( )Tj /P <>BDC (compared to 16,200kg on classics). EMC ET ( )Tj BT 8 0 0 8 314.4333 745.9528 Tm BT (across the world, since they are proven to)Tj 6 0 0 6 513.0339 701.9528 Tm BT /P <>BDC ET /P <>BDC ET EMC 0 Tc BT EMC 0 Tc EMC (24)Tj /P <>BDC (similar rate, with Boeing having delivered)Tj 7 0 0 7 445.619 617.7654 Tm (217)Tj ( )Tj 6 0 0 6 327.5828 701.9528 Tm ET https://simpleflying.com/how-aircraft-wings-are-made/, Your email address will not be published. (2,732)Tj /P <>BDC 7 0 0 7 440.0906 408.9528 Tm 0 Tc ET BT EMC BT ( )Tj 6 0 0 6 465.9579 659.9528 Tm /P <>BDC /P <>BDC -.02 Tc ET ET /P <>BDC (165)Tj ( )Tj BT ET EMC 6 0 0 6 153.2734 687.9528 Tm ET Boeing has its 737 in almost every single developed nation. ( )Tj ET 7 0 0 7 508.4124 496.7654 Tm BT /P <>BDC (483)Tj 7 0 0 7 473.8245 298.9528 Tm [(OM)8.1(M)-12.9(E)-24.9(R)7.1(C)8.1(E)]TJ (have any payload limitations on the routes)Tj ET ET BT (that in scenario 1 both aircraft carry 170)Tj q 1 0 0 1 36.85 797.54 cm 0 0 m 9 0 0 9 204.9907 467.8898 Tm 9 0 0 9 53.8578 269.8898 Tm Boeing uses Rockwell Collins avionics for the 737-800. 0 Tc ( )Tj 7 0 0 7 362.3891 342.9528 Tm /OC /MC5097 BDC ET /P <>BDC ET 6.5 0 0 6.5 499.1421 722.9529 Tm ET (. ET 6 0 0 6 184.9362 743.9528 Tm 0 Tc -.02 Tc ET BT ( )Tj BT ET EMC 7 0 0 7 258.2805 441.7654 Tm ET /F2 1 Tf -.02 Tc -.02 Tc ET /P <>BDC ET (comparison of the fuel burn performance. EMC EMC ET ET EMC The website is currently in the process of optimizing and will have further functions added in order to improve the usability. ET EMC (4,000nm with maximum passenger)Tj ET ET ET 9 0 0 9 361.016 49.8898 Tm Fokker 100, the Netherlands regional jet. BT Your email address will not be published. /P <>BDC ( )Tj 0 Tc 0 Tw 6.5 0 0 6.5 64.6596 532.9529 Tm ( )Tj ET /P <>BDC ( )Tj EMC ET ET /P <>BDC ET ET /P <>BDC BT ( )Tj /P <>BDC 7 0 0 7 43.6039 441.9528 Tm EMC ( )Tj ET EMC 0 Tw /P <>BDC /P <>BDC provision for a ferry kit. EMC ( )Tj 7 0 0 7 247.7395 221.7654 Tm BT ( )Tj BT ET /P <>BDC -.02 Tc ( )Tj BT EMC /P <>BDC EMC /P <>BDC 9 0 0 9 571.1344 742.8898 Tm BT ( )Tj ET EMC /P <>BDC ( )Tj EMC -.01 Tc EMC BT -.01 Tc (44,352)Tj 53.85 621.704 518.723 183.336 re ( )Tj /GS1 gs ET ET 7 0 0 7 230.7317 463.9528 Tm 6.5 0 0 6.5 191.7926 702.9529 Tm ( )Tj (1,311)Tj 0 Tc /P <>BDC BT )Tj /P <>BDC EMC EMC 9 0 0 9 356.2376 236.8898 Tm 9 0 0 9 215.4313 