(0.0146)Tj air speed, altitude, and similar flight parameters were made available from BT ET ET /P <>BDC BT ET /P <>BDC EMC 0 Tc 9 0 0 9 68.0314 258.8898 Tm 9 0 0 9 215.4313 269.8898 Tm EMC 7 0 0 7 258.2805 386.7654 Tm EMC 9 0 0 9 542.2986 192.8898 Tm ET ( )Tj EMC EMC ( )Tj BT EMC /P <>BDC BT BT sectors to ensure an even fuel balance. 0 Tc /P <>BDC EMC )Tj 8 0 0 8 365.7704 675.9528 Tm /P <>BDC q 1 0 0 1 215.433 150.878 cm 0 0 m BT EMC EMC Airbus A330 Assembly A story of collaboration between nations. ( )Tj Therefore to study)Tj 7 0 0 7 113.1366 221.9528 Tm ET /P <>BDC 7 0 0 7 141.7322 474.9528 Tm /P <>BDC In one insistence a 737-800 on a route from Istanbul crashing in a field near the Polderbaan. ET ET ET EMC EMC 0 Tc EMC 6.5 0 0 6.5 552.6508 565.9529 Tm 0 Tc EMC EMC EMC /P <>BDC EMC EMC ET 7 0 0 7 440.3636 540.9528 Tm ET /P <>BDC ET EMC ( )Tj EMC BT ET (this evaluation are all in the same weight)Tj 9 0 0 9 215.433 104.8898 Tm /P <>BDC 8 0 0 8 543.5282 797.8898 Tm 0 Tc /P <>BDC EMC EMC EMC /P <>BDC BT (3,443)Tj 7 0 0 7 518.4953 232.9528 Tm /P <>BDC EMC )Tj 6 0 0 6 277.7064 715.9528 Tm /P <>BDC ET 9 0 0 9 394.0123 335.8898 Tm BT EMC BT 7 0 0 7 99.8582 595.7654 Tm (5,183)Tj EMC Hi Jeffrey, ( )Tj 0 Tc EMC ET /P <>BDC 7 0 0 7 187.0858 331.9528 Tm EMC 9 0 0 9 553.271 434.8898 Tm BT EMC 6.5 0 0 6.5 500.4941 565.9529 Tm ( )Tj EMC /P <>BDC ET ET BT 9 0 0 9 170.752 368.8898 Tm ET (0.0158)Tj 7 0 0 7 241.5317 298.9528 Tm ET ET ET ET (737-9)Tj /Artifact <>BDC EMC ET The)Tj (39,732)Tj /P <>BDC ET -.01 Tc /P <>BDC (average 3.6% less fuel over the 14 sectors)Tj 0 Tc BT 9 0 0 9 206.7178 181.8898 Tm (requirements of the A320neo, it is 1,200lbs)Tj (0.0158)Tj ( )Tj 7 0 0 7 258.2805 144.7654 Tm 7 0 0 7 204.0935 705.7654 Tm ET BT EMC ET EMC /P <>BDC EMC ( )Tj 7 0 0 7 520.6108 738.9528 Tm EMC 7 0 0 7 354.6933 617.7654 Tm EMC /P <>BDC (150)Tj 0 Tc BT /P <>BDC 9 0 0 9 530.5354 665.8898 Tm (23)Tj ET /P <>BDC -.02 Tc 0 Tc BT /P <>BDC 0 Tc BT 7 0 0 7 294.4014 309.7654 Tm (216,240)Tj 0 Tc EMC ET In addition, with many airlines)Tj ( )Tj 515.814 89.864 l BT (0.0120)Tj BT /P <>BDC ET /OC /MC208 BDC /P <>BDC 6 0 0 6 309.5222 701.9528 Tm ( )Tj ET 7 0 0 7 355.3163 144.7654 Tm ( )Tj BT .0161 Tc ET EMC ( )Tj 0 Tc EMC BT EMC (\(see table, this page\))Tj /P <>BDC ( )Tj ( )Tj /P <>BDC /P <>BDC EMC BT )Tj /P <>BDC 9 0 0 9 184.2244 203.8898 Tm EMC -.02 Tc ET /P <>BDC ET ( )Tj (Top), Specification Table Boeing 737 Next Gen and Max.