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ET 9 0 0 9 177.6653 445.8898 Tm BT -.02 Tc BT 8 0 0 8 239.3289 771.7654 Tm BT BT EMC EMC EMC EMC BT -.02 Tc /P <>BDC ( )Tj EMC 0 Tc ( )Tj ET /P <>BDC (178-187)Tj 9 0 0 9 232.4408 797.8898 Tm 7 0 0 7 338.6433 419.7654 Tm BT (A320ceo: )Tj ET ET 0 Tc BT ET BT BT /P <>BDC 9 0 0 9 232.4217 38.8898 Tm ( )Tj EMC Reads payload (passenger and baggage) weights via FSUIPC. ET EMC ET /P <>BDC -.02 Tc /P <>BDC BT EMC EMC ( )Tj 7 0 0 7 107.1165 474.9528 Tm ET ( )Tj /P <>BDC ( )Tj ET /P <>BDC -.01 Tc BT ET ET ET 7 0 0 7 230.7317 166.9528 Tm ( )Tj 7 0 0 7 535.5029 683.7654 Tm /P <>BDC concentration at eight different locations. /P <>BDC /P <>BDC /P <>BDC 6 0 0 6 115.2799 687.9528 Tm 8 0 0 8 225.1837 661.9528 Tm /GS2 gs ET BT ( )Tj /P <>BDC EMC ET /P <>BDC /P <>BDC -.02 Tc 9 0 0 9 411.0097 181.8898 Tm ET 6 0 0 6 434.211 701.9528 Tm ET EMC BT ET EMC BT 7 0 0 7 380.2788 441.7654 Tm (. ET ET 9 0 0 9 551.4604 269.8898 Tm BT EMC /P <>BDC ET -.02 Tc BT /P <>BDC EMC /P <>BDC EMC ET ( )Tj BT BT ( )Tj BT EMC BT /P <>BDC BT [(737-900E)-33(R)]TJ 7 0 0 7 316.0679 320.7654 Tm -.02 Tc /F6 1 Tf /F6 1 Tf q 7 0 0 7 320.7537 78.9528 Tm ET EMC ET /P <>BDC EMC EMC BT ET BT 0 Tc BT BT EMC EMC /F1 1 Tf /P <>BDC ( )Tj /P <>BDC /P <>BDC 7 0 0 7 316.0679 331.7654 Tm BT 9 0 0 9 215.4409 269.8898 Tm -.02 Tc EMC EMC /P <>BDC .7 -.5345 .9114 -1.2305 y /P <>BDC ET ( )Tj EMC -.02 Tc /P <>BDC (compared to the CFM56-7B-powered 737-)Tj /GS1 gs BT EMC /P <>BDC 0 Tc /P <>BDC 0 Tc ET ( )Tj BT 9 0 0 9 388.8047 390.8898 Tm BT BT (1,161)Tj /P <>BDC /P <>BDC BT (2,517)Tj EMC /P <>BDC error codes 1, 3, 5 or 7 /P <>BDC ET EMC /P <>BDC EMC BT f BT -.02 Tc 7 0 0 7 337.6855 232.9528 Tm BT ET (CFM56-5B3/P)Tj /P <>BDC -.02 Tc /GS2 gs -.01 Tc EMC /P <>BDC /P <>BDC BT /P <>BDC 9 0 0 9 53.8578 148.8898 Tm EMC 0 Tc ( )Tj /P <>BDC EMC (0.0154)Tj 19.84 0 l (209)Tj ET ET EMC 0 Tc EMC BT BT BT 0 Tc 9 0 0 9 394.0157 599.8898 Tm ET 0 Tc /P <>BDC BT BT /P <>BDC /P <>BDC EMC ( )Tj /P <>BDC BT BT ET 9 0 0 9 207.4166 137.8898 Tm /P <>BDC EMC BT 9 0 0 9 186.0353 291.8898 Tm EMC 7 0 0 7 258.2805 133.7654 Tm BT /P <>BDC 10 0 0 10 64.6596 794.2914 Tm EMC BT ET ( )Tj refuelling panel to AUX TANKS. ET /P <>BDC /P <>BDC 6.5 0 0 6.5 54.2794 