737 800 fuel capacity pounds

/P <>BDC EMC EMC ET ( )Tj ET 7 0 0 7 440.0906 342.9528 Tm .151 .147 .15 rg (2,149)Tj 7 0 0 7 294.4014 584.7654 Tm BT BT ET BT BT ( )Tj /P <>BDC ( )Tj BT /P <>BDC /P <>BDC -.02 Tc EMC /P <>BDC 0 Tc BT BT 0 Tc BT BT EMC 7 0 0 7 439.2087 210.9528 Tm /P <>BDC BT /P <>BDC (0.0140)Tj ET 9 0 0 9 394.0123 522.8898 Tm ET /P <>BDC BT BT S 7 0 0 7 380.2788 606.7654 Tm BT /P <>BDC EMC BT /P <>BDC (burn and operating)Tj 7 0 0 7 508.4124 375.7654 Tm /P <>BDC /P <>BDC EMC /P <>BDC EMC EMC /P <>BDC [(F)43(uel burn/)]TJ 5.25 0 0 5.25 515.3989 11.5129 Tm 9 0 0 9 229.6045 104.8898 Tm /P <>BDC 0 Tc /P <>BDC /P <>BDC /P <>BDC 7 0 0 7 99.5912 507.9528 Tm .0063 7.6255 l EMC BT BT ( )Tj BT BT EMC -.02 Tc 9 0 0 9 232.4217 104.8898 Tm ( )Tj 6 0 0 6 433.9826 659.9528 Tm EMC 7 0 0 7 404.101 100.7654 Tm /P <>BDC ( )Tj ET EMC ( )Tj /P <>BDC /P <>BDC /P <>BDC The Honeywell NGS was certified by the FAA on 21 Feb 2006 after over 1000hrs flight testing on two 737-NGs. 0 Tc EMC BT each aircraft is sourced from different places. /P <>BDC [(CFM L)17.1(E)-8.1(AP-1B27)]TJ 0 Tc 6.5 0 0 6.5 549.8557 585.9529 Tm ET /P <>BDC EMC 9 0 0 9 341.1717 478.8898 Tm ET ET EMC /P <>BDC 0 Tc ET 7 0 0 7 36.8504 11.5129 Tm EMC 0 Tc EMC BT 9 0 0 9 229.6141 115.8898 Tm 9 0 0 9 201.2426 445.8898 Tm EMC BT 9 0 0 9 190.8846 379.8898 Tm 6.5 0 0 6.5 378.2463 598.9529 Tm BT BT BT ET 9 0 0 9 232.438 489.8898 Tm /P <>BDC /F7 1 Tf 9 0 0 9 548.4747 115.8898 Tm EMC BT /P <>BDC EMC 7 0 0 7 187.0858 232.9528 Tm EMC BT /P <>BDC ( )Tj 7 0 0 7 299.0601 122.9528 Tm /P <>BDC - Non Perele - News Online, Council Post: Aviation Is The Driving Force Of Hydrogen | QNewsHub, When will the Boeing 737 MAX fly again? BT (performance. ( )Tj EMC 9 0 0 9 408.1854 291.8898 Tm 9 0 0 9 547.2866 390.8898 Tm ( )Tj \p+\rWef6lfL6;U1E5/6lUYyVebaHfQM]$q|L>_ SO9_sXa 3@"G;C=zlPY[?B ( )Tj /P <>BDC ET 0 Tc 5 0 0 5 484.5872 11.5129 Tm EMC /P <>BDC EMC 7 0 0 7 294.4014 177.7654 Tm BT EMC BT ET BT 0 Tc BT BT 7 0 0 7 338.6433 430.7654 Tm 6.5 0 0 6.5 426.4819 663.9529 Tm EMC BT -.02 Tc 9 0 0 9 36.8504 313.8898 Tm BT 7 0 0 7 321.6356 243.9528 Tm /P <>BDC BT ET EMC ET BT ET EMC ( )Tj BT ET 7 0 0 7 474.7064 441.9528 Tm EMC 0 Tc EMC /F6 1 Tf /P <>BDC EMC BT BT 6 0 0 6 309.2404 715.9528 Tm /P <>BDC EMC EMC .0161 Tc 7 0 0 7 141.7322 265.9528 Tm ( )Tj ( )Tj (136)Tj 6.5 0 0 6.5 244.2974 545.9529 Tm BT ET ( )Tj 9 0 0 9 394.0315 368.8898 Tm 9 0 0 9 394.0123 368.8898 Tm ( )Tj ET /P <>BDC BT ET ( )Tj 6.5 0 0 6.5 296.4841 702.9529 Tm BT BT q 1 0 0 1 53.834 601.878 