Boeing 767: Difference between revisions

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==767-400ER==
==767-400ER==
==Specifications==
==Specifications==
Powerplants
Two 213.5kN (48,000lb) Pratt & Whitney JT9D-7R4 turbofans or 222.4kN (50,000lb) JT9D-7R4Es, or 222.4kN (50,000lb) PW-4050, or 233.5kN (52,000lb) PW-4052s, or 213.5kN (48,000lb) General Electric CF6-80As or 213.5kN (48,000lb) CF6-80A2s, or 231.3kN (52,500lb) CF6-80C2B2s, or 257.5kN (57,900lb) CF6-80C2B4Fs, or 269.9kN (60,000lb) RollsRoyce RB-211-524Gs.
767-300ER - Same options or 252.4kN (56,750lb) PW-4056s or 266.9kN (60,000lb) CF6-80C2B6s, or two PW-4060 rated at 60,000 lbs MTO


Performance
Max cruising speed 900km/h (486kt), economical cruising speed 850km/h (460kt). Higher gross weight version range with design payload and PW-4050s 7835km (4230nm), with CF6-80C2B2s 7890km (4260nm).
767-300ER - Range with design payload with PW-4060s 10,880km (5875nm), with CF6-80C2B4Fs 10,195km (5505nm).
Weights
767-300 - Empty with PW-4050s 79,560kg (175,400lb), with CF6-80C2B2s 79,379kg (175,000lb). Operating empty with PW-4050s 87,135kg (192,100lb), with CF6-80C2B2s 86,955kg (191,700lb). Higher gross weight version max takeoff with PW-4050s or CF6-80C2B2s 159,210kg (351,000lb).
767-300ER - Empty with PW-4060s 81,374kg (179,400lb), with CF6-80C2B4s 80,603kg (177,700lb). Operating empty with PW-4060s 90,535kg (199,600lb), with CF6-80C2B4s 90,175kg (198,800lb). Max takeoff with PW-4060s 181,890kg (401,000lb), with CF6-80C2B4Fs 175,540kg (387,000lb).
Dimensions
Wing span 47.57m (156ft 1in), length 54.94m (180ft 3in), height 15.85m (52ft 0in). Wing area 283.3m2 (3050sq ft).
Capacity
Flightcrew of two. Typical three class layout for 210, two class 269 (24 premium & 245 economy seven abreast) max seating for 350 at eight abreast. Underfloor capacity for 20 LD2s.
Production
565 767-300s (including ERs) had been ordered by late 1998, of which 496 had been delivered.


[[Category:Widebody Jetliners]]
[[Category:Widebody Jetliners]]

Revision as of 12:42, 9 September 2009

Boeing 767 at a Glance
Role Widebody Jetliner
Country of Origin United States
Manufacturer Boeing
Status In Production
Number Built 977
Unit Cost 80,000,000-139,000,000
File:Airplanes-Boeing 767.jpg


767-200

767-200ER

767-200ERF

767-300

767-300ER

767-300F

767-400ER

Specifications

Powerplants Two 213.5kN (48,000lb) Pratt & Whitney JT9D-7R4 turbofans or 222.4kN (50,000lb) JT9D-7R4Es, or 222.4kN (50,000lb) PW-4050, or 233.5kN (52,000lb) PW-4052s, or 213.5kN (48,000lb) General Electric CF6-80As or 213.5kN (48,000lb) CF6-80A2s, or 231.3kN (52,500lb) CF6-80C2B2s, or 257.5kN (57,900lb) CF6-80C2B4Fs, or 269.9kN (60,000lb) RollsRoyce RB-211-524Gs. 767-300ER - Same options or 252.4kN (56,750lb) PW-4056s or 266.9kN (60,000lb) CF6-80C2B6s, or two PW-4060 rated at 60,000 lbs MTO

Performance Max cruising speed 900km/h (486kt), economical cruising speed 850km/h (460kt). Higher gross weight version range with design payload and PW-4050s 7835km (4230nm), with CF6-80C2B2s 7890km (4260nm). 767-300ER - Range with design payload with PW-4060s 10,880km (5875nm), with CF6-80C2B4Fs 10,195km (5505nm).

Weights 767-300 - Empty with PW-4050s 79,560kg (175,400lb), with CF6-80C2B2s 79,379kg (175,000lb). Operating empty with PW-4050s 87,135kg (192,100lb), with CF6-80C2B2s 86,955kg (191,700lb). Higher gross weight version max takeoff with PW-4050s or CF6-80C2B2s 159,210kg (351,000lb). 767-300ER - Empty with PW-4060s 81,374kg (179,400lb), with CF6-80C2B4s 80,603kg (177,700lb). Operating empty with PW-4060s 90,535kg (199,600lb), with CF6-80C2B4s 90,175kg (198,800lb). Max takeoff with PW-4060s 181,890kg (401,000lb), with CF6-80C2B4Fs 175,540kg (387,000lb).

Dimensions Wing span 47.57m (156ft 1in), length 54.94m (180ft 3in), height 15.85m (52ft 0in). Wing area 283.3m2 (3050sq ft).

Capacity Flightcrew of two. Typical three class layout for 210, two class 269 (24 premium & 245 economy seven abreast) max seating for 350 at eight abreast. Underfloor capacity for 20 LD2s.

Production 565 767-300s (including ERs) had been ordered by late 1998, of which 496 had been delivered.