9 0 0 9 373.4379 324.8898 Tm ET ET -.02 Tc EMC BT BT ET 9 0 0 9 531.902 467.8898 Tm BT /P <>BDC EMC ET EMC 6.5 0 0 6.5 499.7986 637.9529 Tm BT ET EMC q EMC /P <>BDC ET 9 0 0 9 553.8705 93.8898 Tm (150)Tj BT /P <>BDC ET EMC 7 0 0 7 158.74 683.7654 Tm EMC /P <>BDC 0 Tc (464,440)Tj BT -.02 Tc ET ( )Tj /P <>BDC EMC (I)Tj 0 Tc /P <>BDC /P <>BDC . EMC ( )Tj BT 6.5 0 0 6.5 382.9199 735.9529 Tm ( )Tj Versions / Variants There are many variants of the 737. 10 0 0 10 422.8 814.1973 Tm 0 Tc /P <>BDC ET /P <>BDC 7 0 0 7 554.7883 100.7654 Tm 6.5 0 0 6.5 346.1424 545.9529 Tm 8 0 0 8 124.845 717.9528 Tm ( )Tj /P <>BDC ET EMC ET /P <>BDC BT BT )Tj BT (fan diameter of 78 inches, and a bypass)Tj EMC ET ET (used is 16/30/114, giving a seat count of)Tj ET ET ET 7 0 0 7 297.632 661.9528 Tm 9 0 0 9 213.1228 368.8898 Tm ( )Tj ( )Tj ET Q /P <>BDC /P <>BDC 7 0 0 7 71.6694 639.9528 Tm EMC /P <>BDC 5.25 0 0 5.25 525.4061 11.5132 Tm 9 0 0 9 215.4409 500.8898 Tm EMC EMC ET (737-9)Tj ET ET 9 0 0 9 229.6064 269.8898 Tm /P <>BDC 9 0 0 9 455.0733 60.8898 Tm (page\))Tj .151 .147 .15 rg /P <>BDC BT ET ET EMC EMC EMC ET ( )Tj EMC ET EMC /P <>BDC The AFM limits are higher, but not normally BT ET 7 0 0 7 439.7405 738.9528 Tm BT EMC EMC ET EMC ET /P <>BDC EMC /OC /MC1956 BDC BT ET ( )Tj /P <>BDC ( )Tj /F7 1 Tf /P <>BDC 0 Tc BT 9 0 0 9 386.9059 280.8898 Tm EMC 0 Tc /P <>BDC ( )Tj 7 0 0 7 554.7883 661.7654 Tm 7 0 0 7 77.36 11.5132 Tm (70)Tj BT BT 137 )Tj ET /F6 1 Tf 0 Tc BT ET BT EMC BT /P <>BDC ET /P <>BDC /P <>BDC 7 0 0 7 82.8504 177.9528 Tm BT (/S)Tj EMC ( )Tj 9 0 0 9 181.0402 335.8898 Tm (158)Tj BT BT 7 0 0 7 554.7883 573.7654 Tm ET What is the mass of the wings and everything attached, except for the engine on the 737-800? EMC EMC BT EMC EMC 13 0 0 13 53.8578 181.8898 Tm /P <>BDC (. ET ET 9 0 0 9 232.4217 269.8898 Tm EMC ( )Tj -.02 Tc ET EMC 7 0 0 7 404.101 232.7654 Tm EMC EMC 7 0 0 7 440.0906 166.9528 Tm (37,653)Tj 6 0 0 6 302.9128 729.9528 Tm EMC )Tj EMC (294)Tj EMC ( )Tj /P <>BDC ET )Tj 8 0 0 8 394.0157 764.8898 Tm 9 0 0 9 346.6898 280.8898 Tm BT ET /P <>BDC EMC ET /P <>BDC q S 0 Tc ET BT BT EMC EMC BT EMC EMC /P <>BDC ET (737-800W)Tj EMC EMC ET ET /P <>BDC ET ( )Tj EMC ( )Tj BT EMC 9 0 0 9 68.0314 126.8898 Tm /P <>BDC 7 0 0 7 241.5317 89.9528 Tm /P <>BDC BT BT ( )Tj BT EMC /P <>BDC /P <>BDC EMC ET BT BT /P <>BDC 0 Tc ET 8 0 0 8 334.994 619.9528 Tm ET EMC /P <>BDC 8 0 0 8 507.5134 771.7654 Tm 9 0 0 9 365.1022 170.8898 Tm ( )Tj BT ET ( )Tj -.02 Tc BT EMC BT 7 0 0 7 99.8582 419.7654 Tm /P <>BDC EMC ET 8 0 0 8 225.1837 661.9528 Tm /P <>BDC 0 Tc /P <>BDC ET 6.5 0 0 6.5 296.4841 702.9529 Tm BT ET 9 0 0 9 175.8821 467.8898 Tm (number of