71.8898 Tm 7 0 0 7 355.3163 320.7654 Tm 9 0 0 9 369.4048 456.8898 Tm ET EMC (fan diameter of 81 inches, and a bypass)Tj BT 7 0 0 7 125.6292 287.7654 Tm ( )Tj BT ET (2,732)Tj /P <>BDC 8 0 0 8 164.9203 771.9528 Tm EMC (831)Tj ET EMC ET EMC BT (152)Tj ET BT ET EMC BT EMC EMC BT 9 0 0 9 232.4217 522.8898 Tm /P <>BDC /P <>BDC ET /P <>BDC (a 3.3% advantage for the A321neo on the)Tj (191,240)Tj BT BT EMC EMC EMC (financial cost structure and their fuel)Tj BT EMC /P <>BDC BT 0 Tc /P <>BDC BT (the IAE V2533-A5 engine, rated at)Tj -.02 Tc (Max payload - lbs)Tj EMC 0 Tc -.02 Tc (2,094)Tj ( )Tj 0 Tc i.e..what is the maximum lateral distance the doors swing away from the aircraft, before they get to rest in the fully open position? ET /P <>BDC -.01 Tc ( )Tj 9 0 0 9 36.8504 467.8898 Tm ( )Tj ET BT BT ( )Tj BT ( )Tj ET 7 0 0 7 141.7322 298.9528 Tm BT /P <>BDC EMC /P <>BDC /P <>BDC ET /P <>BDC ET /P <>BDC ( )Tj (737-8)Tj )Tj .559 .331 .619 rg tank. ET EMC EMC ( )Tj ET BT /P <>BDC BT /P <>BDC BT EMC BT )Tj 7 0 0 7 37.5838 540.9528 Tm /Artifact <>BDC /P <>BDC /P <>BDC ET BT (976)Tj ET ( )Tj BT BT /P <>BDC EMC 9 0 0 9 112.6132 302.8898 Tm /P <>BDC EMC (1,162)Tj S EMC ( )Tj EMC 0 Tc 7 0 0 7 187.0858 309.9528 Tm /P <>BDC /P <>BDC 7 0 0 7 36.8504 155.9528 Tm BT 6 0 0 6 507.2798 715.9528 Tm EMC EMC EMC EMC BT ET BT }Qi_I0A"j EMC ( )Tj /P <>BDC BT /P <>BDC ( )Tj /P <>BDC EMC EMC (when using a cost index. BT (0.0140)Tj EMC ET BT EMC BT /P <>BDC The Boeing 737 has four distinct families of variants within the type. 9 0 0 9 361.7 456.8898 Tm q ET (and even the individual aircraft registration)Tj ET ET (5,843)Tj BT /P <>BDC ( )Tj ET (earlier counterpart. ET EMC ( )Tj ( )Tj (this page\))Tj BT ET BT ( )Tj 0 Tc /P <>BDC 7 0 0 7 491.7142 89.7654 Tm /P <>BDC ET ( )Tj ET ( C)Tj /Artifact <>BDC (34,650lbs)Tj EMC /P <>BDC 7 0 0 7 141.7322 672.9528 Tm Other data such as fuel load, [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ ( )Tj EMC /P <>BDC EMC 0 Tc BT ( )Tj BT ET ET /P <>BDC ET EMC .001 Tc (111)Tj ( )Tj 0 Tc (challenge for all airlines. (152)Tj ET 0 Tc /P <>BDC BT 0 Tc /P <>BDC EMC ET 7 0 0 7 440.3636 474.9528 Tm 7 0 0 7 95.225 11.5132 Tm /GS2 gs (163)Tj (0.0141)Tj 7 0 0 7 535.5029 474.7654 Tm BT 17 0 0 17 36.8606 775.1944 Tm ( )Tj /P <>BDC BT EMC /P <>BDC BT ET (I)Tj BT EMC /P <>BDC BT BT 10 0 0 10 278.2126 794.2914 