Length: 93 ft 10 in (28.60 m)
Wingspan: 86 ft 0 in (26.21 m)
Height: 28 ft 2 in (8.59 m)
Wing area: 832.0 ft² (77.30 m²)
Empty weight: 52,684 lb (23,897 kg)]
Max takeoff weight: 93,000 lb (42,184 kg)
Powerplant: 4× Textron Lycoming ALF 502R-5 turbofans, 6,970 lbf (31.0 kN) each

Cruise speed: 498 mph (432 knots, 801 km/h) at 29,000 ft (8,840 m) (high speed cruise)
Range: 1,808 mi (1,570 nmi, 2,909 km) (Standard fuel)

 Length: 93 ft 10 in (28.60 m)
Wingspan: 86 ft 0 in (26.21 m)
Height: 28 ft 2 in (8.59 m)
Wing area: 832.0 ft² (77.30 m²)
Empty weight: 52,684 lb (23,897 kg)]
Max takeoff weight: 93,000 lb (42,184 kg)
Powerplant: 4× Textron Lycoming ALF 502R-5 turbofans, 6,970 lbf (31.0 kN) each

Cruise speed: 498 mph (432 knots, 801 km/h) at 29,000 ft (8,840 m) (high speed cruise)
Range: 1,808 mi (1,570 nmi, 2,909 km) (Standard fuel)

 Length: 93 ft 10 in (28.60 m)
Wingspan: 86 ft 0 in (26.21 m)
Height: 28 ft 2 in (8.59 m)
Wing area: 832.0 ft² (77.30 m²)
Empty weight: 52,684 lb (23,897 kg)]
Max takeoff weight: 93,000 lb (42,184 kg)
Powerplant: 4× Textron Lycoming ALF 502R-5 turbofans, 6,970 lbf (31.0 kN) each

Cruise speed: 498 mph (432 knots, 801 km/h) at 29,000 ft (8,840 m) (high speed cruise)
Range: 1,808 mi (1,570 nmi, 2,909 km) (Standard fuel)

 Length: 93 ft 10 in (28.60 m)
Wingspan: 86 ft 0 in (26.21 m)
Height: 28 ft 2 in (8.59 m)
Wing area: 832.0 ft² (77.30 m²)
Empty weight: 52,684 lb (23,897 kg)]
Max takeoff weight: 93,000 lb (42,184 kg)
Powerplant: 4× Textron Lycoming ALF 502R-5 turbofans, 6,970 lbf (31.0 kN) each

Cruise speed: 498 mph (432 knots, 801 km/h) at 29,000 ft (8,840 m) (high speed cruise)
Range: 1,808 mi (1,570 nmi, 2,909 km) (Standard fuel)

This medium size city to city commuter jet first went operational in 1976 and had the longer fuselage of the Mk 2000 with a passenger capacity of 85. Wingspan was increased by 1.57 m and more powerful Rolls-Royce RB183 "Spey" Mk555-15P of 44 kN (9,901 lbf) thrust.

 General characteristics

• Length: 51 ft 2 in (15.6 m)
• Wingspan: 54 ft 4 in (16.6 m)
• Height: 18 ft 1 in (5.5 m)
• Wing area: ft² (m²)
• Empty weight: 15,670 lb (7,110 kg)
• Useful load: 11,790 lb (5,350 kg)
• Max takeoff weight: 28,000 lb (12,700 kg)
• Powerplant: 2× Honeywell TFE731-5BR turbofans, 4,660 lbf (20.8 kN) each

Performance

• Maximum speed: 514 mph (446 kts, 830 km/h)
• Cruise speed: 463 mph (402 kn, 745 km/h)
• Range: 2,522 mi (2,191 NM, 4,059 km)
• Service ceiling: 41,000 ft (12,500 m)
• Rate of climb: 1,950 ft/min (9.9 m/s)

 The Boeing 737 is a short to medium range, single aisle, narrow body jet airliner. The 737-200 is a 737-100 with an extended fuselage. It was launched by United Airlines in 1965. The -200 was rolled out on June 29, 1967 and entered service in 1968. The 737-200 Advanced is an improved version of the -200, introduced by All Nippon Airways on May 20, 1971. The aircraft has improved aerodynamics, automatic wheel brakes, more powerful engines, more fuel capacity and longer range than the -200.