/P <>BDC BT /P <>BDC (CFM56-5B3/P)Tj EMC EMC cumulative errors it is recommended that the wings are filled once every few ( )Tj /P <>BDC EMC ET ( )Tj BT 7 0 0 7 258.2805 738.7654 Tm 6.5 0 0 6.5 499.1812 663.9529 Tm /P <>BDC (aircraft types, all the flights were evaluated)Tj 7 0 0 7 554.7883 419.7654 Tm ( )Tj BT /P <>BDC 9 0 0 9 545.0725 434.8898 Tm ET ET /P <>BDC ET available a Boeing 737 for modification and testing. (170)Tj /P <>BDC ET BT BT 7 0 0 7 294.4014 595.7654 Tm ET ET 0 Tc /P <>BDC 9 0 0 9 411.0097 599.8898 Tm 8 0 0 8 520.6337 771.7654 Tm 7 0 0 7 158.74 419.7654 Tm /P <>BDC 9 0 0 9 374.0663 335.8898 Tm -.02 Tc /P <>BDC /P <>BDC ( C)Tj BT (35,112)Tj EMC ET EMC -.02 Tc ( )Tj /P <>BDC ( )Tj This is because it)Tj 7 0 0 7 294.4014 727.7654 Tm ET 7 0 0 7 247.7395 628.7654 Tm -.02 Tc /P <>BDC ET (LEAP-1B engine. 7 0 0 7 54.7071 122.7654 Tm EMC ET EMC ET EMC ET 9 0 0 9 215.433 434.8898 Tm 9 0 0 9 515.9449 654.8898 Tm EMC BT /P <>BDC BT /P <>BDC (All the flights were in a westerly)Tj EMC /P <>BDC EMC 7 0 0 7 99.8582 144.7654 Tm ET BT BT ET ET ET ET ET 0 Tc ( )Tj ( )Tj ( )Tj 0 Tc (68.3 inches and a bypass ratio of up to)Tj 1 i BT EMC 7 0 0 7 82.8504 353.9528 Tm EMC ET /P <>BDC BT BT 8 0 0 8 334.994 619.9528 Tm 7 0 0 7 554.7883 496.7654 Tm (thereby giving it a seat capacity of 160)Tj 6.5 0 0 6.5 375.6529 702.9529 Tm BT ET EMC ET 9 0 0 9 215.433 401.8898 Tm BT /P <>BDC /P <>BDC ( )Tj BT 9 0 0 9 394.0157 511.8898 Tm /P <>BDC EMC ET (A321neo)Tj 7 0 0 7 196.5683 617.7654 Tm (The main operating parameters are: )Tj -.02 Tc (5,277)Tj -.02 Tc ET /P <>BDC ET ET /P <>BDC ET 6.5 0 0 6.5 477.8064 676.9529 Tm ( )Tj ET 7 0 0 7 338.3085 342.9528 Tm -.02 Tc .151 .147 .15 rg 0 Tc ET capacitors in the tanks with fuel acting as the dielectric. EMC /F1 1 Tf BT Boeing 737 800 Hainan Airlines Alan Wilson. /P <>BDC /P <>BDC /P <>BDC /P <>BDC BT ET /P <>BDC /P <>BDC endobj 6.5 0 0 6.5 549.8557 585.9529 Tm EMC 9 0 0 9 411.0234 676.8898 Tm BT /P <>BDC 6.5 0 0 6.5 447.8411 663.9529 Tm ( )Tj /F1 1 Tf EMC BT .014984 841.89 609.45 -841.89 re 7 0 0 7 403.478 628.7654 Tm ( )Tj ET ( )Tj 7 0 0 7 247.7395 496.7654 Tm BT /P <>BDC 9 0 0 9 36.8504 181.8898 Tm [(OEW/DO)7.1(W - lbs)]TJ BT ET BT /P <>BDC ( )Tj 13 0 0 13 36.8504 412.8898 Tm ( )Tj BT 7 0 0 7 473.8245 364.9528 Tm EMC EMC EMC EMC 9 0 0 9 497.8043 313.8898 Tm BT EMC 9 0 0 9 53.8578 280.8898 Tm (planning software was allowed to optimise)Tj /P <>BDC .151 .147 .15 rg 7 0 0 7 456.4753 573.7654 Tm 7 0 0 7 298.514 628.9528 Tm 8 0 0 8 187.3427 675.9528 Tm EMC EMC ET ET EMC EMC ET ET ( )Tj 5.25 0 0 5.25 64.5461 11.5129 Tm 56 0 0 56 36.8606 622.1944 Tm 9 0 0 9 53.8582 291.8898 Tm EMC ( )Tj EMC 9 0 0 9 229.6064 456.8898 Tm (977)Tj ET ( )Tj 7 0 0 7 54.7071 430.7654 Tm /P <>BDC /P <>BDC ( C)Tj /P <>BDC /P <>BDC BT ( )Tj ( )Tj 7 0 0 7 536.3849 628.7654 Tm [(OM)8.1(M)-12.9(E)-24.9(R)7.1(C)8.1(E)]TJ 0 Tc BT 3.0566 -3.9073 l BT 9 0 0 9 466.0881 203.8898 Tm 7 0 0 7 343.2355 496.7654 Tm -.02 Tc 0 Tc EMC ET /P <>BDC BT ET 0 Tc 9 0 0 9 53.8582 731.8898 Tm BT EMC /P <>BDC BT )Tj /P <>BDC 7 0 0 7 474.3564 562.9528 Tm /P <>BDC -.02 Tc /P <>BDC ( )Tj /P <>BDC (manufacturers, with Airbus reducing the)Tj EMC /P <>BDC (between: the Pratt & Whitney PW1127G,)Tj ET ( )Tj 9 0 0 9 36.8583 335.8898 Tm EMC /P <>BDC /P <>BDC ET EMC 13 0 0 13 411.0097 467.8898 Tm EMC )21(The )]TJ 5 0 0 5 484.5872 11.5129 Tm /P <>BDC BT 0 Tc EMC EMC 8 0 0 8 554.6981 771.7654 Tm BT ET 6.5 0 0 6.5 379.0655 650.9529 Tm ( )Tj ( )Tj ET 9 0 