737 800 fuel capacity pounds737 800 fuel capacity pounds

/P <>BDC ( )Tj /P <>BDC BT /P <>BDC 6.5 0 0 6.5 276.4014 650.9529 Tm ET ET ET 10 0 0 10 408.34 814.1973 Tm [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ BT 0 Tc 9 0 0 9 207.8168 445.8898 Tm BT endobj /P <>BDC 0 Tc EMC /P <>BDC 7 0 0 7 294.4014 298.7654 Tm ET 7 0 0 7 490.5101 584.9528 Tm EMC Worlds Most Popular Passenger Airplane for $ 89.1 million. ( )Tj ( )Tj EMC BT EMC 0 Tw 9 0 0 9 207.3361 115.8898 Tm EMC [(CFM L)17.1(E)-8.1(AP-1A32)]TJ (considered include fleet commonality,)Tj /P <>BDC EMC ET <>/ExtGState<>/Properties<>>> /P <>BDC 7 0 0 7 321.6356 188.9528 Tm /P <>BDC BT ( )Tj [(P)11(ayload)]TJ BT ( )Tj BT EMC EMC 7 0 0 7 316.0679 386.7654 Tm BT Digital Sunburst Fuel Gauges - Simmonds 4 Tank. BT ET ( )Tj 0 Tc 7 0 0 7 299.0601 309.9528 Tm ET BT /P <>BDC (CFM56-7B26)Tj 9 0 0 9 68.3339 544.8898 Tm (which could reduce this difference. EMC ET /P <>BDC 6 0 0 6 371.479 715.9528 Tm (136)Tj 9 0 0 9 212.5589 148.8898 Tm 9 0 0 9 568.024 148.8898 Tm ( )Tj 0 Tc EMC ( )Tj 9 0 0 9 548.1865 522.8898 Tm 6 0 0 6 389.0654 673.9528 Tm ( )Tj ET ( )Tj 7 0 0 7 380.2788 265.7654 Tm ET /P <>BDC 7 0 0 7 366.0641 694.9528 Tm ET EMC BT ( )Tj .41 .161 .508 RG ( )Tj /P <>BDC EMC (difference to an average of 2.1% over the)Tj EMC 7 0 0 7 404.101 78.7654 Tm /P <>BDC BT 0 Tc 7 0 0 7 141.7322 177.9528 Tm EMC ET BT The)Tj /P <>BDC BT /P <>BDC ( )Tj EMC EMC ET EMC ( )Tj ET 9 0 0 9 382.4508 159.8898 Tm -.02 Tc BT BT It is assumed that the aircraft in)Tj 7 0 0 7 337.9444 639.9528 Tm Airbus A340, history of a long haul airliner. (equal basis, since the number of seats will)Tj -.02 Tc BT 7 0 0 7 338.6433 298.7654 Tm BT /P <>BDC 9 0 0 9 571.1344 742.8898 Tm EMC ( )Tj /P <>BDC [(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 0 Tc (with 2,000 feet separation. ET EMC (assume that the optimum flight level could)Tj EMC (150)Tj ( )Tj EMC EMC /P <>BDC (page\))Tj ( )Tj 9 0 0 9 346.6898 280.8898 Tm /P <>BDC EMC BT EMC EMC EMC (0.0123)Tj (2.31 cents per ASM. BT EMC 7 0 0 7 444.737 177.7654 Tm 9 0 0 9 394.0157 632.8898 Tm /P <>BDC BT BT ( A)Tj BT ET BT ( )Tj /P <>BDC EMC ET /P <>BDC ET ET ET EMC (573)Tj 7 0 0 7 321.6356 166.9528 Tm ( )Tj EMC [(BOS-D)17.1(T)-11(W)]TJ /F6 1 Tf BT (. BT BT /P <>BDC ET ET ( )Tj /F1 1 Tf ET BT BT ET ET EMC Thanks for stopping by. 7 0 0 7 380.2788 507.7654 Tm ET [(737-900E)-33(R)]TJ /P <>BDC Engine size EMC 9 0 0 9 411.0097 170.8898 Tm /P <>BDC -.02 Tc /P <>BDC /P <>BDC EMC BT ET 9 0 0 9 36.8504 467.8898 Tm BT q BT 8 0 0 8 471.0755 760.9528 Tm EMC /P <>BDC (166,669)Tj 9 0 0 9 411.0097 500.8898 Tm BT ET /P <>BDC /P <>BDC 7 0 0 7 429.157 584.9528 Tm /P <>BDC /P <>BDC BT 7 0 0 7 379.3969 320.7654 Tm ( )Tj -.07 Tc EMC ET BT BT ET BT ET (1,824)Tj 56 0 0 56 