British Aerospace 125

Airplanes

Length

15.24 m

Flat Wing Span

14.3256 m

Height

5.1816 m

Flat Wing Area

32.7948 m²

Flat Wing Aspect Ratio

6.25

Max Seating

Cruise Speed

840.8073 km/h

Max Mach

0.78 Mach

Max Ceiling

12496.8 m

Number of Engines

Aircraft Engine

First Flight

1962-08-13

Number Built

1720

Maximum Take-Off Weight

11.3398 t (paragliders: kg)

Total Fuel Capacity

5368.932

Maximum Range

3055.8 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
British Aerospace 125	11.3398	5368.932	3055.8

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Mikoyan-Gurevich I-320	Klimov VK-1	15.775	14.2		Compare
IAI Westwind		15.93	13.65	7	Compare
McDonnell F2H Banshee		14.6304	12.4968		Compare
Lockheed L-133	Lockheed J37	14.73	14.22		Compare
Hawker 800 (Raytheon)		15.5448	15.5448		Compare
Grumman F7F Tigercat		13.716	15.5448		Compare

All data (28 fields)

Name: British Aerospace 125
Manufacturer: British Aerospace
Description: The British Aerospace 125 is a twinjet mid-size business jet.
First Flight: 1962-08-13
Production End: 2013-01-01
Designer: British Aerospace
Type: Mid-size business jet
Length (m): 15.24
Height (m): 5.1816
Cockpit Crew: 2
Max Seating: 8
Cruise Speed (km/h): 840.8073
Min Speed (km/h): 153.7159
Max Ceiling (m): 12496.8
Rate of Climb (m/s): 24.892
Capacity Description: 8 passengers (normal layout), 14 passengers in high density layout
Max Mach (Mach): 0.78
National Origin: United Kingdom
Number Built: 1720
Powerplant Description: 2 × Rolls-Royce Viper 601-22 turbojet engines
Primary Users: Japan Air Self-Defense Force, Brazilian Air Force
Status: Active service
Wikipedia Article (URL): en.wikipedia.org/wiki/British_Aerospace_125
Flat Wing Span (m): 14.3256
Flat Wing Area (m²): 32.7948
Flat Wing Aspect Ratio: 6.25
Aircraft Engine: Armstrong Siddeley Viper
Number of Engines: 2