Aircraft › Flight Design › CT Series › CTLS-ELA
The Flight Design CTLS-ELA is a model in the CT Series family. It is described here as a Two-seat composite high-wing piston single. EASA type-certificate reference: EASA.A.537.
Flight Design CTLS-ELA specifications
| Manufacturer | Flight Design |
|---|---|
| Model | CTLS-ELA |
| Aircraft type | Two-seat composite high-wing piston single |
| Seats | 2 |
| Landing gear | Fixed tricycle |
| Certification | EASA EASA.A.537 |
Flight Design CTLS-ELA weights and capacities
| Maximum takeoff weight | 1,323 lb |
|---|---|
| Standard fuel capacity | 34.3 gal total |
Use the CTLS-ELA AFM for baggage and loading limits.
Flight Design CTLS-ELA engine and configuration
| Engine | BRP-Rotax · 912 S · 100 hp |
|---|
Baggage and loading applicability
| Baggage | Use the CTLS-ELA AFM for baggage and loading limits. |
|---|
Flight Design CTLS-ELA history and development
The CTLS-ELA is the EASA-certified member of the Flight Design CT family. It is a two-seat composite high-wing aeroplane with fixed tricycle gear and Rotax 912-series power. The certified ELA version is associated with a 600 kg maximum takeoff mass. CT-series technical data identify about 130 L fuel capacity. National ultralight and S-LSA CT variants can use different maximum masses or equipment and should not be merged into this reference.
Flight Design CTLS-ELA fuel capacity
Standard total fuel: 34.3 U.S. gallons. CT-family technical data identify approximately 130 L fuel capacity.
Flight Design CTLS-ELA model applicability and configuration
This page is specific to CTLS-ELA under EASA.A.537. Confirm serial number, Rotax installation, parachute/equipment fit and AFM revision before applying model-level loading data.
Flight Design CTLS-ELA weight and balance
Maximum takeoff weight: 1,323 lb. Use the CTLS-ELA AFM for baggage and loading limits. The represented MTOW is 600 kg (1,323 lb). Fuel capacity is approximately 130 L (34.3 U.S. gal). Operational CG and baggage limits come from the individual aircraft AFM. 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 CTLS-ELA calculator.
Flight Design CTLS-ELA frequently asked questions
What engine does the Flight Design CTLS-ELA use?
The engine listed for this model is BRP-Rotax 912 S.
What is the maximum takeoff weight of the Flight Design CTLS-ELA?
The represented maximum takeoff weight is 1,323 lb.
Reference sources
EASA: Type Certificate Data Sheet EASA.A.537 - Flight Design CT
Flight Design: CTLS/CT technical data