419.9569 622.1944 Tm (427,890)Tj ( )Tj (2,500)Tj EMC ( )Tj 7 0 0 7 321.6356 397.9528 Tm /P <>BDC (types will only be made where unrestricted)Tj EMC /P <>BDC EMC /P <>BDC /Artifact <>BDC 9 0 0 9 68.0071 577.8898 Tm 9 0 0 9 420.5961 38.3073 Tm /F8 1 Tf ET (34,650)Tj 7 0 0 7 456.4753 639.7654 Tm ET BT BT ET /P <>BDC ( )Tj 9 0 0 9 411.0097 82.8898 Tm /F7 1 Tf 0 Tc BT (483)Tj /P <>BDC EMC -.02 Tc ET BT ( )Tj /P <>BDC ET (setting. /P <>BDC ( )Tj ET /P <>BDC EMC ET BT 7 0 0 7 279.1575 232.9528 Tm 7 0 0 7 37.8848 452.9528 Tm EMC EMC ( )Tj ( )Tj /P <>BDC EMC BT BT ET EMC EMC 8 0 0 8 189.0627 717.9528 Tm 0 J 0 j 5 w 10 M [] 0 d /P <>BDC EMC ET EMC ET EMC EMC EMC /P <>BDC 7 0 0 7 554.7883 397.7654 Tm EMC BT ( )Tj ( )Tj /P <>BDC 7 0 0 7 199.5784 397.7654 Tm 0 Tc .41 .161 .508 rg /P <>BDC /P <>BDC 0 Tc EMC EMC (68.3 inches and a bypass ratio of up to)Tj (I)Tj 9 0 0 9 385.5399 115.8898 Tm EMC ET EMC EMC ET /P <>BDC 7 0 0 7 456.2165 342.7654 Tm BT (A321neo)Tj /P <>BDC ET /P <>BDC /P <>BDC /P <>BDC I cannot find any more information anywhere, but if I stumble across it, I will be sure to post it! EMC BT (132,872)Tj ( )Tj 9 0 0 9 215.4409 423.8898 Tm ( )Tj ( )Tj 6.5 0 0 6.5 499.1812 663.9529 Tm /P <>BDC /P <>BDC 9 0 0 9 548.4747 115.8898 Tm BT (1,547)Tj 0 Tc ( )Tj ( )Tj ( )Tj /P <>BDC 9 0 0 9 75.273 467.8898 Tm -.02 Tc ( )Tj ( )Tj 10 0 0 10 425.05 814.1973 Tm ET 7 0 0 7 258.2805 89.7654 Tm /P <>BDC BT )Tj ET ( )Tj ET (350-365)Tj BT BT BT 7 0 0 7 439.2087 221.9528 Tm /P <>BDC /P <>BDC /GS2 gs ( )Tj ET BT /P <>BDC ET /P <>BDC BT BT BT EMC ET EMC BT 6 0 0 6 426.8235 743.9528 Tm ET (remain competitive aircraft. ET /P <>BDC EMC 6.5 0 0 6.5 432.488 624.9529 Tm 7 0 0 7 182.5706 177.9528 Tm BT ( )Tj EMC /P <>BDC EMC /P <>BDC /P <>BDC ET ET EMC EMC /P <>BDC ET ET 0 Tc ( )Tj EMC EMC q ET /P <>BDC BT BT 9 0 0 9 376.579 434.8898 Tm ET ( )Tj /P <>BDC /P <>BDC BT 7 0 0 7 535.5029 78.7654 Tm ET EMC ( )Tj /P <>BDC BT BT BT /P <>BDC (150)Tj 9 0 0 9 394.0315 159.8898 Tm ET ( )Tj BT ( A)Tj ET -.02 Tc 7 0 0 7 82.8504 342.9528 Tm BT /F6 1 Tf EMC /P <>BDC BT I am looking forward to your responses. BT ET 0 Tc EMC BT BT BT ET BT ET EMC (382,736)Tj -.02 Tc ET (seating, while both the economy-plus and)Tj BT EMC ( )Tj ET ( )Tj BT BT /P <>BDC ET 7 0 0 7 82.8504 320.9528 Tm ET (was planned with fuel to reach a defined)Tj EMC EMC EMC BT ( )Tj ( )Tj ( )Tj /P <>BDC ( )Tj 7 0 0 7 445.7203 11.5129 Tm (1,668)Tj 9 0 0 9 411.0181 467.8898 Tm (277,248)Tj 7 0 0 7 554.7883 122.7654 Tm /P <>BDC BT 7 0 0 7 321.6356 122.9528 Tm EMC 0 Tc 9 0 0 9 411.0181 445.8898 Tm ( )Tj /P <>BDC BT /P <>BDC ET /P <>BDC 0 Tc /P <>BDC BT 5 0 0 5 484.5872 11.5129 Tm /P <>BDC 6 0 0 6 143.5527 673.9528 Tm /P <>BDC 6.5 0 0 6.5 549.8557 611.9529 Tm (CFM56-7B27B3)Tj ( )Tj ET ET ( )Tj EMC