available seat-miles \(ASM\))Tj /F1 1 Tf ( )Tj BT ( )Tj 7 0 0 7 113.1366 221.9528 Tm ET /P <>BDC EMC -.02 Tc EMC Boeing 737 800 Hainan Airlines Alan Wilson. BT /P <>BDC (increase in engine efficiency to offer)Tj ET The)Tj EMC ( )Tj /P <>BDC /P <>BDC /P <>BDC EMC [(7)-33(3)8.1(7-900ER & 7)-33(3)8.1(7-9 )]TJ EMC BT ET BT 7 0 0 7 158.74 562.7654 Tm )Tj 7 0 0 7 380.2788 540.7654 Tm ET ( )Tj EMC 0 Tc ET ET /P <>BDC 788 0 obj ()Tj 9 0 0 9 565.9882 214.8898 Tm ET /P <>BDC ( )Tj -.02 Tc ET /P <>BDC /GS2 gs 7 0 0 7 88.196 11.5129 Tm ET 9 0 0 9 195.0251 434.8898 Tm BT EMC EMC EMC ( )Tj EMC /P <>BDC 9 0 0 9 546.6454 60.8898 Tm ET 9 0 0 9 215.4313 324.8898 Tm ET BT BT BT ET ( )Tj ( )Tj ET BT /P <>BDC /P <>BDC (5B4/P)Tj BT ET 9 0 0 9 394.0157 247.8898 Tm /P <>BDC 8 0 0 8 54.0516 771.7654 Tm ET /P <>BDC 6.5 0 0 6.5 176.1172 585.9529 Tm /P <>BDC BT (A321neo)Tj 9 0 0 9 36.8504 49.8898 Tm EMC BT ( )Tj EMC ET /P <>BDC BT BT ET )Tj BT ( )Tj ET And the 800 has shown to be one of the most popular models for filling this role. EMC /P <>BDC [(E)-7.8(P)16.1(T)9(E)-13.9(MBE)-16.9(R)]TJ f 7 0 0 7 474.7064 342.9528 Tm BT 9 0 0 9 215.433 71.8898 Tm 9 0 0 9 53.8582 434.8898 Tm ET BT ET ( )Tj 7 0 0 7 315.5217 584.7654 Tm EMC (38,168)Tj ( )Tj /GS1 gs EMC ET ET /P <>BDC BT BT .008 Tc /P <>BDC ( )Tj ET ( )Tj 859 0 obj 0 Tc (0.0123)Tj ET ET Hi I was just wondering where you got this data from. -.01 Tc ET 7 0 0 7 99.8582 518.7654 Tm ( )Tj (252-264)Tj ET BT /P <>BDC EMC BT /P <>BDC /P <>BDC ET EMC BT ( N)Tj /P <>BDC -.005 Tc ( )Tj BT (1,272)Tj 7 0 0 7 314.6398 716.7654 Tm EMC )Tj 8 0 0 8 43.6039 703.9528 Tm /P <>BDC BT 7 0 0 7 364.1531 584.9528 Tm 5.25 0 0 5.25 492.6848 11.5129 Tm EMC -.01 Tc ( )Tj ET ET 9 0 0 9 191.0032 225.8898 Tm BT 7 0 0 7 521.4928 672.9528 Tm ET /P <>BDC /P <>BDC S /P <>BDC BT EMC /P <>BDC (A320ceo)Tj EMC [(P)11(ayload scenario two)]TJ EMC (capacity, so that payload is reduced to)Tj /P <>BDC ( )Tj /P <>BDC BT ET EMC /P <>BDC EMC /P <>BDC BT ( )Tj BT /P <>BDC BT ( )Tj 7 0 0 7 54.7071 287.7654 Tm 0 Tc ET ET BT BT /P <>BDC /P <>BDC (A321neo)Tj EMC /P <>BDC BT /P <>BDC BT BT BT BT ET 7 0 0 7 158.74 100.7654 Tm /F6 1 Tf EMC /P <>BDC 9 0 0 9 546.3135 258.8898 Tm BT -.02 Tc ET 9 0 0 9 36.8504 423.8898 Tm EMC /P <>BDC /P <>BDC q BT ET BT /P <>BDC /P <>BDC 9 0 0 9 362.6813 357.8898 Tm ET EMC )Tj BT .151 .147 .15 rg ( )Tj 0 Tc EMC ET ET EMC ( )Tj BT ET EMC /OC /MC5078 BDC BT ET /P <>BDC ET EMC ET EMC /P <>BDC /P <>BDC ET (0.0129)Tj EMC ET -.01 Tc /P <>BDC ET BT BT BT BT S ET /P <>BDC EMC /P <>BDC 7 0 0 7 247.7395 276.7654 Tm (379)Tj 9 0 0 9 194.061 324.8898 Tm 7 0 0 7 444.737 276.7654 Tm /P <>BDC 7 0 0 7 247.7395 606.7654 Tm 7 