(2,040)Tj /P <>BDC BT /P <>BDC ( )Tj ( )Tj EMC (CFM56-5B4/P)Tj ( )Tj /P <>BDC (19 seats more than the -800, and 13)Tj ET EMC BT (105,800lbs )Tj /P <>BDC /P <>BDC EMC /P <>BDC ET ET 432 0 obj /P <>BDC BT BT ET 7 0 0 7 457.0984 243.7654 Tm 9 0 0 9 112.3045 346.8898 Tm 9 0 0 9 193.0552 434.8898 Tm ET 6 0 0 6 433.7979 771.9528 Tm 9 0 0 9 356.2376 236.8898 Tm 7 0 0 7 297.632 496.9528 Tm (CFM56-7B26)Tj EMC ( )Tj (0.0154)Tj /P <>BDC BT EMC ( )Tj (450,780)Tj BT (2,731)Tj 6.5 0 0 6.5 295.8145 611.9529 Tm EMC BT BT (20)Tj BT 8 0 0 8 520.6337 771.7654 Tm 7 0 0 7 241.5317 419.9528 Tm 6.5 0 0 6.5 243.8814 663.9529 Tm /P <>BDC BT ET ET 7 0 0 7 457.0984 232.7654 Tm ET (136)Tj ET 9 0 0 9 393.233 203.8898 Tm /P <>BDC 7 0 0 7 247.7395 595.7654 Tm 0 Tc -.02 Tc 6 0 0 6 561.1918 659.9528 Tm 6 0 0 6 403.6028 743.9528 Tm ET BT EMC /P <>BDC EMC /P <>BDC /P <>BDC ET EMC /F1 1 Tf -.02 Tc 7 0 0 7 508.4124 606.7654 Tm ET EMC (1A26-powered aircraft that is used in this)Tj /P <>BDC EMC EMC /P <>BDC 9 0 0 9 187.5717 126.8898 Tm /P <>BDC ( )Tj (37,416)Tj ( )Tj BT 6 0 0 6 403.0689 729.9528 Tm BT 7 0 0 7 456.2165 166.7654 Tm /P <>BDC (they are replacing. /P <>BDC 9 0 0 9 214.7728 247.8898 Tm /P <>BDC EMC As stated, this makes a fair)Tj EMC A previous model which had success was Airbuses A320. -.01 Tc EMC 26.0355 0 TD 0 Tc ( )Tj BT 9 0 0 9 53.8582 115.8898 Tm 0 Tc ET 9 0 0 9 205.6978 291.8898 Tm -.015 Tc /P <>BDC (18)Tj ET (significant enough that operating the)Tj BT (47,000)Tj EMC ET BT EMC EMC 7 0 0 7 536.3849 166.7654 Tm -.02 Tc /P <>BDC 7 0 0 7 380.2788 518.7654 Tm 7 0 0 7 427.7291 232.9528 Tm /P <>BDC This is because as the)Tj (been carried on the similar-sized aircraft. EMC EMC 5.25 0 0 5.25 465.7151 11.5129 Tm 9 0 0 9 365.3999 511.8898 Tm /P <>BDC BT 7 0 0 7 204.0935 727.7654 Tm 7 0 0 7 445.619 727.7654 Tm BT -.02 Tc BT .964 .834 .406 rg BT BT 0 Tc EMC /P <>BDC ET EMC 9 0 0 9 213.8067 159.8898 Tm /P <>BDC ( )Tj ET (The aircraft are examined on the basis)Tj ( )Tj /P <>BDC ( )Tj (10)Tj EMC ( )Tj ET BT ( )Tj /P <>BDC BT ( )Tj EMC 0 Tc BT /P <>BDC /P <>BDC BT /P <>BDC EMC /OC /MC2281 BDC ET EMC -.02 Tc 7 0 0 7 508.4124 738.7654 Tm ( )Tj -.02 Tc 9 0 0 9 543.0273 192.8898 Tm 7 0 0 7 554.7883 342.7654 Tm EMC 0 J 0 j 5 w 10 M [] 0 d BT 9 0 0 9 232.4217 313.8898 Tm ET -.02 Tc EMC ET [(UG)-17.1(U)-8(S)8.1(T)]TJ ET ( )Tj BT BT 9 0 0 9 356.1657 445.8898 Tm EMC BT BT (analysis has an MTOW of 194,700lbs, an)Tj EMC EMC ET BT ( )Tj (0.0117)Tj 7 0 0 7 387.0932 320.9528 Tm EMC ET 0 Tc EMC /P <>BDC BT /P <>BDC /P <>BDC 9 0 0 9 541.6875 489.8898 Tm EMC ET /P <>BDC 7 0 0 7 457.0984 496.7654 Tm 0 Tc /P <>BDC ET ET (193,344)Tj BT 10 0 0 10 420.16 814.1973 Tm 7 0 0 7 554.7883 298.7654 Tm EMC BT EMC 7 0 0 7 258.2805 606.7654 Tm -.02 Tc ( )Tj 7 0 0 7 456.4753 584.7654 Tm EMC /P <>BDC BT 7 0 0 7 299.0601 210.9528 Tm EMC ( )Tj BT W* n /P <>BDC /P <>BDC /P <>BDC EMC 0 Tc [(SS)-9(U)8.1(E)]TJ 7 0 0 7 491.4046 232.9528 Tm ET EMC BT ET /P <>BDC /P <>BDC BT ET BT (2,349nm because of strong headwind. EMC BT EMC ( )Tj /P <>BDC 9 0 0 9 215.433 302.8898 Tm The typical range for this)Tj /F6 1 Tf EMC 7 0 0 7 204.0935 111.7654 Tm -.02 Tc warm conditions! EMC 9 0 0 9 53.8582 203.8898 Tm 9 0 0 9 36.8583 445.8898 Tm BT 6 0 0 6 61.517 