( )Tj 10 0 0 10 420.16 814.1973 Tm /P <>BDC 6.5 0 0 6.5 346.1035 637.9529 Tm -.02 Tc /P <>BDC ET EMC 7 0 0 7 444.737 177.7654 Tm (39,270)Tj 6.5 0 0 6.5 549.8557 585.9529 Tm /P <>BDC 7 0 0 7 279.1575 342.9528 Tm /P <>BDC .008 Tc ET 7 0 0 7 456.4753 430.7654 Tm 0 Tc EMC 0 Tw /P <>BDC ET /P <>BDC ET BT EMC A nitrogen-enriched air EMC BT BT ( )Tj ( )Tj -.02 Tc BT /P <>BDC 36.861 533.759 518.74 271.281 re /P <>BDC ( )Tj BT /P <>BDC BT /P <>BDC 0 Tc The A320ceo and)Tj 6 0 0 6 527.699 701.9528 Tm ET EMC -.02 Tc BT ET ( )Tj 9 0 0 9 439.4008 324.8898 Tm 7 0 0 7 37.6993 419.9528 Tm ( )Tj ET 0 Tc ET EMC BT EMC ET [(E)-7.8(P)16.1(T)9(E)-13.9(MBE)-16.9(R)]TJ BT /P <>BDC ( )Tj 9 0 0 9 566.9709 126.8898 Tm 9 0 0 9 232.438 203.8898 Tm BT The controls for main tanks 1 and 2 change to aft BT /P <>BDC BT 7 0 0 7 241.2727 276.9528 Tm 10.486 7.6165 l BT ET 9 0 0 9 53.8338 269.8898 Tm (assumes that an equal number of)Tj /P <>BDC /P <>BDC 7 0 0 7 247.7395 188.7654 Tm 7 0 0 7 71.6694 738.9528 Tm 9 0 0 9 394.0123 577.8898 Tm EMC EMC [(E)-7.8(P)16.1(T)9(E)-13.9(MBE)-16.9(R)]TJ BT BT (192 seats versus 179 on the 737-9. 7 0 0 7 554.7883 683.7654 Tm /P <>BDC -.02 Tc (0.0124)Tj ( )Tj BT BT ET (In the payload 2 scenario, the fuel burn)Tj -.02 Tc /P <>BDC (MAX family. 7 0 0 7 508.4124 441.7654 Tm EMC 9 0 0 9 206.3371 731.8898 Tm EMC ET (976)Tj ET /P <>BDC /F1 1 Tf (allow a direct comparison of trip fuel burn)Tj /P <>BDC BT EMC EMC ( )Tj /P <>BDC ( )Tj 7 0 0 7 193.1059 89.9528 Tm q 1 0 0 1 508.103 86.641 cm 0 0 m (-62)Tj 8 0 0 8 315.034 760.7654 Tm allowed to run dry or be left running unsupervised. 7 0 0 7 338.6433 122.7654 Tm BT BT ET /P <>BDC (BOS, and take 10 minutes to taxi in at all)Tj EMC /P <>BDC BT EMC ET BT ( )Tj 8 0 0 8 225.1837 633.9528 Tm EMC 9 0 0 9 188.1863 170.8898 Tm EMC 7 0 0 7 158.74 232.7654 Tm /P <>BDC /P <>BDC ET /P <>BDC 9 0 0 9 169.0072 511.8898 Tm 0 Tc ET BT /P <>BDC EMC /F4 1 Tf /P <>BDC 7 0 0 7 519.3773 364.9528 Tm /P <>BDC /P <>BDC Boeing has its 737 in almost every single developed nation. ET ( )Tj 0 Tc BT ET (aircraft types: the A320ceo, A321ceo,)Tj /P <>BDC EMC ET BT ET (136)Tj ET EMC EMC (the longest sector BOS-SFO. (remain key aircraft for many operators)Tj /P <>BDC ET BT BT BT (408)Tj BT BT /P <>BDC /P <>BDC 9 0 0 9 534.7635 203.8898 Tm /P <>BDC 183,380 Litres: 47,210 US Gal. -.02 Tc /P <>BDC ET BT ( )Tj (variant used in this study is the CFM)Tj BT (445,316)Tj (375)Tj 7 0 0 7 490.5101 496.9528 Tm (the fuel burn and operating performance of)Tj BT /P <>BDC -.02 Tc 0 Tc 518.697 0 l ET ET ET ET BT ( )Tj /P <>BDC 7 0 0 7 314.6398 606.7654 Tm EMC ET For the wheels, I will give you two measurements. ( )Tj ET BT EMC BT (comparison of both block- and flight-fuel)Tj /Artifact <>BDC 9 0 0 9 53.8578 280.8898 Tm 8 0 0 8 365.7704 745.9528 Tm ET /P <>BDC EMC BT EMC 0 Tc BT /P <>BDC EMC ( )Tj /P <>BDC /P <>BDC /F5 1 Tf BT ( )Tj /P <>BDC EMC ET thank you for stopping by. ET /P <>BDC ET 7 0 0 7 82.8504 364.9528 Tm 6.5 0 0 6.5 64.6596 598.9529 Tm /P <>BDC /P <>BDC In the 90s Boeing produced 80% of components in house including the wings, fuselage and tall assemblies. ET /P <>BDC /P <>BDC ET /F1 1 Tf -.02 Tc 7 0 0 7 99.8582 628.7654 Tm BT BT BT ET BT /P <>BDC /P <>BDC ET (0.0155)Tj /P <>BDC BT BT 7 0 0 7 520.6108 705.9528 Tm EMC -.02 Tc -.02 Tc -.02 Tc ET BT /P <>BDC /P <>BDC /P <>BDC ET ET ET EMC ET (1,161)Tj EMC BT EMC (engine bypass ratio in the case of the 737)Tj 6.5 0 0 6.5 191.942 532.9529 Tm /P <>BDC ET ET ET /P <>BDC ET (4,541)Tj BT /P <>BDC EMC BT EMC /P <>BDC ET BT 7 0 0 7 403.478 485.7654 Tm ET BT ( )Tj 6.5 0 0 6.5 499.1421 722.9529 Tm EMC [(A3)24.9(20ceo v)12.9(ersus 7)-33(3)8.1(7-800 )]TJ 8 0 0 8 270.7815 771.9528 Tm /P <>BDC ( )Tj 7 0 0 7 130.1443 617.7654 Tm -.02 Tc BT EMC 0 Tc ET (150)Tj /P <>BDC 6.5 0 0 6.5 176.1172 558.9529 Tm EMC 7 0 0 7 343.2355 529.7654 Tm ET BT (significant enough that operating the)Tj BT EMC )Tj /P <>BDC ( )Tj EMC ( )Tj /P <>BDC 9 0 0 9 215.4409 379.8898 Tm /P <>BDC ( )Tj BT 7 0 0 7 294.4014 276.7654 Tm EMC -.02 Tc 7 0 0 7 294.4014 716.7654 Tm 9 0 0 9 534.2559 302.8898 Tm /P <>BDC )Tj /P <>BDC BT BT ( )Tj 9 0 0 9 411.0181 258.8898 Tm -.02 Tc 9 0 0 9 195.5727 104.8898 Tm /Artifact <>BDC 0 Tc ET ET /P <>BDC /P <>BDC -.02 Tc /P <>BDC 7 0 0 7 539.8962 716.9528 Tm 9 0 0 9 232.438 214.8898 Tm 0 Tc /P <>BDC (737-9 will have the same cabin layout and)Tj EMC (105,000lbs. ( )Tj ET ET ET BT /OC /MC4591 BDC (4,158)Tj EMC /P <>BDC BT BT ET /P <>BDC -.02 Tc 7 0 0 7 363.2711 496.9528 Tm EMC BT EMC BT EMC 0 Tc BT EMC 7 0 0 7 403.478 738.7654 Tm /P <>BDC /P <>BDC 9 0 0 9 373.4722 49.8898 Tm /P <>BDC - Modern Airliners, A New Opportunity For Hydrogen is Aviation Aeronautics, A New Opportunity For Hydrogen is Aviation - Revolution-Green, Southwest CEO Says It's Safe to Fly Again. 