cm 0 0 m 6 0 0 6 519.1239 687.9528 Tm BT 0 Tc BT ( )Tj /P <>BDC EMC ET (31,416)Tj 7 0 0 7 54.7071 485.7654 Tm /P <>BDC (0.0142)Tj BT ET EMC -.02 Tc BT ( )Tj 5.25 0 0 5.25 123.5367 11.5132 Tm ET /P <>BDC EMC ET EMC /P <>BDC BT 19.843 0 l BT EMC BT 9 0 0 9 343.5117 489.8898 Tm BT ET BT Boeings main competitor is with Airbus. BT (used is 16/30/114, giving a seat count of)Tj ET 8 0 0 8 266.591 745.9528 Tm BT ( 2021)Tj 0 Tw ET /P <>BDC ET EMC EMC 9 0 0 9 194.5132 38.8898 Tm EMC 0 J 0 j 15 w 10 M [] 0 d Usually, you can find technical manuals, sometimes in PDF form which are full of information. EMC EMC ET BT EMC 0 Tc 7 0 0 7 364.1531 133.9528 Tm 7 0 0 7 338.6433 67.7654 Tm 6.5 0 0 6.5 433.3069 585.9529 Tm (409,800)Tj EMC ET 9 0 0 9 187.813 126.8898 Tm 0 Tc /F1 1 Tf (is 2.54 cents per ASM for the same)Tj 0 Tc ( )Tj 9 0 0 9 215.433 423.8898 Tm EMC 0 Tc /P <>BDC /P <>BDC EMC (cents, with a network average)Tj ET 9 0 0 9 394.0123 115.8898 Tm EMC EMC EMC /TT2 1 Tf /P <>BDC /P <>BDC ET (I)Tj /P <>BDC 6 0 0 6 271.9128 729.9528 Tm 7 0 0 7 241.2727 364.9528 Tm /P <>BDC ET /P <>BDC -.02 Tc /P <>BDC /P <>BDC q 1 0 0 1 53.85 797.54 cm 0 0 m BT /P <>BDC 6.5 0 0 6.5 432.488 558.9529 Tm 9 0 0 9 206.7178 181.8898 Tm /P <>BDC (832)Tj BT )Tj 9 0 0 9 394.0315 632.8898 Tm ET -.02 Tc 7 0 0 7 535.5029 496.7654 Tm 0 Tc 0 Tc EMC EMC ( )Tj /F6 1 Tf ET BT /P <>BDC EMC (0.0171)Tj (344-358)Tj EMC 9 0 0 9 394.0315 555.8898 Tm ET (number for the neo family. EMC /P <>BDC (Both the younger generation of Airbus)Tj BT EMC EMC /P <>BDC EMC ET BT (977)Tj BT BT EMC EMC ET ( )Tj ET (37,653)Tj EMC ET /P <>BDC (136)Tj /P <>BDC ET ET /P <>BDC EMC (214)Tj BT /P <>BDC (to 165 passengers on BOS-LAX. BT 9 0 0 9 394.0123 335.8898 Tm to the centre tank through a manual valve by cabin pressure. BT BT [(UG)-17.1(U)-8(S)8.1(T)]TJ 9 0 0 9 53.8578 346.8898 Tm 0 Tc /P <>BDC ( )Tj (375)Tj ET 6.5 0 0 6.5 449.1864 611.9529 Tm /P <>BDC BT /P <>BDC EMC (2,516)Tj ET /P <>BDC BT ET ( )Tj 9 0 0 9 53.8338 49.8898 Tm ( )Tj BT 7 0 0 7 37.6993 210.9528 Tm EMC BT 0 Tc ET BT 9 0 0 9 36.8504 38.8898 Tm EMC /OC /MC835 BDC 9 0 0 9 531.8156 280.8898 Tm ET /P <>BDC ( )Tj /P <>BDC ET EMC the climb. ET BT BT ET EMC ET 9 0 0 9 206.8407 412.8898 Tm /P <>BDC EMC ET ET EMC ( )Tj BT ET BT 9 0 0 9 195.9803 247.8898 Tm BT ET BT 9 0 0 9 548.1057 610.8898 Tm /P <>BDC Today the Next Generation 737 sub-family includes the 700, -800 and 900models. ( )Tj ET EMC 7 0 0 7 158.74 111.7654 Tm ET /P <>BDC EMC BT 9 0 0 9 386.9059 280.8898 Tm 6.5 0 0 6.5 76.9446 715.9529 