BT EMC ET ( )Tj -.02 Tc BT ET -.02 Tc EMC 0 Tc EMC ET ( )Tj ET 6 0 0 6 466.0123 687.9528 Tm 9 0 0 9 394.0157 390.8898 Tm BT (0.0113)Tj BT ( )Tj /P <>BDC Q /P <>BDC 0 Tc EMC [(C)17.1(OS/104)]TJ 9 0 0 9 53.8338 214.8898 Tm 9 0 0 9 232.4217 489.8898 Tm /P <>BDC BT BT ET ( )Tj EMC /P <>BDC /P <>BDC /P <>BDC ( )Tj -.02 Tc 7 0 0 7 108.6215 529.9528 Tm /P <>BDC ET ET -.02 Tc ( )Tj 6.5 0 0 6.5 282.0695 735.9529 Tm /P <>BDC 7 0 0 7 320.7537 67.9528 Tm /P <>BDC ET EMC /OC /MC852 BDC ( )Tj EMC 6.5 0 0 6.5 54.877 624.9529 Tm 7 0 0 7 362.3891 144.9528 Tm EMC 0 Tc BT BT 9 0 0 9 425.183 544.8898 Tm EMC 0 Tc BT (31,416)Tj EMC ET EMC EMC 0 Tc EMC (CFM56-7B26)Tj BT ( )Tj ET /P <>BDC EMC /P <>BDC (A321ceo)Tj BT /P <>BDC ( )Tj [(737 M)-8.1(A)-24.9(X-9:)]TJ ET 9 0 0 9 173.6527 500.8898 Tm /P <>BDC (The evaluation uses US domestic flight)Tj EMC ET (1,288)Tj EMC BT EMC (rating on the CFM LEAP-1A32 to)Tj -.02 Tc 7 0 0 7 554.7883 232.7654 Tm 9 0 0 9 189.8423 467.8898 Tm Both fuel pump low pressure lights in any tank are required BT Boeing 737-800 commercial aircraft. EMC BT 0 Tc /P <>BDC /P <>BDC 0 Tc ET 7 0 0 7 242.1547 78.9528 Tm ( )Tj ET EMC (The A320ceo is payload-restricted to)Tj /P <>BDC -.02 Tc 6.5 0 0 6.5 448.8744 558.9529 Tm /P <>BDC 9 0 0 9 366.3893 445.8898 Tm EMC BT /P <>BDC BT /P <>BDC 7 0 0 7 403.478 573.7654 Tm EMC 0 Tc EMC /P <>BDC /P <>BDC ( )Tj ET ( )Tj EMC ET EMC ( )Tj /P <>BDC BT EMC ( )Tj 0 Tc ( )Tj BT /P <>BDC BT -.01 Tc (105,000lbs. The BBJ is based on the 737-700 airliner and the BBJ2 on the 737-800. 7 0 0 7 519.3773 221.9528 Tm ET EMC BT 7 0 0 7 258.2805 584.7654 Tm 7 0 0 7 518.3203 430.9528 Tm ET /P <>BDC EMC /P <>BDC BT q ET 9 0 0 9 36.8504 60.8898 Tm EMC BT /P <>BDC /P <>BDC /P <>BDC 0 Tc ( )Tj ( )Tj ET EMC BT ET 9 0 0 9 232.4408 687.8898 Tm ( )Tj ET BT ( )Tj ET EMC (US gallons \(USG\) )Tj BT BT 7 0 0 7 338.6433 232.7654 Tm ET (than the 737-9. -.02 Tc EMC 0 Tc 9 0 0 9 547.6174 467.8898 Tm 9 0 0 9 548.3564 225.8898 Tm 9 0 0 9 546.4149 456.8898 Tm ET BT 7 0 0 7 113.1366 320.9528 Tm 10 0 0 10 420.16 814.1973 Tm EMC 0 Tc ET /P <>BDC ( )Tj EMC ( )Tj EMC ET ET (0.0157)Tj EMC /P <>BDC )Tj 6.5 0 0 6.5 346.9224 650.9529 Tm ET ET ET /P <>BDC -.02 Tc ( )Tj BT /P <>BDC BT 7 0 0 7 43.6039 540.9528 