737 800 fuel capacity pounds

EMC (the CFM LEAP-1A32 variant. EMC EMC /P <>BDC /P <>BDC EMC -.01 Tc /P <>BDC 6.5 0 0 6.5 549.8557 624.9529 Tm 0 Tc /P <>BDC BT ET 7 0 0 7 54.7071 133.7654 Tm EMC ET ET -.01 Tc /P <>BDC -.02 Tc 8 0 0 8 270.7815 771.9528 Tm (0.0142)Tj EMC q ( )Tj BT 7 0 0 7 363.2711 397.9528 Tm ET ET ET 7 0 0 7 294.4014 309.7654 Tm ( )Tj BT 5.25 0 0 5.25 492.6848 11.5129 Tm EMC 8 0 0 8 136.5171 758.9528 Tm EMC ET ET 7 0 0 7 428.6112 386.9528 Tm /P <>BDC /F5 1 Tf EMC .151 .147 .15 rg 6 0 0 6 55.0668 645.9528 Tm EMC ( )Tj -.02 Tc [(BOS-A)56.9(TL)]TJ BT 9 0 0 9 394.0315 786.8898 Tm EMC 6.5 0 0 6.5 64.6596 532.9529 Tm ET 7 0 0 7 535.5029 672.7654 Tm /P <>BDC EMC BT ( )Tj ET ( )Tj 0 Tc 7 0 0 7 337.6855 210.9528 Tm /P <>BDC /P <>BDC 0 Tc EMC In which manual could you find the cross-sectional dimensions of the wing spars and stabilizer (737-300) 7 0 0 7 491.7142 67.7654 Tm BT 9 0 0 9 215.4409 236.8898 Tm (0.0137)Tj ( )Tj ( )Tj ET [(P)11(ayload)]TJ 6.5 0 0 6.5 448.4195 722.9529 Tm /P <>BDC /P <>BDC BT /P <>BDC 9 0 0 9 204.9907 467.8898 Tm ET BT ET (170)Tj 6.5 0 0 6.5 398.369 585.9529 Tm 9 0 0 9 212.5589 148.8898 Tm BT ( )Tj 6 0 0 6 195.6824 659.9528 Tm (38,168)Tj ET /P <>BDC BT ET 7 0 0 7 543.7693 11.5132 Tm 9 0 0 9 215.433 445.8898 Tm The average headwind)Tj ( )Tj EMC 0 Tc /P <>BDC EMC ( )Tj 8 0 0 8 187.3427 675.9528 Tm /P <>BDC 0 Tc 7 0 0 7 247.7395 672.7654 Tm /P <>BDC ET /P <>BDC 9 0 0 9 232.438 170.8898 Tm BT (109,800lbs )Tj /P <>BDC /P <>BDC /P <>BDC BT EMC ( )Tj ET 9 0 0 9 411.0097 60.8898 Tm BT 9 0 0 9 394.0315 544.8898 Tm ET next aircraft -.01 Tc /P <>BDC BT 7 0 0 7 518.4953 309.9528 Tm EMC EMC ET ET BT 7 0 0 7 230.6618 430.9528 Tm 6 0 0 6 115.1719 701.9528 Tm /P <>BDC ET ET (2,220)Tj 6.5 0 0 6.5 336.3428 611.9529 Tm BT I will be very happy to share with you once I get decent results. /F6 1 Tf ( )Tj EMC /P <>BDC ( )Tj ET BT -.02 Tc ET EMC EMC ET -.02 Tc 8 0 0 8 365.7704 619.9528 Tm /P <>BDC BT ( )Tj ET (1,920)Tj /P <>BDC ET (passengers are carried on each of the four)Tj BT /P <>BDC BT ( )Tj ( )Tj EMC BT q EMC (0.0129)Tj BT (0.0133)Tj ET BT 168 0 obj EMC ET ET BT -.02 Tc ( )Tj 5.25 0 0 5.25 525.4061 11.5132 Tm .151 .147 .15 rg endobj ET BT BT EMC ET 7 0 0 7 258.2805 694.7654 Tm EMC EMC /P <>BDC 0 Tc ET The CFM56-7B26 engine on the heavier weight 7 0 0 7 86.3128 540.7654 Tm EMC EMC EMC BT (1, which is 5% higher than the same)Tj BT EMC ET EMC ET ET ET BT (20)Tj EMC 0 Tc 7 0 0 7 554.7883 639.7654 Tm BT EMC /P <>BDC EMC BT ET EMC (150)Tj BT EMC /P <>BDC 7 0 0 7 108.6215 738.9528 Tm 1 i 7 0 0 7 338.5674 166.9528 Tm /P <>BDC ( )Tj -.02 Tc /P <>BDC BT -.02 Tc 0 Tc BT /P <>BDC EMC -.01 Tc 3-Tank Classics, 20,800kgs for NG/MAX's and up to 37,712kgs for BBJ's depending ( )Tj ET BT ET /P <>BDC ET EMC 0 Tc /P <>BDC /P <>BDC BT 7 0 0 7 99.5912 705.9528 Tm (34,650)Tj /P <>BDC ET [(S)8(eats)]TJ 9 0 0 9 197.9514 148.8898 Tm BT BT 7 0 0 7 537.7804 364.9528 Tm EMC EMC BT /P <>BDC /P <>BDC ET EMC EMC /P <>BDC 0 Tc ET EMC EMC 6 0 0 6 527.6392 715.9528 Tm /P <>BDC ( )Tj /P <>BDC ( )Tj ( )Tj BT ( )Tj ET BT (2,732)Tj EMC BT ET permissible, provided the following are met: The standard number of fuel tanks is three. /P <>BDC /P <>BDC ET BT ET (428,060)Tj /P <>BDC /P <>BDC 9 0 0 9 568.555 82.8898 Tm BT ET -.02 Tc 7 0 0 7 99.8582 408.7654 Tm /P <>BDC 7 0 0 7 37.5838 738.9528 Tm ET ET -.02 Tc ET ET ET /P <>BDC /P <>BDC BT /P <>BDC /P <>BDC ET ET ET 0 Tc This is larger)Tj 9 0 0 9 215.4409 269.8898 Tm BT /P <>BDC (0.0113)Tj /P <>BDC (passengers and the 737-900ER\(W\) 152)Tj 9 0 0 9 383.331 401.8898 Tm EMC (Boeing aircraft, the 737-800 has a 2.5%)Tj 6 0 0 6 475.3427 715.9528 Tm BT ( )Tj ( )Tj ( )Tj W n ( )Tj ( )Tj ( )Tj BT /P <>BDC ET ET EMC ( )Tj 7 0 0 7 279.1575 441.9528 Tm EMC ET ET ( )Tj /P <>BDC 9 0 0 9 192.1006 456.8898 Tm /P <>BDC (5,183)Tj .023 .567 .626 RG ( )Tj ET EMC 7 0 0 7 386.3929 716.9528 Tm (2,431)Tj 7 0 0 7 141.7322 111.9528 Tm EMC (171,520)Tj EMC -.02 Tc (The fuel tank capacity means the)Tj 7 0 0 7 230.7317 639.9528 Tm ( )Tj EMC /P <>BDC ET 0 Tc 9 0 0 9 246.595 302.8898 Tm ET ET (CFM56-)Tj EMC /P <>BDC EMC ( )Tj (3,693)Tj ET 7 0 0 7 469.2222 11.5129 Tm -.02 Tc /P <>BDC 0 J 0 j 5 w 10 M [] 0 d 7 0 0 7 474.7064 276.9528 Tm /P <>BDC EMC BT (277,248)Tj BT BT ET ( )Tj BT EMC BT BT ET ( )Tj /P <>BDC BT ET EMC -.02 Tc -.02 Tc 7 0 0 7 444.737 430.7654 Tm ET W n ET 0 Tc ( )Tj ( )Tj 0 Tc /P <>BDC ( )Tj (aircraft again in the future. ET (1,272)Tj /P <>BDC EMC ( )Tj BT EMC ( 2021)Tj BT ET ET EMC (342,312)Tj -.02 Tc BT EMC Airbus A320 History a new player in the short-haul market. 9 0 0 9 552.2312 676.8898 Tm /Artifact <>BDC /P <>BDC The 800 being based of the 400 is designed for short routes. ET BT BT This fuel would give a EMC ET ET /P <>BDC /P <>BDC /P <>BDC BT ET (. 0 Tc ET 7 0 0 7 537.7804 320.9528 Tm EMC 7 0 0 7 536.3849 265.7654 Tm -.02 Tc BT -.02 Tc ( )Tj -.02 Tc /P <>BDC BT Q /P <>BDC (208)Tj /GS1 gs [(CFM L)17.1(E)-8.1(AP-1A32)]TJ ET 9 0 0 9 190.2715 38.8898 Tm ( )Tj -.02 Tc BT ( )Tj (can carry the 150-passenger payload. BT BT BT ET (112)Tj BT EMC EMC ET EMC EMC BT /GS2 gs EMC 7 0 0 7 193.1059 683.9528 Tm BT 7 0 0 7 250.5326 100.7654 Tm BT 0 Tc EMC ET ET /P <>BDC EMC 9 0 0 9 394.0315 445.8898 Tm ( )Tj /P <>BDC (A320ceo)Tj 7 0 0 7 278.2756 78.9528 Tm BT 9 0 0 9 534.7515 599.8898 Tm (passenger seat capacity as the older models)Tj ET /P <>BDC (cost index calculated by the airline to the)Tj ET /P <>BDC 7 0 0 7 37.6993 386.9528 Tm EMC /P <>BDC -.02 Tc ET EMC EMC ( )Tj ET (170)Tj BT 7 0 0 7 297.632 694.9528 Tm BT /P <>BDC ET Hi All, ET ( )Tj BT (flight and block time, wind components,)Tj BT ( )Tj ( )Tj (- mins)Tj BT -2.5295 -5.0573 -2.1058 -5.3146 -1.5527 -5.3151 c BT BT 0 Tc 6 0 0 6 226.1079 659.9528 Tm ET 7 0 0 7 439.7405 584.9528 Tm /P <>BDC BT ET 7 0 0 7 141.7322 166.9528 Tm 9 0 0 9 36.8504 148.8898 Tm -.02 Tc (. (152)Tj -.02 Tc 0 Tc EMC (108 on BOS-SEA \(Seattle\); 123 on BOS-)Tj 0 Tc ( )Tj ET (603)Tj ET BT q 1 0 0 1 215.431 128.878 cm 0 0 m -.02 Tc (original equipment manufacturer \(OEM\))Tj EMC 9 0 0 9 394.0315 412.8898 Tm BT (176)Tj /P <>BDC BT [(T)53.9(r)10(acked distance - nm)]TJ BT ( )Tj 6.5 0 0 6.5 54.877 663.9529 Tm BT 7 0 0 7 439.7405 529.9528 Tm BT EMC BT 0 Tc EMC ( )Tj 9 0 0 9 554.3696 269.8898 Tm BT (A320ceo)Tj /P <>BDC ( )Tj BT EMC 7 0 0 7 387.0932 221.9528 Tm /Artifact <>BDC /P <>BDC ET /P <>BDC less heating from the smaller hydraulic system A. 9 0 0 9 551.4784 797.8898 Tm EMC /P <>BDC 8 0 0 8 82.2047 771.9528 Tm -.02 Tc BT 7 0 0 7 204.0935 727.7654 Tm 9 0 0 9 142.2128 335.8898 Tm BT 9 0 0 9 215.433 324.8898 Tm EMC /P <>BDC /P <>BDC (29,359)Tj /P <>BDC 6 0 0 6 215.4988 701.9528 Tm EMC ET /P <>BDC 9 0 0 9 522.1112 247.8898 Tm BT [(MR)32(TX - lbs)]TJ BT ET EMC BT 9 0 0 9 394.0157 632.8898 Tm EMC .41 .161 .508 rg ( )Tj ET 9 0 0 9 376.0468 401.8898 Tm BT EMC /P <>BDC ( )Tj /P <>BDC 7 0 0 7 54.7071 463.7654 Tm BT ET It sports its powerful crew and passenger carrying abilities elegantly as it takes flight. /P <>BDC ET EMC ET BT BT /F4 1 Tf BT ET -.02 Tc EMC (. BT EMC ET BT ET BT 10 0 0 10 54.8804 814.1973 Tm -.02 Tc /F4 1 Tf -.02 Tc ET BT BT /P <>BDC EMC /P <>BDC ET EMC BT 9 0 0 9 215.4313 82.8898 Tm BT ( )Tj 1 g /P <>BDC /P <>BDC 9 0 0 9 215.4409 104.8898 Tm EMC EMC ET EMC BT ET ET /P <>BDC 0 Tc 9 0 0 9 571.9847 181.8898 Tm /P <>BDC BT 7 0 0 7 362.3891 144.9528 Tm /P <>BDC BT ET 7 0 0 7 344.1175 595.7654 Tm ( )Tj 7 0 0 7 537.7804 89.9528 Tm EMC EMC /P <>BDC -.02 Tc 9 0 0 9 394.0237 203.8898 Tm (I)Tj ET S ( )Tj 7 0 0 7 487.0872 11.5129 Tm EMC 0 Tc 9 0 0 9 173.6527 500.8898 Tm 7 0 0 7 439.2087 199.9528 Tm EMC 7 0 0 7 118.104 67.7654 Tm BT EMC /P <>BDC 0 Tc BT (seat layout of 16/18/126 as the A320ceo,)Tj ( )Tj BT 9 0 0 9 372.0688 324.8898 Tm 9 0 0 9 411.0097 214.8898 Tm ET