(Top). BT ( )Tj ET 7 0 0 7 387.0932 166.9528 Tm ( )Tj ET ET /P <>BDC (the longest sector BOS-SFO. BT BT ( )Tj /P <>BDC ( )Tj EMC EMC 7 0 0 7 403.478 617.7654 Tm /P <>BDC ET BT 9 0 0 9 187.2574 302.8898 Tm (0.0117)Tj EMC EMC ET (covers a 3,300-3,400nm range with a full)Tj /P <>BDC /P <>BDC /P <>BDC /P <>BDC 7 0 0 7 337.6855 408.9528 Tm [(E)-7.8(P)16.1(T)9(E)-13.9(MBE)-16.9(R)]TJ 9 0 0 9 77.618 82.8898 Tm ET /P <>BDC 7 0 0 7 148.0554 11.5132 Tm -.02 Tc 8 0 0 8 394.0157 775.8898 Tm (737-9)Tj ET BT ( )Tj 9 0 0 9 394.0123 368.8898 Tm 6.5 0 0 6.5 448.257 598.9529 Tm 6.5 0 0 6.5 477.8064 676.9529 Tm EMC ( )Tj ET ET BT EMC /P <>BDC ( )Tj ET 19.848 0 l 7 0 0 7 535.5029 705.7654 Tm EMC -.02 Tc ( )Tj -.02 Tc 7 0 0 7 554.7883 100.7654 Tm -.02 Tc defuelling or transferring fuel, if quantity is below 453kgs. 7 0 0 7 258.2805 584.7654 Tm BT EMC 9 0 0 9 199.3017 401.8898 Tm ( )Tj (CFM56-7B27B3)Tj BT /P <>BDC EMC 7 0 0 7 338.5674 122.9528 Tm /P <>BDC EMC /P <>BDC ( )Tj BT ( )Tj ( )Tj ET f FQIS accuracy: +/- 1.0% overall 9 0 0 9 411.0181 357.8898 Tm .661 .752 .896 rg 0 Tc /P <>BDC -.02 Tc [(737-900E)-33(R)]TJ -.02 Tc ET BT ET /P <>BDC ET 6 0 0 6 277.7064 757.9528 Tm BT BT (The three main operational costs for)Tj ( )Tj ET /P <>BDC ET ET /P <>BDC /P <>BDC /P <>BDC ET 6 0 0 6 215.373 715.9528 Tm document.getElementById( "ak_js_1" ).setAttribute( "value", ( new Date() ).getTime() ); Airbus A320 Introduction The very popular short haul airliner. ET -.01 Tc ET /P <>BDC 9 0 0 9 36.8504 49.8898 Tm (31,416)Tj 7 0 0 7 338.5674 584.9528 Tm (a different trend for the two)Tj EMC /P <>BDC BT 7 0 0 7 404.101 342.7654 Tm ET BT ET 9 0 0 9 541.5243 720.8898 Tm EMC ET BT 7 0 0 7 187.0858 166.9528 Tm ( )Tj /P <>BDC BT It sports its powerful crew and passenger carrying abilities elegantly as it takes flight. /P <>BDC especially during start. (483)Tj /P <>BDC 9 0 0 9 183.0113 214.8898 Tm 9 0 0 9 411.0234 709.8898 Tm ( )Tj (977)Tj (31,416)Tj 0 Tc ( )Tj BT 7 0 0 7 363.2711 232.9528 Tm ( )Tj (standard passenger weight of 231lbs that)Tj /P <>BDC ( )Tj -.01 Tc BT BT EMC 9 0 0 9 394.0315 621.8898 Tm /P <>BDC BT [(differ)10(ences in fuel burn betw)6.1(een the types ar)10(e examined by Ian Britchfor)7.1(d. )]TJ BT 6.5 0 0 6.5 191.8316 637.9529 Tm /P <>BDC /P <>BDC -.02 Tc EMC EMC (achieved more than 6,000 orders for the)Tj /P <>BDC /P <>BDC ( )Tj -.02 Tc ( )Tj ET /P <>BDC 7 0 0 7 403.478 122.7654 Tm BT BT 7 0 0 7 520.6108 562.9528 Tm EMC 9 0 0 9 369.892 412.8898 Tm /P <>BDC 9 0 0 9 190.2832 49.8898 Tm 7 0 0 7 473.4744 518.9528 Tm BT /P <>BDC BT ( )Tj BT ET 7 0 0 7 518.4953 133.9528 Tm ( )Tj 7 0 0 7 101.0963 210.9528 Tm ( )Tj ( )Tj (CFM56-7B27B3)Tj 0 Tc EMC BT 7 0 0 7 314.6398 705.7654 Tm ( )Tj EMC ET ( )Tj BT 7 0 0 7 294.4014 628.7654 Tm /P <>BDC BT 8 0 0 8 275.7172 760.7654 Tm EMC 9 0 0 9 191.0032 225.8898 Tm ( )Tj BT ( )Tj EMC ET (The alternate airports were selected based)Tj /P <>BDC ( )Tj EMC point +3C, whichever is EMC 9 0 0 9 374.4497 214.8898 Tm EMC 10 0 0 10 425.05 814.1973 Tm BT ( )Tj ( )Tj /P <>BDC ET 9 0 0 9 53.8582 753.8898 Tm (MAX family. EMC /P <>BDC EMC ET ET 6 0 0 6 381.7993 715.9528 Tm 0 Tc EMC EMC -.02 Tc ( )Tj (\(see)Tj /P <>BDC /P <>BDC 7 0 0 7 279.1575 419.9528 Tm EMC BT /P <>BDC BT /P <>BDC EMC EMC -.02 Tc 8 0 0 8 43.6039 703.9528 Tm (seat capacity, with no additional cargo. 