Tm EMC 6 0 0 6 184.3662 673.9528 Tm -.02 Tc 9 0 0 9 175.0911 269.8898 Tm ET /P <>BDC EMC ( )Tj EMC BT ET EMC ET /P <>BDC BT BT EMC /P <>BDC 0 Tc (0.0129)Tj EMC EMC BT 0 Tc (34,650)Tj BT (the aircraft in this study are shown )Tj (30,000lbs to 33,000lbs, a fan diameter of)Tj 7 0 0 7 230.7317 694.9528 Tm 9 0 0 9 394.0157 302.8898 Tm 9 0 0 9 394.0123 555.8898 Tm /P <>BDC EMC 7 0 0 7 294.4014 276.7654 Tm BT 7 0 0 7 88.196 11.5129 Tm /P <>BDC ( )Tj /P <>BDC /P <>BDC EMC aux (AA) and fwd aux (FA) respectively. /P <>BDC 9 0 0 9 548.2598 489.8898 Tm ( )Tj /P <>BDC EMC 9 0 0 9 546.4149 456.8898 Tm /P <>BDC ET BT BT ( )Tj (831)Tj ET /P <>BDC /P <>BDC EMC ET 0 Tc -.02 Tc /P <>BDC BT BT ET /P <>BDC (737-8)Tj ( )Tj ET EMC BT ET (are taxi fuel burn, flight fuel burn, the)Tj EMC 9 0 0 9 394.0315 797.8898 Tm EMC BT ET /P <>BDC ( )Tj ( )Tj /P <>BDC 6 0 0 6 54.1367 771.9528 Tm ET 9 0 0 9 73.1083 522.8898 Tm ET ET -.02 Tc ET -.02 Tc /P <>BDC EMC /P <>BDC (31,416)Tj /P <>BDC 9 0 0 9 53.8582 621.8898 Tm BT BT /P <>BDC /P <>BDC EMC EMC ET 9 0 0 9 392.5848 346.8898 Tm 9 0 0 9 232.4217 566.8898 Tm BT 7 0 0 7 141.7322 89.9528 Tm EMC BT (172,842)Tj BT ET ( )Tj ( )Tj EMC EMC EMC 0 Tc ( )Tj ET 9 0 0 9 552.5312 687.8898 Tm BT EMC EMC EMC EMC [(P)11(ayload)]TJ EMC EMC ( )Tj ( )Tj Alaska Airlines launched the 737-900 in 1997, the 737-900 made its first . ( )Tj 9 0 0 9 528.7084 742.8898 Tm ( )Tj In the cargo configuration, The 737-700C can carry up to 18,780 kg (41,420 pounds) of cargo on eight . /P <>BDC /P <>BDC /P <>BDC BT /P <>BDC BT ET /P <>BDC EMC 8 0 0 8 337.3163 771.9528 Tm /GS2 gs /P <>BDC EMC -.01 Tc EMC /P <>BDC EMC BT 7 0 0 7 258.2805 265.7654 Tm BT 7 0 0 7 535.5029 738.7654 Tm -.02 Tc ET /P <>BDC BT EMC ( )Tj 9 0 0 9 394.0157 643.8898 Tm 6.5 0 0 6.5 104.3885 722.9529 Tm EMC 7 0 0 7 473.8245 210.9528 Tm 6.5 0 0 6.5 375.6529 689.9529 Tm /P <>BDC /P <>BDC [(BOS-D)17.1(T)-11(W)]TJ /P <>BDC EMC 7 0 0 7 427.7291 100.9528 Tm EMC BT BT ET ( )Tj EMC 7 0 0 7 247.7395 716.7654 Tm Digital Sunburst Fuel Gauges - Simmonds 4 Tank. BT EMC 9 0 0 9 551.0557 467.8898 Tm ( )Tj EMC ( )Tj EMC BT ( )Tj ( )Tj 7 0 0 7 99.8582 221.7654 Tm ( )Tj ( )Tj ET BT ( )Tj EMC BT BT ET BT (A320neo)Tj BT ET (would need to consider many more factors)Tj ( )Tj ET BT EMC 6.5 0 0 6.5 295.5027 624.9529 Tm EMC EMC -.02 Tc BT -.02 Tc 6.5 0 0 6.5 540.4371 611.9529 