701.9528 Tm [(r)10(atio)]TJ 9 0 0 9 564.1726 588.8898 Tm ET /P <>BDC ET ( )Tj 6.5 0 0 6.5 192.41 598.9529 Tm EMC /P <>BDC BT /P <>BDC ET ET BT ET /P <>BDC EMC 6 0 0 6 495.9995 659.9528 Tm /P <>BDC BT Low fuel quantity indication illuminates below ET EMC .023 .567 .626 rg -.02 Tc /P <>BDC /P <>BDC 0 Tc EMC EMC ET EMC EMC EMC ( )Tj ET (51,500)Tj ET 8 0 0 8 83.5638 703.9528 Tm 9 0 0 9 373.2203 368.8898 Tm .661 .752 .896 rg /P <>BDC ET EMC EMC /P <>BDC BT 7 0 0 7 297.632 540.9528 Tm EMC /P <>BDC 0 Tc Whatever the reason, we hope that both Boeing and the F.A.A. ET -.02 Tc (37,653)Tj BT 7 0 0 7 380.2788 628.7654 Tm 10 0 0 10 49.2604 814.1973 Tm (1,272)Tj ( )Tj BT ( )Tj BT (2,481)Tj 0 Tc 7 0 0 7 230.7317 529.9528 Tm EMC BT /P <>BDC ET /P <>BDC EMC /P <>BDC ( )Tj BT /P <>BDC -.02 Tc [(AIRL)8.1(INE & AIR)7.1(CRAF)-12.9(T)18.1( OPERA)56.9(T)-8.1(ION)-13.9(S)]TJ -.02 Tc /P <>BDC ET /P <>BDC 9 0 0 9 73.1083 489.8898 Tm ( )Tj BT BT BT EMC 9 0 0 9 207.9609 511.8898 Tm -.02 Tc 7 0 0 7 258.2805 210.7654 Tm 0 Tc /P <>BDC -.02 Tc EMC ( )Tj EMC ET (737-9)Tj BT 7 0 0 7 241.5317 122.9528 Tm 9 0 0 9 36.8504 115.8898 Tm 7 0 0 7 247.7395 386.7654 Tm ET BT EMC -.02 Tc 0 Tc /P <>BDC ( )Tj EMC 0 Tc BT Irkut MC-21, Russias homegrown modern airliner. /P <>BDC BT BT 9 0 0 9 394.0237 500.8898 Tm ET 7 0 0 7 473.8245 386.9528 Tm EMC ( )Tj BT ET 7 0 0 7 82.8504 144.9528 Tm EMC (1,162)Tj ET ET BT )Tj ( )Tj )Tj 7 0 0 7 99.8582 716.7654 Tm EMC 7 0 0 7 187.0858 727.9528 Tm EMC EMC BT EMC ET EMC /P <>BDC EMC The accuracy of the fuel flow transmitter is a function of the fuel flow. 0 Tc /P <>BDC /P <>BDC EMC ET /P <>BDC /P <>BDC ET 7 0 0 7 554.7883 496.7654 Tm ET /P <>BDC (216,240)Tj ET ( )Tj BT /P <>BDC BT The cruise speed to the alternate was)Tj ET /P <>BDC 7 0 0 7 404.101 243.7654 Tm ET EMC EMC EMC /P <>BDC S ( )Tj ET /P <>BDC ( )Tj ( )Tj ET ET ET ET 7 0 0 7 554.7883 243.7654 Tm EMC /P <>BDC /P <>BDC EMC 5.25 0 0 5.25 492.6848 11.5129 Tm 0 Tc /P <>BDC ( )Tj 7 0 0 7 54.7071 265.7654 Tm EMC EMC (35,112)Tj 7 0 0 7 404.101 177.7654 Tm ET 9 0 0 9 408.2047 566.8898 Tm ET 7 0 0 7 99.8582 144.7654 Tm EMC BT 6.5 0 0 6.5 448.3675 532.9529 Tm (571)Tj BT 7 0 0 7 439.1464 430.9528 Tm ET /F1 1 Tf ET EMC ET 8 0 0 8 43.6039 661.9528 Tm (I)Tj ET 0 Tc 7 0 0 7 337.6855 573.9528 Tm /P <>BDC ET BT remain illuminated for more than 19 seconds then this is probably what has ET ET (273,600)Tj 9 0 0 9 193.8472 236.8898 Tm EMC 6 0 0 6 277.9531 771.9528 Tm ET ( )Tj /P <>BDC ( )Tj [(D)12.9(A)-8.1(L/36)]TJ EMC EMC -.02 Tc EMC [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ ET -.02 Tc ( )Tj EMC ( )Tj EMC 6 0 0 6 320.3167 757.9528 Tm ET /P <>BDC 0 Tc ET 9 0 0 9 182.0906 467.8898 Tm 0 Tc EMC ET .023 .567 .626 rg BT 9 0 0 9 561.5176 522.8898 Tm /P <>BDC BT EMC ET /P <>BDC EMC EMC ET EMC ET ET /P <>BDC ET EMC EMC 6.5 0 0 6.5 76.9446 715.9529 Tm EMC 0 Tc /P <>BDC ET 6 0 0 6 208.1569 743.9528 Tm 9 0 0 9 267.7671 489.8898 Tm ( )Tj ET BT BT EMC ET EMC 0 J 0 j 5 w 10 M [] 0 d (136)Tj /P <>BDC /P <>BDC ET .023 .567 .626 rg -.02 Tc BT /P <>BDC /P <>BDC BT -.02 Tc /P <>BDC ET BT 7 0 0 7 299.0601 287.9528 Tm BT EMC ET 0 Tc Main tanks < 50%, -1 to 5 deg pitch, +/- 1 deg roll: +/- 1.0% EMC /P <>BDC ET BT W n BT /P <>BDC EMC (All the mission lengths are within the)Tj ET /P <>BDC /P <>BDC ET -.02 Tc BT ET ( N)Tj ET The VNE or never exceed speed for the Boeing 737-800 is 340 KIAS(Knots indicated airspeed) or Mach 0.82. 