2006 SkyStar Pulsar III

The Pulsar was a development of the StarLite Aircraft StarLite and features a cantilever low-wing, a two-seats-in-side-by-side configuration open cockpit under a bubble canopy, fixed tricycle landing gear or optionally conventional landing gear with wheel pants and a single engine in tractor configuration.

The aircraft is made from composites. Its 25.00 ft (7.6 m) span wing employs a NASA MS(1)-0313 airfoil, mounts flaps and has a wing area of 80.00 sq ft (7.432 m2). The cabin width is 39 in (99 cm). The acceptable power range is 64 to 115 hp (48 to 86 kW) and this particular aircraft is equipped with a 100 HP Rotax 912ULS.


Crew one
Capacity one passenger
Length 6.10 m
Wingspan 7.62 m
Wing area 7.4 m2
Empty weight 299 kg
Maximum Take Off Mass 544 kg
Fuel capacity 72 kg/96 L
Powerplant Rotax 912ULS
Propeller Woodcomp SR 2000xa
Design Load Factors +4/-2 G
Cruise speed 115 kts
Stall speed 43 kts
Range 450 NM
Ceiling 13.000 ft
Rate of Climb 900 ft/min
Wing Loading 73 kg/m2



  • Exterior_2
  • Exterior_1
  • Panel_1
  • Exterior_3


Type: SkyStar Aircraft Corp. Pulsar III
Aircraft Registration: PH-UGO
Manufacturer Serial Number: P98010548
Maximum Take-Off Mass: 544 kg
Year of Manufacturing: 2006
Total Time on Airframe: 39
Engines: Bombardier-Rotax GmbH 912 ULS
Engine Power: 100 HP
Total Time on Engines: 39
Propellers: Woodcomp SR 2000xa (Adjustable Pitch, 3-bladed)
Total Time on Propellers: 39

GTX-328 Mode-S Transponder (Mode-S)
Dittel KRT-2 VHF COM (8.33 Khz)


Fabric seats and carpet floor and side panels


Ferrari red with yellow registration markings

Price: EUR. 35.000 (VAT free)
  • Exterior_2
  • Exterior_1
  • Panel_1
  • Exterior_3