BT ( )Tj 7 0 0 7 554.7883 606.7654 Tm /P <>BDC 9 0 0 9 408.2047 489.8898 Tm 0 Tc fuel and de-ice the fuel filter. EMC EMC ET EMC (34,650lbs)Tj 5.25 0 0 5.25 447.6106 11.5129 Tm ET ET -.01 Tc ET ( )Tj 7 0 0 7 444.737 100.7654 Tm 0 Tc /P <>BDC ( )Tj /P <>BDC 8 0 0 8 222.3212 771.9528 Tm 7 0 0 7 490.5101 738.9528 Tm (192)Tj 7 0 0 7 141.7322 331.9528 Tm (737-9)Tj BT BT /P <>BDC 9 0 0 9 53.8578 49.8898 Tm ET ET 0 Tc EMC 0 Tc /P <>BDC BT ( )Tj .151 .147 .15 rg ET ET BT EMC 6.5 0 0 6.5 224.5532 598.9529 Tm EMC /P <>BDC 7 0 0 7 508.4124 375.7654 Tm ET ET /P <>BDC /P <>BDC EMC EMC -.02 Tc ET EMC ET BT [(r)10(atio)]TJ All the flights are in a westerly)Tj ET /P <>BDC (158)Tj EMC EMC ET 6 0 0 6 153.9401 659.9528 Tm 6.5 0 0 6.5 397.5498 558.9529 Tm EMC (39,270)Tj /F7 1 Tf EMC 6.5 0 0 6.5 191.7926 702.9529 Tm /P <>BDC ET /P <>BDC EMC 9 0 0 9 215.433 247.8898 Tm )Tj 9 0 0 9 367.2172 269.8898 Tm BT BT (30,000lbs to 33,000lbs, a fan diameter of)Tj (72% of the NG fleet in service. 8 0 0 8 334.994 633.9528 Tm EMC (MLW of 174,606lb; and an OEW of)Tj ET 9 0 0 9 536.024 533.8898 Tm EMC EMC /P <>BDC ET 13 0 0 13 53.8578 181.8898 Tm 6 0 0 6 154.2695 743.9528 Tm -.02 Tc Thank you. BT 7 0 0 7 294.4014 89.7654 Tm ET /P <>BDC (number of available seat-miles \(ASM\))Tj ET BT /P <>BDC /P <>BDC /P <>BDC ( )Tj EMC ( )Tj EMC ( )Tj 9 0 0 9 565.1979 478.8898 Tm BT ( )Tj ET ( )Tj ( )Tj ET EMC /P <>BDC ET ET ( )Tj 7 0 0 7 539.8962 573.9528 Tm /F6 1 Tf BT (A321ceo)Tj EMC (310,080)Tj waiting with pax BT 56 0 0 56 419.9569 622.1944 Tm ET 0 Tc /P <>BDC /P <>BDC (179)Tj EMC BT .41 .161 .508 rg (CFM56-7B26)Tj ET 7 0 0 7 338.3085 309.9528 Tm (4,000)Tj 7 0 0 7 508.4124 738.7654 Tm /P <>BDC (capacity and potentially improved)Tj ( )Tj ( )Tj ET EMC ET /P <>BDC 9 0 0 9 392.5848 379.8898 Tm /P <>BDC ( )Tj BT ET BT ET /P <>BDC 13 0 0 13 118.3688 390.8898 Tm ET EMC ET ( )Tj 9 0 0 9 195.0251 434.8898 Tm (2,115)Tj 0 Tc /P <>BDC (194,700)Tj ( )Tj The seat configuration)Tj EMC 6 0 0 6 547.0496 673.9528 Tm ( )Tj BT ( )Tj BT BT EMC 0 Tc ( )Tj /F6 1 Tf EMC 9 0 0 9 229.6141 214.8898 Tm ET 7 0 0 7 54.7071 584.7654 Tm (table, page 19\))Tj ET ET ET BT 8 0 0 8 43.6039 675.9528 Tm (4,541)Tj ( )Tj EMC 1 w 1 g BT ET BT /P <>BDC ( )Tj /P <>BDC /P <>BDC /P <>BDC EMC 7 0 0 7 507.7893 595.7654 Tm EMC ET /P <>BDC BT ET /P <>BDC 7 0 0 7 99.8582 232.7654 Tm EMC EMC BT /P <>BDC (346,583)Tj /P <>BDC 9 0 0 9 394.0123 467.8898 Tm EMC EMC EMC ( )Tj ET /P <>BDC ET ET EMC 9 0 0 9 388.8047 390.8898 Tm /P <>BDC ( )Tj /P <>BDC BT (0.0171)Tj BT ET EMC ET ( )Tj 7 0 0 7 241.5317 606.9528 Tm -.02 Tc ET 7 0 0 7 326.2278 540.9528 Tm /P <>BDC BT EMC /P <>BDC EMC 7 0 0 7 258.2805 683.7654 Tm EMC EMC ET /P <>BDC BT (is 16/30/114, giving a maximum passenger)Tj BT BT EMC ( )Tj EMC BT BT ( )Tj /P <>BDC BT ( )Tj .151 .147 .15 rg /P <>BDC BT 6.5 0 0 6.5 296.3931 532.9529 Tm /P <>BDC ET ET BT ET EMC ET 0 Tc ET (earlier counterpart. 