Hawker Siddeley Andover

· Hawker Siddeley

Airplanes

Length

23.7744 m

Flat Wing Span

29.8704 m

Height

9.144 m

Flat Wing Area

77.2396 m²

Max Seating

Cruise Speed

435.2196 km/h

Max Speed

514.8556 km/h

Max Ceiling

7315.2 m

Number of Engines

First Flight

1963-12-21

Number Built

Maximum Take-Off Weight

23.1332 t (paragliders: kg)

Total Fuel Capacity

6546.37

Maximum Range

2294.628 km

Pictures

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Hawker Siddeley Andover	23.1332	6546.37	2294.628

Name	Length (m)	Flat Wing Span (m)	Max Seating
Antonov An-30	24.26	29.2		Compare
An-26	23.8	29.3	40	Compare
De Havilland Canada DHC-5 Buffalo	24.0792	29.2608	41	Compare
Xi'an Y-7	24.218	29.666	52	Compare
Xi'an MA60	24.71	29.2	62	Compare
Xi'an MA600	24.71	29.2	60	Compare

All data (27 fields)

Name: Hawker Siddeley Andover
Manufacturer: Hawker Siddeley
Description: The Hawker Siddeley HS 780 Andover is a twin-engined turboprop military transport aircraft produced by Hawker Siddeley for the Royal Air Force (RAF), developed from the Avro-designed HS 748 airliner.
ICAO Code: A748
First Flight: 1963-12-21
Service End: 1998-01-01
Designer: Hawker Siddeley
Type: Transport aircraft
Length (m): 23.7744
Height (m): 9.144
Cockpit Crew: 2
Max Seating: 52
Max Speed (km/h): 514.8556
Cruise Speed (km/h): 435.2196
Min Speed (km/h): 144.4559
Max Ceiling (m): 7315.2
Rate of Climb (m/s): 6.096
Capacity Description: 52 troops, 40 paratroops or 24 stretcher cases / 14365 lb payload
Number Built: 37
Powerplant Description: 2 × Rolls-Royce RDa.12 Dart Mk 201 turboprop engines, 2420 kW (3245 hp) each
Primary Users: Royal Air Force, Royal New Zealand Air Force, 748 Air Services
Status: Retired
Wikipedia Article (URL): en.wikipedia.org/wiki/Hawker_Siddeley_Andover
Flat Wing Span (m): 29.8704
Flat Wing Area (m²): 77.2396
Wake Category: M
Number of Engines: 2