7 0 0 7 507.7893 507.7654 Tm /P <>BDC 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 ET /P <>BDC EMC ET /P <>BDC 9 0 0 9 568.555 82.8898 Tm BT ET -.02 Tc BT 9 0 0 9 232.438 467.8898 Tm ( )Tj BT 6 0 0 6 527.6392 757.9528 Tm BT /P <>BDC (0.0140)Tj ( )Tj EMC (The A321ceo has a maximum fuel)Tj 10 0 0 10 408.1099 814.1973 Tm ( )Tj EMC EMC 7 0 0 7 508.4124 540.7654 Tm ( )Tj EMC ( )Tj /P <>BDC 7 0 0 7 241.5317 529.9528 Tm ET ( )Tj ET /P <>BDC BT -.005 Tc (170)Tj /P <>BDC (4,836)Tj ET ET (7B26)Tj 7 0 0 7 337.9444 628.9528 Tm (0.0158)Tj 9 0 0 9 394.0157 313.8898 Tm (CFM56-7B26)Tj 56 0 0 56 36.8606 622.1944 Tm EMC (method of operation that balances the cost)Tj ET EMC ( )Tj 19.841 0 l ( )Tj /P <>BDC 6 0 0 6 541.7341 659.9528 Tm (104-112)Tj /P <>BDC EMC /P <>BDC /P <>BDC 9 0 0 9 361.5742 192.8898 Tm BT ( )Tj -.02 Tc 7 0 0 7 233.5248 78.9528 Tm ET ET EMC BT 7 0 0 7 141.7322 122.9528 Tm EMC ET /Figure <>BDC -.02 Tc ( )Tj /F4 1 Tf -.01 Tc BT ( )Tj (166,090)Tj /P <>BDC 9 0 0 9 547.2866 390.8898 Tm EMC [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ BT EMC EMC 7 0 0 7 338.6433 232.7654 Tm (The A321ceo is equipped with either:)Tj BT BT /P <>BDC /F1 1 Tf BT (calculate the fuel burns and times. 7 0 0 7 187.0858 628.9528 Tm 0 Tc 9 0 0 9 374.0759 203.8898 Tm BT EMC /P <>BDC 7 0 0 7 491.4046 100.9528 Tm EMC ( )Tj BT ( )Tj ( )Tj -.02 Tc EMC BT 7 0 0 7 554.7883 507.7654 Tm /P <>BDC 6.5 0 0 6.5 83.1789 742.9529 Tm [(CFM L)17.1(E)-8.1(AP-1B27)]TJ EMC EMC EMC BT -.02 Tc 0 Tc BT EMC [(BOS-L)-31(A)-24.9(X)]TJ -.02 Tc (A320neo:)Tj EMC ET ET BT /P <>BDC EMC BT EMC 13 0 0 13 411.0234 786.8898 Tm BT 7 0 0 7 298.514 573.9528 Tm /P <>BDC ET 6.5 0 0 6.5 276.4014 637.9529 Tm ET EMC ET /P <>BDC BT 7 0 0 7 364.1531 122.9528 Tm ( )Tj EMC EMC /P <>BDC 9 0 0 9 146.3 346.8898 Tm ET EMC BT ET EMC (A)Tj -.02 Tc BT 8 0 0 8 542.9269 786.8898 Tm 7 0 0 7 387.0932 166.9528 Tm (1,824)Tj ( )Tj /P <>BDC /P <>BDC BT /P <>BDC (is 0.01 to 0.15 cents better than the)Tj 7 0 0 7 343.2355 727.7654 Tm EMC /P <>BDC 0 Tc EMC /P <>BDC EMC /Artifact <>BDC ( The cruise speed and flight profile )Tj 0 Tc (158)Tj ET W n /OC /MC208 BDC BT 9 0 0 9 373.9458 159.8898 Tm /P <>BDC BT /F6 1 Tf /P <>BDC EMC BT ( )Tj 9 0 0 9 411.0097 49.8898 Tm /GS1 gs BT ( )Tj 7 0 0 7 294.4014 166.7654 Tm 7 0 0 7 196.5683 221.7654 Tm 0 Tc ET /P <>BDC EMC 7 0 0 7 473.8245 111.9528 Tm BT /P <>BDC BT EMC /P <>BDC 9 0 0 9 394.0237 269.8898 Tm EMC 7 0 0 7 230.7317 320.9528 Tm /P <>BDC EMC (A321neo carry the same passenger)Tj 9 0 0 9 553.4085 203.8898 Tm 7 0 0 7 326.2278 672.9528 Tm -.02 Tc BT EMC EMC EMC 6 0 0 6 214.7788 729.9528 Tm I found this image that might have some of the answers you need. 7 0 0 7 355.3163 320.7654 Tm 6 0 0 6 457.0716 687.9528 Tm /P <>BDC BT -.02 Tc (A321neo)Tj BT (485)Tj 7 0 0 7 199.3614 100.7654 Tm EMC [(7)-33(3)8.1(7-9)]TJ 7 0 0 7 445.619 584.7654 Tm 7 0 0 7 101.0963 386.9528 Tm /P <>BDC /P <>BDC ET BT EMC [(In addition to lo)12(w)6.1(er fuel burn compar)10(ed to its)]TJ .001 Tc BT 7 0 0 7 279.1575 287.9528 Tm -.01 Tc /P <>BDC ( )Tj 7 0 0 7 