6 0 0 6 107.8523 659.9528 Tm BT -.02 Tc ( )Tj ET ET BT /P <>BDC ET )Tj ( )Tj /P <>BDC BT BT /P <>BDC BT ( )Tj 7 0 0 7 457.0984 485.7654 Tm EMC ET EMC EMC A weight reduction of 700 pounds (320 kg) on a 737-800 results in 0.5% reduction in fuel burn. ET -.02 Tc -.02 Tc /P <>BDC ( )Tj ET /P <>BDC ( )Tj ET /P <>BDC ET EMC BT ET ET BT /P <>BDC ET (0.0123)Tj BT /P <>BDC 9 0 0 9 232.4217 566.8898 Tm EMC /P <>BDC 0 Tc .12988 .27633 .58575 rg ( )Tj EMC ET ( )Tj BT on board for a late slot. /P <>BDC ( )Tj BT BT ET EMC EMC ET (The first table is the payload scenario)Tj BT BT 0 Tc ( )Tj (aircraft is not viable, so these sectors have)Tj /P <>BDC EMC ET /Artifact <>BDC 7 0 0 7 241.5317 221.9528 Tm ET ( )Tj (an OEW of 98,500lbs )Tj ( )Tj EMC EMC ET /P <>BDC 9 0 0 9 181.4073 335.8898 Tm .0161 Tc EMC BT EMC BT 9 0 0 9 79.8339 434.8898 Tm BT f ET -.02 Tc BT ET EMC 7 0 0 7 82.2047 672.9528 Tm (487)Tj EMC ET /F6 1 Tf BT 8 0 0 8 531.7294 771.9529 Tm ET 9 0 0 9 560.68 60.8898 Tm ( )Tj EMC 0 Tc ET BT ET 7 0 0 7 338.6433 232.7654 Tm ( )Tj ET BT ET /P <>BDC ET ( )Tj /P <>BDC BT EMC BT /P <>BDC BT [(CFM L)17.1(E)-8.1(AP-1B27)]TJ ( )Tj (7B26)Tj /P <>BDC /P <>BDC 9 0 0 9 361.9937 60.8898 Tm ( )Tj BT -.02 Tc /P <>BDC EMC ( )Tj /P <>BDC /P <>BDC ( )Tj ET BT BT ( )Tj 7 0 0 7 338.3085 144.9528 Tm /P <>BDC 6.5 0 0 6.5 296.3606 735.9529 Tm EMC EMC (977)Tj /P <>BDC [(7)-33(3)8(7-800)]TJ -.02 Tc BT BT ET /P <>BDC EMC (The fuel burn improvement on the)Tj (the A320neo. EMC 9 0 0 9 200.4718 38.8898 Tm [(P)11(ayload)]TJ /P <>BDC 0 Tc ( )Tj 0 Tc BT 7 0 0 7 247.7395 320.7654 Tm /P <>BDC 9 0 0 9 198.5183 445.8898 Tm 7 0 0 7 337.6855 529.9528 Tm /P <>BDC BT /P <>BDC ET ET 0 Tc (0.0133)Tj 0 Tc BT ( )Tj (with an ESAD of 2,576nm in payload)Tj [(R)30(elativ)12.9(e oper)10(ational cost )]TJ ET ET (0.0134)Tj BT ET Boeing 737Specs Tablefor Original and Classic. ET EMC ET BT BT /P <>BDC (5,000 aircraft delivered and making up)Tj /P <>BDC BT 7 0 0 7 196.5683 419.7654 Tm BT EMC ( )Tj EMC BT (\(neo\) families, and the 737NG family. (0.0121)Tj BT EMC BT /P <>BDC ET 0 Tc 6 0 0 6 309.2107 771.9528 Tm EMC /P <>BDC EMC /P <>BDC ( )Tj (Any seating configuration is defined by)Tj /P <>BDC ET (124,800)Tj EMC -.02 Tc EMC BT BT ( )Tj BT (408)Tj BT 7 0 0 7 204.0935 232.7654 Tm 7 0 0 7 337.4684 716.9528 Tm /GS2 gs 6.5 0 0 6.5 332.6961 735.9529 Tm BT ( )Tj 0 Tc 7 0 0 7 204.0935 606.7654 Tm EMC -.02 Tc 0 Tc /P <>BDC 0 Tc EMC EMC BT There are many variants of the 737. EMC ET (737-9)Tj EMC BT ( )Tj (page 23\))Tj (this page\))Tj )Tj 0 Tc /P <>BDC EMC BT (342,312)Tj /P <>BDC ( )Tj ( )Tj /P <>BDC ET (comparative performance. 