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Aviation History
2000
2000-1 - 1797.PDF
3 Engine Max Thrust Dry Length Fan Variant kN lb weight (kg) m diameter (m) EPR Dassault Falcon 10, CASA C-101, Bombardier Learjet 35/36, FMA IA.63, AIDCAT-3; TFE731-3 Cessna Citatior 16.24kN thrust TFE7314 Cessna Citatior TFE731-20 Bombarier Lear 16 3,700 342 III, Dassault Falcon 50, BAe 125-700 powers Cessna Citation III and IV 18 4,100 373 VII, Aero Vodochody L-139 16 3,500 406 1.52 0.72 14.6 IAI Westwind 1/2, Galaxy Ast 1.48 1.55 et 45; max thrust 16.29kN, 15.56kN in Learje TFE731-40 19 4,200 406 Dassault Falcon 50EX, Galaxy Astra SPX, Raytheon H TFE731-5 20 4,500 400 Raytheon Hawker 800, CASA C-101; -5A powers Pass TFE731-60 Daasult Falcon 22 5,000 448 900EX tmiimmmmMMmnw V2500 V2500-A1 Airbus A320-10 111 25,000 2,365 0 V2522-A5 98 22,000 2,374 Airbus A319; flat rated from sea level to 55°C V2524-A5 Airbus A319, A V2525-D5 Boeing MD-90-. 107 24,000 2,374 "J; flat rated from sea level to 55°C 111 25,000 2,540 0 V2527-A5 118 26,500 2,374 Airbus A320-200; flat rated from sea level to 55°C V2527E-A5 111 25,000 2,374 Airbus A320-200; E denotes revised thrust managem V2527M-A5 111- 25,000 2,374 1.55 wker4t 1.39 ault Falc 2.08 3.20 3.20 3.20 3.20 3.20 3.20 >nt softw 3.20 0.72 0.72 45 0.72 0 0.76 14.8 14.3 16.3 14.6 SFC take-off BPR mg/Ns Ib/h/lb -2A powers NAMC/PAC K-8 2.8 a, Rockwe •-• 3.1 2.9 3.5 •>n 900 and r&engined Falcon 21 0.78 1.60 1.61 1.61 1.61 1.61 1.61 are optimisec 1.61 17.8 29.8 25.6 26.4 27.2 for high 3.9 5.4 4.9 4.9 4.8 4.8 4.8 altitude a 4.8 A319, ACJ; M denotes revised thrust management software optimised for higher MTOW V2528-D5 125 28,000 2,546 Boeing MD-90-30 V2530-A5 140 31,400 2,374 Airbus A321-100 V2533-A5 A321-200 •l'M!ld!l! 147 33,000 2,374 "1 II li^™ Al-22 AI-22 37 8,400 765 Tupolev Tu-324 D-18T D-18T 230 51,600 4,100 Anotonov An-124, An-225; D-18TM powers An-218 D-27 D-27 1,650 AntonovAn-70, An-70T, An-180, BerievBe-42 D-36 D-36-5A Under developr 64 14,300 1,200 nent D-436 D436-T1/TP/T 75 16,900 1,450 Tupolev Tu-334, Beriev Be-200, Yakovlev Yak-42M mjHMOMMimiriLI^^^^^ JT8D-15A 69 15,500 1,577 JT8D-17 72 16,200 1,557 Boeing 727. 737, Douglas DC-9 JT8D-200 97 21,700 2,056 3.20 3.20 3.20 * 3.01 5.40 4.21 3.73 4.17 3.92 3.92 3.92 •217 powers Boeing MD-82; -217A powers MD-82 and MDS7; JT8D-209 86 19,200 2,013 Boeing MD£2 JT8D-217 89 20,000 2,029 Boeing MD42 3.92 3.92 1.61 1.61 1.61 1.04 2.33 0.97 1.37 1.37 1.25 1.25 1.25 30.0 32.1 33.4 15.5 25.0 22.0 18.9 22.8 16.5 16.9 17.1 -217C powers MDS2 1.25 1.25 17.4 18.6 4.7 4.5 4.5 4.8 5.6 - 5.3 5.0 1.0 1.0 1.8 MD-83.K 1.8 1.7 14.93 II Sabrelint 14.39 13.97 13.37 13.30 ); -5B powe 11.47 15.36 15.36 15.36 15.36 15.36 15.36 rport and 1 15.36 15.36 15.36 15.36 11.33 9.77 64.20 10.14 10.47 16.95 18.25 14.15 1DS7and 14.17 14.43 0.528 r65A.CAS/ 0.508 0.494 0.472 0.470 rs Falcon 9C 0.405 0.543 0.543 0.543 0.543 0.543 0.543 Fans 1 C-101, 1 1 1 1 WB 1 1 1 1 1 1 1 Compressors Low Irrterm High 4 FMA IA 63; 4 4 4 4 4 3 4 4 4 4 4 igher MTOW applications. 0.543 0.543 0.543 0.543 0.400 0.345 2.269 0.358 0.370 0.599 0.645 • 0.500 VID-88;-219 0.501 0.510 1 1 1 1 1 1 1 1+1B 1 1 1 powers 1 1 4 4 4 4 5 5 6 6 ^^^^_ 6 6 * 6 1 Turbines Low Irrterm 3 -3A powers. Learjet 55 and Astra, 1 1 1 1- 1 10 10 10 10 10 10 10 10 10 10 7 7 7 3 7 7 7 7 7 3 3 3 3 3 5 5 5 5 5 5 5 5 5 5 3 4 1 4 1 3 1 3 1 3 3 1 MCh82, MDS3, MD-87 andMDS8 6 • 6 7 7 3 3 High 1 3Bat 1 1 1 1 1 2 2 2 2 2 2 2 2 2 2 1 1 1 1 1 1 1 1 1 1 FLIGHT INTERNATIONAL 14 - 20 November 2000 57
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