737 800 fuel capacity pounds737 800 fuel capacity pounds

7 0 0 7 241.5317 408.9528 Tm ET ET 8 0 0 8 394.0157 797.8898 Tm 13 0 0 13 512.6883 71.8898 Tm -.02 Tc 9 0 0 9 540.3891 544.8898 Tm EMC -.02 Tc ET ( )Tj -2.9413 -1.4846 -3.0524 -2.0356 -3.053 -2.8052 c ET BT EMC /P <>BDC ET 7 0 0 7 109.3921 430.9528 Tm ET BT EMC EMC ET ET 7 0 0 7 518.4953 397.9528 Tm EMC EMC 0 Tc BT BT 6 0 0 6 153.0397 715.9528 Tm BT BT BT /P <>BDC 0 Tc ET /P <>BDC /P <>BDC 7 0 0 7 82.8504 320.9528 Tm /P <>BDC (170)Tj EMC -.01 Tc 7 0 0 7 403.478 606.7654 Tm EMC /P <>BDC /GS2 gs /P <>BDC 9 0 0 9 394.0237 192.8898 Tm EMC BT ( )Tj /P <>BDC [(OM)8(M)-13(E)-25(R)7(C)8(E)]TJ BT 7 0 0 7 241.2727 177.9528 Tm ET /P <>BDC 9 0 0 9 177.7731 181.8898 Tm /F4 1 Tf EMC EMC Q EMC 503.534 80.74 l EMC The system tolerance is then +/- 200 KG at any fuel level within the tank. /P <>BDC (The 737-8 has a block fuel burn)Tj BT EMC BT 0 Tc BT EMC ET /P <>BDC ET ET BT 7 0 0 7 141.7322 672.9528 Tm For more detailed information on the Boeing 737 Specs, you can click on this Boeing 737 PDF. EMC /P <>BDC EMC ( )Tj ET ET BT ET -.02 Tc ( )Tj ET 9 0 0 9 551.8838 324.8898 Tm /P <>BDC BT 0 Tc EMC BT EMC EMC BT -.02 Tc /OC /MC5086 BDC EMC ET 0 Tc BT (136)Tj /P <>BDC BT BT /P <>BDC /P <>BDC 7 0 0 7 536.3849 166.7654 Tm -.01 Tc /P <>BDC /P <>BDC ( )Tj /F6 1 Tf /P <>BDC ET EMC BT (aircraft types; and with no additional cargo)Tj EMC EMC ET -.02 Tc ET EMC EMC BT BT ET 9 0 0 9 394.0157 236.8898 Tm BT (1,705)Tj /P <>BDC 7 0 0 7 354.6933 265.7654 Tm ET ET 9 0 0 9 215.4409 335.8898 Tm ET EMC ( )Tj 6 0 0 6 352.5857 659.9528 Tm BT EMC ( )Tj 7 0 0 7 430.039 573.9528 Tm (377,550)Tj BT ( )Tj BT 0 Tc ET /P <>BDC 0 Tc ET 0 Tc (The 737-9 uses the same CFM LEAP-)Tj 9 0 0 9 232.438 115.8898 Tm EMC 7 0 0 7 88.196 11.5129 Tm q ET 8 0 0 8 38.4438 619.9528 Tm /P <>BDC /P <>BDC BT 7 0 0 7 429.157 518.9528 Tm BT EMC /P <>BDC BT EMC EMC BT (give the newer type a further advantage. /P <>BDC 7 0 0 7 537.7804 232.9528 Tm (1,272)Tj /P <>BDC BT BT 9 0 0 9 392.5128 236.8898 Tm (128-137)Tj BT /P <>BDC (5,000 aircraft delivered and making up)Tj /F2 1 Tf BT BT 7 0 0 7 507.7893 166.7654 Tm 9 0 0 9 547.6725 346.8898 Tm ET 7 0 0 7 535.5029 177.7654 Tm BT EMC EMC ET ET EMC /P <>BDC (34,650)Tj /P <>BDC /P <>BDC ET EMC BT ET BT ET /P <>BDC /P <>BDC 0 841.89 609.449 -841.89 re -.3479 2.7359 l 9 0 0 9 394.0123 544.8898 Tm /P <>BDC BT BT ET ( )Tj EMC ET ET BT ET EMC ET ET 9 0 0 9 372.2987 181.8898 Tm ET /P <>BDC 7 0 0 7 114.6416 496.9528 Tm (lower fuel burn compared to the 737-)Tj (151)Tj Like the)Tj 9 0 0 9 375.0299 434.8898 Tm 7 0 0 7 182.5706 144.9528 Tm BT -.6563 -2.3409 l 13 0 0 13 358.8579 60.8898 Tm /P <>BDC /P <>BDC BT (performance )Tj 7 0 0 7 82.2047 573.9528 Tm ET ET 7 0 0 7 204.0935 584.7654 Tm -.01 Tc -.02 Tc As stated, this makes a fair)Tj BT BT ( )Tj ( )Tj ( )Tj EMC 7 0 0 7 279.1575 485.9528 Tm /P <>BDC ET /P <>BDC 6.5 0 0 6.5 485.8925 735.9529 Tm /P <>BDC -.02 Tc EMC ET ( )Tj /P <>BDC These sectors)Tj ( )Tj 7 0 0 7 379.3969 243.7654 Tm EMC EMC EMC ET EMC -.02 Tc 9 0 0 9 155.8226 368.8898 Tm -.02 Tc 8 0 0 8 43.6039 633.9528 Tm /P <>BDC /P <>BDC Other)Tj 137 )Tj BT ET <> [(UG)-17.1(U)-8(S)8.1(T)]TJ BT EMC /P <>BDC 0 Tc 9 0 0 9 389.8867 269.8898 Tm ET /P <>BDC ET /P <>BDC /P <>BDC /P <>BDC EMC Both fuel pump low pressure lights in any tank are required EMC EMC (136)Tj 0 Tc ET /P <>BDC 9 0 0 9 394.0315 280.8898 Tm ET EMC BT EMC BT ET ET ( )Tj -.02 Tc BT BT EMC (types will only be made where unrestricted)Tj 6.5 0 0 6.5 191.7926 702.9529 Tm BT EMC /P <>BDC 9 0 0 9 545.546 115.8898 Tm BT /P <>BDC BT /P <>BDC /GS1 gs /P <>BDC EMC (737-900ER\(W\) has an MTOW of)Tj /P <>BDC BT 6.5 0 0 6.5 540.4371 611.9529 Tm EMC EMC ( )Tj 518.74 0 l EMC EMC ET BT BT ET ( )Tj (network. ET BT ET BT /P <>BDC 0 Tc EMC ( )Tj EMC ( )Tj 7 0 0 7 43.6039 441.9528 Tm 0 Tc 9 0 0 9 370.8228 302.8898 Tm 7 0 0 7 554.7883 716.7654 Tm 6.5 0 0 6.5 327.0283 598.9529 Tm ET 6.5 0 0 6.5 534.5352 585.9529 Tm /P <>BDC 7 0 0 7 241.5317 386.9528 Tm 7 0 0 7 43.6039 342.9528 Tm /P <>BDC (207,336)Tj EMC 7 0 0 7 99.8582 661.7654 Tm BT /P <>BDC /P <>BDC ET 6.5 0 0 6.5 477.8064 702.9529 Tm /P <>BDC ( )Tj 7 0 0 7 82.2047 694.9528 Tm (capacity, whereas the A321neo, with the)Tj /GS1 gs Because of EMC 6 0 0 6 327.5828 701.9528 Tm EMC 0 Tc EMC BT ( )Tj /P <>BDC 0 Tc EMC BT BT EMC BT ET EMC 0 Tc /P <>BDC ET ( )Tj 0 841.89 609.449 -841.89 re /P <>BDC BT 9 0 0 9 53.8338 82.8898 Tm Cheers Peter. 7 0 0 7 258.2805 628.7654 Tm /P <>BDC BT EMC BT /P <>BDC Hi Jeffrey, EMC (on the longest sector. BT ET /P <>BDC BT BT /P <>BDC EMC /P <>BDC /P <>BDC BT EMC BT /P <>BDC -.02 Tc 7 0 0 7 158.74 584.7654 Tm 0 Tc /P <>BDC EMC 9 0 0 9 274.8953 313.8898 Tm 7 0 0 7 535.5029 287.7654 Tm /P <>BDC /P <>BDC 9 0 0 9 411.0181 456.8898 Tm 8 0 0 8 72.3645 771.9528 Tm EMC BT ( )Tj EMC /P <>BDC BT BT ET EMC ( )Tj /P <>BDC ET )Tj /P <>BDC EMC [(7)-33(3)8.1(7-800 & 7)-33(3)8.1(7-8 )]TJ BT -.02 Tc (831)Tj EMC BT 6.5 0 0 6.5 64.6596 650.9529 Tm BT ( )Tj BT 9 0 0 9 36.8504 511.8898 Tm 7 0 0 7 490.5101 540.9528 Tm EMC /F6 1 Tf wiring in tanks, proximity to hot air-conditioning or pneumatic systems, etc. BT 6 0 0 6 521.632 729.9528 Tm EMC /P <>BDC ( )Tj 7 0 0 7 355.3163 177.7654 Tm BT -.02 Tc BT ( )Tj ( )Tj 6.5 0 0 6.5 296.2827 637.9529 Tm ET EMC The charges are split by weight)Tj BT ET BT ET EMC -.02 Tc This is because it)Tj ET ( )Tj ET 6.5 0 0 6.5 296.4841 676.9529 Tm 7 0 0 7 297.632 694.9528 Tm 9 0 0 9 372.6154 236.8898 Tm /P <>BDC 8 0 0 8 187.3427 619.9528 Tm 7 0 0 7 337.9444 639.9528 Tm 7 0 0 7 508.4124 518.7654 Tm EMC 7 0 0 7 429.157 496.9528 Tm ET ( )Tj 9 0 0 9 53.8582 324.8898 Tm BT EMC 1 i BT BT ( )Tj 53.858 511.715 518.74 293.325 re 9 0 0 9 195.5727 104.8898 Tm EMC 7 0 0 7 230.7317 683.9528 Tm ET BT Q EMC ET ( )Tj EMC EMC BT BT /P <>BDC ( )Tj /P <>BDC ( )Tj 6.5 0 0 6.5 379.0655 650.9529 Tm 6 0 0 6 561.1918 701.9528 Tm 9 0 0 9 394.0123 368.8898 Tm /Artifact <>BDC /P <>BDC (152)Tj (scenario 2, where all types carry an 85%)Tj /P <>BDC /P <>BDC BT BT ET EMC /P <>BDC ET ET EMC ( )Tj 6 0 0 6 286.5632 771.9528 Tm ET -.02 Tc BT BT ET )Tj 6.5 0 0 6.5 64.6596 722.9529 Tm The payload reduction is)Tj (ASM. BT (737-9)Tj ET 7 0 0 7 445.619 364.7654 Tm BT EMC (150)Tj 7 0 0 7 387.0932 232.9528 Tm 6.5 0 0 6.5 279.814 585.9529 Tm EMC 7 0 0 7 241.5317 397.9528 Tm 0 Tc ET ET ET 7 0 0 7 430.039 628.9528 Tm (34,650)Tj /P <>BDC /P <>BDC 7 0 0 7 543.7693 11.5132 Tm /P <>BDC ( )Tj Report (DOT/FAA/AR-01/63) (4.8Mb), MAX: 