EMC ET ET (CFM56-7B27B3)Tj EMC ET EMC EMC EMC -.02 Tc /P <>BDC EMC EMC -.2034 -.7911 -.1202 -.4766 0 0 c ET BT EMC /F7 1 Tf BT BT 8 0 0 8 187.3427 703.9528 Tm /P <>BDC /P <>BDC ( )Tj ( )Tj BT ET 7 0 0 7 490.5101 485.9528 Tm (3,341)Tj BT 0 Tc BT 7 0 0 7 158.74 67.7654 Tm BT BT /P <>BDC -.02 Tc [(737 M)-8.1(A)-24.9(X-9)]TJ ( )Tj /P <>BDC 0 Tc ET /F1 1 Tf /P <>BDC /P <>BDC /P <>BDC /P <>BDC ( )Tj 7 0 0 7 118.104 562.7654 Tm ET EMC ET EMC 7 0 0 7 247.7395 518.7654 Tm BT BT EMC EMC BT 9 0 0 9 76.2256 412.8898 Tm EMC EMC ( )Tj /P <>BDC EMC /P <>BDC BT /P <>BDC /P <>BDC EMC W n EMC EMC ( )Tj /P <>BDC 7 0 0 7 37.6993 364.9528 Tm BT 9 0 0 9 543.767 93.8898 Tm ( )Tj (A321ceo)Tj /P <>BDC ET ( )Tj ET -.02 Tc ET (34,650)Tj /P <>BDC /P <>BDC BT /P <>BDC q 1 0 0 1 394.016 758.971 cm 0 0 m 9 0 0 9 36.8504 390.8898 Tm ( )Tj The Boeing 737-800 is a twin-engined short-to-medium-range narrowbody airliner with a capacity of maximum 189 passengers produced by the American manufacturer Boeing Commercial Airplanes. BT /P <>BDC ( )Tj 9 0 0 9 53.8578 357.8898 Tm EMC ( )Tj 9 0 0 9 383.3617 346.8898 Tm /P <>BDC 7 0 0 7 354.6933 265.7654 Tm 0 Tc ET .7 -.5345 .9114 -1.2305 y 0 Tc EMC 36.85 824.882 572.599 17.008 re /P <>BDC 6.5 0 0 6.5 347.0393 565.9529 Tm /P <>BDC These sectors)Tj (252-264)Tj 9 0 0 9 366.7762 390.8898 Tm /P <>BDC BT ET ET ET BT ( )Tj /P <>BDC 0 Tc /P <>BDC 7 0 0 7 294.4014 617.7654 Tm BT -.02 Tc 9 0 0 9 370.9507 38.8898 Tm ET /F4 1 Tf (737-8)Tj ( )Tj ET 9 0 0 9 182.0482 379.8898 Tm -.0001 Tw W n ET (comprehensive comparison of the aircraft)Tj BT (aircraft an economic advantage in terms of)Tj EMC -.02 Tc BT BT EMC ( )Tj BT 0 Tc /P <>BDC (37,653)Tj BT 26.0355 0 TD ET 6.5 0 0 6.5 432.488 558.9529 Tm 7 0 0 7 427.7291 177.9528 Tm BT /P <>BDC /P <>BDC 7 0 0 7 445.619 463.7654 Tm /P <>BDC 7 0 0 7 386.4701 408.9528 Tm BT EMC 7 0 0 7 380.2788 199.7654 Tm 0 Tc EMC ET (\(see table, this)Tj -.02 Tc ( )Tj 7 0 0 7 508.4124 199.7654 Tm -.02 Tc 9 0 0 9 232.4217 82.8898 Tm ET ET 0 Tc 0 Tc /OC /MC1663 BDC (418)Tj ET BT -1.2026 -5.3154 -.8984 -5.2108 -.5848 -4.9925 c EMC (34,650)Tj /P <>BDC ( )Tj ET ET ET /P <>BDC ET ET ET ( )Tj /P <>BDC (carriers. )Tj EMC BT ET ET ( )Tj 7 0 0 7 554.7883 276.7654 Tm BT BT /P <>BDC (the CFM56-5B with thrust ratings of)Tj ET /P <>BDC (with a thrust rating of 26,000lbs, an intake)Tj /GS2 gs ET ET /P <>BDC 7 0 0 7 404.101 243.7654 Tm W n ( )Tj )Tj EMC EMC ET (34,650)Tj ET /P <>BDC BT EMC EMC BT EMC ET /P <>BDC (172,992)Tj /P <>BDC /P <>BDC /P <>BDC 7 0 0 7 363.2711 386.9528 Tm BT 9 0 0 9 394.0315 247.8898 Tm 9 0 0 9 411.0097 291.8898 Tm 7 0 0 7 95.225 11.5132 Tm EMC 7 0 0 7 320.7537 78.9528 Tm 9 0 0 9 53.8338 335.8898 Tm ET ( )Tj <>/ExtGState<>/Properties<>>> /P <>BDC ( )Tj (34,650)Tj /P <>BDC EMC BT ( )Tj 