Tm (flight relate to fuel burn, overflight and)Tj ET /F4 1 Tf EMC EMC EMC /P <>BDC EMC /P <>BDC ET 0 Tw 7 0 0 7 337.6855 408.9528 Tm (136)Tj -.02 Tc ET /P <>BDC /P <>BDC 7 0 0 7 54.7071 485.7654 Tm Q /P <>BDC BT 6 0 0 6 55.0668 715.9528 Tm 0 Tc BT 0 Tc ( )Tj EMC ET /P <>BDC ET 7 0 0 7 258.2805 210.7654 Tm BT ( )Tj 7 0 0 7 403.478 617.7654 Tm BT /P <>BDC 9 0 0 9 539.8684 280.8898 Tm ( The cruise speed and flight profile )Tj BT EMC /P <>BDC ( )Tj BT EMC 7 0 0 7 54.5916 738.7654 Tm EMC BT ET 7 0 0 7 36.8504 11.5129 Tm ( )Tj EMC ET /P <>BDC ET BT BT ( )Tj EMC ( )Tj ( )Tj -.02 Tc 7 0 0 7 535.5029 441.7654 Tm ( )Tj /P <>BDC /P <>BDC EMC BT 9 0 0 9 53.8578 93.8898 Tm EMC ( )Tj BT 9 0 0 9 182.8313 346.8898 Tm 7 0 0 7 491.392 727.9528 Tm It is assumed that the aircraft in)Tj 6.5 0 0 6.5 381.6589 558.9529 Tm BT EMC /GS1 gs ( )Tj EMC EMC /P <>BDC ( )Tj EMC /P <>BDC 0 Tc /P <>BDC S ( )Tj ET (900ER\(W\). BT 0 Tc BT -9.719 805.04 386.723 -270.624 re ET /P <>BDC ( )Tj EMC /F6 1 Tf EMC BT EMC ET There seem to be a lot of answers that come up, some of which might be what youre looking for. /P <>BDC BT ET warmer air or accelerate to increase the kinetic heating. 9 0 0 9 115.2588 214.8898 Tm /P <>BDC BT /P <>BDC 8 0 0 8 334.994 703.9528 Tm EMC BT ET EMC battery bus but have a dedicated battery to ensure that there is always .023 .567 .626 rg /P <>BDC BT ET ( )Tj EMC 9 0 0 9 270.2513 93.8898 Tm /P <>BDC EMC EMC 9 0 0 9 534.3536 577.8898 Tm ( )Tj BT BT ( )Tj ET [(737-900E)-33(R)]TJ ET EMC BT (CFM56-7B27B3)Tj ET 0 Tc EMC 9 0 0 9 53.8582 236.8898 Tm BT EMC (CFM56-7B27B3)Tj -.02 Tc ET 7 0 0 7 99.8582 144.7654 Tm 9 0 0 9 184.2244 203.8898 Tm ( )Tj Since no two)Tj /P <>BDC BT ET (18.3% on the sectors where an equivalent)Tj /GS2 gs /P <>BDC ( )Tj (34,650)Tj 7 0 0 7 387.0159 584.9528 Tm 9 0 0 9 36.8504 192.8898 Tm EMC 8 0 0 8 319.1147 771.9528 Tm ( )Tj ET ET EMC ( )Tj BT ( )Tj /P <>BDC ET 6.5 0 0 6.5 191.942 611.9529 Tm EMC EMC /P <>BDC .0063 7.6255 l 7 0 0 7 473.8245 111.9528 Tm 7 0 0 7 490.7815 276.9528 Tm BT /P <>BDC (0.0160)Tj 7 0 0 7 459.6601 11.5129 Tm (188,400)Tj -.02 Tc ( )Tj BT EMC BT EMC BT ET /P <>BDC 7 0 0 7 490.5101 661.9528 Tm ET f /P <>BDC 9 0 0 9 420.5961 38.3073 Tm ET BT Boeing 767 the first American