Tm EMC -.02 Tc Q ET ET EMC EMC /P <>BDC 9 0 0 9 68.0314 258.8898 Tm EMC ( )Tj ET EMC 7 0 0 7 535.5029 661.7654 Tm /P <>BDC BT Q 7 0 0 7 82.2047 639.9528 Tm -.02 Tc -.02 Tc /P <>BDC ET /P <>BDC /P <>BDC EMC /P <>BDC EMC /P <>BDC ( )Tj EMC (minutes between aircraft types or 3.7% on)Tj ET BT ( )Tj ET ET /P <>BDC /P <>BDC 7 0 0 7 247.7395 595.7654 Tm /P <>BDC (ESAD)Tj ( )Tj EMC /P <>BDC BT ( )Tj ET BT ET ( )Tj EMC 5 0 0 5 484.5872 11.5129 Tm EMC /P <>BDC -.02 Tc ( )Tj 7 0 0 7 380.2788 298.7654 Tm BT BT EMC BT ET 7 0 0 7 490.7815 221.9528 Tm EMC /P <>BDC EMC BT 9 0 0 9 36.8504 412.8898 Tm ET /P <>BDC BT 7 0 0 7 554.7883 397.7654 Tm ( )Tj ET ET ET EMC ET ( )Tj /P <>BDC EMC ( )Tj ET ( )Tj /F6 1 Tf BT ET EMC BT Economy-plus is also)Tj EMC EMC 0 Tc BT /P <>BDC ( )Tj 7 0 0 7 380.2788 397.7654 Tm (486)Tj ET ( )Tj ( )Tj EMC /F7 1 Tf 304.725 420.96 m BT The aux tanks are located at EMC ( )Tj /P <>BDC /P <>BDC These carriers)Tj )Tj BT /P <>BDC EMC 9 0 0 9 394.0315 511.8898 Tm /P <>BDC /P <>BDC 9 0 0 9 394.0237 456.8898 Tm 0 Tc EMC BT ( )Tj BT ( )Tj 8 0 0 8 43.6039 703.9528 Tm ( )Tj (216,240)Tj ( )Tj 7 0 0 7 141.7322 298.9528 Tm 8 0 0 8 38.4438 675.9528 Tm EMC BT .151 .147 .15 rg ( )Tj EMC 6 0 0 6 561.1918 687.9528 Tm ( )Tj ET 7 0 0 7 387.0159 584.9528 Tm 10 0 0 10 49.3644 814.1973 Tm ET (170)Tj ET BT BT /P <>BDC ET BT ET EMC ( )Tj 0 Tc ET ET /P <>BDC /P <>BDC ET 8 0 0 8 74.9636 591.9528 Tm /P <>BDC ( )Tj EMC BT EMC EMC BT ( )Tj EMC (737-800 and 737-8; and 170 passengers on)Tj ET (34,650)Tj BT 7 0 0 7 82.2047 463.9528 Tm 7 0 0 7 403.478 584.7654 Tm EMC 7 0 0 7 158.74 221.7654 Tm /P <>BDC (737-8)Tj (The A320neo family and 737 MAX)Tj /P <>BDC /P <>BDC BT /P <>BDC BT EMC /P <>BDC .1334 -5.7288 l ET (39,270)Tj /P <>BDC .534 .14 .504 RG BT ( )Tj 0 Tc 9 0 0 9 105.3138 82.8898 Tm BT BT BT 7 0 0 7 429.157 540.9528 Tm ( )Tj /P <>BDC -.02 Tc )Tj 6.5 0 0 6.5 296.4841 650.9529 Tm EMC /P <>BDC /P <>BDC ( )Tj BT (similar-sized and directly competing)Tj ( )Tj /P <>BDC /P <>BDC 9 0 0 9 550.3341 313.8898 Tm ET 0 Tc (the analysis is 20/29/143, so a total of 192)Tj BT 0 Tc /P <>BDC -.02 Tc /P <>BDC ET ET ( )Tj EMC BT /OC /MC199 BDC ( )Tj 7 0 0 7 337.7614 144.7654 Tm The classics have 5 dripsticks in each wing tank and none in the centre ( )Tj 0 Tc 9 0 0 9 564.1726 588.8898 Tm ET -.005 Tc BT 9 0 0 9 252.5351 214.8898 Tm BT 7 0 0 7 344.1175 617.7654 Tm BT BT 7 0 0 7 474.3564 628.9528 Tm 0 J 0 j 15 w 10 M [] 0 d /P <>BDC ( )Tj EMC 9 0 0 9 193.0552 434.8898 Tm (5,025)Tj EMC (2,515)Tj 0 Tc BT BT EMC 9 0 0 9 