82.8504 298.9528 Tm -.02 Tc EMC (72,450)Tj EMC (124,650)Tj q 1 0 0 1 505.328 82.247 cm 0 0 m BT 0 Tc /P <>BDC ET (427,890)Tj EMC EMC 0 Tc EMC 0 Tc /P <>BDC EMC ET EMC BT ET BT EMC BT BT BT 7 0 0 7 99.8582 89.7654 Tm /P <>BDC BT ET /P <>BDC ET -.02 Tc ET /GS1 gs [(Y)-7.1(XX/104)]TJ ET EMC -.02 Tc 9 0 0 9 357.6917 192.8898 Tm /P <>BDC )Tj 7 0 0 7 99.8582 331.7654 Tm /P <>BDC EMC 9 0 0 9 53.8338 93.8898 Tm 0 Tc EMC /P <>BDC BT /P <>BDC ET BT 6 0 0 6 246.7063 715.9528 Tm [(A3)24.9(20ceo v)12.9(ersus 7)-33(3)8.1(7-800 )]TJ EMC (up to 3,200nm when equipped with)Tj 7 0 0 7 520.6108 628.9528 Tm 9 0 0 9 394.0237 181.8898 Tm (A potential operator would need to)Tj 0 Tw EMC EMC 9 0 0 9 170.752 368.8898 Tm EMC ET ET ( )Tj BT EMC BT BT -.01 Tc BT EMC EMC (50,800)Tj Hi. ET EMC /P <>BDC EMC ( )Tj ET ET ET ET /P <>BDC BT 9 0 0 9 232.438 214.8898 Tm Firstly, thank you for reply. 7 0 0 7 316.0679 408.7654 Tm (burn difference is 2.2%, and results in an)Tj ET (might have over an older aircraft would)Tj /P <>BDC EMC BT BT /P <>BDC BT BT q 1 0 0 1 232.438 95.878 cm 0 0 m (A320ceo)Tj EMC ( )Tj EMC BT ET ET 9 0 0 9 36.8504 214.8898 Tm -.01 Tc EMC ET BT ET .151 .147 .15 rg (737-8 has a 0.8-3.0% higher trip fuel burn than)Tj 9 0 0 9 68.0314 38.8898 Tm 7 0 0 7 204.0935 507.7654 Tm EMC .0161 Tc W n ET EMC 9 0 0 9 215.4409 390.8898 Tm BT ET ET 0 Tc What was the Super Sonic Transport (SST) Concorde plane?? ( )Tj ET S EMC /P <>BDC 6.5 0 0 6.5 282.0695 735.9529 Tm /P <>BDC .014984 841.89 609.45 -841.89 re BT /P <>BDC 9 0 0 9 529.3116 533.8898 Tm EMC BT ET /P <>BDC BT BT 7 0 0 7 537.7804 265.9528 Tm 6 0 0 6 394.3996 687.9528 Tm /P <>BDC BT 0 Tc ( )Tj ET (170)Tj EMC ( )Tj BT ET ( )Tj BT 7 0 0 7 456.4753 716.7654 Tm /P <>BDC /P <>BDC EMC BT -.02 Tc (39,270)Tj /P <>BDC /P <>BDC EMC 7 0 0 7 366.0641 738.9528 Tm /P <>BDC ET BT ET (39,270)Tj ( )Tj ET EMC ET [(O)7.1(W)-2(E/DO)7.1(W/seat - lbs)]TJ /P <>BDC ( )Tj /P <>BDC ET ( )Tj BT 7 0 0 7 199.5784 199.7654 Tm BT ET 7 0 0 7 299.0601 199.9528 Tm ( )Tj /P <>BDC ET /P <>BDC 9 0 0 9 36.8504 148.8898 Tm EMC EMC BT 6 0 0 6 106.1775 729.9528 Tm ET EMC ET ET /P <>BDC ET As)Tj ET ( )Tj EMC ET /P <>BDC EMC BT BT /P <>BDC 7 0 0 7 99.8582 287.7654 Tm EMC BT -.02 Tc 9 0 0 9 53.8578 225.8898 Tm /F4 1 Tf 9 0 0 9 53.8582 93.8898 Tm EMC 7 0 0 7 37.5838 463.9528 Tm 7 0 0 7 279.1575 243.9528 Tm EMC BT ( )Tj ( )Tj EMC EMC 5.25 0 0 5.25 100.8225 11.5132 Tm EMC EMC ET BT /P <>BDC BT (150)Tj BT ET BT 0 Tc /P <>BDC ET ( )Tj BT ET ET ( )Tj ET ET /P <>BDC 7 0 0 7 338.6433 342.7654 Tm ( )Tj ET BT ET /P <>BDC EMC EMC [(Aircr)10(aft )]TJ BT BT from cockpit door to the kitchen alley . ET ET EMC /P <>BDC ET -.02 Tc q q 9 0 0 9 215.4313 500.8898 Tm (/S)Tj -.01 Tc ET /P <>BDC ( )Tj BT 7 0 0 7 241.5317 606.9528 Tm 7 0 0 7 241.2727 661.9528 Tm /P <>BDC /P <>BDC 10 0 0 10 425.05 814.1973 Tm BT /P <>BDC 8 0 0 8 43.6039 717.9528 Tm ( )Tj /P <>BDC BT EMC ET It was demonstrated under ( )Tj (190-199)Tj )Tj /P <>BDC 6 0 0 6 138.6506 757.9528 Tm -.02 Tc Blended Winglets provide a simple and elegant solution to measurably improving aircraft fuel burn, managing operating costs and extending the economic life of an aircraft. EMC -.01 Tc ( )Tj EMC BT ET -.01 Tc /P <>BDC 28.5749 0 TD ET 9 0 0 9 394.0123 104.8898 Tm EMC ET /P <>BDC 9 0 0 9 542.2972 203.8898 Tm 9 0 0 9 190.8053 247.8898 Tm -.02 Tc -.02 Tc EMC /P <>BDC /P <>BDC ET /P <>BDC (l)Tj EMC ET ET /P <>BDC (2,518)Tj /P <>BDC /P <>BDC BT 7 0 0 7 363.2711 232.9528 Tm ET (includes checked and carry-on luggage. 