Widebody Twin. /P <>BDC ET ( )Tj EMC /GS1 gs ET 9 0 0 9 511.9579 335.8898 Tm -.02 Tc 9 0 0 9 53.8582 346.8898 Tm ET <>stream EMC ( )Tj /P <>BDC BT ET EMC EMC 7 0 0 7 491.7142 595.7654 Tm 7 0 0 7 299.0601 331.9528 Tm ET /P <>BDC EMC (cost compared to fuel. 7 0 0 7 380.2788 617.7654 Tm /P <>BDC BT 9 0 0 9 394.0237 192.8898 Tm 6.5 0 0 6.5 296.4841 702.9529 Tm ( )Tj (LEAP-1B. /F7 1 Tf BT BT 7 0 0 7 258.2805 298.7654 Tm BT /P <>BDC )Tj BT /P <>BDC 7 0 0 7 141.7322 507.9528 Tm ET EMC ET /P <>BDC (937)Tj /P <>BDC Boeing 737 800 Hainan Airlines Alan Wilson. ( )Tj /P <>BDC 9 0 0 9 36.8504 291.8898 Tm (0.0134)Tj EMC EMC EMC 9 0 0 9 258.18 60.8898 Tm (improvement of 13.1%. /P <>BDC BT ET 7 0 0 7 141.7322 463.9528 Tm /P <>BDC /P <>BDC -.02 Tc ( )Tj EMC EMC ET 6 0 0 6 309.4742 687.9528 Tm BT ET EMC [(P)11(ayload scenario one)]TJ ( )Tj 7 0 0 7 404.101 166.7654 Tm ( )Tj 9 0 0 9 394.0237 203.8898 Tm [(AIRL)8.1(INE & AIR)7.1(CRAF)-12.9(T)18.1( OPERA)56.9(T)-8.1(ION)-13.9(S)]TJ (31,416)Tj 7 0 0 7 337.4684 672.9528 Tm /P <>BDC ( )Tj BT EMC (1,500)Tj ( )Tj BT /Artifact <>BDC (A)Tj ET BT BT ET ET BT ET BT 9 0 0 9 36.8504 104.8898 Tm BT 0 Tc ET The weight configuration used)Tj /P <>BDC /P <>BDC /P <>BDC (CFM56-5B4/P)Tj What are the ATR 42 and ATR 72 aircraft made by Arospatiale and Leonardo? EMC 7 0 0 7 297.632 529.9528 Tm 9 0 0 9 525.2239 324.8898 Tm The total tolerance for the FQIS system is based on a full tank. BT 7 0 0 7 99.8582 100.7654 Tm ( 2021)Tj 7 0 0 7 182.5706 375.9528 Tm 7 0 0 7 487.0872 11.5129 Tm /P <>BDC /P <>BDC ( )Tj 0 Tc ET EMC /P <>BDC ET (hour and per mile reduces . ET EMC ET /P <>BDC ET ET /P <>BDC ET 7 0 0 7 37.0536 573.9528 Tm EMC 7 0 0 7 158.74 199.7654 Tm EMC ( )Tj The three-class cabin)Tj ( )Tj BT BT Aux fuel control panel (Aft overhead panel). ET ET W n 8 0 0 8 136.4919 633.9528 Tm EMC 8 0 0 8 419.0258 760.9528 Tm BT 8 0 0 8 124.845 661.9528 Tm ET BT ET /GS2 gs EMC ET 7 0 0 7 344.1175 573.7654 Tm ET /P <>BDC (148,504)Tj EMC ET 7 0 0 7 158.74 221.7654 Tm EMC /P <>BDC ET /P <>BDC 0 Tc /P <>BDC ET BT ET 9 0 0 9 394.0123 621.8898 Tm /P <>BDC /P <>BDC /P <>BDC 0 Tc /P <>BDC ( )Tj 9 0 0 9 53.8338 247.8898 Tm 7 0 0 7 508.4124 727.7654 Tm 9 0 0 9 370.2239 390.8898 Tm (sectors where a 170-passenger