( C)Tj 7 0 0 7 491.7142 496.7654 Tm -.02 Tc 9 0 0 9 378.6646 797.8898 Tm 8 0 0 8 540.2806 60.8898 Tm BT /P <>BDC 9 0 0 9 53.8338 280.8898 Tm /P <>BDC 7 0 0 7 204.0935 309.7654 Tm ( )Tj ( )Tj -.02 Tc EMC .498 .4095 .5623 .1043 v /P <>BDC BT ET -.02 Tc ET EMC EMC (34,650lbs)Tj 7 0 0 7 403.478 694.7654 Tm EMC /P <>BDC BT (2,518)Tj BT ET .151 .147 .15 rg EMC (4,787)Tj 9 0 0 9 257.2834 214.8898 Tm 7 0 0 7 70.1644 540.9528 Tm BT EMC -.02 Tc ET EMC BT .0161 Tc /P <>BDC EMC ET BT (The comparison of the A320ceo)Tj /P <>BDC /P <>BDC ET 7 0 0 7 457.0984 89.7654 Tm -.02 Tc /P <>BDC 7 0 0 7 326.2278 496.9528 Tm 0 Tc BT /P <>BDC BT BT BT /F1 1 Tf (CFM56-7B27B3)Tj ( )Tj 7 0 0 7 539.8962 606.9528 Tm (410,271)Tj 9 0 0 9 368.9649 423.8898 Tm 7 0 0 7 439.2087 243.9528 Tm BT /F4 1 Tf Cheers Peter, Thanks, peter! BT 6.5 0 0 6.5 295.5027 565.9529 Tm 9 0 0 9 367.8099 335.8898 Tm BT /P <>BDC ET EMC BT ( )Tj EMC BT 9 0 0 9 232.4217 313.8898 Tm 9 0 0 9 187.8443 346.8898 Tm -.02 Tc 0 Tw ( )Tj ET /P <>BDC (0.0119)Tj EMC 7 0 0 7 380.2788 463.7654 Tm BT BT We dont actually have access to a table of these variants and their features. (3,916)Tj 9 0 0 9 53.8338 368.8898 Tm Hi. /P <>BDC /P <>BDC /P <>BDC -.02 Tc 6.5 0 0 6.5 499.7986 637.9529 Tm ET EMC (evaluation both taxi-out and taxi-in were)Tj 7 0 0 7 241.5317 309.9528 Tm ET ET /P <>BDC EMC ( )Tj 0 Tc EMC BT ET /P <>BDC (2,748)Tj EMC [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ 0 Tc 7 0 0 7 107.1165 474.9528 Tm BT .001 Tc BT 6 0 0 6 527.699 701.9528 Tm BT EMC ET (As with the comparison of the)Tj (5,448)Tj ET EMC 0 Tc (same 85% passenger payload of 136. 0 Tc 9 0 0 9 365.3999 511.8898 Tm 7 0 0 7 456.2165 342.7654 Tm EMC /P <>BDC (fuel capacity of 6,303USG )Tj EMC 7 0 0 7 247.7395 243.7654 Tm -.02 Tc EMC /GS1 gs /P <>BDC (seat layout of 16/18/126 as the A320ceo,)Tj EMC 8 0 0 8 43.6039 619.9528 Tm 7 0 0 7 279.1575 287.9528 Tm 7 0 0 7 518.4953 331.9528 Tm ( )Tj /P <>BDC (0.0123)Tj -.02 Tc BT /P <>BDC EMC 9 0 0 9 232.438 357.8898 Tm /P <>BDC (1,074)Tj /P <>BDC ET ET BT BT ( )Tj ET /P <>BDC ET /P <>BDC ET BT ( )Tj [(AIRL)8.1(INE & AIR)7.1(CRAF)-12.9(T)18.1( OPERA)56.9(T)-8.1(ION)-13.9(S)]TJ (ASM is 0.09 cents better for the A321neo. ET /P <>BDC ET The aircraft broke into 3 pieces after crashing. -.01 Tc .0161 Tc ( )Tj ET /P <>BDC BT 6 0 0 6 561.1317 771.9528 Tm BT 9 0 0 9 394.0157 412.8898 Tm (737-8)Tj /P <>BDC EMC /P <>BDC EMC 10 0 0 10 225.1837 771.9528 Tm ( )Tj EMC /P <>BDC EMC BT f 9 0 0 9 411.0097 104.8898 Tm EMC 7 0 0 7 230.7317 243.9528 Tm ET 7 0 0 7 491.7142 89.7654 Tm ( )Tj ET ET EMC 8 0 0 8 543.5282 797.8898 Tm ET 3.0566 -3.9073 l -.01 Tc The aux tanks are located at -.02 Tc /P <>BDC EMC /P <>BDC ET BT 7 0 0 7 54.5916 243.7654 Tm BT EMC ET ET 6.5 0 0 6.5 387.561 611.9529 Tm EMC /P <>BDC /GS1 gs 0 Tc 0 Tc /P <>BDC ( )Tj EMC ET BT ET /P <>BDC /P <>BDC /F6 1 Tf 7 0 0 7 520.6108 606.9528 Tm /P <>BDC 7 0 0 7 520.6108 661.9528 Tm .151 .147 .15 rg 0 Tc ET )Tj /P <>BDC /P <>BDC Any)Tj BT EMC (0.0113)Tj EMC /P <>BDC ET -.02 Tc 7 0 0 7 54.7071 507.7654 Tm EMC EMC -.02 Tc EMC /P <>BDC ET -.02 Tc 0 Tc /P <>BDC BT ET ET EMC EMC EMC ( )Tj BT 7 0 0 7 355.5753 595.7654 Tm /P <>BDC ET 9 0 0 9 107.6178 269.8898 Tm ET 9 0 0 9 378.9498 368.8898 Tm 7 0 0 7 535.5029 287.7654 Tm BT EMC /P <>BDC EMC /P <>BDC EMC ( )Tj EMC /P <>BDC The -800 has sold strongly since its launch . BT EMC 7 0 0 7 380.2788 518.7654 Tm ET 6.5 0 0 6.5 295.8145 611.9529 Tm 7 0 0 7 116.3631 11.5132 Tm BT /P <>BDC ET BT 7 0 0 7 241.5317 441.9528 Tm ET 0 Tc ( )Tj 6.5 0 0 6.5 114.9382 611.9529 Tm BT ET 7 0 0 7 338.6433 188.7654 Tm /P <>BDC BT BT /P <>BDC ET BT BT ( )Tj ET /P <>BDC /P <>BDC ET /P <>BDC 0 Tc /P <>BDC EMC ( )Tj (297,312)Tj EMC 9 0 0 9 545.8785 489.8898 Tm (variant. Q ET BT /P <>BDC EMC EMC 6 0 0 6 205.0069 701.9528 Tm 7 0 0 7 187.0858 496.9528 Tm 7 0 0 7 363.2711 540.9528 Tm EMC BT 9 0 0 9 394.0315 709.8898 Tm 9 0 0 9 408.1968 159.8898 Tm BT On older aircraft the trimmers were accessible from the ET /P <>BDC (136)Tj ET ( )Tj BT ( )Tj EMC BT EMC 0 Tc ET /P <>BDC ET EMC ET ET 0 Tc /F6 1 Tf ET /P <>BDC /F1 1 Tf ET /P <>BDC /P <>BDC EMC EMC EMC 6.5 0 0 6.5 499.4541 735.9529 Tm BT 9 0 0 9 215.4409 522.8898 Tm ET 9 0 0 9 36.8504 467.8898 Tm (39,270)Tj 9 0 0 9 352.4841 313.8898 Tm ET BT (72% of the NG fleet in service. /P <>BDC -2.5306 -6.3496 -3.213 -6.0519 -3.7399 -5.4283 c 0 Tc BT ( )Tj 7 0 0 7 490.8321 386.7654 Tm 9 0 0 9 527.0365 456.8898 Tm EMC EMC EMC BT -.01 Tc ET ET (economy seating by 12 seats when)Tj /P <>BDC /P <>BDC ET EMC -.02 Tc ( )Tj ET 9 0 0 9 206.8842 522.8898 Tm EMC (CFM LEAP-1B28B1s thrust rating to)Tj ET /P <>BDC EMC BT 6.5 0 0 6.5 327.0283 637.9529 Tm /F4 1 Tf /GS1 gs EMC ( )Tj ( The wind component and)Tj /P <>BDC ET ( )Tj /P <>BDC EMC ET BT EMC (maintenance. /P <>BDC (1,272)Tj 9 0 0 9 543.3065 555.8898 Tm ET 7 0 0 7 210.1137 364.7654 Tm 7 0 0 7 297.632 595.9528 Tm BT /P <>BDC 7 0 0 7 508.4124 320.7654 Tm /P <>BDC EMC EMC /P <>BDC EMC EMC 7 0 0 7 297.632 738.9528 Tm ET 518.697 0 l /P <>BDC /P <>BDC q 1 0 0 1 394.012 84.878 cm 0 0 m /P <>BDC 7 0 0 7 535.5029 606.7654 Tm ET ( )Tj EMC ET EMC /P <>BDC BT EMC ET BT 9 0 0 9 36.8504 192.8898 Tm ( )Tj (final comparison of the two manufacturers)Tj 0 Tc BT EMC EMC /P <>BDC BT /P <>BDC BT BT EMC 7 0 0 7 241.2727 474.9528 Tm -.02 Tc (a cost index, which is a more cost-efficient)Tj EMC ( )Tj ET /P <>BDC /P <>BDC ET (\(see table, this page\))Tj BT 0 Tc -.02 Tc ET BT ET EMC ET 9 0 0 9 36.8504 159.8898 Tm -.02 Tc allowed for deposit of the ground-based NEA into the center wing tank (CWT). -.02 Tc /P <>BDC EMC 7 0 0 7 539.8962 738.9528 Tm EMC EMC /P <>BDC 737-800 & 737-8 The 737NG family has a single engine offering: the 737NG with the CFM56-7B; and the 737 MAX family with the CFM LEAP-1B. 7 0 0 7 250.5326 100.7654 Tm EMC ET EMC 0 Tc BT EMC EMC BT (152)Tj /P <>BDC /P <>BDC ET ET 9 0 0 9 411.0181 236.8898 Tm -.02 Tc EMC ET ET ( )Tj -.02 Tc .406 .403 .405 rg /F6 1 Tf /GS1 gs /P <>BDC 0 Tc BT ( )Tj BT (load factor, the A321neo carries a heavier)Tj Waking the giant, the return of the Airbus A380. EMC /P <>BDC /P <>BDC ET 6 0 0 6 309.5222 701.9528 Tm ( )Tj EMC ET /P <>BDC 7 0 0 7 537.8154 430.9528 Tm 6.5 0 0 6.5 64.6596 624.9529 Tm 0 Tc (inches and a bypass ratio of 11.0:1. /GS2 gs ( )Tj ( )Tj BT EMC ET The increase in OEW of)Tj (150)Tj -.02 Tc ET EMC EMC 6.5 0 0 6.5 397.1339 702.9529 Tm BT /P <>BDC ( )Tj q 1 0 0 1 411.01 480.878 cm 0 0 m /P <>BDC ET ET 7 0 0 7 101.0963 210.9528 Tm BT EMC EMC (packages, it will be interesting to re-)Tj EMC ET /P <>BDC 7 0 0 7 88.196 11.5129 Tm BT 6.5 0 0 6.5 399.2659 565.9529 Tm EMC ET EMC /P <>BDC ET ET [(737-900E)-33(R)]TJ EMC EMC /P <>BDC /P <>BDC (the two scenarios are detailed )Tj BT .014984 824.882 572.583 17.008 re ET EMC /P <>BDC EMC ET /P <>BDC /P <>BDC -.005 Tc ET /P <>BDC (166,090)Tj /GS1 gs ET ET 0 Tc /P <>BDC ET EMC (lower fuel burn compared to the 737-)Tj BT -.02 Tc 7 0 0 7 187.0858 727.9528 Tm 9 0 0 9 536.1277 247.8898 Tm /P <>BDC BT ET /P <>BDC BT BT /P <>BDC BT BT ET EMC (170)Tj /P <>BDC ET ET EMC 9 0 0 9 537.9817 445.8898 Tm ( )Tj BT ( )Tj (152)Tj EMC ET 9 0 0 9 394.0315 742.8898 Tm (the results show