Tm /P <>BDC ET /P <>BDC BT ( )Tj /P <>BDC ( )Tj automatically moved back to OFF after one minute. ( )Tj ET BT (403)Tj EMC 7 0 0 7 554.7883 309.7654 Tm 7 0 0 7 230.7317 628.9528 Tm ( )Tj ET BT BT /P <>BDC 7 0 0 7 241.2727 144.9528 Tm ( )Tj BT EMC 7 0 0 7 187.0858 331.9528 Tm /P <>BDC BT 9 0 0 9 545.1909 346.8898 Tm ET 0 Tc /P <>BDC ET ( )Tj BT EMC ET [(CFM L)17.1(E)-8.1(AP-1A26)]TJ BT 9 0 0 9 570.6951 291.8898 Tm -.02 Tc 9 0 0 9 394.0315 643.8898 Tm BT /P <>BDC EMC 7 0 0 7 37.6993 287.9528 Tm BT Hi Andrey, EMC EMC /P <>BDC ET BT -.02 Tc ET ET ET /P <>BDC ET /P <>BDC /P <>BDC EMC )Tj /P <>BDC EMC ET EMC Airbus A330 History How did one of the worlds most popular twin jets evolve. /P <>BDC (977)Tj /P <>BDC EMC ET EMC BT ( )Tj 7 0 0 7 82.2047 595.9528 Tm /P <>BDC EMC -.02 Tc /P <>BDC /P <>BDC BT (\(see table, page 19\))Tj 7 0 0 7 82.8504 353.9528 Tm /P <>BDC ET ( )Tj /P <>BDC ( )Tj BT 9 0 0 9 408.2047 423.8898 Tm 9 0 0 9 382.3068 489.8898 Tm EMC ET 7 0 0 7 457.0984 628.7654 Tm The 1/200's had heater switches; these used bleed air to heat the EMC 9 0 0 9 408.1854 511.8898 Tm 6.5 0 0 6.5 536.8751 722.9529 Tm 9 0 0 9 232.438 269.8898 Tm 7 0 0 7 321.6356 265.9528 Tm EMC 0 Tc 0 Tc ( )Tj BT /P <>BDC ET EMC 0 Tc -.02 Tc BT /P <>BDC ( )Tj (39,270)Tj 9 0 0 9 386.3946 137.8898 Tm EMC /P <>BDC ET ( )Tj /P <>BDC ( )Tj EMC ( )Tj BT 9 0 0 9 53.8582 357.8898 Tm BT 0 Tc 0 Tc ET BT 9 0 0 9 53.8578 115.8898 Tm EMC EMC 0 Tc 9 0 0 9 394.0157 214.8898 Tm 0 Tc EMC 9 0 0 9 325.0684 434.8898 Tm EMC /P <>BDC /P <>BDC BT /P <>BDC ( )Tj 7 0 0 7 459.6601 11.5129 Tm ( )Tj 6.5 0 0 6.5 244.2974 545.9529 Tm 9 0 0 9 394.0315 742.8898 Tm EMC BT BT 0 Tc 6 0 0 6 277.7663 673.9528 Tm EMC ( )Tj /P <>BDC BT EMC -.02 Tc /P <>BDC /P <>BDC ( )Tj EMC ( )Tj ET EMC BT 9 0 0 9 377.4586 676.8898 Tm BT 9 0 0 9 408.1889 467.8898 Tm ( )Tj 7 0 0 7 386.3929 639.9528 Tm ET BT 7 0 0 7 108.6215 364.9528 Tm 8 0 0 8 153.6923 591.9528 Tm BT [(737-900E)-33(R)]TJ 7 0 0 7 321.6356 199.9528 Tm 7 0 0 7 314.6398 463.7654 Tm /P <>BDC BT BT ET /P <>BDC These are: Below is a table of the main features and specifications for the Boeing 737 family of aircraft. Q EMC EMC 0 Tc ( )Tj start a self test of the display and the fuel quantity indicating system. /P <>BDC ET BT /P <>BDC ET 5.25 0 0 5.25 73.853 11.5132 Tm ET [(7)-33(3)8.1(7-900ER\(W)-19(\) v)12.9(ersus 7)-33(3)8.1(7-9 )]TJ /P <>BDC EMC -.01 Tc 17 0 0 17 560.3929 742.1944 Tm EMC EMC EMC ( )Tj 7 0 0 7 141.7322 78.9528 Tm 6.5 0 0 6.5 375.6529 702.9529 Tm 9 0 0 9 394.0315 192.8898 Tm 7 0 0 7 241.2727 276.9528 Tm EMC ET /OC /MC1320 BDC ET 7 0 0 7 193.1059 584.9528 Tm EMC ET BT 0 Tc 7 0 0 7 279.1575 738.9528 Tm BT 0 Tc (2,431)Tj /P <>BDC BT EMC 7 0 0 7 279.1575 408.9528 Tm BT /P <>BDC 7 0 0 7 77.36 11.5132 Tm (number of available seat-miles \(ASM\))Tj EMC 9 0 0 9 411.0097 379.8898 Tm BT /P <>BDC /P <>BDC ET /P <>BDC ET 0 Tc ( )Tj BT /P <>BDC BT ET ET (0.0126)Tj (to allow a clearer performance and fuel)Tj ( )Tj 8 0 0 8 302.5117 717.9528 Tm ET ET (104)Tj (207,336)Tj 9 0 0 9 536.6833 500.8898 Tm BT BT .41 .161 .508 rg (referred to as premium, main cabin extra)Tj ET ET soaked fuel causing frost to form on the wings during the turnarounds - even in 0 Tc (977)Tj ET 9 0 0 9 200.4718 38.8898 Tm 7 0 0 7 82.8504 221.9528 Tm BT [(737-900E)-33(R)]TJ ET ET 9 0 0 9 545.7273 731.8898 Tm ( )Tj /P <>BDC ET ( )Tj ET /P <>BDC ( )Tj /P <>BDC EMC 0 Tc 9 0 0 9 209.838 60.8898 Tm (A320, the A321 neo is significantly heavier)Tj (aircraft types, all the flights were evaluated)Tj 9 0 0 9 214.4188 478.8898 Tm ( )Tj EMC /P <>BDC 9 0 0 9 75.273 445.8898 Tm 9 0 0 9 215.4313 49.8898 Tm ET The 737-9 has a)Tj ET BT (. /P <>BDC /P <>BDC 9 0 0 9 36.8504 511.8898 Tm /P <>BDC ET 9 0 0 9 207.5518 588.8898 Tm )21(This ar)-23(ticle)]TJ 7 0 0 7 298.1781 111.9528 Tm EMC ET 0 Tc /P <>BDC /P <>BDC ET ET /P <>BDC /P <>BDC EMC 9 0 0 9 411.0234 742.8898 Tm /P <>BDC EMC ET 7 0 0 7 537.7804 331.9528 Tm BT EMC ET ET BT EMC BT BT -.02 Tc -.02 Tc /P <>BDC ( )Tj ( )Tj ET EMC ET EMC 6 0 0 6 289.3167 715.9528 Tm BT BT BT ( )Tj BT /P <>BDC /P <>BDC ET ( )Tj 9 0 0 9 53.8578 313.8898 Tm 9 0 0 9 394.0315 731.8898 Tm BT BT ( )Tj )Tj BT [(CFM L)17.1(E)-8.1(AP-1A26)]TJ /P <>BDC /P <>BDC BT /P <>BDC EMC ET -.02 Tc BT (mainline carriers may in fact opt to use a)Tj 9 0 0 9 68.0314 467.8898 Tm ( )Tj /P <>BDC BT W n (and in fuel burn per ASM. BT 0 Tc 9 0 0 9 552.2133 291.8898 Tm 9 0 0 9 36.8504 38.8898 Tm ET BT ( A)Tj ET BT 7 0 0 7 491.7142 606.7654 Tm ( )Tj ET /P <>BDC -.02 Tc ( )Tj BT /P <>BDC BT -.01 Tc NG/MAX: The engine spar valves and APU are normally powered by the hot /P <>BDC 6.5 0 0 6.5 243.7903 611.9529 Tm BT 0 Tc 17 0 0 17 536.8649 791.6944 Tm 7 0 0 7 99.8582 430.7654 