408.1854 60.8898 Tm (27,000lbs of thrust compared to the)Tj /P <>BDC EMC BT ET EMC BT EMC ET 10 0 0 10 425.05 814.1973 Tm /P <>BDC EMC BT 7 0 0 7 321.6356 177.9528 Tm 0 Tc ( )Tj EMC (150)Tj 9 0 0 9 178.1318 71.8898 Tm BT BT /P <>BDC 7 0 0 7 230.7317 265.9528 Tm -.02 Tc (148,504)Tj 0 Tc EMC ET ET 9 0 0 9 36.8504 236.8898 Tm EMC (3,021)Tj 9 0 0 9 366.6417 137.8898 Tm BT 7 0 0 7 337.6855 177.9528 Tm EMC ( )Tj ( )Tj EMC ( )Tj ET /F7 1 Tf /P <>BDC EMC 7 0 0 7 535.5029 375.7654 Tm /P <>BDC EMC 8 0 0 8 43.6039 717.9528 Tm BT /P <>BDC EMC ET ( )Tj /P <>BDC BT BT -.02 Tc ET BT EMC ET Hi I was just wondering where you got this data from. 7 0 0 7 366.0641 727.9528 Tm ET (. 0 Tc 6 0 0 6 457.0716 687.9528 Tm BT ET -.02 Tc BT BT ET ( )Tj -.02 Tc ET /P <>BDC EMC /P <>BDC /P <>BDC BT ET /P <>BDC BT BT ET /P <>BDC (283)Tj /P <>BDC ( )Tj ET /P <>BDC /P <>BDC EMC ET /P <>BDC (369-383)Tj ( C)Tj (120-128)Tj ET ET BT ET BT 7 0 0 7 427.7291 100.9528 Tm (28,000lbs compared to 27,000lbs for the)Tj (in a more efficient engine. ( The time spent in potential holding)Tj EMC BT ( )Tj 0 Tc /P <>BDC /P <>BDC EMC BT EMC 7 0 0 7 315.5217 617.7654 Tm (the fuel consumption for each type over)Tj -.01 Tc /P <>BDC BT (evaluate the physical configuration of the)Tj 9 0 0 9 368.9994 225.8898 Tm 6 0 0 6 403.4411 757.9528 Tm BT ( )Tj ( )Tj 7 0 0 7 54.7071 210.7654 Tm ET ET EMC 7 0 0 7 490.5226 78.9528 Tm ET EMC 6.5 0 0 6.5 178.4573 722.9529 Tm EMC /P <>BDC 8 0 0 8 74.9636 717.9528 Tm 7 0 0 7 258.2805 364.7654 Tm 9 0 0 9 53.8578 225.8898 Tm BT 9 0 0 9 189.8338 49.8898 Tm /P <>BDC (burns. /P <>BDC ET 0 841.89 609.449 -841.89 re /P <>BDC BT 6.5 0 0 6.5 296.3606 735.9529 Tm 7 0 0 7 337.6855 540.9528 Tm 7 0 0 7 355.3163 78.7654 Tm -.02 Tc 0 Tc /P <>BDC EMC ET 9 0 0 9 411.0097 60.8898 Tm BT (prices, and can vary by the aircraft type)Tj /P <>BDC 9 0 0 9 215.433 280.8898 Tm /P <>BDC ET .023 .567 .626 rg (configuration, because this study shows)Tj BT BT The accuracy of the fuel flow transmitter is a function of the fuel flow. ET /P <>BDC EMC 7 0 0 7 82.8504 144.9528 Tm /P <>BDC EMC 7 0 0 7 476.1204 694.9528 Tm /OC /MC1950 BDC ET BT /P <>BDC To allow a fair)Tj /P <>BDC EMC BT BT EMC EMC EMC BT BT ( )Tj ( )Tj ET EMC /P <>BDC 0 Tc 7 0 0 7 365.035 639.9528 Tm ET The BBJ can have up to 9 aux fuel tanks giving it a maximum fuel quantity of 37,712kgs (83,000lbs) although in practice this would /P <>BDC 7 0 0 7 230.7317 111.9528 Tm ET 7 0 0 7 299.0601 221.9528 Tm ET ( )Tj ( )Tj /P <>BDC EMC [(T)92(axi out time - mins)]TJ /P <>BDC 9 0 0 9 