that the lighter payload on)Tj ET BT 0 Tc BT EMC EMC BT 19.843 0 l /P <>BDC 6 0 0 6 184.072 659.9528 Tm ET BT -.02 Tc EMC /P <>BDC BT /P <>BDC EMC /P <>BDC EMC /P <>BDC ( )Tj BT ET 9 0 0 9 36.8504 148.8898 Tm ET (150)Tj endobj /P <>BDC EMC BT ET EMC 0 Tc /P <>BDC ET 7 0 0 7 457.0984 276.7654 Tm 7 0 0 7 247.7395 672.7654 Tm (passengers and the 737-900ER\(W\) 152)Tj 8 0 0 8 225.1837 717.9528 Tm EMC /P <>BDC BT BT BT 9 0 0 9 246.6141 709.8898 Tm /P <>BDC EMC /OC /MC4794 BDC [(737-900E)-33(R)]TJ BT 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 /P <>BDC ( )Tj 0 Tc BT BT BT BT (in a more efficient engine. /P <>BDC (. ET (the destination airports. 7 0 0 7 386.3929 573.9528 Tm BT (405)Tj /GS1 gs ET ET EMC ( )Tj (. ET ET /P <>BDC BT BT 9 0 0 9 439.4008 324.8898 Tm ET ET BT EMC 0 Tc BT EMC /P <>BDC 7 0 0 7 44.5789 463.9528 Tm EMC [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ 7 0 0 7 321.6356 221.9528 Tm EMC /P <>BDC ET 7 0 0 7 444.737 320.7654 Tm ET /P <>BDC ET /P <>BDC /P <>BDC EMC BT 340.964 0 0 625.44 232.441 31.168 cm BT ET EMC (in engine cool-down times. -.02 Tc (planned 170 passengers as follows: 145 on)Tj /P <>BDC ET EMC EMC ET -.02 Tc ET ( )Tj 7 0 0 7 116.3631 11.5132 Tm ( )Tj (174,165lbs, an MLW of 148,592lbs, and a)Tj (56,869)Tj (BOS-MIA)Tj 6.5 0 0 6.5 54.877 689.9529 Tm (sectors where a 170-passenger payload is)Tj 6 0 0 6 554.8917 743.9528 Tm BT -.02 Tc 0 Tc 0 Tc EMC EMC ET ET EMC 7 0 0 7 258.2805 584.7654 Tm 8 0 0 8 456.5927 771.7654 Tm EMC 7 0 0 7 258.2805 463.7654 Tm BT ( )Tj /P <>BDC 7 0 0 7 108.6215 67.9528 Tm 6 0 0 6 153.0397 715.9528 Tm The)Tj EMC 7 0 0 7 326.2278 727.9528 Tm BT (27,000lbs of thrust compared to the)Tj ET BT ( )Tj BT /F7 1 Tf EMC ( )Tj /P <>BDC Cheers Peter. EMC 7 0 0 7 456.2165 375.7654 Tm /P <>BDC BT BT ET ET [(Aircr)10(aft )]TJ ET BT (CFM56-5B4/P)Tj ( )Tj /GS2 gs /P <>BDC Main tanks > 50%, -1 to 5 deg pitch, +/- 1 deg roll: +/- 2.5% /P <>BDC /P <>BDC ET BT ET 7 0 0 7 82.8504 100.9528 Tm (increases to 0.22 to 0.29 cents or 8.7%)Tj BT BT BT ET ET ( )Tj 8 0 0 8 531.7294 771.9529 Tm /P <>BDC ET /P <>BDC BT BT /P <>BDC BT /P <>BDC 7 0 0 7 338.3085 331.9528 Tm EMC (2,094)Tj EMC /P <>BDC /P <>BDC 7 0 0 7 539.8962 628.9528 Tm 7 0 0 7 521.4928 573.9528 Tm EMC BT ET BT 7 0 0 7 314.6398 716.7654 Tm 9 0 0 9 564.1726 588.8898 Tm ( )Tj /P <>BDC EMC /P <>BDC 9 0 0 9 215.4313 60.8898 Tm EMC /P <>BDC /P <>BDC EMC BT ET 0 Tc ET /P <>BDC ( )Tj -.01 Tc /P <>BDC /P <>BDC 7 0 0 7 457.0984 529.7654 Tm /P <>BDC /P <>BDC ( )Tj Boeing has its 737 in almost every single developed nation. 