FlightGlobal.com
Home
Premium
Archive
Video
Images
Forum
Atlas
Blogs
Jobs
Shop
RSS
Email Newsletters
You are in:
Home
Aviation History
1973
1973 - 2602.PDF
FLIGHT International, 18 October 1973 649 Speeds kt, km/hr) V2 VAT 'NO'MNO VNE/MNE Max cruise Cruise performance Speed: kt (km/hr) Altitude: ft (m) Fuel consumption: Ib/hr (kg/hr) Cost economical Long range Payload-range ISA, still air, no reserves Max payload Full tanks in lb (kg) over payload in lb (kg) range of n.m. (km) over range of at cost econ. n.m. (km) at cruise long-range cruise (267) (252) (667)/0-84 506 (938) 25,000 (7,620) 17,800 (8,075) 481 (891) 31,000 (9,450) 14,700 (6,670) 454 (841) 33,000 (10,060) 12,500 (5,670) 70,000 (31,750) 1,300 (2,410) 39,500 (17,920) 2,700 (5,000) 300,0001b (136,080kg). Price $175 million (.FLIGHT index). n.a, n.a. n.a. n.a. Mach 0 80 30,000 (9,150) Mach 0-73 30,000 (9,150) 1,900 n.m./Mach 0 8/191 pax 2,100 n.m./Mach 0 8/191 pax (FAR domestic reserves) For s.l., ISA -r 20°C, 500 n.m. sector. For s.l., ISA + 20°C, 2,000 n.m. sector. For s.!., ISA + 20"C, max landing weight. n.a. n.a. (623)/0-78tt n.a. n.a. 1 (589)/0-78tt n.a. 1 (283) 1 (243) I (648)/0 84 n.a. i(270) > (219) ) (648)/0 84 n.a. )(705)/0 85 ) i (265) >/0-88 n.a. » (248) ' (235) ) (647)/0-84 -> (785)/0-89 ' (272) » (238) ) (647)/0-84 i (785) 10 89 (289) 1 (242) ) (628)/0-84 i (785)/0 89 '(291) i (252) l(630)/0-84 1 (264) > (257) ' (603) 10 82 459 (85l)() 30,000 (9,150) 6,059 (2,748) 457(847)§ 30,000 (9,150) 6,1 1 1 (2,772) 479 (887) 20,000 (6,096) 8,048 (3,650) 490 (908) 25,000 (7,600) 9,477 (4,293) 502 (930) 25.000 (7,600) 9,400 (4,260)" 488 (904) 28,000 (8,534) 9,250 (4,196) 504 (930) 23,000 (7,000) 8,810 (4,000) 497 (918) 25,000 (7,600) 8,230 (3,740) 488 (903) 27,000 (8,200) 8,190 (3,720) 490 (908) 27,000 (8,200) 9,250 (4,190) 486 (898) 28,000 (8,500) 7,561 (3,430) 459 (85l)tj 30,000(9,150) 6,059 (2,748) 457 (847) § 30,000 (9,150) 6,1 1 1 (2,772) 460 (853) 30,000 (9,150) 6,470 (2,940) 460 (853) 30,000 (9,100) 6,560 (2,980) 480 (890) 30,000 (9,150) 7,320 (4,260)*" . — 465 (860) 33,000 (10,000) 5,170 (2,340) 465 (860) 33,000 (10,000) 5,430 (2,490) 465 (860) 33,000 (10,000) 6,210 (2,820) 465 (861) 33,000 (10,000) 7,000 (3,170) 459 (849) 36,000 (11,000) 4,842 (2,650) 410 (760)§ 35,000 (10,700) 4,300 (1,950) 423 (784) § 35,000 (10.700) 4,953 (2,247) 418 (774) 35,000 (10,700) 5,000 (2,268) 418 (774) 35,000 (10,700) *" 5,070 (2,296) 446 (825) 35,000 (10,700) 5,570 (2,530)** 470 (870) 30,000 (9,144) 7,975 (3,617) 432 (798) 35,000 (10,700) 4,190 (1,900) 431 (796) 35,000 (10,700) 4,420 (2,000) 437 (806) 35,000 (10,700) 5,000 (2,270) 442 (819) 35,000 (10,700) 5,650 (2,560) 405 (749) 36,000 (1 1,000) 4,585 (2,080) 20,866 (9,465) 1,389 (2,574) 26,187 (I 1,879) 1,303 (2,415) 33,980 (15,393) 1,240 (2,300) 35,000 (15,855) 1,280 (2,370) 32,850 (14,900) 905 (1,680) 35,350(16,034) 1,990 (3,687) 31,500 (14,300) 1,090 (2,020)t 30,200 (13,700) 1,370 (2,530)** 36,500 (16,200) 1,080 (2,000)t 33,000 (14,950) 1,275 (2,360)t I 6,980 (7,700) 1,538 (2,840) 15,186 (6,888) 2,245 (4,160) 20,159 (9,144) 2,026 (3,755) 22,759 (10,307) 2,460 (4,560) 21,369 (9,680) 2,740 (5,074) 18,340 (8,320) 2,225 (4,120) 28,250 (12,814) 2,375 (4,400) 23,000(10,450) 2,000 (3,700) 26,700 (12,200) 1,750 (3,230) 30,500 (13,850) 1,650 (3.050) 21,400 (9,700) 2,420 (4,480) 8,820 (4,000) 2,536 (4,670) All field lengths to BCAR * Up to 98,5001b (44,680kg) ** with 89 seats, t At 90.2001b (40,915kg) tt At MZW § At 81,500 (36,968 kg) All field lengths to BCAR. * Optional 104,5001b (47,401kg). ** I 19 seats. t At 91,0281b (41,290kg). t At 82,6951b (37,510kg). tt At max ZFW. § At 89,0001b (40,370kg). Price $5-2 million (FLIGHT index). Price $5-2 million (FLIGHT index). At II 0,0001b (50,000kg). At 100,0001b (45,000kg). Includes water injection. * Second-segment limited. ** Approach-climb limited, t At Mach 0 80. Second segment limited. At Mach 0 80. * Second-segment limited. ** Approach-climb limited, t At Mach 0 80. Price $5 2 million (FLIGHT index). * Second-segment limited. ** Approach-climb limited, t At Mach 0-80. * For data on Tu-I34A see page 667. ** Gravity fuelling. 450 (830) 25,000 (7,700) n.a. 450 (830) 2,500 (7,700) n.a. 458 (848) 21,000 (6,400) 6,180 (2,800) 458 (848) 21,000 (6,400) 6,180 (2,800) 427 (790) 22,00 (6,706) 5,850 (2,654) 411 (762) 22,000 (6,706) 5,750 (2,608) 397 (735) 21,000 (6,400) 3,700 (1,680) 297 (548) 18,000 (6,000) _ 451 (834) 25,000 (7.600) 5,470 (2,480) 451 (834) 25,000 (7,600) 5,470 (2,480) — 390 (720) 25,000 (7,600) 3,180 (916) 270 (498) n.a. 404 (750) 35,000 (10,700) n.a. 404 (750) 35,000 (10,700) n.a. 359 (666) 30,000 (9,150) 3,260(1,480) 359 (666) 30,000 (9,150) 3,260 (1,480) 364 (675) 30,000 (9,144) 3,850(1,746) 364 (675) 30,000 (9,144) 4,150 (1,882) 293 (543) 25,000 (7,600) 1,960 (889) n.a. 24,000 (8,000) 7,500 (3,400) 830 (1,540) 8,000 (3,625) 770 (1,430) 18,983 (8,629) 920 (1,705) 17,547(7,976) 920 (1,705) 18,500 (8,390) 800 (1,483) 20,500 (9,300) 1,340 (2,483) 9,040 (4,100) 650 (1,200) 5.080 (2,310) 540 (1,000) 4,200 (1,900) 1,950 (3,610) 4,200 (1,900) 1,950 (3,610) 6,533 (2,970)* 2,620 (4,855) 5,100 (2,318)* 2,620 (4,855)* 13,300 (6,035) , 1,590 (2,947) 19,500 (8,845) 1,830 (3,390) 5,320 (2,415) 1,563 (2,896) 3,140(1,425) 800 (1,475) With centre-section wing tank. Price $4 million (FLIGHT index). Details of slatted version, page 659. With centre-section wing tank. 81,0001b take-off weight. 76,2001b landing weight. Second-segment limited. Price DM9 7 million.
Sign up to
Flight Digital Magazine
Flight Print Magazine
Airline Business Magazine
E-newsletters
RSS
Events