ET EMC ET EMC EMC -.02 Tc EMC BT BT BT ET EMC (A320neo, A321neo, 737-800, 737-)Tj BT EMC BT BT ET /P <>BDC -.02 Tc ET BT /P <>BDC BT (150)Tj ET EMC ET BT ( )Tj BT .023 .567 .626 rg BT 0 Tc ET /P <>BDC EMC 7 0 0 7 344.1175 617.7654 Tm (reduce the variability caused by differences)Tj BT EMC BT /P <>BDC ( )Tj EMC EMC /P <>BDC ET EMC (travelled for the aircraft on each route is)Tj /P <>BDC BT /F4 1 Tf BT 6.5 0 0 6.5 332.6961 735.9529 Tm 0 Tc ET ( )Tj 9 0 0 9 191.3244 324.8898 Tm EMC ET 9 0 0 9 182.0482 379.8898 Tm /P <>BDC (this study, the 737-9 is operated with the)Tj EMC EMC 9 0 0 9 394.0237 467.8898 Tm 9 0 0 9 411.0181 159.8898 Tm ET (977)Tj BT ET BT .014984 841.89 609.45 -841.89 re EMC (increase in seat numbers a newer type)Tj BT /P <>BDC -.01 Tc ( )Tj /P <>BDC -.02 Tc BT EMC ( )Tj W n EMC /P <>BDC 0 Tc BT ET ET ET ET ET /P <>BDC ET EMC BT EMC 9 0 0 9 53.8582 324.8898 Tm /P <>BDC /P <>BDC /GS1 gs /P <>BDC BT EMC BT EMC (737-800W)Tj 8 0 0 8 38.4438 731.9528 Tm )Tj /F4 1 Tf ET EMC 0 Tc 6.5 0 0 6.5 480.4 637.9529 Tm EMC 0 Tc 6 0 0 6 184.9964 715.9528 Tm BT 7 0 0 7 101.0963 89.9528 Tm EMC BT 9 0 0 9 551.4604 269.8898 Tm /P <>BDC /P <>BDC BT EMC BT EMC /P <>BDC 7 0 0 7 54.7071 485.7654 Tm ET (39,270)Tj fuel temp -45C or freezing 0 Tc 8 0 0 8 43.6039 731.9528 Tm ET BT /F4 1 Tf BT ET ET EMC 9 0 0 9 411.0097 181.8898 Tm BT /P <>BDC 0 Tc [(BOS-SE)-13.9(A)]TJ ET ET 9 0 0 9 394.0237 390.8898 Tm ET BT 9 0 0 9 343.6557 148.8898 Tm /P <>BDC /P <>BDC EMC (CFM56-7B26)Tj ( )Tj 6.5 0 0 6.5 296.4841 676.9529 Tm /P <>BDC ( )Tj BT 19.841 0 l 9 0 0 9 366.7762 390.8898 Tm EMC 0 Tc ( )Tj ( )Tj /P <>BDC ET 0 Tc EMC /P <>BDC 7 0 0 7 88.196 11.5129 Tm EMC BT BT ET ET BT BT ET /P <>BDC 0 Tc (39,270)Tj /P <>BDC 7 0 0 7 457.0984 232.7654 Tm 6.5 0 0 6.5 398.3298 650.9529 Tm ( )Tj /P <>BDC ET The A320neos ASM)Tj 9 0 0 9 374.6152 269.8898 Tm ( )Tj (to allow a clearer performance and fuel)Tj ( )Tj BT 7 0 0 7 537.7804 243.9528 Tm ( )Tj ET EMC ( )Tj 7 0 0 7 37.6993 430.9528 Tm BT EMC ( )Tj 9 0 0 9 394.0123 258.8898 Tm /P <>BDC /P <>BDC EMC EMC ET (35,112)Tj -.01 Tc (In the same trend as on the A320)Tj /P <>BDC ET ET 5.25 0 0 5.25 73.853 11.5132 Tm 8 0 0 8 95.6042 633.9528 Tm ET 6 0 0 6 403.6028 743.9528 Tm 9 0 0 9 411.0097 390.8898 Tm /F4 1 Tf /P <>BDC 7 0 0 7 518.4953 331.9528 Tm EMC ET 9 0 0 9 547.562 126.8898 Tm 0 Tc /P <>BDC EMC -.01 Tc BT 0 Tw /P <>BDC 9 0 0 9 68.0071 577.8898 Tm BT ( )Tj 7 0 0 7 82.2047 628.9528 Tm ET 7 0 0 7 118.104 463.7654 Tm 9 0 0 9 232.4217 434.8898 Tm [(A3)24.9(21neo v)12.9(ersus 7)-33(3)8.1(7-9 )]TJ ( )Tj EMC BT BT EMC /P <>BDC /GS2 gs -.01 Tc 7 0 0 7 490.7815 265.9528 Tm 0 Tc -.02 Tc (A321neo:)Tj BT EMC ET ET 7 0 0 7 247.7395 694.7654 Tm BT ET BT ET -.02 Tc The trigger for the scavenge pump is different for the series as follows: NB On the classics, when departing with less than 1,000kg of fuel in the centre tank, an imbalance may occur during ET [(BOS-Y)-49.1(VR)]TJ BT /P <>BDC This includes the weight of the plane, which is about 41,000 kg (90,000 lbs), and the weight of the fuel which is about 18,000 kg (40,000 lbs). EMC ( )Tj /P <>BDC BT ET ( )Tj BT ET ET (174,606)Tj 7 0 0 7 37.5838 540.9528 Tm EMC 6.5 0 0 6.5 397.5498 558.9529 Tm EMC /P <>BDC ET ET (the aircraft variants. (35,112)Tj /P <>BDC 7 0 0 7 299.0601 210.9528 Tm ( )Tj 0 Tc ( )Tj BT 8 0 0 8 394.0237 82.8898 Tm /P <>BDC (206,132lbs, an MLW of 171,500lbs, and)Tj BT /P <>BDC (31,416)Tj ET 0 Tc 9 0 0 9 36.8504 181.8898 Tm EMC (737-9)Tj BT EMC /P <>BDC BT (163)Tj BT /P <>BDC ( )Tj /P <>BDC 9 0 0 9 232.4217 588.8898 Tm /P <>BDC /P <>BDC 9 0 0 9 213.7241 467.8898 Tm ( )Tj ( )Tj ET BT /F1 1 Tf EMC ET ET 0 Tc Q ET /GS1 gs /P <>BDC /P <>BDC ET ( )Tj ET /GS2 gs EMC ( )Tj - 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. BT BT ET 9 0 0 9 68.0314 335.8898 Tm /P <>BDC 9 0 0 9 411.0181 269.8898 Tm EMC /P <>BDC 9 0 0 9 215.4313 225.8898 Tm EMC EMC EMC EMC BT BT EMC Any)Tj ET BT BT 9 0 0 9 377.4407 764.8898 Tm 7 0 0 7 535.5029 177.7654 Tm (ASM. ET -.015 Tc (35,112)Tj ET (also impact the actual flight time. EMC 9 0 0 9 552.0261 555.8898 Tm /P <>BDC BT EMC EMC BT 6.5 0 0 6.5 192.4489 545.9529 Tm ( )Tj 6 0 0 6 164.6501 715.9528 Tm ET ET 9 0 0 9 187.3661 445.8898 Tm 7 0 0 7 321.6356 342.9528 Tm EMC (of being configured like those of the)Tj (159,251)Tj .0081 Tc EMC (34,650)Tj /P <>BDC 0 Tc /P <>BDC ( )Tj ET 7 0 0 7 439.2087 265.9528 Tm 9 0 0 9 552.6437 434.8898 Tm ET BT /P <>BDC ( )Tj (CFM56-7B26)Tj BT 6.5 0 0 6.5 448.2959 585.9529 Tm EMC ET ET BT /P <>BDC (157,300)Tj EMC ET ET 6.5 0 0 6.5 296.4841 702.9529 Tm BT ET ( )Tj EMC BT BT EMC 0 841.89 609.449 -841.89 re BT EMC /GS2 gs /P <>BDC /P <>BDC /P <>BDC EMC 7 0 0 7 279.1575 309.9528 Tm /P <>BDC -.02 Tc 7 0 0 7 299.0601 133.9528 Tm (\(see table, page 19\))Tj 7 0 0 7 338.6433 133.7654 Tm 6 0 0 6 418.9814 701.9528 Tm EMC BT All data presented is for entertainment purposes and should not be used operationally. ( )Tj EMC 7 0 0 7 355.3163 89.7654 Tm /P <>BDC 0 Tc /P <>BDC /P <>BDC ( )Tj EMC EMC ( )Tj 9 0 0 9 232.438 214.8898 Tm 8 0 0 8 38.4438 619.9528 Tm (1,705)Tj 9 0 0 9 425.183 544.8898 Tm (166,090)Tj (alternates used and their distance from the)Tj 7 0 0 7 158.74 