Para Delta Bingo

Bingo 27
Paraglider circa 1997/8.
Wing area: 25.5 sq.m
Certification: Afnor
Pilot weight: 60-95 kg
No. of cells: 23
Wing span: 9.1 m
Aspect ratio: 3.25
Price (1998) 2800000 Lr

Bingo 29
Paraglider circa 1997/8.
Wing area: 27.6 sq.m
Pilot weight: 80-115 kg
No. of cells: 25
Wing span: 9.5 m
Aspect ratio: 3.27
Price (1998) 2900000 Lr

Para Delta Big Bang

Big Bang G
Paraglider circa 1997/8.
Wing area: 31.56 sq.m
Pilot weight: 90-120 kg
No. of cells: 50
Wing span: 10.8 m
Aspect ratio: 3.51
Price (1998) 5610000 Lr

Big Bang M
Paraglider circa 1997/8.
Wing area: 29.26 sq.m
Certification: Afnor
Pilot weight: 85-105 kg
No. of cells: 48
Wing span: 10.45 m
Aspect ratio: 3.73
Price (1998) 5500000 Lr

Para Delta Ben Hur T5

Ben Hur G
Paraglider circa 1997/8.
Wing area: 31.54 sq.m
Pilot weight: 95-125 kg
No. of cells: 63
Wing span: 12.1 m
Aspect ratio: 4.64
Price (1998) 6646000 Lr

Ben Hur M
Paraglider circa 1997/8.
Wing area: 29.2 sq.m
Certification: Afnor
Pilot weight: 85-110 kg
No. of cells: 59
Wing span: 11.2 m
Aspect ratio: 4.37
Price (1998) 6516000 Lr

Ben Hur T 5 deg dg
Paraglider circa 1997/8.
Wing area: 28.1 sq.m
Pilot weight: 85-110 kg
No. of cells: 98
Wing span: 12.71 m
Aspect ratio: 5.75
Price (1998) 8735000 Lr

Ben Hur 5 deg m
Paraglider circa 1997/8.
Wing area: 26.3 sq.m
Certification: Afnor
Pilot weight: 80-105 kg
No. of cells: 90
Wing span: 11.65 m
Aspect ratio: 5.16
Price (1998) 8600000 Lr

Para-Cycle Segovia

First manufactured in the USA in 1997. The unit is a street legal pedalling trike. A parachute and motor are attached by three bolts.

Engine: 2si 460F, 40 hp
hp range: 22-50
Height: 6 ft
Length: 6.8 ft
Wing span: 39 ft
Wing area: 400 sq.ft
Empty weight: 147 lb
Gross weight: 467 lb
Fuel capacity: 2.5 USG
Cruise: 26 mph
Range: 40 sm
Rate of climb: 400 fpm
Takeoff dist: 100 ft
Landing dist: 25 ft
Service ceiling: 10,000 ft
Seats: 1

Paraborne Buckshot / Goodwin Buckshot

The Goodwin Buckshot is an American powered parachute that was designed and produced by FL Goodwin of Phoenix, Arizona and introduced in 1998.

Designed as a US FAR 103 Ultralight Vehicles two seat trainer, it features a parachute-style high-wing, two seats in side-by-side configuration, tricycle landing gear and a single engine in pusher configuration. The standard engines supplied were the 45 hp (34 kW) 2si 460F-45 and the 45 hp (34 kW) Zenoah G-50 engine, although any light, two-cylinder, two-stroke engine can be used.

The aircraft is built from bolted anodized aluminium tubing to save weight. In flight steering is accomplished via foot pedals that actuate the canopy brakes, creating roll and yaw. On the ground the aircraft has tiller-controlled nosewheel steering. The main landing gear does not incorporate suspension and the aircraft relies on large tundra tires to provide this.
The aircraft was distributed by Paraborne Aviation of Kissimmee, Florida. The Buckshot is out of production.
The rectangular canopy is made from double ripstop, mylar and kevlar. The trike design utilises shroud lines and risers.

Engine: Rotax 503, 46 hp
hp range: 40-65
Height: 7 ft
Length: 9 ft
Wing span: 50 ft
Wing area: 502 sq.ft
Empty weight: 230 lb
Gross weight: 730 lb
Fuel capacity: 13.5 USG
Cruise: 26 mph
Rate of climb: 700 fpm
Takeoff dist: 50 ft
Landing dist: 30 ft
Service ceiling: 10,000 ft
Seats: 2

Buckshot
Engine: 1 × 2si 460F-45, 45 hp (34 kW)
Empty weight: 230 lb / 104 kg
Fuel capacity: 13.5 U.S. gallons / 51 lt / 11.2 imp gal
Cruise speed: 25 mph / 22 kph / 40 km/h
Crew: one
Capacity: one passenger
Unit cost: US$9000 (2001)