Special Conditions; De Havilland Aircraft of Canada Ltd., Model DHC-8 Series \nAirplane
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 October 20, 1983 for De Havilland Aircraft Company of Canada. System: engine.
What it applies to
- Applicant
- De Havilland Aircraft Company of Canada
- Makes
- de Havilland
- Models
- —
- Published
- October 20, 1983
- Effective
- November 20, 1983
- The FAA's document
- On the FAA's site
The FAA's summary their words, unchanged
These special conditions are issued pursuant to §§ 21.16 and 21.17 of the Federal Aviation Regulations (FAR) to De Havilland Aircraft of Canada Ltd. for a type certificate for the DHC-8 series airplane. The DHC-8 airplane will have novel or unusual design features associated with an automatic takeoff power control system (ATPCS) for which the applicable airworthiness regulations do not contain adequate or appropriate safety standards. The ATPCS will allow the airplane to take off with less than maximum takeoff thrust approved for the airplane; and, if an engine fails, the system will automatically provide maximum takeoff thrust on the operating engine. These special conditions contain safety standards which the Administrator finds necessary to establish a level of safety equivalent to that provided by the regulations applicable to the De Havilland DHC-8 series airplane because of the novel or unusual features.
Source: FAA special conditions (final) from the Dynamic Regulatory System; the Federal Register carries the same notices.
