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Lists key dimensions, airfoils, engine, and propeller specifications.
Specifies fuel type, total capacity, usable fuel, and acrobatic requirements.
Specifies VNE, VNO, and maneuvering speeds for normal and acrobatic flight.
Defines maximum allowed empty, takeoff, and landing weights.
Step-by-step procedures for engine failures and malfunctions.
Outlines procedures for emergency and precautionary landings.
Covers engine fires on the ground and in flight.
Describes steps for abandoning the aircraft and using a parachute.
Steps for before take-off checks and the take-off maneuver.
Steps for descent, approach, before landing, and normal landing.
General guidance and procedures for performing acrobatic maneuvers.
Example calculations and graphical representation of CG determination.
Tables for calculating weights and moments for pilot and fuel loads.
Graphical representation of weight and CG operational limits.
General| Manufacturer | Extra Flugzeugbau |
|---|---|
| Role | Aerobatic aircraft |
| Crew | 1 |
| Gross weight | 950 kg (2, 094 lb) |
| Engine | Lycoming AEIO-540-L1B5 |
| G-limits | +10/-10 |
| First flight | 1988 |
| Power | 300 hp (224 kW) |
| Maximum speed | 407 km/h (253 mph) |
| Stall speed | 104 km/h (65 mph) |