0 Tc /P <>BDC 9 0 0 9 542.6167 159.8898 Tm 9 0 0 9 493.9938 357.8898 Tm ET BT /P <>BDC ( )Tj 7 0 0 7 77.36 11.5132 Tm EMC 6 0 0 6 371.7013 771.9528 Tm EMC ET BT 7 0 0 7 474.7064 331.9528 Tm ET 9 0 0 9 411.0097 390.8898 Tm ( )Tj 9 0 0 9 232.4408 775.8898 Tm BT ET /P <>BDC higher. 9 0 0 9 229.6141 478.8898 Tm ET BT EMC 9 0 0 9 568.024 148.8898 Tm ET 9 0 0 9 469.5781 577.8898 Tm /F4 1 Tf BT EMC 9 0 0 9 394.0157 346.8898 Tm BT /P <>BDC EMC 7 0 0 7 321.6356 320.9528 Tm /P <>BDC 7 0 0 7 297.632 727.9528 Tm /GS1 gs /Artifact <>BDC /P <>BDC ET 0 Tc BT 8 0 0 8 153.6923 591.9528 Tm BT -.01 Tc ET ET 9 0 0 9 215.433 170.8898 Tm EMC 0 Tc /P <>BDC ET /P <>BDC 9 0 0 9 547.3786 71.8898 Tm ET EMC .0081 Tc /P <>BDC /P <>BDC /P <>BDC EMC (737-800:)Tj 9 0 0 9 551.0015 291.8898 Tm 0 Tc EMC /P <>BDC ET BT /P <>BDC 6.5 0 0 6.5 480.4 637.9529 Tm 7 0 0 7 99.8582 386.7654 Tm ET 7 0 0 7 363.2711 573.9528 Tm EMC 7 0 0 7 387.0932 309.9528 Tm EMC BT BT 9 0 0 9 393.5047 181.8898 Tm (CFM56-7B26)Tj (3,200)Tj -.02 Tc (141,270)Tj ET W n ( )Tj ET BT EMC /P <>BDC ET /F4 1 Tf ( )Tj 7 0 0 7 554.7883 287.7654 Tm /P <>BDC /TT2 1 Tf /P <>BDC 9 0 0 9 408.1968 324.8898 Tm -.02 Tc ET ( )Tj ( )Tj 7 0 0 7 158.74 408.7654 Tm BT 7 0 0 7 474.3564 496.9528 Tm /P <>BDC (7,168)Tj ( )Tj BT /P <>BDC /P <>BDC (1,272)Tj EMC /P <>BDC BT ()Tj /P <>BDC EMC /P <>BDC EMC ( )Tj /GS1 gs ET ET EMC BT (1,913)Tj /P <>BDC BT BT BT EMC /P <>BDC 7 0 0 7 294.4014 617.7654 Tm ( )Tj BT -.02 Tc Note: for aircraft delivered after May 2004, centre tank EMC ( )Tj 7 0 0 7 537.7804 232.9528 Tm ( )Tj BT 0 Tc 9 0 0 9 212.0769 71.8898 Tm BT 0 Tc BT BT (114)Tj /P <>BDC /P <>BDC ( )Tj /P <>BDC /P <>BDC /P <>BDC 7 0 0 7 113.1366 716.9528 Tm (34,650)Tj /P <>BDC ET (158)Tj -.01 Tc /P <>BDC -.02 Tc (900ER\(W\) across the 14 routes with the)Tj BT .41 .161 .508 rg ET 9 0 0 9 354.463 49.8898 Tm /P <>BDC BT /P <>BDC ET 7 0 0 7 554.7883 485.7654 Tm BT 0 Tc -.02 Tc EMC ( )Tj 7 0 0 7 474.7064 441.9528 Tm ET BT (1,019)Tj 9 0 0 9 194.5468 71.8898 Tm ET /P <>BDC /GS2 gs (163)Tj (aircraft in terms of engine rating, operating)Tj ET ET 9 0 0 9 411.0097 181.8898 Tm /P <>BDC (1,729)Tj ( )Tj /GS2 gs 0 Tc BT (operation. 0 Tc 9 0 0 9 197.0674 258.8898 Tm ET /P <>BDC /P <>BDC ( )Tj BT 0 Tc EMC BT ( )Tj BT (39,270)Tj ET soaked fuel causing frost to form on the wings during the turnarounds - even in 0 Tc 9 0 0 9 563.3529 368.8898 Tm ET ( )Tj EMC ET 7 0 0 7 543.7693 11.5132 Tm (0.0124)Tj /P <>BDC (294)Tj (0.0112)Tj 9 0 0 9 53.8582 786.8898 Tm 0 Tc EMC EMC EMC q BT ( )Tj -.02 Tc ET ( )Tj /P <>BDC /P <>BDC Wing provisioning for the 737-800 adds approx. 