9 0 0 9 43.6039 794.2914 Tm ET EMC ET EMC -.01 Tc EMC 8 0 0 8 72.3645 771.9528 Tm ET /P <>BDC 0 Tc [(CFM L)17.1(E)-8.1(AP-1B27)]TJ /P <>BDC -.02 Tc 9 0 0 9 215.4409 412.8898 Tm ( )Tj /GS2 gs /P <>BDC EMC EMC /P <>BDC BT /P <>BDC /P <>BDC -.02 Tc EMC ( )Tj ET EMC /P <>BDC BT /OC /MC3457 BDC ( )Tj EMC (aircraft operators plan and fly using the)Tj still drawing fuel from the centre tank. 9 0 0 9 229.6141 214.8898 Tm -.02 Tc /P <>BDC BT probably take you over MTOW if any payload was carried. ET EMC EMC -.02 Tc /P <>BDC EMC /P <>BDC BT 7 0 0 7 294.4014 705.7654 Tm ET ( )Tj BT 7 0 0 7 507.7893 67.7654 Tm EMC /P <>BDC BT allow for a measurement of fuel tank inerting and heating during the ET EMC /F6 1 Tf (192 seats. ET /P <>BDC EMC 0 J 0 j 5 w 10 M [] 0 d 0 Tc EMC 6.5 0 0 6.5 227.9655 565.9529 Tm (174,165lbs, an MLW of 148,592lbs, and a)Tj 7 0 0 7 380.2788 430.7654 Tm /GS1 gs ( )Tj /P <>BDC EMC BT ET /P <>BDC ET ET .151 .147 .15 rg /P <>BDC ET 9 0 0 9 210.9209 104.8898 Tm ( )Tj BT /P <>BDC 9 0 0 9 181.3643 335.8898 Tm EMC ( )Tj /P <>BDC BT ET EMC EMC 9 0 0 9 555.1594 379.8898 Tm BT BT [(Aircr)10(aft )]TJ 0 Tc ET BT q ET ( )Tj ( )Tj ( )Tj EMC ( )Tj ET 6 0 0 6 195.3167 715.9528 Tm ( )Tj ( )Tj [(CFM L)17.1(E)-8.1(AP-1A32)]TJ 9 0 0 9 211.1071 764.8898 Tm /P <>BDC /P <>BDC BT /P <>BDC 9 0 0 9 178.8353 478.8898 Tm ET /P <>BDC 7 0 0 7 113.1366 419.9528 Tm f 9 0 0 9 549.8481 632.8898 Tm /F6 1 Tf . ET ET ET ( )Tj BT -.02 Tc After 0 Tc ET (5,025)Tj EMC EMC /P <>BDC EMC 8 0 0 8 83.5638 703.9528 Tm ET EMC /P <>BDC 9 0 0 9 530.4152 423.8898 Tm EMC BT (A)Tj EMC Boeing 747 8 Intercontinental and Freighter History. EMC 6 0 0 6 309.5222 701.9528 Tm ET ET EMC EMC 9 0 0 9 215.4313 71.8898 Tm 9 0 0 9 36.8504 313.8898 Tm 9 0 0 9 36.8504 38.8898 Tm 7 0 0 7 387.0932 133.9528 Tm ( )Tj (second payload scenario using the 85%)Tj ( )Tj /P <>BDC EMC /P <>BDC BT Aircraft have been NGS provisioned since l/n 1935 and it has been installed since l/n 2620 onwards. /P <>BDC /P <>BDC EMC endobj 6 0 0 6 412.4713 757.9528 Tm BT ET BT [(M)21(T)39.1(O)7.1(W)0( - lbs)]TJ ET 8 0 0 8 189.0627 717.9528 Tm EMC 7 0 0 7 490.5101 595.9528 Tm EMC ET 9 0 0 9 521.2213 170.8898 Tm BT ET EMC ( )Tj 9 0 0 9 411.0181 357.8898 Tm /P <>BDC BT EMC EMC /P <>BDC /P <>BDC 9 0 0 9 36.8504 203.8898 Tm /P <>BDC ET BT /P <>BDC ( )Tj 0 Tc 9 0 0 9 246.6113 247.8898 