0 Tc BT /P <>BDC ( )Tj 7 0 0 7 141.7322 672.9528 Tm /P <>BDC ET ET 6 0 0 6 496.3652 743.9528 Tm BT ET 7 0 0 7 315.5217 617.7654 Tm BT (The 737-9 has an 11.2% to 12.7%)Tj ET (aircraft having to operate at the non-)Tj /P <>BDC 7 0 0 7 439.7405 705.9528 Tm A fuel sampling and testing kit is kept on the flight deck of all BT ( )Tj EMC ( )Tj ET /P <>BDC /P <>BDC EMC /GS2 gs /P <>BDC BT /P <>BDC (A320ceo)Tj /P <>BDC EMC BT EMC /P <>BDC /P <>BDC /P <>BDC BT EMC ET BT /F7 1 Tf -.02 Tc 7 0 0 7 247.7395 694.7654 Tm EMC EMC ET BT 9 0 0 9 394.0237 280.8898 Tm EMC BT (LEAP-1B engine. ( )Tj BT BT BT 0 Tc (56,901)Tj BT (same cost index, and the method that each)Tj ET EMC /P <>BDC /P <>BDC ET ET ET /P <>BDC /P <>BDC (26)Tj (the two scenarios are detailed )Tj ET ET /P <>BDC /P <>BDC .41 .161 .508 rg /P <>BDC BT /P <>BDC EMC EMC EMC ET BT ( )Tj 6 0 0 6 396.1516 743.9528 Tm ( )Tj 7 0 0 7 316.0679 265.7654 Tm /P <>BDC BT BT Airbus seals the deal to reinvigorate the QANTAS Fleet. /P <>BDC 9 0 0 9 194.9803 478.8898 Tm EMC ET ET BT EMC (737-9)Tj EMC 9 0 0 9 232.4217 291.8898 Tm EMC /P <>BDC EMC ET 7 0 0 7 554.7883 276.7654 Tm EMC -.02 Tc EMC BT ( )Tj 6.5 0 0 6.5 429.0755 637.9529 Tm BT ET ( )Tj /P <>BDC (method of operation that balances the cost)Tj ET EMC EMC BT /P <>BDC EMC ET -.01 Tc 0 Tc BT ( )Tj BT /P <>BDC BT ( )Tj ET Boeing 777 Specs, what makes this giant twin work? BT ( )Tj .151 .147 .15 RG /P <>BDC BT /P <>BDC ET [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ ( )Tj BT 8 0 0 8 189.0627 717.9528 Tm ET ( )Tj /F6 1 Tf (177)Tj Compared with the -400 the -800 is 3.02m (9ft 9in) longer, taking typical two class seating from 146 to 162, while range is significantly increased. BT /P <>BDC BT 7 0 0 7 457.0984 67.7654 Tm 7 0 0 7 539.9176 11.5129 Tm EMC EMC ET 7 0 0 7 537.7804 111.9528 Tm ET EMC /P <>BDC 0 Tc ET ET ET BT BT 7 0 0 7 230.7317 562.9528 Tm 0 Tc /P <>BDC /P <>BDC [(CFM L)17.1(E)-8.1(AP-1A26)]TJ 6.5 0 0 6.5 233.8677 611.9529 Tm /P <>BDC f /P <>BDC EMC EMC /P <>BDC ET ET (burn and operating)Tj (36,960)Tj BT EMC BT EMC pumps on the forward wall of the wheel well on the NG's, since the forward wall ( )Tj BT ET BT EMC 9 0 0 9 525.9757 60.8898 Tm ET ET 9 0 0 9 380.2477 247.8898 Tm BT /P <>BDC ET ( )Tj -.02 Tc ET ( )Tj /P <>BDC EMC ET 0 Tc EMC BT ET EMC (0.0157)Tj 9 0 0 9 210.9209 104.8898 Tm .014984 841.89 609.45 -841.89 re 9 0 0 9 232.4217 126.8898 Tm /P <>BDC .151 .147 .15 