0 Tc 7 0 0 7 508.4124 177.7654 Tm ET 0 Tc ( )Tj EMC 6 0 0 6 527.699 673.9528 Tm ET EMC EMC -.02 Tc /P <>BDC (31,416)Tj /P <>BDC /P <>BDC 7 0 0 7 343.2355 540.7654 Tm ET /P <>BDC EMC EMC ET BT (capacity and potentially improved)Tj /P <>BDC (1A26-powered aircraft that is used in this)Tj /P <>BDC ET [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ endstream EMC (scheduled times planned by the carrier may)Tj 0 J 0 j .5 w 10 M [] 0 d /P <>BDC ET EMC (342,448)Tj /P <>BDC ( )Tj ET ET 7 0 0 7 469.2222 11.5129 Tm BT BT ET 858 0 obj EMC /P <>BDC /P <>BDC /P <>BDC (assumes that an equal number of)Tj BT /P <>BDC EMC (increases to 0.22 to 0.29 cents or 8.7%)Tj /P <>BDC -.02 Tc ( )Tj 7 0 0 7 258.2805 298.7654 Tm 9 0 0 9 36.8504 280.8898 Tm capacitors in the tanks with fuel acting as the dielectric. 0 Tc /P <>BDC -.02 Tc BT ( )Tj ET EMC /P <>BDC BT ( )Tj (0.0139)Tj /P <>BDC 8 0 0 8 136.4919 703.9528 Tm ET BT .151 .147 .15 rg EMC EMC (orders, while the 737-800 and 737-900ER)Tj EMC 9 0 0 9 183.8303 324.8898 Tm ET (to higher bypass ratios provide better)Tj 9 0 0 9 232.438 434.8898 Tm /P <>BDC ET ET 8 0 0 8 339.6345 760.7654 Tm 9 0 0 9 383.9197 412.8898 Tm BT /P <>BDC ( )Tj ET ET EMC .964 .834 .406 rg [(AS)29(M)]TJ 7 0 0 7 326.2278 529.9528 Tm EMC 7 0 0 7 230.7317 408.9528 Tm 7 0 0 7 536.3849 595.7654 Tm -.01 Tc /Artifact <>BDC 0 Tc (2,732)Tj EMC BT BT -.02 Tc 7 0 0 7 294.4014 287.7654 Tm 9 0 0 9 198.2937 126.8898 Tm /P <>BDC /P <>BDC ET BT BT /P <>BDC ET BT /P <>BDC ET /P <>BDC Q BT ET 0 Tc BT EMC /P <>BDC ( )Tj ET (passengers. /Artifact <>BDC 9 0 0 9 137.7566 49.8898 Tm ET BT ET ET /P <>BDC /P <>BDC ET 7 0 0 7 297.632 683.9528 Tm 0 Tc ( )Tj /P <>BDC 7 0 0 7 404.101 320.7654 Tm /P <>BDC 9 0 0 9 394.0315 412.8898 Tm /P <>BDC (20)Tj BT /P <>BDC EMC ET ( )Tj -.02 Tc EMC -.01 Tc BT EMC EMC BT EMC -.02 Tc 9 0 0 9 36.8504 324.8898 Tm BT ( )Tj ET (offering: the 737NG with the CFM56-7B;)Tj EMC BT BT EMC EMC EMC ET /GS1 gs BT -.02 Tc ET EMC ET EMC BT ET 0 Tc 7 0 0 7 429.157 562.9528 Tm BT 9 0 0 9 232.438 445.8898 Tm ET 7 0 0 7 230.7317 628.9528 Tm EMC /P <>BDC /P <>BDC 8 0 0 8 225.1837 675.9528 Tm 7 0 0 7 473.8245 364.9528 Tm 7 0 0 7 99.8582 573.7654 Tm EMC /P <>BDC 0 Tc )Tj -.02 Tc 6.5 0 0 6.5 191.942 532.9529 Tm ( )Tj /P <>BDC BT ( )Tj EMC 6 0 0 6 504.5564 771.9528 Tm BT /P <>BDC ET ET ( )Tj -.02 Tc 0 Tc /P <>BDC 7 0 0 7 247.7395 309.7654 Tm EMC ET BT 9 0 0 9 394.0157 555.8898 Tm /P <>BDC ET /P <>BDC )]TJ /P <>BDC 7 0 0 7 158.74 320.7654 Tm 7 0 0 7 337.4684 694.9528 Tm ET EMC BT EMC (A321ceo)Tj 9 0 0 9 551.4604 269.8898 Tm BT EMC BT EMC 7 0 0 7 379.3969 78.7654 Tm ( )Tj EMC ( )Tj 13 0 0 13 530.7245 434.8898 Tm BT ET ET BT /P <>BDC [(AIR)7.1(CRAF)-12.9(T)18.1( P)30(A)52(YL)32(O)6.1(ADS