6.5 0 0 6.5 449.1864 611.9529 Tm (150)Tj /P <>BDC EMC EMC BT BT -.005 Tc BT EMC /P <>BDC (Since all eight aircraft types are in)Tj 56 0 obj 9 0 0 9 411.0181 247.8898 Tm [(F)43(uel burn/)]TJ /P <>BDC (404)Tj EMC BT 9 0 0 9 352.4841 313.8898 Tm ET cumulative errors it is recommended that the wings are filled once every few /P <>BDC EMC 0 Tc BT /P <>BDC ( )Tj EMC ET 7 0 0 7 258.2805 287.7654 Tm BT /P <>BDC /Artifact <>BDC ET BT ET ET /P <>BDC ( )Tj /P <>BDC /P <>BDC 7 0 0 7 537.7804 320.9528 Tm EMC (350-365)Tj ET 9 0 0 9 191.7472 379.8898 Tm ( )Tj BT BT ET /P <>BDC ET ( )Tj /P <>BDC ET EMC ( )Tj 7 0 0 7 520.6108 507.9528 Tm 0 Tc /P <>BDC BT /P <>BDC /P <>BDC -3.5781 -.0449 -2.6539 .5294 -1.6216 .5285 c 7 0 0 7 242.0225 430.9528 Tm BT [(737-900E)-33(R)]TJ BT /P <>BDC BT /P <>BDC -.01 Tc EMC ET EMC 7 0 0 7 204.0935 133.7654 Tm ET (160)Tj 0 Tc ( C)Tj 7 0 0 7 82.8504 188.9528 Tm ET /P <>BDC EMC ( )Tj ET BT BT ET 0 Tc ET (dependent on the operators internal)Tj EMC /P <>BDC EMC 9 0 0 9 542.1815 786.8898 Tm (A320ceo and A320neo in this study. EMC BT 1 i [(BOS-A)56.9(TL)]TJ /P <>BDC ET -.02 Tc EMC ET BT ET 7 0 0 7 125.6292 89.7654 Tm ET 0 Tc /P <>BDC 9 0 0 9 552.2133 291.8898 Tm ET EMC BT /P <>BDC /P <>BDC EMC 9 0 0 9 411.0181 71.8898 Tm EMC ( )Tj (163)Tj /P <>BDC The 737-9 has a)Tj BT ET /P <>BDC /P <>BDC ET /P <>BDC A series of ten tests were performed (five flight, -.02 Tc 6.5 0 0 6.5 397.5498 558.9529 Tm ( )Tj EMC /P <>BDC BT BT ET BT EMC /P <>BDC -.01 Tc EMC 6 0 0 6 540.5396 757.9528 Tm 6 0 0 6 442.408 771.9528 Tm ( )Tj ( )Tj EMC /P <>BDC ET /P <>BDC ET ( )Tj EMC /P <>BDC ET (the A320neo. ET EMC Boeing 737 800 Hainan Airlines Alan Wilson. BT /P <>BDC /P <>BDC /P <>BDC BT ET /P <>BDC ET -.01 Tc EMC /P <>BDC 8 0 0 8 136.4919 591.9528 Tm (customers better performance and lower)Tj ET ET /P <>BDC ET BT EMC 7 0 0 7 315.1859 100.7654 Tm 6.5 0 0 6.5 327.0283 598.9529 Tm ET EMC 10 0 0 10 425.05 814.1973 Tm /P <>BDC