Commercial Aircraft Directory - Aircraft Specification

Shorts - Belfast

Originally conceived as a strategic freighter for the Royal Air Force, the Belfast was designed to utilise the same wing as the Bristol Britannia, which Shorts had experience of building; allied to a new fuselage following the configuration of the Lockheed C-130. Only ten Belfast’s were built the first being delivered to 53 Sqdn of the RAF on 20/06/1966. Following a defence review the Belfast was retired from RAF service in 1976. Five aircraft were acquired by TAC Heavylift and modified to meet civil certification requirements. This work was carried out by Marshal Aerospace and involved changes to the engines, flight control systems, avionics and autopilot. Three aircraft were modified the first entering service with Heavylift following certification in 1980, and they operated successfully for a number of years with this operator. In 2005 only one Belfast is in service with an operator in Australia.

View specification units in: METRIC | IMPERIAL

SPECIFICATION

First Flight date: Feb 1959  
Certification date: 6 May 1980  

PRINCIPAL DIMENSIONS

Fuselage width: 4.9 m 
Fuselage height:  
Fuselage length: 41.58 m 
Cabin length: 25.7 m 
Cabin width: 4.9 m 
Cabin height: 4.06 m 
Cabin volume: 321 m3 
Hold volume:  

WEIGHTS

Empty operating: 58,976 kg 
Max zero fuel: 92,986 kg 
MTOW: 104,325 kg 
MLW: 97,520 kg 
Standard fuel capacity: 48,822 kg 
Max fuel capacity: 48,822 kg 

SPEEDS

Normal cruise: 510 km/h 
Max cruise: 566 km/h 

PERFORMANCE

Long Range Cruise alt: 9,144 m 
Max ceiling: 9,144 m 
Take off field length: 2,500 m 
Landing field length: 2,075 m 
Max Payload Range: 1,575 m 
Range notes:  
Max passengers: 19  
Typical passengers: 0  

POWERPLANT

Category: Turboprop  
Manufacturer: Rolls-Royce  
Model/Submodel: TyneMk.515/101W (RTy 12)  
Thrust: 0 kN