The Boeing 737-200 is a mid sized passenger jet that operates as a win-engined short-range narrowbody airliner. It was developed from the 737-100 series with a stretched fuselage. In the year 1968 the B732 was priced at $4 million, but in 1972 its price surpassed that to $5.2 million. Manufactured in the year 1965 by the United Stated based Boeing company, the Boeing 737 200 series was discontinued in the year 1988.
Model No :
Boeing 737 200
Country :
United States
Manufactured :
1965 to: 1988
ICAO :
B732
B732
Avionics :
ARINC 500 series
Engine :
2x Pratt Whitney JT8D-17turbofan
Power :
16,000 pound-force
Max Cruise Speed :
504 knots - 933 Km/h
Approach Speed :
150 knots
Travel Range :
2,600 Nautical Miles - 4,815 Kilometers
Fuel Economy :
Fuel Economy:
Service Ceiling :
37,000 feet
Rate of Climb :
1500 feet/minute - 7.62metre/second
Take Off Distance :
1830 metre - 6,003.86 feet
Landing Distance :
1400 metre - 4,593.12 feet
Max Tak eOff Weight :
52,390 Kg - 115,499 lbs
Max Payload :
12,791 Kg - 28,199 lbs
Fuel Tank Capacity :
4,720 gallon - 17,867 litre
Baggage Volume :
24.8 m3 / 876 ft3
Seats Economy/General Class :
136 seats
Seats Business Class :
NA
Seats First Class :
NA
Cabin Height :
2.11 metre - 6.92 feet
Cabin Width :
3.54 metre - 11.61 feet
Cabin Length :
29.54 metre - 96.91 feet
Exterior Length :
30.53 metre - 100.16 feet
Tail Height :
11.35 metre - 37.24 feet
Fuselage Diameter :
3.8 metre - 12.47 feet
Wing Span Rotor Diameter :
28.35 metre - 93.01 feet
Specifications
Also recognized as the F35 Lightning II Aerial Refueling, the plane was a part of the ARINC 500 series. It’s engine was of the 2x
Pratt & Whitney JT8D-17 variation and equipped with a turbofan. Because of the powerful force behind this engine, the aircraft possessed a power of 16,000 pound-force, along with a maximum cruise speed of 504 knots or 933 kilometers per hour. The approach speed amounted to nearly 150 knots, but the travel range for this was about 2,600 nautical miles, which when converted amounted to 4,815 kilometers. Part of the reason why it may have been discontinued was because it had low fuel efficiency and a service ceiling of 37,000 feet, as well as a rate of climb for 1500 feet per minute, which in metric terms looks like 7.62metre / second. What made this aircraft impressive was the landing and take off distance, as the former amounted to 1400 metres to 4,593.12 feet and the latter to 1830 metres to 6,003.86 feet.
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