(newer aircraft types will have the same)Tj /P <>BDC next aircraft ET ET ET . )Tj ( )Tj BT EMC 6 0 0 6 433.7979 771.9528 Tm ET ( )Tj /P <>BDC 0 Tc EMC ET BT BT 7 0 0 7 182.5706 177.9528 Tm 7 0 0 7 337.6855 232.9528 Tm .151 .147 .15 rg ET EMC BT EMC ET 7 0 0 7 230.7317 507.9528 Tm ET ET BT 0 Tc EMC /P <>BDC EMC EMC ET ( )Tj 6.5 0 0 6.5 332.6961 735.9529 Tm ET ET (The fuel cost per ASM improves with)Tj EMC BT BT EMC (737-800W)Tj <>stream /P <>BDC -.02 Tc EMC BT EMC /P <>BDC ET EMC /P <>BDC -.02 Tc BT (A320ceo)Tj ET /P <>BDC EMC EMC 7 0 0 7 99.8582 111.7654 Tm 7 0 0 7 381.1608 584.7654 Tm ET 0 Tc EMC EMC BT [(737-900E)-33(R)]TJ /P <>BDC 0 Tw BT EMC BT ET EMC BT BT EMC .001 Tc ( )Tj The world's largest commercial airplane the Antanov AN-225 can carry over 98,000Gal/375,000 liters of fuel compared to a Beechcraft 1900D commuter airplane which carries 665Gal/2,520 liters. /P <>BDC BT 7 0 0 7 427.7291 210.9528 Tm ET ET ET ( )Tj 0 Tc ET BT ET EMC 0 Tc BT 7 0 0 7 294.4014 232.7654 Tm ET 7 0 0 7 492.5963 738.7654 Tm ET /P <>BDC /P <>BDC /P <>BDC BT /P <>BDC ( )Tj 6.5 0 0 6.5 324.4345 702.9529 Tm 7 0 0 7 491.392 727.9528 Tm /F7 1 Tf EMC -.02 Tc ( N)Tj EMC /OC /MC1974 BDC /P <>BDC /P <>BDC BT 7 0 0 7 294.4014 430.7654 Tm BT 0 Tc ( )Tj ET 9 0 0 9 53.8578 412.8898 Tm /P <>BDC 0 Tc EMC 8 0 0 8 412.41 771.9529 Tm 7 0 0 7 294.4014 287.7654 Tm 7 0 0 7 362.3891 298.9528 Tm -.02 Tc fuel pumps were running in high ambient temperatures with empty or almost empty EMC ET /P <>BDC EMC EMC ET ET -.02 Tc /P <>BDC /P <>BDC 7 0 0 7 473.8245 397.9528 Tm ET /P <>BDC ET EMC -.01 Tc EMC ET ET EMC ( )Tj /P <>BDC BT .0161 Tc -.02 Tc /P <>BDC ( )Tj 7 0 0 7 403.478 727.7654 Tm EMC -.02 Tc EMC /GS2 gs 6.5 0 0 6.5 557.8578 742.9529 Tm (number of seats and ASMs will give an)Tj EMC (A320ceo)Tj 7 0 0 7 535.5029 474.7654 Tm /Artifact <>BDC (20)Tj 9 0 0 9 190.1653 456.8898 Tm EMC BT Q BT (A320ceo)Tj ( )Tj BT 6 0 0 6 226.9834 715.9528 Tm BT /P <>BDC ET EMC EMC 6.5 0 0 6.5 499.597 558.9529 Tm ( )Tj 13 0 0 13 215.4313 115.8898 Tm BT BT 7 0 0 7 258.2805 518.7654 Tm BT EMC 7 0 0 7 258.2805 595.7654 Tm EMC ET (0.0286)Tj BT BT ET ET EMC BT EMC EMC /P <>BDC BT /P <>BDC ET 7 0 0 7 241.2727 463.9528 Tm BT BT BT 7 0 0 7 491.7142 232.7654 Tm 0 Tc ET 9 0 0 9 332.7796 225.8898 Tm EMC BT ET 7 0 0 7 474.7064 441.9528 Tm EMC 7 0 0 7 247.7395 375.7654 Tm 108 lbs (49 kgs) to the 737-800 basic MEW. BT EMC ET 0 Tc ET The flight)Tj BT BT ET BT 432 0 obj EMC ( )Tj BT ET EMC ( )Tj 0 Tc EMC [(BOS-SE)-13.9(A)]TJ BT BT EMC /F6 1 Tf 0 Tc It sounds like you have a bit of a project on your hands. /P <>BDC EMC BT 7 0 0 7 338.5674 166.9528 Tm EMC ( )Tj ET /P <>BDC BT /P <>BDC /P <>BDC EMC EMC ET ET EMC 9 0 0 9 411.0097 555.8898 Tm EMC /GS1 gs Since development and production Boeing has built 10,574 737-800s. EMC BT /P <>BDC ET BT BT ( )Tj 7 0 0 7 508.4124 375.7654 Tm /P <>BDC Boeing 737 Max, a new generation of this highly successful City Jet. ( )Tj BT 7 0 0 7 490.5101 584.9528 Tm BT 7 0 0 7 404.101 89.7654 Tm (187,700lbs, an MLW of 157,300lbs and a)Tj 10 0 0 10 407.56 814.1973 Tm EMC ( )Tj ( )Tj ET The Boeing 737-800 is an example of an average sized airplane. /P <>BDC BT EMC EMC 7 0 0 7 241.5317 199.9528 Tm (104)Tj ( )Tj EMC 6.5 0 0 6.5 172.7047 650.9529 Tm BT (379)Tj /P <>BDC /P <>BDC 7 0 0 7 539.8962 683.9528 Tm 0 Tc 7 0 0 7 130.1443 518.7654 Tm (A321ceo, in contrast to the A320neo over)Tj (payload. /P <>BDC (989)Tj -.02 Tc EMC /P <>BDC /P <>BDC /P <>BDC ET 0 Tc /P <>BDC EMC -.02 Tc -.02 Tc ET 9 0 0 9 547.3786 71.8898 Tm EMC ET /P <>BDC The cabin layout used for)Tj /P <>BDC ( )Tj BT /P <>BDC -.02 Tc /F4 1 Tf 9 0 0 9 232.438 225.8898 Tm 8 0 0 8 545.8474 786.8898 Tm ET /P <>BDC EMC BT (2,731)Tj /P <>BDC 7 0 0 7 279.1575 397.9528 Tm /P <>BDC ET /P <>BDC EMC Centre tank pumps EMC BT BT ET (planned for each aircraft type. EMC ET ( )Tj EMC EMC 7 0 0 7 247.7395 518.7654 Tm This makes it more challenging to)Tj (31,416)Tj ET /P <>BDC 0 Tc /P <>BDC EMC 7 0 0 7 279.1575 705.9528 Tm /P <>BDC BT EMC ET .41 .161 .508 rg Even an empty tank has some unusable fuel /P <>BDC (5,350)Tj BT 9 0 0 9 518.0203 170.8898 Tm /P <>BDC /P <>BDC ET ET ( )Tj 7 0 0 7 518.4953 287.9528 Tm 7 0 0 7 387.0159 584.9528 Tm /P <>BDC ET EMC BT EMC (O)Tj 1 g W n 6.5 0 0 6.5 347.0329 532.9529 Tm ET 0 Tc /P <>BDC ( )Tj BT 6.5 0 0 6.5 331.0061 722.9529 Tm 9 0 0 9 43.6039 794.2914 Tm (32,000lbs of thrust, a fan diameter of 78)Tj ET BT EMC BT ET BT ET EMC BT /P <>BDC ( )Tj 0 Tc EMC ( )Tj (A321neo)Tj ( )Tj 6.5 0 0 6.5 480.5169 565.9529 Tm BT 7 0 0 7 457.1753 727.7654 Tm BT (economy seating by 12 seats when)Tj /P <>BDC BT ET ET ( )Tj 0 Tc ( )Tj EMC ( )Tj 6.5 0 0 6.5 499.8375 545.9529 Tm ( )Tj /F8 1 Tf /P <>BDC ET BT BT 6.5 0 0 6.5 280.6329 545.9529 Tm 7 0 0 7 37.5838 441.9528 Tm BT ET (158)Tj BT The service ceiling is 41,000 feet. -.02 Tc ET ET EMC ET BT -.01 Tc 0 Tc ET (The A321neo has a lower fuel burn)Tj BT /P <>BDC BT /P <>BDC /P <>BDC .151 .147 .15 rg EMC (65,552)Tj EMC 9 0 0 9 552.2133 291.8898 