Tm (1,800 - )Tj ( )Tj ET ET EMC ( )Tj /P <>BDC BT (5.7:1)Tj ET 9 0 0 9 215.433 280.8898 Tm 9 0 0 9 534.0193 390.8898 Tm BT /P <>BDC EMC ( )Tj EMC ET ( )Tj BT (be charged the same in operation for this)Tj BT (213,848)Tj ET -.02 Tc ( )Tj ( )Tj /P <>BDC /P <>BDC BT EMC 9 0 0 9 53.8582 115.8898 Tm 9 0 0 9 541.3533 522.8898 Tm ET BT EMC 9 0 0 9 232.438 181.8898 Tm EMC (A320neo will be evaluated with the same)Tj EMC EMC /P <>BDC /P <>BDC BT 7 0 0 7 427.7291 177.9528 Tm -.02 Tc 9 0 0 9 36.8504 346.8898 Tm 7 0 0 7 148.0554 11.5132 Tm BT (The thrust ratings on the engines show)Tj /P <>BDC EMC ET 9 0 0 9 525.3974 192.8898 Tm /P <>BDC 7 0 0 7 469.2222 11.5129 Tm /GS1 gs /P <>BDC BT EMC BT EMC BT /P <>BDC 9 0 0 9 229.6141 335.8898 Tm At engine idle, the system tolerance can be 12%. /P <>BDC /P <>BDC -.005 Tc ET ( )Tj ET EMC BT 8 0 0 8 275.7172 760.7654 Tm EMC (2,517)Tj 9 0 0 9 215.4313 445.8898 Tm EMC (The Sky interior means the MAX)Tj ET BT BT /P <>BDC ET /P <>BDC ET ET /P <>BDC BT BT BT ET 7 0 0 7 258.2805 727.7654 Tm 8 0 0 8 105.6516 760.9528 Tm ( )Tj EMC 7 0 0 7 554.7883 320.7654 Tm /P <>BDC 0 Tc ET ET (The first-class layout uses four-abreast)Tj ET /P <>BDC 7 0 0 7 87.8179 738.7654 Tm .0081 Tc /P <>BDC BT ET /F4 1 Tf BT There are no pumps in the aux fuel system. ET /P <>BDC ( )Tj ( )Tj 7 0 0 7 387.0932 199.9528 Tm 9 0 0 9 394.0157 280.8898 Tm BT 6 0 0 6 434.151 757.9528 Tm BT ET -.02 Tc 7 0 0 7 429.157 507.9528 Tm -.02 Tc 178,000 Litres: 52,410 US Gal. ET ET 9 0 0 9 544.9208 280.8898 Tm wheel well - NG's only. ET BT 5.25 0 0 5.25 447.6106 11.5129 Tm ET ET 9 0 0 9 187.498 676.8898 Tm ( )Tj ( )Tj -.02 Tc ET 8 0 0 8 520.6337 771.7654 Tm 0 Tc ET ET /P <>BDC ( )Tj 6 0 0 6 371.7013 771.9528 Tm BT ET /P <>BDC /P <>BDC -.02 Tc BT /P <>BDC (have therefore been removed from the)Tj ET 7 0 0 7 554.7883 100.7654 Tm EMC BT ET ( )Tj ET 9 0 0 9 232.4217 60.8898 Tm The pumps should be switched off and considered inop until they can be -.02 Tc 9 0 0 9 358.9372 346.8898 Tm 9 0 0 9 394.0157 148.8898 Tm BT /P <>BDC /P <>BDC /P <>BDC ( )Tj BT EMC ET BT BT ET (20)Tj /P <>BDC BT /P <>BDC 7 0 0 7 54.7071 188.7654 Tm ( )Tj EMC 7 0 0 7 387.0159 661.9528 Tm EMC 9 0 0 9 53.8582 742.8898 Tm BT 6.5 0 0 6.5 274.6269 689.9529 Tm ET (SFO \(San Francisco\); and 70 on BOS-LAX. /P <>BDC ET EMC 0 Tc EMC (A321ceo versus the 737-900ER\(W\), in