7 0 0 7 54.5916 441.7654 Tm EMC ET BT ( )Tj 6.5 0 0 6.5 433.3069 545.9529 Tm ET EMC /P <>BDC EMC (passengers are carried on each of the four)Tj ( )Tj 0 Tc EMC EMC 8 0 0 8 314.3535 619.9528 Tm 9 0 0 9 361.2861 181.8898 Tm ( )Tj BT -.01 Tc BT (challenge for all airlines. -.01 Tc EMC EMC /P <>BDC (34,650lbs)Tj 0 Tc /P <>BDC 9 0 0 9 358.9372 346.8898 Tm ET 6 0 0 6 132.3631 659.9528 Tm ET EMC ET EMC /P <>BDC (0.0157)Tj /P <>BDC 7 0 0 7 439.7405 738.9528 Tm (standard passenger weight of 231lbs that)Tj ( )Tj /P <>BDC ( )Tj /P <>BDC EMC (- mins)Tj EMC /P <>BDC 7 0 0 7 130.1443 716.7654 Tm BT /P <>BDC 7 0 0 7 457.0984 287.7654 Tm Can you confirm if Im right or wrong? BT ( )Tj (13.1% to 18.9% improvements in block)Tj BT EMC 0 Tc ET BT BT ( )Tj -.02 Tc 6.5 0 0 6.5 346.1424 545.9529 Tm ( )Tj /P <>BDC (capacity has been configured as the same)Tj /P <>BDC ET 0 Tc )Tj 9 0 0 9 528.0345 511.8898 Tm ET /P <>BDC ET (977)Tj EMC /P <>BDC (136-145)Tj -2.5306 -6.3496 -3.213 -6.0519 -3.7399 -5.4283 c /P <>BDC 9 0 0 9 198.2937 126.8898 Tm ET (127 passengers on the longest sector,)Tj (159,251)Tj EMC 0 Tw /P <>BDC -.02 Tc /P <>BDC EMC EMC 13 0 0 13 411.0097 467.8898 Tm Boeing 737 Max, a new generation of this highly successful City Jet. EMC BT ( )Tj EMC EMC 7 0 0 7 148.0554 11.5132 Tm 8 0 0 8 91.2605 771.9529 Tm ET /P <>BDC 0 Tc EMC -.02 Tc BT ( )Tj (reducing their in-flight service offering, this)Tj ET /P <>BDC EMC /GS1 gs /P <>BDC EMC 0 Tc ( )Tj BT ET -.02 Tc ( )Tj ET BT At engine idle, the system tolerance can be 12%. EMC EMC -.02 Tc BT EMC BT /P <>BDC ET EMC ( )Tj EMC ET (4,615)Tj /P <>BDC 7 0 0 7 316.0679 232.7654 Tm ET BT /P <>BDC /P <>BDC 0 Tc BT (375)Tj 9 0 0 9 36.8504 192.8898 Tm EMC /P <>BDC BT 9 0 0 9 195.4853 126.8898 Tm /P <>BDC /P <>BDC EMC (1,619)Tj ( )Tj EMC (136)Tj 7 0 0 7 474.7064 133.9528 Tm ET ET (19)Tj ( )Tj 6 0 0 6 496.9595 715.9528 Tm /P <>BDC /P <>BDC EMC 0 841.89 609.449 -841.89 re BT /P <>BDC ET BT [(CFM L)17.1(E)-8.1(AP-1A32)]TJ ( )Tj (flight relate to fuel burn, overflight and)Tj /P <>BDC 9 0 0 9 215.4409 203.8898 Tm BT /P <>BDC (273,600)Tj ET -.01 Tc /P <>BDC EMC BT BT ( )Tj ET /P <>BDC /P <>BDC EMC (170)Tj ( )Tj ET EMC ET [(o)16.1(v)12.9(er 14 r)10(outes that hav)12.9(e ESADs betw)6.1(een 484nm and 2,7)-33(30nm. /P <>BDC (2,517)Tj ( )Tj BT ( )Tj BT /P <>BDC /P <>BDC EMC EMC EMC ET /P <>BDC /P <>BDC 9 0 0 9 182.0906 467.8898 Tm ET /P <>BDC EMC 8 0 0 8 542.3528 764.8898 Tm 7 0 0 7 326.2278 727.9528 Tm BT ( )Tj -.02 Tc BT EMC 0 Tc 8 0 0 8 474.6331 771.7654 Tm /P <>BDC ET ET 0 Tc How much fuel does a A350 burn? EMC 0 Tc q 1 0 0 1 36.85 797.54 cm 0 0 m /P <>BDC [(F)-21(LL/47)]TJ 