0 9 566.3776 192.8898 Tm 7 0 0 7 130.1443 419.7654 Tm BT EMC 7 0 0 7 490.8321 540.7654 Tm BT /P <>BDC 7 0 0 7 107.1165 573.9528 Tm 7 0 0 7 539.8962 573.9528 Tm 0 Tc EMC ET /F1 1 Tf ( )Tj BT /F1 1 Tf ET For example, if the fuel tank maximum capacity is 10,000 KG, then the tolerance of the gauging is 0.02 (airplane without a densitometer) * 10000 = 200 KG. 0 Tc (allow a direct comparison of trip fuel burn)Tj EMC 6 0 0 6 277.7663 673.9528 Tm ET 7 0 0 7 474.5665 430.9528 Tm (flight and block time, wind components,)Tj ET 6.5 0 0 6.5 296.3931 532.9529 Tm EMC )Tj (404)Tj /P <>BDC BT ET ET 7 0 0 7 337.6855 573.9528 Tm BT (economics of the aircraft types with more)Tj EMC /P <>BDC EMC /P <>BDC BT ET )Tj BT 9 0 0 9 411.0097 93.8898 Tm 0 Tc BT 7 0 0 7 82.2047 716.9528 Tm BT ( )Tj /P <>BDC (170)Tj BT BT /P <>BDC 0 Tc (A320neo:)Tj /P <>BDC /P <>BDC EMC (. BT ET 7 0 0 7 294.4014 342.7654 Tm ET ET EMC ( )Tj ( )Tj /F7 1 Tf The fwd and aft tanks are switched off when the ( )Tj BT ( )Tj 9 0 0 9 418.9315 59.9073 Tm /P <>BDC 7 0 0 7 108.6215 738.9528 Tm ET 7 0 0 7 101.0963 287.9528 Tm ET ET /P <>BDC )Tj 7 0 0 7 539.8962 463.9528 Tm /P <>BDC EMC ET EMC EMC ET ( )Tj ET EMC ( )Tj 10 0 0 10 50.1204 814.1973 Tm /P <>BDC /P <>BDC /P <>BDC BT ET ET ET 7 0 0 7 130.1443 716.7654 Tm EMC /P <>BDC 7 0 0 7 387.0932 375.9528 Tm 6 0 0 6 433.8509 687.9528 Tm BT ET BT ( )Tj 7 0 0 7 99.8582 683.7654 Tm EMC (1,272)Tj ET ET ( )Tj /P <>BDC BT EMC BT ET ET BT 7 0 0 7 380.2788 287.7654 Tm 7 0 0 7 141.7322 507.9528 Tm 7 0 0 7 299.0601 320.9528 Tm ( )Tj BT EMC /P <>BDC 0 Tc 0 Tc 9 0 0 9 349.9551 302.8898 Tm (performed with both engines operating to)Tj ( )Tj [(CFM L)17.1(E)-8.1(AP-1B27)]TJ (10)Tj /P <>BDC W* n ( )Tj EMC ET 7 0 0 7 54.7071 496.7654 Tm 5 0 0 5 484.5872 11.5129 Tm ET BT /P <>BDC EMC EMC /P <>BDC ET ET EMC -.02 Tc EMC (difference. /P <>BDC /P <>BDC EMC Due to airframe)Tj /P <>BDC ET BT BT /P <>BDC /P <>BDC ( )Tj /P <>BDC 7 0 0 7 199.5784 441.7654 Tm /F6 1 Tf BT 7 0 0 7 554.7883 485.7654 Tm /P <>BDC /P <>BDC /P <>BDC (follow in their footsteps, having already)Tj BT (145,505)Tj ( )Tj ET EMC ET (35,112)Tj [(OM)8(M)-13(E)-25(R)7(C)8(E)]TJ ET 0 841.89 609.449 -841.89 re 9 0 0 9 232.4217 291.8898 Tm /P <>BDC ET /P <>BDC 0 Tc upper surface of the wings where this frost is allowable for despatch under the EMC 7 0 0 7 158.74 540.7654 Tm 0 Tc /P <>BDC 9 0 0 9 215.4313 478.8898 Tm .151 .147 .15 rg /P <>BDC ( )Tj ( )Tj EMC ET 10 0 0 10 408.34 814.1973 Tm 0 Tc /P <>BDC ET 0 Tc BT BT EMC 9 0 0 9 394.0123 115.8898 Tm BT /Artifact <>BDC /OC /MC2261 BDC ( )Tj (482)Tj BT EMC 7 0 0 7 491.7142 529.7654 Tm ET ET ET /P <>BDC (4,158)Tj EMC 0 Tc BT 0 Tc /P <>BDC EMC BT BT EMC (3,341)Tj q 1 0 0 1 505.328 82.247 cm 0 0 m ET EMC BT ( )Tj BT EMC /P <>BDC ET EMC /P <>BDC ( )Tj /P <>BDC BT 9 0 0 9 408.2047 753.8898 Tm Economy-plus is also)Tj EMC BT 9 0 0 9 36.8504 379.8898 Tm 7 0 0 7 187.0858 562.9528 Tm ET /P <>BDC 7 0 0 7 362.3891 331.9528 Tm /P <>BDC ET BT 7 0 0 7 365.035 617.9528 Tm (sector. -.02 Tc /P <>BDC ( )Tj -.02 Tc 8 0 0 8 302.5117 675.9528 Tm BT ET ( )Tj 6.5 0 0 6.5 282.0695 735.9529 Tm ( )Tj ( )Tj BT EMC 7 0 0 7 445.619 496.7654 Tm ET BT -.02 Tc /P <>BDC /P <>BDC 0 Tc ET BT EMC 7 0 0 7 258.2805 408.7654 Tm ( )Tj BT EMC 0 Tc ET /P <>BDC /P <>BDC BT (LEAP-1B. EMC /P <>BDC 137 )Tj 7 0 0 7 99.8582 562.7654 Tm EMC ( )Tj BT /P <>BDC 7 0 0 7 297.632 727.9528 Tm -.02 Tc BT /P <>BDC 8 0 0 8 404.6235 771.7654 Tm 6.5 0 0 6.5 295.7432 545.9529 Tm 0 Tc -.01 Tc /GS2 