 35123) and one commenter, (FAC), responded to that notice.\n\nA similar set of special conditions were published as Notice of Proposed Special Conditions Notice No. 23-ACE-9 (49 FR 35121, September 6, 1984) for the British Aerospace Jetstream Model 3101 airplane. No comments were received in response to that notice. These special conditions were subsequently adopted as final special conditions and published in the Federal Register (50 FR 7, January 2, 1985), effective February 1, 1985.

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