rg -.02 Tc [(BOS-SE)-13.9(A)]TJ 8 0 0 8 296.665 771.9529 Tm BT /P <>BDC EMC -.02 Tc ET 0 Tc /P <>BDC /P <>BDC .023 .567 .626 rg 7 0 0 7 355.3163 243.7654 Tm ET 7 0 0 7 354.6933 518.7654 Tm /GS1 gs -.02 Tc /P <>BDC ( )Tj BT -.02 Tc /P <>BDC /P <>BDC /P <>BDC /P <>BDC /P <>BDC 9 0 0 9 541.1655 478.8898 Tm support combustion. EMC EMC EMC /P <>BDC ( )Tj ET /P <>BDC ET (1,059)Tj (170)Tj ET BT EMC ET /P <>BDC ET /P <>BDC BT /P <>BDC EMC /P <>BDC ET /P <>BDC (37,653)Tj 7 0 0 7 446.5009 716.7654 Tm /P <>BDC (CFM56-5B4/P)Tj 9 0 0 9 535.2051 500.8898 Tm ET 9 0 0 9 51.0236 335.8898 Tm 7 0 0 7 508.2252 11.5129 Tm -.02 Tc BT -.02 Tc BT (off weight \(MTOW\) of 171,961lbs, a)Tj 7 0 0 7 404.101 89.7654 Tm 9 0 0 9 541.0135 159.8898 Tm /P <>BDC EMC ET ET EMC /P <>BDC BT ET EMC 9 0 0 9 212.1598 302.8898 Tm ET 7 0 0 7 82.2047 540.9528 Tm /P <>BDC /OC /MC1320 BDC /P <>BDC /P <>BDC BT 8 0 0 8 259.5105 675.9528 Tm 7 0 0 7 279.1575 397.9528 Tm ET (- USG)Tj /P <>BDC BT EMC 0 Tc 7 0 0 7 403.478 628.7654 Tm 0 Tc EMC 7 0 0 7 118.104 364.7654 Tm 0 Tc BT 9 0 0 9 569.5997 566.8898 Tm EMC /P <>BDC (737-800W)Tj ( )Tj EMC ( )Tj ET -.02 Tc 7 0 0 7 316.0679 177.7654 Tm 7 0 0 7 355.5753 595.7654 Tm ( )Tj /P <>BDC 8 0 0 8 394.0237 38.8898 Tm /P <>BDC 9 0 0 9 188.8887 60.8898 Tm ET ET ( )Tj 10 0 0 10 417.91 814.1973 Tm EMC 7 0 0 7 258.2805 540.7654 Tm ET /P <>BDC 0 Tc ET EMC BT (seat layout of 16/18/126 as the A320ceo,)Tj /P <>BDC /P <>BDC /P <>BDC ET (170)Tj BT ET (CFM56-5B3/P)Tj After BT BT ( )Tj .7 -.5345 .9114 -1.2305 y 7 0 0 7 439.7405 716.9528 Tm ( )Tj ( )Tj 7 0 0 7 475.2383 639.9528 Tm 6.5 0 0 6.5 426.4819 702.9529 Tm ( )Tj ET 6 0 0 6 371.7013 771.9528 Tm ( 2021)Tj ET ET ( )Tj EMC 9 0 0 9 53.8582 214.8898 Tm ET (4,158)Tj ( )Tj ET ET 9 0 0 9 394.0123 214.8898 Tm -.02 Tc ET EMC /P <>BDC (reducing their in-flight service offering, this)Tj ET 0 Tc ET 0 Tc 9 0 0 9 215.4409 489.8898 Tm ET /P <>BDC BT /P <>BDC 9 0 0 9 36.8504 434.8898 Tm 6.5 0 0 6.5 297.8076 558.9529 Tm /P <>BDC 9 0 0 9 528.0825 368.8898 Tm ET BT It has a maximum takeoff weight of about 80,000 kg (175,000 lbs). BT 7 0 0 7 355.3163 89.7654 Tm BT 9 0 0 9 215.433 434.8898 Tm /P <>BDC 7 0 0 7 338.6433 67.7654 Tm ( )Tj 7 0 0 7 99.8582 89.7654 Tm ( )Tj -.02 Tc ET ET EMC 0 Tc EMC /P <>BDC EMC 9 0 0 9 394.0157 511.8898 Tm ET 0 Tc 7 0 0 7 279.1575 595.9528 Tm 7 0 0 7 37.0536 606.9528 Tm EMC (346,583)Tj 7 0 0 7 554.7883 430.7654 Tm (68.3 inches and a bypass ratio of up to)Tj -.02 Tc 7 0 0 7 158.74 507.7654 Tm 0 Tc EMC EMC 7 0 0 7 82.8504 386.9528 Tm EMC /P <>BDC 8 0 0 8 365.7704 591.9528 Tm BT EMC /P <>BDC EMC EMC EMC EMC -.02 Tc 9 0 0 9 394.0315 412.8898 Tm /P <>BDC 9 0 0 9 394.0315 456.8898 Tm EMC ( )Tj ET ET BT BT EMC /P <>BDC /P <>BDC ( )Tj /P <>BDC /P <>BDC EMC ET ET -.01 Tc EMC /P <>BDC 9 0 0 9 388.6428 357.8898 Tm 7 0 0 7 258.2805 188.7654 Tm 7 0 0 7 337.6855 518.9528 Tm EMC EMC ( )Tj -.02 Tc ( )Tj 9 0 0 9 394.0123 478.8898 Tm ( )Tj ET -.02 Tc ( )Tj 0 Tc (0.0111)Tj EMC 0 Tc (on distance from the destination airport)Tj 9 0 0 9 53.8338 115.8898 Tm ( )Tj ET EMC /P <>BDC ET 7 0 0 7 507.7893 628.7654 Tm [(OM)8(M)-13(E)-25(R)7(C)8(E)]TJ BT ET ET (higher OEW. .023 .567 .626 rg ET ( )Tj /P <>BDC /F6 1 Tf EMC ET 6.5 0 0 6.5 521.8278 742.9529 Tm 7 0 0 7 403.478 364.7654 Tm (737-9)Tj EMC ET EMC -.02 Tc BT ET 7 0 0 7 258.2805 111.7654 Tm (0.0119)Tj <> ET EMC /P <>BDC EMC BT ET EMC BT ( )Tj ( )Tj (passengers and the 737-900ER\(W\) 152)Tj (A320ceo)Tj ET EMC 7 0 0 7 445.619 496.7654 Tm EMC ( )Tj 7 0 0 7 37.0536 518.9528 Tm EMC 9 0 0 9 53.8582 203.8898 Tm ET EMC BT EMC Inside this highly popular City Jet. ET /P <>BDC EMC /P <>BDC /P <>BDC EMC BT /P <>BDC BT /P <>BDC ( )Tj EMC ET /P <>BDC EMC If AC power is available, select ET /P <>BDC ET 8 0 0 8 225.1837 577.9528 Tm /P <>BDC Q /P <>BDC [(A3)24.9(21neo v)12.9(ersus 7)-33(3)8.1(7-9 )]TJ ET 10 0 0 10 37.304 794.2914 Tm /P <>BDC ET EMC (packages, it will be interesting to re-)Tj 7 0 0 7 492.5963 716.7654 Tm 6 0 0 6 191.3929 771.9528 Tm /P <>BDC )Tj EMC 7 0 0 7 508.6712 232.7654 Tm /P <>BDC (408)Tj ET 0 Tc ET 0 Tc ET /P <>BDC ET 7 0 0 7 355.3163 320.7654 Tm /P <>BDC ET 9 0 0 9 394.0157 522.8898 Tm BT 7 0 0 7 457.0984 331.7654 Tm EMC 9 0 0 9 270.2513 313.8898 Tm 7 0 0 7 59.2108 11.5129 Tm -.02 Tc ET 9 0 0 9 408.1889 533.8898 Tm /P <>BDC 737-300/-400/-500, (379)Tj ET /P <>BDC ET EMC /P <>BDC EMC ET ET ET ET 9 0 0 9 186.1613 49.8898 Tm -.02 Tc ( )Tj /P <>BDC ET /P <>BDC /P <>BDC 7 0 0 7 387.0932 375.9528 Tm BT 0 Tc EMC 9 0 0 9 548.3564 225.8898 Tm 9 0 0 9 345.4916 412.8898 Tm EMC /P <>BDC (112)Tj ( )Tj ET -.02 Tc /P <>BDC This will)Tj EMC EMC 5.25 0 0 5.25 64.5461 11.5129 Tm /P <>BDC EMC EMC BT 0 Tc ( )Tj ( )Tj (409,650)Tj ( )Tj 9 0 0 9 194.7833 236.8898 Tm ET /P <>BDC 9 0 0 9 137.7566 49.8898 Tm /P <>BDC /P <>BDC EMC 3 i ET /P <>BDC ET EMC -.02 Tc BT ET 518.735 0 l EMC BT /P <>BDC -.02 Tc BT EMC -.02 Tc 0 Tc EMC /P <>BDC (original equipment manufacturer \(OEM\))Tj ET EMC 9 0 0 9 537.7245 676.8898 Tm 9 0 0 9 394.0315 137.8898 Tm /P <>BDC ( )Tj 9 0 0 9 566.9717 236.8898 Tm EMC 9 0 0 9 200.7278 170.8898 Tm ( )Tj ( )Tj EMC 7 0 0 7 82.8504 375.9528 Tm EMC /P <>BDC /P <>BDC 6.5 0 0 6.5 398.3298 650.9529 Tm )Tj /P <>BDC EMC ET /P <>BDC EMC EMC ET (A321ceo)Tj BT 7 0 0 7 258.2805 683.7654 Tm EMC BT 7 0 0 7 230.7317 397.9528 Tm EMC -.02 Tc /P <>BDC -.02 Tc ET /P <>BDC ( )Tj [(737-900E)-33(R)]TJ 7 0 0 7 113.1366 518.9528 Tm EMC aircraft ET /P <>BDC ET /P <>BDC ET 7 0 0 7 490.5101 529.9528 