0 0 7 258.2805 243.7654 Tm EMC BT At least with the Max 8, looking into the ACAP of Boeing (Rev E), I found it is 2500nm. 7 0 0 7 355.3163 111.7654 Tm ET ( )Tj ( )Tj ET /GS2 gs 737-300/-400/-500, BT BT (industry is 210 US cents per USG for Jet A-)Tj /P <>BDC EMC .023 .567 .626 RG /P <>BDC /P <>BDC /P <>BDC 0 Tc (136)Tj 5.25 0 0 5.25 64.5461 11.5129 Tm ET /P <>BDC EMC EMC ( )Tj /P <>BDC 137 )Tj 7 0 0 7 277.3936 474.9528 Tm ET ( )Tj (2,732)Tj BT It is assumed that the aircraft in)Tj -.02 Tc ET EMC EMC 7 0 0 7 37.0536 584.9528 Tm (A320ceo and A320neo in this study. ( )Tj EMC EMC 9 0 0 9 36.8504 126.8898 Tm 7 0 0 7 82.2047 496.9528 Tm BT ET /P <>BDC ET BT -.01 Tc BT BT 7 0 0 7 363.2711 397.9528 Tm /P <>BDC 0 Tc 0 Tc EMC 7 0 0 7 537.7804 243.9528 Tm ET 7 0 0 7 37.6993 331.9528 Tm EMC ( )Tj (192)Tj BT ( )Tj [(OM)8.1(M)-12.9(E)-24.9(R)7.1(C)8.1(E)]TJ ET 8 0 0 8 365.7704 619.9528 Tm /P <>BDC /P <>BDC ( )Tj ( )Tj ET ( )Tj EMC ( )Tj -.02 Tc ET ( )Tj ( )Tj -.02 Tc 7 0 0 7 380.2788 441.7654 Tm /P <>BDC EMC BT ( )Tj -.02 Tc 7 0 0 7 247.7395 507.7654 Tm (310,080)Tj ( )Tj /P <>BDC /P <>BDC EMC EMC /P <>BDC ( )Tj ET 13 0 0 13 205.5668 412.8898 Tm EMC 7 0 0 7 36.8504 749.9528 Tm ET EMC (assumed that no additional cargo is taken)Tj ET BT 6.5 0 0 6.5 528.5291 650.9529 Tm 0 Tc (-58)Tj /P <>BDC /P <>BDC There was no additional)Tj 9 0 0 9 555.4203 346.8898 Tm BT BT BT /P <>BDC ET EMC /P <>BDC 6.5 0 0 6.5 549.8557 689.9529 Tm EMC ET EMC ET ET /P <>BDC /P <>BDC (136-145)Tj /P <>BDC /P <>BDC BT /P <>BDC EMC /P <>BDC /P <>BDC ( )Tj ET ET EMC ( )Tj ( )Tj BT EMC ET /P <>BDC ET BT -.01 Tc ET BT ET ET 9 0 0 9 394.0315 797.8898 Tm (total cost for fuel burn, time-related costs,)Tj 7 0 0 7 258.2805 672.7654 Tm ET BT /P <>BDC BT 0 Tc EMC .023 .567 .626 rg In this case I believe TUI fly is the main customer. ( )Tj /P <>BDC Hi Ben, BT 9 0 0 9 493.9938 357.8898 Tm /P <>BDC ( )Tj ( )Tj EMC ET EMC -.02 Tc (150)Tj /P <>BDC 9 0 0 9 497.8043 313.8898 Tm (737-9)Tj EMC 9 0 0 9 570.8806 720.8898 Tm 8 0 0 8 225.1837 745.9528 Tm ET ET Federal Aviation Administration and the Boeing Company to evaluate the ET ( )Tj ( )Tj Boeing 747 8 Specs. -.02 Tc EMC BT ET ET /P <>BDC They were solenoid held and ET Cheers Peter. BT BT (41,349)Tj 9 0 0 9 394.0315 621.8898 Tm /P <>BDC /OC /MC225 BDC 6.5 0 0 6.5 295.5027 565.9529 Tm ( )Tj BT EMC BT not sure where to find that kind of detail. 