735.9529 Tm 9 0 0 9 394.0237 269.8898 Tm /F1 1 Tf /P <>BDC ET ET /P <>BDC /F1 1 Tf EMC BT EMC ( )Tj ET BT (0.0153)Tj BT /P <>BDC EMC endobj /P <>BDC /P <>BDC [(CFM L)17.1(E)-8.1(AP-1B27)]TJ -.02 Tc /P <>BDC ( )Tj ( )Tj /P <>BDC .176 .307 .621 rg BT /P <>BDC ( )Tj /F6 1 Tf /P <>BDC 7 0 0 7 427.7291 375.9528 Tm ET BT ET /P <>BDC 9 0 0 9 411.0181 467.8898 Tm [(CFM L)17.1(E)-8.1(AP-1B27)]TJ ( )Tj BT BT EMC 7 0 0 7 355.3163 144.7654 Tm ET ET /P <>BDC ET BT 7 0 0 7 125.6292 639.7654 Tm EMC -.01 Tc /P <>BDC EMC This fuel would give a EMC ET (0.0149)Tj EMC /P <>BDC 9 0 0 9 372.9598 170.8898 Tm /P <>BDC ET (The second comparison is payload)Tj 0 Tc EMC /P <>BDC /P <>BDC 9 0 0 9 190.8846 379.8898 Tm EMC BT (70)Tj 9 0 0 9 546.6454 60.8898 Tm ( )Tj /P <>BDC ET (between: the Pratt & Whitney PW1127G,)Tj BT ET ( )Tj ET /P <>BDC /P <>BDC EMC EMC BT BT 161.574 0 l ( )Tj EMC 1 i /P <>BDC 6.5 0 0 6.5 273.8079 676.9529 Tm 0 Tc BT EMC q 1 0 0 1 411.023 799.878 cm 0 0 m EMC 0 Tc 6.5 0 0 6.5 549.8557 650.9529 Tm BT ET ET ET 9 0 0 9 68.3339 467.8898 Tm /P <>BDC 7 0 0 7 118.104 111.7654 Tm /P <>BDC q 1 0 0 1 36.85 469.878 cm 0 0 m /P <>BDC BT ( )Tj EMC /P <>BDC ( )Tj ( )Tj (190,800)Tj ET (170)Tj ET 0 Tc EMC (379)Tj BT -.02 Tc ( )Tj ET ( )Tj /P <>BDC EMC /P <>BDC 6.5 0 0 6.5 549.8557 585.9529 Tm (he 737 MAX returned to revenue)Tj /P <>BDC (be charged the same in operation for this)Tj BT EMC EMC BT BT /P <>BDC EMC EMC 0 Tc ET EMC /P <>BDC ET 9 0 0 9 36.8504 335.8898 Tm 7 0 0 7 536.3849 584.7654 Tm BT ET /P <>BDC ET /Artifact <>BDC ET ET BT BT EMC ET -.02 Tc /P <>BDC BT EMC 9 0 0 9 232.4408 742.8898 Tm /P <>BDC 9 0 0 9 564.8379 269.8898 Tm ( )Tj /P <>BDC EMC ET /P <>BDC 0 Tc Hi. ( )Tj 7 0 0 7 193.1059 584.9528 Tm BT (3,300 -)Tj ET EMC BT /P <>BDC ET 5 0 0 5 484.5872 11.5129 Tm EMC /P <>BDC EMC /P <>BDC 9 0 0 9 394.0123 621.8898 Tm (heavier than the A320ceo. /P <>BDC BT EMC 7 0 0 7 457.0984 243.7654 Tm 7 0 0 7 141.7322 276.9528 Tm ( )Tj ( )Tj 0 Tc /P <>BDC ( )Tj -.02 Tc 9 0 0 9 203.511 621.8898 Tm EMC 7 0 0 7 321.6356 210.9528 Tm BT ET /P <>BDC (All the flights were in a westerly)Tj EMC /P <>BDC ( )Tj EMC EMC 0 Tc BT 9 0 0 9 392.5128 236.8898 Tm 6.5 0 0 6.5 397.8619 611.9529 Tm EMC 6 0 0 6 55.0668 701.9528 Tm 9 0 0 9 232.4217 