Tm ( )Tj ET ( )Tj BT 9 0 0 9 232.4217 456.8898 Tm /P <>BDC 6.5 0 0 6.5 489.7146 611.9529 Tm ( )Tj ( )Tj ET 7 0 0 7 258.2805 441.7654 Tm EMC -.02 Tc /P <>BDC ( )Tj BT 6.5 0 0 6.5 536.1732 545.9529 Tm BT BT 7 0 0 7 230.7317 573.9528 Tm Values can be entered and displayed in pounds or kilograms. ET -.02 Tc EMC -.02 Tc BT /P <>BDC /P <>BDC /P <>BDC EMC ET 0 Tc EMC -.01 Tc (0.0124)Tj /P <>BDC ET The fuel flow indication is integrated over time to calculate the fuel used for each engine. EMC 7 0 0 7 314.6398 716.7654 Tm EMC BT Boeing 777X The New Triple Seven Family. /P <>BDC EMC /P <>BDC ET BT 0 Tc EMC BT 7 0 0 7 294.4014 463.7654 Tm -.02 Tc EMC ET /OC /MC477 BDC EMC (1,729)Tj /P <>BDC EMC [(E)-7.8(P)16.1(T)9(E)-13.9(MBE)-16.9(R)]TJ EMC EMC My Dad was a captain and I am curious if he flew the Flt 800 aircraft or not. (82,110)Tj /P <>BDC EMC /P <>BDC ET BT )Tj ET EMC BT /P <>BDC ET 7 0 0 7 508.2252 11.5129 Tm ( A)Tj 0 Tc EMC BT ET 9 0 0 9 369.3136 698.8898 Tm -.02 Tc /P <>BDC /P <>BDC ET EMC /P <>BDC 7 0 0 7 241.5317 716.9528 Tm 0 Tc ET /P <>BDC ET /P <>BDC 7 0 0 7 403.478 639.7654 Tm EMC EMC ( )Tj /P <>BDC BT /P <>BDC -.02 Tc /P <>BDC BT /GS1 gs EMC BT ET )Tj BT EMC 7 0 0 7 536.3849 507.7654 Tm 7 0 0 7 158.74 67.7654 Tm 7 0 0 7 536.3849 210.7654 Tm 0 Tc BT (passengers and 163 passengers on the)Tj 0 Tc /P <>BDC 9 0 0 9 68.0071 412.8898 Tm EMC /P <>BDC BT EMC W n ET ET 7 0 0 7 338.3085 309.9528 Tm ( )Tj /P <>BDC ( )Tj ET ET ET /P <>BDC BT /P <>BDC /P <>BDC EMC /P <>BDC EMC /P <>BDC ET ET APU fuel pump in the No 1 tank which operates automatically during the start /P <>BDC (163)Tj ET /P <>BDC 6 0 0 6 371.6897 659.9528 Tm ( )Tj ET /P <>BDC EMC /P <>BDC EMC ET EMC EMC BT 7 0 0 7 187.0858 133.9528 Tm 7 0 0 7 537.7804 331.9528 Tm EMC The)Tj /P <>BDC -.02 Tc ET -.02 Tc BT [(7)-33(3)8.1(7-800 v)12.9(ersus 7)-33(3)8.1(7-8 )]TJ ( )Tj EMC /P <>BDC ET /P <>BDC ET -.02 Tc (l)Tj -.02 Tc -.01 Tc ET EMC /P <>BDC BT /P <>BDC EMC BT ET (I)Tj /P <>BDC 7 0 0 7 99.8582 265.7654 Tm 13 0 0 13 190.8018 137.8898 Tm /P <>BDC (39,270)Tj 9 0 0 9 215.4409 170.8898 Tm BT /P <>BDC EMC /P <>BDC ET ET ( )Tj 8 0 0 8 490.9813 771.9528 Tm /P <>BDC EMC EMC BT ( )Tj /P <>BDC BT -.01 Tc ( )Tj 9 0 0 9 51.0236 258.8898 Tm ET EMC ET EMC ET /P <>BDC ET BT BT (573)Tj BT (The overflight and airport charges are)Tj 0 Tc BT 7 0 0 7 316.0679 364.7654 Tm BT what we have done is sourced a document that gives the various dimensions of a 737 cockpit with which you should be able to find your desired outcome. 