7 0 0 7 279.1575 199.9528 Tm /P <>BDC /P <>BDC /P <>BDC 0 Tc 9 0 0 9 189.1673 137.8898 Tm /P <>BDC /P <>BDC ET /P <>BDC EMC BT ET BT /P <>BDC /P <>BDC EMC W n 6 0 0 6 55.0668 687.9528 Tm BT BT ET 0 Tc 0 Tc BT EMC (2,205)Tj BT ET -.01 Tc ET (seat count as the 737-900ER\(W\). (The first table is the payload scenario)Tj 7 0 0 7 380.2788 199.7654 Tm 9 0 0 9 215.4409 324.8898 Tm ( )Tj 7 0 0 7 294.4014 540.7654 Tm BT (with 2,000 feet separation. 9 0 0 9 411.0234 698.8898 Tm EMC 7 0 0 7 429.157 518.9528 Tm BT /P <>BDC BT 0 Tc /P <>BDC ET /P <>BDC ( )Tj BT ET 7 0 0 7 258.2805 628.7654 Tm [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ BT 6 0 0 6 154.2695 743.9528 Tm ET ( )Tj /P <>BDC -.02 Tc ET EMC (0.0112)Tj ( )Tj 7 0 0 7 337.6855 397.9528 Tm BT /P <>BDC EMC 9 0 0 9 351.6906 456.8898 Tm 0 Tc BT ET EMC BT BT ET [(CFM L)17.1(E)-8.1(AP-)]TJ ( )Tj 7 0 0 7 508.6712 232.7654 Tm ET /P <>BDC /P <>BDC ET 7 0 0 7 554.7883 386.7654 Tm 7 0 0 7 187.0858 397.9528 Tm BT 8 0 0 8 386.5214 771.9528 Tm BT 9 0 0 9 215.4313 357.8898 Tm ET ET /P <>BDC /P <>BDC 0 Tc ET ET BT (operating the 737 has increased its)Tj ( )Tj EMC /P <>BDC /P <>BDC EMC /P <>BDC EMC ET ( )Tj EMC BT /P <>BDC 9 0 0 9 539.9583 236.8898 Tm ET /P <>BDC ET -.02 Tc BT 9 0 0 9 529.6118 302.8898 Tm ( )Tj ( )Tj BT BT ( )Tj ( )Tj ( )Tj BT ( )Tj EMC 0 Tc EMC 0 Tc EMC ( )Tj /P <>BDC (150)Tj ET 8 0 0 8 338.514 745.9528 Tm ET ( )Tj BT BT BT -.02 Tc ET ( )Tj EMC ET (NEA) distribution manifold, designed, built, and installed by Boeing, ET BT EMC BT 6.5 0 0 6.5 399.2659 565.9529 Tm 9 0 0 9 535.2051 500.8898 Tm BT ET ( )Tj ET BT 6.5 0 0 6.5 346.7208 624.9529 Tm ET (not been used for the A321ceo against the)Tj /P <>BDC (with a thrust rating of 26,000lbs, an intake)Tj EMC /TT2 1 Tf ET ET EMC (7,379)Tj ( )Tj ( )Tj /P <>BDC BT 9 0 0 9 439.4008 324.8898 Tm EMC 7 0 0 7 537.7804 265.9528 Tm /P <>BDC 7 0 0 7 116.3631 11.5132 Tm ET ( )Tj ( )Tj BT /P <>BDC 0 Tc BT EMC (ratio of 12.5:1; and the CFM LEAP-1A26)Tj 9 0 0 9 53.8578 137.8898 Tm EMC 8 0 0 8 314.3535 661.9528 Tm ET EMC (1,138)Tj ET BT EMC ET 7 0 0 7 258.2805 386.7654 Tm ET EMC (297,312)Tj (35,112)Tj -.01 Tc BT EMC ET /P <>BDC EMC 0 Tc ET ET 7 0 0 7 387.0159 661.9528 Tm BT /P <>BDC EMC BT ET BT ( )Tj 9 0 0 9 551.4681 368.8898 Tm ( )Tj 8 0 0 8 38.4438 619.9528 Tm ( )Tj (operationally safe to do so, in the)Tj 9 0 0 9 229.6141 434.8898 Tm ET BT /P <>BDC )Tj BT [(737 M)-8.1(A)-24.9(X-9:)]TJ /F4 1 Tf ( )Tj /P <>BDC /P <>BDC ET BT 7 0 0 7 518.4953 342.9528 Tm /P <>BDC (have any payload limitations on the routes)Tj /P <>BDC ET BT (37,653)Tj EMC -.02 Tc 36.85 824.882 572.599 17.008 re ( )Tj EMC ET /P <>BDC /P <>BDC /P <>BDC ET EMC BT ET 7 0 0 7 445.619 375.7654 Tm <> 6 0 0 6 132.3631 659.9528 Tm /P <>BDC ( )Tj EMC BT (average 0.06 cents per ASM advantage for)Tj (The 737-800 is the most popular)Tj ET 9 0 0 9 408.2047 566.8898 Tm EMC /P <>BDC /P <>BDC /P <>BDC BT ET ET /P <>BDC /P <>BDC -.01 Tc BT /P <>BDC /P <>BDC ET BT /P <>BDC . BT EMC Until its launch on September 5, 1994 the 737-800 was known as the 737-400X Stretch. BT -.02 Tc BT (34,650)Tj 0 Tc 6 0 0 6 153.2734 687.9528 Tm ( )Tj BT 6.5 0 0 6.5 83.1789 742.9529 Tm BT BT ET (give the newer type a further advantage. ( )Tj 10 0 0 10 49.9904 814.1973 Tm BT BT /GS1 gs 6.5 0 0 6.5 397.1339 663.9529 Tm BT -.01 Tc (A320ceo)Tj 6 0 0 6 403.4411 715.9528 Tm 0 Tc ET (0.0150)Tj /P <>BDC BT 7 0 0 7 321.6356 122.9528 Tm Federal Aviation Administration and the Boeing Company to evaluate the EMC 0 Tc 7 0 0 7 187.0858 727.9528 Tm (0.0139)Tj BT EMC Airbus A320 History a new player in the short-haul market. BT 0 Tc EMC /F4 1 Tf EMC 0 Tc 9 0 0 9 411.0181 324.8898 Tm /P <>BDC ET 9 0 0 9 176.5402 280.8898 Tm EMC 7 0 0 7 427.7291 298.9528 Tm /P <>BDC BT ET /P <>BDC /P <>BDC (159,251)Tj (482)Tj EMC EMC (1,945)Tj /P <>BDC EMC /P <>BDC BT BT BT BT ET BT W n (I)Tj (2,729)Tj /P <>BDC /P <>BDC -.01 Tc EMC (176)Tj EMC 0 Tc ET EMC Q 7 0 0 7 490.5101 540.9528 Tm 6.5 0 0 6.5 276.4014 650.9529 Tm EMC ET 0 Tc 9 0 0 9 411.0097 49.8898 Tm BT BT -.02 Tc EMC BT ET /P <>BDC For the purposes of)Tj /P <>BDC ET ET /P <>BDC EMC EMC 7 0 0 7 230.7317 562.9528 Tm ET EMC /P <>BDC /P <>BDC ET EMC (. /P <>BDC (73,720)Tj EMC BT 7 0 0 7 429.157 727.9528 Tm -.02 Tc EMC ET EMC 6.5 0 0 6.5 222.7786 676.9529 Tm -.02 Tc /P <>BDC -.02 Tc BT /P <>BDC 9 0 0 9 36.8504 148.8898 Tm (900ER\(W\) compared to the A321ceo in)Tj ET Any)Tj /P <>BDC /P <>BDC -.02 Tc ( )Tj BT 9 0 0 9 394.0157 478.8898 Tm waiting with pax EMC EMC ET /F1 1 Tf -.9858 .528 -.35 .3166 0 0 c 7 0 0 7 387.0159 485.9528 Tm /OC /MC225 BDC 0 Tc -.01 Tc ( )Tj 7 0 0 7 199.5784 441.7654 