291.8898 Tm 7 0 0 7 54.7071 375.7654 Tm EMC sectors to ensure an even fuel balance. /P <>BDC Hi Jeffrey, /P <>BDC ET ET /P <>BDC /P <>BDC ET 7 0 0 7 258.2805 485.7654 Tm EMC 7 0 0 7 427.7291 243.9528 Tm BT ET BT ET /P <>BDC 9 0 0 9 195.4763 258.8898 Tm Note: Specifications are listed as standard and may vary slightly. /P <>BDC (26,000lbs thrust on the A320neo powered)Tj 8 0 0 8 332.978 591.9528 Tm ( )Tj EMC /P <>BDC /P <>BDC BT -.02 Tc EMC ( )Tj ET ( )Tj -.02 Tc '''''''''' z" ( )Tj BT BT EMC /P <>BDC /P <>BDC /P <>BDC 7 0 0 7 445.619 364.7654 Tm 0 Tc EMC /P <>BDC /P <>BDC EMC (Block fuel)Tj ( )Tj ( )Tj ( )Tj BT ( )Tj BT /P <>BDC 0 Tc /GS2 gs BT (0.0129)Tj BT EMC ET 7 0 0 7 321.6356 419.9528 Tm /P <>BDC /P <>BDC BT EMC EMC EMC BT (0.0113)Tj EMC /P <>BDC /P <>BDC /OC /MC1974 BDC -.02 Tc EMC BT BT [(T)95.9(o)0( do)12(wnload mor)10(e than 1,200)]TJ ET /P <>BDC ( )Tj 7 0 0 7 258.2805 67.7654 Tm /F4 1 Tf BT /P <>BDC EMC ET ET ALERT light illuminates on the main panel. ET -.02 Tc ( )Tj (A321ceo)Tj /P <>BDC (34,650)Tj ET 7 0 0 7 316.0679 375.7654 Tm /P <>BDC ET ET BT (404)Tj (A320neo)Tj BT EMC ET EMC 6 0 0 6 178.2463 729.9528 Tm /P <>BDC (-61)Tj 7 0 0 7 554.7883 595.7654 Tm BT /P <>BDC EMC not sure where to find that kind of detail. EMC 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? BT (. 7 0 0 7 440.0906 232.9528 Tm EMC EMC EMC BT /P <>BDC ET W n /P <>BDC (550)Tj 9 0 0 9 394.0315 368.8898 Tm [(O)7.1(W)-2(E/DO)7.1(W/seat - lbs)]TJ EMC (27,000lbs of thrust compared to the)Tj EMC 6 0 0 6 247.27 771.9528 Tm EMC /P <>BDC (120-128)Tj BT EMC The typical range for this)Tj BT 8 0 0 8 225.1837 717.9528 Tm EMC (-59)Tj EMC 9 0 0 9 53.8582 412.8898 Tm /F7 1 Tf /P <>BDC ( )Tj BT ET EMC BT 6.5 0 0 6.5 233.8677 532.9529 Tm EMC ET ( )Tj /P <>BDC BT 7 0 0 7 365.035 617.9528 Tm W n ( )Tj ( )Tj ET 9 0 0 9 553.1277 291.8898 Tm BT ET 7 0 0 7 473.8245 122.9528 Tm 7 0 0 7 447.3829 705.7654 Tm EMC /P <>BDC ( )Tj EMC 9 0 0 9 524.3162 214.8898 Tm EMC ET (this evaluation. EMC BT ET BT 0 Tc EMC ET ET EMC 9 0 0 9 232.438 225.8898 Tm 7 0 0 7 316.0679 309.7654 Tm BT (which has the lowest fuel burn rate per)Tj BT /P <>BDC 0 Tc 7 0 0 7 457.0984 595.7654 Tm EMC ET ET 0 Tc -.02 Tc EMC /P <>BDC 0 Tc BT 7 0 0 7 355.3163 320.7654 Tm /P <>BDC 6.5 