Tm BT EMC /P <>BDC /P <>BDC 7 0 0 7 491.4046 188.9528 Tm -.02 Tc 7 0 0 7 141.7322 683.9528 Tm EMC BT EMC /P <>BDC /P <>BDC BT 9 0 0 9 528.0345 511.8898 Tm ET BT BT EMC 0 Tc EMC EMC BT (BOS-MIA)Tj ET BT -.02 Tc 9 0 0 9 554.8713 709.8898 Tm 9 0 0 9 326.8538 60.8898 Tm )Tj EMC /P <>BDC BT [(BOS-L)-31(A)-24.9(X)]TJ BT BT EMC BT (In this comparison, the A321neo)Tj /P <>BDC 7 0 0 7 54.7071 309.7654 Tm EMC 0 Tc BT /P <>BDC (483)Tj BT ( )Tj EMC (0.0160)Tj /P <>BDC ET 0 Tc 7 0 0 7 241.5317 529.9528 Tm ET BT 7 0 0 7 54.7071 111.7654 Tm -.02 Tc EMC 6.5 0 0 6.5 435.6469 722.9529 Tm -.02 Tc /P <>BDC [(AS)29(M)21(s)]TJ -.02 Tc BT 7 0 0 7 535.5029 738.7654 Tm ET 0 Tc /P <>BDC ET /F2 1 Tf EMC 7 0 0 7 82.8504 441.9528 Tm ET EMC BT 8 0 0 8 394.0237 71.8898 Tm 7 0 0 7 82.8504 89.9528 Tm EMC ET EMC 9 0 0 9 180.5261 423.8898 Tm ET BT 7 0 0 7 314.6398 683.7654 Tm ( )Tj Fuel temp is taken from main tank 1 because this will be the coldest as it has /GS1 gs 7 0 0 7 403.478 408.7654 Tm BT (. BT (different available options, and gives the)Tj (170)Tj /P <>BDC BT ET 7 0 0 7 247.7395 276.7654 Tm BT 1 i Main tanks smaller at 3900kg each but centre tank much larger giving total fuel capacity of 20,800kg. EMC /P <>BDC 7 0 0 7 380.2788 408.7654 Tm BT BT /P <>BDC /P <>BDC 6.5 0 0 6.5 549.8557 611.9529 Tm ET /P <>BDC -.02 Tc /P <>BDC ET ( )Tj -2.5306 -6.3496 -3.213 -6.0519 -3.7399 -5.4283 c EMC /P <>BDC q EMC ( )Tj EMC 0 Tc ET 6 0 0 6 547.0496 673.9528 Tm ET 7 0 0 7 204.0935 529.7654 Tm ( )Tj ET 6.5 0 0 6.5 499.4541 735.9529 Tm ( )Tj ( )Tj ET (The A320 and the 737 families will)Tj (capacity has been configured as the same)Tj EMC BT BT /P <>BDC 6 0 0 6 286.5632 771.9528 Tm BT BT EMC 7 0 0 7 204.0935 111.7654 Tm BT (1,824)Tj The Honeywell NGS was certified by the FAA on 21 Feb 2006 after over 1000hrs flight testing on two 737-NGs. (considered include fleet commonality,)Tj 0 Tc ET BT /P <>BDC 9 0 0 9 215.433 214.8898 Tm ( )Tj BT /P <>BDC ET (Flight time - mins)Tj 10 0 0 10 36.8504 814.1973 Tm ( )Tj ET /P <>BDC ( )Tj BT ( )Tj (900ER\(W\) has a 4.3% lower fuel burn)Tj /P <>BDC 7 0 0 7 37.6993 188.9528 Tm ET 6 0 0 6 403.6028 743.9528 Tm BT (CFM56-5B4/P)Tj BT ( )Tj ET 0 Tc ( )Tj 7 0 0 7 536.3849 562.7654 Tm 7 0 0 7 439.7405 606.9528 Tm BT BT EMC /P <>BDC EMC ET /P <>BDC BT 7 0 0 7 109.3921 430.9528 Tm EMC ET BT ET BT BT BT /P <>BDC 9 0 0 9 68.0314 302.8898 Tm BT EMC ET BT ( )Tj BT /P <>BDC 0 Tc ET /P <>BDC ET BT /GS2 gs /GS2 gs BT ET 0 Tc BT 0 Tc /P <>BDC ET BT BT ET /P <>BDC ET 7 0 0 7 354.6933 639.7654 Tm /P <>BDC BT ET ( )Tj /P <>BDC ( )Tj ET ET ET ( )Tj ET ( )Tj EMC /P <>BDC ET BT EMC It sports its powerful crew and passenger carrying abilities elegantly as it takes flight. 