Tm ET .0161 Tc ET 7 0 0 7 54.7071 298.7654 Tm These sectors)Tj /P <>BDC BT BT ET 8 0 0 8 43.6039 605.9528 Tm /P <>BDC EMC (175,047)Tj (City-pair)Tj EMC BT 0 Tc BT ET (273,750)Tj /P <>BDC BT BT EMC (44,121)Tj (I)Tj (similar rate, with Boeing having delivered)Tj /P <>BDC EMC EMC BT /P <>BDC (404)Tj EMC BT ( )Tj 6 0 0 6 153.1846 771.9528 Tm BT 7 0 0 7 537.7804 166.9528 Tm ET Q ( )Tj ET BT EMC EMC BT ( )Tj (sectors as listed above, and the 737-)Tj ( )Tj -.02 Tc /P <>BDC (35,112)Tj ( )Tj ET BT EMC 7 0 0 7 316.0679 397.7654 Tm 9 0 0 9 544.8295 236.8898 Tm EMC EMC BT EMC ( )Tj BT BT BT /P <>BDC (\(see)Tj 7 0 0 7 187.0858 67.9528 Tm BT BT EMC EMC BT EMC 9 0 0 9 191.0032 225.8898 Tm .014984 824.882 572.583 17.008 re /P <>BDC 9 0 0 9 232.438 291.8898 Tm (737-800W)Tj EMC /P <>BDC /P <>BDC 161.566 0 l 6 0 0 6 554.6981 760.7654 Tm 9 0 0 9 215.4409 247.8898 Tm ET 7 0 0 7 187.0858 628.9528 Tm ET BT ( )Tj EMC -.02 Tc /P <>BDC BT 0 Tc ET /P <>BDC ( )Tj ET BT /P <>BDC EMC ( )Tj ( )Tj EMC ET ( )Tj /P <>BDC ET /P <>BDC ET /P <>BDC 9 0 0 9 215.4313 346.8898 Tm ( )Tj ( )Tj S ET BT EMC BT It has a maximum takeoff weight of about 80,000 kg (175,000 lbs). -.02 Tc ( )Tj (0.0111)Tj /P <>BDC 7 0 0 7 429.157 529.9528 Tm Waking the giant, the return of the Airbus A380. 7 0 0 7 99.8582 320.7654 Tm /OC /MC5080 BDC ( )Tj 9 0 0 9 394.0157 368.8898 Tm EMC 7 0 0 7 279.1575 595.9528 Tm /P <>BDC EMC BT 9 0 0 9 198.0774 280.8898 Tm EMC /P <>BDC /P <>BDC /P <>BDC ET ET ET 7 0 0 7 82.8504 375.9528 Tm EMC ET BT EMC EMC 7 0 0 7 554.7883 111.7654 Tm /P <>BDC EMC (5.1:1)Tj ET ( )Tj ET BT EMC /P <>BDC /P <>BDC ( )Tj /P <>BDC BT /P <>BDC ET ( )Tj 0 Tc /P <>BDC ET (the IAE V2533-A5 engine, rated at)Tj 7 0 0 7 258.2805 485.7654 Tm (0.0141)Tj /P <>BDC BT BT EMC BT (190,800)Tj EMC 0 Tc ( )Tj ET /GS2 gs BT -.02 Tc 7 0 0 7 445.619 617.7654 Tm 7 0 0 7 82.8504 331.9528 Tm EMC /P <>BDC ET 8 0 0 8 187.3427 745.9528 Tm EMC BT ET /P <>BDC EMC ET 7 0 0 7 554.7883 221.7654 Tm ET -.02 Tc EMC 6.5 0 0 6.5 536.1732 545.9529 Tm 0 Tc ET Low fuel quantity indication illuminates below EMC BT EMC EMC 9 0 0 9 369.4048 467.8898 Tm 9 0 0 9 36.8504 291.8898 Tm /P <>BDC ET 7 0 0 7 491.4046 177.9528 Tm ET BT BT 0 Tc EMC ET ET /P <>BDC 7 0 0 7 118.104 166.7654 Tm BT -.02 Tc 0 Tc ET -.02 Tc 6 0 0 6 434.3127 743.9528 Tm EMC [(P)11(ayload scenario one)]TJ -.02 Tc BT ET ET EMC /P <>BDC BT EMC ET ET 9 0 0 9 215.4409 192.8898 Tm ( )Tj We welcome your comment below, is there more we could be showing or are there topics you would like to see? -.02 Tc /P <>BDC ( )Tj EMC 7 0 0 7 363.2711 397.9528 Tm EMC EMC BT 9 0 0 9 196.4663 137.8898 Tm ET 0 Tc EMC Having a higher)Tj ET ET BT ( )Tj 7 0 0 7 444.737 287.7654 Tm /P <>BDC /P <>BDC EMC ( )Tj ET ( )Tj 0 Tc 7 0 0 7 354.6933 617.7654 Tm this question can have so many answers depending on the conditions, such as weight, air density, required speed etc. /P <>BDC EMC ET EMC 7 0 0 7 491.4046 397.9528 Tm flugzeuginfo.net is a non-commercial webproject. /F7 1 Tf .0063 7.6255 l ET ET ET EMC 7 0 0 7 338.6433 309.7654 Tm BT EMC BT /P <>BDC (109,800)Tj BT /P <>BDC 7 0 0 7 294.4014 562.7654 Tm EMC ET BT EMC the permissible CSFF area, the outside air temperature is above freezing(0 C, 32 0 Tc EMC EMC BT BT BT ET /P <>BDC ET EMC ( )Tj EMC 0 Tc ET EMC /P <>BDC ET BT /P <>BDC /P <>BDC 7 0 0 7 247.7395 595.7654 Tm 0 Tc ET 7 0 0 7 473.8245 122.9528 Tm /P <>BDC 0 Tc EMC ET /P <>BDC ET (170)Tj /P <>BDC /P <>BDC achievable with standard SG's. 0 Tc EMC /P <>BDC ( )Tj /P <>BDC ET (1,091)Tj BT ET ET EMC BT [(CFM L)17.1(E)-8.1(AP-1A26)]TJ /P <>BDC /P <>BDC /P <>BDC 0 Tc EMC 7 0 0 7 439.2087 287.9528 Tm ET ( )Tj /P <>BDC 9 0 0 9 215.433 423.8898 Tm BT ET BT Q BT EMC BT (0.0141)Tj 0 Tc BT EMC 7 0 0 7 326.2278 738.9528 Tm /P <>BDC BT 7 0 0 7 379.3969 210.7654 Tm EMC (page\))Tj EMC ET 0 Tc ( )Tj ET ( )Tj EMC 0 Tc EMC ( )Tj /P <>BDC ET EMC (170)Tj ET 6.5 0 0 6.5 426.4819 663.9529 Tm (The comparison will be for eight)Tj 7 0 0 7 508.4124 320.7654 Tm ET BT ( )Tj 5.25 0 0 5.25 465.7151 11.5129 Tm BT /P <>BDC 9 0 0 9 411.0234 764.8898 Tm EMC ( )Tj (and taxi-in times would vary by flight. /P <>BDC ET EMC EMC BT BT (152)Tj (LRC; the same as the primary sector. BT 7 0 0 7 230.7317 419.9528 Tm EMC ET EMC (34,650)Tj /P <>BDC 7 0 0 7 537.7804 386.9528 Tm BT BT -.02 Tc EMC (737-800W)Tj EMC BT /P <>BDC ET ET ET /P <>BDC BT /P <>BDC ( )Tj ( )Tj EMC 7 0 0 7 314.6398 705.7654 Tm 7 0 0 7 476.1204 694.9528 Tm ET f EMC ( )Tj ( )Tj EMC EMC /P <>BDC /P <>BDC ( )Tj BT 9 0 0 9 394.0315 456.8898 Tm BT 9 0 0 9 187.2574 302.8898 Tm 0 Tc BT 9 0 0 9 411.0097 203.8898 Tm 7 0 0 7 338.6433 397.7654 Tm /P <>BDC ET EMC EMC /P <>BDC BT -.02 Tc EMC BT 6.5 0 0 6.5 489.7146 611.9529 Tm BT /P <>BDC Max T/O Weight: 174200 Lb Max Landing Weight: 146300 Lb Operating Weight: 102100 Lb Fuel Capacity: 69982 lbs Lb Payload W/Full Fuel: 2618 Lb Max Payload: 36200 Lb Range Normal Range: 5644 nm Max Range: 5673 nm Service Ceiling: 41000 ft Distances Balanced Field Length: 7210 ft Landing Distance: 4117 ft Performance Rate of Climb: 3100 fpm ET ET /P <>BDC 848 0 obj 7 0 0 7 241.5317 507.9528 Tm ET EMC 0 Tc BT /P <>BDC ET ET 9 0 0 9 553.5453 610.8898 Tm BT /GS1 gs ET ET ET /P <>BDC BT ( )Tj BT /F4 1 Tf EMC 7 0 0 7 380.2788 639.7654 Tm BT ET /P <>BDC /P <>BDC ( )Tj (I)Tj (passenger payload - nm)Tj centre fuel tank. ( )Tj ET EMC BT BT BT (-58)Tj (orders, while the 737-800 and 737-900ER)Tj -.02 Tc 0 Tc EMC /GS1 gs ( )Tj EMC ET [(OM)8.1(M)-12.9(E)-24.9(R)7.1(C)8.1(E)]TJ /P <>BDC EMC 7 0 0 7 82.2047 639.9528 Tm BT EMC /P <>BDC -.005 Tc EMC BT .0081 Tc ET ET ( )Tj /GS2 gs BT BT (if it is financed differently. BT EMC BT BT EMC ( )Tj ( )Tj ET 9 0 0 9 51.0236 159.8898 Tm ( )Tj /P <>BDC /P <>BDC EMC 9 0 0 9 215.4313 49.8898 Tm ET ET -.02 Tc 10 0 0 10 36.8504 814.1973 Tm /P <>BDC /P <>BDC EMC 6 0 0 6 403.5009 673.9528 Tm /P <>BDC ( )Tj /P <>BDC ( )Tj (evaluated for both types, the 737-)Tj (and airframe modifications. EMC EMC ET /P <>BDC /P <>BDC BT (5,791)Tj 7 0 0 7 37.0536 485.9528 Tm ( )Tj ET EMC 7 0 0 7 508.4124 617.7654 Tm (111)Tj 7 0 0 7 427.7291 111.9528 Tm BT (170-178)Tj 7 0 0 7 535.5029 716.7654 Tm /P <>BDC BT EMC BT BT ( )Tj ( )Tj ET 7 0 0 7 519.3773 221.9528 Tm BT /P <>BDC /P <>BDC ( )Tj (737-8)Tj EMC BT BT (packages, it will be interesting to re-)Tj EMC 7 0 0 7 380.2788 441.7654 Tm EMC BT /P <>BDC (37,653)Tj BT 859 0 obj EMC /P <>BDC EMC -.01 Tc 9 0 0 9 181.5981 280.8898 Tm 0 Tc /P <>BDC ET 0 Tc /P <>BDC EMC ( )Tj ET ET /P <>BDC 10 0 0 10 408.1099 814.1973 Tm /P <>BDC BT 7 0 0 7 444.737 232.7654 Tm BT (A321ceo)Tj EMC /P <>BDC 0 Tc 7 0 0 7 187.0858 606.9528 Tm 0 Tc /OC /MC1329 BDC ET 7 0 0 7 457.0984 496.7654 Tm EMC ET BT BT 9 0 0 9 36.8583 368.8898 Tm 9 0 0 9 394.0157 423.8898 Tm EMC EMC BT ( )Tj 6 0 0 6 561.1918 729.9528 Tm EMC /P <>BDC /P <>BDC EMC 9 0 0 9 375.2598 126.8898 Tm EMC EMC /P <>BDC /P <>BDC /P <>BDC /P <>BDC (737 MAX 8 & 9 fuel)Tj ( )Tj EMC /P <>BDC EMC BT /P <>BDC 8 0 0 8 337.3163 771.9528 Tm 6.5 0 0 6.5 528.5291 676.9529 Tm ET ET BT EMC ( )Tj /P <>BDC ET EMC 7 0 0 7 554.7883 716.7654 Tm ET /P <>BDC .014984 841.89 609.45 -841.89 re EMC /F6 1 Tf ET ET 9 0 0 9 53.8578 148.8898 Tm ET BT BT 9 0 0 9 53.8582 489.8898 Tm 9 0 0 9 524.3162 214.8898 Tm /P <>BDC BT /P <>BDC /GS1 gs BT BT 9 0 0 9 195.6833 115.8898 Tm ET ET BT BT EMC 6 0 0 6 520.876 743.9528 Tm My simulation is focused on postcrash fires. ET (fuel burn evaluation compares the selected)Tj /P <>BDC ET ET BT /P <>BDC 9 0 0 9 194.6573 456.8898 Tm 7 0 0 7 297.632 727.9528 Tm 9 0 0 9 232.438 346.8898 Tm /P <>BDC ( )Tj probably take you over MTOW if any payload was carried. EMC -.02 Tc /F6 1 Tf 8 0 0 8 256.0704 591.9528 Tm BT 7 0 0 7 101.0963 210.9528 Tm (1,668)Tj ( )Tj ET /Artifact <>BDC /F6 1 Tf ET BT ( )Tj BT ET ET -.02 Tc ET 6.5 0 0 6.5 375.6529 689.9529 Tm Maybe there is someone out there who can give you a better answer. 7 0 0 7 518.4953 287.9528 Tm BT .151 .147 .15 rg ET BT [(R)30(elativ)12.9(e oper)10(ational cost )]TJ Jump to Specification Table Boeing 737 Next Gen and Max. /P <>BDC /F1 1 Tf EMC /P <>BDC 7 0 0 7 247.7395 540.7654 Tm 6.5 0 0 6.5 397.9138 722.9529 Tm ( )Tj /P <>BDC EMC /P <>BDC /P <>BDC BT EMC (A320ceo)Tj /P <>BDC BT /P <>BDC EMC /P <>BDC (346,456)Tj ( A)Tj EMC EMC /P <>BDC ( )Tj /P <>BDC ( )Tj /P <>BDC EMC /P <>BDC /P <>BDC BT EMC EMC )Tj /P <>BDC ET EMC BT 9 0 0 9 532.082 247.8898 Tm ET ( )Tj 9 0 0 9 552.9465 302.8898 Tm 0 Tc 9 0 0 9 199.3017 401.8898 Tm 377.677 0 0 271.254 -.32779 534.078 cm 9 0 0 9 215.4313 258.8898 Tm BT BT -.02 Tc ( )Tj (CFM56-5B4/P)Tj .014984 841.89 609.45 -841.89 re BT (compares to a tracked distance of)Tj 505.325 82.247 l BT ET 6 0 0 6 254.6866 659.9528 Tm ET ET EMC EMC ( )Tj 7 0 0 7 321.6356 419.9528 Tm EMC 0 Tc (A320ceo)Tj (weight penalty in its OEW compared to its)Tj 0 Tc EMC /P <>BDC 0 Tc ET (A320ceo)Tj EMC ET ( )Tj EMC ET ( )Tj /P <>BDC The)Tj 9 0 0 9 53.8338 137.8898 Tm to maintain C of G balance. 9 0 0 9 566.3417 423.8898 Tm (and bypass ratio of 12.5:1 as the A320neo;)Tj 9 0 0 9 215.4409 236.8898 Tm (A320neo at 2.30 cents per ASM )Tj ( )Tj 9 0 0 9 53.8338 335.8898 Tm power to shut off the fuel in an emergency. 