7 0 0 7 279.1575 111.9528 Tm 9 0 0 9 36.8504 49.8898 Tm BT /P <>BDC BT ( )Tj BT /P <>BDC ET BT /P <>BDC ET -.02 Tc ET /P <>BDC 6 0 0 6 554.6981 760.7654 Tm /P <>BDC ( )Tj ET /P <>BDC 7 0 0 7 355.3163 133.7654 Tm BT ET /P <>BDC EMC EMC 7 0 0 7 490.5101 529.9528 Tm /P <>BDC ET EMC EMC 9 0 0 9 527.5473 390.8898 Tm 9 0 0 9 394.0157 621.8898 Tm EMC ET 9 0 0 9 363.9759 115.8898 Tm /P <>BDC /P <>BDC W n ET 8 0 0 8 72.3645 771.9528 Tm 9 0 0 9 211.7668 225.8898 Tm /P <>BDC ET /P <>BDC ET ( )Tj BT /P <>BDC 10 0 0 10 230.6475 794.2914 Tm ET 7 0 0 7 554.7883 507.7654 Tm ( )Tj /P <>BDC 7 0 0 7 386.3929 694.9528 Tm 6.5 0 0 6.5 387.561 611.9529 Tm BT 9 0 0 9 189.8423 467.8898 Tm /Figure <>BDC (13.1% to 18.9% improvements in block)Tj /P <>BDC EMC BT (737-9)Tj /P <>BDC BT BT ET ET ET EMC BT 0 Tc EMC 9 0 0 9 53.8578 236.8898 Tm /P <>BDC 6 0 0 6 240.5796 729.9528 Tm /P <>BDC ET 0 Tc ET EMC 7 0 0 7 354.6933 276.7654 Tm BT EMC BT ET EMC EMC 0 Tc 0 Tc ET EMC EMC -.02 Tc BT Each version in the 737 family fills a differ role. /Artifact <>BDC EMC ( )Tj 6 0 0 6 346.935 771.9528 Tm ET will be centre fuel tank inerting. ( )Tj 7 0 0 7 554.7883 166.7654 Tm EMC /P <>BDC 9 0 0 9 199.3017 401.8898 Tm BT BT /OC /MC4800 BDC EMC BT ET EMC ET /P <>BDC BT EMC BT ( )Tj ET 6 0 0 6 277.7663 673.9528 Tm ET .534 .14 .504 RG /OC /MC1329 BDC )Tj EMC BT /P <>BDC 7 0 0 7 124.1242 199.7654 Tm ET 6.5 0 0 6.5 489.7146 611.9529 Tm BT BT ET /P <>BDC ET /P <>BDC EMC 0 Tc BT EMC 9 0 0 9 215.4409 269.8898 Tm BT BT BT /F6 1 Tf EMC BT (0.0132)Tj /P <>BDC ( )Tj ET ( )Tj EMC EMC BT /P <>BDC 7 0 0 7 118.104 111.7654 Tm ET 0 Tc BT ET q 1 0 0 1 53.858 194.878 cm 0 0 m 7 0 0 7 148.0554 11.5132 Tm EMC soaked fuel causing frost to form on the wings during the turnarounds - even in /P <>BDC EMC Most of the differences comes from lighting in the overhead giving clear readings of digital gauges. 9 0 0 9 195.9803 247.8898 Tm BT 0 Tc /P <>BDC ( )Tj 7 0 0 7 315.5217 595.7654 Tm BT ET BT ( )Tj ( )Tj EMC 9 0 0 9 381.9109 456.8898 Tm ET EMC EMC /P <>BDC 7 0 0 7 230.7317 67.9528 Tm BT BT ET ET 2001 - 2019, Karsten Palt, Leipzig / Germany - All rights reserved, Brussel/Bruxelles - Brussels Airport (EBBR / BRU). ( )Tj Calculates enroute fuel burn based on cruise altitude and trip distance. BT BT EMC -.02 Tc BT BT EMC /P <>BDC /OC /MC186 BDC ( )Tj 0 Tc EMC /P <>BDC /P <>BDC ET EMC EMC /P <>BDC (might have over an older aircraft would)Tj /P <>BDC ( )Tj 6 0 0 6 144.9509 687.9528 Tm As a result of its lower fuel burn,)Tj /P <>BDC BT /P <>BDC /P <>BDC ET This fuel would give a BT EMC /P <>BDC BT ( )Tj BT 0 Tc ET ET ( )Tj ET 0 Tc BT 9 0 0 9 215.433 379.8898 Tm BT /P <>BDC EMC /P <>BDC BT 9 0 0 9 411.0097 181.8898 Tm ET 7 0 0 7 125.6292 727.7654 Tm 5.25 0 0 5.25 447.6106 11.5129 Tm EMC -.02 Tc 7 0 0 7 247.7395 628.7654 Tm EMC 7 0 0 7 37.0536 617.9528 Tm /P <>BDC BT -.02 Tc /P <>BDC 6.5 0 0 6.5 54.877 702.9529 Tm /P <>BDC BT EMC 9 0 0 9 425.1913 93.8898 Tm ET