Specifications
Data from Boeing Aircraft since 1916
| 727-100 (Passenger) |
727-200 | 727-200 Advanced | |
|---|---|---|---|
| Seating capacity | 149 passengers (one-class) 131 passengers (two-class) |
189 passengers (one-class) 145 passengers (two-class) |
|
| Cargo capacity | |||
| Crew | 3 flight crew plus ca. 4 cabin crew | ||
| Total length | 133ft 2in (40.6m) | 153 ft 2 in (46.69 m) | |
| Fuselage length | |||
| Fuselage width | |||
| Wingspan | 108 ft 0 in (32.92 m) | ||
| Wing area | 1,650 sq ft (153 m2) | ||
| Tail height | 34 ft 0 in (10.36 m) | ||
| Maximum Takeoff Weight (MTOW) * |
170,000 lb (77,000 kg) | 184,800 lb (83,800 kg) | 209,500 lb (95,000 kg) |
| Operating empty weight | 80,602 lb (36,560 kg) | 98,400 lb (44,600 kg) | 102,900 lb (46,700 kg) |
| Max. fuel capacity | 7,680 USgal (29,100 l) | 8,090 USgal (30,600 l) | 10,520 USgal (39,800 l) |
| Take-off distance at MTOW | |||
| Max range (with typical load) |
2,700 nmi (5,000 km) | 2,433 nmi (4,506 km) | 3,165 nmi (5,862 km) |
| Max cruise speed | Mach 0.9 | ||
| Typical cruise speed | 599 mph (521 kn) | ||
| Service ceiling | 36,100 ft (11,000 m) | 42,000 ft (13,000 m) | 42,000 ft (13,000 m) |
| Rate of climb | 2,940 ft/min (14.9 m/s) | ||
| Engines (3x) | Pratt & Whitney JT8D-1 14,000 lbf (62 kN) thrust each |
Pratt & Whitney JT8D-9 14,500 lbf (64 kN) thrust each |
Pratt & Whitney JT8D-17R 17,400 lbf (77 kN) thrust each |
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