186.5212 225.8898 Tm 6 0 0 6 418.9814 673.9528 Tm BT ( )Tj /P <>BDC ET EMC BT 7 0 0 7 82.8504 100.9528 Tm /P <>BDC BT -.01 Tc EMC EMC /P <>BDC ( )Tj ET /P <>BDC /P <>BDC ET BT /P <>BDC EMC /P <>BDC BT ET ( )Tj EMC /P <>BDC (The aircraft are examined on the basis)Tj ( )Tj ET (Any seating configuration is defined by)Tj 7 0 0 7 37.6993 375.9528 Tm BT EMC EMC (compares to a tracked distance of)Tj EMC EMC EMC BT 7 0 0 7 475.2383 639.9528 Tm /P <>BDC 9 0 0 9 563.4796 324.8898 Tm BT 6.5 0 0 6.5 549.8557 637.9529 Tm (1,272)Tj ET BT 7 0 0 7 277.3936 463.9528 Tm ET 7 0 0 7 241.2727 144.9528 Tm EMC [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ BT EMC /P <>BDC ET BT EMC ( )Tj BT /P <>BDC 9 0 0 9 36.8504 467.8898 Tm q 1 0 0 1 36.85 84.878 cm 0 0 m (34,650)Tj (31,416lbs)Tj 7 0 0 7 491.4046 419.9528 Tm BT BT [(P)11(ayload scenario one)]TJ [(MR)32(TX - lbs)]TJ BT 6.5 0 0 6.5 346.1035 637.9529 Tm EMC EMC EMC BT /P <>BDC EMC BT BT fuel pumps will automatically shut off when they detect a low output pressure. EMC /P <>BDC EMC 0 Tc /P <>BDC -.02 Tc BT 9 0 0 9 369.4947 357.8898 Tm BT /P <>BDC ( )Tj -.02 Tc BT ( )Tj ( )Tj ( )Tj BT (170)Tj q 1 0 0 1 215.433 150.878 cm 0 0 m -.02 Tc BT EMC 9 0 0 9 361.016 49.8898 Tm it seems that Boeing has not leaped ahead with the 737 as much as they have with the 787. ET /P <>BDC BT /P <>BDC BT (ONT/73)Tj 0 Tc Hello! EMC /P <>BDC ( )Tj -.01 Tc ET /P <>BDC (or scenarios in this study. (146,550)Tj /P <>BDC /P <>BDC EMC BT ( )Tj BT BT ( )Tj ( )Tj (0.0119)Tj BT (1,581)Tj ET EMC ( )Tj ( )Tj (The 737-9 has an 11.2% to 12.7%)Tj EMC EMC ET ET /P <>BDC 9 0 0 9 394.0315 577.8898 Tm ( )Tj EMC 0 Tc EMC BT ET (82,110)Tj EMC /P <>BDC )Tj ET ET BT 9 0 0 9 536.4734 313.8898 Tm BT 10 0 0 10 312.5146 771.9528 Tm 7 0 0 7 247.7395 232.7654 Tm (earlier counterpart. ET /P <>BDC 7 0 0 7 230.7317 518.9528 Tm ET BT EMC /P <>BDC 1 i (0.0126)Tj EMC ET 7 0 0 7 294.4014 375.7654 Tm /Artifact <>BDC [(737 M)-8.1(A)-24.9(X-9)]TJ BT ET (170)Tj 7 0 0 7 163.8846 11.5132 Tm S EMC 8 0 0 8 275.7172 760.7654 Tm 9 0 0 9 204.06 742.8898 Tm 7 0 0 7 54.7071 100.7654 Tm ET 9 0 0 9 215.4409 500.8898 Tm BT The Boeing 737-800 variant has as mentioned 27300 pound-force delivered by two turbo fans. /P <>BDC BT ET /P <>BDC (0.0135)Tj EMC EMC /P <>BDC .41 .161 .508 rg ( )Tj ET BT EMC (68.3 inches and a bypass ratio of up to)Tj ET 7 0 0 7 297.632 672.9528 Tm 9 0 0 9 372.2129 192.8898 Tm EMC BT (capacity, so that payload is reduced to)Tj BT EMC 7 0 0 7 99.8582 298.7654 Tm ( )Tj /P <>BDC /P <>BDC BT /P <>BDC