EMC 6 0 0 6 371.479 715.9528 Tm ET EMC ( )Tj 8 0 0 8 43.6039 745.9528 Tm ( )Tj EMC BT /P <>BDC EMC /P <>BDC EMC (0.0140)Tj /OC /MC1976 BDC 7 0 0 7 141.7322 188.9528 Tm EMC [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ /P <>BDC -.02 Tc 786 0 obj /P <>BDC EMC /P <>BDC EMC EMC EMC -.01 Tc (171,961)Tj BT BT (l)Tj EMC 9 0 0 9 36.8504 104.8898 Tm ET ( )Tj 8 0 0 8 141.7322 760.9528 Tm BT (A)Tj EMC ET BT 8 0 0 8 99.8582 760.7654 Tm BT EMC 6 0 0 6 520.876 743.9528 Tm EMC ET (157,300)Tj ( )Tj BT EMC ( )Tj (A320ceo: )Tj ET 5 0 0 5 484.5872 11.5129 Tm BT ET /F4 1 Tf ET 7 0 0 7 474.3564 617.9528 Tm ET 0 Tc /P <>BDC 7 0 0 7 387.0159 584.9528 Tm ( )Tj EMC ET ( )Tj 7 0 0 7 163.8846 11.5132 Tm 9 0 0 9 550.3618 324.8898 Tm /P <>BDC EMC /F6 1 Tf BT (I)Tj (0.0112)Tj EMC /P <>BDC BT 7 0 0 7 54.7071 672.7654 Tm /P <>BDC ET ( )Tj 9 0 0 9 36.8504 148.8898 Tm 9 0 0 9 229.6045 489.8898 Tm BT 7 0 0 7 258.2805 364.7654 Tm /P <>BDC ( )Tj EMC (A321neo)Tj BT BT /P <>BDC For example, if the fuel tank maximum capacity is 10,000 KG, then the tolerance of the gauging is 0.03 (airplane with analog indicators) * 10000 = 300 KG. EMC /P <>BDC /P <>BDC BT BT 0 Tc 7 0 0 7 182.3536 78.9528 Tm ET ET -.02 Tc EMC BT (on the same sector is almost the same as)Tj BT 9 0 0 9 215.433 236.8898 Tm -.02 Tc BT BT 7 0 0 7 520.6108 683.9528 Tm ET EMC 9 0 0 9 165.0289 60.8898 Tm ET /P <>BDC 7 0 0 7 316.0679 232.7654 Tm 7 0 0 7 474.3564 507.9528 Tm ( )Tj ET 7 0 0 7 37.0536 628.9528 Tm 0 Tc ET ( )Tj /Artifact <>BDC (4,836)Tj /P <>BDC /P <>BDC EMC 9 0 0 9 232.438 291.8898 Tm ET BT /P <>BDC /P <>BDC The A320ceo and)Tj /GS1 gs /P <>BDC 6 0 0 6 412.4713 715.9528 Tm ET 9 0 0 9 395.1859 258.8898 Tm It has a maximum range of 10,140km. ( )Tj (1,773)Tj /P <>BDC BT ET ET EMC ET /P <>BDC 9 0 0 9 394.0315 60.8898 Tm ( )Tj EMC BT /P <>BDC EMC 6.5 0 0 6.5 107.0213 650.9529 Tm (passengers. ET ET /P <>BDC than the main wing tanks. BT ( )Tj 0 Tc BT ET /P <>BDC ET ET EMC BT /P <>BDC (of fuel against time-related costs. EMC /P <>BDC ET ET EMC ET /P <>BDC /P <>BDC /P <>BDC ET 7 0 0 7 429.157 485.9528 Tm -.02 Tc 7 0 0 7 158.74 276.7654 Tm ET (0.0120)Tj 6 0 0 6 394.3996 687.9528 Tm 7 0 0 7 210.1137 364.7654 Tm EMC 7 0 0 7 507.7893 210.7654 Tm EMC /P <>BDC 9 0 0 9 232.4217 38.8898 Tm (A321neo)Tj (I)Tj ( )Tj 7 0 0 7 429.157 474.9528 Tm BT EMC BT /GS1 gs /P <>BDC EMC /P <>BDC 6.5 0 0 6.5 54.877 715.9529 Tm ET 7 0 0 7 521.4089 11.5132 Tm /P <>BDC -.02 Tc BT ET BT 9 0 0 9 232.4217 71.8898 Tm ( )Tj 7 0 0 7 490.8321 78.7654 Tm ( )Tj BT 7 0 0 7 88.196 11.5129 Tm EMC ( )Tj /P <>BDC 6 0 0 6 433.7979 771.9528 Tm ET BT ET [(AS)29(M)]TJ ( )Tj BT ( )Tj (Using the evaluation payloads of 