9 0 0 9 196.1514 390.8898 Tm -.02 Tc BT BT (ASM of 0.55 to 0.88 cents per ASM)Tj 7 0 0 7 554.7883 287.7654 Tm 9 0 0 9 394.0157 423.8898 Tm 8 0 0 8 531.9995 82.8898 Tm ( )Tj /P <>BDC BT ET BT /P <>BDC ( )Tj (974)Tj (operating potential for these aircraft. EMC 10 0 0 10 52.7604 814.1973 Tm EMC 0 Tc ET BT 6 0 0 6 226.9834 715.9528 Tm /P <>BDC /P <>BDC 9 0 0 9 53.8582 60.8898 Tm EMC -.02 Tc -.02 Tc (aircraft operators fly their aircraft based on)Tj ET ET BT ( )Tj endobj EMC /P <>BDC ( )Tj 7 0 0 7 279.1575 419.9528 Tm ( )Tj EMC (2,054)Tj /P <>BDC BT /P <>BDC BT /P <>BDC ET /P <>BDC (CFM56-7B26)Tj (I)Tj 0 Tc /P <>BDC BT This would make)Tj 9 0 0 9 246.6141 786.8898 Tm EMC BT EMC Just wondering, where did you get the information about what specific aluminium alloys are used on different parts of the aircraft? 0 Tc ET 7 0 0 7 519.3773 364.9528 Tm -.02 Tc /F4 1 Tf 0 Tc EMC 7 0 0 7 114.6416 397.9528 Tm W n /P <>BDC /GS1 gs BT /P <>BDC 7 0 0 7 490.7815 265.9528 Tm /P <>BDC 6 0 0 6 489.6948 743.9528 Tm /P <>BDC ( )Tj ET /P <>BDC EMC 0 Tc ( )Tj ET .0161 Tc 0 Tc EMC 0 Tc ( )Tj EMC ( )Tj 0 Tc EMC ET -.02 Tc (37,653)Tj EMC EMC /P <>BDC flugzeuginfo.net is a non-commercial webproject. design and maintenance of fuel tanks to reduce the chances of such explosions in 9 0 0 9 215.4409 478.8898 Tm -.02 Tc ET ET /P <>BDC (efficiency and so lower fuel burn. 0 Tc BT /P <>BDC (24)Tj BT 15 w /P <>BDC BT ET /P <>BDC EMC 9 0 0 9 199.4908 192.8898 Tm .559 .331 .619 rg EMC /P <>BDC ET -.02 Tc -.02 Tc ET -.02 Tc /P <>BDC .0161 Tc ( )Tj 7 0 0 7 82.8504 210.9528 Tm BT 7 0 0 7 279.1575 243.9528 Tm /P <>BDC ET 7 0 0 7 403.478 540.7654 Tm BT /P <>BDC ET BT EMC ET ET EMC ( )Tj 9 0 0 9 391.4889 192.8898 Tm ( )Tj ( )Tj ET EMC /P <>BDC (9.0:1)Tj EMC BT ( )Tj BT 7 0 0 7 258.2805 738.7654 Tm 7 0 0 7 199.5784 496.7654 Tm 7 0 0 7 444.737 78.7654 Tm EMC BT ET 9 0 0 9 522.1225 555.8898 Tm ET ET 9 0 0 9 194.7833 236.8898 Tm BT 0 Tc BT ET ET /P <>BDC /P <>BDC EMC ET 0 Tc /P <>BDC ET 9 0 0 9 191.0032 225.8898 Tm ET EMC EMC EMC ( )Tj 7 0 0 7 475.2383 683.9528 Tm /P <>BDC /P <>BDC (the aircraft operator, but in this evaluation)Tj 7 0 0 7 337.6855 408.9528 Tm (900ER and 737-9, A320ceo and A320neo,)Tj -.02 Tc ( )Tj ( )Tj 7 0 0 7 491.7142 210.7654 Tm BT BT )Tj EMC Note: Specifications are listed as standard and may vary slightly. ET (831)Tj /P <>BDC ( )Tj ET 6.5 0 0 6.5 54.877 715.9529 Tm ET ET ET ( )Tj BT /P <>BDC BT ET /P <>BDC 7 0 0 7 279.1575 331.9528 Tm 0 Tc BT /P <>BDC ET /P <>BDC EMC /P <>BDC /P <>BDC /P <>BDC 7 0 0 7 99.8582 166.7654 Tm BT In the)Tj EMC 0 Tc 10 0 0 10 60.6037 794.2914 Tm 0 Tc (family, Airbus has reduced the thrust)Tj ET Calibration ET EMC BT ( )Tj 9 0 0 9 185.4953 214.8898 Tm EMC EMC ET ( )Tj BT 5.25 0 0 5.25 515.3989 11.5129 Tm EMC EMC BT BT BT ( )Tj ET BT EMC ET ET /P <>BDC -3.5781 -.0449 -2.6539 .5294 -1.6216 .5285 c ET 0 Tc 7 0 0 7 77.36 11.5132 Tm EMC /P <>BDC -.02 Tc 0 Tc Airbus A320 Specs What is behind one of the most popular short-haul airliners? Whilst bigger than the Embraer E-Jets, Boeing feels this is an optimum size range for a small city jet which can also be used for medium-haul international services. ET The VNE or never exceed speed for the Boeing 737-800 is 340 KIAS(Knots indicated airspeed) or Mach 0.82. [(P)11(ayload)]TJ ( )Tj EMC /P <>BDC 9 0 0 9 36.8504 49.8898 Tm 7 0 0 7 294.4014 661.7654 Tm EMC BT EMC 7 0 0 7 37.6993 430.9528 Tm ( )Tj )Tj ET /P <>BDC EMC BT 9 0 0 9 215.4409 324.8898 Tm BT ( )Tj -.02 Tc BT /F4 1 Tf (486)Tj ET 7 0 0 7 554.7883 738.7654 Tm ( )Tj BT EMC BT (/S)Tj /P <>BDC EMC EMC ET 9 0 0 9 232.438 38.8898 Tm /P <>BDC /P <>BDC )Tj (6,303)Tj EMC EMC BT /P <>BDC ET (1B engine as the 737-8. /P <>BDC BT EMC -.02 Tc 8 0 0 8 141.7322 771.9528 Tm ET 6.5 0 0 6.5 267.1065 742.9529 Tm ET -.02 Tc ET ET BT /GS1 gs BT ( )Tj EMC EMC /P <>BDC ( )Tj 7 0 0 7 158.74 331.7654 Tm EMC 7 0 0 7 469.2222 11.5129 Tm (operating performance are analysed here,)Tj 9 0 0 9 53.8582 698.8898 Tm ET 0 Tc EMC BT EMC BT /P <>BDC EMC ET EMC (2,517)Tj EMC /P <>BDC /P <>BDC /P <>BDC BT /P <>BDC /P <>BDC 15 w EMC 0 Tc ET (377,550)Tj /P <>BDC ET EMC 7 0 0 7 326.2278 661.9528 Tm -.02 Tc (10)Tj 9 0 0 9 215.4409 280.8898 Tm 7 0 0 7 315.1859 111.7654 Tm 8 0 0 8 43.6039 591.9528 Tm 0 Tc warmer air or accelerate to increase the kinetic heating. BT EMC 7 0 0 7 204.0935 89.7654 Tm ET ET 8 0 0 8 365.7704 703.9528 Tm (39,270)Tj /P <>BDC ET EMC )Tj ET EMC /P <>BDC /P <>BDC 6 0 0 6 333.1569 743.9528 Tm ( )Tj /P <>BDC EMC EMC /F1 1 Tf EMC (136)Tj ET /P <>BDC EMC ET ( )Tj /P <>BDC /P <>BDC 7 0 0 7 279.1575 298.9528 Tm 7 0 0 7 430.039 