IN )21(T)-11(W)25.9(O C)13.9(OMP)30(ARISON SCENARIOS )]TJ Leaving a fuel pump on with a low pressure light Over the nine)Tj -.02 Tc 6.5 0 0 6.5 221.1405 702.9529 Tm 9 0 0 9 206.8767 148.8898 Tm BT 7 0 0 7 439.2087 364.9528 Tm /P <>BDC EMC centre fuel tank. BT /GS1 gs (150 passengers on the A320ceo, A320neo,)Tj 9 0 0 9 215.4313 478.8898 Tm BT /P <>BDC ET BT /P <>BDC 7 0 0 7 440.0906 133.9528 Tm ( )Tj (weights plus the interior cabin)Tj /P <>BDC ET (192 seats. ET -.02 Tc (. BT EMC BT EMC (831)Tj (CFM56-5B3/P)Tj BT EMC EMC EMC ( )Tj ET /P <>BDC BT 7 0 0 7 508.4124 122.7654 Tm EMC ET /P <>BDC (evaluation it has been assumed that the)Tj EMC 9 0 0 9 411.0234 687.8898 Tm ( )Tj ET 9 0 0 9 531.7939 104.8898 Tm 0 Tc BT /P <>BDC BT EMC ET ( )Tj /P <>BDC )Tj /P <>BDC /P <>BDC EMC BT BT EMC -.02 Tc .014984 841.89 609.45 -841.89 re ET .559 .331 .619 rg EMC -.02 Tc ET BT ET EMC BT (Both the younger generation of Airbus)Tj fuel pumps were running in high ambient temperatures with empty or almost empty BT EMC BT /P <>BDC EMC BT EMC BT 0 Tc /P <>BDC -.02 Tc ( )Tj EMC ( )Tj ET BT BT BT (O)Tj ( )Tj ET BT /F4 1 Tf BT ET /P <>BDC -.02 Tc BT On the)Tj My simulation is focused on postcrash fires. /P <>BDC ( )Tj (Block fuel)Tj 9 0 0 9 215.4409 500.8898 Tm 7 0 0 7 187.0858 529.9528 Tm /P <>BDC ET /P <>BDC BT BT /P <>BDC EMC /P <>BDC BT ET BT BT /P <>BDC ( )Tj ET <>/XObject<>/ExtGState<>/Properties<>>> ( )Tj /P <>BDC BT EMC The total tolerance for the FQIS system is based on a full tank. /P <>BDC BT -.02 Tc ET 7 0 0 7 230.7317 243.9528 Tm ET 9 0 0 9 385.5399 115.8898 Tm W* n (have a 20-minute taxi-out time departing)Tj -.02 Tc EMC ET BT 9 0 0 9 544.9208 280.8898 Tm -.2034 -.7911 -.1202 -.4766 0 0 c BT BT 9 0 0 9 205.7907 236.8898 Tm BT EMC /P <>BDC ET BT /P <>BDC 9 0 0 9 394.0315 478.8898 Tm BT EMC /P <>BDC BT ET .0063 7.6255 l ET 6 0 0 6 450.9814 701.9528 Tm 9 0 0 9 425.1913 181.8898 Tm -.02 Tc 7 0 0 7 294.4014 617.7654 Tm 0 Tc BT (lower than the difference on the smaller)Tj ( )Tj EMC BT BT (The first is payload scenario 1, which)Tj /P <>BDC /P <>BDC <>/ExtGState<>/Properties<>>> -.01 Tc EMC EMC /P <>BDC ET EMC EMC BT Regarding winglets, I think Simple Flying explains it well. /P <>BDC ( )Tj /P <>BDC /P <>BDC /P <>BDC EMC EMC /P <>BDC 0 Tc /P <>BDC [(P)11(ayload)]TJ Boeing 777X The New Triple Seven Family. BT EMC ET ET (The engine choice on the A320neo is)Tj /P <>BDC EMC ( )Tj EMC ET (170)Tj For Example: 7 0 0 7 490.8321 540.7654 Tm -.02 Tc 9 0 0 9 426.0987 687.8898 Tm BT BT /P <>BDC ( )Tj Its fuel burn and)Tj /P <>BDC BT /P <>BDC .023 .567 .626 RG BT -.02 Tc (151)Tj ET 7 0 0 7 204.0935 331.7654 Tm BT /P <>BDC /P <>BDC ET ET /P <>BDC /P <>BDC BT 7 0 0 7 158.74 485.7654 Tm EMC (1,162)Tj )Tj BT EMC 7 0 0 7 99.8582 705.7654 Tm ET ET 7 0 0 7 491.7142 232.7654 Tm /P <>BDC EMC BT EMC 0 Tc q 1 0 0 1 394.012 447.878 cm 0 0 m BT BT (37,653)Tj 7 0 0 7 247.7395 111.7654 Tm 0 Tc BT (4,182)Tj Q BT 7 0 0 7 474.5665 430.9528 Tm EMC ET BT -.02 Tc /P <>BDC 7 0 0 7 182.5706 243.9528 Tm 5.25 0 0 5.25 492.6848 11.5129 Tm 7 0 0 7 457.0984 683.7654 Tm EMC EMC /P <>BDC /P <>BDC /P <>BDC EMC ( )Tj ( )Tj BT 7 0 0 7 518.4953 419.9528 Tm (900ER and 737-9, A320ceo and A320neo,)Tj ( )Tj 7 0 0 7 337.4684 738.9528 Tm BT EMC ( )Tj EMC BT /P <>BDC (5,791)Tj BT (CFM56-5B4/P)Tj 0 Tc 0 Tc 0 Tc /P <>BDC /P <>BDC ET EMC How much fuel does a A350 burn? -.02 Tc 0 Tc 7 0 0 7 314.6398 529.7654 Tm BT ET ET EMC ET 6.5 0 0 6.5 173.5238 637.9529 Tm From July 2004 NGs have been delivered with markings on the BT warm conditions! ET BT BT (25)Tj EMC BT ( )Tj ( )Tj q 1 0 0 1 36.85 797.54 cm 0 0 m BT pump will also transfer any remaining centre tank fuel into main tank 1, thereby BT (39,270)Tj EMC Perhaps somebody has experience in shipment of landing gear. BT BT ( )Tj /P <>BDC ET BT 0 Tc EMC BT ( )Tj /P <>BDC (6,353)Tj BT /P <>BDC EMC 13 0 0 13 202.8899 533.8898 Tm /P <>BDC BT ET /P <>BDC ET ET 7 0 0 7 230.7317 485.9528 Tm ET BT BT 9 0 0 9 394.0237 313.8898 Tm ( )Tj /GS2 gs -.02 Tc 7 0 0 7 492.5963 584.7654 Tm 6 0 0 6 547.0496 701.9528 Tm BT ET 7 0 0 7 536.3849 364.7654 Tm BT ( )Tj ( )Tj ET EMC ET /P <>BDC BT ET 7 0 0 7 316.0679 199.7654 Tm /P <>BDC /P <>BDC /P <>BDC /P <>BDC EMC 6.5 0 0 6.5 276.5184 565.9529 Tm /P <>BDC EMC The)Tj BT ET EMC ( )Tj BT BT 9 0 0 9 394.0123 522.8898 Tm EMC -.02 Tc BT BT 7 0 0 7 475.5884 89.9528 Tm (1,581)Tj 0 Tc ( )Tj 9 0 0 9 394.0315 467.8898 Tm BT ET 7 0 0 7 536.3849 408.7654 Tm ET ET EMC 7 0 0 7 379.3969 144.7654 Tm BT 7 0 0 7 354.6933 298.7654 Tm EMC ET ET 9 0 0 9 51.0236 71.8898 Tm /P <>BDC 9 0 0 9 75.273 467.8898 Tm /P <>BDC EMC BT EMC BT /P <>BDC /P <>BDC /P <>BDC BT (2,042)Tj BT (the aircraft types. 9 0 0 9 408.1854 566.8898 Tm /OC /MC5086 BDC BT ( )Tj ET BT EMC /P <>BDC (the engine option chosen for this study is)Tj BT BT (The thrust ratings on the engines show)Tj 7 0 0 7 507.7893 628.7654 Tm 36.85 541.416 340.159 263.624 re (and A321neo respectively. BT /P <>BDC BT BT BT /P <>BDC -.02 Tc ET BT /P <>BDC /P <>BDC 7 0 0 7 537.7804 78.9528 Tm ET 7 0 0 7 125.6292 188.7654 Tm /P <>BDC /P <>BDC ET EMC -.01 Tc EMC (A320neos cost per ASM advantage. EMC .014984 841.89 609.45 -841.89 re 7 0 0 7 247.7395 166.7654 Tm ET 9 0 0 9 171.8783 434.8898 Tm EMC 8 0 0 8 153.6923 661.9528 Tm ET EMC 0 Tc There arent to many differences between each variant. /GS2 gs 7 0 0 7 294.4014 540.7654 Tm 6.5 0 0 6.5 