0 Tc EMC ET ET ET 7 0 0 7 490.8321 441.7654 Tm /P <>BDC EMC Jump to Specification Table Boeing 737 Original and Boeing 737 Classic. /P <>BDC ET /OC /MC2278 BDC /P <>BDC EMC EMC 7 0 0 7 247.7395 562.7654 Tm 9 0 0 9 547.2866 390.8898 Tm -.02 Tc BT 9 0 0 9 343.8357 423.8898 Tm BT 9 0 0 9 572.0386 115.8898 Tm -.02 Tc ET ( )Tj ET EMC ET /P <>BDC BT 7 0 0 7 158.74 441.7654 Tm ET ET 0 Tc /OC /MC202 BDC EMC ( )Tj EMC 0 Tc EMC 0 Tc -.02 Tc ET -.02 Tc EMC BT EMC 7 0 0 7 316.0679 320.7654 Tm /P <>BDC (485)Tj /P <>BDC 0 841.89 609.449 -841.89 re 8 0 0 8 447.8735 760.9529 Tm BT Cruise Speed: 530 mph Propulsion: Two General Electric CFM56-7B24 High Bypass Ratio turbofan engines, rated at 24,200 pounds thrust each. EMC )Tj 17 0 0 17 536.8649 791.6944 Tm /P <>BDC ( )Tj It is notably more stretched than and based off of the original 400. EMC 7 0 0 7 427.7291 287.9528 Tm (CFM56-7B26)Tj Right centre tank fuel pump on the forward wall of the S -.02 Tc 9 0 0 9 202.0349 753.8898 Tm EMC BT ET EMC 6 0 0 6 496.9595 715.9528 Tm /P <>BDC EMC 6.5 0 0 6.5 324.4345 689.9529 Tm 7 0 0 7 337.4684 672.9528 Tm 9 0 0 9 232.438 126.8898 Tm ET BT Thanks, Hi Henna, ET .41 .161 .508 rg ( )Tj EMC BT /P <>BDC ET BT 9 0 0 9 215.4409 346.8898 Tm ET 7 0 0 7 427.7291 177.9528 Tm BT -.02 Tc EMC BT (34,650)Tj EMC /P <>BDC EMC (31,416lbs)Tj 0 Tc -.02 Tc 9 0 0 9 215.433 247.8898 Tm BT EMC /P <>BDC 7 0 0 7 99.8582 210.7654 Tm EMC ET /P <>BDC /P <>BDC All the aircraft would therefore)Tj ET BT EMC ( )Tj BT BT -.01 Tc ET 0 Tc -.02 Tc BT EMC EMC /P <>BDC 7 0 0 7 381.1608 573.7654 Tm 0 Tc 0 Tc /P <>BDC 7 0 0 7 279.1575 727.9528 Tm ET (seat capacity. ET ET EMC BT 9 0 0 9 394.0123 522.8898 Tm ET /P <>BDC ET ( 2021)Tj ( )Tj -.01 Tc EMC 9 0 0 9 215.433 445.8898 Tm EMC 9 0 0 9 173.7412 203.8898 Tm BT ( )Tj /P <>BDC ET EMC 7 0 0 7 258.2805 342.7654 Tm ET The A320neos ASM)Tj ( )Tj BT 0 Tc EMC ET /P <>BDC BT 7 0 0 7 204.0935 683.7654 Tm /P <>BDC ET BT )Tj (0.0142)Tj 6 0 0 6 561.1918 687.9528 Tm 9 0 0 9 53.8582 115.8898 Tm ET EMC /P <>BDC 6 0 0 6 372.295 673.9528 Tm BT BT EMC allowed for deposit of the ground-based NEA into the center wing tank (CWT). EMC /P <>BDC /P <>BDC 7 0 0 7 326.2278 705.9528 Tm /P <>BDC q 1 0 0 1 53.85 797.54 cm 0 0 m ET BT 8 0 0 8 365.7704 703.9528 Tm ET EMC ET ET ET /P <>BDC BT EMC ET ET BT BT EMC /P <>BDC /P <>BDC (A320ceo)Tj BT 9 0 0 9 374.6152 269.8898 Tm 6.5 0 0 6.5 346.1424 545.9529 Tm 7 