6.5 0 0 6.5 499.1812 702.9529 Tm ET 7 0 0 7 321.6356 419.9528 Tm 0 Tc ET BT ET /P <>BDC (CFM56-7B26 engine on the heavier weight)Tj ET ET BT ET 9 0 0 9 417.7488 511.8898 Tm ( )Tj ET EMC BT BT (charges combined with the time-related)Tj ET EMC ET 7 0 0 7 520.6108 474.9528 Tm 9 0 0 9 232.4408 764.8898 Tm (0.0133)Tj /P <>BDC ET 7 0 0 7 258.2805 694.7654 Tm ( )Tj (the defined LRC speed, this has resulted in)Tj /P <>BDC EMC ET (2,933)Tj BT /P <>BDC BT 7 0 0 7 508.4124 518.7654 Tm BT ( )Tj 6.5 0 0 6.5 233.8677 611.9529 Tm /P <>BDC /P <>BDC 9 0 0 9 394.0315 786.8898 Tm 9 0 0 9 411.0097 434.8898 Tm /P <>BDC EMC /P <>BDC ( )Tj EMC ( )Tj 9 0 0 9 215.4313 302.8898 Tm ET BT ( )Tj BT -.02 Tc 7 0 0 7 37.0536 694.9528 Tm /P <>BDC BT BT BT /P <>BDC EMC ET ( )Tj EMC 9 0 0 9 562.507 203.8898 Tm The Boeing 737-800 variant has as mentioned 27300 pound-force delivered by two turbo fans. ET /P <>BDC It works by transferring fuel from the aux 9 0 0 9 380.2477 247.8898 Tm (against the 737-800 is interesting. ET /P <>BDC EMC 8 0 0 8 74.9636 577.9528 Tm /F1 1 Tf ( )Tj EMC BT /P <>BDC EMC EMC /P <>BDC ET EMC 0 Tc ET /P <>BDC ( )Tj EMC /F1 1 Tf EMC EMC /P <>BDC EMC BT ( )Tj EMC (The A320ceo is payload-restricted to)Tj BT BT /P <>BDC ET ET ( )Tj /P <>BDC 7 0 0 7 490.5101 606.9528 Tm /P <>BDC EMC 7 0 0 7 187.0858 727.9528 Tm /P <>BDC /P <>BDC 7 0 0 7 496.3063 705.7654 Tm 7 0 0 7 321.6356 320.9528 Tm /P <>BDC ET 7 0 0 7 187.0858 562.9528 Tm ET /P <>BDC ET 9 0 0 9 394.0315 269.8898 Tm /P <>BDC f ET (206,132lbs, an MLW of 171,500lbs, and)Tj 9 0 0 9 197.1772 82.8898 Tm ET EMC /P <>BDC BBJ Aux fuel panel located on Capt's & F/O's main % BT 0 Tc /P <>BDC /P <>BDC EMC ET /P <>BDC ( )Tj 8 0 0 8 365.7704 745.9528 Tm BT ET [(SS)-9.1(U)8(E)]TJ EMC BT BT BT BT ( )Tj 6.5 0 0 6.5 433.3069 545.9529 Tm /P <>BDC BT BT /P <>BDC EMC EMC EMC /P <>BDC BT 7 0 0 7 294.4014 529.7654 Tm ( )Tj (evaluation both taxi-out and taxi-in were)Tj )Tj 9 0 0 9 347.6589 478.8898 Tm 6.5 0 0 6.5 397.0428 532.9529 Tm 0 Tc EMC ET endobj BT EMC BT (efficiency and so lower fuel burn. 7 0 0 7 299.0601 221.9528 Tm BT 7 0 0 7 440.3636 474.9528 Tm 9 0 0 9 551.4604 269.8898 Tm 7 0 0 7 108.6215 738.9528 Tm /P <>BDC ET BT EMC EMC EMC EMC BT BT ET 7 0 0 7 87.8179 144.7654 Tm EMC BT /P <>BDC - Simmonds, Digital Fuel Quantity