683.9528 Tm -.01 Tc /P <>BDC 7 0 0 7 445.619 738.7654 Tm 9 0 0 9 394.0157 643.8898 Tm ET 0 Tc 7 0 0 7 380.2788 386.7654 Tm 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 ET /P <>BDC 7 0 0 7 338.6433 408.7654 Tm 1 i EMC 8 0 0 8 339.6345 760.7654 Tm /P <>BDC ET /P <>BDC (158)Tj /P <>BDC EMC EMC /P <>BDC ET endobj For example, if the fuel tank maximum capacity is 10,000 KG, then the tolerance of the gauging is 0.03 (airplane with analog indicators) * 10000 = 300 KG. 7 0 0 7 554.7883 595.7654 Tm EMC 630,000 pounds (285,763 kg) Fuel capacity: 53,611 gallons (203,129 L) Range: 7,800 statute miles: Wing span: 195 feet, 8 inches (59.64 m) Length: 231 feet, 10 inches (70.66 m) Height: 7 0 0 7 362.3891 364.9528 Tm BT (2,013)Tj /P <>BDC EMC You can see the location of the centre tank (Flight time - mins)Tj BT ET (performance improvement over the)Tj ET ET EMC BT 0 Tc BT BT /P <>BDC /P <>BDC ( )Tj ET ET ET BT /P <>BDC /P <>BDC ( )Tj EMC /P <>BDC ET 0 Tc .7 -.5345 .9114 -1.2305 y ET 6.5 0 0 6.5 328.6662 585.9529 Tm 7 0 0 7 404.101 89.7654 Tm EMC BT EMC )Tj EMC ET (In the payload 2 scenario, the fuel burn)Tj -.02 Tc BT EMC EMC /P <>BDC ET (this evaluation are all in the same weight)Tj (operating the 737 has increased its)Tj ( )Tj BT (The second comparison is payload)Tj 13 0 0 13 215.433 467.8898 Tm /Artifact <>BDC -.01 Tc )Tj BT 9 0 0 9 553.5856 467.8898 Tm 7 0 0 7 363.2711 419.9528 Tm /P <>BDC What makes the newest 747 Jumbo tick? 0 Tc It was demonstrated under BT ( )Tj .014984 841.89 609.45 -841.89 re BT ( )Tj 0 Tc 7 0 0 7 314.6398 672.7654 Tm (It is analysed with an MTOW of)Tj /P <>BDC ET ET EMC /P <>BDC EMC BT EMC EMC 8 0 0 8 365.7704 619.9528 Tm EMC (977)Tj BT ET 8 0 0 8 158.74 771.7654 Tm BT The A320neos ASM)Tj (- nm)Tj /P <>BDC (136)Tj 9 0 0 9 394.0237 203.8898 Tm ET BT 7 0 0 7 107.1165 375.9528 Tm Q 7 0 0 7 247.7395 430.7654 Tm ( )Tj /P <>BDC ET 9 0 0 9 36.8504 49.8898 Tm EMC 7 0 0 7 37.0536 529.9528 Tm ET /P <>BDC BT Hello! -.07 Tc BT 9 0 0 9 208.0289 632.8898 Tm 9 0 0 9 137.7566 49.8898 Tm /P <>BDC ET 0 Tc ET 0 Tc ET 7 0 0 7 337.6855 386.9528 Tm EMC 7 0 0 7 230.7317 694.9528 Tm EMC 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). ET 6.5 0 0 6.5 346.019 742.9529 Tm ET /P <>BDC /P <>BDC ET (table, page 19\))Tj [(SS)-9.1(U)8(E)]TJ ET 9 0 0 9 215.433 434.8898 Tm EMC EMC EMC /P <>BDC EMC 9 0 0 9 192.0203 313.8898 Tm EMC /P <>BDC