payload is)Tj 0 Tc /P <>BDC W n 7 0 0 7 37.6993 287.9528 Tm BT 6.5 0 0 6.5 192.0331 663.9529 Tm 6 0 0 6 507.6099 659.9528 Tm 0 Tc 7 0 0 7 37.0536 727.9528 Tm /P <>BDC /P <>BDC EMC (support, operating procedures and)Tj (2,517)Tj ET 9 0 0 9 191.3244 324.8898 Tm (same number of passengers is carried on)Tj 7 0 0 7 457.0984 463.7654 Tm /P <>BDC ( )Tj ET ( )Tj [(CFM L)17.1(E)-8.1(AP-1A26)]TJ (737-8 has a 0.8-3.0% higher trip fuel burn than)Tj /P <>BDC 6.5 0 0 6.5 540.4371 611.9529 Tm (sector. 5.25 0 0 5.25 492.6848 11.5129 Tm EMC EMC /P <>BDC ET ( )Tj ET ET /P <>BDC /P <>BDC /P <>BDC ET EMC ( )Tj /P <>BDC (based on the cost index set is different, it)Tj EMC 7 0 0 7 294.4014 177.7654 Tm /GS1 gs ET ET -.02 Tc 7 0 0 7 321.6356 210.9528 Tm ( )Tj The NG series are prone to "Upper Wing Surface 9 0 0 9 394.0123 544.8898 Tm (performance of the two reduces to 0.8%)Tj ET EMC EMC (economy cabins. EMC /P <>BDC 737-600/-700/-800/-900 with densitometer: ET /P <>BDC (A321neo)Tj The 737-800 project began in 1994, with Hapag-Lloyd Airlines ofGermany placing the first order for this aircraft. /P <>BDC EMC 7 0 0 7 158.74 595.7654 Tm EMC 7 0 0 7 141.7322 452.9528 Tm /P <>BDC EMC 7 0 0 7 363.2711 419.9528 Tm /P <>BDC (31,416)Tj EMC /P <>BDC endobj ET 7 0 0 7 387.0932 232.9528 Tm /P <>BDC BT (A321neo)Tj (\(see tables,)Tj ET (2,729)Tj ET 7 0 0 7 343.2355 683.7654 Tm [(W)7.1(ind component - kts)]TJ EMC 0 Tc 7 0 0 7 537.7804 210.9528 Tm 7 0 0 7 439.9995 694.9528 Tm 7 0 0 7 241.2727 661.9528 Tm EMC 0 Tc 9 0 0 9 554.0057 566.8898 Tm ET -.02 Tc /P <>BDC ET -.02 Tc /P <>BDC ( )Tj ET ET ET BT ET /P <>BDC BT EMC ET BT ET 7 0 0 7 230.7317 243.9528 Tm EMC BT EMC ET BT (136)Tj BT 7 0 0 7 403.478 67.7654 Tm BT BT -.02 Tc EMC ET EMC 13 0 0 13 53.8582 137.8898 Tm BT (superior fuel burn per seat-mile of all)Tj /P <>BDC EMC 9 0 0 9 36.8504 423.8898 Tm EMC ET 0 Tc ET /P <>BDC ET (36,960)Tj 7 0 0 7 316.0679 430.7654 Tm BT EMC (0.0123)Tj 7 0 0 7 387.0159 562.9528 Tm 8 0 0 8 551.3604 71.8898 Tm 17 0 0 17 36.8606 758.6944 Tm EMC BT BT ET -.01 Tc (Flight time - mins)Tj ( )Tj BT ET /P <>BDC ET ET BT /P <>BDC EMC 7 0 0 7 99.8582 562.7654 Tm 7 0 0 7 294.4014 705.7654 Tm /P <>BDC /P <>BDC BT On the Digital Sunburst fuel gauges, pressing