Indicator Error Codes (37,653)Tj /P <>BDC 7 0 0 7 241.5317 705.9528 Tm 9 0 0 9 190.3643 368.8898 Tm /P <>BDC .151 .147 .15 rg /P <>BDC EMC /P <>BDC ET ET BT -.02 Tc /P <>BDC BT BT BT /P <>BDC BT EMC 7 0 0 7 187.0858 507.9528 Tm 7 0 0 7 130.1443 122.7654 Tm EMC /P <>BDC BT /GS2 gs BT ET EMC ET ET ( )Tj [(D)12.9(A)-8.1(L/36)]TJ /P <>BDC EMC BT ET ET ET (977)Tj BT BT ET ( )Tj /P <>BDC ( 2021)Tj 2002-19-52 which requires the crew to maintain certain minimum fuel EMC 7 0 0 7 118.104 364.7654 Tm 7 0 0 7 37.6993 100.9528 Tm -.02 Tc BT EMC /F1 1 Tf BT 7 0 0 7 445.619 584.7654 Tm 7 0 0 7 491.7142 276.7654 Tm ( )Tj EMC EMC 8 0 0 8 136.4919 633.9528 Tm 9 0 0 9 212.3652 775.8898 Tm /P <>BDC 0 Tc ET ET 5.25 0 0 5.25 64.5461 11.5129 Tm BT ET 5.25 0 0 5.25 100.8225 11.5132 Tm ET EMC EMC ET (into service in 2023. 6 0 0 6 184.9964 757.9528 Tm -.02 Tc /P <>BDC ET ( )Tj The fuel was fed /P <>BDC BT EMC ET EMC EMC EMC ET (977)Tj /P <>BDC BT /P <>BDC EMC /P <>BDC /P <>BDC 7 0 0 7 403.478 221.7654 Tm ( )Tj ( )Tj 7 0 0 7 326.2278 661.9528 Tm EMC 0 Tc EMC ET BT ET (124,650)Tj ET /P <>BDC EMC [(737 M)-8.1(A)-24.9(X-8:)]TJ ( )Tj 0 Tc EMC 6.5 0 0 6.5 397.1339 676.9529 Tm ( )Tj EMC BT ET (25,160)Tj BT /P <>BDC EMC ET ET /Artifact <>BDC EMC ( )Tj /P <>BDC ET EMC EMC EMC endobj /P <>BDC BT 0 Tc EMC (passenger payload. EMC EMC /P <>BDC /P <>BDC (The A321neo is offered to airlines with)Tj EMC /P <>BDC BT ET /P <>BDC 9 0 0 9 408.1854 159.8898 Tm BT EMC /P <>BDC EMC BT EMC /P <>BDC /P <>BDC /P <>BDC BT /P <>BDC ET EMC /P <>BDC ( )Tj (page 21\))Tj BT EMC EMC ( )Tj EMC EMC ( )Tj -.02 Tc EMC ET /P <>BDC /P <>BDC 0 Tc BT .023 .567 .626 rg /P <>BDC 8 0 0 8 38.4438 619.9528 Tm EMC 9 0 0 9 232.4217 357.8898 Tm h 7 0 0 7 107.1165 276.9528 Tm ET ET 7 0 0 7 539.9176 11.5129 Tm q 1 0 0 1 394.024 91.644 cm 0 0 m ( )Tj ET BT EMC BT ET /P <>BDC BT 7 0 0 7 179.5605 518.9528 Tm BT EMC BT /P <>BDC ET ET ET /P <>BDC /P <>BDC <> ET /P <>BDC The CFM56-5B4/P is rated)Tj EMC 7 0 0 7 299.0601 276.9528 Tm EMC 7 0 0 7 381.1608 562.7654 Tm BT EMC ET ET ( )Tj ET BT BT (A320neo:)Tj ET EMC /P <>BDC EMC ET EMC 7 0 0 7 108.6215 540.9528 Tm BT These sectors)Tj BT 7 0 0 7 294.4014 496.7654 Tm 0 Tc One carrier)Tj ( )Tj )Tj BT ( )Tj /P <>BDC (105)Tj /P <>BDC BT /P <>BDC /P <>BDC /P <>BDC /P <>BDC /P <>BDC 7 0 0 7 344.1175 617.7654 Tm ET 6.5 0 0 6.5 387.561 611.9529 Tm EMC EMC /P <>BDC the years. ET 6.5 0 0 6.5 279.814 558.9529 Tm ET /OC /MC200 BDC BT ET ( )Tj 7 0 0 7 247.7395 595.7654 Tm EMC BT /P <>BDC /P <>BDC 7 