7 0 0 7 187.0858 562.9528 Tm /P <>BDC BT /P <>BDC 0 841.89 609.449 -841.89 re /P <>BDC ( )Tj EMC EMC 7 0 0 7 326.2278 540.9528 Tm ( )Tj (which has the lowest fuel burn rate per)Tj [(737-900E)-33(R)]TJ BT ET EMC EMC ET EMC /P <>BDC ET BT /P <>BDC /P <>BDC 7 0 0 7 404.101 133.7654 Tm ET 6.5 0 0 6.5 378.2463 598.9529 Tm (planning solution to achieve the lowest)Tj /P <>BDC /P <>BDC 7 0 0 7 204.0935 89.7654 Tm EMC /P <>BDC 0 Tc (1,049)Tj )Tj (improvement in fuel burn compared with)Tj BT EMC [(A3)24.9(20ceo v)12.9(ersus 7)-33(3)8.1(7-800 )]TJ EMC BT EMC EMC ET 0 Tc 9 0 0 9 53.8582 291.8898 Tm /P <>BDC BT EMC EMC 7 0 0 7 37.5838 56.9528 Tm ( )Tj BT 6.5 0 0 6.5 64.6596 558.9529 Tm ET (In the 85% passenger payload)Tj EMC 7 0 0 7 554.7883 694.7654 Tm 7 0 0 7 230.7317 188.9528 Tm 9 0 0 9 394.0157 599.8898 Tm 10 0 0 10 422.8 814.1973 Tm EMC BT EMC (destination airport are listed )Tj EMC ( )Tj 7 0 0 7 355.3163 188.7654 Tm BT EMC 9 0 0 9 394.0315 632.8898 Tm ET /P <>BDC BT BT BT 0 Tc BT EMC BT /P <>BDC /P <>BDC /P <>BDC BT -.02 Tc (operation. EMC /P <>BDC ( )Tj ET /P <>BDC EMC ET ET ET /P <>BDC [(AIRL)8.1(INE & AIR)7.1(CRAF)-12.9(T)18.1( OPERA)56.9(T)-8.1(ION)-13.9(S)]TJ EMC ( )Tj BT EMC /GS2 gs EMC ET 0 Tc (carriers. BT BT ET EMC /P <>BDC ET (the longest sector BOS-SFO. BT EMC /P <>BDC /P <>BDC EMC 9 0 0 9 531.902 467.8898 Tm ET ET EMC /P <>BDC EMC ET EMC ET ET BT Right centre tank fuel pump on the forward wall of the (A320neos 7,000lbs higher MTOW. BT /P <>BDC /P <>BDC /P <>BDC /P <>BDC /P <>BDC 7 0 0 7 439.2087 397.9528 Tm ( )Tj BT /P <>BDC EMC BT /P <>BDC EMC 0 Tc BT ( )Tj 6 0 0 6 215.373 757.9528 Tm 9 0 0 9 527.7692 511.8898 Tm -.02 Tc 9 0 0 9 505.9675 632.8898 Tm ET /P <>BDC ( )Tj -.02 Tc (737-800W)Tj ET (by the CFM LEAP-1A26. ( )Tj BT ET /GS2 gs EMC Digital Sunburst Fuel Gauges - Simmonds 4 Tank. EMC ( )Tj ET /P <>BDC BT EMC .008 Tc EMC EMC 9 0 0 9 394.0157 115.8898 Tm /P <>BDC BT EMC 8 0 0 8 54.8194 760.9529 Tm ( )Tj BT 6 0 0 6 61.517 673.9528 Tm 7 0 0 7 379.3969 177.7654 Tm BT BT /P <>BDC /P <>BDC /P <>BDC 7 0 0 7 37.0536 485.9528 Tm ET ( )Tj EMC EMC 7 0 0 7 37.5838 540.9528 Tm 9 0 0 9 53.8582 456.8898 Tm (3,300 -)Tj )Tj BT BT