the "Qty test" button will BT (31,416)Tj EMC -.01 Tc EMC 7 0 0 7 508.2252 11.5129 Tm 0 Tc /P <>BDC )Tj 8 0 0 8 334.994 675.9528 Tm /P <>BDC /P <>BDC ( )Tj /P <>BDC ET ( )Tj ET 28.5749 0 TD BT 10 0 0 10 52.7604 814.1973 Tm ET EMC could you point me in the right direction or tell me what the weight of the landing gear would be on a 737? ET 9 0 0 9 53.8578 401.8898 Tm /P <>BDC ET EMC ET ET BT EMC 7 0 0 7 321.6356 265.9528 Tm 7 0 0 7 321.6356 177.9528 Tm BT .0081 Tc ( )Tj 7 0 0 7 295.2833 199.7654 Tm ( )Tj ( )Tj S /P <>BDC BT ( )Tj BT EMC 9 0 0 9 36.8504 181.8898 Tm ET (or the CFM LEAP-1A32, rated at)Tj BT ET 6 0 0 6 115.2799 687.9528 Tm 9 0 0 9 339.3695 192.8898 Tm BT /P <>BDC EMC ET ET /P <>BDC BT /P <>BDC /P <>BDC /GS2 gs EMC /P <>BDC 0 Tc /F6 1 Tf /P <>BDC EMC ET ET -.02 Tc /P <>BDC ET /P <>BDC EMC /P <>BDC ET 9 0 0 9 191.7774 423.8898 Tm EMC /P <>BDC (5,448)Tj /P <>BDC 7 0 0 7 187.0858 364.9528 Tm Economy-plus is also)Tj The average fuel)Tj (comparative performance. ( )Tj -.07 Tc 7 0 0 7 338.6433 441.7654 Tm EMC [(737 M)-8.1(A)-24.9(X-8:)]TJ BT EMC 0 Tc 6 0 0 6 247.27 771.9528 Tm /P <>BDC [(2,575nmn, the 737-8 has an av)12.9(er)10(age 13% lo)12(w)6.1(e)0(r)]TJ ( )Tj EMC 0 Tc BT BT ET EMC -.02 Tc /P <>BDC EMC BT EMC -.02 Tc /P <>BDC BT BT ET 6 0 0 6 425.0715 687.9528 Tm 7 0 0 7 439.4675 89.9528 Tm 7 0 0 7 99.5912 606.9528 Tm (the 14 sectors with the 85% passenger)Tj /P <>BDC 7 0 0 7 387.0932 78.9528 Tm BT EMC (216,240)Tj EMC EMC /P <>BDC (0.0129)Tj EMC /P <>BDC 7 0 0 7 316.0679 67.7654 Tm (34,650lbs )Tj BT ET 0 Tc ET BT ET 7 0 0 7 354.6933 507.7654 Tm /P <>BDC BT /P <>BDC /P <>BDC (831)Tj ET 9 0 0 9 389.8867 269.8898 Tm BT -.01 Tc /P <>BDC 0 Tc EMC BT BT BT ET /F4 1 Tf ET /P <>BDC /P <>BDC BT ET ( )Tj (HGW2 option with an MTOW of)Tj ( )Tj ET /P <>BDC 0 Tc EMC 8 0 0 8 83.5638 619.9528 Tm BT EMC 7 0 0 7 54.5916 254.7654 Tm BT BT BT /P <>BDC /P <>BDC 0 Tc EMC /P <>BDC BT 0 Tc EMC EMC ET EMC /F4 1 Tf (19 seats more than the -800, and 13)Tj BT BT -.02 Tc Typical freezing point of Jet A1 is -47C. /P <>BDC 7 0 0 7 247.7395 595.7654 Tm BT EMC BT (The A320ceo, A321ceo and 737-)Tj ET /P <>BDC ( )Tj ET 9 0 0 9 372.6154 236.8898 Tm 8 0 0 8 315.7776 591.9528 Tm EMC BT 7 0 0 7 387.0932 67.9528 Tm ( )Tj