0 0 7 258.2805 727.7654 Tm ( )Tj ET BT 7 0 0 7 444.737 166.7654 Tm 0 Tc ET 6 0 0 6 466.3124 715.9528 Tm 0 Tc (105)Tj EMC (which could reduce this difference. (The fuel burn improvement on the)Tj ( )Tj ET /P <>BDC ET BT EMC BT /P <>BDC ET EMC BT ET EMC /F1 1 Tf /P <>BDC 7 0 0 7 258.2805 342.7654 Tm EMC 7 0 0 7 294.4014 221.7654 Tm 7 0 0 7 439.2087 111.9528 Tm ET /P <>BDC BT /P <>BDC ET (3,535)Tj BT BT -.9858 .528 -.35 .3166 0 0 c EMC /P <>BDC [(OM)8(M)-13(E)-25(R)7(C)8(E)]TJ /P <>BDC EMC ET /P <>BDC ET /P <>BDC EMC BT BT EMC BT BT BT The relative high)Tj BT f /F6 1 Tf /P <>BDC 7 0 0 7 508.4124 540.7654 Tm ET /P <>BDC /P <>BDC 9 0 0 9 386.3055 687.8898 Tm /F6 1 Tf /P <>BDC /P <>BDC ET BT 9 0 0 9 544.921 225.8898 Tm -.02 Tc EMC /P <>BDC ( 2021)Tj 0 Tc EMC (91,300)Tj 10 0 0 10 425.05 814.1973 Tm /P <>BDC 0 841.89 609.449 -841.89 re BT EMC ET ET (375)Tj ET q 1 0 0 1 215.441 458.878 cm 0 0 m EMC /P <>BDC BT /P <>BDC 7 0 0 7 230.7317 397.9528 Tm 7 0 0 7 59.2108 11.5129 Tm BT (increase in seat numbers a newer type)Tj /P <>BDC (carried - lbs)Tj -.9038 -.6598 -1.2447 -.5357 -1.6041 -.5355 c (376)Tj ET /P <>BDC ( )Tj /P <>BDC 7 0 0 7 258.2805 617.7654 Tm BT ET BT 9 0 0 9 382.6146 368.8898 Tm BT 0 Tc ( )Tj /P <>BDC ( )Tj /P <>BDC /P <>BDC BT ET BT /P <>BDC BT EMC ET ( )Tj BT ET BT 7 0 0 7 279.1575 628.9528 Tm 7 0 0 7 354.6933 441.7654 Tm ( C)Tj BT ()Tj EMC 9 0 0 9 53.8578 82.8898 Tm 0 Tc 0 Tc 7 0 0 7 554.7883 738.7654 Tm ET 9 0 0 9 232.4217 258.8898 Tm -.02 Tc /P <>BDC ET EMC BT BT 6 0 0 6 339.7639 757.9528 Tm EMC /P <>BDC ET 9 0 0 9 36.8504 203.8898 Tm ( )Tj /P <>BDC ET ET /P <>BDC /P <>BDC /P <>BDC (Engine)Tj 9 0 0 9 53.8338 115.8898 Tm BT ( )Tj /P <>BDC BT 9 0 0 9 232.438 302.8898 Tm BT BT (1,272)Tj 9 0 0 9 565.9277 60.8898 Tm ( )Tj (10)Tj EMC BT ( )Tj ( )Tj EMC ET ET BT EMC ET ( )Tj 9 0 0 9 53.8582 511.8898 Tm 9 0 0 9 411.0097 115.8898 Tm 7 0 0 7 241.5317 133.9528 Tm BT ET EMC BT BT EMC BT EMC BT ET BT 7 0 0 7 554.7883 419.7654 Tm 7 0 0 7 387.0932 111.9528 Tm ET BT ( )Tj ET ET BT ET /P <>BDC ( )Tj 9 0 0 9 363.4443 390.8898 Tm ( )Tj /P <>BDC BT 9 0 0 9 425.1967 775.8898 Tm (150)Tj ET 9 0 0 9 349.1188 500.8898 Tm ET ET BT BT 7 0 0 7 535.5029 617.7654 Tm EMC EMC /P <>BDC EMC ET /F4 1 Tf BT ( )Tj BT EMC 0 Tc EMC (737-8 has a 0.8-3.0% higher trip fuel burn than)Tj EMC 7 0 0 7 54.7071 89.7654 Tm EMC EMC EMC EMC ET ( )Tj BT EMC ET 7 0 0 7 294.4014 386.7654 Tm /P <>BDC (study has been configured with the same)Tj /P <>BDC BT EMC ( )Tj EMC ET 0 Tc What are the