0 0 6.5 474.3939 663.9529 Tm 9 0 0 9 150.2504 434.8898 Tm /P <>BDC EMC 7 0 0 7 99.5912 507.9528 Tm EMC 7 0 0 7 554.7883 408.7654 Tm /P <>BDC /P <>BDC 9 0 0 9 194.6103 401.8898 Tm BT EMC BT /P <>BDC BT BT ( )Tj 7 0 0 7 518.4953 331.9528 Tm 9 0 0 9 53.8338 269.8898 Tm 7 0 0 7 241.5317 221.9528 Tm (-62)Tj /P <>BDC EMC ( )Tj ( )Tj BT S ( )Tj BT (0.0158)Tj EMC /P <>BDC (163)Tj EMC BT /P <>BDC EMC ET EMC ( )Tj (SEA, SFO, YVR and LAX. /P <>BDC ET EMC ET 5 0 0 5 92.725 11.5132 Tm /P <>BDC BT ( )Tj BT ET /P <>BDC 9 0 0 9 36.8504 478.8898 Tm ET EMC EMC 7 0 0 7 387.0159 617.9528 Tm )Tj ET ( )Tj /P <>BDC EMC ( )Tj ET 7 0 0 7 456.2165 100.7654 Tm (0.0112)Tj EMC EMC ET (and bypass ratio of 12.5:1 as the A320neo;)Tj /P <>BDC /P <>BDC 0 Tc 0 Tc 7 0 0 7 196.5683 320.7654 Tm BT 9 0 0 9 36.8504 203.8898 Tm 9 0 0 9 394.0237 357.8898 Tm /P <>BDC (109)Tj /P <>BDC BT BT ET 0 Tc ET ET EMC EMC /P <>BDC 9 0 0 9 232.438 115.8898 Tm ( )Tj EMC /P <>BDC ( )Tj (A)Tj 0 Tc ET BT 7 0 0 7 427.7291 199.9528 Tm 0 Tc ET 9 0 0 9 393.5047 181.8898 Tm ( )Tj BT ( )Tj /P <>BDC /P <>BDC /P <>BDC 0 Tc ET ET (l)Tj BT .014984 841.89 609.45 -841.89 re (operation. BT ET EMC BT EMC ET ET ET EMC ( )Tj /P <>BDC fuel pumps will automatically shut off when they detect a low output pressure. f ET ET ET ET [(equal-siz)6.1(ed 737NG counterpar)-23(ts and A320ceo)]TJ (737-9)Tj 7 0 0 7 82.2047 463.9528 Tm /P <>BDC ET ET /P <>BDC (A320ceo)Tj 9 0 0 9 215.4313 181.8898 Tm ET EMC ( )Tj /P <>BDC to the centre tank through a manual valve by cabin pressure. EMC ET 9 0 0 9 394.0157 159.8898 Tm BT EMC EMC /P <>BDC -.01 Tc BT EMC 9 0 0 9 207.5339 280.8898 Tm -.02 Tc /P <>BDC ET EMC ET EMC (31,416)Tj 7 0 0 7 444.737 232.7654 Tm ET ET ( )Tj [(OM)8.1(M)-12.9(E)-24.9(R)7.1(C)8.1(E)]TJ -.02 Tc /P <>BDC EMC EMC EMC BT ( )Tj /P <>BDC Neither the 737-800 nor the 737-8)Tj 7 0 0 7 380.2788 496.7654 Tm 9 0 0 9 201.162 500.8898 Tm BT ET -.02 Tc 0 Tc BT EMC ( )Tj /P <>BDC BT /P <>BDC (and the 737 MAX family with the CFM)Tj 7 0 0 7 364.1531 463.9528 Tm ET ET 0 Tc /P <>BDC [(Oper)10(ating Assumptions )]TJ ET ET 9 0 0 9 211.035 709.8898 Tm (packages, it will be interesting to re-)Tj ET 7 0 0 7 141.7322 78.9528 Tm This)Tj -.01 Tc EMC /P <>BDC 7 0 0 7 338.6433 188.7654 Tm ET EMC ET ET BT ET 