0 Tc 9 0 0 9 394.0157 203.8898 Tm 9 0 0 9 53.8582 269.8898 Tm EMC (increase in engine efficiency to offer)Tj BT 8 0 0 8 297.7943 771.9528 Tm EMC EMC 8 0 0 8 394.0237 38.8898 Tm 6 0 0 6 246.6462 743.9528 Tm 7 0 0 7 539.8962 573.9528 Tm 0 Tc ET -.02 Tc ( )Tj EMC 0 Tc BT BT EMC /P <>BDC ET 0 Tc ET ET [(E)-7.8(P)16.1(T)9(E)-13.9(MBE)-16.9(R)]TJ ET BT /P <>BDC (737-800W)Tj ET 36.85 824.882 572.599 17.008 re 7 0 0 7 99.8582 133.7654 Tm (170)Tj /P <>BDC Fully loaded, the jet can fly up to 3,159 miles without refueling. 7 0 0 7 204.0935 628.7654 Tm /P <>BDC 7 0 0 7 337.4684 672.9528 Tm BT -.02 Tc EMC 6.5 0 0 6.5 471.1051 742.9529 Tm ET EMC BT 7 0 0 7 469.2222 11.5129 Tm BT ET EMC ET BT ET EMC /P <>BDC BT /P <>BDC /P <>BDC 7 0 0 7 429.4931 122.9528 Tm ET 0 Tc /P <>BDC ET ( )Tj EMC 7 0 0 7 404.101 133.7654 Tm 0 Tc ET Q EMC ( )Tj -.02 Tc (150)Tj EMC /P <>BDC /P <>BDC EMC /P <>BDC [(737-900E)-33(R)]TJ /P <>BDC EMC /P <>BDC BT -4.5143 -2.2339 -4.3751 -1.5784 -4.0786 -1.0086 c /P <>BDC 0 Tc EMC BT /P <>BDC BT ET 6.5 0 0 6.5 330.4406 565.9529 Tm ET 8 0 0 8 136.4919 661.9528 Tm ( )Tj ( )Tj 6 0 0 6 547.0496 701.9528 Tm Q EMC ( )Tj 0 Tc BT 169 0 obj (0.0141)Tj 6.5 0 0 6.5 499.597 558.9529 Tm /P <>BDC BT EMC 0 841.89 609.449 -841.89 re (152)Tj EMC (34,650)Tj /P <>BDC ET ET 7 0 0 7 338.3085 265.9528 Tm ET )Tj /P <>BDC ET 9 0 0 9 394.0157 599.8898 Tm 7 0 0 7 294.4014 265.7654 Tm 0 Tc decrease the oxygen content to a level where the air volume (ullage) will not ( )Tj BT BT EMC EMC It is notably more stretched than and based off of the original 400. /P <>BDC (36,960)Tj ET The massive 800 variant is powered by two 2Snecma / CFM56-7B27 underwing turbofans putting out a respectable 27,300 pound-force. /P <>BDC EMC /P <>BDC EMC 7 0 0 7 430.039 573.9528 Tm If there is more you want to learn about this airliner, please visit: Boeing 737 Home, Boeing 737 Interior, Boeing 737 Order Book, Boeing 737 History, Boeing 737 Assembly and Boeing 737 Max. (21)Tj EMC (The 737-9 has an 11.2% to 12.7%)Tj BT BT /P <>BDC EMC ET 0 Tc /P <>BDC EMC /P <>BDC ET ET [(T)92(axi in time - mins)]TJ 0 Tc ET ( )Tj EMC 9 0 0 9 385.2246 148.8898 Tm 9 0 0 9 356.2376 236.8898 Tm (342,448)Tj /P <>BDC (or the CFM LEAP-1A32, rated at)Tj /P <>BDC -.9858 .528 -.35 .3166 0 0 c A unique variant in the 737 family is the 737 Convertible which is both a passenger and cargo airliner. 