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.
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).
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).
Wing span 47.57m (156ft 1in), length 54.94m (180ft 3in), height 15.85m (52ft 0in). Wing area 283.3m2 (3050sq ft).
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.
652 767-300s (including ERs) had been ordered by late 2002, of which 607 had been delivered.
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