Specs of the Airbus A380 Super Jumbo? BT -.02 Tc ET ET 7 0 0 7 473.8245 122.9528 Tm /P <>BDC /P <>BDC EMC ( )Tj (lower fuel burn compared to the 737-)Tj 304.725 420.96 m (portion of the flight in the cruise phase,)Tj ET 7 0 0 7 337.6855 210.9528 Tm 0 Tc 7 0 0 7 125.6292 639.7654 Tm Classics could 8 0 0 8 43.6039 703.9528 Tm BT BT 0 Tc BT BT ET EMC 0 Tc /P <>BDC EMC BT /P <>BDC /OC /MC199 BDC 0 Tc What is the History behind the Airbus A380 Super Jumbo? 7 0 0 7 490.7815 364.9528 Tm In reality, most models will operate in a combination of classes. 9 0 0 9 126.1392 522.8898 Tm (66,096)Tj /P <>BDC /P <>BDC EMC 6 0 0 6 271.9128 729.9528 Tm ET EMC 0 Tc 9 0 0 9 411.0097 379.8898 Tm EMC EMC (The overflight and airport charges are)Tj ET EMC BT BT ET BT ET BT EMC EMC /P <>BDC BT 7 0 0 7 429.4931 122.9528 Tm BT EMC BT EMC BT 0 Tc /GS1 gs (slimmer galleys, increased passenger)Tj EMC [(AIRL)8.1(INE & AIR)7.1(CRAF)-12.9(T)18.1( OPERA)56.9(T)-8.1(ION)-13.9(S)]TJ ET ET EMC /P <>BDC (124,650)Tj /P <>BDC EMC BT EMC EMC (35,112)Tj /P <>BDC ( )Tj EMC EMC ( )Tj 9 0 0 9 215.433 423.8898 Tm 9 0 0 9 526.8993 643.8898 Tm ET EMC /P <>BDC BT 9 0 0 9 190.9763 38.8898 Tm 9 0 0 9 381.9109 456.8898 Tm 9 0 0 9 53.8578 247.8898 Tm (1,272)Tj EMC [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ 0 Tc 9 0 0 9 394.0315 797.8898 Tm ( )Tj 28.5749 0 TD 0 Tc /F1 1 Tf BT 9 0 0 9 386.9059 280.8898 Tm /F4 1 Tf (operational factors that also have to be)Tj EMC /P <>BDC ET ET /P <>BDC -.02 Tc /P <>BDC BT EMC ET 6.5 0 0 6.5 346.9224 585.9529 Tm EMC /P <>BDC /P <>BDC 7 0 0 7 163.8846 11.5132 Tm ET ET /P <>BDC 5 0 0 5 484.5872 11.5129 Tm ET BT EMC ET ( )Tj ET 7 0 0 7 37.5838 254.9528 Tm 0 Tc /P <>BDC 7 0 0 7 82.8504 408.9528 Tm ET (737-800W)Tj 6 0 0 6 339.6853 659.9528 Tm EMC -.02 Tc /P <>BDC BT ET ET /P <>BDC EMC BT 0 Tc BT ET 7 0 0 7 82.2047 518.9528 Tm EMC EMC EMC 0 Tc EMC BT 7 0 0 7 519.3773 221.9528 Tm ET /P <>BDC 7 0 0 7 543.7693 11.5132 Tm BT 517.252 90.783 l /P <>BDC ET /P <>BDC BT BT BT EMC 7 0 0 7 429.157 463.9528 Tm ET BT ( )Tj /F1 1 Tf 13 0 0 13 319.14 445.8898 Tm BT EMC BT EMC (0.0126)Tj ET BT 0 Tc BT 7 0 0 7 37.0536 716.9528 Tm BT EMC BT 0 Tc -.01 Tc ET EMC BT /P <>BDC EMC BT 7 0 0 7 354.6933 485.7654 Tm EMC /P <>BDC BT 9 0 0 9 182.8313 346.8898 Tm BT Delta Air Lines received the first Next-Gen 737 model with this brake package, a . 