0 Tc ET /P <>BDC -.02 Tc ET /P <>BDC ET /P <>BDC ( )Tj 9 0 0 9 554.8713 709.8898 Tm /P <>BDC BT 7 0 0 7 36.8504 11.5129 Tm BT (same maximum fuel capacity, had no)Tj (900ER\(W\) are the only aircraft in the)Tj 0 Tc (831)Tj 7 0 0 7 337.6855 386.9528 Tm -.01 Tc ( )Tj ET (1,351)Tj ET EMC (5,338)Tj 6.5 0 0 6.5 176.1172 585.9529 Tm ET ET /P <>BDC ET /F6 1 Tf /P <>BDC ET ET EMC /P <>BDC .151 .147 .15 rg The NG series are prone to "Upper Wing Surface /P <>BDC ( )Tj (0.0194)Tj /P <>BDC EMC 0 Tc 9 0 0 9 332.7796 225.8898 Tm ET EMC /P <>BDC EMC EMC ET EMC EMC 0 Tc -.02 Tc /P <>BDC 7 0 0 7 445.619 122.7654 Tm BT BT ET 9 0 0 9 411.0181 192.8898 Tm ( )Tj <>/XObject<>/ExtGState<>/Properties<>>> /P <>BDC (3,535)Tj /P <>BDC ET EMC BT 0 Tc ( )Tj /P <>BDC ( )Tj ET BT BT /P <>BDC ET 53.858 511.715 518.74 293.325 re BT 0 Tc EMC ET EMC BT EMC (407)Tj 8 0 0 8 457.2727 760.7654 Tm ET /P <>BDC EMC BT ET EMC ET 0 Tc ET 7 0 0 7 519.3773 265.9528 Tm EMC /Artifact <>BDC EMC ( C)Tj Neither the 737-800 nor the 737-8)Tj 9 0 0 9 394.0315 269.8898 Tm /P <>BDC 7 0 0 7 37.0536 595.9528 Tm /P <>BDC 9 0 0 9 408.1968 324.8898 Tm ET ET BT (0.0124)Tj EMC ( )Tj [(BOS-Y)-49.1(VR)]TJ 0 Tc /F6 1 Tf /P <>BDC [(UG)-17.1(U)-8(S)8.1(T)]TJ /P <>BDC EMC ET /P <>BDC -.02 Tc ET ET ET BT EMC 0 Tc (A321ceo versus the 737-900ER\(W\), in the)Tj EMC BT 0 Tc ( )Tj 0 Tc (between the A320ceo and A320neo. /P <>BDC ET EMC [(OM)8(M)-13(E)-25(R)7(C)8(E)]TJ 7 0 0 7 196.5683 221.7654 Tm /P <>BDC ET /P <>BDC /P <>BDC .151 .147 .15 rg ET BT ET 7 0 0 7 537.7804 210.9528 Tm -.02 Tc -.02 Tc BT /P <>BDC 7 0 0 7 230.7317 683.9528 Tm ET ET EMC (component is stated )Tj 9 0 0 9 548.4937 71.8898 Tm ( )Tj 9 0 0 9 194.5132 38.8898 Tm /GS2 gs 53.85 621.704 518.723 183.336 re /F6 1 Tf -.02 Tc /P <>BDC EMC ( )Tj 0 Tc 7 0 0 7 387.0932 177.9528 Tm ET 7 0 0 7 141.7322 518.9528 Tm EMC BT BT EMC ET ET -.015 Tc ET ET EMC BT /P <>BDC 0 Tc /P <>BDC /P <>BDC BT (310,080)Tj (56,901)Tj BT ( )Tj /P <>BDC /P <>BDC ( )Tj BT -.01 Tc 0 Tc 6.5 0 0 6.5 279.814 585.9529 Tm (39,270)Tj /P <>BDC 9 0 0 9 552.4684 71.8898 Tm ( )Tj ET /P <>BDC BT 0 Tc 9 0 0 9 179.5372 313.8898 Tm )Tj EMC (346,456)Tj /P <>BDC ET /P <>BDC (0.0135)Tj ( )Tj 9 0 0 9 556.2501 181.8898 Tm 7 0 0 7 429.157 606.9528 Tm /P <>BDC BT ET /P <>BDC (comparison. EMC 9 0 0 9 411.0097 93.8898 Tm EMC /P <>BDC (1,272)Tj ( )Tj 7 0 0 7 521.4928 463.9528 Tm BT /F1 1 Tf 9 0 0 9 232.438 434.8898 Tm [(v)21(ariant)]TJ ( )Tj ET 9 0 0 9 394.0315 544.8898 Tm (- mins)Tj EMC 7 0 0 7 379.3969 144.7654 Tm (CFM56-5B4/P)Tj 7 0 0 7 507.7893 507.7654 Tm 9 0 0 9 189.8423 467.8898 Tm EMC BT ET ET 6 0 0 6 61.517 673.9528 Tm /P <>BDC 9 0 0 9 229.6141 390.8898 Tm /P <>BDC ET (0.0158)Tj 7 0 0 7 364.1531 133.9528 Tm /P <>BDC 7 0 0 7 279.1575 683.9528 Tm ET EMC /P <>BDC EMC 0 841.89 609.449 -841.89 re /P <>BDC ET ET BT BT EMC -.01 Tc ( )Tj 6.5 0 0 6.5 448.257 650.9529 Tm /F6 1 Tf ( )Tj ET 8 0 0 8 338.6644 760.9528 Tm (9,451)Tj /P <>BDC 7 0 0 7 37.0536 474.9528 Tm 1 i EMC The A320neo in this study)Tj EMC -.02 Tc BT -.02 Tc /P <>BDC 0 Tc ET EMC /P <>BDC EMC 9 0 0 9 115.2588 214.8898 Tm /P <>BDC )Tj EMC (0.0126)Tj EMC EMC EMC ( )Tj ET /P <>BDC (190,800)Tj 0 Tc BT /P <>BDC /F6 1 Tf ( )Tj ET ( )Tj /P <>BDC 9 0 0 9 515.9449 654.8898 Tm /P <>BDC ET BT ET (in ASMs between the eight aircraft types. ET ET /P <>BDC 0 Tc BT /P <>BDC 7 0 0 7 258.2805 617.7654 Tm EMC ET ET 0 Tc 6 0 0 6 61.517 687.9528 Tm /P <>BDC ET /P <>BDC BT ET EMC (The fuel cost per ASM improves with)Tj BT /P <>BDC /P <>BDC 7 0 0 7 537.7804 89.9528 Tm BT BT (150)Tj ( )Tj /GS2 gs ET /P <>BDC 7 0 0 7 297.632 694.9528 Tm ET 9 0 0 9 565.1979 478.8898 Tm ET 6 0 0 6 507.6099 659.9528 Tm ( )Tj BT (3,069)Tj ET /P <>BDC BT ( )Tj EMC 0 Tc ( )Tj )Tj EMC EMC /P <>BDC -.02 Tc BT EMC ( )Tj ET /P <>BDC [(Aircr)10(aft type)]TJ 7 0 0 7 457.0984 562.7654 Tm /P <>BDC 9 0 0 9 563.0415 775.8898 Tm EMC 7 0 0 7 125.6292 738.7654 Tm /P <>BDC EMC EMC BT ( )Tj BT ET /P <>BDC /P <>BDC ET ET /Artifact <>BDC 9 0 0 9 344.8161 214.8898 Tm ET /P <>BDC 0 Tc BT ET ET EMC (34,650)Tj ET effective for a large portion of the flight, or until aircraft descent. ( )Tj /P <>BDC BT ET /P <>BDC ( )Tj BT /P <>BDC BT (39,270)Tj 7 0 0 7 158.74 584.7654 Tm /P <>BDC ET ET BT -.02 Tc EMC .661 .752 .896 rg EMC ( )Tj EMC ET -.02 Tc BT /P <>BDC 6.5 0 0 6.5 64.6596 611.9529 Tm ET ( )Tj BT -.02 Tc ( )Tj (The A320neo family and 737 MAX)Tj /P <>BDC /P <>BDC EMC ET ET /P <>BDC 7 0 0 7 199.5784 639.7654 Tm -.02 Tc (1,089)Tj BT ET (CFM56-7B26)Tj ( )Tj ET EMC BT ET 0 Tc /P <>BDC -.02 Tc EMC ET 6 0 0 6 434.151 715.9528 Tm Whatever the reason, we hope that both Boeing and the F.A.A. /P <>BDC BT BT 6.5 0 0 6.5 499.597 624.9529 Tm ET EMC ET 9 0 0 9 126.1392 522.8898 Tm While the MAX 10 is still yet to be certified, the legacy of the -900ER lives on, and the type will likely continue to fly for many more years before retirement. /P <>BDC 9 0 0 9 53.8578 324.8898 Tm 7 0 0 7 294.4014 683.7654 Tm ET (170)Tj EMC The initial concept included podded engines and a T-tail as seen on the 727. /P <>BDC BT 9 0 0 9 193.6853 357.8898 Tm ( )Tj -.02 Tc BBJ3 has 35% more cabin space than the BBJ and 11% more cabin space than the BBJ 2. 7 0 0 7 204.0935 331.7654 Tm 15 w ET (482)Tj /P <>BDC EMC 7 0 0 7 116.3631 11.5132 Tm 6.5 0 0 6.5 244.4599 676.9529 Tm 0 Tc EMC ( )Tj 7 0 0 7 354.7351 683.7654 Tm BT BT ET ET EMC ( )Tj EMC /P <>BDC 7 0 0 7 125.6292 188.7654 Tm ET BT 0 Tc .014984 841.89 609.45 -841.89 re 7 0 0 7 355.3163 210.7654 Tm 0 Tc /P <>BDC BT 7 0 0 7 338.6433 309.7654 Tm ( )Tj /P <>BDC ET 6.5 0 0 6.5 486.1525 722.9529 Tm 7 0 0 7 387.619 430.9528 Tm ( )Tj BT EMC ET /P <>BDC EMC 7 0 0 7 491.4046 188.9528 Tm /F6 1 Tf BT 7 0 0 7 258.2805 518.7654 Tm ( )Tj ( )Tj 0 Tc 7 0 0 7 82.2047 518.9528 Tm ET EMC /P <>BDC 7 0 0 7 294.4014 727.7654 Tm BT ET ET BT [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ (A320neos aircraft interior design and)Tj /P <>BDC (380-396)Tj EMC Hi Peter, /P <>BDC ET 7 0 0 7 337.6855 441.9528 Tm (10)Tj /P <>BDC -.02 Tc ( )Tj -.015 Tc /P <>BDC ( )Tj BT pack on and this should be considered in the fuel calculations if expecting a long turnaround or BT [(UG)-17.1(U)-8(S)8.1(T)]TJ /P <>BDC ET ( )Tj )Tj ET BT /P <>BDC 7 0 0 7 536.3849 309.7654 Tm ET (second payload scenario using the 85%)Tj /P <>BDC ET 9 0 0 9 539.8684 280.8898 Tm -.01 Tc 6.5 0 0 6.5 192.111 735.9529 Tm 5 0 0 5 92.725 11.5132 Tm 0 Tc 7 0 0 7 445.7203 11.5129 Tm ET ET EMC BT ( )Tj -.02 Tc BT ( )Tj /P <>BDC EMC BT BT 9 0 0 9 552.2133 291.8898 Tm -.02 Tc BT /P <>BDC EMC ( )Tj BT 0 Tc 9 0 0 9 186.0353 291.8898 Tm EMC ET (420)Tj EMC BT 6 0 0 6 61.517 645.9528 Tm -.02 Tc BT /P <>BDC EMC (39,270)Tj 7 0 0 7 355.5753 562.7654 Tm BT ET BT EMC ET BT EMC ( )Tj W n -.02 Tc /P <>BDC EMC (passenger seat capacity as the older models)Tj /P <>BDC 9 0 0 9 232.438 170.8898 Tm /P <>BDC ET BT ( )Tj 6 0 0 6 326.0708 673.9528 Tm BT /P <>BDC 9 0 0 9 276.2863 115.8898 Tm ( )Tj 7 0 0 7 535.5029 540.7654 Tm ET BT /P <>BDC 0 Tc 7 0 0 7 439.9995 661.9528 Tm ET 7 0 0 7 230.6618 430.9528 Tm 7 0 0 7 230.7317 617.9528 Tm /GS1 gs 0 Tc 0 J 0 j 5 w 10 M [] 0 d /P <>BDC EMC .023 .567 .626 rg /P <>BDC (to higher bypass ratios provide better)Tj BT Since development and production Boeing has built 10,574 737-800s. EMC EMC BT 0 Tc BT ET /P <>BDC ET BT ET 7 0 0 7 101.0963 386.9528 Tm (ASM is 0.09 cents better for the A321neo. ET (737-800 is more efficient with up to a)Tj Thank you. (35,112)Tj ET EMC (273,600)Tj /P <>BDC EMC ET EMC -.02 Tc /GS1 gs BT 9 0 0 9 229.6064 335.8898 Tm 7 0 0 7 520.6108 540.9528 Tm (A321ceo)Tj BT 6.5 0 0 6.5 489.7146 611.9529 Tm 0 Tc /P <>BDC BT EMC (operator. 9 0 0 9 371.6638 247.8898 Tm allow for a measurement of fuel tank inerting and heating during the /P <>BDC -.02 Tc EMC ET BT BT (170)Tj 9 0 0 9 274.8953 313.8898 Tm ET BT BT EMC BT (of fuel against time-related costs. /P <>BDC ( )Tj 7 0 0 7 179.5605 122.9528 Tm /GS2 gs EMC 7 0 0 7 114.6416 595.9528 Tm EMC Boeing 747 8 Intercontinental and Freighter History. BT 9 0 0 9 232.4408 775.8898 Tm 6.5 0 0 6.5 191.8316 585.9529 Tm /P <>BDC (35,112)Tj 7 0 0 7 343.2355 507.7654 Tm ET EMC ET 7 0 0 7 204.0935 78.7654 Tm EMC 0 Tc /P <>BDC 7 0 0 7 354.6933 386.7654 Tm BT W n BT ( )Tj EMC ET ( )Tj EMC This narrow body jet airliner had first rolled out on June 30, 1997 and shortly after was had its first test flight with he pilot Jim McRoberts in the cockpit. /P <>BDC BT ET BT ( )Tj /P <>BDC EMC EMC (and 737-9. BT /P <>BDC /P <>BDC ET ( )Tj 0 Tc /P <>BDC BT /P <>BDC /P <>BDC BT ET 0 Tc BT ET /P <>BDC ET 6.5 0 0 6.5 426.4819 689.9529 Tm ET -.02 Tc 56 0 0 56 36.8606 622.1944 Tm ( )Tj EMC EMC 9 0 0 9 394.0315 60.8898 Tm ( )Tj /P <>BDC ET (allow a direct comparison of trip fuel burn)Tj /P <>BDC (A)Tj )Tj 9 0 0 9 232.4217 280.8898 Tm ( )Tj 7 0 0 7 457.0984 331.7654 Tm /P <>BDC 1 i (34,650)Tj 13 0 0 13 215.433 137.8898 Tm -.02 Tc ET BT 9 0 0 9 487.056 434.8898 Tm (uses one of the 11 certified weight variants. 