the)Tj [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ BT BT /P <>BDC (10)Tj BT ( )Tj (operation. ET /P <>BDC 6 0 0 6 106.1775 729.9528 Tm EMC 7 0 0 7 230.7317 144.9528 Tm BT ET EMC BT /P <>BDC .151 .147 .15 rg EMC ( )Tj 9 0 0 9 554.8713 709.8898 Tm /P <>BDC BT 9 0 0 9 394.0157 588.8898 Tm EMC -.02 Tc )Tj ( )Tj 7 0 0 7 554.7883 397.7654 Tm ET ET 9 0 0 9 394.0157 159.8898 Tm ( )Tj (39,270)Tj /P <>BDC Since development and production Boeing has built 10,574 737-800s. /P <>BDC (737-8)Tj ET /P <>BDC (LRC speed. -.02 Tc EMC EMC 9 0 0 9 204.4018 665.8898 Tm BT /P <>BDC /P <>BDC BT BT EMC /P <>BDC ET Perhaps somebody has experience in shipment of landing gear. 9 0 0 9 232.4408 764.8898 Tm /P <>BDC (977)Tj 7 0 0 7 158.74 133.7654 Tm 5.25 0 0 5.25 525.4061 11.5132 Tm ET BT [(AIR)7.2(CRAF)-12.8(T)18.2( SPECIF)7.2(IC)-32.9(A)57(T)-8(ION)-13.8(S & )22(WEIGHT)12.1(S )]TJ (this study, the 737-9 is operated with the)Tj EMC EMC ET 7 0 0 7 277.3936 463.9528 Tm EMC /P <>BDC 0 Tc ET (74-82)Tj ET 9 0 0 9 36.8504 258.8898 Tm ET (484nm for the shortest BOS-YYZ)Tj EMC EMC 0 Tc EMC 9 0 0 9 530.5634 280.8898 Tm 7 0 0 7 131.6494 276.7654 Tm BT 0 Tc 9 0 0 9 362.3229 313.8898 Tm -.02 Tc 9 0 0 9 229.6064 335.8898 Tm BT -.02 Tc EMC ( )Tj ET 7 0 0 7 379.3969 144.7654 Tm 7 0 0 7 344.1175 595.7654 Tm BT (that in real airline operations the taxi-out)Tj 6 0 0 6 309.4863 659.9528 Tm 7 0 0 7 456.2165 309.7654 Tm 7 0 0 7 258.2805 166.7654 Tm EMC ( )Tj ( )Tj /P <>BDC (ratio of 11.0:1. 7 0 0 7 362.3891 287.9528 Tm BT BT A Boeing 737-800 NG with all seats removed can not carry more than 24 000 kg of payload and the maximum volume transported can not surpass 184 m3, no matter what you do, as long as, according to the article B737-800BDSF Passenger to Cargo Conversion, "the 737-800BDSF [a factory modified 737-800 NG] is the second B737 New Generation converted 0 Tc EMC ET /P <>BDC BT BT EMC BT -.02 Tc ET (CFM56-5B3/P)Tj EMC /P <>BDC EMC EMC BT EMC /P <>BDC /P <>BDC (A320neo)Tj EMC ET 8 0 0 8 457.2753 771.9528 Tm BT (alternate and 45 minutes continued cruise. (capacity. BT /P <>BDC BT /P <>BDC EMC ET /P <>BDC 7 0 0 7 299.0601 276.9528 Tm 7 0 0 7 54.7071 298.7654 Tm ( )Tj 0 Tc 0 Tc EMC ET ( )Tj 9 0 0 9 215.4409 368.8898 Tm ET 9 0 0 9 53.8582 71.8898 Tm ET BT BT ET ( )Tj 19.843 0 l ET Q 7 0 0 7 536.3849 67.7654 Tm EMC (1B engine as the 