430.7654 Tm ET /P <>BDC (737-8)Tj /P <>BDC 7 0 0 7 354.4763 738.7654 Tm EMC 0 Tc BT EMC 7 0 0 7 355.3163 67.7654 Tm /P <>BDC 6.5 0 0 6.5 379.1824 565.9529 Tm -.02 Tc 7 0 0 7 82.8504 342.9528 Tm 9 0 0 9 352.4841 313.8898 Tm (7,379)Tj ET ET EMC ET ET 9 0 0 9 232.4217 335.8898 Tm BT EMC BT EMC ET /P <>BDC /P <>BDC BT 7 0 0 7 158.74 78.7654 Tm EMC (to 165 passengers on BOS-LAX. BT BT /P <>BDC 7 0 0 7 521.4089 11.5132 Tm BT /P <>BDC ET 9 0 0 9 36.8504 60.8898 Tm EMC (141,270)Tj EMC EMC BT BT [(737-900E)-33(R)]TJ ET EMC EMC BT BT /P <>BDC endstream ET /P <>BDC ET BT 7 0 0 7 37.6993 78.9528 Tm (0.0122)Tj ET BT BT (37,653lbs)Tj EMC BT /P <>BDC /P <>BDC 6.5 0 0 6.5 64.6596 585.9529 Tm BT EMC BT BT (Engine)Tj /P <>BDC Cheers Peter. (20)Tj ET 0 Tc 7 0 0 7 294.4014 397.7654 Tm (150)Tj -.02 Tc ( )Tj ( )Tj ET 7 0 0 7 475.2383 683.9528 Tm ( )Tj BT ET BT EMC . 9 0 0 9 53.8582 588.8898 Tm BT 304.725 420.96 m EMC /P <>BDC ET ET ET ET 7 0 0 7 230.7317 562.9528 Tm ET ( )Tj .12988 .27633 .58575 rg BT /P <>BDC EMC ET (74-82)Tj 7 0 0 7 490.8321 221.7654 Tm ET BT (capacity has been configured as the same)Tj 7 0 0 7 258.2805 166.7654 Tm EMC BT (A320neo)Tj (weight penalty in its OEW compared to its)Tj 137 )Tj BT 9 0 0 9 411.0234 698.8898 Tm EMC design and maintenance of fuel tanks to reduce the chances of such explosions in /P <>BDC BT 9 0 0 9 548.0225 368.8898 Tm BT ( )Tj BT (2,514)Tj (39,270lbs)Tj 9 0 0 9 346.6898 280.8898 Tm 7 0 0 7 187.0858 298.9528 Tm 5.25 0 0 5.25 64.5461 11.5129 Tm 7 0 0 7 520.6108 639.9528 Tm -.02 Tc 0 Tc ET /P <>BDC 0 Tc BT /P <>BDC /P <>BDC ( )Tj (464,270)Tj -.02 Tc 7 0 0 7 158.74 375.7654 Tm /P <>BDC ( )Tj BT 9 0 0 9 195.3413 181.8898 Tm (based on the cost index set is different, it)Tj 5.25 0 0 5.25 123.5367 11.5132 Tm 9 0 0 9 166.1068 313.8898 Tm ( )Tj EMC 9 0 0 9 368.2199 247.8898 Tm /P <>BDC ( )Tj [(SS)-9.1(U)8(E)]TJ EMC ET 7 0 0 7 196.5683 221.7654 Tm /P <>BDC ET BT (737 MAX 8 & 9 fuel)Tj EMC (difference. /P <>BDC /P <>BDC 9 0 0 9 68.3339 467.8898 Tm 36.85 541.416 340.159 263.624 re EMC BT BT /GS1 gs -.02 Tc ET /P <>BDC 9 0 0 9 541.6875 489.8898 Tm /P <>BDC (/S)Tj /P <>BDC EMC ET EMC (0.0129)Tj /P <>BDC ( )Tj ( )Tj /P <>BDC BT EMC /P <>BDC /P <>BDC 7 0 0 7 362.3891 309.9528 Tm BT ET 0 Tc ( )Tj 2002-19-52 which requires the crew to maintain certain minimum fuel ET /F4 1 Tf 0 Tc /F7 1 Tf BT EMC ET BT EMC ( )Tj 7 0 0 7 474.3564 716.9528 Tm BT ET BT ET BT (The A321neo is offered to airlines with)Tj EMC -.02 Tc -.02 Tc 7 0 0 7 326.2278 485.9528 Tm EMC ET EMC 0 Tc BT ( )Tj automatically shut off when they detect a low output