7 0 0 7 37.0536 584.9528 Tm BT /P <>BDC /P <>BDC ( )Tj 6 0 0 6 55.0668 743.9528 Tm 7 0 0 7 108.6215 67.9528 Tm ET 789 0 obj ET /P <>BDC 0 Tc 7 0 0 7 37.6993 265.9528 Tm BT -.02 Tc EMC BT 7 0 0 7 108.6215 265.9528 Tm /OC /MC860 BDC /P <>BDC ET EMC EMC BT (5,183)Tj BT BT EMC (113,152)Tj (0.0122)Tj ET 7 0 0 7 387.0932 144.9528 Tm BT ( )Tj /P <>BDC 10 0 0 10 48.9263 771.9528 Tm -.02 Tc EMC ET ET EMC BT ET 9 0 0 9 204.483 104.8898 Tm 7 0 0 7 247.7395 606.7654 Tm EMC /P <>BDC EMC ET ( )Tj (47,000)Tj BT EMC 0 Tc ET Q EMC /P <>BDC It has a maximum range of 10,140km. ( )Tj (\(see table,)Tj 505.331 89.873 m [(AS)29.1(M)21(s)]TJ EMC EMC 7 0 0 7 337.7614 111.7654 Tm (The A320neo has a 0.55-0.69 cents per)Tj BT ET 0 Tc (409,650)Tj BT 9 0 0 9 197.8317 379.8898 Tm EMC BT -.02 Tc 7 0 0 7 125.6292 243.7654 Tm BT The service ceiling is 41,000 feet. 0 Tc /P <>BDC 9 0 0 9 232.438 456.8898 Tm EMC /P <>BDC 9 0 0 9 362.6813 357.8898 Tm ET 9 0 0 9 211.8218 533.8898 Tm The pumps should be switched off and considered inop until they can be #"""#'''''''''' /P <>BDC 7 0 0 7 344.1175 584.7654 Tm ET /P <>BDC ET /F1 1 Tf 7 0 0 7 158.74 276.7654 Tm /P <>BDC Q EMC BT -.02 Tc ET 0 Tc [(737-900E)-33(R)]TJ EMC BT /P <>BDC /P <>BDC EMC ET 0 Tc ET 6 0 0 6 208.1569 743.9528 Tm 0 Tc FQIS accuracy: +/- 2.0% overall (A321neo:)Tj ET (375)Tj ( )Tj 7 0 0 7 539.8962 485.9528 Tm /P <>BDC /P <>BDC 9 0 0 9 394.0123 335.8898 Tm /P <>BDC /P <>BDC /P <>BDC 9 0 0 9 394.0123 49.8898 Tm EMC 8 0 0 8 43.6039 605.9528 Tm EMC ET 0 Tc /P <>BDC /P <>BDC EMC 7 0 0 7 474.5665 430.9528 Tm BT 7 0 0 7 539.9176 11.5129 Tm 6.5 0 0 6.5 244.2585 598.9529 Tm ( )Tj ( )Tj (1,138)Tj EMC 7 0 0 7 321.6356 419.9528 Tm EMC (CFM56-5B3/P)Tj EMC BT BT -.02 Tc ET ET /P <>BDC ( )Tj /P <>BDC /P <>BDC 7 0 0 7 107.1165 276.9528 Tm 9 0 0 9 394.0157 478.8898 Tm 9 0 0 9 36.8504 280.8898 Tm EMC /P <>BDC 7 0 0 7 429.157 540.9528 Tm EMC BT 9 0 0 9 36.8504 335.8898 Tm -.01 Tc -.02 Tc )Tj 7 0 0 7 403.478 364.7654 Tm ET (37,653)Tj 7 0 0 7 507.7893 166.7654 Tm [(UG)-17.1(U)-8(S)8.1(T)]TJ /P <>BDC /P <>BDC ET EMC EMC -.01 Tc /P <>BDC /P <>BDC /P <>BDC ( )Tj 8 0 0 8 64.6596 760.9529 Tm ET ( )Tj (ASM of 0.55 to 0.88 cents per ASM)Tj BT ( )Tj -.02 Tc The 737-800 has a maximum fuel capacity of 6,875 gallons, which it carries in fuel tanks in its wings, as seen here, and in a fuel tank located underneath the passenger cabin's midsection. 9 0 0 9 373.4379 324.8898 Tm 0 Tc ( )Tj /P <>BDC 6.5 0 0 6.5 448.7448 742.9529 Tm /GS1 gs

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