ET EMC EMC ET EMC ET (104)Tj ET /P <>BDC /P <>BDC (0.0129)Tj /P <>BDC (1B28B1)Tj EMC 7 0 0 7 508.4124 188.7654 Tm (109,800)Tj EMC 7 0 0 7 141.7322 111.9528 Tm (34,650lbs)Tj (1,311)Tj BT BT BT 9 0 0 9 121.2888 38.8898 Tm ET EMC (A320ceo)Tj ( )Tj [(E)-7.8(P)16.1(T)9(E)-13.9(MBE)-16.9(R)]TJ (and considered against the A320 current)Tj 9 0 0 9 394.0315 346.8898 Tm EMC ET (or scenarios in this study. EMC 5 0 0 5 484.5872 11.5129 Tm BT 0 Tc BT ET BT BT BT 7 0 0 7 316.0679 397.7654 Tm EMC BT (178)Tj BT ET -2.9413 -1.4846 -3.0524 -2.0356 -3.053 -2.8052 c ( )Tj /P <>BDC /P <>BDC EMC BT 0 Tc BT BT 6 0 0 6 527.3389 687.9528 Tm /P <>BDC ( )Tj 6 0 0 6 444.3028 659.9528 Tm -.02 Tc -.01 Tc ( )Tj 7 0 0 7 82.8504 265.9528 Tm 0 Tc ( )Tj /P <>BDC 7 0 0 7 430.039 705.9528 Tm EMC (using long-range cruise \(LRC\))Tj (10)Tj ( )Tj ( )Tj ET 0 Tc ET BT EMC ET BT /P <>BDC Additional Aircraft accessibility information is available online for customers with disabilities.. Aircraft specifications. ET 7 0 0 7 518.4953 386.9528 Tm 9 0 0 9 36.8504 192.8898 Tm EMC (2,498)Tj (passengers. /P <>BDC 0 Tc 9 0 0 9 547.3802 566.8898 Tm 7 0 0 7 258.2805 694.7654 Tm BT 0 Tc ( )Tj BT ET /P <>BDC (68.3 inches and a bypass ratio of up to)Tj /P <>BDC EMC ( )Tj BT EMC ( )Tj 7 0 0 7 537.7804 408.9528 Tm EMC ( )Tj 9 0 0 9 215.4409 445.8898 Tm EMC (977)Tj EMC 9 0 0 9 411.0181 269.8898 Tm EMC ET 6.5 0 0 6.5 54.877 611.9529 Tm /P <>BDC 7 0 0 7 487.0872 11.5129 Tm 5.25 0 0 5.25 64.5461 11.5129 Tm EMC 9 0 0 9 215.4313 247.8898 Tm BT ( )Tj 8 0 0 8 551.3604 71.8898 Tm 0 Tc The pumps should be switched off and considered inop until they can be /P <>BDC /P <>BDC BT 7 0 0 7 37.0536 606.9528 Tm ET ET 9 0 0 9 394.0315 302.8898 Tm /F6 1 Tf /P <>BDC /P <>BDC /Artifact <>BDC /P <>BDC 6 0 0 6 153.9401 659.9528 Tm (150)Tj /P <>BDC [(v)21(ariant)]TJ EMC EMC ( )Tj 7 0 0 7 445.619 617.7654 Tm EMC -.01 Tc /P <>BDC ET ET /P <>BDC (0.0141)Tj 7 0 0 7 125.6292 628.7654 Tm 7 0 0 7 294.4014 639.7654 Tm /P <>BDC 7 0 0 7 474.3564 529.9528 Tm /P <>BDC EMC EMC ET EMC BT (977)Tj ET EMC ( )Tj BT /P <>BDC BT Q 6.5 0 0 6.5 375.6529 702.9529 Tm ET /P <>BDC BT ET EMC BT 6.5 0 0 6.5 244.3754 565.9529 Tm ( )Tj BT ET ET (compared to the A320ceo. /TT2 1 Tf EMC /P <>BDC ET BT BBJ style winglets are offered as an optional feature for the -800. BT This narrow body jet airliner had first rolled out on June 30, 1997 and shortly after was had its first test flight with he pilot Jim McRoberts in the cockpit. 