ET EMC 7 0 0 7 456.2165 320.7654 Tm (Engine)Tj EMC ET /P <>BDC ( )Tj EMC BT EMC 0 Tc ET /P <>BDC EMC 0 841.89 609.449 -841.89 re BT ( )Tj BT 7 0 0 7 539.8962 496.9528 Tm ET /P <>BDC ( )Tj 9 0 0 9 363.052 357.8898 Tm (higher OEW. 7 0 0 7 299.0601 243.9528 Tm BT EMC EMC EMC /P <>BDC ET ET BT EMC /P <>BDC BT EMC ET 7 0 0 7 403.478 606.7654 Tm ET BT EMC BT EMC BT /P <>BDC /P <>BDC EMC /P <>BDC 7 0 0 7 439.2087 397.9528 Tm BT (2,731)Tj EMC ( )Tj /P <>BDC EMC The engine option used in this)Tj BT -.02 Tc /P <>BDC /P <>BDC /P <>BDC 19.843 0 l 9 0 0 9 374.2211 379.8898 Tm BT .41 .161 .508 RG capacitors in the tanks with fuel acting as the dielectric. EMC A lower)Tj ET S /P <>BDC (4,218)Tj (direction, with an initial heading ranging)Tj EMC EMC -.01 Tc 9 0 0 9 36.8504 357.8898 Tm ( )Tj 10 0 0 10 52.6304 814.1973 Tm [(CFM L)17.1(E)-8.1(AP-1A32)]TJ /P <>BDC EMC ( )Tj ET BT (171,520)Tj Our Math Says It Isn't. BT BT /P <>BDC 6 0 0 6 412.4713 715.9528 Tm (range for both the A320ceo and A320neo. EMC 7 0 0 7 326.2278 529.9528 Tm (34,650lbs)Tj EMC (CFM56-5B3/P)Tj EMC [(MR)32(TX - lbs)]TJ /P <>BDC EMC flammability exposure of the center wing tank to a level equivalent to or less /P <>BDC /P <>BDC 0 Tc EMC BT ET /P <>BDC ( )Tj EMC EMC /P <>BDC ET BT EMC ET 7 0 0 7 230.7317 331.9528 Tm /P <>BDC EMC /F1 1 Tf BT /P <>BDC /P <>BDC )Tj (have won more than 5,600. EMC ET /P <>BDC The total capacity is 526 seats broken down to 162 first class seats, 175 business class and 189 economy seats. EMC EMC ( )Tj (l)Tj BT ET ET /P <>BDC EMC /P <>BDC /P <>BDC ET ET 0 Tc ET /P <>BDC (132,872)Tj EMC ET EMC EMC 7 0 0 7 456.2165 441.7654 Tm (0.0111)Tj ET EMC BT /P <>BDC EMC -.02 Tc BT ( )Tj 7 0 0 7 247.7395 496.7654 Tm 7 0 0 7 37.6993 166.9528 Tm less heating from the smaller hydraulic system A. ( )Tj EMC /P <>BDC /P <>BDC BT /P <>BDC 9 0 0 9 374.2479 71.8898 Tm (10)Tj 9 0 0 9 312.9828 38.8898 Tm .151 .147 .15 rg /P <>BDC 0 Tc ET 0 Tc /P <>BDC EMC EMC (BOS-ORD)Tj 9 0 0 9 544.0105 258.8898 Tm /P <>BDC ET BT EMC 7 0 0 7 446.5009 672.7654 Tm EMC (The aircraft are examined on the basis)Tj (136)Tj 0 Tc BT /F1 1 Tf BT 7 0 0 7 141.7322 364.9528 Tm ET 0 Tc /P <>BDC EMC BT /P <>BDC BT ET ET ( )Tj ET EMC /P <>BDC 7 0 0 7 277.3936 474.9528 Tm