9 0 0 9 374.887 346.8898 Tm -.02 Tc /P <>BDC EMC ( )Tj /P <>BDC (1,272)Tj BT /P <>BDC ET ET -.02 Tc ET ET EMC ( )Tj 8 0 0 8 314.8021 771.7654 Tm (superior fuel burn per seat-mile of all)Tj (give the newer type a further advantage. /P <>BDC ET (CFM56-7B27B3)Tj BT ET 7 0 0 7 99.8582 540.7654 Tm /P <>BDC EMC /P <>BDC 7 0 0 7 403.478 540.7654 Tm EMC /P <>BDC 9 0 0 9 68.031 170.8898 Tm ET ET EMC /P <>BDC BT /P <>BDC (achieved more than 6,000 orders for the)Tj BT ( )Tj ET -.01 Tc 7 0 0 7 343.2355 606.7654 Tm EMC The 747-800 can climb to 40,000 feet and will burn 0.44 nautical mile per gallon. BT ET 7 0 0 7 297.632 672.9528 Tm ( )Tj /P <>BDC (377,550)Tj -.02 Tc BT ( )Tj /P <>BDC ( )Tj EMC EMC 7 0 0 7 196.5683 518.7654 Tm -.01 Tc EMC ET 7 0 0 7 315.1859 100.7654 Tm /P <>BDC 7 0 0 7 158.74 265.7654 Tm ( )Tj EMC EMC 7 0 0 7 403.478 67.7654 Tm oxygen in the air. EMC (150)Tj /P <>BDC 9 0 0 9 359.0967 786.8898 Tm 9 0 0 9 53.8578 456.8898 Tm [(737-900E)-33(R\(W)-19(\):)]TJ BT EMC BT EMC BT BT BT /P <>BDC (0.0142)Tj BT ET EMC 8 0 0 8 276.7109 633.9528 Tm (0.0149)Tj EMC (comparison of the performance of the eight)Tj 10 0 0 10 52.7604 814.1973 Tm EMC /P <>BDC -.02 Tc BT EMC BT EMC BT 7 0 0 7 37.0536 562.9528 Tm BT EMC 7 0 0 7 130.1443 518.7654 Tm ET BT EMC /P <>BDC ET ET BT BT -.02 Tc ET 9 0 0 9 36.8504 324.8898 Tm /P <>BDC EMC EMC Can you confirm if Im right or wrong? NG/MAX: The engine spar valves and APU are normally powered by the hot ET EMC EMC /P <>BDC /P <>BDC BT ( )Tj ET (2,500)Tj ET EMC ET BT /P <>BDC ET (will take into account the additional)Tj ET /P <>BDC EMC EMC /P <>BDC EMC BT ET /P <>BDC 9 0 0 9 571.1344 742.8898 Tm 7 0 0 7 247.7395 408.7654 Tm 9 0 0 9 51.0236 401.8898 Tm ( )Tj /P <>BDC (\(Toronto Pearson\) sector, to 2,730nm for)Tj ( )Tj ET ( )Tj ( )Tj ET ET Boeings 737-800 isnt called the most popular airliner for no reason. 7 0 0 7 457.0984 276.7654 Tm BT endobj 9 0 0 9 394.0315 544.8898 Tm ET ( )Tj BT ( )Tj /P <>BDC EMC ET /P <>BDC BT /P <>BDC -.02 Tc 6.5 0 0 6.5 521.8278 742.9529 Tm ET BT ET 9 0 0 9 425.1913 181.8898 Tm 7 0 0 7 204.0935 210.7654 Tm (65,552)Tj The aux fuel BT BT EMC ET 7 0 0 7 37.0536 507.9528 Tm /P <>BDC EMC .151 .147 .15 rg /P <>BDC ( )Tj 7 0 0 7 518.4953 188.9528 Tm ET BT ET BT 7 0 0 7 107.1165 672.9528 Tm EMC ET /P <>BDC 0 Tc f [(CFM L)17.1(E)-8.1(AP-1A32)]TJ ET 6.5 0 0 6.5 499.1812 676.9529 Tm ( )Tj EMC /P <>BDC -.02 Tc /P <>BDC 7 0 0 7 141.7322 606.9528 Tm /P <>BDC /P <>BDC 9 0 0 9 194.7718 456.8898 Tm (2,220)Tj EMC 7 0 0 7 241.5317 727.9528 Tm ( )Tj ET 9 0 0 9 53.8578 291.8898 Tm ET 7 0 0 7 37.6993 232.9528 Tm ET ET /P <>BDC ET 0 Tc EMC ET BT ET 0 Tc /P <>BDC BT EMC /P <>BDC EMC 0 Tc (111)Tj (in ASMs between the eight aircraft types. 