7 0 0 7 387.0159 661.9528 Tm 7 0 0 7 380.2788 485.7654 Tm 7 0 0 7 445.619 496.7654 Tm BT /P <>BDC BT BT ( )Tj (capacity of 6,353USG, giving it a range of)Tj EMC -.02 Tc (5,376)Tj , http://toulouse747.com/wp-content/uploads/2018/12/Boeing-B737-700-800-900-Operations-Manual.pdf. ( )Tj BT ET /P <>BDC BT 7 0 0 7 158.74 188.7654 Tm ET EMC ET BT /P <>BDC ET /P <>BDC EMC 7 0 0 7 386.3929 716.9528 Tm ET BT ( )Tj (1,392)Tj ( )Tj -.02 Tc ET ( )Tj ET BT .014984 824.882 572.583 17.008 re BT BT EMC BT /P <>BDC 0 Tc /P <>BDC EMC EMC 0 Tc ( )Tj .41 .161 .508 rg ET 7 0 0 7 37.8848 452.9528 Tm .0081 Tc ET BT BT BT <>/ExtGState<>/Properties<>>> /P <>BDC EMC ( )Tj (0.0124)Tj ET ET BT (208)Tj ET /P <>BDC /P <>BDC EMC BT BT ET /P <>BDC EMC /P <>BDC EMC -.02 Tc (136)Tj EMC EMC -.02 Tc BT 7 0 0 7 241.2727 661.9528 Tm 0 Tc -.02 Tc EMC EMC /P <>BDC (same number of passengers is carried on)Tj .41 .161 .508 RG 9 0 0 9 68.0314 38.8898 Tm ET /P <>BDC (on the same sector is almost the same as)Tj (34,650)Tj 5.25 0 0 5.25 123.5367 11.5132 Tm ET (mainline carriers may in fact opt to use a)Tj BT /P <>BDC /P <>BDC ET ET ( )Tj EMC ET ET (0.0149)Tj ( )Tj /P <>BDC BT 6.5 0 0 6.5 346.5844 735.9529 Tm [(E)-7.8(P)16.1(T)9(E)-13.9(MBE)-16.9(R)]TJ 0 Tc ( )Tj As stated, this makes a fair)Tj BT ( )Tj 7 0 0 7 457.0984 408.7654 Tm 7 0 0 7 381.1608 562.7654 Tm ( )Tj /P <>BDC 0 Tc EMC 9 0 0 9 526.8993 643.8898 Tm (The A321ceo is equipped with either:)Tj EMC EMC BT ET EMC ET ET 9 0 0 9 553.3671 214.8898 Tm EMC ( )Tj BT BT EMC BT (equivalent engine thrust ratings for the neo)Tj 6 0 0 6 371.479 757.9528 Tm /P <>BDC BT ( )Tj /P <>BDC EMC /P <>BDC EMC /P <>BDC 56 0 0 56 36.8606 562.1944 Tm BT ET ET 7 0 0 7 474.7064 133.9528 Tm ( )Tj -.02 Tc ( )Tj 7 0 0 7 456.2165 540.7654 Tm BT 7 0 0 7 141.7322 606.9528 Tm BT (128-137)Tj /P <>BDC -.01 Tc /P <>BDC BT EMC BT BT 7 0 0 7 355.3163 67.7654 Tm ET ET 9 0 0 9 68.0314 401.8898 Tm EMC BT BT BT 6.5 0 0 6.5 448.257 598.9529 Tm -.02 Tc /P <>BDC -.02 Tc /P <>BDC /P <>BDC ET ET EMC BT