Aircraft › Evektor › EV-97 VLA › EV-97 VLA
The Evektor EV-97 VLA is a model in the EV-97 VLA family. It is described here as a Two-seat all-metal low-wing piston single. EASA type-certificate reference: EASA.A.029.
Evektor EV-97 VLA specifications
| Manufacturer | Evektor |
|---|---|
| Model | EV-97 VLA |
| Aircraft type | Two-seat all-metal low-wing piston single |
| Seats | 2 |
| Landing gear | Fixed tricycle |
| Certification | EASA EASA.A.029 |
Evektor EV-97 VLA weights and capacities
| Maximum takeoff weight | 992 lb |
|---|---|
| Standard fuel capacity | 17.7 gal total / 17 gal usable |
Use the approved EV-97 VLA flight manual for baggage station and mass limits.
Evektor EV-97 VLA engine and configuration
| Engine | BRP-Rotax · 912 S · 100 hp |
|---|
Baggage and loading applicability
| Baggage | Use the approved EV-97 VLA flight manual for baggage station and mass limits. |
|---|
Evektor EV-97 VLA history and development
The EV-97 VLA is the certified very-light-aircraft member of Evektor's two-seat low-wing family. EASA.A.029 describes an all-metal, side-by-side, fixed-tricycle-gear aeroplane powered by the Rotax 912 S. The TCDS gives 73.5 kW takeoff power, a 67 L total fuel capacity and 64.5 L usable. This page deliberately represents the EASA VLA type rather than later SportStar RTC or national ultralight variants, which can have different maximum masses and operating data.
Evektor EV-97 VLA fuel capacity
Standard total fuel: 17.7 U.S. gallons. Standard usable fuel: 17 U.S. gallons. Fuel type: EN228 unleaded automotive fuel or AVGAS 100LL.
Evektor EV-97 VLA model applicability and configuration
Do not interchange EV-97 VLA data with SportStar RTC or national ultralight configurations. Use the AFM and loading schedule for the individual aircraft.
Evektor EV-97 VLA weight and balance
Maximum takeoff weight: 992 lb. Use the approved EV-97 VLA flight manual for baggage station and mass limits. The fuel system represented here contains 67 L total and 64.5 L usable. Operational loading must remain within the EASA-approved mass/CG envelope and the aircraft's current empty-mass data. Use the approved aircraft-specific documentation and current weight-and-balance record for operational calculations. WBcalc does not currently provide a model-specific Evektor EV-97 VLA calculator.
Evektor EV-97 VLA frequently asked questions
What engine does the Evektor EV-97 VLA use?
The engine listed for this model is BRP-Rotax 912 S.
What is the maximum takeoff weight of the Evektor EV-97 VLA?
The represented maximum takeoff weight is 992 lb.
How much usable fuel does the Evektor EV-97 VLA carry?
The represented standard usable fuel capacity is 17 U.S. gallons.
Reference sources
EASA: Type Certificate Data Sheet EASA.A.029 - EV-97 VLA