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General| Type | Electric Aircraft |
|---|---|
| Manufacturer | Pipistrel |
| Powerplant | Electric |
| Engine | Pipistrel E-811 |
| Power | 57.6 kW (77 hp) |
| Seats | 2 |
| Certification | EASA CS-LSA |
| Endurance | 50 minutes |
| Wingspan | 10.71 m |
| Height | 1.85 m |
| Empty Weight | 428 kg |
| Maximum Takeoff Weight | 600 kg |
| Payload | 172 kg |
Overview of the contents and purpose of Section 1.
Detailed description of the VELIS Electro's construction and features.
Illustrative drawings showing the aircraft's dimensions and profile.
Key dimensions and weight specifications of the aircraft.
Definitions and explanations of terms used throughout the handbook.
Overview of operating limitations for safe aircraft usage.
Specifies the critical airspeed limits for various flight conditions.
Defines the operational limits for the engine and propeller systems.
Critical weight and CG limits for safe flight envelope.
Lists specific restrictions and prohibitions for aircraft operation.
General guidance for handling emergencies and critical flight situations.
Details on the aircraft's systems for warning and caution indications.
Procedures for handling emergencies occurring on the ground.
Procedures for responding to emergencies during flight.
Procedures for handling landings under emergency conditions.
Overview of standard operating procedures for the aircraft.
Specifies recommended airspeeds for standard flight phases.
Detailed checklist for preflight checks before each flight.
Step-by-step guide for performing a normal take off.
Detailed procedures for normal and special landing conditions.
Explanation of the performance data and its derivation.
Table showing temperature variations relative to ISA conditions.
Data on stall speeds under various conditions.
Performance data for take off distances.
Information on expected flight endurance and range.
Guidance on calculating aircraft weight and balance.
Example calculation for determining the Center of Gravity.
Graphical representation of the aircraft's CG envelope.
Overview of the aircraft's systems and components.
Description of the aircraft's fuselage, wings, and empennage.
Details on the aircraft's flight control mechanisms.
Description of the electric propulsion system components.
Overview of the aircraft's high and low voltage electrical systems.
Description of installed flight instruments and avionics.
Guidance on proper aircraft handling and servicing.
Instructions and safety guidelines for battery recharging.
Procedures for servicing tires, brakes, and propeller.
Procedures for moving and parking the aircraft on the ground.
Guidelines for cleaning the aircraft's exterior and interior.
Detailed description of the EPSI570C avionics system.