Tm 7 0 0 7 316.0679 331.7654 Tm ET ET 7 0 0 7 518.4953 441.9528 Tm /P <>BDC EMC EMC EMC 9 0 0 9 36.8504 49.8898 Tm ( )Tj 9 0 0 9 36.8504 423.8898 Tm ET ET 0 Tc (types over a wide range of mission lengths)Tj /P <>BDC ET /P <>BDC EMC (and considered against the A320 current)Tj BT ( )Tj BT /P <>BDC - Non Perele - News Online, Hi, EMC BT 178,000 Litres: 52,410 US Gal. ET EMC EMC (CFM56-5B4/P)Tj /P <>BDC EMC ( )Tj BT /P <>BDC EMC EMC EMC Maybe there is someone out there who can give you a better answer. 0 Tc /P <>BDC ( )Tj EMC ( )Tj ET ET EMC BT -.02 Tc ET ET /P <>BDC 7 0 0 7 355.3163 78.7654 Tm 9 0 0 9 394.0315 731.8898 Tm EMC ET Since no two)Tj 7 0 0 7 258.2805 727.7654 Tm /P <>BDC -.01 Tc EMC /P <>BDC BT 0 Tc /P <>BDC Regarding winglets, I think Simple Flying explains it well. 7 0 0 7 297.632 485.9528 Tm /P <>BDC ET 7 0 0 7 326.2278 474.9528 Tm /TT2 1 Tf BT EMC /P <>BDC /P <>BDC 9 0 0 9 541.0405 621.8898 Tm EMC ( )Tj EMC ( )Tj BT ET EMC BT /P <>BDC )Tj /P <>BDC ET BT BT /P <>BDC 10 0 0 10 420.16 814.1973 Tm EMC ET EMC 7 0 0 7 491.7142 133.7654 Tm EMC /P <>BDC (payload is carried. 7 0 0 7 338.3085 265.9528 Tm ( )Tj /P <>BDC /P <>BDC (35,112)Tj /P <>BDC /GS1 gs BT (283)Tj /P <>BDC 0 Tc EMC Centre tank pumps should not be 0 Tc /P <>BDC (fuel capacity of 6,303USG )Tj 161.566 0 l BT /P <>BDC ET 6.5 0 0 6.5 324.4345 663.9529 Tm (0.0134)Tj EMC /P <>BDC W* n ET BT ( )Tj EMC (176)Tj ( )Tj ET EMC /P <>BDC BT 7 0 0 7 326.2278 529.9528 Tm EMC 7 0 0 7 456.2165 144.7654 Tm ET 9 0 0 9 367.9911 71.8898 Tm 9 0 0 9 73.1083 511.8898 Tm EMC ( )Tj ET 161.574 0 l BT ET EMC (376)Tj ( )Tj /P <>BDC The 737-800 project began in 1994, with Hapag-Lloyd Airlines ofGermany placing the first order for this aircraft. 9 0 0 9 36.8504 258.8898 Tm -.02 Tc (and in fuel burn per ASM. EMC /F4 1 Tf EMC 0 Tc BT /P <>BDC EMC BT /P <>BDC -.02 Tc BT ( )Tj ET ET BT ET /P <>BDC /P <>BDC EMC EMC Jump to Specification Table Boeing 737 Next Gen and Max. (1,824)Tj BT EMC (same passenger payload. ET BT EMC ET EMC BT (163)Tj EMC Cheers Peter. /P <>BDC q 1 0 0 1 53.901 797.54 cm 0 0 m (variant offers 26,000lbs of thrust, with a)Tj EMC ET BT /P <>BDC BT 7 0 0 7 445.619 628.7654 Tm .151 .147 .15 rg /P <>BDC EMC BT -.005 Tc BT ET (900ER\(W\) is limited to 165 passengers on)Tj ET ET BT EMC EMC ET 0 Tc Other data such as fuel load, BT 0 Tc ET (720)Tj 7 0 0 7 490.8321 540.7654 Tm ET 9 0 0 9 215.4313 335.8898 Tm ET /P <>BDC BT ( )Tj EMC /P <>BDC EMC 7 0 0 7 387.0932 298.9528 Tm to maintain C of G balance. 