0 Tc (20)Tj EMC (3,031)Tj BT 7 0 0 7 508.4124 694.7654 Tm BT -.02 Tc /P <>BDC /P <>BDC (configurations used for these aircraft types)Tj EMC EMC ( )Tj 7 0 0 7 365.035 639.9528 Tm ( )Tj ET BT 8 0 0 8 187.3427 577.9528 Tm EMC 7 0 0 7 130.1443 221.7654 Tm 7 0 0 7 490.7815 166.9528 Tm 0 Tc /P <>BDC EMC 7 0 0 7 445.7203 11.5129 Tm ET ET 0 Tc (2,517)Tj /P <>BDC /P <>BDC BT 9 0 0 9 394.0315 522.8898 Tm /P <>BDC BT BT BT /P <>BDC 0 Tc EMC 6 0 0 6 371.6897 659.9528 Tm BT /GS2 gs ET (l)Tj 7 0 0 7 99.8582 595.7654 Tm ET ET /P <>BDC /P <>BDC /P <>BDC 7 0 0 7 82.8504 100.9528 Tm BT 9 0 0 9 533.0564 181.8898 Tm 19.848 0 l S BT /P <>BDC /P <>BDC 7 0 0 7 258.2805 540.7654 Tm BT 0 Tc BT ET BT EMC ET 0 Tw /P <>BDC /P <>BDC ( )Tj /P <>BDC [(BOS-C)-8.1(V)18.1(G)]TJ ( )Tj EMC BT BT /P <>BDC BT 6 0 0 6 184.072 659.9528 Tm BT /P <>BDC /P <>BDC /F7 1 Tf ET ( )Tj 9 0 0 9 540.3981 588.8898 Tm ET ET 0 Tc ( )Tj -.015 Tc 7 0 0 7 141.7322 320.9528 Tm 10 0 0 10 312.5146 771.9528 Tm (sharklets. EMC BT 15 w Having a higher)Tj 8 0 0 8 319.1147 771.9528 Tm EMC BT ET BT ET 9 0 0 9 385.5399 115.8898 Tm (163)Tj ( )Tj BT ( C)Tj BT [(A3)24.9(21ceo)]TJ ET BT EMC /P <>BDC EMC BT /P <>BDC ET -.01 Tc (/S)Tj /P <>BDC 0 Tc 6 0 0 6 278.7028 659.9528 Tm 9 0 0 9 36.8504 38.8898 Tm EMC BT 8 0 0 8 124.845 577.9528 Tm EMC EMC Boeing 777X The New Triple Seven Family. ET 1 i ( )Tj support combustion. ( )Tj BT BT /P <>BDC .014984 824.882 572.583 17.008 re /P <>BDC 0 Tc 0 Tc /GS1 gs EMC 7 0 0 7 343.2355 606.7654 Tm /Artifact <>BDC 0 Tc ( )Tj /P <>BDC ET 0 Tc .023 .567 .626 RG 6.5 0 0 6.5 398.369 545.9529 Tm BT EMC 10 0 0 10 54.8804 814.1973 Tm /P <>BDC /P <>BDC 6.5 0 0 6.5 222.7786 676.9529 Tm [(SS)-9(U)8.1(E)]TJ 0 J 0 j 15 w 10 M [] 0 d /P <>BDC EMC ET ET BT EMC /P <>BDC .001 Tc ET ET EMC 7 0 0 7 379.3969 166.7654 Tm EMC 0 Tc BT ( )Tj .7 -.5345 .9114 -1.2305 y EMC Q ET 9 0 0 9 541.5243 720.8898 Tm /P <>BDC ET /P <>BDC ET ( )Tj /P <>BDC ET 0 Tc ET 7 0 0 7 316.0679 133.7654 Tm -.02 Tc ( )Tj ET ( )Tj ( )Tj 6 0 0 6 527.8009 743.9528 Tm /P <>BDC EMC BT to standardise the total tank capacitance and allows for the replacement 0 Tw 8 0 0 8 394.0237 71.8898 Tm (or any airborne or ground delays. /F1 1 Tf EMC ( )Tj /OC /MC188 BDC (the equivalent aircraft types, the lowest fuel)Tj EMC ET ( )Tj (2,189)Tj EMC BT (configuration as the 737-900ER\(W\), but)Tj EMC 9 0 0 9 368.9994 456.8898 Tm (same number of passengers is carried on)Tj EMC 9 0 0 9 53.8582 764.8898 Tm BT /P <>BDC [(v)21(ariant)]TJ ET BT /P <>BDC 7 0 0 7 518.4953 331.9528 Tm ( )Tj BT (146,550)Tj /P <>BDC EMC /P <>BDC The information is surely out there, but maybe the questions need to be a bit more specific. /P <>BDC /P <>BDC ET -.02 Tc 