Blackburn Beverley

Airplanes

Length

30.1752 m

Flat Wing Span

49.3776 m

Height

11.5824 m

Flat Wing Area

270.9053 m²

Flat Wing Aspect Ratio

Max Seating

Cruise Speed

278.4165 km/h

Max Speed

383.0239 km/h

Max Ceiling

4876.8 m

Number of Engines

Aircraft Engine

First Flight

1950-06-20

Entry Into service

1955-01-01

Number Built

Maximum Take-Off Weight

61.235 t (paragliders: kg)

Total Fuel Capacity

31277.1

Maximum Range

2092.147 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Blackburn Beverley	61.235	31277.1	2092.147

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Boeing XB-39 Superfortress	Allison V-3420	30.18	43.05		Compare
Boeing B-29 Superfortress		30.1752	42.9768		Compare
Tupolev Tu-4	Shvetsov ASh-73	30.18	43.05		Compare
Martin 156	Wright R-1820 Cyclone	28.11	47.87	53	Compare
Consolidated XPB3Y		31.9	51.5		Compare
Short Shetland		33.528	45.72		Compare

All data (27 fields)

Name: Blackburn Beverley
Manufacturer: Blackburn Aircraft
Description: The Blackburn B-101 Beverley is a heavy transport aircraft produced by the British aircraft manufacturer Blackburn Aircraft.
First Flight: 1950-06-20
Entry Into service: 1955-01-01
Production End: 1958-01-01
Service End: 1967-01-01
Designer: Blackburn Aircraft
Type: Military transport aircraft
Length (m): 30.1752
Height (m): 11.5824
Cockpit Crew: 4
Max Seating: 94
Max Speed (km/h): 383.0239
Cruise Speed (km/h): 278.4165
Max Ceiling (m): 4876.8
Rate of Climb (m/s): 3.8608
Capacity Description: ; 94 troops or; 70 paratroopers
Number Built: 49
Powerplant Description: 4 × Bristol Centaurus 173 18-cylinder air-cooled Sleeve valve, radial engines, 2125 kW (2850 hp) each
Primary Users: Royal Air Force
Wikipedia Article (URL): en.wikipedia.org/wiki/Blackburn_Beverley
Flat Wing Span (m): 49.3776
Flat Wing Area (m²): 270.9053
Flat Wing Aspect Ratio: 9
Aircraft Engine: Bristol Centaurus
Number of Engines: 4