gs BT BT EMC EMC BT -.02 Tc BT ( )Tj ET BT BT 7 0 0 7 491.7142 408.7654 Tm ET /P <>BDC BT EMC BT 7 0 0 7 99.8582 485.7654 Tm EMC ET ET EMC 9 0 0 9 190.0677 203.8898 Tm EMC BT 0 Tc ET BT 7 0 0 7 474.3564 617.9528 Tm BT /P <>BDC EMC /GS1 gs /P <>BDC /P <>BDC EMC ET BT /P <>BDC BT BT ( )Tj BT EMC -.02 Tc /P <>BDC /P <>BDC 7 0 0 7 196.5683 518.7654 Tm EMC BT BT EMC 0 Tc /P <>BDC EMC EMC /P <>BDC BT W n BT 9 0 0 9 394.0157 368.8898 Tm BT ( )Tj 8 0 0 8 439.2348 771.9528 Tm 5.25 0 0 5.25 492.6848 11.5129 Tm ( )Tj ( )Tj 7 0 0 7 299.0601 364.9528 Tm ET 0 Tc BT ET /P <>BDC /OC /MC5093 BDC BT (403-418)Tj 9 0 0 9 36.8504 115.8898 Tm BT /P <>BDC ET EMC EMC EMC EMC BT 7 0 0 7 299.0601 243.9528 Tm 7 0 0 7 490.8321 177.7654 Tm ET /P <>BDC EMC EMC /P <>BDC EMC 7 0 0 7 179.5605 122.9528 Tm EMC EMC 7 0 0 7 520.6108 683.9528 Tm /P <>BDC The charges are split by weight)Tj ET /P <>BDC EMC /P <>BDC .0081 Tc ET /P <>BDC /P <>BDC EMC 7 0 0 7 445.619 408.7654 Tm BT ( )Tj EMC ( )Tj BT (1,824)Tj (105)Tj (. /P <>BDC BT 7 0 0 7 337.6855 496.9528 Tm 9 0 0 9 391.7137 104.8898 Tm 9 0 0 9 392.5848 379.8898 Tm EMC -.015 Tc 6.5 0 0 6.5 273.8079 702.9529 Tm This is because the RH centre tank pump will stop feeding due to the ET ET BT ( )Tj /P <>BDC 9 0 0 9 391.278 313.8898 Tm 9 0 0 9 394.0157 390.8898 Tm (LRC; the same as the primary sector. /P <>BDC ( )Tj /P <>BDC 7 0 0 7 141.7322 144.9528 Tm BT 7 0 0 7 440.0906 276.9528 Tm BT 7 0 0 7 54.7071 705.7654 Tm ( )Tj -.02 Tc /P <>BDC BT BT BT ET EMC ET ET (economy cabin, but some airlines can)Tj 7 0 0 7 82.2047 694.9528 Tm ( )Tj 9 0 0 9 552.6886 533.8898 Tm EMC EMC BT ( )Tj EMC /P <>BDC ET (126,312)Tj ET What was the Super Sonic Transport (SST) Concorde plane?? EMC ( )Tj /P <>BDC EMC ET BT 9 0 0 9 346.8148 104.8898 Tm ET ET BT /P <>BDC BT ( )Tj /P <>BDC /P <>BDC 7 0 0 7 446.5009 716.7654 Tm ET EMC ET EMC 9 0 0 9 215.433 368.8898 Tm /P <>BDC BT EMC The website is currently in the process of optimizing and will have further functions added in order to improve the usability. 6 0 0 6 561.1918 743.9528 Tm -.02 Tc ET ET 515.808 82.238 l 7 0 0 7 241.2727 562.9528 Tm ET EMC BT /P <>BDC ET ( )Tj /P <>BDC ET BT EMC 6.5 0 0 6.5 244.3689 532.9529 Tm BT Hi Ben, BT ET (Like the A321neo, the 737-9 has a)Tj BT 7 0 0 7 365.035 628.9528 Tm (207,336)Tj 9 0 0 9 394.0157 214.8898 Tm /P <>BDC EMC /GS1 gs ET BT 7 0 0 7 258.2805 661.7654 Tm EMC 7 0 0 7 95.225 11.5132 Tm /P <>BDC 7 0 0 7 113.1366 518.9528 Tm BT 9 0 0 9 53.8582 104.8898 Tm ET [(BOS-SE)-13.9(A)]TJ (better for the A321neo due to its increased)Tj /P <>BDC ET /P <>BDC ( )Tj -.02 Tc /P <>BDC ET (CFM56-7B26)Tj ET ET ( )Tj ET ET BT /P <>BDC 6 0 0 6 277.7064 715.9528 Tm 7 0 0 7 355.3163 133.7654 Tm /P <>BDC BT [(AIRL)8.1(INE & AIR)7.1(CRAF)-12.9(T)18.1( OPERA)56.9(T)-8.1(ION)-13.9(S)]TJ (2.5% lower fuel burn for the 737-800. BT 9 0 0 9 187.498 676.8898 Tm 7 0 0 7 337.6855 111.9528 Tm ( )Tj (between the aircraft types even greater. 304.725 420.96 m /P <>BDC ( )Tj BT /P <>BDC 9 0 0 9 386.3055 687.8898 Tm ET BT 7 0 0 7 108.6215 529.9528 Tm /P <>BDC ET ET BT /P <>BDC BT 6 0 0 6 365.7265 729.9528 Tm EMC ET 7 0 0 7 518.4953 122.9528 Tm ET BT ET )Tj BT allow for a measurement of fuel tank inerting and heating during the BT BT BT /P <>BDC EMC q 1 0 0 1 508.103 86.641 cm 0 0 m 0 Tc EMC ET 7 0 0 7 242.1547 672.9528 Tm tank is refuelled. BT 9 0 0 9 411.0181 368.8898 Tm /P <>BDC EMC the most hazardous condition-an empty center wing tank-that GBI would remain 9 0 0 9 394.0237 