UL Electric Glider Silent AE-1
2001 · Unknown · UL-Elektrosegler Silent AE-1 · Unknown
- Year
- 2001
- Registration No
- -
- Manufacturer
- Unknown
- Total Time (TTAF)
- -
- Model
- UL-Elektrosegler Silent AE-1
- Seats
- -
- Engine Type + Power
- -
- Location
- Germany
- Home Base
- -
- Serial Number
- -
UL-Elektrosegler Silent AE-1 - Image 1
External aircraft listing discovered on ulpro.de.
Trade:Aero republishes this aircraft listing with 14 translations and reference data to improve discoverability. The original seller has not yet claimed the aircraft listing.
UL Electric Glider Silent AE-1
No email contact for this listing
This listing was imported from another marketplace that didn't publish a seller email. Please use the original listing to reach the seller directly.
View original aircraft listingDescription
The future-proof, self-launching UL club class glider Silent AE1, built in 2001, with only approx. 200 flight hours, featuring a Geiger HPD 20 kW motor (50 hrs) and 9.3 kWh battery, JNP 10/2026. This legendary electric glider was celebrated in 1999 as the world's first production electric aircraft, and was electrified by Stefan Gehrmann from the Italian Alisport Silent airframe in a limited number of units – at that time still with NiCd cells. From 2019 to 2023, it was equipped with current drive components, including the Geiger HPD 20 kW motor and 3 x 3.1 kWh Geiger lithium-ion batteries, and kept technically up to date. The Silent AE1 holds a supplemental type certificate as an UL. With a wingspan of 12 m, this fine glider achieves a glide ratio of 31 (at 95 km/h) and is perfect for independent thermal soaring in the club class, without relying on launch infrastructure such as winch or aerotow – however, it is also suitable for aerotow with a nose coupling. Particularly future-oriented: when using solar power, it flies CO2-free. Low energy consumption: approx. 1.5 kWh for one launch to 400 m. A detailed report on AirEnergy describes it with the old electrics (NiCd cells!). Technical data: Wingspan: 12.02 m, Empty weight: 201 kg, MTOW: 300 kg, vstall: 67 km/h, vne: 180 km/h, va: 130 km/h, Glide ratio: 31 at 95 km/h, Minimum sink: 0.84 m/s at 80 km/h, Take-off run: 150 m, Maximum altitude under power: 3000 m, ADS-B IN / OUT, FLARM IN/OUT, canopy flasher, XCSoar navigation on Kobo surface, 6" flaps, camber flaps down to -7°, winglets, drum wheel brake coupled with spoilers, wing tip wheels, on-board toilet, removable canopy, new emergency parachute + harness system, trailer (Pfeiffer) with TÜV 11/27. Sale due to class change. Further information on request.