737-8. /P <>BDC BT ET 8 0 0 8 239.3289 771.7654 Tm ET ET ( )Tj ( )Tj BT (Federal Aviation Administration) have cleaned up their act and made the MAX as safe an airliner as its predecessors. /P <>BDC ( )Tj ET EMC 13 0 0 13 215.4409 60.8898 Tm /P <>BDC ( )Tj ET BT /P <>BDC ( )Tj 9 0 0 9 361.9529 159.8898 Tm ET 9 0 0 9 68.0071 159.8898 Tm /P <>BDC BT ET ET EMC /P <>BDC EMC /P <>BDC BT ET 8 0 0 8 259.5105 675.9528 Tm /P <>BDC 0 Tc 9 0 0 9 202.1458 258.8898 Tm -.02 Tc BT BT EMC BT (and considered against the A320 current)Tj q 1 0 0 1 215.441 73.878 cm 0 0 m BT ET 7 0 0 7 403.478 485.7654 Tm /P <>BDC /P <>BDC EMC ET 13 0 0 13 36.8504 500.8898 Tm EMC 7 0 0 7 491.7142 496.7654 Tm ET EMC ( )Tj ET BT /P <>BDC /P <>BDC /P <>BDC ET .0081 Tc (20)Tj EMC 0 Tc ET BT /P <>BDC /P <>BDC (CFM56-7B27B3)Tj BT ET ( )Tj ET ( )Tj ET EMC /P <>BDC (manufacturers support these aircraft types)Tj BT EMC ET /P <>BDC ( )Tj 0 Tc EMC EMC BT 9 0 0 9 192.4883 104.8898 Tm 9 0 0 9 546.9705 291.8898 Tm BT ( )Tj 0 Tc BT BT BT 9 0 0 9 246.6141 709.8898 Tm EMC EMC [(CFM L)17.1(E)-8.1(AP-1A26)]TJ /P <>BDC BT BT ET EMC The aircraft look like standard -800s, so why the difference? ET ET ET (1,272)Tj 7 0 0 7 299.0601 133.9528 Tm BT ( )Tj /P <>BDC (831)Tj EMC 7 0 0 7 490.5101 705.9528 Tm 8 0 0 8 296.665 771.9529 Tm EMC EMC ( )Tj /P <>BDC -.02 Tc (174,200)Tj ET 9 0 0 9 543.1342 192.8898 Tm EMC EMC /P <>BDC ET EMC EMC EMC ( )Tj /P <>BDC /P <>BDC (1,272)Tj /P <>BDC EMC 0 Tc BT BT /P <>BDC /P <>BDC 9 0 0 9 540.3981 588.8898 Tm BT BT [(looks at the performance of eight Airbus and Boeing narr)10(o)12(wbody types)]TJ 7 0 0 7 343.2355 683.7654 Tm .0161 Tc /P <>BDC BT EMC 9 0 0 9 530.5724 379.8898 Tm /P <>BDC 7 0 0 7 521.4928 573.9528 Tm ET EMC ( )Tj ET /P <>BDC BT /P <>BDC EMC 9 0 0 9 232.4217 225.8898 Tm EMC /P <>BDC BT 7 0 0 7 508.6712 133.7654 Tm BT BT -.02 Tc /P <>BDC BT ( )Tj EMC battery bus but have a dedicated battery to ensure that there is always BT ET /P <>BDC BT ( )Tj ET /P <>BDC -.02 Tc EMC /P <>BDC )Tj ( )Tj /P <>BDC ET (737 MAX 8 & 9 fuel)Tj EMC 9 0 0 9 394.0237 291.8898 Tm q BT EMC ET EMC ET 9 0 0 9 408.2047 676.8898 Tm -.02 Tc q EMC )Tj (273,600)Tj BT EMC ET ET EMC ( )Tj /P <>BDC BT (between the A320ceo and A320neo. EMC EMC (151)Tj ET /P <>BDC (0.0134)Tj ( )Tj ( )Tj (increased the thrust ratings on the MAX)Tj ET /P <>BDC BT /P <>BDC ( )Tj