0 Tc ET ET 9 0 0 9 198.5183 445.8898 Tm EMC /P <>BDC 6.5 0 0 6.5 530.1996 735.9529 Tm 7 0 0 7 445.7203 11.5129 Tm ( )Tj -.02 Tc ET /P <>BDC BT 0 Tc EMC ( )Tj ET EMC /P <>BDC /P <>BDC ( )Tj BT EMC ( )Tj ET 7 0 0 7 469.2222 11.5129 Tm ( )Tj ( )Tj EMC ET BT ET BT (and bypass ratio of 12.5:1 as the A320neo;)Tj /P <>BDC ( )Tj ET BT ( )Tj ET 0 Tc ET EMC /P <>BDC Engine size /P <>BDC EMC 7 0 0 7 199.5784 639.7654 Tm BT (CFM56-7B27B3)Tj Fuel Capacity 6,875 U.S. gal (26,020 L) Seat Pitch: 40 inches Premier World 32 inches Economy Max. ET 7 0 0 7 473.8245 386.9528 Tm BT ET ET /P <>BDC 7 0 0 7 230.7317 441.9528 Tm 9 0 0 9 394.0123 225.8898 Tm EMC BT BT EMC BT /P <>BDC EMC <> /P <>BDC 7 0 0 7 539.8962 639.9528 Tm EMC ( )Tj 0 Tc EMC EMC BT 7 0 0 7 241.5317 309.9528 Tm BT /P <>BDC ( )Tj EMC BT (136)Tj /P <>BDC 9 0 0 9 394.0157 247.8898 Tm EMC EMC BT ET ET BT 5.25 0 0 5.25 55.7484 11.5132 Tm 7 0 0 7 277.3936 474.9528 Tm BT BT ET EMC 10 0 0 10 47.8705 814.1973 Tm - Non Perele - News Online, Council Post: Aviation Is The Driving Force Of Hydrogen | QNewsHub, When will the Boeing 737 MAX fly again? /P <>BDC BT 9 0 0 9 394.0157 335.8898 Tm ET EMC BT ( )Tj ( )Tj 7 0 0 7 242.1547 78.9528 Tm 9 0 0 9 53.8578 93.8898 Tm ET ET EMC BT ( )Tj EMC 7 0 0 7 387.0159 529.9528 Tm 7 0 0 7 337.6855 595.9528 Tm BT 9 0 0 9 36.8583 456.8898 Tm BT EMC -.02 Tc /P <>BDC -.02 Tc BT BT /P <>BDC BT BT EMC 9 0 0 9 53.8582 324.8898 Tm EMC ET 0 Tc ET ( )Tj BT BT /P <>BDC ET EMC 7 0 0 7 158.74 210.7654 Tm /P <>BDC Calibration -.02 Tc /P <>BDC /P <>BDC -.02 Tc ET EMC EMC ( )Tj ET BT 7 0 0 7 99.8582 144.7654 Tm /P <>BDC ET -.02 Tc 9 0 0 9 196.1514 390.8898 Tm BT /P <>BDC EMC ET (The later generation aircraft are set to)Tj ET EMC /P <>BDC BT 8 0 0 8 239.3289 771.7654 Tm /P <>BDC ET BT /P <>BDC /P <>BDC EMC 7 0 0 7 520.6108 496.9528 Tm /P <>BDC ET BT /P <>BDC 0 Tc 9 0 0 9 408.2047 489.8898 Tm The fuel tank was instrumented with gas sample tubing and thermocouples to EMC /P <>BDC /P <>BDC ( )Tj (performance of the two reduces to 0.8%)Tj ( )Tj /P <>BDC EMC /P <>BDC /P <>BDC EMC ET /P <>BDC 7 0 0 7 37.0536 661.9528 Tm /OC /MC835 BDC BT BT BT 6 0 0 6 184.0127 771.9528 Tm /P <>BDC BT /P <>BDC BT On the Digital Sunburst fuel gauges, pressing the "Qty test" button will /P <>BDC 9 0 0 9 215.4409 258.8898 Tm BT BT BT /P <>BDC BT 7 0 0 7 444.737 100.7654 Tm ET ( )Tj /P <>BDC You are right, it does look very much like a 737-800. 9 0 0 9 212.5107 313.8898 Tm BT 6.5 0 0 6.5 176.1172 585.9529 Tm BT EMC EMC /P <>BDC ( )Tj ET 7 0 0 7 321.6356 210.9528 Tm 9 0 0 9 229.6045 390.8898 Tm /P <>BDC /P <>BDC BT 6.5 0 0 6.5 375.6529 689.9529 Tm BT /P <>BDC BT 0 Tc EMC ( )Tj ET 7 0 0 7 54.7071 287.7654 Tm ET /P <>BDC ET 9 0 0 9 529.6118 302.8898 Tm 6 0 0 6 89.371 673.9528 Tm BT 6 0 0 6 527.6392 715.9528 Tm BT (26,000lbs thrust on the A320neo powered)Tj EMC /P <>BDC ET ET (576)Tj ET EMC /P <>BDC EMC 6 0 0 6 61.517 757.9528 Tm BT -.02 Tc /P <>BDC ET ET /P <>BDC /P <>BDC 7 0 0 7 379.3969 122.7654 Tm ( )Tj 7 0 0 7 507.7893 419.7654 Tm -.02 Tc EMC (9.0:1)Tj EMC EMC EMC 7 0 0 7 54.7071 111.7654 Tm 7 0 0 7 381.1608 573.7654 Tm /P <>BDC BT BT /P <>BDC ( )Tj /P <>BDC ( )Tj -.01 Tc /P <>BDC -.02 Tc BT The fwd and aft tanks are switched off when the EMC EMC ET ET 6.5 0 0 6.5 328.6662 585.9529 Tm BT BT ET BT 9 0 0 9 411.0097 280.8898 Tm 9 0 0 9 68.0071 577.8898 Tm (170)Tj /P <>BDC ( )Tj ET 7 0 0 7 241.5317 485.9528 Tm EMC -.01 Tc /P <>BDC /P <>BDC /P <>BDC ( )Tj BT EMC (A320neos 7,000lbs higher MTOW. ET 0 Tc /P <>BDC /P <>BDC -.01 Tc /P <>BDC BT BT 9 0 0 9 425.183 401.8898 Tm EMC /P <>BDC EMC EMC BT -.02 Tc 0 Tc 0 Tc 7 0 0 7 535.5029 375.7654 Tm BT -.02 Tc /P <>BDC EMC ( )Tj /P <>BDC BT BT ET (10)Tj /P <>BDC ET ( )Tj (162,701)Tj ET EMC BT EMC (31,416)Tj 9 0 0 9 53.8578 137.8898 Tm ET EMC 13 0 0 13 36.8504 456.8898 Tm (might have over an older aircraft would)Tj -.01 Tc (427,890)Tj EMC (2.31 cents per ASM. BT 9 0 0 9 68.031 71.8898 Tm 6.5 0 0 6.5 549.8557 585.9529 Tm (171,961)Tj EMC -.02 Tc /P <>BDC ( )Tj /P <>BDC ( )Tj BT /P <>BDC (163,900)Tj EMC 9 0 0 9 552.5493 357.8898 Tm ( )Tj ET -.02 Tc 6 0 0 6 554.8917 743.9528 Tm ET 9 0 0 9 190.8846 379.8898 Tm 6.5 0 0 6.5 172.7047 598.9529 Tm /P <>BDC BT /P <>BDC ET BT -.02 Tc overboard. (. ET BT 7 0 0 7 43.6039 540.9528 Tm ( )Tj /P <>BDC EMC EMC EMC 9 0 0 9 198.0774 280.8898 Tm BT 9 0 0 9 201.162 500.8898 Tm 7 0 0 7 315.1859 89.7654 Tm (choice of engine variant. /P <>BDC ET /P <>BDC EMC 9 0 0 9 36.8504 390.8898 Tm BT EMC EMC ( )Tj As you can appreciate, the cockpit of any aircraft is always a non-standard shape. /P <>BDC /P <>BDC 7 0 0 7 124.1242 199.7654 Tm (35,112)Tj ET ET 7 0 0 7 320.7537 78.9528 Tm BT ET (420)Tj (A321neo)Tj 505.325 82.247 l The weight configuration used)Tj (the A320ceo. EMC BT EMC /P <>BDC BT /P <>BDC BT /GS2 gs BT ( )Tj 13 0 0 13 512.6883 71.8898 Tm ET S BT 7 0 0 7 354.6933 474.7654 Tm -.02 Tc /P <>BDC EMC BT This study uses a)Tj BT -.02 Tc EMC EMC 0 Tc 7 0 0 7 404.3599 661.7654 Tm BT 9 0 0 9 215.4313 302.8898 Tm 7 0 0 7 82.8504 221.9528 Tm 9 0 0 9 53.8578 368.8898 Tm 9 0 0 9 411.0181 49.8898 Tm -.02 Tc /P <>BDC /P <>BDC (34,650)Tj -.01 Tc EMC EMC 9 0 0 9 215.4409 401.8898 Tm 9 0 0 9 332.7796 225.8898 Tm BT -.02 Tc BT BT ET ET ( )Tj 7 0 0 7 354.6933 397.7654 Tm 7 0 0 7 125.6292 232.7654 Tm -.02 Tc ET EMC /P <>BDC ( )Tj EMC /P <>BDC It was demonstrated under /P <>BDC ET /P <>BDC 7 0 0 7 108.6215 166.9528 Tm EMC EMC BT EMC 5 0 0 5 484.5872 11.5129 Tm ET BT 7 0 0 7 321.6356 309.9528 Tm (constraints, the 737 MAX has a smaller)Tj 9 0 0 9 394.0315 588.8898 Tm EMC /P <>BDC /P <>BDC /P <>BDC EMC /P <>BDC (fuel burn than the 737-8.

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