170)Tj /P <>BDC BT ET /P <>BDC ( )Tj EMC BT EMC (network. BT 9 0 0 9 192.5225 489.8898 Tm BT (have a 20-minute taxi-out time departing)Tj BT Hi All, 9 0 0 9 386.0797 71.8898 Tm ET BT 0 Tc [(F)-21(LL/47)]TJ 7 0 0 7 440.0906 342.9528 Tm BT EMC ( )Tj BT ( )Tj 0 Tc 6.5 0 0 6.5 448.257 598.9529 Tm 0 Tc ET EMC EMC BT 7 0 0 7 404.101 177.7654 Tm 0 Tc 9 0 0 9 36.8504 346.8898 Tm ( )Tj EMC 9 0 0 9 411.0181 137.8898 Tm BT EMC (5B3)Tj BT (CFM56-7B27B3)Tj EMC /P <>BDC ET EMC /P <>BDC /P <>BDC Q ET EMC 9 0 0 9 563.6848 401.8898 Tm EMC EMC 7 0 0 7 158.74 342.7654 Tm /P <>BDC ET ( )Tj (have therefore been removed from the)Tj 9 0 0 9 569.5997 566.8898 Tm /P <>BDC EMC EMC ET 9 0 0 9 183.3893 456.8898 Tm /P <>BDC -.02 Tc ET 7 0 0 7 491.7142 232.7654 Tm /P <>BDC EMC BT BT With a)Tj EMC BT (56,901)Tj ET ( )Tj ET ET ET 0 Tc /P <>BDC (150)Tj ET [(737-900E)-33(R)]TJ 7 0 0 7 241.5317 320.9528 Tm BT -.02 Tc ET (127)Tj /P <>BDC BT /P <>BDC (3,341)Tj -.02 Tc 6.5 0 0 6.5 531.2397 565.9529 Tm ET 7 0 0 7 490.5101 705.9528 Tm /P <>BDC BT EMC /P <>BDC /P <>BDC EMC BT /P <>BDC -.02 Tc 7 0 0 7 230.7317 309.9528 Tm ( )Tj EMC ( )Tj /P <>BDC .023 .567 .626 rg EMC EMC (10)Tj EMC /P <>BDC ET 7 0 0 7 118.104 67.7654 Tm ET ET ET EMC EMC EMC ET [(P)11(ayload)]TJ 7 0 0 7 490.5101 540.9528 Tm /P <>BDC /P <>BDC BT BT EMC BT 7 0 0 7 299.0601 408.9528 Tm ET ( )Tj 7 0 0 7 99.8582 375.7654 Tm 7 0 0 7 230.7317 221.9528 Tm EMC /P <>BDC BT BT /P <>BDC ET 0 Tc /P <>BDC BT 9 0 0 9 191.7774 423.8898 Tm EMC BT /P <>BDC EMC /P <>BDC ( )Tj EMC BT ET /P <>BDC ET EMC ( )Tj ET 6 0 obj ET 9 0 0 9 411.0097 335.8898 Tm /P <>BDC ( )Tj /F4 1 Tf BT ET ET ET ET BT /P <>BDC EMC (\(see)Tj 0 Tc /P <>BDC ET ET 9 0 0 9 556.3508 137.8898 Tm 7 0 0 7 54.7071 562.7654 Tm ( )Tj BT 0 Tc /F6 1 Tf EMC 7 0 0 7 439.2087 78.9528 Tm ET BT EMC ET -.02 Tc 0 Tc 0 Tc ET 10 0 0 10 47.8705 814.1973 Tm /P <>BDC EMC BT /F4 1 Tf /P <>BDC -.02 Tc /P <>BDC ( )Tj But the biggest improvement (CFM56-7B26)Tj EMC ( )Tj EMC BT /P <>BDC EMC (I)Tj ET BT /P <>BDC EMC EMC 6.5 0 0 6.5 64.6596 650.9529 Tm /P <>BDC /P <>BDC -.02 Tc [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ BT (800 is not as large as the difference)Tj ET -.02 Tc ET ET 2002-19-52 which requires the crew to maintain certain minimum fuel (1,074)Tj /P <>BDC ET 0 Tc /P <>BDC BT [(AIRL)8.1(INE & AIR)7.1(CRAF)-12.9(T)18.1( OPERA)56.9(T)-8.1(ION)-13.9(S)]TJ 7 0 0 7 163.8846 11.5132 Tm EMC ( )Tj (On the sectors where the A321ceo and)Tj 7 0 0 7 130.1443 518.7654 Tm 7 0 0 7 82.8504 265.9528 Tm (seat capacity over the NG series. ( )Tj (0.0146)Tj ET (different available options, and gives the)Tj 7 0 0 7 294.4014 331.7654 Tm ( )Tj .008 Tc (evaluation, the 737-8 and 737-9 are 2.2%)Tj 9 0 0 9 181.6136 456.8898 Tm ET 6.5 0 0 6.5 433.3069 545.9529 Tm 7 0 0 7 107.1165 562.9528 Tm ET (1,272)Tj EMC 9 0 0 9 215.433 181.8898 Tm 9 0 0 9 232.4217 115.8898 Tm /GS1 gs BT 7 0 0 7 337.4684 705.9528 Tm /P <>BDC 1 i ET ET ET 0 Tc 9 0 0 9 352.4841 313.8898 Tm (34,650)Tj BT (737-900ER\(W\) rather than the 737-900,)Tj 7 0 0 7 314.6398 474.7654 Tm BT EMC EMC BT ET -.02 Tc BT /P <>BDC /P <>BDC (158)Tj APU fuel pump in the No 1 tank which operates automatically during the start BT /P <>BDC -.02 Tc EMC /P <>BDC EMC ET ( )Tj EMC 7 0 0 7 537.7804 408.9528 Tm 7 0 0 7 491.4046 232.9528 Tm ET EMC (0.0127)Tj ET ( )Tj 9 0 0 9 564.1726 588.8898 Tm 1 i BT BT /F7 1 Tf EMC ET BT (403)Tj /P <>BDC ET BT -.02 Tc BT ( )Tj 7 0 0 7 37.0536 562.9528 Tm ET /P <>BDC ET /P <>BDC /F4 1 Tf EMC -.02 Tc (78,729)Tj (into service in 2023. ET 7 0 0 7 131.6494 672.7654 Tm 0 Tc 6.5 0 0 6.5 347.0329 532.9529 Tm /P <>BDC ET (The fuel burn difference is greater on)Tj EMC /P <>BDC ET EMC EMC EMC 7 0 0 7 321.6356 309.9528 Tm ( )Tj 7 0 0 7 380.2788 375.7654 Tm (342,312)Tj ET BT EMC (216,240)Tj ET BT EMC (Both the younger generation of Airbus)Tj BT /Artifact <>BDC (remain key aircraft for many operators)Tj ( )Tj ET 6 0 0 6 333.9129 729.9528 Tm /P <>BDC [(UG)-17.1(U)-8(S)8.1(T)]TJ EMC /P <>BDC BT BT (0.0115)Tj 0 Tc ( )Tj 7 0 0 7 247.7395 419.7654 Tm BT EMC 0 Tc ET BT EMC -.02 Tc /P <>BDC ET (number of seats and ASMs will give an)Tj /P <>BDC ( )Tj /P <>BDC (977)Tj -.02 Tc /P <>BDC /P <>BDC 0 Tc BT (486)Tj -.02 Tc /P <>BDC 0 Tc ET EMC EMC 0 Tc 8 0 0 8 531.1443 775.8898 Tm (6,353)Tj /P <>BDC /P <>BDC EMC /P <>BDC /P <>BDC q ET ( )Tj (ONT/73)Tj EMC BT This study uses a)Tj 7 0 0 7 445.619 474.7654 Tm /P <>BDC BT -.02 Tc 7 0 0 7 537.7804 364.9528 Tm EMC /P <>BDC 0 Tc ET 9 0 0 9 372.6154 236.8898 Tm 9 0 0 9 550.3917 456.8898 Tm ET BT /P <>BDC (163)Tj 503.534 80.74 l EMC BT ( )Tj (9.0:1)Tj BT 6.5 0 0 6.5 232.6392 735.9529 Tm 0 Tc ( )Tj EMC ET The design of the 800 comes from studying the pitfalls of the 727. EMC ET ET (1,800 - )Tj /P <>BDC 0 Tc EMC -.02 Tc ET 7 0 0 7 99.8582 166.7654 Tm /P <>BDC EMC ET ()Tj 7 0 0 7 444.737 320.7654 Tm ET ET ET BT 7 0 0 7 82.2047 617.9528 Tm BT (I)Tj 9 0 0 9 550.1644 170.8898 Tm ET 7 0 0 7 37.6993 133.9528 Tm 7 0 0 7 440.0906 331.9528 Tm 0 Tc /F4 1 Tf /P <>BDC EMC BT In this)Tj 7 0 0 7 82.8504 342.9528 Tm BT /P <>BDC 0 Tc (aircraft types, all the flights were evaluated)Tj EMC 9 0 0 9 183.72 797.8898 Tm f ET BT EMC .964 .834 .406 rg ( )Tj 9 0 0 9 394.0237 225.8898 Tm (fuel burn. BT EMC BT ( )Tj ET 9 0 0 9 68.3339 555.8898 Tm /P <>BDC BT BT BT ET /P <>BDC 0 Tc 9 0 0 9 53.8578 