pressure and there have BT 7 0 0 7 474.5665 430.9528 Tm BT /P <>BDC ET ET EMC (136)Tj BT (149,300)Tj 6.5 0 0 6.5 64.6596 722.9529 Tm /P <>BDC BT (A321ceo)Tj BT (376)Tj ( )Tj BT BT ( )Tj /OC /MC3431 BDC EMC (maximise their service offering. ET (39,270)Tj EMC ET ET EMC ET 9 0 0 9 215.4313 170.8898 Tm -.02 Tc ET ( )Tj /P <>BDC EMC ET /P <>BDC BT (283)Tj BT 9 0 0 9 36.8583 445.8898 Tm BT 0 Tc ET /P <>BDC BT ET -.02 Tc EMC EMC 6.5 0 0 6.5 327.0283 598.9529 Tm BT EMC ( )Tj 6.5 0 0 6.5 296.2827 598.9529 Tm EMC /P <>BDC ET ( )Tj 28.5749 0 TD ( )Tj ET BT EMC ET (direction lead to a headwind component)Tj 7 0 0 7 125.6292 683.7654 Tm ET /P <>BDC BT EMC /P <>BDC /P <>BDC (O)Tj EMC ET ET 7 0 0 7 337.4684 705.9528 Tm The Boeing 737-800 is together with the 737-600, 737-700 and 737-900 member of the 737-Next Generation-Family. /P <>BDC 5.25 0 0 5.25 40.8474 11.5129 Tm ET ( )Tj BT /F6 1 Tf (418)Tj BT EMC /P <>BDC 7 0 0 7 43.6039 243.9528 Tm /P <>BDC overboard. /P <>BDC -.005 Tc ( )Tj ET EMC -.02 Tc BT 9 0 0 9 202.845 357.8898 Tm BT /F6 1 Tf EMC 9 0 0 9 394.0237 335.8898 Tm EMC 7 0 0 7 60.6117 144.7654 Tm ET 7 0 0 7 355.3163 122.7654 Tm ET ( )Tj BT 9 0 0 9 564.1726 588.8898 Tm EMC EMC /P <>BDC ET ( )Tj ( )Tj BT ET 7 0 0 7 403.478 562.7654 Tm ET /P <>BDC BT 6.5 0 0 6.5 64.6596 611.9529 Tm /P <>BDC /P <>BDC ( )Tj ET ( )Tj /P <>BDC The maximum declarable fuel capacity for tech log, nav log, etc is 16,200kgs for 3-Tank Classics, 20,800kgs for NG/MAX's and up to 37,712kgs for BBJ's depending upon how many tanks the customer has specified (max 12). 9 0 0 9 385.2246 148.8898 Tm ET /P <>BDC /P <>BDC ET ET 0 Tc EMC ET (bypass ratio than the A320/321neo. BT 6 0 0 6 339.9257 729.9528 Tm centre fuel tank. /P <>BDC 8 0 0 8 158.74 760.7654 Tm 304.725 420.96 m BT EMC EMC ( )Tj ET 9 0 0 9 215.4409 423.8898 Tm EMC 0 Tc 5.25 0 0 5.25 447.6106 11.5129 Tm 9 0 0 9 568.6457 357.8898 Tm -.02 Tc 9 0 0 9 394.0123 599.8898 Tm (Block fuel)Tj 7 0 0 7 338.3085 364.9528 Tm -.01 Tc /P <>BDC ET /P <>BDC /P <>BDC ( )Tj EMC 9 0 0 9 418.9315 59.9073 Tm (977)Tj 0 Tc 0 Tc 0 Tc ET ( )Tj -.02 Tc 5.25 0 0 5.25 549.1047 11.5132 Tm ET /P <>BDC BT BT ET BT In November 2005, Boeing unveiled the BBJ3, based on the 737-900ER. BT ET 9 0 0 9 368.9994 225.8898 Tm 7 0 0 7 196.5683 617.7654 Tm (35,112)Tj BT 7 0 0 7 187.0858 133.9528 Tm /P <>BDC EMC /P <>BDC ET I am looking forward to your responses. 