6 0 0 6 444.4713 715.9528 Tm (170)Tj /P <>BDC EMC 7 0 0 7 404.101 166.7654 Tm (rating on the CFM LEAP-1A32 to)Tj ET (2,730)Tj ET /P <>BDC ET ET 7 0 0 7 247.7395 419.7654 Tm The APU burns about 160Kgs/hr with electrics and an air-conditioning ET /P <>BDC 9 0 0 9 215.4409 489.8898 Tm BT 6 0 0 6 507.2798 715.9528 Tm BT ET ET /P <>BDC (163)Tj BT /P <>BDC BT 8 0 0 8 153.6923 703.9528 Tm 9 0 0 9 570.6951 291.8898 Tm 7 0 0 7 37.5838 551.9528 Tm /P <>BDC 9 0 0 9 214.4188 478.8898 Tm 0 Tc 7 0 0 7 316.0679 287.7654 Tm (0.0115)Tj BT -.02 Tc ET EMC BT 9 0 0 9 215.4409 368.8898 Tm (CFM56-7B26)Tj BT EMC ( )Tj 7 0 0 7 294.4014 320.7654 Tm /P <>BDC ET (maintenance costs. EMC EMC /P <>BDC (170)Tj ET /P <>BDC /P <>BDC /F1 1 Tf BT EMC EMC /P <>BDC /P <>BDC EMC 0 Tc -.02 Tc 0 Tc /P <>BDC ( )Tj ET EMC /P <>BDC (900ER\(W\), 737 MAX-8 \(737-8\), and the)Tj 9 0 0 9 565.2708 313.8898 Tm 0 Tc EMC ( )Tj ET ET -.6563 -2.3409 l [(CFM L)17.1(E)-8.1(AP-)]TJ BT EMC ET 7 0 0 7 490.5101 716.9528 Tm BT /P <>BDC /P <>BDC 544,000 lbs 246,754 Kg: Maximum Fuel Capacity: 48,445 US Gal. ET ET ET -.02 Tc 17 0 0 17 36.8606 742.1944 Tm BT (fixed speed of LRC can be applied to all)Tj EMC (Engine)Tj (39,270)Tj ( )Tj 9 0 0 9 351.8271 203.8898 Tm (0.0130)Tj 6.5 0 0 6.5 499.8375 545.9529 Tm /P <>BDC ET 9 0 0 9 36.8504 214.8898 Tm -.02 Tc 7 0 0 7 354.6933 199.7654 Tm BT ET EMC ( )Tj /P <>BDC 0 Tc 0 Tc ET 9 0 0 9 36.8504 181.8898 Tm -.01 Tc (5,338)Tj [(SS)-9.1(U)8(E)]TJ /P <>BDC EMC /P <>BDC BT ET ET 7 0 0 7 403.478 364.7654 Tm (operation the overflight and airport)Tj ET /P <>BDC /P <>BDC BT ET ET BT BT ET /GS2 gs ( )Tj BT ET 9 0 0 9 568.1771 115.8898 Tm 6 0 0 6 339.5547 771.9528 Tm ET 7 0 0 7 429.157 738.9528 Tm /P <>BDC 0 Tc BT EMC BT 9 0 0 9 370.9169 379.8898 Tm ET BT )Tj 1 1 1 rg ET 7 0 0 7 444.737 133.7654 Tm EMC ( )Tj 9 0 0 9 53.8338 82.8898 Tm ( )Tj (288)Tj (0.0149)Tj 9 0 0 9 53.8578 82.8898 Tm 9 0 0 9 550.3341 313.8898 Tm /P <>BDC EMC 9 0 0 9 542.1815 786.8898 Tm (11.0:1)Tj BT EMC ET EMC EMC /GS2 gs 7 0 0 7 37.0536 474.9528 Tm /P <>BDC (capacity. ET ET )Tj /P <>BDC 0 Tc ET BT EMC -.02 Tc /P <>BDC ET EMC ( )Tj 7 0 0 7 99.8582 617.7654 Tm /P <>BDC ET /P <>BDC EMC EMC (104)Tj ( )Tj ET EMC ET 0 Tc 6 0 0 6 254.6866 659.9528 Tm ( )Tj ( )Tj BT BT EMC /P <>BDC 0 Tc /P <>BDC BT EMC ET 7 0 0 7 82.2047 628.9528 Tm /P <>BDC BT 7 0 0 7 298.514 573.9528 Tm ET ET /F6 1 Tf BT 9 0 0 9 36.8504 60.8898 Tm BT ET ( C)Tj (evaluation routes are listed )Tj ( )Tj .014984 841.89 609.45 -841.89 re /P <>BDC ET EMC 9 0 0 9 508.3771 698.8898 Tm EMC BT EMC ET ET EMC EMC /F7 1 Tf It is)Tj -.02 Tc 0 Tc /P <>BDC (2,220)Tj ET EMC 0 Tc BT (1A32)Tj BT ( )Tj 0 Tc 9 0 0 9 232.4217 456.8898 Tm BT 7 0 0 7 439.1464 430.9528 Tm /P <>BDC ( )Tj ET /P <>BDC (Engine)Tj /F7 1 Tf Good luck. /P <>BDC (A321ceo)Tj ET -.02 Tc 9 0 0 9 190.4723 71.8898 Tm BT BT ( )Tj EMC EMC /P <>BDC 9 0 0 9 393.4057 379.8898 Tm BT ET 0 Tc EMC EMC (977)Tj /P <>BDC /P <>BDC BT BT BT EMC /P <>BDC 9 0 0 9 53.8582 698.8898 Tm 9 0 0 9 548.3644 533.8898 Tm ET ET /P <>BDC ET 0 Tc ET EMC 9 0 0 9 215.4409 434.8898 Tm ( )Tj ( )Tj /P <>BDC ( )Tj EMC -.02 Tc ET 7 0 0 7 387.0159 584.9528 Tm /P <>BDC )Tj BT 5.25 0 0 5.25 55.7484 11.5132 Tm (150)Tj ET BT EMC 0 Tc ET (CFM56-7B27B3)Tj BT /P <>BDC ET 9 0 0 9 229.6064 126.8898 Tm /P <>BDC 0 Tc BT 6.5 0 0 6.5 430.0114 565.9529 Tm BT (the aircraft operator, but in this evaluation)Tj BT BT /P <>BDC BT BT BT 7 0 0 7 43.6039 540.9528 Tm /P <>BDC BT 6.5 0 0 6.5 244.2974 545.9529 Tm EMC ET The 800 was developed to replace the 727 on short routes. /P <>BDC BT /P <>BDC 7 0 0 7 54.7071 221.7654 Tm ET ET EMC ET /P <>BDC BT BT 0 Tc EMC EMC BT -.02 Tc BT ( )Tj BT /P <>BDC EMC 0 Tc /P <>BDC 7 0 0 7 537.7804 100.9528 Tm BT /P <>BDC 168 0 obj EMC ( )Tj We welcome your comment below, is there more we could be showing or are there topics you would like to see? 9 0 0 9 523.7694 214.8898 Tm 9 0 0 9 229.6141 434.8898 Tm EMC -.02 Tc ( )Tj ET ET 7 0 0 7 439.7405 485.9528 Tm /P <>BDC BT ( )Tj EMC /P <>BDC ET 8 0 0 8 153.6923 633.9528 Tm /P <>BDC /P <>BDC (273,750)Tj 9 0 0 9 184.215 478.8898 Tm ( )Tj BT EMC 7 0 0 7 473.8245 298.9528 Tm EMC /F1 1 Tf -.01 Tc 9 0 0 9 232.4217 203.8898 Tm ET BT BT BT BT /P <>BDC /P <>BDC BT ET 7 0 0 7 539.8962 628.9528 Tm BT [(7)-33(3)8.1(7-900ER & 7)-33(3)8.1(7-9 )]TJ /P <>BDC 7 0 0 7 537.7804 298.9528 Tm EMC ET 9 0 0 9 394.0123 577.8898 Tm EMC 7 0 0 7 444.737 243.7654 Tm (HGW2 option with an MTOW of)Tj 9 0 0 9 204.4018 665.8898 Tm BT 7 0 0 7 107.1165 573.9528 Tm ( )Tj 9 0 0 9 411.0234 753.8898 Tm EMC EMC EMC /P <>BDC /P <>BDC 7 0 0 7 316.0679 364.7654 Tm EMC <>/ExtGState<>/Properties<>>> BT ET BT BT ET ( )Tj 0 Tc EMC BT /P <>BDC ET /P <>BDC BT /P <>BDC [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ EMC ET /P <>BDC /P <>BDC (variants increases from 5.1:1 on the 737-)Tj /F6 1 Tf -.005 Tc ( )Tj 7 0 0 7 491.4046 100.9528 Tm EMC (. /P <>BDC ET BT EMC 0 Tc /P <>BDC (The A321neo is offered to airlines with)Tj BT /P <>BDC /P <>BDC BT (4,552)Tj -.02 Tc BT BT 0 Tc /P <>BDC EMC BT (better for the A321neo due to its increased)Tj BT EMC EMC -.02 Tc BT ( )Tj 9 0 0 9 53.8578 291.8898 Tm -.02 Tc ET (0.0154)Tj /P <>BDC BT (2,800 -)Tj BT (11,593)Tj 0 Tc BT ET 9 0 0 9 36.8504 236.8898 Tm /P <>BDC BT BT ET ( )Tj BT /P <>BDC /P <>BDC /P <>BDC ET BT EMC 9 0 0 9 545.0725 434.8898 Tm 9 0 0 9 103.7478 390.8898 Tm /P <>BDC -.02 Tc BT 5.25 0 