3,869 + 12,990 + 3,869 = 20,729kg, 1/200: BT /P <>BDC ( )Tj BT EMC ( )Tj ET ET ( )Tj EMC /P <>BDC /P <>BDC /P <>BDC /P <>BDC BT 7 0 0 7 247.7395 419.7654 Tm /P <>BDC BT ( )Tj EMC BT 7 0 0 7 88.196 11.5129 Tm ( )Tj Hi, How can I learn aerospace materails about a and b basis allowables for Boeing-737 ? (The in-service fleet of the newer)Tj 7 0 0 7 118.104 210.7654 Tm /P <>BDC (A321ceo)Tj (the fuel burn and operating performance of)Tj (ASM. /P <>BDC /GS1 gs ET BT ( )Tj EMC ( )Tj 6.5 0 0 6.5 528.5291 676.9529 Tm (hour, increases, the average fuel burn per)Tj 7 0 0 7 258.2805 342.7654 Tm BT 0 Tc /P <>BDC -.02 Tc 7 0 0 7 54.7071 276.7654 Tm -.02 Tc BT (a cost index, which is a more cost-efficient)Tj /P <>BDC ET /P <>BDC ET 9 0 0 9 394.0237 280.8898 Tm (The 737-900ER\(W\) is payload-limited)Tj 0 Tc EMC EMC ( )Tj 7 0 0 7 537.7804 320.9528 Tm -.2034 -.7911 -.1202 -.4766 0 0 c BT .014984 841.89 609.45 -841.89 re 9 0 0 9 379.3098 269.8898 Tm 7 0 0 7 141.7322 584.9528 Tm 9 0 0 9 36.8504 368.8898 Tm (fuselage length. ( )Tj 0 Tc ET EMC -.02 Tc ( A)Tj EMC EMC EMC BT /P <>BDC (163)Tj BT (. /P <>BDC In this case I believe TUI fly is the main customer. /P <>BDC (170)Tj 7 0 0 7 427.7291 265.9528 Tm EMC 9 0 0 9 172.0312 357.8898 Tm EMC EMC /F4 1 Tf BT /P <>BDC ( )Tj -.02 Tc EMC BT /P <>BDC 7 0 0 7 379.3969 320.7654 Tm ( )Tj ( )Tj (2,517)Tj /P <>BDC BT ET BT 7 0 0 7 535.5029 78.7654 Tm BT /P <>BDC It therefore offers no)Tj 9 0 0 9 408.1968 159.8898 Tm /P <>BDC 6.5 0 0 6.5 191.8316 637.9529 Tm /P <>BDC 0 Tc 8 0 0 8 314.3535 717.9528 Tm 0 Tc ( )Tj -.02 Tc 0 Tc EMC 19.851 0 l EMC BT W n /P <>BDC 7 0 0 7 490.5101 694.9528 Tm ET /P <>BDC /P <>BDC EMC ET Federal Aviation Administration and the Boeing Company to evaluate the 9 0 0 9 411.0181 170.8898 Tm 0 Tc ET EMC EMC (3,400 )Tj /P <>BDC /P <>BDC -.02 Tc ET ( )Tj ET ET as shown at the top of the page. BT BT .023 .567 .626 rg /P <>BDC ET (0.0129)Tj BT /P <>BDC In the cargo configuration, The 737-700C can carry up to 18,780 kg (41,420 pounds) of cargo on eight . The cabin layout used for)Tj /P <>BDC EMC waiting with pax ET BT 9 0 0 9 455.0733 60.8898 Tm ET EMC BT EMC BT BT ( )Tj BT ( )Tj ( )Tj ET EMC /Artifact <>BDC 7 0 0 7 457.0984 298.7654 Tm BT 9 0 0 9 394.0237 335.8898 Tm BT BT 9 0 0 9 566.4993 698.8898 Tm ET /P <>BDC 6.5 0 0 6.5 285.7159 611.9529 Tm 6 0 0 6 153.6996 673.9528 Tm ( )Tj /P <>BDC 7 0 0 7 37.0536 617.9528 Tm BT ( )Tj /P <>BDC /P <>BDC EMC BT EMC BT 6.5 0 0 6.5 64.6596 742.9529 Tm ET BT ET -.02 Tc (1,025)Tj .014984 824.882 572.583 17.008 re /P <>BDC -.02 Tc EMC BT EMC (4,000)Tj ET ET BT EMC -.02 Tc ET /P <>BDC ET ET 7 0 0 7 321.6356 210.9528 Tm BT ( )Tj /P <>BDC BT EMC EMC 0 Tc /P <>BDC BT 7 0 0 7 179.5605 122.9528 Tm /P <>BDC ( )Tj EMC upper surface of the wings where this frost is allowable for despatch under the q /P <>BDC BT /F1 1 Tf 6.5 0 0 6.5 227.9655 565.9529 Tm BT /P <>BDC -.02 Tc BT EMC ( )Tj (the A321ceo, A321neo, 737-900ER\(W\))Tj EMC /F4 1 Tf EMC BT EMC ( )Tj 0 841.89 609.449 -841.89 re /P <>BDC 8 0 0 8 542.3528 764.8898 Tm ET 7 0 0 7 387.0159 496.9528 Tm -.02 Tc ET /P <>BDC 6.5 0 0 6.5 398.2453 742.9529 Tm (\(see table, page 19\))Tj BT BT ET (0.0133)Tj /P <>BDC 6 0 0 6 409.8614 771.9528 Tm -.01 Tc -.02 Tc /P <>BDC 9 0 0 9 229.6064 49.8898 Tm [(CFM L)17.1(E)-8.1(AP-)]TJ EMC ET 9 0 0 9 369.2608 38.8898 Tm BT 178,000 Litres: 52,410 US Gal. /P <>BDC ET 515.814 89.864 l BT /P <>BDC 1 i ET BT 7 0 0 7 297.632 716.9528 Tm 7 0 0 7 204.0935 375.7654 Tm ET 9 0 0 9 161.2491 126.8898 Tm ( )Tj EMC 9 0 0 9 215.4313 225.8898 Tm /P <>BDC -.02 Tc EMC 0 Tc BT /P <>BDC EMC (CFM56-7B26)Tj 9 0 0 9 229.6141 390.8898 Tm EMC 304.725 420.96 m BT 361 0 obj BT EMC BT EMC EMC ET (comparison to allow a better review of the)Tj ET ET ET EMC EMC ET EMC EMC ET 7 0 0 7 230.7317 111.9528 Tm EMC /P <>BDC -.02 Tc (150-158)Tj 0 Tc EMC ET ET 7 0 0 7 473.8245 67.9528 Tm EMC Boeing 787 Dreamliner Orders and Deliveries. EMC ET 0 Tc BT BT /P <>BDC 7 0 0 7 54.7071 287.7654 Tm ET (cents, with a network average)Tj 7 0 0 7 277.3936 67.9528 Tm (seat capacity over the NG series. (-58)Tj 7 0 0 7 99.8582 518.7654 Tm [(trip fuel burn compar)10(ed to the 737-800. EMC 9 0 0 9 394.0237 390.8898 Tm BT Thank you. EMC 9 0 0 9 170.626 357.8898 Tm /P <>BDC 8 0 0 8 225.1837 745.9528 Tm 7 0 0 7 241.2727 364.9528 Tm EMC /P <>BDC ( )Tj ET ( )Tj BT BT ET (ratio of 5.1:1. EMC 9 0 0 9 36.8504 93.8898 Tm EMC (-58)Tj ET ET /P <>BDC EMC EMC EMC ( )Tj EMC 9 0 0 9 215.4409 203.8898 Tm 0 Tc ET BT ET 6 0 0 6 357.8844 701.9528 Tm (136)Tj /GS2 gs ( )Tj ET EMC /GS2 gs .559 .331 .619 rg ( )Tj 7 0 0 7 125.6292 584.7654 Tm BT 7 0 0 7 354.6933 397.7654 Tm .0081 Tc BT 6.5 0 0 6.5 54.877 572.9529 Tm EMC ( )Tj ET ET EMC BT BT 7 0 0 7 54.7071 419.7654 Tm Hi Peter, BT -.02 Tc 9 0 0 9 534.7124 401.8898 Tm EMC EMC EMC (economy seating by 12 seats when)Tj ET ( )Tj /P <>BDC /P <>BDC Engine size BT BT 5 0 0 5 484.5872 11.5129 Tm 9 0 0 9 53.8338 214.8898 Tm EMC EMC /P <>BDC 6 0 0 6 278.7028 659.9528 Tm EMC 9 0 0 9 544.5291 665.8898 Tm BT EMC BT BT ( )Tj /P <>BDC /P <>BDC 0 Tc ET ET EMC The 800 was developed to replace the 727 on short routes. /P <>BDC EMC /P <>BDC ET EMC -9.719 805.04 386.723 -270.624 re BT ET /P <>BDC EMC EMC EMC /F4 1 Tf /P <>BDC BT (that in scenario 1 both aircraft carry 170)Tj BT EMC 8 0 0 8 314.3535 675.9528 Tm BT /P <>BDC EMC (. (737-8)Tj EFVU(eufv7GWgw8HXhx)9IYiy*:JZjz m !1AQa"q2#BRbr3$4CS%cs5DT EMC EMC /P <>BDC BT BT /P <>BDC /P <>BDC EMC ( )Tj ET BT (35,112)Tj EMC /P <>BDC 0 Tc EMC EMC 7 0 0 7 298.1781 78.9528 Tm (ASM. 7 0 0 7 230.7317 221.9528 Tm 0 Tc EMC /P <>BDC ET BT 6.5 0 0 6.5 521.8278 742.9529 Tm 9 0 0 9 394.0157 577.8898 Tm EMC 7 0 0 7 230.7317 518.9528 Tm ET ( )Tj (This comparison is made using the)Tj /P <>BDC ET ET BT EMC /P <>BDC ET .014984 841.89 609.45 -841.89 re BT /P <>BDC ( )Tj BT ET BT BT ET EMC EMC 0 Tc ( )Tj EMC ET BT /P <>BDC EMC /P <>BDC /P <>BDC (37,653)Tj EMC /P <>BDC 0 Tc /P <>BDC EMC /P <>BDC EMC ( )Tj 9 0 0 9 546.1516 445.8898 Tm EMC 7 0 0 7 204.0935 232.7654 Tm 199,158 Litres: . EMC 7 0 0 7 439.2087 287.9528 Tm (The wind speed was based on an 85%)Tj (A321neo)Tj 7 0 0 7 230.7317 694.9528 Tm If anyone does, please feel free to share with us all. BT 7 0 0 7 108.6215 166.9528 Tm ET /P <>BDC EMC ( )Tj 0 Tc ET (I)Tj /P <>BDC EMC ET /P <>BDC /P <>BDC <>/ExtGState<>/Properties<>>> ET BT ET (LEAP-1B. 19.841 0 l ET ET BT (the relative operational cost difference)Tj /P <>BDC ( )Tj ( )Tj EMC ( )Tj