EMC 9 0 0 9 548.1865 522.8898 Tm BT BT BT ET BT 0 Tc 0 Tc EMC /P <>BDC ET ET /P <>BDC BT /P <>BDC ET EMC 9 0 0 9 232.438 280.8898 Tm /P <>BDC EMC ( )Tj EMC /P <>BDC BT 9 0 0 9 36.8504 49.8898 Tm /P <>BDC EMC ( )Tj ET ET BT (150)Tj (74-82)Tj (The fuel burn improvement on the)Tj EMC EMC /P <>BDC EMC 6.5 0 0 6.5 296.2827 637.9529 Tm /Artifact <>BDC 7 0 0 7 230.7317 232.9528 Tm BT BT /P <>BDC ( )Tj Boeings main competitor is with Airbus. /P <>BDC 7 0 0 7 440.0906 331.9528 Tm 8 0 0 8 334.994 661.9528 Tm BT ET ( )Tj 7 0 0 7 508.4124 243.7654 Tm EMC 9 0 0 9 543.767 93.8898 Tm ET BT ET ( )Tj ( )Tj sectors to ensure an even fuel balance. 9 0 0 9 394.0123 49.8898 Tm ET ET -.02 Tc /P <>BDC EMC BT /P <>BDC ET (bypass ratio of 9.0:1. BT BT /P <>BDC (31,416lbs)Tj BT EMC EMC BT Do you have a reference please? BT EMC /P <>BDC Q 0 Tw 7 0 0 7 141.7322 364.9528 Tm EMC 9 0 0 9 408.2047 489.8898 Tm BT EMC ET 786 0 obj BT ET -.02 Tc BT 9 0 0 9 193.6853 357.8898 Tm [(737-900E)-33(R)]TJ The aux tanks are located at I am looking for some spec information in more detail for a project (900ER\(W\) is limited to 165 passengers on)Tj 7 0 0 7 326.2278 485.9528 Tm BT ET ( )Tj /P <>BDC EMC EMC /P <>BDC EMC EMC EMC ET ET (A321neo)Tj EMC ET (. 0 Tc 0 Tc 8 0 0 8 74.9636 675.9528 Tm /P <>BDC /P <>BDC (l)Tj BT 7 0 0 7 53.8582 11.5132 Tm 9 0 0 9 232.4217 368.8898 Tm ( )Tj [(OM)8.1(M)-12.9(E)-24.9(R)7.1(C)8.1(E)]TJ /P <>BDC 9 0 0 9 53.8338 126.8898 Tm /P <>BDC ET ET /P <>BDC 7 0 0 7 363.2711 507.9528 Tm ET /P <>BDC -.02 Tc ET /P <>BDC ET ET (39,270)Tj ET ET (420)Tj EMC BT [(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 (152)Tj ET EMC EMC 9 0 0 9 553.1277 291.8898 Tm 7 0 0 7 554.7883 89.7654 Tm EMC BT (A321neo)Tj EMC 7 0 0 7 258.2805 265.7654 Tm ET /P <>BDC 7 0 0 7 297.632 738.9528 Tm EMC ET ET EMC EMC BT ET 7 0 0 7 474.3564 584.9528 Tm BT 5 0 0 5 92.725 11.5132 Tm /P <>BDC /P <>BDC 7 0 0 7 279.1575 419.9528 Tm /P <>BDC ET ET EMC EMC ( )Tj EMC /P <>BDC BT BT (487)Tj ( )Tj BT /GS2 gs BT (passengers fewer than the A321ceo )Tj ET BT /P <>BDC BT 7 0 0 7 444.737 430.7654 Tm ET ET ET EMC 9 0 0 9 215.4313 181.8898 Tm [(BOS-D)17.1(T)-11(W)]TJ ET ET EMC 7 0 0 7 490.5101 617.9528 Tm /P <>BDC /P <>BDC ( )Tj EMC 0 Tc EMC /P <>BDC EMC (ASM for the 737-8 with the same payload)Tj EMC EMC (10)Tj ET EMC ET /P <>BDC .151 .147 .15 rg ET EMC 7 0 0 7 82.2047 474.9528 Tm EMC BT BT EMC EMC EMC BT EMC 7 0 0 7 54.5916 738.7654 Tm /P <>BDC BT BT /P <>BDC ET EMC EMC 9 0 0 9 186.9983 500.8898 Tm /OC /MC1329 BDC ET ET 9 0 0 9 389.8867 269.8898 Tm BT 0 Tc ET (makes a flight-for-flight comparison)Tj BT 0 Tc EMC (297,312)Tj ( The time spent in potential holding)Tj 19.843 0 l /P <>BDC /P <>BDC 0 Tc 6 0 0 6 339.5547 771.9528 Tm /P <>BDC /P <>BDC -.02 Tc BT BT /P <>BDC 0 Tc BT ET ET EMC ( )Tj /P <>BDC 7 0 0 7 354.6933 540.7654 Tm EMC EMC ET EMC A lower)Tj 0 Tc 9 0 0 9 194.7718 456.8898 Tm (0.0194)Tj /P <>BDC ET 9 0 0 9 53.8578 49.8898 Tm 0 Tc EMC /P <>BDC -.02 Tc EMC /F6 1 Tf ( )Tj 0 Tc /P <>BDC 7 0 0 7 535.5029 672.7654 Tm /P <>BDC 9 0 0 9 394.0315 555.8898 Tm BT (5,466)Tj BT ( )Tj ( )Tj ET (977)Tj (Boeing aircraft, the 737-800 has a 2.5%)Tj ET ET /P <>BDC BT /P <>BDC BT ET /P <>BDC 9 0 0 9 68.0314 522.8898 Tm 7 0 0 7 99.8582 320.7654 Tm BT BT ET /P <>BDC EMC /P <>BDC 8 0 0 8 99.8582 760.7654 Tm BT ET ET BT 7 0 0 7 321.4957 430.9528 Tm 6 0 0 6 507.6099 659.9528 Tm EMC ET BT BT EMC 7 0 0 7 539.8962 705.9528 Tm /P <>BDC ( )Tj 7 0 0 7 554.7883 562.7654 Tm ( )Tj ( )Tj )21(The r)10(elativ)12.9(e)]TJ ( )Tj (376)Tj EMC 7 0 0 7 321.6356 133.9528 Tm BT ET 17 0 0 17 36.8606 775.1944 Tm ET ET EMC 6 0 0 6 55.0668 729.9528 Tm BT (operator. 0 Tc ET BT BT /P <>BDC 7 0 0 7 456.2165 122.7654 Tm ( )Tj 7 0 0 7 490.5101 606.9528 Tm ET /GS2 gs ET 7 0 0 7 241.5317 595.9528 Tm 7 0 0 7 294.4014 463.7654 Tm ( )Tj 6.5 0 0 6.5 528.5291 676.9529 Tm -.02 Tc (A321ceo, in contrast to the A320neo over)Tj BT ET BT 9 0 0 9 543.3065 555.8898 Tm ( )Tj /P <>BDC )Tj 7 0 0 7 536.3849 67.7654 Tm 7 0 0 7 387.0932 298.9528 Tm BT 0 Tc ( )Tj EMC ET 9 0 0 9 53.8582 797.8898 Tm BT EMC ( )Tj BT 0 Tc BT (powered by either the CFM56-5 series or)Tj ET 7 0 0 7 337.6855 111.9528 Tm (486)Tj /P <>BDC ( )Tj 304.725 420.96 m 6.5 0 0 6.5 398.369 545.9529 Tm ( )Tj EMC /P <>BDC BT 0 Tc ET 7 0 0 7 380.2788 386.7654 Tm BT ET BT ET 7 0 0 7 131.6494 177.7654 Tm BT /P <>BDC /P <>BDC /P <>BDC /P <>BDC -.02 Tc f ET BT 7 0 0 7 279.1575 617.9528 Tm EMC EMC ET BT BT ( )Tj [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ EMC EMC (482)Tj EMC BT 9 0 0 9 181.3643 335.8898 Tm -.02 Tc ( )Tj 8 0 0 8 339.6345 760.7654 Tm 7 0 0 7 298.514 639.9528 Tm -.02 Tc 0 Tc EMC 7 0 0 7 518.4953 122.9528 Tm ( )Tj 9 0 0 9 204.4018 665.8898 Tm /P <>BDC (415,112)Tj BT BT /P <>BDC 9 0 0 9 215.4409 170.8898 Tm ET In contrast, Boeing has)Tj BT 0 Tc ET /P <>BDC /F1 1 Tf )Tj EMC (1,202)Tj /P <>BDC EMC BT ET EMC -.02 Tc BT 0 Tc ET BT 0 Tc 7 0 0 7 366.0641 694.9528 Tm ( )Tj 7 0 0 7 99.5912 683.9528 Tm (136)Tj /P <>BDC /P <>BDC /P <>BDC (37,653lbs)Tj ET EMC ET 9 0 0 9 53.8582 214.8898 Tm 9 0 0 9 36.8504 412.8898 Tm (977)Tj 8 0 0 8 394.0157 797.8898 Tm BT ET EMC /P <>BDC 0 Tc /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 8 0 0 8 394.0237 38.8898 Tm EMC (1,824)Tj BT /P <>BDC ( )Tj 9 0 0 9 246.6113 401.8898 Tm ET ( )Tj ET BT BT 9 0 0 9 211.1709 412.8898 Tm EMC ( )Tj EMC to the centre tank through a manual valve by cabin pressure. ( )Tj EMC 9 0 0 9 554.9974 456.8898 Tm ( )Tj EMC /P <>BDC ET 7 0 0 7 362.3891 243.9528 Tm BT ET (409,650)Tj BT .023 .567 .626 rg BT BT 0 Tc BT BT EMC BT (34,650)Tj BT )Tj /P <>BDC EMC ET ( )Tj Cheers Peter. EMC BT BT ( )Tj EMC /P <>BDC ( )Tj ( )Tj 7 0 0 7 279.1575 529.9528 Tm BT 7 0 0 7 539.8962 672.9528 Tm /P <>BDC ET /P <>BDC Note: for aircraft delivered after May 2004, centre tank -.02 Tc BT BT ET 7 0 0 7 125.6292 188.7654 Tm EMC -.02 Tc ET 6.5 0 0 6.5 427.5934 742.9529 Tm /P <>BDC /P <>BDC EMC BT /P <>BDC ET 9 0 0 9 537.6038 170.8898 Tm /P <>BDC EMC EMC BT /P <>BDC /P <>BDC BT /P <>BDC /P <>BDC EMC ET /F6 1 Tf EMC 0 Tc ET ET BT EMC BT BT BT /P <>BDC ET ET /P <>BDC (0.0122)Tj BT W n (A321ceo is passenger payload-restricted on)Tj 7 0 0 7 321.6356 188.9528 Tm [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ EMC ( )Tj BT BT /P <>BDC EMC BT 9 0 0 9 536.0613 49.8898 Tm 7 0 0 7 230.7317 738.9528 Tm /P <>BDC BT BT EMC ET ET The)Tj .661 .752 .896 rg /P <>BDC /P <>BDC BT (which is BOS-LAX, whereas the 737-800)Tj 6.5 0 0 6.5 191.63 565.9529 Tm BT 9 0 0 9 408.1854 566.8898 Tm ET EMC 8 0 0 8 257.7904 661.9528 Tm ET ( )Tj 7 0 0 7 125.6292 243.7654 Tm EMC /P <>BDC 0 Tc BT (compares to a tracked distance of)Tj /P <>BDC EMC ( )Tj EMC /P <>BDC
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