7 0 0 7 294.4014 133.7654 Tm BT 9 0 0 9 36.8504 82.8898 Tm BT ( )Tj ET ( )Tj ET BT ET 0 Tc EMC EMC [(OM)8(M)-13(E)-25(R)7(C)8(E)]TJ EMC ET ET -.02 Tc /P <>BDC 6.5 0 0 6.5 112.0328 637.9529 Tm 583 0 obj ET ET ET [(T)92(axi out time - mins)]TJ /P <>BDC ET ( )Tj ET (route structure so these charges would not)Tj /P <>BDC -.02 Tc EMC ET (190,800)Tj Q /P <>BDC (CFM56-5B4/P)Tj ET 7 0 0 7 490.8321 166.7654 Tm 9 0 0 9 53.8578 434.8898 Tm ET /P <>BDC EMC )Tj /P <>BDC ( )Tj (A320ceo is limited to 127 passengers on)Tj /P <>BDC /P <>BDC 6.5 0 0 6.5 54.877 663.9529 Tm ( )Tj (5,121)Tj /P <>BDC 6.5 0 0 6.5 397.9138 722.9529 Tm BT (All the flights were in a westerly)Tj 0 Tc EMC ET (CFM LEAP-1B28B1s thrust rating to)Tj .023 .567 .626 rg BT (results in the same payload being carried in)Tj 9 0 0 9 232.4408 742.8898 Tm EMC BT /F4 1 Tf /F4 1 Tf 9 0 0 9 542.3175 522.8898 Tm EMC ( )Tj 0 Tc EMC /F1 1 Tf (Any seating configuration is defined by)Tj (0.0149)Tj ET ET 9 0 0 9 181.2747 170.8898 Tm /P <>BDC /P <>BDC ET (-62)Tj EMC /P <>BDC /P <>BDC BT EMC .014984 841.89 609.45 -841.89 re 0 Tc 0 Tc -.005 Tc /P <>BDC BT ( )Tj (equal basis, since the number of seats will)Tj ET ( )Tj BT /P <>BDC ET (1,089)Tj EMC 0 Tc EMC EMC /OC /MC1950 BDC 0 Tc BT ET ET 9 0 0 9 232.4217 379.8898 Tm ( )Tj ( )Tj 7 0 0 7 445.619 639.7654 Tm /P <>BDC ET EMC ET [(737 M)-8.1(A)-24.9(X-8:)]TJ (0.0136)Tj 8 0 0 8 225.1837 633.9528 Tm (Block time)Tj ( )Tj /P <>BDC -.01 Tc BT /P <>BDC (of 170 passengers, the A321neo burns an)Tj BT EMC 7 0 0 7 82.8504 309.9528 Tm 7 0 0 7 37.5838 551.9528 Tm 0 841.89 609.449 -841.89 re BT -.02 Tc ( )Tj ET This is due to cold ET EMC BT EMC ET BT 0 Tc /P <>BDC 0 Tc ET ( )Tj ET EMC -.02 Tc ( )Tj BT 0 Tc (equipped with the more fuel-efficient CFM)Tj /P <>BDC ET ET EMC 0 Tc in later aircraft). EMC 7 0 0 7 53.8582 11.5132 Tm (the defined LRC speed, this has resulted in)Tj ( )Tj ( )Tj EMC /P <>BDC ET ET (increases to 0.22 to 0.29 cents or 8.7%)Tj EMC ( )Tj /P <>BDC /P <>BDC EMC differential pressure (and bleed air as a backup) is used to maintain a head of pressure in the q (the A320neo in the 85% payload scenario. BT EMC 7 0 0 7 54.7071 507.7654 Tm BT ET /P <>BDC BT BT ( )Tj -.02 Tc BT BT /P <>BDC BT (sectors where a 170-passenger payload is)Tj ET [(CFM L)17.1(E)-8.1(AP-1A32)]TJ /P <>BDC -.01 Tc ET ET (1,824)Tj EMC (based on the cost index set is different, it)Tj EMC EMC EMC EMC EMC EMC (\(see table, page 19\))Tj /F7 1 Tf BT EMC BT EMC BT -.02 Tc EMC /P <>BDC 7 0 0 7 508.4124 144.7654 Tm BT ET ET /P <>BDC 7 0 0 7 445.619 408.7654 Tm 6.5 0 0 6.5 557.8578 742.9529 Tm 6 0 0 6 55.0668 729.9528 Tm /P <>BDC /P <>BDC BT ET 0 Tc 28.5749 0 TD 7 0 0 7 338.6433 419.7654 Tm /P <>BDC BT /P <>BDC 9 0 0 9 206.6251 236.8898 Tm BT ( )Tj Inside this highly popular City Jet. 0 Tc ( )Tj BT 7 0 0 7 158.74 463.7654 Tm 9 0 0 9 411.0181 335.8898 Tm EMC (have been optimised by the PPS flight)Tj /P <>BDC EMC ET BT -.02 Tc 7 0 0 7 554.7883 78.7654 Tm EMC ( )Tj ET (0.0123)Tj BT ET 9 0 0 9 215.4409 423.8898 Tm ET /P <>BDC -.02 Tc BT EMC (41,349)Tj /P <>BDC ET EMC All the flights are in a westerly)Tj EMC ET BT EMC BT 10 0 0 10 230.6475 794.2914 Tm -.02 Tc EMC 6 0 0 6 561.1918 757.9528 Tm 0 Tc ET /P <>BDC ( )Tj EMC 0 Tc /P <>BDC Jump to Specification Table Boeing 737 Next Gen and Max. 6.5 0 0 6.5 379.0655 585.9529 Tm /P <>BDC ( )Tj /P <>BDC 9 0 0 9 51.0236 258.8898 Tm /P <>BDC EMC EMC BT ( )Tj BT ( )Tj ( )Tj EMC BT ET /P <>BDC BT BT EMC BT ET 9 0 0 9 215.433 401.8898 Tm EMC