ET ( )Tj 0 Tc EMC (CFM56-7B26)Tj -.02 Tc BT EMC 0 Tc EMC W n EMC ET 0 Tc /P <>BDC ET ET (91,300)Tj EMC ET ET BT ( )Tj ET EMC /P <>BDC /P <>BDC BT 7 0 0 7 279.1575 89.9528 Tm BT 6.5 0 0 6.5 54.877 598.9529 Tm 7 0 0 7 380.2788 617.7654 Tm 9 0 0 9 204.06 742.8898 Tm 9 0 0 9 53.8338 335.8898 Tm EMC ET /P <>BDC ET ET 7 0 0 7 490.5101 705.9528 Tm 9 0 0 9 343.8357 423.8898 Tm EMC EMC 9 0 0 9 392.5848 346.8898 Tm .1202 .4955 .3052 1.277 y /P <>BDC ( )Tj EMC 7 0 0 7 315.1859 144.7654 Tm [(CFM L)17.1(E)-8.1(AP-1A32)]TJ /F6 1 Tf (0.0129)Tj 7 0 0 7 182.5706 375.9528 Tm EMC ET ( )Tj 0 Tc [(CFM L)17.1(E)-8.1(AP-1A26)]TJ ( )Tj EMC (0.0108)Tj EMC 7 0 0 7 258.2805 496.7654 Tm ET )Tj air speed, altitude, and similar flight parameters were made available from (A320neo)Tj BT Q EMC /P <>BDC -.02 Tc 6.5 0 0 6.5 94.8855 689.9529 Tm EMC (1,272)Tj ET /Artifact <>BDC EMC -.02 Tc BT BT EMC ET /P <>BDC BT 7 0 0 7 141.7322 188.9528 Tm 9 0 0 9 571.3269 38.8898 Tm ET /P <>BDC BT ET ( )Tj ( )Tj ET ( )Tj (A321ceo is passenger payload-restricted on)Tj BT /P <>BDC (50,800)Tj ( )Tj 9 0 0 9 522.7491 280.8898 Tm /GS1 gs EMC /P <>BDC BT 9 0 0 9 570.8806 720.8898 Tm Q EMC BT EMC BT 9 0 0 9 369.406 104.8898 Tm ET BT EMC Later on Boeing contracted out such production to other suppliers. (greater on the shorter sectors. /P <>BDC /P <>BDC 9 0 0 9 366.1367 731.8898 Tm (2,899)Tj (CFM56-7B26)Tj ( )Tj BT F), there is no precipitation or visible moisture at the q 1 0 0 1 53.85 797.54 cm 0 0 m /F4 1 Tf EMC ( )Tj /P <>BDC ( C)Tj ET 7 0 0 7 241.2727 463.9528 Tm EMC ET 9 0 0 9 193.4424 38.8898 Tm 7 0 0 7 141.7322 89.9528 Tm W n /P <>BDC 6.5 0 0 6.5 448.2959 585.9529 Tm 0 Tc [(AIRL)8.1(INE & AIR)7.1(CRAF)-12.9(T)18.1( OPERA)56.9(T)-8.1(ION)-13.9(S)]TJ ET (29,359)Tj 7 0 0 7 141.7322 265.9528 Tm in later aircraft). ( )Tj -.02 Tc ( )Tj Happy Flying. /P <>BDC 7 0 0 7 338.3085 188.9528 Tm 6 0 0 6 132.3631 659.9528 Tm ( )Tj ET BT (I)Tj BT ET 0 Tc /P <>BDC EMC ( )Tj EMC /P <>BDC EMC BT 7 0 0 7 247.7395 221.7654 Tm /P <>BDC BT /P <>BDC EMC ET q /P <>BDC (136)Tj ET /P <>BDC BT ( )Tj q 1 0 0 1 215.431 128.878 cm 0 0 m /P <>BDC 7 0 0 7 130.1443 716.7654 Tm ET ET (portion of the flight in the cruise phase,)Tj BT EMC BT BT ( )Tj 0 Tc EMC (page 21\))Tj ( )Tj BT /P <>BDC EMC BT ( )Tj ET ET ET (class cabin configuration used in this study)Tj BT 7 0 0 7 124.1242 100.7654 Tm ET EMC ( )Tj (177)Tj 6.5 0 0 6.5 176.9362 545.9529 Tm 9 0 0 9 195.69 181.8898 Tm 7 0 0 7 380.2788 298.7654 Tm The weight increase in)Tj ET BT /P <>BDC ET 7 0 0 7 247.7395 727.7654 Tm ET 9 0 0 9 53.8582 181.8898 Tm BT EMC /P <>BDC (A)Tj ET 9 0 0 9 36.8504 104.8898 Tm 0 Tc EMC /GS2 gs EMC BT (37,653)Tj For the purposes of)Tj EMC BT EMC ( )Tj ET ET BT EMC EMC 7 0 0 7 316.0679 276.7654 Tm ( )Tj /P <>BDC EMC 5.25 0 0 5.25 73.853 11.5132 Tm ( )Tj BT EMC BT 7 0 0 7 277.3936 144.9528 Tm 9 0 0 9 190.3643 368.8898 Tm 9 0 0 9 554.9974 456.8898 Tm 0 Tc ( )Tj EMC 9 0 0 9 53.8582 687.8898 Tm BT /P <>BDC 0 Tc /P <>BDC 6 0 0 6 372.295 673.9528 Tm ET BT /P <>BDC BT 7 0 0 7 82.8504 199.9528 Tm I think in the table you are talking about the range where payload is limited by MTOW. 7 0 0 7 258.2805 133.7654 Tm EMC /P <>BDC /P <>BDC BT /P <>BDC /P <>BDC EMC ET /P <>BDC /P <>BDC /P <>BDC ET 0 Tc EMC EMC ET )Tj 9 0 0 9 200.4401 258.8898 Tm ( )Tj /P <>BDC ( )Tj ET .023 .567 .626 rg -.02 Tc EMC BT /P <>BDC EMC 36.85 824.882 572.599 17.008 re 7 0 0 7 403.7368 705.7654 Tm ET EMC ET ( )Tj BT ET EMC /P <>BDC /P <>BDC to test 0 Tc /P <>BDC BT EMC ET to standardise the total tank capacitance and allows for the replacement ET (31,416)Tj 7 0 0 7 294.4014 364.7654 Tm /P <>BDC 7 0 0 7 536.3849 67.7654 Tm BT /P <>BDC BT ET ET (airport charges, while the time-dependent)Tj 9 0 0 9 215.4313 38.8898 Tm ET EMC ET EMC ( )Tj EMC 6 0 0 6 495.9463 771.9528 Tm 9 0 0 9 395.1859 258.8898 Tm [(BOS-L)-31(A)-24.9(X)]TJ /P <>BDC BT BT .661 .752 .896 rg ET ( )Tj ( )Tj ( )Tj ET /P <>BDC 0 Tc EMC (19)Tj BT /P <>BDC /P <>BDC /P <>BDC /P <>BDC BT /P <>BDC ET EMC Boeing 737 Max, a new generation of this highly successful City Jet. /P <>BDC ET EMC (to 165 passengers on BOS-LAX. 7 0 0 7 445.619 606.7654 Tm /P <>BDC ET .41 .161 .508 rg /P <>BDC 9 0 0 9 411.0181 357.8898 Tm ET ( )Tj BT EMC ET /P <>BDC 9 0 0 9 545.1909 346.8898 Tm BT BT EMC BT ET BT /P <>BDC BT [(CFM L)17.1(E)-8.1(AP-1A32)]TJ /P <>BDC /P <>BDC (150)Tj 7 0 0 7 491.7142 694.7654 Tm ET EMC 7 0 0 7 116.3631 11.5132 Tm ET /P <>BDC (1,130)Tj EMC [(Aircr)10(aft)]TJ ( )Tj ET ET ET 7 0 0 7 537.7804 199.9528 Tm [(AIRL)8.1(INE & AIR)7.1(CRAF)-12.9(T)18.1( OPERA)56.9(T)-8.1(ION)-13.9(S)]TJ 0 Tc ( )Tj ( )Tj /P <>BDC EMC 8 0 0 8 43.6039 661.9528 Tm ET ET EMC 0 Tc /P <>BDC ET ( )Tj /P <>BDC 7 0 0 7 507.7893 67.7654 Tm EMC 9 0 0 9 375.8752 258.8898 Tm /P <>BDC ( )Tj BT BT (737 MAX 8 & 9 fuel)Tj ET (HGW2 option with an MTOW of)Tj BT ( )Tj EMC ET /P <>BDC BT ET (989)Tj ET 7 0 0 7 554.7883 463.7654 Tm 9 0 0 9 51.0315 379.8898 Tm 7 0 0 7 158.74 122.7654 Tm ET -.02 Tc (direction, with an initial heading ranging)Tj ( )Tj ET ( )Tj EMC 7 0 0 7 386.4701 419.9528 Tm ET BT ( )Tj ET BT EMC ET 0 Tc ( )Tj 7 0 0 7 439.7405 562.9528 Tm ET ( C)Tj ET [(AS)29(M)21(s)]TJ BT -.005 Tc ET ET ( 2021)Tj 424 0 obj /P <>BDC BT BT EMC BT BT ET /P <>BDC ET ET 0 Tc 9 0 0 9 542.2986 192.8898 Tm /P <>BDC BT /P <>BDC EMC -.02 Tc /P <>BDC ET ET 5.25 0 0 5.25 492.6848 11.5129 Tm ET ET EMC ( )Tj ET BT ET /P <>BDC /GS1 gs ET EMC BT ET W n 7 0 0 7 187.0858 562.9528 Tm ( )Tj (0.0134)Tj /P <>BDC 9 0 0 9 547.6174 467.8898 Tm 0 Tc ( )Tj BT EMC -.02 Tc /P <>BDC EMC 9 0 0 9 552.0261 555.8898 Tm (737-9 compared to the 737-900ER\(W\) is)Tj EMC /P <>BDC /P <>BDC /P <>BDC EMC 6 0 0 6 466.3124 715.9528 Tm ET EMC BT ET ET ET BT W n BT (170)Tj /P <>BDC ET EMC 6 0 0 6 278.3662 701.9528 Tm EMC 8 0 0 8 53.9373 760.7654 Tm Maybe there is someone out there who can give you a better answer. 9 0 0 9 411.0234 687.8898 Tm ET 9 0 0 9 382.3068 489.8898 Tm (157)Tj following conditions: Takeoff with CSFF on the upper wing surfaces is /F6 1 Tf 6.5 0 0 6.5 448.257 598.9529 Tm BT 7 0 0 7 258.2805 694.7654 Tm /P <>BDC 7 0 0 7 141.7322 441.9528 Tm EMC 0 Tc ( )Tj ( )Tj /P <>BDC /P <>BDC 7 0 0 7 107.1165 573.9528 Tm 6 0 0 6 513.0339 701.9528 Tm the two components of the air are separated, the nitrogenenriched air (NEA) is ( )Tj (operating the 737 has increased its)Tj BT BT EMC 9 0 0 9 360.0909 115.8898 Tm /P <>BDC ET 0 Tc 15 w /P <>BDC ET /P <>BDC /P <>BDC EMC EMC 9 0 0 9 386.2848 170.8898 