0 Tc ( )Tj ET ET ET (1,824)Tj 0 Tc 9 0 0 9 232.438 181.8898 Tm 8 0 0 8 136.4919 661.9528 Tm [(BL)32(OCK F)8.1(UEL)31( PERF)8.1(ORMANCE OF A3)24.9(20CEO, A3)24.9(20NEO, A3)24.9(21CEO, A3)24.9(21NEO, 7)-33(3)8.1(7-800, 7)-33(3)8(7-900ER, 7)-33(3)8(7-8 & 7)-33(3)8.1(7-9 - P)30(A)52(YL)32(O)6.1(AD SCENARIO 2 )]TJ EMC [(Aircr)10(aft type)]TJ ET (6,875)Tj BT BT /P <>BDC (170)Tj -.02 Tc ET 7 0 0 7 363.2711 386.9528 Tm EMC 3.0566 -3.9073 l (1.5 mm) thick, the extent of the frost is similar on both wings, the frost is on or between the black lines defining ET ET (152)Tj /P <>BDC .151 .147 .15 rg .151 .147 .15 rg ET /P <>BDC /P <>BDC )Tj /P <>BDC ET ET (CFM56-7B27B3)Tj EMC EMC ET EMC 7 0 0 7 427.7291 199.9528 Tm -.02 Tc 9 0 0 9 394.0123 632.8898 Tm BT /P <>BDC /P <>BDC ET BT /P <>BDC (powered by either the CFM56-5 series or)Tj ( )Tj (737-800W)Tj BT EMC ET EMC /P <>BDC 7 0 0 7 445.619 606.7654 Tm ET EMC 0 Tc ET /P <>BDC /P <>BDC /P <>BDC /P <>BDC 9 0 0 9 200.4401 258.8898 Tm EMC (188,400)Tj (MAX family. ET ( )Tj BT BT ET ET (PPS flight planning software is used to)Tj BT (assumed that no additional cargo is taken)Tj 0 Tc BT BT /P <>BDC BT BT /P <>BDC /P <>BDC /P <>BDC BT (831)Tj 10 0 0 10 425.05 814.1973 Tm -.01 Tc ( )Tj BT (an improvement in fuel cost per ASM of)Tj 7 0 0 7 82.2047 474.9528 Tm ( )Tj EMC (maximum passenger payload of 160. EMC BT ET BT 7 0 0 7 158.74 100.7654 Tm BT BT BT ( )Tj 5.25 0 0 5.25 55.7484 11.5132 Tm 9 0 0 9 36.8504 181.8898 Tm /P <>BDC BT 9 0 0 9 203.484 192.8898 Tm EMC ET 7 0 0 7 316.0679 331.7654 Tm /P <>BDC EMC /P <>BDC ( )Tj BT ET 9 0 0 9 73.1083 489.8898 Tm 503.542 90.794 m BT EMC EMC EMC 7 0 0 7 37.6993 408.9528 Tm /P <>BDC ET EMC EMC BT (O)Tj ET BT ET BT /P <>BDC BT /GS1 gs BT ET EMC ET EMC ET 680kg; All other series: 453kg, Main tanks to be full if centre contains over 453kg, If a fuel gauge is u/s the quantity 0 Tc /P <>BDC 9 0 0 9 367.0732 423.8898 Tm ET 7 0 0 7 490.5101 628.9528 Tm ( )Tj ( )Tj ET 7 0 0 7 187.0858 397.9528 Tm EMC /P <>BDC /F4 1 Tf BT 7 0 0 7 554.7883 320.7654 Tm BT BT ( )Tj (shorter sectors. 9 0 0 9 561.5176 522.8898 Tm /P <>BDC 0 Tc -.02 Tc BT ET BT ET -.02 Tc EMC ET BT ET 9 0 0 9 232.438 478.8898 Tm This)Tj BT ET EMC 7 0 0 7 82.2047 463.9528 Tm ET /P <>BDC BT ET EMC /P <>BDC 9 0 0 9 36.8504 148.8898 Tm 9 0 0 9 432.7111 49.1073 Tm 0 Tc ET BT /P <>BDC BT 6.5 0 0 6.5 296.5232 585.9529 Tm 7 0 0 7 99.8582 595.7654 Tm -.02 Tc ET 9 0 0 9 348.0922 511.8898 Tm ET EMC /P <>BDC ( )Tj /P <>BDC EMC EMC ET BT EMC 9 0 0 9 215.433 170.8898 Tm /P <>BDC ( )Tj /F4 1 Tf ( )Tj /P <>BDC /P <>BDC EMC EMC ( )Tj ( )Tj ET (3,069)Tj /P <>BDC 0 Tc ( )Tj ET 9 0 0 9 408.1889 324.8898 Tm BT BT EMC ( )Tj BT 7 0 0 7 294.4014 320.7654 Tm 9 0 0 9 36.8583 467.8898 Tm

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