EMC ET EMC BT [(trip fuel burn compar)10(ed to the 737-800. ( )Tj BT EMC BT BT 7 0 0 7 491.7142 485.7654 Tm ET /P <>BDC /P <>BDC EMC /P <>BDC Fuel burn in cruise for B737-800 is 5,511lbs/hr Fuel burn at idle of a CFM56 engine = 661lbs/hr, so for the half hour descent two engines burn through 661 Total fuel for a 2 hour flight is 16,753lbs 6 More answers below Teodor Negru Passioned about flight and the art of flying Author has 425 answers and 1.8M answer views 4 y /P <>BDC ET S /P <>BDC ET ET BT (737-800W)Tj /P <>BDC BT ET BT )Tj 0 Tc BT /P <>BDC ET (342,312)Tj BT BT tank. /P <>BDC EMC The aircraft in this)Tj EMC ( )Tj EMC /P <>BDC /P <>BDC EMC EMC /P <>BDC ( )Tj ( )Tj -.07 Tc 9 0 0 9 408.1968 236.8898 Tm 9 0 0 9 553.5453 610.8898 Tm BT ( )Tj (types, but it is worth noting that in)Tj (136)Tj 9 0 0 9 36.8504 203.8898 Tm 7 0 0 7 279.1575 683.9528 Tm ( )Tj ET BT EMC 0 Tc BT (difference in fuel cost per ASM, however,)Tj -.02 Tc 0 Tc EMC BT 7 0 0 7 445.619 364.7654 Tm BT 7 0 0 7 337.7614 144.7654 Tm EMC EMC EMC EMC /P <>BDC ET EMC -.02 Tc EMC 7 0 0 7 507.7893 67.7654 Tm 7 0 0 7 327.1097 584.9528 Tm 848 0 obj W n During cruise, the tolerance is less than 1.5%. EMC /F6 1 Tf /P <>BDC /P <>BDC (179)Tj ( )Tj .023 .567 .626 rg ET ET /P <>BDC 6.5 0 0 6.5 346.3049 702.9529 Tm ET /P <>BDC EMC EMC /Artifact <>BDC BT Q /P <>BDC EMC EMC ET /P <>BDC ET ET ( )Tj (increase the passenger weight assumptions)Tj (l)Tj 137 )Tj 0 Tc ET BT EMC (using the same payload and seat)Tj ET EMC EMC BT BT EMC /P <>BDC -.02 Tc EMC BT /P <>BDC (0.0282)Tj EMC BT ( )Tj [(P)11(assengers)]TJ 9 0 0 9 36.8504 181.8898 Tm (Although it is most fuel-efficient to)Tj 6 0 0 6 205.0069 673.9528 Tm (409,800)Tj EMC (113,016)Tj ET BT (73,720)Tj EMC /GS1 gs EMC 9 0 0 9 206.7178 181.8898 Tm (0.0133)Tj (141,270)Tj EMC 9 0 0 9 73.1083 511.8898 Tm ( )Tj EMC ( )Tj 7 0 0 7 247.7395 331.7654 Tm (1,995)Tj /P <>BDC 0 Tc ( )Tj BT BT 8 0 0 8 264.6706 703.9528 Tm 7 0 0 7 491.4046 419.9528 Tm /P <>BDC EMC 6.5 0 0 6.5 448.7448 742.9529 Tm /P <>BDC ET 7 0 0 7 279.1575 595.9528 Tm BT In addition to keeping the)Tj BT BT BT waiting with pax 13 0 0 13 202.8899 533.8898 Tm The wheelbase which is the distance from the nosewheel to the line between the main wheels, which is 11.07 metres. /P <>BDC ET EMC (scenarios have been run. ET ET [(R)13.9(ange with full)]TJ BT /P <>BDC EMC EMC ET 9 0 0 9 394.0237 170.8898 Tm ET BT 9 0 0 9 408.1854 346.8898 Tm ( )Tj BT ET EMC /P <>BDC ET /P <>BDC BT /P <>BDC /P <>BDC ET /P <>BDC 9 0 0 9 394.0123 654.8898 Tm EMC BT ( )Tj (29,432)Tj /P <>BDC BT BT 7 0 0 7 337.6855 529.9528 Tm -.02 Tc /F6 1 Tf BT ET BT -.02 Tc (1, which is 5% higher than the same)Tj BT ET ET ( )Tj 6 0 0 6 134.6187 715.9528 Tm ( )Tj /P <>BDC 6.5 0 0 6.5 448.4585 689.9529 Tm (1,272)Tj -.02 Tc ET EMC ( )Tj (performing better on the shorter sectors. 6 0 0 6 309.3004 673.9528 Tm (all eight aircraft types. 