379.1824 565.9529 Tm EMC (63.5 inches and a bypass ratio of 4.5:1; or)Tj ET EMC ( )Tj EMC [(CFM L)17.1(E)-8.1(AP-1A26)]TJ (379)Tj ET [(D)12.9(A)42(Y/57)]TJ /P <>BDC (31,416)Tj ( )Tj /P <>BDC /P <>BDC EMC ET EMC ( )Tj EMC EMC 6.5 0 0 6.5 429.8944 598.9529 Tm ( )Tj BT q BT BT 7 0 0 7 141.7322 265.9528 Tm ET ( )Tj /P <>BDC /P <>BDC 6 0 0 6 153.9401 659.9528 Tm ET 9 0 0 9 203.5468 379.8898 Tm EMC /P <>BDC 9 0 0 9 215.4409 357.8898 Tm ET ET ET BT ET ( )Tj 7 0 0 7 277.3936 562.9528 Tm (of 170 passengers, the A321neo burns an)Tj BT /P <>BDC ET flightdeck (below the F/O's FMC) but they have since been removed to a 9 0 0 9 53.8338 236.8898 Tm .023 .567 .626 RG ( )Tj 7 0 0 7 204.0935 177.7654 Tm .0161 Tc /P <>BDC /P <>BDC )Tj 6.5 0 0 6.5 54.877 532.9529 Tm 19.841 0 l /P <>BDC ET EMC EMC EMC 7 0 0 7 490.5101 617.9528 Tm ET (performance than the 737-9. /P <>BDC ET BT BT EMC ET BT /P <>BDC Jump to Specification Table Boeing 737 Original and Boeing 737 Classic. -.02 Tc ET /F6 1 Tf (132,872)Tj BT -.02 Tc /P <>BDC ET ET BT /P <>BDC /P <>BDC BT 6 0 0 6 418.9814 701.9528 Tm 7 0 0 7 108.6215 342.9528 Tm -.02 Tc ET BT 9 0 0 9 350.8719 390.8898 Tm (483)Tj 7 0 0 7 457.0984 463.7654 Tm 0 Tc 7 0 0 7 82.8504 188.9528 Tm ET ET /P <>BDC ET /P <>BDC 7 0 0 7 539.8962 507.9528 Tm ( )Tj ( )Tj 9 0 0 9 215.4409 434.8898 Tm EMC /P <>BDC /P <>BDC EMC ET ( )Tj BT EMC ET 17 0 0 17 36.8606 742.1944 Tm EMC BT /P <>BDC EMC BT During cruise, the tolerance is less than 0.5%. EMC BT ET -.01 Tc ( )Tj BT BT The Boeing 737-800 to date has around 5000 units produced and 2019 saw 138 of the 800 roll of the production line. 6.5 0 0 6.5 64.6596 702.9529 Tm 7 0 0 7 118.104 67.7654 Tm 7 0 0 7 77.36 11.5132 Tm (2.5% lower fuel burn for the 737-800. 9 0 0 9 394.0157 632.8898 Tm ( )Tj BT .41 .161 .508 rg (A321ceo)Tj BT 0 Tc /P <>BDC /P <>BDC 6 0 0 6 527.6392 757.9528 Tm BT ET ET BT /P <>BDC 9 0 0 9 394.0123 225.8898 Tm EMC (379)Tj (831)Tj EMC 8 0 0 8 256.0704 717.9528 Tm ET 9 0 0 9 531.3621 148.8898 Tm EMC (CFM56-7B26)Tj (. (heavier than the A320ceo. 9 0 0 9 394.0123 38.8898 Tm EMC 0 Tc /P <>BDC ( )Tj EMC ET 7 0 0 7 258.2805 430.7654 Tm BT 7 0 0 7 241.2727 177.9528 Tm /P <>BDC ET 0 Tc /P <>BDC /P <>BDC /P <>BDC (The evaluation uses US domestic flight)Tj 0 Tc EMC ET BT 8 0 0 8 471.0755 760.9528 Tm EMC (170)Tj BT ET ( )Tj 19.84 0 l 9 0 0 9 570.6951 291.8898 Tm ET BT (rating on the CFM LEAP-1A32 to)Tj BT /P <>BDC /P <>BDC (bypass ratio of 5.7:1, and is rated at)Tj /P <>BDC /P <>BDC EMC ET 7 0 0 7 537.7804 111.9528 Tm 7 0 0 7 337.6855 485.9528 Tm ET EMC ET EMC /P <>BDC 7 0 0 7 537.267 133.7654 Tm BT (with a thrust rating of 27,000lbs, an intake)Tj BT (This comparison is made using the)Tj /P <>BDC ( )Tj