BT /P <>BDC 7 0 0 7 387.0932 309.9528 Tm EMC (The 737NG family has a single engine)Tj BT ET 6 0 0 6 482.6087 673.9528 Tm ET ET BT BT ET 28.5749 0 TD 9 0 0 9 195.231 423.8898 Tm BT ET /P <>BDC Any)Tj (404)Tj EMC BT ( )Tj (415,112)Tj /P <>BDC BT ( )Tj BT BT q ET /P <>BDC ET (The spot fuel price for the US aviation)Tj ET EMC 7 0 0 7 199.3614 100.7654 Tm -.02 Tc ET /P <>BDC 0 Tc ET ET Hi and thanks for your question. EMC BT 9 0 0 9 550.3618 324.8898 Tm [(A3)24.9(21neo v)12.9(ersus 7)-33(3)8.1(7-9 )]TJ BT -.02 Tc BT EMC BT ( )Tj 7 0 0 7 294.4014 89.7654 Tm Thanks now. BT ( )Tj 7 0 0 7 108.6215 166.9528 Tm /P <>BDC ( )Tj /P <>BDC 0 Tc /P <>BDC ET BT EMC 0 Tc 9 0 0 9 53.8582 115.8898 Tm EMC EMC BT ( )Tj ET (same cost index, and the method that each)Tj (172,992)Tj ( )Tj 7 0 0 7 429.157 606.9528 Tm ET 9 0 0 9 165.5977 478.8898 Tm EMC EMC supplied to the center wing tank and the oxygenenriched air (OEA) is vented ( )Tj 8 0 0 8 225.1837 745.9528 Tm /P <>BDC /P <>BDC 7 0 0 7 247.7395 573.7654 Tm ET BT 6.5 0 0 6.5 398.2453 742.9529 Tm Therefore, the Boeing 777-200 can carry 24,125 more gallons of fuel than the Boeing 737-800. BT BT (covers a 3,300-3,400nm range with a full)Tj 0 Tc /GS1 gs EMC EMC EMC 8 0 0 8 275.7172 760.7654 Tm EMC ET 7 0 0 7 355.3163 67.7654 Tm 7 0 0 7 491.4046 232.9528 Tm ET BT 9 0 0 9 215.433 104.8898 Tm BT ( )Tj BT 7 0 0 7 404.101 331.7654 Tm EMC ET BT /P <>BDC 7 0 0 7 163.8846 11.5132 Tm /F1 1 Tf /P <>BDC ET 6 0 0 6 258.3167 757.9528 Tm 9 0 0 9 36.8504 126.8898 Tm EMC ET BT (I)Tj 6 0 0 6 403.4411 757.9528 Tm (737-800W)Tj ET -.02 Tc BT BT BT 0 Tc ( )Tj BT /P <>BDC /P <>BDC EMC ET BT ET (371,416)Tj EMC 0 Tc ET /P <>BDC BT /P <>BDC EMC BT /P <>BDC ( )Tj 6.5 0 0 6.5 536.8751 722.9529 Tm BT BT BT 7 0 0 7 363.2711 232.9528 Tm /P <>BDC ET BT ET BT ET 7 0 0 7 387.0159 496.9528 Tm BT EMC /P <>BDC EMC EMC EMC This fuel would give a /P <>BDC EMC ET /P <>BDC EMC /P <>BDC BT ET 7 0 0 7 554.7883 408.7654 Tm -.02 Tc 6 0 0 6 226.9834 757.9528 Tm EMC /P <>BDC ET /P <>BDC BT 7 0 0 7 387.0159 474.9528 Tm /P <>BDC ET EMC BT ET -.02 Tc BT EMC ( )Tj EMC EMC (\(see table, page 19\))Tj -.02 Tc EMC /P <>BDC ET BT EMC BT ( )Tj ET q ET ( )Tj BT (City-pair)Tj BT ET BT Main tanks smaller at 3900kg each but centre tank much larger giving total fuel capacity of 20,800kg. 9 0 0 9 411.0234 742.8898 Tm
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