737 800 fuel capacity pounds737 800 fuel capacity pounds
/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
Ustica Lines Boat Crash, Biggest Elephant Tusks Ever Recorded, Mobile Homes For Rent In Marlboro County, Sc, Articles OTHER
Ustica Lines Boat Crash, Biggest Elephant Tusks Ever Recorded, Mobile Homes For Rent In Marlboro County, Sc, Articles OTHER