2013 Puma Sport - BDC Aero Industries

2013 Puma Sport – BDC Aero Industries

November 11, 2025 4:48 pm
Quebec

New

$110,000

Overview

Model: Puma Sport
Year of Manufacture: 2013
Total Time Since Overhaul: 250
Airframe Total Time: 207.9
Engine Manufacturer: Rotax
GPS: other
Engine Type: 4-Stroke
Engine Model: 912 iS
Interior Condition: Excellent
Manufacturer: BDC Aero Industries
Avionics Suite: Dynon Skyview Classic including GPS, 6 packs, transponder, VHF radio linked to NAV database, tachometer, oil pressure and temperature, coolant temperature, EGT, fuel pressure, battery voltage, ammeter, trim position, flaps position, throttle position Analog compass, altimeter and airspeed indicator, timers (hobbs, tach, air time etc.) ZAON anticollision systems (PCAS)
Exterior Color:
Airframe Condition: Excellent

Description

Just bought, I’m regretfully selling because of a financial issue.
See aircraft manufacturing process: https://www.youtube.com/watch?v=NsCYTd7uMZI

Airplane
Registration: C-GWYI
S/N: AB-59-20-615
TTSN (air time): 207.9 hours
Special Certificate of airworthiness – Limited: always maintaned by an AME + it allows a MTOW of 1320 lb
Possibility to revert it to advanced ultralight
Journey Log, Technical Logs available

Maintenance
Maintained by the same AME from day one according to a maintenance schedule
Hangared
Annual inspection done in October 2025
All rubber parts changed in October 2025 (oil hoses, lubricant hoses, rubbers of the engine mount) as per Rotax scheduled maintenance
Propeller bolts changed in October 2025

Engine
Rotax 912 iS SPORT
Year 2013 – S/N: 4417273
100 HP @ 5800 RPM
Hobbs time: 250 hours

Airframe
Fuselage is epoxy resin fiber glass
Wings, ailerons, horizontal stabilizer, and elevator are aluminum (6061 T6 and 7129 T5).
Turbulators along the whole wing, excellent stall characteristics
Free castering nose wheel, great ground maneuverability
Flaps continuous control 0-45 degrees
Cockpits lights (red)
Engine cowls controlled form the cockpit

Fuel and Tanks
AVGAS or MOGAS
Two tanks in the wings with fuel valve featuring Right, Left and Both positions
Total fuel 23.64 US Gallons
Usable fuel 20 US Gallons
Endurance 5.3 hours

Weights
Useful load: 512 lbs (with Special CoA – Limited) MTOW: 1320 lbs (with Special CoA – Limited; 1220 lbs if reverted to Advanced Ultralight Airplane)
Basic empty weight: 808.0 lbs (including oil 0.79 gallons, coolant liquid 0.79 gallons, 3.83 gallons fuel, installed items)
Luggage compartment max capacity: 50 lbs

Performance
Vso 35 KIAS
Vs 43 KIAS
Vno 120 KIAS
Vne 138 KIAS

Takeoff ground roll distance 330 ft (asphalt, MTOW, 5 kts headwind)
Takeoff distance (50 feet obstacle) 720 ft (asphalt, MTOW, 5 kts headwind)
Climb rate 900 fpm
Max cruise speed 120 KIAS (5500 RPM)
Fuel consumption at normal cruise <3.7 GPH
Landing distance (50 feet obstacle) 720 ft (asphalt, MTOW, full flaps)
Landing ground roll distance 395 ft (asphalt, MTOW, full flaps)