412.8898 Tm EMC EMC ET /GS2 gs ( )Tj /F6 1 Tf /P <>BDC 9 0 0 9 394.0237 390.8898 Tm ( )Tj BT 6 0 0 6 247.3662 673.9528 Tm BT EMC EMC (\(neo\) families, and the 737NG family. EMC /P <>BDC /P <>BDC 7 0 0 7 539.8962 694.9528 Tm 7 0 0 7 487.0872 11.5129 Tm ET /P <>BDC (CFM56-5B4/P)Tj ( )Tj /P <>BDC BT 7 0 0 7 429.157 672.9528 Tm EMC 8 0 0 8 124.845 577.9528 Tm BT q 1 0 0 1 411.023 799.878 cm 0 0 m 0 Tc EMC BT W n ET BT BT EMC /P <>BDC EMC BT BT (4,218)Tj ( )Tj EMC -.02 Tc 9 0 0 9 206.8496 346.8898 Tm /P <>BDC EMC EMC -.02 Tc BT ET ET 9 0 0 9 36.8504 60.8898 Tm /Figure <>BDC 7 0 0 7 37.0536 617.9528 Tm 9 0 0 9 53.8582 599.8898 Tm ET 7 0 0 7 54.7071 67.7654 Tm ET /P <>BDC EMC BT EMC 9 0 0 9 53.8578 159.8898 Tm EMC ET ET -.02 Tc (44,352)Tj (influence the payloads carried and the)Tj (166,090)Tj ET 0 Tc BT EMC BT 9 0 0 9 204.5367 93.8898 Tm ET /P <>BDC EMC EMC /GS1 gs ET /P <>BDC EMC ET 9 0 0 9 369.2608 38.8898 Tm /P <>BDC EMC BT ET ET ET /P <>BDC ( )Tj ET 0 Tc ET EMC (passenger numbers are 136 for the)Tj -.02 Tc EMC BT ( )Tj BT EMC BT 5.25 0 0 5.25 100.8225 11.5132 Tm 0 Tc /P <>BDC 7 0 0 7 125.6292 683.7654 Tm ET 9 0 0 9 185.7888 489.8898 Tm EMC /P <>BDC ( )Tj /P <>BDC 9 0 0 9 215.433 313.8898 Tm ET EMC The APU uses fuel from the number 1 tank. ( )Tj EMC 7 0 0 7 534.621 100.7654 Tm 9 0 0 9 36.8583 423.8898 Tm /P <>BDC BT (192 seats. 0 Tc ET 7 0 0 7 381.1608 595.7654 Tm )Tj ( )Tj BT /P <>BDC ET 9 0 0 9 374.887 346.8898 Tm 7 0 0 7 258.2805 342.7654 Tm 9 0 0 9 542.4784 115.8898 Tm (175,047)Tj EMC EMC BT -.02 Tc /P <>BDC BT EMC ( )Tj (The fuel burn improvement on the)Tj 7 0 0 7 326.2278 727.9528 Tm ET ET /F6 1 Tf BT 7 0 0 7 36.8504 11.5129 Tm 0 Tc EMC EMC BT EMC EMC BT EMC EMC BT ET /P <>BDC /P <>BDC ET /P <>BDC ET BT /P <>BDC ET -.02 Tc /P <>BDC BT BT This is larger)Tj ( )Tj EMC ( )Tj EMC 7 0 0 7 158.74 507.7654 Tm EMC 232.441 655.706 340.157 -624.522 re (977)Tj 8 0 0 8 258.2687 771.7654 Tm 17 0 0 17 36.8606 742.1944 Tm EMC (160, which is the same total as on the)Tj ET /P <>BDC /P <>BDC Fully . 7 0 0 7 182.5706 144.9528 Tm BT ET ( )Tj BT /P <>BDC 0 841.89 609.449 -841.89 re BT ( )Tj /P <>BDC BT ET ET (passengers fewer than the A321ceo )Tj BT EMC 9 0 0 9 187.8892 159.8898 Tm The total tolerance for the FQIS system is based on a full tank. ET ET /P <>BDC BT BT 6 0 0 6 55.0668 715.9528 Tm ( )Tj /P <>BDC EMC ET EMC ET 0 Tc (170)Tj ET /P <>BDC ( )Tj S BT (2,800 -)Tj EMC ET /P <>BDC BT /P <>BDC ET BT /P <>BDC 1 i ET ET .014984 841.89 609.45 -841.89 re (737-8)Tj ( )Tj ET 6 0 0 6 258.3167 715.9528 Tm EMC EMC 6.5 0 0 6.5 295.8145 611.9529 Tm EMC EMC 9 0 0 9 394.0123 335.8898 Tm BT ( )Tj BT 304.725 420.96 m /P <>BDC EMC /P <>BDC /P <>BDC (CFM56-7B27B3)Tj 7 0 0 7 130.1443 320.7654 Tm EMC EMC EMC ET -.02 Tc ET 7 0 0 7 82.2047 562.9528 Tm BT /P <>BDC /P <>BDC /P <>BDC BT EMC ( )Tj BT -.02 Tc BT 9 0 0 9 36.8504 269.8898 Tm EMC ET BT /P <>BDC ( )Tj (483)Tj /P <>BDC 0 Tc BT 0 Tc BT ET ET /P <>BDC ET 9 0 0 9 388.6428 357.8898 Tm 8 0 0 8 243.3422 771.9529 Tm ( )Tj ET (the analysis is 20/29/143, so a total of 192)Tj ( )Tj ET EMC ET Q ( )Tj /P <>BDC BT /P <>BDC ET /P <>BDC BT BT 9 0 0 9 394.0157 588.8898 Tm -.02 Tc ET 8 0 0 8 412.41 771.9529 Tm Happy Flying. /P <>BDC ET ET BT ET (737-8)Tj /P <>BDC ( )Tj EMC /P <>BDC 9 0 0 9 378.9498 368.8898 Tm ET EMC EMC ET /P <>BDC /P <>BDC BT BT BT 8 0 0 8 141.7322 771.9528 Tm 9 0 0 9 547.562 126.8898 Tm ET /P <>BDC EMC BT EMC EMC Is the same happening with the 737? (BOS, and take 10 minutes to