6.5 0 0 6.5 499.7986 637.9529 Tm 9 0 0 9 372.6154 236.8898 Tm EMC 7 0 0 7 507.7893 309.7654 Tm (150)Tj BT EMC ET 7 0 0 7 491.7142 408.7654 Tm BT /P <>BDC EMC ( )Tj EMC EMC /P <>BDC 8 0 0 8 505.7415 771.9528 Tm 9 0 0 9 215.4313 467.8898 Tm (comparing the 737-800 with the 737-8,)Tj ET BT 8 0 0 8 315.034 760.7654 Tm EMC ET BT This is equivalent to)Tj 0 Tc BT 7 0 0 7 444.737 100.7654 Tm 108 lbs (49 kgs) to the 737-800 basic MEW. BT ET ET ET 7 0 0 7 294.4014 441.7654 Tm ET ( )Tj /P <>BDC 7 0 0 7 158.74 540.7654 Tm ET EMC 7 0 0 7 537.7804 331.9528 Tm BT (the longest BOS-LAX sector. 0 J 0 j 5 w 10 M [] 0 d ET 6.5 0 0 6.5 233.8677 611.9529 Tm BT 0 Tc ET ET /P <>BDC EMC ET BT ET .559 .331 .619 rg /P <>BDC ET (150)Tj 0 Tc /F6 1 Tf (297,312)Tj EMC ( )Tj BT BT 7 0 0 7 230.7317 100.9528 Tm (482)Tj (evaluation both taxi-out and taxi-in were)Tj EMC endstream EMC /P <>BDC BT ET EMC ET BT EMC /P <>BDC BT .008 Tc ( )Tj EMC EMC EMC 9 0 0 9 411.0097 126.8898 Tm 9 0 0 9 53.8582 511.8898 Tm ( )Tj ( )Tj ET 9 0 0 9 394.0315 434.8898 Tm 0 Tc -.02 Tc EMC BT 1 i BT BT BT EMC BT Hi, How can I learn aerospace materails about a and b basis allowables for Boeing-737 ? (831)Tj ET 6 0 0 6 154.1438 757.9528 Tm BT /GS2 gs BT -.01 Tc EMC ( )Tj Because of EMC 0 Tc 0 Tc 7 0 0 7 520.6108 639.9528 Tm EMC 9 0 0 9 411.0234 731.8898 Tm /P <>BDC BT -.02 Tc BT ( )Tj 9 0 0 9 36.8583 478.8898 Tm EMC BT ( )Tj 7 0 0 7 445.619 518.7654 Tm 9 0 0 9 165.1286 137.8898 Tm /F1 1 Tf 7 0 0 7 108.6215 133.9528 Tm (CFM56-5B3/P)Tj BT BT ( )Tj 9 0 0 9 361.7 456.8898 Tm /P <>BDC BT 9 0 0 9 36.8504 93.8898 Tm ET /P <>BDC ET 17 0 0 17 36.8606 791.6944 Tm BT EMC 7 0 0 7 278.9827 430.9528 Tm BT 7 0 0 7 204.0935 133.7654 Tm 9 0 0 9 68.0314 467.8898 Tm /P <>BDC <>stream /P <>BDC 0 Tc ET ET [(CFM L)17.1(E)-8.1(AP-1B27)]TJ 9 0 0 9 367.9911 71.8898 Tm /P <>BDC /P <>BDC /P <>BDC /P <>BDC EMC 8 0 0 8 38.4438 591.9528 Tm EMC /OC /MC1956 BDC (types )Tj (171,961)Tj BT /P <>BDC Can you confirm if Im right or wrong? /P <>BDC /P <>BDC -.02 Tc /P <>BDC EMC 6 0 0 6 236.6735 673.9528 Tm ET ET (BOS-PHX)Tj 6.5 0 0 6.5 484.6315 545.9529 Tm )Tj /P <>BDC Hi Ben, 0 Tc 304.725 420.96 m .151 .147 .15 rg BT EMC /P <>BDC BT ET -.02 Tc ET BT /P <>BDC 9 0 0 9 555.1066 434.8898 Tm 7 0 0 7 37.0536 