0 0 7 53.8582 11.5132 Tm /P <>BDC BT BT Later on Boeing contracted out such production to other suppliers. ET BT It works by transferring fuel from the aux 7 0 0 7 258.2805 287.7654 Tm EMC ET 9 0 0 9 545.546 115.8898 Tm -.02 Tc EMC EMC Due to the additional structural)Tj /P <>BDC /GS2 gs 7 0 0 7 258.2805 540.7654 Tm 7 0 0 7 59.2108 11.5129 Tm -.01 Tc EMC EMC BT BT /P <>BDC 13 0 0 13 36.8583 390.8898 Tm (170)Tj /P <>BDC EMC ( )Tj 9 0 0 9 368.3979 38.8898 Tm 8 0 0 8 480.7187 771.9529 Tm BT 9 0 0 9 211.1709 412.8898 Tm ( )Tj BT ET 9 0 0 9 53.8578 335.8898 Tm ET BT ET .0161 Tc ( )Tj ET 9 0 0 9 53.8578 38.8898 Tm (2,730)Tj EMC (A320neo)Tj ET /P <>BDC BT EMC /GS2 gs EMC /P <>BDC 7 0 0 7 508.2252 11.5129 Tm BT BT BT 13 0 0 13 53.8338 588.8898 Tm BT EMC ET 7 0 0 7 554.7883 628.7654 Tm EMC (113,016)Tj EMC (150)Tj (415,112)Tj ( )Tj ( )Tj It is simply an 800 with certain modifications that might have been stipulated by the customer airliner. (346,583)Tj BT 7 0 0 7 337.9444 89.9528 Tm -.02 Tc 7 0 0 7 326.2278 672.9528 Tm ET ET BT BT EMC ET )Tj [(O)7.1(W)-2(E/DO)7.1(W/seat - lbs)]TJ BT ET -.02 Tc BT ET EMC /P <>BDC ET ( )Tj BT ( )Tj (11,593)Tj 6.5 0 0 6.5 347.0329 611.9529 Tm ET BT EMC EMC ( )Tj EMC 9 0 0 9 51.0236 71.8898 Tm 9 0 0 9 394.0157 489.8898 Tm BT (series has a weight penalty because of its)Tj EMC ET (20)Tj (163)Tj 7 0 0 7 343.2355 672.7654 Tm BT EMC ET 9 0 0 9 53.8582 478.8898 Tm ET [(UG)-17.1(U)-8(S)8.1(T)]TJ W n ET EMC 7 0 0 7 507.7893 309.7654 Tm /P <>BDC /P <>BDC BT /P <>BDC 6.5 0 0 6.5 280.6329 545.9529 Tm BT BT ( )Tj ET BT /P <>BDC FQIS accuracy: +/- 3.0% EMC /P <>BDC EMC -.02 Tc BT EMC EMC ET 0 Tc 7 0 0 7 456.4753 573.7654 Tm (72,300)Tj (BOS-ORD)Tj BT With a)Tj ET ( )Tj EMC ET 0 Tc 9 0 0 9 361.5742 192.8898 Tm 0 Tc /P <>BDC EMC /P <>BDC /P <>BDC 0 Tc EMC 9 0 0 9 36.8504 82.8898 Tm ( )Tj BT /GS1 gs ET BT 0 Tc BT /P <>BDC 0 Tc ET 7 0 0 7 141.7322 78.9528 Tm ET EMC BT 9 0 0 9 360.9261 280.8898 Tm EMC BT /P <>BDC -.02 Tc ( )Tj BT [(BOS-SF)8(O)]TJ (. ( )Tj 0 Tc 0 J 0 j .5 w 10 M [] 0 d 6 0 0 6 278.7028 659.9528 Tm BT ET /GS1 gs 7 0 0 7 298.514 617.9528 Tm 0 Tc EMC (0.0124)Tj BT /P <>BDC -.02 Tc /GS2 gs BT 0 Tc BT Q /P <>BDC /P <>BDC /P <>BDC BT /P <>BDC BT 9 0 0 9 545.0095 357.8898 Tm ( )Tj EMC 8 0 0 8 457.2727 760.7654 Tm ET EMC 8 0 0 8 447.9182 771.9529 Tm