Aircraft › Flight Design › F2-CS23 › F2-CS23
The Flight Design F2-CS23 is a model in the F2-CS23 family. It is described here as a Two-seat composite high-wing piston single. EASA type-certificate reference: EASA.A.647.
Flight Design F2-CS23 specifications
| Manufacturer | Flight Design |
|---|---|
| Model | F2-CS23 |
| Aircraft type | Two-seat composite high-wing piston single |
| Seats | 2 |
| Landing gear | Fixed tricycle |
| Certification | EASA EASA.A.647 |
Flight Design F2-CS23 weights and capacities
| Maximum takeoff weight | 1,433 lb |
|---|---|
| Standard fuel capacity | 35.7 gal total |
| Maximum baggage | 110 lb combined |
Flight Design F2-CS23 engine and configuration
| Engine | BRP-Rotax · 912 iS · 100 hp |
|---|
Flight Design F2-CS23 history and development
The F2-CS23 is the certified CS-23 development of Flight Design's F-series two-seat composite high-wing aircraft. EASA.A.647 was issued in December 2021. The certified production configuration uses a 100 hp Rotax 912 iS-family engine and a 650 kg maximum takeoff mass. Published F2 technical material identifies roughly 135 L fuel capacity and a 50 kg baggage allowance. The CS-23 F2 must be kept distinct from 600 kg LSA/ultralight F2 configurations.
Flight Design F2-CS23 fuel capacity
Standard total fuel: 35.7 U.S. gallons. Published F2 technical data list approximately 135 L fuel capacity.
Flight Design F2-CS23 model applicability and configuration
This page represents the EASA CS-23 model, not the lighter LSA configuration. Confirm AFM revision, engine designation, parachute installation and equipment fit for the individual aircraft.
Flight Design F2-CS23 weight and balance
Maximum takeoff weight: 1,433 lb. Maximum combined baggage: 110 lb. Maximum takeoff mass is 650 kg (1,433 lb). Published F2 data identify about 135 L fuel and 50 kg baggage capacity. Use aircraft-specific empty weight and CG for flight planning. Use the approved aircraft-specific documentation and current weight-and-balance record for operational calculations. WBcalc does not currently provide a model-specific Flight Design F2-CS23 calculator.
Flight Design F2-CS23 frequently asked questions
What engine does the Flight Design F2-CS23 use?
The engine listed for this model is BRP-Rotax 912 iS.
What is the maximum takeoff weight of the Flight Design F2-CS23?
The represented maximum takeoff weight is 1,433 lb.
Reference sources
EASA: Type Certificate Data Sheet EASA.A.647 - F2-CS23
Flight Design: F2-CS23 certification and technical data