617.9528 Tm BT EMC /P <>BDC ( )Tj EMC The A321neo takes advantage of)Tj EMC ( )Tj ( )Tj ET /P <>BDC 9 0 0 9 371.548 291.8898 Tm BT ( )Tj BT /P <>BDC 6.5 0 0 6.5 192.111 735.9529 Tm BT 0 Tc EMC ( )Tj BT 0 Tc endobj ET EMC 9 0 0 9 211.249 302.8898 Tm .014984 824.882 572.583 17.008 re BT EMC 0 Tc BT BT BT 0 Tc 6 0 0 6 371.6897 659.9528 Tm BT /P <>BDC endstream /GS2 gs BT )Tj /P <>BDC BT EMC BT ET (temperature was set at ISA. ( )Tj 6.5 0 0 6.5 244.4599 676.9529 Tm ET /P <>BDC BT 7 0 0 7 210.1137 463.7654 Tm -.02 Tc BT BT [(Y)-7.1(XX/64)]TJ 7 0 0 7 158.74 221.7654 Tm ( )Tj ( )Tj EMC BT /P <>BDC 7 0 0 7 54.7071 199.7654 Tm ET /P <>BDC 9 0 0 9 36.8504 104.8898 Tm EMC EMC ET ET FQIS accuracy: +/- 2.0% overall EMC BT 7 0 0 7 445.619 727.7654 Tm (Although there have recently been)Tj /P <>BDC /GS2 gs /P <>BDC 8 0 0 8 37.0439 771.9528 Tm ET 9 0 0 9 408.1889 324.8898 Tm EMC ET EMC 7 0 0 7 491.4046 111.9528 Tm (20)Tj /P <>BDC 9 0 0 9 215.4409 38.8898 Tm BT EMC BT (\(ATC\) charges. /P <>BDC EMC )Tj 7 0 0 7 199.5784 639.7654 Tm /P <>BDC BT /P <>BDC 7 0 0 7 474.7064 133.9528 Tm /P <>BDC [(SS)-9.1(U)8(E)]TJ ET ( )Tj EMC BT (longest sectors from BOS to PHX,)Tj ET BT EMC /P <>BDC BT BT BT 7 0 0 7 387.0932 199.9528 Tm EMC BT ET /P <>BDC 6.5 0 0 6.5 384.8179 722.9529 Tm ( )Tj ET EMC ET EMC /P <>BDC [(737 M)-8.1(A)-24.9(X-8)]TJ .0081 Tc /P <>BDC BT BT /P <>BDC ET EMC /P <>BDC /P <>BDC ET ET ET BT ET EMC BT 7 0 0 7 490.5101 507.9528 Tm /P <>BDC The classics have 5 dripsticks in each wing tank and none in the centre 8 0 0 8 319.1147 771.9528 Tm 0 Tc -.01 Tc ET [(BOS-A)56.9(TL)]TJ ( )Tj BT 7 0 0 7 430.039 628.9528 Tm -.02 Tc [(CFM L)17.1(E)-8.1(AP-1A26)]TJ 0 Tc ET q 1 0 0 1 215.433 150.878 cm 0 0 m 9 0 0 9 372.2129 192.8898 Tm (39,270)Tj 0 Tc (19 seats more than the -800, and 13)Tj EMC (. EMC ( )Tj ( )Tj EMC ET [(CFM L)17.1(E)-8.1(AP-1B27)]TJ ( 2021)Tj BT ET /P <>BDC /P <>BDC ( )Tj /P <>BDC ET <> 7 0 0 7 337.9444 100.9528 Tm 7 0 0 7 141.7322 221.9528 Tm Q /P <>BDC ( )Tj -.02 Tc (Most mainline US carriers are using the)Tj EMC BT BT (operating performance are analysed here,)Tj BT BT /P <>BDC BT BT ET 7 0 0 7 456.2165 397.7654 Tm ET 9 0 0 9 386.9059 280.8898 Tm -.02 Tc BT -.3738 -6.1596 -.9177 -6.351 -1.6458 -6.3504 c -.02 Tc EMC /P <>BDC /P <>BDC EMC ( )Tj ET EMC /P <>BDC /P <>BDC ET 9 0 0 9 546.3754 159.8898 Tm 9 0 0 9 394.0237 423.8898 Tm ET ET ( )Tj 6 0 0 6 277.7064 715.9528 Tm EMC /P <>BDC BT BT 6 0 0 6 540.5396 715.9528 Tm [(BOS-Y)-50.1(YZ)]TJ /P <>BDC BT The same alternate airport was)Tj ET (for the purposes of this performance)Tj /P <>BDC /P <>BDC /P <>BDC ( )Tj EMC 8 0 0 8 165.2278 760.9528 Tm /P <>BDC BT ET ( )Tj EMC ( )Tj ET EMC EMC ET (96,500)Tj /P <>BDC 9 0 0 9 73.1083 500.8898 Tm /P <>BDC 9 0 0 9 375.0299 434.8898 Tm (These results will allow a better)Tj 5.25 0 0 5.25 492.6848 11.5129 Tm BT BT /P <>BDC 7 0 0 7 518.4953 89.9528 Tm EMC (10)Tj EMC 7 0 0 7 490.5101 562.9528 Tm 0 Tc BT /P <>BDC 9 0 0 9 411.0181 379.8898 Tm 9 0 0 9 553.0217 93.8898 Tm -.02 Tc /P <>BDC BT BT /P <>BDC /P <>BDC ET ( )Tj /OC /MC2261 BDC BT 13 0 0 13 205.5668 412.8898 Tm /P <>BDC 7 0 0 7 321.6356 342.9528 Tm EMC 9 0 0 9 207.867 368.8898 Tm -.02 Tc BT BT 9 0 0 9 425.1967 720.8898 Tm BT /P <>BDC ET (31,416lbs)Tj ( )Tj 9 0 0 9 192.1913 38.8898 Tm BT EMC q EMC 6.5 0 0 6.5 477.8064 689.9529 Tm EMC ET 7 0 0 7 539.8962 529.9528 Tm EMC 10 0 0 10 54.2544 814.1973 Tm /P <>BDC ET ET 0 Tc ET BT EMC EMC ET /P <>BDC /OC /MC21 BDC /P <>BDC /P <>BDC (170)Tj (the analysis is 20/29/143, so a total of 192)Tj EMC /P <>BDC ET EMC (98-107)Tj 9 0 0 9 565.1177 280.8898 Tm ET 9 0 0 9 232.4217 170.8898 Tm /P <>BDC EMC EMC 7 0 0 7 543.7693 11.5132 Tm ET ET (further improve the fuel cost per ASM)Tj )Tj EMC /P <>BDC /P <>BDC ( )Tj /P <>BDC (0.0126)Tj BT BT EMC 6.5 0 0 6.5 521.8278 742.9529 Tm BT EMC BT ( )Tj /P <>BDC 7 0 0 7 337.4684 738.9528 Tm ET BT ( )Tj 28.5749 0 TD 6.5 0 0 6.5 327.0283 637.9529 Tm /P <>BDC ET (31,416)Tj 7 0 0 7 82.2047 683.9528 Tm ET BT ET 0 Tc 0 Tc (2,731)Tj BT 7 0 0 7 241.5317 606.9528 Tm BT EMC EMC BT EMC EMC ET EMC 7 0 0 7 59.2108 11.5129 Tm /P <>BDC BT ET 0 Tc BT -2.4549 -3.9026 m BT ET ET ( )Tj /P <>BDC -.02 Tc /P <>BDC ET % -.02 Tc 0 Tc ET q 1 0 0 1 53.858 546.878 cm 0 0 m /P <>BDC )Tj -.02 Tc BT /P <>BDC ( )Tj /P <>BDC EMC 6.5 0 0 6.5 499.1812 650.9529 Tm ( )Tj 9 0 0 9 383.6209 423.8898 Tm 7 0 0 7 338.5674 474.9528 Tm ( )Tj ( )Tj 304.725 420.96 m ( )Tj ( )Tj EMC ET /P <>BDC BT Aux fuel control panel (Aft overhead panel). ET 6 0 0 6 472.7745 771.9528 