avia.wikisort.org - Aeroplane

The Pegasus PE-210A is a prototype of a single-engine Trainer with canard developed by Oaxaca Aerospace and TechBA.

PE-210A
Role	Trainer/aerobatic Type of aircraft
National origin	Mexico
Manufacturer	Oaxaca Aerospace
Status	In development
Number built	1

Design and development

Oaxaca Aerospace began the project in 2011 with the objective of designing an agile, fast and inexpensive two-seat airplane and concluded in mid-2013, the year in which the ground tests began. The aircraft has a rear mounted Lycoming AEIO-390 engine, canards and a tandem design cockpit with dual flight controls. The rear seat is at a higher level with respect to the front seat, which allows a view of 300° vertical and 240° horizontal. The aircraft was first presented to the public at Feria Aeroespacial México (FAMEX) 2015.[1]

Specifications

Data from FAMEX 2015[2]

General characteristics

• Crew: 2
• Length: 7.4 m
• Wingspan: 8.9 m
• Wing area: 12.5 m^2
• Canard area: 1.48 m^2
• Max. takeoff weight: 1250 kg
• Payload: 350 kg
• Powerplant: 1x Lycoming AEIO-390 210 HP
• Fuel capacity: 210 L

Performance

• Maximum speed: 221 kn / 410 km/h
• Cruise speed: 162 kn / 300 km/h
• Stall speed: 64 kn / 118 km/h
• Service ceiling: 18000 ft / 5400 m
• Range: 864 nmi / 1600 km

References

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