ET EMC 9 0 0 9 36.8504 137.8898 Tm /P <>BDC EMC EMC ET BT 7 0 0 7 279.1575 694.9528 Tm 8 0 0 8 187.3427 703.9528 Tm 7 0 0 7 380.2788 485.7654 Tm 53.85 621.704 518.723 183.336 re BT BT 7 0 0 7 535.5029 683.7654 Tm 9 0 0 9 36.8504 302.8898 Tm EMC (273,600)Tj EMC 0 Tc /P <>BDC BT 0 Tw (\(see table, page 21\))Tj /P <>BDC BT /P <>BDC EMC /P <>BDC ET BT endobj BT 7 0 0 7 101.0963 89.9528 Tm ( )Tj /OC /MC860 BDC EMC /P <>BDC EMC EMC 9 0 0 9 394.0123 544.8898 Tm 7 0 0 7 539.8962 496.9528 Tm ET /P <>BDC ( )Tj ET EMC BT EMC BT EMC BT EMC 9 0 0 9 172.0312 357.8898 Tm q ET (0.0127)Tj (170)Tj 7 0 0 7 475.2383 683.9528 Tm ( )Tj EMC 6.5 0 0 6.5 54.877 715.9529 Tm /P <>BDC (31,416)Tj EMC ET 0 Tc -.02 Tc ET BT ( )Tj BT ET ET ( )Tj 9 0 0 9 518.5923 511.8898 Tm 9 0 0 9 555.1526 368.8898 Tm W n BT (10)Tj 7 0 0 7 554.7883 463.7654 Tm BT 10 0 0 10 60.6037 794.2914 Tm EMC 7 0 0 7 554.7883 716.7654 Tm ET 6.5 0 0 6.5 273.8079 702.9529 Tm ( )Tj ( )Tj 6.5 0 0 6.5 64.6596 663.9529 Tm BT /P <>BDC BT (104-112)Tj ( )Tj EMC <>/XObject<>/ExtGState<>/Properties<>>> /P <>BDC (163)Tj (113)Tj 9 0 0 9 365.1022 170.8898 Tm ( )Tj -.02 Tc tank. /P <>BDC /P <>BDC EMC (CFM56-7B26)Tj EMC /P <>BDC /P <>BDC EMC 9 0 0 9 411.0097 170.8898 Tm BT ( )Tj 7 0 0 7 440.3636 474.9528 Tm ET 7 0 0 7 131.6494 276.7654 Tm BT ET ET 7 0 0 7 469.2222 11.5129 Tm /GS1 gs 7 0 0 7 158.74 584.7654 Tm ET ET ET -.02 Tc EMC ( )Tj /P <>BDC EMC BT 0 Tc EMC 1 i BT EMC BT 9 0 0 9 232.438 214.8898 Tm /P <>BDC EMC ET /P <>BDC ET ( )Tj BT 9 0 0 9 394.0315 335.8898 Tm -.02 Tc 0 Tc EMC EMC BT i would like to know the dimension of both nose and main landing gear crates also the approximate weight of the shipment. 9 0 0 9 361.2861 181.8898 Tm 5.25 0 0 5.25 40.8474 11.5129 Tm 7 0 0 7 321.6356 419.9528 Tm BT EMC (288)Tj -.02 Tc ( )Tj -.02 Tc ( )Tj BT EMC ET EMC EMC ET ET Airbus A320 Interior Inside the cabin of this city hopper. /P <>BDC /P <>BDC 6.5 0 0 6.5 243.8814 689.9529 Tm /P <>BDC ( )Tj /P <>BDC (\(see table,)Tj BT /P <>BDC /P <>BDC /Artifact <>BDC 7 0 0 7 99.8582 67.7654 Tm ET 7 0 0 7 535.5029 122.7654 Tm /P <>BDC /GS2 gs /P <>BDC 7 0 0 7 429.157 463.9528 Tm /P <>BDC BT 6.5 0 0 6.5 54.877 689.9529 Tm /P <>BDC BT 6 0 0 6 541.7341 659.9528 Tm (BOS-LAX due to the strong headwind)Tj -.02 Tc /P <>BDC EMC /P <>BDC ET /P <>BDC -.02 Tc ET 0 Tc (This comparison is made using the)Tj ET ET -.02 Tc /P <>BDC 0 Tc 0 Tc BT ( )Tj BT ET BT BT EMC 0 Tc ET /F4 1 Tf ET /P <>BDC Pisquali 19/05/2018 at 16:07 Reply. BT 7 0 0 7 343.2355 518.7654 Tm ET ET ( )Tj EMC 9 0 0 