EASA CS-23
EASA CS-23 is the European Aviation Safety Agency Certification Specification for Normal, Utility, Aerobatic, and Commuter Category Aeroplanes.[1]
The somewhat relaxed certification procedure is available for aircraft satisfying the following criteria:
- Single-engine aeroplanes in the normal, utility and aerobatic categories that have a seating configuration, excluding the pilot seat(s), of 9 or fewer and a maximum certificated take-off weight MTOW of 5670 kg (12 500 lb) or less (these aircraft are also known as class B under EU-OPS 1),
- Twin-engined propeller-driven aeroplanes in the commuter category that have a seating configuration, excluding the pilot seat(s), of 19 or fewer and a maximum certificated take-off weight of 8618 kg (19 000 lb) or less (some of these aircraft are also known as class C under EU-OPS 1),
- Aeroplanes in this category can be used for flying in VFR, SVFR, NVFR and IFR conditions day and night and also in known icing conditions if they are equipped so,
- Aeroplane in this category can be pressurized
The main part of professional pilots training is done on this category. Example of typical CS-23 aeroplanes: Cessna 152,[2] Diamond DA20, Cessna 172, Piper PA-28 Cherokee Cessna 182, Mooney M20, Beechcraft Bonanza, Diamond DA42, Piper PA-34 Seneca, Piper PA-46, Beechcraft King Air, Cessna Citation Mustang.
See also
- List of current production certified light aircraft
- EASA CS-LSA
- EASA CS-VLA
- EASA CS-25
References
- ↑ "EASA CS-23 Takes Effect On Aug. 15". Aviation Week. Aviation Week. Retrieved 15 August 2018.
- ↑ "Safety Aspects of Light Aircraft Spin Resistance Concept" (PDF). EASA. EASA. Retrieved 15 August 2018.
External links
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