0 5.25 549.1047 11.5132 Tm BT (150)Tj ET /P <>BDC 7 0 0 7 337.7614 100.7654 Tm 0 Tc 6 0 0 6 109.2916 743.9528 Tm 0 Tc /P <>BDC ET BT /P <>BDC EMC 5.25 0 0 5.25 525.4061 11.5132 Tm ( )Tj EMC /P <>BDC 10 0 0 10 54.1596 794.2914 Tm 9 0 0 9 232.4217 577.8898 Tm BT EMC 6 0 0 6 540.5396 757.9528 Tm ( )Tj BT EMC ET ET BT EMC 9 0 0 9 204.9907 467.8898 Tm BT ET Modern Airliners and Civil Aviation Aircraft. 9 0 0 9 246.595 49.8898 Tm EMC ( )Tj 0 Tc /P <>BDC -.02 Tc -.02 Tc We have rechecked with Boeing and the figure should now be up to date and correct. EMC ET BT 0 Tc ET /P <>BDC -1.2026 -5.3154 -.8984 -5.2108 -.5848 -4.9925 c BT 8 0 0 8 394.0237 49.8898 Tm 6.5 0 0 6.5 54.877 572.9529 Tm /P <>BDC EMC EMC /P <>BDC -.01 Tc /P <>BDC /P <>BDC ET EMC ET ET /P <>BDC ET BT ( )Tj BT BT (CFM56-7B27B3)Tj 8 0 0 8 337.3163 771.9528 Tm 28.5749 0 TD /P <>BDC /P <>BDC 9 0 0 9 332.7796 225.8898 Tm /P <>BDC ET EMC 0 Tc /P <>BDC /P <>BDC BT ET EMC h EMC W n BT EMC 7 0 0 7 241.2727 166.9528 Tm /P <>BDC /P <>BDC ET (Similar to the A320 family, the 737 MAX)Tj Hi, How can I learn aerospace materails about a and b basis allowables for Boeing-737 ? ET EMC /P <>BDC 7 0 0 7 554.7883 507.7654 Tm /P <>BDC 7 0 0 7 279.1575 210.9528 Tm ET BT EMC (152)Tj /P <>BDC This article will)Tj (10)Tj [(UG)-17.1(U)-8(S)8.1(T)]TJ EMC 7 0 0 7 507.7893 265.7654 Tm BT (150)Tj -.02 Tc 7 0 0 7 247.7395 243.7654 Tm BT /OC /MC19 BDC /P <>BDC EMC BT The 800 shares a lineage with the 300, 400, and 500. /P <>BDC ET 7 0 0 7 258.2805 617.7654 Tm /P <>BDC 5.25 0 0 5.25 525.4061 11.5132 Tm EMC BT /P <>BDC ET EMC EMC /P <>BDC -.02 Tc /P <>BDC BT /P <>BDC 6.5 0 0 6.5 448.257 598.9529 Tm ()Tj EMC ET BT 10 0 0 10 225.1837 771.9528 Tm 7 0 0 7 535.5029 496.7654 Tm 7 0 0 7 315.1859 100.7654 Tm 9 0 0 9 411.0234 698.8898 Tm 9 0 0 9 232.4408 764.8898 Tm (150)Tj )Tj (O)Tj from cockpit door to the kitchen alley . ( )Tj (In the 85% passenger payload)Tj BT EMC /P <>BDC ( )Tj /P <>BDC (150)Tj EMC /P <>BDC /OC /MC27 BDC BT BT 9 0 0 9 229.6064 269.8898 Tm (136)Tj /Figure <>BDC ET 0 Tc ET ET 0 Tc 0 Tc EMC /P <>BDC EMC /P <>BDC /P <>BDC BT ET /P <>BDC EMC EMC /P <>BDC /P <>BDC The Boeing 737 is a narrow-body aircraft produced by Boeing at its Renton Factory in Washington.Developed to supplement the Boeing 727 on short and thin routes, the twinjet retains the 707 fuselage width and six abreast seating with two underwing turbofans.Envisioned in 1964, the initial 737-100 made its first flight in April 1967 and entered service in February 1968 with Lufthansa. EMC EMC ET ET EMC 7 0 0 7 534.621 100.7654 Tm BT The Boeing 737-800 has a maximum fuel capacity of 6,875 gallons or 26,020 liters. /P <>BDC /P <>BDC /P <>BDC