taxi in at all)Tj EMC (31,416)Tj (450,780)Tj /P <>BDC ET BT 6 0 0 6 379.0815 771.9528 Tm /F4 1 Tf EMC BT BT ET EMC BT /P <>BDC 8 0 0 8 471.0755 760.9528 Tm 9 0 0 9 369.0981 93.8898 Tm !! BT -.02 Tc 7 0 0 7 158.74 485.7654 Tm (-53)Tj -.01 Tc /P <>BDC The)Tj EMC BT EMC BT BT ET -.02 Tc /P <>BDC (96,500)Tj (ratio of 5.1:1. /P <>BDC (distance - nm )Tj (CFM56-7B27B3)Tj EMC /P <>BDC BT (273,750)Tj BT BT [(CFM L)17.1(E)-8.1(AP-)]TJ EMC BT 9 0 0 9 36.8504 148.8898 Tm BT BT BT EMC EMC 7 0 0 7 279.1575 419.9528 Tm EMC BT /P <>BDC EMC /P <>BDC 9 0 0 9 51.0236 71.8898 Tm ( )Tj Just wondering, where did you get the information about what specific aluminium alloys are used on different parts of the aircraft? EMC 9 0 0 9 193.8472 236.8898 Tm /P <>BDC ( N)Tj /P <>BDC /P <>BDC /P <>BDC /P <>BDC ( )Tj 7 0 0 7 158.74 694.7654 Tm BT (CFM56-7B26)Tj /P <>BDC (2,481)Tj 7 0 0 7 54.7071 408.7654 Tm ()Tj EMC 9 0 0 9 187.2749 610.8898 Tm (190,800)Tj /P <>BDC ET /P <>BDC 9 0 0 9 186.1613 49.8898 Tm start a self test of the display and the fuel quantity indicating system. 8 0 0 8 225.1837 717.9528 Tm ET ET EMC BT BT EMC 7 0 0 7 54.7071 419.7654 Tm 7 0 0 7 536.3849 507.7654 Tm ET BT The)Tj /P <>BDC EMC ( )Tj document.getElementById( "ak_js_1" ).setAttribute( "value", ( new Date() ).getTime() ); Airbus A320 Introduction The very popular short haul airliner. ET /P <>BDC /P <>BDC ( )Tj /P <>BDC /P <>BDC EMC EMC /P <>BDC ET 0 Tc 6.5 0 0 6.5 176.1172 585.9529 Tm /P <>BDC 0 Tc 0 Tc 7 0 0 7 404.101 342.7654 Tm /P <>BDC /P <>BDC ET ET 7 0 0 7 490.5101 595.9528 Tm BT ( )Tj 6 0 0 6 130.4965 771.9528 Tm 7 0 0 7 354.4763 705.7654 Tm ( )Tj 9 0 0 9 394.0315 654.8898 Tm /P <>BDC BT 7 0 0 7 491.7142 507.7654 Tm BT BT BT 0 Tc EMC ET BT .151 .147 .15 rg 8 0 0 8 60.6117 771.7654 Tm tank. 7 0 0 7 444.737 177.7654 Tm EMC /Figure <>BDC 9 0 0 9 348.3267 324.8898 Tm 7 0 0 7 158.74 606.7654 Tm ET /P <>BDC BT -.02 Tc ET BT -.02 Tc BT (the A320ceo. ET 9 0 0 9 552.2312 676.8898 Tm 7 0 0 7 247.7395 298.7654 Tm What are the Specs of the Airbus A380 Super Jumbo? EMC ( )Tj EMC EMC EMC ET EMC 6 0 0 6 301.1609 687.9528 Tm ET BT BT BT 7 0 0 7 258.2805 386.7654 Tm EMC 0 J 0 j 15 w 10 M [] 0 d ET 0 J 0 j .5 w 10 M [] 0 d ( )Tj /P <>BDC ET 10 0 0 10 417.91 814.1973 Tm EMC /P <>BDC BT ( )Tj ET [(CFM L)17.1(E)-8.1(AP-1A26)]TJ The seat configuration)Tj ET 6.5 0 0 6.5 244.0438 722.9529 Tm ( )Tj ET EMC (10)Tj BT -.02 Tc BT S BT -.02 Tc /P <>BDC EMC ( )Tj /P <>BDC EMC 7 0 0 7 354.6933 529.7654 Tm /P <>BDC 7 0 0 7 258.2805 287.7654 Tm 7 0 0 7 247.7395 683.7654 Tm ET (fan diameter of 81 inches, and a bypass)Tj EMC /P <>BDC BT EMC EMC The Boeing 737-800 has a maximum fuel capacity of 6,875 gallons or 26,020 liters. ET 6.5 0 0 6.5 244.4599 702.9529 Tm ( C)Tj EMC EMC /P <>BDC (1,825)Tj EMC EMC BT EMC ET /P <>BDC EMC ( )Tj BT 7 0 0 7 518.3203 430.9528 Tm ET BT BT /F6 1 Tf /P <>BDC 6 0 0 6 426.8235 743.9528 Tm BT EMC -.02 Tc ET 9 0 0 9 68.0071 357.8898 Tm ET BT /P <>BDC 0 Tc BT BT BT BT 7 0 0 7 444.737 188.7654 Tm BT ( )Tj BT EMC q 1 0 0 1 394.016 758.971 cm 0 0 m ( )Tj EMC BT BT ET 9 0 0 9 384.8177 445.8898 Tm /P <>BDC EMC EMC 7 0 0 7 247.7395 507.7654 Tm BT (maintenance. EMC 6.5 0 0 6.5 274.6269 689.9529 Tm 9 0 0 9 455.0733 60.8898 Tm 7 0 0 7 294.4014 331.7654 Tm ( )Tj EMC 7 0 0 7 241.5317 408.9528 Tm x&o[v?vr&D6oi#9v I7JW\'18pLq2qN8hbeebfvlV7pr (1,272)Tj -.02 Tc BT ET BT BT EMC EMC /P <>BDC EMC /P <>BDC BT (208)Tj /GS2 gs /OC /MC477 BDC ( )Tj 7 0 0 7 148.0554 11.5132 Tm ET /P <>BDC EMC -.01 Tc ET 9 0 0 9 426.0987 687.8898 Tm (163)Tj ET /P <>BDC /P <>BDC ET /P <>BDC ET EMC ( )Tj 0 Tc 8 0 0 8 83.5638 619.9528 Tm BT EMC /P <>BDC BT 0 Tc EMC 7 0 0 7 182.5706 573.9528 Tm EMC /P <>BDC Boeing 787 Dreamliner Orders and Deliveries. /P <>BDC EMC (163,900)Tj 0 Tc BT BT EMC ET BT 0 Tc EMC EMC ET 6.5 0 0 6.5 243.3486 742.9529 Tm BT 7 0 0 7 440.0906 408.9528 Tm /P <>BDC 9 0 0 9 527.3954 313.8898 Tm BT 7 0 0 7 294.4014 430.7654 Tm ( )Tj ET ( )Tj ( )Tj /P <>BDC -.01 Tc ET EMC EMC BT ET BT ( )Tj 9 0 0 9 530.7301 59.9073 Tm /P <>BDC ET BT /P <>BDC BT EMC 9 0 0 9 189.8338 49.8898 Tm /P <>BDC /P <>BDC 0 Tc ET /P <>BDC ET ( )Tj ET -.02 Tc /P <>BDC -.02 Tc EMC EMC EMC -.01 Tc /P <>BDC BT 9 0 0 9 267.0826 500.8898 Tm 10 0 0 10 52.6304 814.1973 Tm ET The fuel was fed EMC /P <>BDC ET 0 Tc -.02 Tc BT EMC /P <>BDC 7 0 0 7 299.0601 419.9528 Tm EMC EMC ET 7 0 0 7 108.6215 727.9528 Tm BT EMC ET /P <>BDC ( )Tj /P <>BDC ET -.02 Tc BT ET ET ( )Tj /P <>BDC BT EMC ET -.02 Tc BT ( )Tj ( )Tj BT 9 0 0 9 394.0237 335.8898 Tm 9 0 0 9 564.1726 588.8898 Tm /P <>BDC ET /GS2 gs /P <>BDC BT EMC BT 9 0 0 9 186.0353 291.8898 Tm BT BT ( )Tj [(M)21(T)39.1(O)7.1(W)0( / seat - lbs )]TJ EMC EMC EMC BT ET ( )Tj ( )Tj EMC BT 9 0 0 9 36.8504 390.8898 Tm /P <>BDC EMC ET (179)Tj 505.325 82.247 l EMC EMC BT BT BT (This weight variant is one of more than 20)Tj /P <>BDC EMC 7 0 0 7 279.1575 309.9528 Tm -.01 Tc -.02 Tc W n /P <>BDC EMC ( )Tj 7 0 0 7 430.039 694.9528 Tm 7 0 0 7 321.6356 419.9528 Tm /GS1 gs (132,872)Tj ET /P <>BDC 7 0 0 7 354.6933 496.7654 Tm 6.5 0 0 6.5 191.8316 637.9529 Tm EMC -407.02 814.197 m 7 0 0 7 379.3969 188.7654 Tm /P <>BDC ET /P <>BDC BT /P <>BDC /P <>BDC EMC the rear of the fwd hold and the front of the aft hold, this reduces the C of G EMC ( 2021)Tj EMC /P <>BDC /P <>BDC EMC BT (1,823)Tj ( )Tj ( )Tj ET (A)Tj ET EMC 0 Tc /P <>BDC ET EMC ET 0 Tc ( )Tj (737-800W)Tj ET /P <>BDC BT BT ( )Tj BT BT /OC /MC188 BDC BT ET BT /P <>BDC EMC ( )Tj /P <>BDC EMC EMC /P <>BDC /P <>BDC 9 0 0 9 187.8353 522.8898 Tm Boeing supplied 10,574 since initial development as of 2020. The 737-200Adv could also be fitted with an EMC 6.5 0 0 6.5 172.8217 565.9529 Tm /P <>BDC 9 0 0 9 36.8504 49.8898 Tm (98,500)Tj /P <>BDC 7 0 0 7 43.6039 551.9528 Tm 9 0 0 9 232.4217 236.8898 Tm BT ET /P <>BDC Do you have a reference please? ( )Tj 0 Tc -.01 Tc BT EMC /P <>BDC ET 9 0 0 9 571.3269 38.8898 Tm /P <>BDC /P <>BDC BT ET ET EMC ET BT -.02 Tc 7 0 0 7 456.2165 474.7654 Tm EMC ET ET EMC (31,416)Tj ET -.005 Tc /P <>BDC EMC BT ET /P <>BDC /P <>BDC ET EMC Im glad you got something out of our site that was helpful. /P <>BDC ET /GS2 gs BT /P <>BDC /P <>BDC 7 0 0 7 298.514 562.9528 Tm (CFM56-7B26 engine on the heavier weight)Tj 9 0 0 9 389.0497 445.8898 Tm BT ET BT /P <>BDC EMC 7 0 0 7 241.2727 276.9528 Tm EMC 9 0 0 9 308.8233 346.8898 Tm /P <>BDC -.02 Tc 0 Tc -.02 Tc -.02 Tc /P <>BDC 0 Tc EMC ( )Tj 7 0 0 7 536.3849 67.7654 Tm 8 0 0 8 394.0157 753.8898 Tm ( )Tj EMC BT 0 Tc /P <>BDC BT /P <>BDC (977)Tj 0 Tc 9 0 0 9 565.9277 60.8898 Tm ET EMC BT /P <>BDC ET EMC 0 Tc 7 0 0 7 518.4953 320.9528 Tm EMC ( )Tj ( )Tj /P <>BDC EMC BT .008 Tc BT /P <>BDC (The longer sectors produce lower fuel)Tj ET 7 0 0 7 77.36 11.5132 Tm 9 0 0 9 200.4718 38.8898 Tm ( )Tj 9 0 0 9 215.4409 368.8898 Tm 0 841.89 609.449 -841.89 re 9 0 0 9 568.6457 357.8898 Tm EMC BT 9 0 0 9 232.4217 379.8898 Tm ( )Tj ET EMC ET 7 0 0 7 554.7883 727.7654 Tm 8 0 0 8 314.3535 703.9528 Tm (31,416)Tj 0 Tc /P <>BDC /P <>BDC /P <>BDC ( )Tj 505.331 89.873 m 0 Tc EMC ET /P <>BDC ET ( )Tj ET 9 0 0 9 68.3339 500.8898 Tm /P <>BDC EMC /P <>BDC 9 0 0 9 173.7412 203.8898 Tm 9 0 0 9 341.1717 478.8898 Tm /P <>BDC BT (0.0109)Tj /P <>BDC ( )Tj /P <>BDC BT /P <>BDC 0 Tc (sharklets. /P <>BDC /P <>BDC /P <>BDC -.02 Tc ET EMC BT /P <>BDC 9 0 0 9 492.5143 500.8898 Tm ET ET (have therefore been removed from the)Tj EMC 0 Tc BT 7 0 0 7 387.0932 111.9528 Tm ET ( )Tj ET 9 0 0 9 214.7728 247.8898 Tm /P <>BDC /P <>BDC .014984 841.89 609.45 -841.89 re ET ET /P <>BDC /P <>BDC /P <>BDC 8 0 0 8 456.5927 771.7654 Tm EMC The 737-800 is used in airlines such as Aircal, Delta Air Lines, New York Air and United Airlines just to name a few. 7 0 0 7 315.1859 144.7654 Tm EMC BT ( )Tj 9 0 0 9 411.0181 236.8898 Tm /F6 1 Tf /GS2 gs ET [(Aircr)10(aft type)]TJ /P <>BDC 9 0 0 9 374.0759 203.8898 Tm 0 Tc /P <>BDC EMC /P <>BDC /P <>BDC [(CFM L)17.1(E)-8.1(AP-1B27)]TJ Reads payload (passenger and baggage) weights via FSUIPC. ET ET ET ET ET 7 0 0 7 36.8504 11.5129 Tm 9 0 0 9 200.4401 258.8898 Tm 9 0 0 9 53.8582 709.8898 Tm BT EMC BT BT BT EMC 0 J 0 j 5 w 10 M [] 0 d ( )Tj ( )Tj The FAA developed an in-flight gas sampling system, integrated with /P <>BDC BT EMC BT 7 0 0 7 539.8962 727.9528 Tm (977)Tj -.02 Tc EMC -.01 Tc -.02 Tc BT BT 7 0 0 7 491.4046 188.9528 Tm ET /P <>BDC ET 7 0 0 7 37.5838 254.9528 Tm -.02 Tc ET 7 0 0 7 404.101 276.7654 Tm -.02 Tc 7 0 0 7 241.5317 419.9528 Tm EMC (50,800)Tj BT BT [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ BT 7 0 0 7 535.5029 122.7654 Tm EMC BT 7 0 0 7 491.4046 331.9528 Tm ET 9 0 0 9 215.433 346.8898 Tm /P <>BDC 0 Tc /P <>BDC 6 0 0 6 195.6824 659.9528 Tm ET 17 0 0 17 526.2604 775.1944 Tm (. BT ET (1,058)Tj EMC ( )Tj BT BT /OC /MC2278 BDC /P <>BDC EMC 6 0 0 6 246.7063 757.9528 Tm ET /P <>BDC ET BT 9 0 0 9 394.0237 368.8898 Tm ET EMC EMC ( )Tj (cost per ASM ranges from 0.06 to 0.16)Tj ET EMC [(the A320neo)16.1(. ET BT /P <>BDC /P <>BDC 6.5 0 0 6.5 121.1068 532.9529 Tm In real)Tj ( )Tj /P <>BDC 7 0 0 7 491.7142 606.7654 Tm ET -.02 Tc ( )Tj (405)Tj ET /P <>BDC BT ET 7 0 0 7 158.74 595.7654 Tm BT ET /P <>BDC ET /P <>BDC EMC 9 0 0 9 394.0237 500.8898 Tm /P <>BDC I think in the table you are talking about the range where payload is limited by MTOW. BT 6.5 0 0 6.5 376.7644 742.9529 Tm The cause of the accident was determined to be a malfunctioning left radar altimeter. ET 7 0 0 7 474.7064 232.9528 Tm 7 0 0 7 230.7317 111.9528 Tm EMC ET 6 0 0 6 55.0668 743.9528 Tm ( )Tj /P <>BDC /P <>BDC EMC ET 0 Tc BT EMC (is 0.01 to 0.15 cents better than the)Tj [(CFM L)17.1(E)-8.1(AP-1A32)]TJ ET /GS1 gs (The fuel tank capacity means the)Tj ET BT EMC EMC ET BT EMC ET ( )Tj (56,901)Tj ( )Tj 10 0 0 10 64.6596 794.2914 Tm /P <>BDC -.02 Tc BT /P <>BDC 0 Tc BT /P <>BDC -.02 Tc /F6 1 Tf /P <>BDC 9 0 0 9 36.8504 82.8898 Tm ( )Tj EMC (seat capacity as the 737-800 due to the exit)Tj The information is surely out there, but maybe the questions need to be a bit more specific. )Tj /P <>BDC /P <>BDC /P <>BDC /P <>BDC EMC ET (152)Tj ET Boeing 737 Interior. ET EMC EMC ( )Tj 7 0 0 7 440.0906 188.9528 Tm EMC EMC 0 Tc 8 0 0 8 302.5117 717.9528 Tm 9 0 0 9 75.273 500.8898 Tm 0 Tc BT EMC BT 9 0 0 9 534.7635 203.8898 Tm BT The CFM56-7B26 engine on the heavier weight ET /P <>BDC ET EMC 7 0 0 7 230.7317 144.9528 Tm ET /P <>BDC /P <>BDC BT ET BT BT /P <>BDC 7 0 0 7 82.8504 232.9528 Tm ( )Tj EMC EMC EMC ET ET BT BT 9 0 0 9 425.1913 214.8898 Tm BT BT /P <>BDC