Home
Fleet
Fleet
Il-76TD
Il-76TD aircraft is the evolution of the transport modification of the Il-76T aircraft.
The transportation efficiency of the aircraft has been improved, in comparison with Il-76T, by way of increasing maximum takeoff weight from 170 to 190 tons, maximum commercial load from 43.4 to 50 tons, and practical flying range with increased maximum load. Due to increased maximum takeoff weight and commercial load, and in order to improve operating life figures, the structures in the wing, fuselage and landing gear have been reinforced.Main Technical Characteristics
| Length: | 46, 6 m |
| Height: | 14,76 m |
| Wingspan: | 50,5 m |
| Number x engine type: | 4 x turbojet engine |
| Engine: | D-30KP series 2 |
| Cruising speed: | 750–780 km/h |
| Flight altitude: | 9 100–12 100 m |
| Flight range with payload of 40 tons: |
4 900 km |
| Takeoff distance: | 1700 m |
| Landing distance: | 930 m |
| Maximum takeoff weight: | 190 tons |
| Maximum payload: | 50 tons |
A300B4-200F
The Airbus A300 (A300F or A300B4) is a medium size cargo aircraft – up to 44 tons payload which large side cargo door and two belly section doors, standard version consists of 20 main deck pallet positions plus additional space for lower deck containers, aircraft is equipped with roller bed floor systems to position pallets and containers inside of the cargo cabin. Loading and discharge of the containers or pallets requires a high loader, aircraft is suitable for cargo of all kinds including live stock and perishables.
The transportation efficiency of the aircraft has been improved, in comparison with Il-76T, by way of increasing maximum takeoff weight from 170 to 190 tons, maximum commercial load from 43.4 to 50 tons, and practical flying range with increased maximum load. Due to increased maximum takeoff weight and commercial load, and in order to improve operating life figures, the structures in the wing, fuselage and landing gear have been reinforced.Main Technical Characteristics
| Wingspan: | 44, 84 m |
| Length: | 54,08 m |
| Height: | 16,53 m |
| Cruising speed: | 847 km/h |
| Max altitude: | 10,670 m |
| Max take-off weight: | 165.000 kg |
| Max gross payload: | 43.500 kg |
| Fuselage diameter: | 5,64 m |
| Cabin clear height: | 2,49 m |
| Gross volume: | 416,4m³ |
| Range (Max payload): | 7.050 kg |
Boeing 767F
The Boeing 767F was designed for cargo operations. The -300F and -300ER variants have the same payload weight and is higher than the -300. The F, like the other variants, has options for winglets which improve fuel efficiency. The aircraft can also be converted from a passenger aircraft by Boeing and other companies around the world. The BCF as it's known, Boeing Converted Freighter, is exactly like the F after the completion of the renovation and includes the cargo door that would not have been there originally.
Main Technical Characteristics
| Registration: | SP-MRF |
| Aircraft: | Boeing 767-200SF |
| MTOW: | 159 755 kg |
| Payload: | 44 452kg |
| Maximal range: | 9 600 km |
| Cruising speed: | 850 km/h |
| Volume: | 450 m³ |