EMC BT BT (superior fuel burn per seat-mile of all)Tj (0.0109)Tj BT BT 7 0 0 7 507.7893 265.7654 Tm 7 0 0 7 99.8582 529.7654 Tm (20)Tj /P <>BDC BT EMC EMC ET EMC EMC BT -.02 Tc BT ET (800 is not as large as the difference)Tj ET EMC 9 0 0 9 36.8583 357.8898 Tm ( )Tj BT /P <>BDC Two panels control the displays one either side of the cabin. BT 9 0 0 9 191.7774 423.8898 Tm BT /P <>BDC -.02 Tc -.02 Tc 7 0 0 7 428.6112 397.9528 Tm EMC ET 9 0 0 9 394.0123 599.8898 Tm /P <>BDC BT /P <>BDC 7 0 0 7 554.7883 287.7654 Tm BT (LEAP-1B engine. 0 Tc /P <>BDC endobj ( )Tj EMC ( )Tj /P <>BDC ( )Tj BT ET .151 .147 .15 rg BT 9 0 0 9 213.294 489.8898 Tm q 1 0 0 1 53.901 797.54 cm 0 0 m EMC flightdeck (below the F/O's FMC) but they have since been removed to a (2,500)Tj /P <>BDC BT 9 0 0 9 190.2832 49.8898 Tm /P <>BDC (A320neo)Tj 9 0 0 9 215.4409 357.8898 Tm ET 0 841.89 609.449 -841.89 re 9 0 0 9 418.1167 335.8898 Tm -.02 Tc EMC /P <>BDC 0 Tc BT BT /P <>BDC BT ET BT /P <>BDC 7 0 0 7 457.0984 133.7654 Tm /F1 1 Tf EMC BT (2,730)Tj BT BT (benefits from improved propulsive)Tj /P <>BDC /P <>BDC BT EMC BT ET /P <>BDC EMC (34,650)Tj BT /P <>BDC ET /P <>BDC BT ( )Tj EMC EMC ET 9 0 0 9 232.4217 434.8898 Tm BT (I)Tj (152)Tj /P <>BDC 7 0 0 7 258.2805 595.7654 Tm (A320ceo)Tj ( )Tj EMC /P <>BDC -.02 Tc EMC BT /P <>BDC /P <>BDC /P <>BDC /P <>BDC 6.5 0 0 6.5 488.8955 532.9529 Tm BT (table, page 19\))Tj ( )Tj (A321neo)Tj EMC BT BT ( )Tj EMC to test BT /GS1 gs EMC EMC 9 0 0 9 165.1286 137.8898 Tm /P <>BDC BT BT 9 0 0 9 156.9898 269.8898 Tm -.02 Tc BT EMC 0 Tc /P <>BDC /P <>BDC endobj (20)Tj ET ET EMC 7 0 0 7 379.3969 221.7654 Tm ET BT /P <>BDC BT ET ET 7 0 0 7 508.4124 298.7654 Tm /P <>BDC BT 0 Tc EMC BT EMC BT ET BT ET (largest operating costs for any aircraft)Tj 7 0 0 7 554.7883 573.7654 Tm EMC /P <>BDC 9 0 0 9 198.8517 280.8898 Tm BT ET ET /P <>BDC BT BT /P <>BDC BT (342,312)Tj EMC 9 0 0 9 75.3887 489.8898 Tm /P <>BDC BT EMC BT BT This is why only the NG's are affected by AD 7 0 0 7 518.4953 298.9528 Tm BT ET (977)Tj (1,272)Tj /P <>BDC 9 0 0 9 232.4217 181.8898 Tm 6.5 0 0 6.5 295.373 742.9529 Tm ET 9 0 0 9 551.4604 269.8898 Tm EMC 7 0 0 7 99.8582 144.7654 Tm -.02 Tc /P <>BDC /P <>BDC ET ET /P <>BDC EMC BT 0 J 0 j .5 w 10 M [] 0 