747-200B

The 747-200B is an improved version of the 747-200, with increased fuel capacity and more powerful engines; it first entered service in February 1971. The -200B aircraft has a full load range of about 6,857 nmi (12,700 km). The 747-200F is the freighter version of the -200 model. It could be fitted with or without a side cargo door. It has a capacity of 105 tons (95.3 tonnes) and an MTOW of up to 833,000 lb (378,000 kg). It entered first service in 1972 with Lufthansa.



  Boeing 747-200B
Cockpit crew: two pilots and a flight engineer.
Passengers single class: - 539.
Passengers two class main deck:

-   32 first class.

- 388 economy class.

Passengers three class main deck:

-  22 first class.

-  84 business class.

- 131 economy class.

Upper deck seating options:

- 15 place lounge.

- 8 first class plus 11 place lounge.

- 16 first class sleeper seats.

- 32 - 45 economy class.

Cabin length: 57,00 m.
Cabin diameter: 6,13 m.
Cabin height: 2,54 m.
Cabin volume: 516 m³.
Baggage compartment: 28,3 m³.
Cargo volume:

- main deck 516 m³.

- under floor 149,96 m³.

- bulk under floor 28,3 m³.

- total load 694 m³.

LD3 Containers in belly: 30.
Standard 2.24m x 3.18m pallets:

- main cargo deck of freighter 28.

Standard 2.24m x 2.99m pallets:

- main cargo deck of freighter 30.

Wing span: 59,64 m.
Wing area: 510,97 m².
Wing sweep: 37.5 degrees.
Fuselage length: 70,66 m.
Fuselage diameter: 6,49 m.
Height: 19,33 m.
Horizontal tail unit: 22,17 m.
Wheelbase: 25,62 m.
Track: 10,36 m.
Engines:

- four Pratt & Whitney JT9D-7AW each rated 205.3 kN.

- four Pratt & Whitney JT9D-7J each rated 222.4 kN.

- four Pratt & Whitney JT9D-7R4G2 each rated 243.5 kN.

- four General Electric CF6-50E2 each rated 230.4 kN.

- four Rolls Royce RB211-524D4 each rated 231.3 kN.

Weight:

- empty: 170.600 Kg.

- max. zero-fuel weight: 238.780 Kg.

- fuel: 198.370 liters.

- max. payload: 68.180 Kg.

Max. take off weight: 377.800 Kg.
Max. landing weight: 285.700 Kg.
Cruise speed: 939 km/h.
Max. speed: 969 km/h.
Landing speed: 259 km/h.
Max. ceiling: 13.716 m.
Range:

13.149 km.

Performance:

- take-off run  3.170 m at max. take-off weight.

- landing run  2.121 m at max. landing weight.