0 Tc /P <>BDC 6.5 0 0 6.5 427.5934 742.9529 Tm ET /P <>BDC 9 0 0 9 543.1465 511.8898 Tm -.02 Tc ( )Tj 9 0 0 9 258.18 60.8898 Tm EMC /Figure <>BDC EMC ET W n BT BT EMC 7 0 0 7 508.4124 177.7654 Tm /P <>BDC /P <>BDC ( )Tj /P <>BDC 9 0 0 9 554.4741 412.8898 Tm BT /P <>BDC EMC /P <>BDC BT The total capacity is 526 seats broken down to 162 first class seats, 175 business class and 189 economy seats. ET EMC EMC ET BT BT /P <>BDC 5.25 0 0 5.25 40.8474 11.5129 Tm EMC EMC EMC ET ET ( )Tj BT (66,096)Tj BT 9 0 0 9 213.0312 335.8898 Tm EMC ET /P <>BDC ET (2,517)Tj (O)Tj [(737-900E)-33(R)]TJ /P <>BDC /P <>BDC BT EMC ( )Tj /P <>BDC 9 0 0 9 394.0315 335.8898 Tm -.01 Tc /P <>BDC (0.0115)Tj EMC ET 6.5 0 0 6.5 243.3486 742.9529 Tm 7 0 0 7 473.8245 221.9528 Tm BT /P <>BDC /P <>BDC For land the 800 needs 1372 meters or 4,501.26 feet. 9 0 0 9 36.8504 192.8898 Tm /GS1 gs BT EMC EMC ( )Tj 0 Tc EMC 9 0 0 9 51.0236 60.8898 Tm 9 0 0 9 515.9449 654.8898 Tm /P <>BDC /P <>BDC 0 Tc 7 0 0 7 158.74 573.7654 Tm ET /P <>BDC ET BT /P <>BDC BT /P <>BDC BT EMC /P <>BDC EMC /P <>BDC /P <>BDC 8 0 0 8 270.7815 771.9528 Tm 0 Tc ET ET (Engine)Tj 6.5 0 0 6.5 499.1812 702.9529 Tm (170)Tj /P <>BDC 0 Tc 9 0 0 9 215.4313 258.8898 Tm EMC BT 9 0 0 9 551.4681 368.8898 Tm EMC 9 0 0 9 394.0157 104.8898 Tm ET /P <>BDC .41 .161 .508 rg EMC EMC EMC /P <>BDC ET (stage lengths or tracked distances of)Tj 7 0 0 7 87.8179 441.7654 Tm EMC ET BT 0 Tc 9 0 0 9 202.684 357.8898 Tm 9 0 0 9 394.0157 302.8898 Tm 7 0 0 7 316.0679 386.7654 Tm EMC 0 Tc (411)Tj 0 Tc /P <>BDC ET ET BT 13 0 0 13 394.0123 434.8898 Tm EMC BT 7 0 0 7 54.7071 617.7654 Tm It sounds like you have a bit of a project on your hands. /P <>BDC BT )Tj ET EMC BT [(737-900E)-33(R)]TJ ET BT BT ET (A320neo)Tj EMC This)Tj EMC 0 Tc -.02 Tc /P <>BDC EMC available a Boeing 737 for modification and testing. Boeing 737-800 commercial aircraft. /P <>BDC BT ( )Tj -.01 Tc ( )Tj 9 0 0 9 362.8235 401.8898 Tm EMC ( )Tj -.02 Tc /P <>BDC (206,132lbs, an MLW of 171,500lbs, and)Tj /P <>BDC /P <>BDC ET EMC ET 7 0 0 7 355.3163 210.7654 Tm ET /P <>BDC ET /P <>BDC /P <>BDC ET 9 0 0 9 207.3361 115.8898 Tm /P <>BDC -.9858 .528 -.35 .3166 0 0 c /P <>BDC 9 0 0 9 394.0237 401.8898 Tm /P <>BDC -.02 Tc BT ET ET /P <>BDC BT ET (2,149)Tj BT EMC BT EMC /P <>BDC -.02 Tc /P <>BDC /P <>BDC BT (sector. ET BT BT ( )Tj /F1 1 Tf /P <>BDC 1 i /P <>BDC ET EMC ET BT 201.803 814.197 m ET (39,270)Tj BT Our Math Says It Isn't. /P <>BDC BT /P <>BDC ET BT (CFM56-5B3/P)Tj EMC (carriers. ET BT 0 Tc 0 841.89 609.449 -841.89 re ET ( )Tj ( )Tj (900ER\(W\) due to the heavier payload. ET 7 0 0 7 321.6356 100.9528 Tm ( )Tj 6 0 0 6 319.5607 715.9528 Tm EMC [(looks at the performance of eight Airbus and Boeing narr)10(o)12(wbody types)]TJ EMC ET /P <>BDC BT ET /P <>BDC . ET 7 0 0 7 445.619 617.7654 Tm 7 0 0 7 554.7883 100.7654 Tm ET 6.5 0 0 6.5 274.6269 689.9529 Tm ET 9 0 0 9 394.0123 313.8898 Tm /P <>BDC /P <>BDC BT -.02 Tc (performance deterioration factor added to)Tj -.02 Tc /P <>BDC ( )Tj 7 0 0 7 37.0536 661.9528 Tm /P <>BDC EMC /P <>BDC i.e..what is the maximum lateral distance the doors swing away from the aircraft, before they get to rest in the fully open position? ET 7 0 0 7 338.6433 276.7654 Tm ET BT BT ET ET ( )Tj the most hazardous condition-an empty center wing tank-that GBI would remain BT .014984 841.89 609.45 -841.89 re /P <>BDC /P <>BDC EMC EMC BT 9 0 0 9 215.433 313.8898 Tm 9 0 0 9 204.9907 467.8898 Tm ( )Tj ET 7 0 0 7 99.8582 463.7654 Tm BT 9 0 0 9 36.8504 313.8898 Tm EMC 0 Tc BT -.02 Tc
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