BT /P <>BDC BT /P <>BDC BT EMC /P <>BDC 0 Tc 7 0 0 7 108.6215 331.9528 Tm BT ( )Tj 6.5 0 0 6.5 499.8375 545.9529 Tm /P <>BDC EMC Newer 500 series aircraft have an extra, DC operated EMC 7 0 0 7 539.8962 716.9528 Tm /P <>BDC ET EMC ET BT ( )Tj ET /P <>BDC ET -.02 Tc ET /P <>BDC /P <>BDC ET EMC 0 Tc /P <>BDC -.02 Tc /P <>BDC BT (CFM56-5B3/P)Tj BT ET -.02 Tc /P <>BDC 7 0 0 7 475.2383 683.9528 Tm ET BT ( )Tj BT ET /P <>BDC /P <>BDC -.01 Tc /P <>BDC EMC EMC BT ( )Tj EMC ET ET /P <>BDC /P <>BDC 10 0 0 10 417.91 814.1973 Tm [(BOS-C)-8.1(V)18.1(G)]TJ The)Tj ET BT 9 0 0 9 216.03 687.8898 Tm /P <>BDC EMC 0 Tc ( )Tj EMC ET 7 0 0 7 158.74 584.7654 Tm EMC BT Cheers Peter. (150)Tj ( )Tj BT /P <>BDC ( )Tj BT ET -.01 Tc BT BT ET .151 .147 .15 rg BT ET 7 0 0 7 429.157 540.9528 Tm ET BT /P <>BDC 9 0 0 9 215.433 82.8898 Tm 0 Tc 7 0 0 7 387.0932 199.9528 Tm EMC ET ET ( )Tj ( )Tj 7 0 0 7 163.8846 11.5132 Tm (The three main operational costs for)Tj (in a more efficient engine. ET (2.31 cents per ASM. BT ( )Tj BT /P <>BDC ( )Tj /P <>BDC EMC /P <>BDC ET 9 0 0 9 68.0071 577.8898 Tm f -.01 Tc EMC (170)Tj /P <>BDC Hi, How can I learn aerospace materails about a and b basis allowables for Boeing-737 ? EMC BT 9 0 0 9 53.8578 269.8898 Tm ( )Tj BT /P <>BDC ET BT EMC (20)Tj /F6 1 Tf 7 0 0 7 508.4124 320.7654 Tm 7 0 0 7 387.0932 210.9528 Tm 7 0 0 7 474.7064 441.9528 Tm EMC EMC ET 7 0 0 7 241.5317 243.9528 Tm /P <>BDC BT 9 0 0 9 383.9197 412.8898 Tm BT 6 0 0 6 346.935 771.9528 Tm ( )Tj ( )Tj 7 0 0 7 490.5101 496.9528 Tm BT EMC ( 2021)Tj /P <>BDC /P <>BDC (configuration used in the study is)Tj (the aircraft in this study are shown )Tj 9 0 0 9 554.3696 269.8898 Tm BT [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ BT (CFM56-7B26)Tj /P <>BDC (0.0160)Tj ET ET ET EMC 9 0 0 9 165.0289 60.8898 Tm BT 9 0 0 9 36.8504 368.8898 Tm ET ET /P <>BDC BT ET EMC (in ASMs between the eight aircraft types. EMC BT ET EMC 7 0 0 7 363.2711 232.9528 Tm EMC -.02 Tc /P <>BDC (The thrust ratings on the engines show)Tj BT 9 0 0 9 361.1316 214.8898 Tm ET EMC EMC ET 9 0 0 9 112.3045 346.8898 Tm ET ET BT ( )Tj BT q /P <>BDC BT Aluminium alloys are still the mainstay of the construction materials used with various blends used according to the strength required for the particular component. 