8 0 0 8 76.6837 661.9528 Tm EMC ET ( )Tj (190-199)Tj ET BT EMC /P <>BDC /P <>BDC ET (288)Tj /P <>BDC ET ET 7 0 0 7 99.8582 738.7654 Tm BT ET (of fuel against time-related costs. -.02 Tc ()Tj BT /P <>BDC 0 Tc EMC 0 Tc EMC EMC EMC 9 0 0 9 425.183 346.8898 Tm /P <>BDC BT ET EMC 0 Tc (passenger load factor based on each types)Tj -.02 Tc BT /P <>BDC (377,550)Tj ET ( )Tj BT /P <>BDC EMC EMC 5.25 0 0 5.25 465.7151 11.5129 Tm 8 0 0 8 124.845 633.9528 Tm ( )Tj ET /P <>BDC BT 9 0 0 9 232.438 456.8898 Tm EMC BT EMC 7 0 0 7 124.1242 496.7654 Tm /P <>BDC /P <>BDC BT EMC EMC ET EMC BT ( )Tj EMC BT 9 0 0 9 394.0237 225.8898 Tm ET /P <>BDC EMC (39,270)Tj /P <>BDC EMC EMC 0 Tc (20)Tj /P <>BDC )Tj EMC ( )Tj 9 0 0 9 214.7728 247.8898 Tm /P <>BDC 7 0 0 7 379.3969 331.7654 Tm ( )Tj 9 0 0 9 545.8646 522.8898 Tm /P <>BDC -.02 Tc EMC EMC EMC 8 0 0 8 314.3535 675.9528 Tm (constraints, the 737 MAX has a smaller)Tj /P <>BDC /P <>BDC BT 9 0 0 9 394.0315 687.8898 Tm BT wiring in tanks, proximity to hot air-conditioning or pneumatic systems, etc. BT BT (1,272)Tj /P <>BDC ET Cheers Peter. 7 0 0 7 554.7883 133.7654 Tm BT 9 0 0 9 394.0123 269.8898 Tm Q ET -.02 Tc /P <>BDC ET 7 0 0 7 473.8245 309.9528 Tm ET BT /P <>BDC EMC ( )Tj BT ET /F6 1 Tf (1,202)Tj ( )Tj /P <>BDC 6 0 0 6 403.4411 757.9528 Tm BT /P <>BDC /P <>BDC ET ( )Tj -.02 Tc EMC BT BT BT .0081 Tc ET For a 737-800 with 162 passengers on a 1000 NM trip, it's 96 mpg per passenger, or 0.593 mpg for the whole plane. /P <>BDC 0 Tc ET EMC BT BT ET /P <>BDC 7 0 0 7 118.104 562.7654 Tm ET EMC EMC /P <>BDC 0 Tc There are no pumps in the aux fuel system. /OC /MC4769 BDC 9 0 0 9 68.0071 412.8898 Tm (737-8)Tj BT ET 5.25 0 0 5.25 492.6848 11.5129 Tm 0 Tc 13 0 0 13 355.5757 115.8898 Tm EMC ET ET [(F)43(uel burn/)]TJ /P <>BDC ET .151 .147 .15 rg BT /F6 1 Tf 0 Tc 9 0 0 9 533.576 236.8898 Tm ET EMC /P <>BDC /P <>BDC [(BOS-L)-31(A)-24.9(X)]TJ EMC W n EMC ET ET EMC BT /P <>BDC EMC /P <>BDC /P <>BDC -.02 Tc 6.5 0 0 6.5 225.3721 585.9529 Tm EMC /P <>BDC ET /P <>BDC (104-112)Tj BT BT /P <>BDC ET /P <>BDC /P <>BDC BT /P <>BDC 0 Tc /P <>BDC /P <>BDC ( )Tj BT .151 .147 .15 rg ET EMC /P <>BDC ET 9 0 0 9 408.2047 676.8898 Tm EMC BT EMC ET /P <>BDC BT /P <>BDC ET EMC 9 0 0 9 165.1286 137.8898 Tm ET /GS1 gs (132,872)Tj -.02 Tc BT 0 Tc 7 0 0 7 456.2165 342.7654 Tm Q /GS2 gs BT EMC 9 0 0 9 394.0315 709.8898 Tm BT EMC 7 0 0 7 554.7883 716.7654 Tm 6 0 0 6 496.2633 673.9528 Tm /F7 1 Tf 7 0 0 7 99.8582 595.7654 Tm BT 0 Tc 8 0 0 8 314.3535 717.9528 Tm BT 9 0 0 9 529.8783 621.8898 Tm 8 0 0 8 225.1837 745.9528 Tm [(CFM L)17.1(E)-8.1(AP-1A32)]TJ
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