Special Condition; Slingsby T67-M260 Airplane
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 August 11, 1992 for Slingsby Aviation. System: other and general.
What it applies to
- Applicant
- Slingsby Aviation
- Makes
- Slingsby Aviation
- Models
- —
- Published
- August 11, 1992
- Effective
- September 10, 1992
- The FAA's document
- On the FAA's site
The FAA's summary their words, unchanged
This special condition is being issued for the Slingsby T67-M260 airplane. The airplane will have a novel and unusual design feature when compared to the state of technology envisaged in the airworthiness standards of 14 CFR part 23 of the Federal Aviation Regulations (FAR). This novel and unusual design feature is the use of composite materials for primary flight structure, for which the regulations do not contain adequate or appropriate airworthiness standards. This final special condition contains the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that provided by the airworthiness standards of part 23.
Source: FAA special conditions (final) from the Dynamic Regulatory System; the Federal Register carries the same notices.