8 0 0 8 225.1837 717.9528 Tm 0 Tc BT (assumed that no additional cargo is taken)Tj (31,416)Tj 9 0 0 9 408.1854 346.8898 Tm BT (the IAE V2533-A5 engine, rated at)Tj BT BT 0 Tc /P <>BDC ( )Tj -.02 Tc EMC BT ET ET BT 0 841.89 609.449 -841.89 re ET (900ER and 737-9, A320ceo and A320neo,)Tj (passenger load factor based on each types)Tj EMC BT /P <>BDC ][F$, c;9M$ C[\SU~s#4B#g"DH V6S[_t099J'Nbqur((h\Yf'urV(nYYW6V*f]+ BT 0 Tc (157)Tj ( )Tj BT ET (evaluation both taxi-out and taxi-in were)Tj (A)Tj ( )Tj BT EMC ET BT BT EMC -.02 Tc EMC EMC BT ET .023 .567 .626 RG BT /P <>BDC The 737-800 has a maximum fuel capacity of 6,875 gallons, which it carries in fuel tanks in its wings, as seen here, and in a fuel tank located underneath the passenger cabin's midsection. EMC ET (34,650lbs)Tj ( )Tj (A321ceo)Tj /P <>BDC BT /P <>BDC EMC /P <>BDC It is produced in the Renton plant in Washington by Boeing Commercial Airplanes. ET /P <>BDC ET /P <>BDC 9 0 0 9 53.8582 753.8898 Tm /F6 1 Tf 9 0 0 9 564.4508 324.8898 Tm 7 0 0 7 474.3564 716.9528 Tm For the purposes of)Tj ( )Tj BT BT -.02 Tc /P <>BDC 6 0 0 6 527.2669 729.9528 Tm (1,938)Tj BT /P <>BDC 7 0 0 7 77.36 11.5132 Tm BT BT BT 9 0 0 9 232.438 280.8898 Tm 9 0 0 9 195.3413 181.8898 Tm BT BT 7 0 0 7 474.3564 628.9528 Tm /P <>BDC 0 841.89 609.449 -841.89 re 0 Tc 7 0 0 7 54.7071 584.7654 Tm BT BT (1,058)Tj 7 0 0 7 387.0159 485.9528 Tm ET BT BT ( )Tj EMC /P <>BDC 7 0 0 7 473.8245 287.9528 Tm (class cabin configuration used in this study)Tj BT /P <>BDC EMC 8 0 0 8 136.4919 661.9528 Tm 9 0 0 9 411.0097 324.8898 Tm ET BT (6,303)Tj /P <>BDC BT ET ET ET BT 8 0 0 8 43.6039 591.9528 Tm 7 0 0 7 241.2727 166.9528 Tm 6.5 0 0 6.5 549.8557 689.9529 Tm 7 0 0 7 439.2087 298.9528 Tm BT EMC ET EMC /P <>BDC 7 0 0 7 338.3085 364.9528 Tm (test programme is well underway for entry)Tj EMC (6,875)Tj ET ET 0 Tc BT ET /P <>BDC ( )Tj EMC 9 0 0 9 195.3055 324.8898 Tm BT BT ( )Tj EMC 10 0 0 10 52.0044 814.1973 Tm 7 0 0 7 366.0641 705.9528 Tm ET 7 0 0 7 321.6356 265.9528 Tm 7 0 0 7 187.0858 265.9528 Tm f ( )Tj (207,336)Tj EMC [(CFM L)17.1(E)-8.1(AP-1A32)]TJ ( )Tj -.01 Tc EMC BT EMC ET BT [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ EMC 0 Tc /F6 1 Tf 9 0 0 9 146.3 346.8898 Tm BT ET EMC BT ET EMC 6.5 0 0 6.5 244.2585 598.9529 Tm BT ( )Tj The AFM limits are higher, but not normally ( )Tj /P <>BDC (288)Tj (BOS-PHX)Tj [(UG)-17.1(U)-8(S)8.1(T)]TJ -.02 Tc ET /P <>BDC /P <>BDC (170)Tj /P <>BDC S /P <>BDC -.02 Tc EMC /P <>BDC ET BT BT (1,059)Tj ( )Tj For more detailed information on the Boeing 737 Specs, you can click on this Boeing 737 PDF. ET ( )Tj [(SS)-9.1(U)8(E)]TJ ET BT EMC EMC EMC EMC EMC ET /P <>BDC 7 0 0 7 440.3636 573.9528 Tm /P <>BDC /P <>BDC ET /P <>BDC /P <>BDC /P <>BDC ET (variant of the four NG models, with nearly)Tj EMC BT the most hazardous condition-an empty center wing tank-that GBI would remain 0 Tc 7 0 0 7 187.0858 100.9528 Tm EMC ET /GS1 gs And I hope I will get some good stuff to post it to you. (uses one of the 11 certified weight variants. .661 .752 .896 rg 137 )Tj /P <>BDC /P <>BDC /P <>BDC /F7 1 Tf -.02 Tc 0 Tc 7 0 0 7 343.2355 518.7654 Tm ET ET 6.5 0 0 6.5 347.0849 722.9529 Tm ET EMC BT EMC BT (1B27)Tj EMC ( )Tj ET ET -.01 Tc ET BT /P <>BDC 9 0 0 9 345.4916 412.8898 Tm BT ET EMC 7 0 0 7 362.3891 320.9528 Tm /P <>BDC ( )Tj ( )Tj certain ground and flight cross flow conditions. BT /P <>BDC Like the)Tj ET .1334 -5.7288 l EMC EMC (174,606)Tj BT BT )Tj 9 0 0 9 194.9081 346.8898 Tm ( )Tj ET ET /P <>BDC 9 0 0 9 53.8582 764.8898 Tm ( )Tj /F4 1 Tf ET BT 7 0 0 7 54.7071 287.7654 Tm )Tj EMC /P <>BDC BT /P <>BDC ET BT ET EMC BT /P <>BDC /F4 1 Tf EMC (temperature )Tj /P <>BDC ET [(737 M)-8.1(A)-24.9(X-9:)]TJ EMC 7 0 0 7 108.6215 232.9528 Tm ( )Tj ET 0 Tc /P <>BDC ET (of fuel against time-related costs. EMC /P <>BDC (the associated taxi fuel burns )Tj BT /P <>BDC ( )Tj ET -.02 Tc /P <>BDC ( )Tj BT /F6 1 Tf EMC /P <>BDC It is notably more stretched than and based off of the original 400. EMC ( )Tj ET ( )Tj BT EMC EMC BT /P <>BDC /P <>BDC /P <>BDC ET -.02 Tc BT ET BT /P <>BDC /P <>BDC -.02 Tc /P <>BDC ET /P <>BDC /P <>BDC /P <>BDC 7 0 0 7 230.7317 375.9528 Tm /P <>BDC EMC 6.5 0 0 6.5 54.877 650.9529 Tm 6.5 0 0 6.5 346.1035 598.9529 Tm ET EMC EMC ET ET /F4 1 Tf EMC 9 0 0 9 553.8705 93.8898 Tm BT (1,547)Tj ET 9 0 0 9 215.433 214.8898 Tm EMC EMC BT /P <>BDC 7 0 0 7 247.7395 78.7654 Tm /P <>BDC BT BT 7 0 0 7 116.3631 11.5132 Tm EMC /P <>BDC (560)Tj (Max payload - lbs)Tj (148,504)Tj 9 0 0 9 394.0315 280.8898 Tm BT ( )Tj 9 0 0 9 215.433 445.8898 Tm EMC /P <>BDC 8 0 0 8 365.7704 619.9528 Tm 9 0 0 9 195.5727 104.8898 Tm 0 Tc 9 0 0 9 411.0181 489.8898 Tm ET 7 0 0 7 321.6356 89.9528 Tm -.02 Tc ET /OC /MC5061 BDC BT EMC BT -.02 Tc EMC 