Special Conditions: Canadair CL-600-2A12 (CL-601)
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 March 23, 1983 for Canadair LTD. System: airframe structure.
What it applies to
- Applicant
- Canadair LTD
- Makes
- Canadair
- Models
- —
- Published
- March 23, 1983
- Effective
- March 7, 1983
- The FAA's document
- On the FAA's site
The FAA's summary their words, unchanged
This action issues special conditions for the Canadair CL-600-2A12 (CL-601) series airplane. The special conditions originally issued for the CL-600-1A11 are amended for this derivative model (CL-601) because an increase in operating altitude is anticipated. Additionally, the CL-600-2A12 (CL-601) airplane will have novel and unusual design features associated with an automatic takeoff thrust control system (ATTCS) for which the applicable airworthiness regulations do not have adequate or appropriate safety standards. These special conditions contain safety standards which the Administrator finds necessary to establish a level of safety equivalent to that established in the regulations applicable to the Canadair CL-600-2A12 (CL-601) series airplane because of novel and unusual features.
Source: FAA special conditions (final) from the Dynamic Regulatory System; the Federal Register carries the same notices.