ET /P <>BDC ET EMC /P <>BDC BT EMC 7 0 0 7 99.8582 661.7654 Tm ET ( )Tj ET ET ET ( )Tj ET /P <>BDC 7 0 0 7 82.2047 606.9528 Tm BT BT ET ( )Tj EMC -.02 Tc -.02 Tc ET EMC ET BT /P <>BDC 8 0 0 8 317.9854 771.9529 Tm EMC ET (104-112)Tj /P <>BDC EMC ET ET 0 Tc ET ET BT ET 7 0 0 7 299.0601 342.9528 Tm BT BT (178)Tj ET BT /P <>BDC /P <>BDC EMC .023 .567 .626 RG 6.5 0 0 6.5 274.6269 689.9529 Tm /P <>BDC ET /P <>BDC 9 0 0 9 77.618 82.8898 Tm 6 0 0 6 394.3996 687.9528 Tm -.02 Tc BT ( )Tj BT ET BT BT EMC 0 Tc /P <>BDC ( )Tj ET ET ET (39,732)Tj BT 7 0 0 7 518.4953 298.9528 Tm ( )Tj EMC ET 7 0 0 7 535.5029 496.7654 Tm 0 Tc /P <>BDC ( )Tj ET ( )Tj -.01 Tc /F1 1 Tf EMC EMC 7 0 0 7 440.0906 166.9528 Tm ET The analysis, however,)Tj (108 on BOS-SEA \(Seattle\); 123 on BOS-)Tj -.02 Tc all the fuel required for priming which will render it inoperative even when the /F6 1 Tf 0 Tc 9 0 0 9 112.6132 302.8898 Tm ET /P <>BDC EMC BT BT EMC BT -.02 Tc ( )Tj 9 0 0 9 232.4217 544.8898 Tm (214,730)Tj ET BT ET BT /P <>BDC BT BT EMC /P <>BDC ( )Tj 7 0 0 7 37.6993 320.9528 Tm BT BT 8 0 0 8 99.8582 771.7654 Tm EMC /P <>BDC ET BT (0.0111)Tj ET -.02 Tc /P <>BDC /P <>BDC ( )Tj BT 0 Tc EMC (376)Tj ET BT BT ( )Tj ET EMC ( )Tj BT (The specifications and weights of all)Tj EMC ET /GS1 gs 0 Tc ET /P <>BDC BT 7 0 0 7 37.6993 408.9528 Tm ( C)Tj BT -.02 Tc 0 Tc ET /P <>BDC ET EMC EMC /P <>BDC -.02 Tc (172,842)Tj /P <>BDC /P <>BDC -.01 Tc BT ET BT /P <>BDC /P <>BDC EMC ET 7 0 0 7 258.2805 496.7654 Tm 8 0 0 8 43.6039 745.9528 Tm EMC q 6.5 0 0 6.5 54.877 598.9529 Tm EMC EMC -.02 Tc -.02 Tc /P <>BDC BT EMC ( )Tj /P <>BDC On the longer sectors, however, the)Tj BT (37,653)Tj 0 Tc (A321ceo)Tj BT /P <>BDC ET BT EMC 7 0 0 7 380.2788 474.7654 Tm 9 0 0 9 394.0315 786.8898 Tm ET /P <>BDC BT endobj /P <>BDC BT ( )Tj Q .151 .147 .15 rg ( )Tj /P <>BDC BT BT BT BT /P <>BDC ET ET EMC -.02 Tc ( )Tj 0 Tc /P <>BDC BT /P <>BDC BT 0 Tc ET /P <>BDC The)Tj 7 0 0 7 141.7322 595.9528 Tm 9 0 0 9 246.595 423.8898 Tm BT ( )Tj EMC EMC -.02 Tc /P <>BDC BT /P <>BDC 7 0 0 7 230.7317 265.9528 Tm BT /P <>BDC (404)Tj ET ET 0 Tc ET (to 3.3% less efficient than the A320neo)Tj 0 Tc BT -.07 Tc ( )Tj BT (6,820)Tj ET ET (170)Tj 9 0 0 9 36.8504 137.8898 Tm )Tj ET Airbus has come