291.8898 Tm 0 Tc BT /P <>BDC /P <>BDC (3,300 - )Tj (similar rate, with Boeing having delivered)Tj 0 Tc BT (CFM56-5B4/P)Tj BT 9 0 0 9 53.8338 225.8898 Tm 0 Tc EMC /P <>BDC -.02 Tc EMC BT BT BT BT /P <>BDC /P <>BDC [(the A320neo)16.1(. [(E)-7.8(P)16.1(T)9(E)-13.9(MBE)-16.9(R)]TJ ET /P <>BDC ( )Tj EMC ( )Tj 9 0 0 9 112.3045 346.8898 Tm ET ET BT BT EMC /P <>BDC -.02 Tc EMC EMC BT 9 0 0 9 68.3339 500.8898 Tm ( )Tj 7 0 0 7 491.4046 133.9528 Tm ET /P <>BDC /P <>BDC (alternates used and their distance from the)Tj /P <>BDC /P <>BDC .151 .147 .15 rg /P <>BDC EMC ( )Tj ( )Tj 9 0 0 9 187.8892 159.8898 Tm BT BT /P <>BDC /P <>BDC -.02 Tc (aircraft types: the A320ceo, A321ceo,)Tj (between: the Pratt & Whitney PW1127G,)Tj 8 0 0 8 181.9279 771.7654 Tm /F4 1 Tf ( )Tj ( )Tj EMC 8 0 0 8 124.845 591.9528 Tm /P <>BDC 9 0 0 9 375.3516 335.8898 Tm 7 0 0 7 490.8321 199.7654 Tm /P <>BDC 9 0 0 9 548.6884 137.8898 Tm EMC ET ( )Tj ( )Tj 7 0 0 7 279.1575 705.9528 Tm /P <>BDC BT EMC 9 0 0 9 232.438 159.8898 Tm /P <>BDC 7 0 0 7 241.5317 683.9528 Tm BT EMC BT /P <>BDC EMC /P <>BDC EMC EMC 232.441 655.706 340.157 -624.522 re 7 0 0 7 507.7893 67.7654 Tm /P <>BDC ET ET BT BT (1,272)Tj /P <>BDC (A fuel density of 6.55lbs per USG was)Tj Do you know how or where I would be able to get details on the dimensions or materials of the wingtip for this aircraft or other similar aircraft? 9 0 0 9 394.0123 654.8898 Tm BT /GS1 gs /P <>BDC ET ET EMC 0 Tc (CFM56-5B3/P)Tj 7 0 0 7 326.2278 705.9528 Tm BT /P <>BDC (1, where equal passenger payloads have)Tj BT ET ET ET 0 Tc ( )Tj BT BT BT /P <>BDC BT BT /P <>BDC EMC 6 0 0 6 403.4411 757.9528 Tm ( )Tj /P <>BDC 7 0 0 7 380.2788 298.7654 Tm BT /P <>BDC BT -.01 Tc -.02 Tc (maximise their service offering. 8 0 0 8 189.0627 717.9528 Tm EMC ( )Tj 7 0 0 7 364.1531 463.9528 Tm 8 0 0 8 419.0258 760.9528 Tm (1,800 - )Tj /P <>BDC 9 0 0 9 246.6113 401.8898 Tm 7 0 0 7 54.7071 298.7654 Tm /P <>BDC A fuel sampling and testing kit is kept on the flight deck of all ET 9 0 0 9 53.8338 269.8898 Tm 9 0 0 9 193.0552 434.8898 Tm All the flights are in a westerly)Tj EMC 7 0 0 7 521.4089 11.5132 Tm EMC -.02 Tc ET ET BT ET [(OM)8.1(M)-12.9(E)-24.9(R)7.1(C)8.1(E)]TJ 9 0 0 9 36.8504 214.8898 Tm /P <>BDC BT /P <>BDC BT 0 Tc ( )Tj 8 0 0 8 505.7415 771.9528 Tm EMC EMC ET ET ET (travelled for the aircraft on each route is)Tj ET /P <>BDC ( )Tj -1.1093 -3.9038 l EMC BT (4,218)Tj BT /P <>BDC ( )Tj 7 0 0 7 457.0984 672.7654 Tm EMC (l)Tj EMC EMC 9 0 0 9 356.4538 258.8898 Tm 0 J 0 j .5 w 10 M [] 0 d ( )Tj BT 0 Tc BT BT ET 9 0 0 9 232.438 225.8898 Tm (831)Tj ET EMC 7 0 0 7 299.0601 419.9528 Tm
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