7 0 0 7 141.7322 408.9528 Tm 7 0 0 7 430.039 639.9528 Tm EMC BT 7 0 0 7 116.3631 11.5132 Tm /P <>BDC BT -.02 Tc BT ( )Tj ET ET EMC BT 0 Tc EMC ET ( )Tj 9 0 0 9 540.3891 544.8898 Tm EMC ( )Tj (214,730)Tj BT /P <>BDC ET 9 0 0 9 36.8504 203.8898 Tm ET /P <>BDC (A)Tj 7 0 0 7 537.7804 408.9528 Tm [(Aircr)10(aft)]TJ ET Note: The gauges are still considered to be operating normally with EMC /P <>BDC ET 9 0 0 9 53.8338 203.8898 Tm BT ET 5 0 0 5 92.725 11.5132 Tm /P <>BDC BT ( )Tj ET 7 0 0 7 354.6933 639.7654 Tm BBJ Aux fuel panel located on Capt's & F/O's main /P <>BDC EMC BT /P <>BDC BT BT BT 6 0 0 6 236.6735 673.9528 Tm ET EMC ET EMC You were right, there were some discrepancies around the range. 0 Tc (3,069)Tj The aux fuel /P <>BDC Adobe d [(737-900E)-33(R)]TJ (2,518)Tj BT BT /P <>BDC 7 0 0 7 490.5101 738.9528 Tm EMC 9 0 0 9 394.0315 137.8898 Tm BT ( )Tj /P <>BDC BT 6 0 0 6 418.9814 701.9528 Tm EMC EMC ET [(P)11(ayload)]TJ BT 9 0 0 9 53.8578 280.8898 Tm 9 0 0 9 75.273 445.8898 Tm /P <>BDC /P <>BDC BT EMC ET ET EMC /P <>BDC (the relative fuel costs between the aircraft)Tj 7 0 0 7 87.8179 243.7654 Tm EMC /P <>BDC It is assumed that the aircraft in)Tj 9 0 0 9 232.4217 434.8898 Tm EMC ( )Tj 7 0 0 7 337.7614 111.7654 Tm EMC ET BT ( )Tj (977)Tj BT 0 Tc 9 0 0 9 215.4409 467.8898 Tm /Artifact <>BDC EMC EMC /P <>BDC /P <>BDC -.02 Tc BT 7 0 0 7 158.74 705.7654 Tm ET .023 .567 .626 rg (831)Tj 7 0 0 7 507.7893 507.7654 Tm ET ET BT 6.5 0 0 6.5 346.3049 676.9529 Tm EMC /P <>BDC ( )Tj /GS2 gs ET /P <>BDC EMC BT 503.542 90.794 m ( )Tj /P <>BDC 7 0 0 7 521.4928 727.9528 Tm EMC EMC /P <>BDC /P <>BDC 1 i 7 0 0 7 294.4014 386.7654 Tm EMC EMC 7 0 0 7 476.1204 661.9528 Tm 7 0 0 7 507.7893 628.7654 Tm -.01 Tc ( )Tj 9 0 0 9 198.0774 280.8898 Tm -.02 Tc (economy seats are at six-abreast. Q BT ET BT ( )Tj ET 7 0 0 7 508.4124 144.7654 Tm 7 0 0 7 258.2805 518.7654 Tm /P <>BDC EMC EMC BT /P <>BDC -.02 Tc EMC BT BT /P <>BDC 0 Tc -.02 Tc ET -.02 Tc BT ( )Tj EMC 0 Tc -.02 Tc EMC ET 7 0 0 7 440.0906 441.9528 Tm /P <>BDC ( )Tj 9 0 0 9 356.2376 236.8898 Tm EMC EMC /P <>BDC /P <>BDC ET /P <>BDC ET ET /P <>BDC ( )Tj -.02 Tc EMC BT /P <>BDC ET /P <>BDC 9 0 0 9 367.2172 269.8898 Tm /P <>BDC EMC BT (831)Tj ( )Tj BT BT 6.5 0 0 6.5 54.877 624.9529 Tm EMC ( )Tj /P <>BDC 6.5 0 0 6.5 295.5027 624.9529 Tm 0 Tc 7 0 0 7 247.7395 133.7654 Tm