For the wheels, I will give you two measurements. EMC /P <>BDC Out of the 135 passengers on board there were 9 fatalities and 84 suffered injuries. ( )Tj 7 0 0 7 520.6108 496.9528 Tm ( )Tj 9 0 0 9 551.1635 181.8898 Tm BT ET ET EMC 0 Tc /OC /MC2269 BDC BT BT -.02 Tc EMC 0 Tc -.02 Tc EMC /P <>BDC 6.5 0 0 6.5 172.7047 598.9529 Tm /P <>BDC (block fuel burn performance of up to)Tj BT 7 0 0 7 387.0159 507.9528 Tm 6 0 0 6 195.3167 715.9528 Tm ( )Tj BT BT ET BT 9 0 0 9 53.8338 192.8898 Tm EMC 9 0 0 9 192.6957 346.8898 Tm (page\))Tj (2,933)Tj EMC ET 0 Tc ( )Tj ET /P <>BDC BT /P <>BDC ( )Tj BT /P <>BDC (32,000lbs of thrust, a fan diameter of 78)Tj /P <>BDC ET BT (airport. 7 0 0 7 67.798 11.5132 Tm BT BT EMC /P <>BDC 9 0 0 9 36.8504 467.8898 Tm EMC ET How many square feet (or cubic feet) of space is in the 737 MAX flight deck? /P <>BDC /P <>BDC EMC ET /P <>BDC BT (1,272)Tj /P <>BDC ( )Tj ET ( )Tj ( )Tj EMC /P <>BDC BT ET BT This is equivalent to)Tj EMC /P <>BDC BT 9 0 0 9 53.8582 665.8898 Tm (I)Tj EMC 7 0 0 7 163.8846 11.5132 Tm 8 0 0 8 38.4438 619.9528 Tm 7 0 0 7 294.4014 375.7654 Tm (newer aircraft types will have the same)Tj (Block time)Tj BT BT air speed, altitude, and similar flight parameters were made available from EMC ET BT EMC /P <>BDC ET /P <>BDC -.01 Tc (1, which is 5% higher than the same)Tj /P <>BDC ET The accuracy tolerance of the fuel flow transmitter is a function of the fuel flow. 9 0 0 9 524.3162 214.8898 Tm ( )Tj /P <>BDC ET 0 Tc /P <>BDC .151 .147 .15 rg 0 Tc (112)Tj ( )Tj -.02 Tc BT 9 0 0 9 342.6025 368.8898 Tm 7 0 0 7 537.7804 111.9528 Tm EMC EMC EMC ET BT ( )Tj BT ( )Tj .151 .147 .15 rg EMC EMC 0 Tc EMC <>/XObject<>/ExtGState<>/Properties<>>> BT EMC 0 Tc /P <>BDC Regarding winglets, I think Simple Flying explains it well. /P <>BDC 6.5 0 0 6.5 528.5291 689.9529 Tm ET BT /P <>BDC 0 Tc EMC 8 0 0 8 314.3535 619.9528 Tm 6 0 0 6 238.0716 687.9528 Tm EMC /P <>BDC ET 0 Tc S ET ET /P <>BDC Is the Range with Max Payload NM(Km) wrong? 7 0 0 7 37.8848 452.9528 Tm BT /P <>BDC BT BT (ASM is 0.09 cents better for the A321neo. BT EMC EMC ( )Tj (across the world, since they are proven to)Tj BT (between 420nm and 2,429nm )Tj BT EMC 6.5 0 0 6.5 346.3049 702.9529 Tm BT /P <>BDC BT ET 7 0 0 7 210.1137 265.7654 Tm 9 0 0 9 394.0237 346.8898 Tm EMC ET BT ( )Tj /P <>BDC 0 Tc EMC ET ET EMC 9 0 0 9 215.4313 60.8898 Tm ET ET EMC 6 0 0 6 496.2034 757.9528 Tm /P <>BDC ET EMC .008 Tc BT 7 0 0 7 279.1575 89.9528 Tm 0 Tc 7 0 0 7 99.8582 232.7654 Tm EMC -.02 Tc (rating on the CFM LEAP-1A32 to)Tj BT EMC ( )Tj (Federal Aviation Administration) have cleaned up their act and made the MAX as safe an airliner as its predecessors. /P <>BDC EMC ET -.02 Tc BT ET ET BT 7 0 0 7 491.7142 628.7654 Tm BT The average fuel)Tj BT /P <>BDC ( )Tj /P <>BDC 7 0 0 7 491.4046 111.9528 Tm 9 0 0 9 387.3578 258.8898 Tm (483)Tj ( )Tj ET BT EMC BT ET (737-8)Tj 7 0 0 7 456.2165 166.7654 Tm EMC /P <>BDC /P <>BDC 9 0 0 9 215.433 115.8898 Tm ET EMC ( )Tj BT EMC /P <>BDC The weight increase in)Tj /P <>BDC EMC 7 0 0 7 241.5317 738.9528 Tm /P <>BDC BT ET 7 0 0 7 118.104 661.7654 Tm EMC 17 0 0 17 36.8606 758.6944 Tm BT /P <>BDC ( )Tj .41 .161 .508 RG BT ET 63 0 obj EMC BT ET EMC -.02 Tc ET BT EMC ( )Tj .001 Tc EMC ( )Tj (page 21\))Tj ( )Tj BT BT [(P)11(ayload)]TJ EMC 7 0 0 7 113.1366 320.9528 Tm ET ( )Tj BT .151 .147 .15 rg ET ( )Tj ET EMC 0 Tc EMC BT ET /P <>BDC (26,000lbs thrust on the A320neo powered)Tj
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