Manta Bi
Wing area: 41 sq.m
Certification: Afnor
Pilot weight: 130-190 kg
Wing span: 14.5 m
Aspect ratio: 4.8
Min sink: 1.1 m/s
Max speed: 47 kph
Price (1998) £1,999
1980->
ADG Line Havane
Havane 24
Wing area: 23.7 sq.m
Certification: Afnor
Pilot weight: 55-70 kg
No. of cells: 41
Wing span: 10.8 m
Aspect ratio: 42
Min sink: 1.2 m/s
Max speed: 41 kph
Price (1998) £1,699
Havane 27
Wing area: 26.9 sq.m
Certification: Afnor
Pilot weight: 70-85 kg
No. of cells: 41
Wing span: 11.1 m
Aspect ratio: 4.6
Min sink: 1.2 m/s
Max speed: 41 kph
Price (1998) £1,699
Havane 30
Wing area: 29.6 sq.m
Certification: Afnor
Pilot weight: 85-105 kg
No. of cells: 41
Wing span: 11.7 m
Aspect ratio: 4.7
Min sink: 1.2 m/s
Max speed: 41 kph
Price (1998) £1,699
ADG Line Frégate
Paraglider circa 1998.
Fregate 28
Wing area: 8.1 sq.m
Certification: Afnor
Pilot weight: 75-90 kg
No. of cells: 51
Wing span: 11.9 m
Aspect ratio: 5.1
Min sink: 1 m/s
Max speed: 43 kph
Price (1998) £1,899
Fregate 31
Wing area: 31.2 sq.m
Certification: Afnor
Pilot weight: 90-110 kg
No. of cells: 51
Wing span: 12.7 m
Aspect ratio: 5.1
Min sink: 1 m/s
Max speed: 43 kph
Price (1998) £1,899
ADG Line Bahia
Paraglider circa 1998.
The Bahia model was designed by Xavier Demoury
Bahia 28
Wing area: 28 sq.m
Certification: Afnor
Pilot weight: 80-95 kg
No. of cells: 62
Wing span: 12.6 m
Aspect ratio: 5.7
Min sink: 0.9 m/s
Max speed: 45 kph
Price (1998) £1,999
Bahia 31
Wing area: 31.2 sq.m
Certification: Afnor
Pilot weight: 95-115 kg
No. of cells: 62
Wing span: 13.3 m
Aspect ratio: 5.7
Min sink: 0.9 m/s
Max speed: 45 kph
Price (1998) £1,999
ADG Line
1998: Z.A de Pernoix, F- 74920 Talloires, France
Paraglider manufacturer.
Adams Luft Baffo 12
The Baffo 12 is constructed of welded stainless steel tube and in 1998 started using an oil cooled BMW 1100 engine.
Empty weight: 182 kg
Wing span: 10 m
Wing area: 15.5 sq.m
Engine: BMW 1100RS , 90 hp
MAUW: 450 kg
Seats: 2
Max speed: 140 kph
Cruise speed: 110 kph
Minimum speed: 56 kph
Fuel consumption: 8 lt/hr
Adams Luft Baffo 11
An aircraft style spaceframe fuselage forms the basis of the Baffo 11, in which a low-mounted inline four cylinder BMW K 100 drives a prop through a long toothed belt.
Empty weight: 188 kg
Wing span: 10 m
Wing area: 15.5 sq.m
Engine: BMW R 100 RS, 90 hp
MAUW: 450 kg
Seats: 2
Max speed: 140 kph
Cruise speed: 110 kph
Minimum speed: 55 kph
Fuel consumption: 8 lt/hr
Adams Luft
1998:
Heide 19
D-41379 Brüggen
Germany
Adams Industries Inc
In 1981 Adams Industries Incorporated produced the T211 two-seat lightplane, designed by John Thorpe from the original T-11 Sky Scooter of 1946.
Adams Aeronautics T-100D
The T-100D was available as a plans only design.
T-100D
Stall: 23 kt / 26 mph / 42 kph
Cruise: 55 kt / 63 mph / 101 kph
Vne: 70 kt / 80 mph / 129 kph
Empty Weight: 115 kg / 254 lbs
MTOW: 229 kg / 504 lbs
Climb Ratio: 600 ft/min / 3 m/s
TO distance (50ft): 350 ft / 107 m
Ldg dist (50ft): 300 ft / 91 m