to dethrone the 737 as the leader of the industry. (payload in scenario 1. /P <>BDC 9 0 0 9 394.0123 467.8898 Tm EMC EMC ( C)Tj ( )Tj ( )Tj 8 0 0 8 136.4919 591.9528 Tm EMC 7 0 0 7 554.7883 507.7654 Tm EMC BT ET /P <>BDC /P <>BDC BT 0 Tc EMC /P <>BDC /P <>BDC 7 0 0 7 54.7071 716.7654 Tm EMC BT 9 0 0 9 207.2279 511.8898 Tm -.02 Tc (0.0119)Tj 7 0 0 7 43.6039 639.9528 Tm 9 0 0 9 394.0237 170.8898 Tm /P <>BDC EMC /P <>BDC 7 0 0 7 148.0554 11.5132 Tm EMC BT 9 0 0 9 365.7772 467.8898 Tm /P <>BDC 7 0 0 7 440.3636 474.9528 Tm /P <>BDC EMC BT ET 9 0 0 9 290.9113 324.8898 Tm ( )Tj /P <>BDC EMC /P <>BDC (2,365)Tj ET EMC EMC BT -.02 Tc 6.5 0 0 6.5 222.7786 676.9529 Tm /P <>BDC EMC ET ET ET BT BT 6 0 0 6 547.0496 673.9528 Tm BT /Figure <>BDC /P <>BDC BT BT /P <>BDC EMC EMC EMC EMC BT BT Q 9 0 0 9 544.921 225.8898 Tm EMC EMC (1,272)Tj 8 0 0 8 124.845 703.9528 Tm ET /P <>BDC /P <>BDC -.02 Tc BT /P <>BDC ET The 800 is mainly used for passenger transport with its 526 seating capacity. /Artifact <>BDC BT ET BT 8 0 0 8 412.41 771.9529 Tm ET ( )Tj ET Airbus A320 Specs What is behind one of the most popular short-haul airliners? )Tj /P <>BDC ET EMC 0 Tc /P <>BDC 7 0 0 7 492.5963 738.7654 Tm 9 0 0 9 411.0097 247.8898 Tm ET /P <>BDC BT BT BT ET ( )Tj ( )Tj 7 0 0 7 241.2727 573.9528 Tm /F7 1 Tf -.02 Tc FQIS accuracy: +/- 2.0% overall ET BT /P <>BDC BT 7 0 0 7 158.74 331.7654 Tm (3,850)Tj BT /P <>BDC /P <>BDC (A321ceo versus the 737-900ER\(W\), in the)Tj BT BT EMC /P <>BDC BT 0 Tc 9 0 0 9 68.0314 302.8898 Tm ET (CFM56-7B26)Tj BT EMC EMC ( )Tj ET BT 9 0 0 9 568.6457 357.8898 Tm ET EMC EMC [(equal-siz)6.1(ed 737NG counterpar)-23(ts and A320ceo)]TJ ET 0 Tc /P <>BDC ET /GS2 gs BT ET BT BT ET [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ 0 Tc 6.5 0 0 6.5 528.5291 663.9529 Tm (types over a wide range of mission lengths)Tj EMC ET BT ET [(BOS-C)-8.1(V)18.1(G)]TJ BT /GS1 gs ET (the fuel consumption for each type over)Tj EMC /GS1 gs BT BT FQIS accuracy: +/- 3.0% ET 6 0 0 6 506.5237 757.9528 Tm ( )Tj -.02 Tc (35,112lbs)Tj EMC [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ )Tj ET /P <>BDC The A320neo in this study)Tj /P <>BDC EMC [(Engine b)6.1(ypass)]TJ 7 0 0 7 278.2756 78.9528 Tm 7 0 0 7 297.632 474.9528 Tm