Tm ( )Tj BT 0 Tc (CFM56-7B27B3)Tj BT 9 0 0 9 232.4217 258.8898 Tm BT ( 2021)Tj EMC (39,270)Tj /P <>BDC /P <>BDC EMC (31,416)Tj BT EMC ET 0 Tc 9 0 0 9 36.8504 390.8898 Tm 5.25 0 0 5.25 465.7151 11.5129 Tm /P <>BDC 7 0 0 7 204.0935 177.7654 Tm 6 0 0 6 184.9964 757.9528 Tm BT EMC BT /F6 1 Tf ET ET ET ( )Tj EMC ET BT /P <>BDC 7 0 0 7 141.7322 705.9528 Tm /P <>BDC /P <>BDC ( )Tj BT BT (1,162)Tj 0 Tc 0 Tc [(family competitors, the 737 M)-8.1(A)-24.9(X also has)]TJ EMC BT EMC ET /P <>BDC 19.841 0 l BT 7 0 0 7 539.8962 573.9528 Tm 7 0 0 7 101.0963 188.9528 Tm /P <>BDC BT 7 0 0 7 82.8504 166.9528 Tm /P <>BDC /P <>BDC EMC 9 0 0 9 411.0181 478.8898 Tm EMC ET ( )Tj (A321ceo)Tj 7 0 0 7 230.7317 441.9528 Tm BT EMC /P <>BDC (214,730)Tj /P <>BDC ET /P <>BDC 0 Tc EMC /P <>BDC /P <>BDC BT (ASM. 7 0 0 7 554.7883 276.7654 Tm BT 6 0 0 6 205.0069 701.9528 Tm 0 Tc BT /P <>BDC (737-800W)Tj BT EMC 0 841.89 609.449 -841.89 re 7 0 0 7 204.0935 386.7654 Tm BT 0 Tc ET 10 0 0 10 49.3644 814.1973 Tm (1,019)Tj BT ( )Tj 7 0 0 7 386.4701 386.9528 Tm 7 0 0 7 37.0536 661.9528 Tm 7 0 0 7 387.0159 606.9528 Tm EMC ( )Tj ET /P <>BDC ET EMC /P <>BDC 6 0 0 6 561.1918 743.9528 Tm 0 Tc ET Share Improve this answer Follow answered Aug 12, 2019 at 15:48 user14897 These variables are also important because there's an assumption that if you're riding a 737, certain load factors and distances are more likely. ET ET EMC 7 0 0 7 337.4684 672.9528 Tm EMC (2,347)Tj 6 0 0 6 433.9826 659.9528 Tm 0 Tc 8 0 0 8 53.9012 749.9529 Tm -.02 Tc ( )Tj ( )Tj EMC 7 0 0 7 118.104 210.7654 Tm ET ( )Tj -.02 Tc EMC BT ET /OC /MC19 BDC ET )Tj BT /P <>BDC ET ET ( )Tj EMC ( )Tj -.02 Tc /P <>BDC BT /P <>BDC ET (403)Tj 7 0 0 7 429.157 727.9528 Tm 8 0 0 8 141.7322 760.9528 Tm 7 0 0 7 490.8321 320.7654 Tm BT BT (484nm for the shortest BOS-YYZ)Tj ET BT /P <>BDC ( )Tj ET The fwd and aft tanks are switched off when the /P <>BDC ( )Tj ET /P <>BDC BT EMC -.02 Tc /P <>BDC EMC BT ( )Tj 0 Tc From July 2004 NGs have been delivered with markings on the ET 0 Tc EMC BT /P <>BDC 6.5 0 0 6.5 64.6596 689.9529 Tm EMC /P <>BDC /P <>BDC EMC BT EMC /P <>BDC 9 0 0 9 53.8582 357.8898 Tm EMC [(BOS-L)-31(A)-24.9(X)]TJ 9 0 0 9 185.6303 225.8898 Tm

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