d [(P)11(ayload)]TJ ( )Tj must be determined by using the dripsticks (floatsticks For this reason, a)Tj ET BT /P <>BDC /P <>BDC 9 0 0 9 411.0181 324.8898 Tm BT ( )Tj /P <>BDC [(Engine b)6.1(ypass)]TJ BT /P <>BDC BT BT BT 7 0 0 7 428.6112 408.9528 Tm ET ET /F4 1 Tf /P <>BDC /P <>BDC EMC /P <>BDC 7 0 0 7 141.7322 375.9528 Tm ( )Tj EMC 8 0 0 8 43.6039 689.9528 Tm /P <>BDC BT q 1 0 0 1 411.023 799.878 cm 0 0 m BT EMC ET BT 8 0 0 8 99.8582 771.7654 Tm allowed for deposit of the ground-based NEA into the center wing tank (CWT). ET 7 0 0 7 204.0935 177.7654 Tm EMC EMC EMC /P <>BDC EMC ET BT BT 7 0 0 7 230.7317 419.9528 Tm ET *PUUqUef\r+vl 0 Tc EMC EMC ( )Tj BT [(BOS-C)-8.1(V)18.1(G)]TJ 6.5 0 0 6.5 549.8557 663.9529 Tm /P <>BDC 10 0 0 10 36.8504 814.1973 Tm /P <>BDC ET (longer routes. /P <>BDC (0.0108)Tj EMC BT 9 0 0 9 555.2855 478.8898 Tm /P <>BDC 0 Tc EMC BT 0 Tc 7 0 0 7 491.4046 287.9528 Tm 7 0 0 7 44.5789 463.9528 Tm BT 6.5 0 0 6.5 64.6596 572.9529 Tm ET ET EMC ET BT 9 0 0 9 232.438 335.8898 Tm ET 73 0 obj -.02 Tc EMC ( )Tj BT /P <>BDC BT /P <>BDC -.02 Tc /P <>BDC BT 6.5 0 0 6.5 54.877 650.9529 Tm /F1 1 Tf ( )Tj 7 0 0 7 196.5683 716.7654 Tm EMC /P <>BDC 9 0 0 9 215.4313 302.8898 Tm ( )Tj 9 0 0 9 347.4891 203.8898 Tm And the 800 has shown to be one of the most popular models for filling this role. [(Aircr)10(aft )]TJ 7 0 0 7 456.2165 474.7654 Tm ET (0.0132)Tj /P <>BDC BT ET ET EMC EMC (LEAP-1B. BT /P <>BDC EMC 7 0 0 7 491.4046 386.9528 Tm EMC We have rechecked with Boeing and the figure should now be up to date and correct. ET /P <>BDC BT ( )Tj ET EMC /P <>BDC 0 Tc /P <>BDC BT (over 400 MAXs, and Airbus a similar)Tj 7 0 0 7 230.7317 441.9528 Tm /P <>BDC /P <>BDC /P <>BDC ET ( )Tj /P <>BDC 9 0 0 9 394.0315 709.8898 Tm /P <>BDC /P <>BDC /P <>BDC /P <>BDC BT 7 0 0 7 299.0601 100.9528 Tm /P <>BDC /P <>BDC -.02 Tc EMC 9 0 0 9 68.3339 555.8898 Tm -.02 Tc -.02 Tc EMC /P <>BDC 7 0 0 7 247.7395 276.7654 Tm EMC EMC ( )Tj )Tj ET /P <>BDC EMC /P <>BDC ET BT /P <>BDC EMC EMC ( )Tj 9 0 0 9 79.8339 489.8898 Tm 7 0 0 7 429.157 474.9528 Tm (passenger load factor based on each types)Tj ET 9 0 0 9 411.0097 115.8898 Tm EMC BT ET ET /GS2 gs 7 0 0 7 82.8504 111.9528 Tm

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