9 556.3508 137.8898 Tm EMC ET BT ( )Tj 9 0 0 9 390.0497 753.8898 Tm )Tj /P <>BDC /F6 1 Tf BT EMC BT ( )Tj ET /P <>BDC /P <>BDC (into service in 2023. ET /P <>BDC 9 0 0 9 376.7938 500.8898 Tm 7 0 0 7 490.5101 716.9528 Tm EMC EMC BT 7 0 0 7 474.3564 485.9528 Tm ( )Tj EMC BT EMC -.02 Tc 7 0 0 7 107.1165 661.9528 Tm BT (342,312)Tj ET EMC 7 0 0 7 241.5317 408.9528 Tm /P <>BDC (give the newer type a further advantage. EMC (976)Tj ET ( )Tj EMC 7 0 0 7 82.8504 331.9528 Tm 0 Tc 9 0 0 9 411.0181 489.8898 Tm EMC ( )Tj 9 0 0 9 375.2598 126.8898 Tm 7 0 0 7 82.2047 727.9528 Tm ( )Tj /P <>BDC EMC (172,992)Tj BT EMC (period in 2020. ET ET EMC BT ( )Tj 7 0 0 7 520.6108 705.9528 Tm ( )Tj ( )Tj ET ( )Tj BT 9 0 0 9 550.8315 247.8898 Tm BT BT 7 0 0 7 496.3063 705.7654 Tm /P <>BDC EMC /P <>BDC /P <>BDC .151 .147 .15 rg 8 0 0 8 225.1837 633.9528 Tm BT /P <>BDC BT EMC EMC EMC ( )Tj -.01 Tc BT (171,520)Tj EMC (206,132)Tj EMC 9 0 0 9 394.0157 368.8898 Tm (variants increases from 5.1:1 on the 737-)Tj The fuel tank was instrumented with gas sample tubing and thermocouples to /P <>BDC ET BT 7 0 0 7 508.2252 11.5129 Tm 0 Tc EMC BT ( )Tj 7 0 0 7 182.5706 474.9528 Tm /P <>BDC ET /P <>BDC On the)Tj ET /P <>BDC 9 0 0 9 53.8338 137.8898 Tm 7 0 0 7 383.0719 672.7654 Tm -.02 Tc EMC ET 0 Tc EMC /P <>BDC (burn difference is 2.2%, and results in an)Tj /P <>BDC error codes 1, 3, 5 or 7 to maintain C of G balance. EMC 7 0 0 7 490.8321 342.7654 Tm ET BT EMC EMC EMC EMC ET ( )Tj ET EMC EMC ET ET (A)Tj /P <>BDC ET /P <>BDC -.02 Tc ( )Tj Do you have the estimated production material used for the 737 Next Gen? EMC ( )Tj BT 9 0 0 9 372.8879 412.8898 Tm ( )Tj ET 9 0 0 9 537.5864 291.8898 Tm ET -.02 Tc ET EMC /P <>BDC /P <>BDC ( )Tj ET BT BT ET EMC BT ET ET BT 9 0 0 9 375.5153 291.8898 Tm EMC ( )Tj ET ( )Tj EMC /P <>BDC ET ( )Tj EMC /F7 1 Tf ET EMC ET 6.5 0 0 6.5 191.7701 558.9529 Tm 9 0 0 9 188.3303 181.8898 Tm ET EMC EMC /P <>BDC /P <>BDC 9 0 0 9 68.0071 566.8898 Tm 7 0 0 7 54.7071 67.7654 Tm 9 0 0 9 51.0236 60.8898 Tm EMC EMC 6.5 0 0 6.5 397.9138 722.9529 Tm (\(see table, page 19\))Tj -.02 Tc /P <>BDC BT (A320neo:)Tj EMC BT 9 0 0 9 551.0194 588.8898 Tm BT ET [(AIRL)8.1(INE & AIR)7.1(CRAF)-12.9(T)18.1( OPERA)56.9(T)-8.1(ION)-13.9(S)]TJ Q BT EMC /P <>BDC -.02 Tc /P <>BDC (39,270)Tj /F6 1 Tf ET /P <>BDC EMC EMC BT As)Tj ( )Tj /P <>BDC ET EMC EMC 6.5 0 0 6.5 552.6508 565.9529 Tm ET ( )Tj 7 0 0 7 247.7395 276.7654 Tm [(Aircr)10(aft types )]TJ ET 7 0 0 7 354.6933 419.7654 Tm BT BT ET /P <>BDC (\(see table, page 19\))Tj ET /P <>BDC /P <>BDC /GS1 gs /P <>BDC EMC 0 Tc [(Aircr)10(aft)]TJ BT ET ( )Tj BT ET BT 9 0 0 9 544.8295 236.8898 Tm ( )Tj ET (O)Tj 7 0 0 7 187.5417 430.9528 Tm /P <>BDC /P <>BDC BT ET /P <>BDC 7 0 0 7 148.0554 11.5132 Tm 8 0 0 8 302.5117 619.9528 Tm /P <>BDC 9 0 0 9 53.8582 357.8898 Tm 9 0 0 9 51.0315 379.8898 Tm EMC BT BT BT BT 7 0 0 7 314.6398 518.7654 Tm /P <>BDC BT /P <>BDC 7 0 0 7 474.3564 606.9528 Tm ET -.02 Tc )Tj BT /OC /MC1974 BDC .41 .161 .508 rg EMC BT EMC ( )Tj EMC /P <>BDC ET /P <>BDC ET 0 Tc 7 0 0 7 37.5838 56.9528 Tm ET ET -.01 Tc [(trip fuel burn compar)10(ed to the 737-800. EMC EMC ET -.02 Tc 9 0 0 9 68.0071 577.8898 Tm 7 0 0 7 445.7203 11.5129 Tm ET EMC !! /P <>BDC BT EMC ET /P <>BDC /P <>BDC ( )Tj EMC (2,575)Tj /P <>BDC 7 0 0 7 490.7815 67.9528 Tm .023 .567 .626 RG BT EMC EMC EMC .151 .147 .15 rg /P <>BDC 9 0 0 9 181.8233 49.8898 Tm /P <>BDC BT /P <>BDC (0.0154)Tj EMC EMC 9 0 0 9 212.7029 390.8898 Tm (0.0127)Tj EMC EMC ET /P <>BDC ET -.02 Tc ( )Tj ET /P <>BDC EMC EMC /P <>BDC -.02 Tc EMC EMC BT -.02 Tc /P <>BDC /P <>BDC EMC 9 0 0 9 275.0764 401.8898 Tm ( )Tj 9 0 0 9 394.0237 467.8898 Tm 13 0 0 13 274.8818 137.8898 Tm (273,600)Tj 0 Tc ET EMC /P <>BDC /P <>BDC EMC /P <>BDC /P <>BDC 7 0 0 7 82.8504 177.9528 Tm BT /P <>BDC (18)Tj EMC Boeings 737-800 isnt called the most popular airliner for no reason. /P <>BDC ET EMC ET /P <>BDC -.02 Tc (4,218)Tj BT 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. EMC BT 0 Tc ( )Tj EMC ( )Tj 7 0 0 7 294.4014 67.7654 Tm /P <>BDC 9 0 0 9 186.7249 511.8898 Tm ( )Tj 6 0 0 6 239.8235 743.9528 Tm EMC 0 Tc ( )Tj q 1 0 0 1 394.012 84.878 cm 0 0 m ET BT ( )Tj ET (CFM56-7B27B3 installed on the 737-)Tj EMC BT /P <>BDC /P <>BDC EMC /P <>BDC (fuel consumption and cost per seat or per)Tj ET EMC f .41 .161 .508 rg ( )Tj 9 0 0 9 232.4408 797.8898 Tm 7 0 0 7 490.8321 122.7654 Tm -.02 Tc ET BT ET 7 0 0 7 355.3163 144.7654 Tm (A)Tj /P <>BDC 9 0 0 9 53.8582 236.8898 Tm BT /P <>BDC EMC ET /P <>BDC ET /P <>BDC EMC BT -.02 Tc BT (35,112lbs)Tj /P <>BDC ET /P <>BDC 9 0 0 9 170.6722 104.8898 Tm (409,650)Tj .559 .331 .619 rg (0.0140)Tj (analysis are: an MTOW of 213,848lbs; an)Tj /P <>BDC 0 Tc /P <>BDC /P <>BDC EMC ET ( )Tj -.02 Tc ( )Tj EMC EMC ET EMC 6 0 0 6 184.3662 701.9528 Tm /P <>BDC ET -.02 Tc (0.0149)Tj /P <>BDC /P <>BDC 0 Tc ET EMC EMC ET /P <>BDC EMC EMC /P <>BDC 5.25 0 0 5.25 447.6106 11.5129 Tm ET ET BT /P <>BDC EMC BT BT -.02 Tc 0 Tc ET BT 7 0 0 7 141.7322 463.9528 Tm /P <>BDC ET BT ( )Tj

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