Tm /OC /MC1183 BDC 7 0 0 7 456.2165 441.7654 Tm ET [(737-900E)-33(R)]TJ 7 0 0 7 363.2711 595.9528 Tm (It was assumed that all flights would)Tj 7 0 0 7 403.478 628.7654 Tm EMC ET .008 Tc 7 0 0 7 204.0935 188.7654 Tm ET BT ( )Tj ET q -.02 Tc EMC 10 0 0 10 36.8504 814.1973 Tm 0 Tc EMC 6.5 0 0 6.5 243.3486 742.9529 Tm BT 7 0 0 7 141.7322 133.9528 Tm -.02 Tc -.02 Tc BT BT 9 0 0 9 369.892 93.8898 Tm /P <>BDC ET ET BT /P <>BDC ET ET (. -.01 Tc ET -.02 Tc 9 0 0 9 212.7029 390.8898 Tm ET BT ET /F2 1 Tf 7 0 0 7 179.5605 320.9528 Tm EMC (difference between the aircraft types)Tj [(737-900E)-33(R)]TJ BT ET ( )Tj ET /P <>BDC BT 7 0 0 7 37.0536 573.9528 Tm EMC ET BT /OC /MC1346 BDC EMC (which could reduce this difference. BT EMC /P <>BDC /P <>BDC (The main operating parameters are: )Tj 7 0 0 7 364.1531 463.9528 Tm BT EMC 7 0 0 7 99.5912 507.9528 Tm ET 0 Tc /P <>BDC ET BT ET ET ET /P <>BDC BT /P <>BDC EMC /P <>BDC BT ET ET 9 0 0 9 394.0315 434.8898 Tm -.02 Tc EMC -.02 Tc ( )Tj -.02 Tc BT (3,078)Tj ( )Tj ET 7 0 0 7 54.7071 210.7654 Tm 9 0 0 9 411.0181 38.8898 Tm ET BT ( )Tj EMC 7 0 0 7 487.0872 11.5129 Tm -.02 Tc BT ( )Tj 0 Tc ( )Tj /F1 1 Tf BT -.01 Tc 5.25 0 0 5.25 447.6106 11.5129 Tm /P <>BDC (make the range. ( )Tj -.02 Tc /P <>BDC /P <>BDC /P <>BDC EMC /F1 1 Tf 6.5 0 0 6.5 499.1421 722.9529 Tm EMC /P <>BDC ( )Tj BT 6.5 0 0 6.5 295.8145 611.9529 Tm ET BT EMC BT -.02 Tc (comprehensive comparison of the aircraft)Tj /P <>BDC /P <>BDC /P <>BDC 7 0 0 7 457.0984 606.7654 Tm ( )Tj ET EMC BT EMC EMC BT 0 Tc 0 Tc (4,541)Tj ET ET EMC 6.5 0 0 6.5 375.6529 689.9529 Tm EMC 9 0 0 9 186.0353 291.8898 Tm /P <>BDC EMC EMC BT /P <>BDC 9 0 0 9 232.4408 753.8898 Tm ET (0.0141)Tj place of FUEL VALVE CLOSED. ET - Modern Airliners, Pingback:A New Opportunity For Hydrogen is Aviation Aeronautics, Pingback:A New Opportunity For Hydrogen is Aviation - Revolution-Green, Pingback:Southwest CEO Says It's Safe to Fly Again. The 737-)Tj /P <>BDC /P <>BDC BT EMC /P <>BDC ET EMC ET BT /P <>BDC (operator, so controlling this cost is a)Tj (737-800W)Tj 6.5 0 0 6.5 382.9199 735.9529 Tm ET 7 0 0 7 444.737 111.7654 Tm 7 0 0 7 158.74 111.7654 Tm ET 9 0 0 9 563.0415 775.8898 Tm /P <>BDC (194,700)Tj )Tj 0 Tc EMC ET EMC 7 0 0 7 554.7883 507.7654 Tm 9 0 0 9 546.3505 566.8898 Tm ( )Tj ( )Tj -.015 Tc 9 0 0 9 211.8218 533.8898 Tm -.02 Tc -.01 Tc ET BT (up to 3,200nm when equipped with)Tj BT /P <>BDC (BOS-DEN)Tj /P <>BDC EMC ( )Tj S ET BT 0 Tc EMC 0 Tc 7 0 0 7 294.4014 474.7654 Tm 518.697 0 l 0 J 0 j 5 w 10 M [] 0 d /P <>BDC /P <>BDC ET ET /P <>BDC /P <>BDC BT ET 9 0 0 9 373.87 258.8898 Tm 8 0 0 8 74.9636 591.9528 Tm (150)Tj BT ET tank (see photo below). ET EMC EMC BT BT BT EMC 7 0 0 7 404.3599 595.7654 Tm 9 0 0 9 53.8582 709.8898 Tm EMC .176 .307 .621 rg (Recent improvements in cabin design)Tj 9 0 0 9 53.8582 170.8898 Tm 9 0 0 9 36.8504 126.8898 Tm ( )Tj /P <>BDC ( )Tj /P <>BDC (passengers and the 737-900ER\(W\) 152)Tj /F6 1 Tf /P <>BDC EMC -.02 Tc 7 0 0 7 131.6494 78.7654 Tm BT (CFM56-)Tj ( )Tj The data for our pages are sourced from various locations, ranging from airliner manufacturer websites, technical airliner manuals etc. EMC ET /P <>BDC 9 0 0 9 394.0237 456.8898 Tm EMC BT EMC BT System Description. BT /P <>BDC -.005 Tc 7 0 0 7 230.7317 177.9528 Tm /P <>BDC (346,456)Tj ET EMC -.02 Tc 7 0 0 7 108.6215 441.9528 Tm /P <>BDC EMC EMC 9 0 0 9 394.0157 82.8898 Tm /P <>BDC BT BT (2.5% lower fuel burn for the 737-800. EMC ( )Tj BT EMC BT BT /P <>BDC BT /P <>BDC (10)Tj /P <>BDC /P <>BDC EMC BT /P <>BDC /Artifact <>BDC BT -.02 Tc ( )Tj EMC 7 0 0 7 354.6933 386.7654 Tm BT 9 0 0 9 411.0097 115.8898 Tm ET BT EMC -.02 Tc 7 0 0 7 118.104 111.7654 Tm A fuel sampling and testing kit is kept on the flight deck of all ET -.01 Tc -.02 Tc [(M)-9(L)51(W - lbs)]TJ -.02 Tc ET BT ET ET ET BT 7 0 0 7 294.4014 485.7654 Tm EMC -.02 Tc BT 0 Tc (486)Tj BT BT 7 0 0 7 82.8504 419.9528 Tm BT Do you have the estimated production material used for the 737 Next Gen? (31,416)Tj EMC /P <>BDC EMC 9 0 0 9 53.8582 225.8898 Tm ( )Tj (66,096)Tj /P <>BDC BT The aircraft look like standard -800s, so why the difference? EMC /P <>BDC /P <>BDC 28.5749 0 TD ET BT BT EMC EMC 9 0 0 9 394.0315 621.8898 Tm BT ET ET ( )Tj EMC The NGS is an onboard inert gas system that uses an ( )Tj 9 0 0 9 524.2249 478.8898 Tm EMC BT 9 0 0 9 411.0097 49.8898 Tm BT ( )Tj BT BT BT /OC /MC835 BDC EMC EMC 9 0 0 9 188.1863 170.8898 Tm EMC 0 Tc EMC ET 7 0 0 7 380.2788 639.7654 Tm ( )Tj EMC ET /P <>BDC ( )Tj -.02 Tc BT ( )Tj [(family competitors, the 737 M)-8.1(A)-24.9(X also has)]TJ ( )Tj /P <>BDC /P <>BDC EMC 6.5 0 0 6.5 379.0655 585.9529 Tm 7 0 0 7 82.2047 705.9528 Tm EMC 7 0 0 7 554.7883 672.7654 Tm EMC BT EMC /P <>BDC /P <>BDC BT BT (483)Tj BT (These are the 737-800 and 737-8, 737-)Tj .014984 841.89 609.45 -841.89 re EMC BT 7 0 0 7 279.1575 133.9528 Tm EMC EMC /P <>BDC 7 0 0 7 247.7395 716.7654 Tm /P <>BDC 7 0 0 7 379.3969 111.7654 Tm 9 0 0 9 545.8646 522.8898 Tm (31,416)Tj (127 passengers on the longest sector,)Tj ET /P <>BDC ET /P <>BDC 6.5 0 0 6.5 381.6589 624.9529 Tm 7 0 0 7 99.8582 430.7654 Tm 7 0 0 7 241.2727 661.9528 Tm /P <>BDC 9 0 0 9 362.8235 401.8898 Tm /F1 1 Tf BT -.02 Tc (/S)Tj (its payload reduced to 165 passengers from)Tj This article will)Tj -.02 Tc /P <>BDC /P <>BDC EMC ET BT 9 0 0 9 411.0097 126.8898 Tm /P <>BDC EMC /P <>BDC ET ( )Tj (be charged the same in operation for this)Tj (CFM56-5B4/P)Tj (31,416)Tj EMC ( )Tj (4,863)Tj /P <>BDC EMC /P <>BDC BT /P <>BDC /P <>BDC /P <>BDC start a self test of the display and the fuel quantity indicating system. ET /P <>BDC ET EMC 8 0 0 8 136.4919 577.9528 Tm /P <>BDC BT /P <>BDC EMC BT ET BT /P <>BDC /GS1 gs (Improvements introduced to the)Tj ET EMC ET ET BT ( )Tj 7 0 0 7 230.7317 232.9528 Tm EMC The flight)Tj ET 0 Tc ET EMC 5.25 0 0 5.25 100.8225 11.5132 Tm /P <>BDC ET /P <>BDC 9 0 0 9 53.8582 192.8898 Tm BT EMC ET ET /P <>BDC ( )Tj BT 9 0 0 9 540.3981 588.8898 Tm ET EMC 0 Tc ( )Tj /GS1 gs /P <>BDC 0 Tc EMC ET ET /P <>BDC 6.5 0 0 6.5 324.4345 689.9529 Tm ( )Tj BT ( )Tj /P <>BDC /P <>BDC /P <>BDC which in hot conditions will evaporate and create an explosive mixture with the ET /P <>BDC ET BT BT ET BT BT EMC BT BT 7 0 0 7 403.478 639.7654 Tm 7 0 0 7 43.6039 639.9528 Tm BT endobj ET ET EMC BT 7 0 0 7 457.0984 518.7654 Tm ET BT 7 0 0 7 543.7693 11.5132 Tm EMC ( )Tj ET (136)Tj -.01 Tc 7 0 0 7 386.3929 705.9528 Tm BT /P <>BDC 7 0 0 7 490.8321 122.7654 Tm ET ET EMC ET /P <>BDC ( )Tj EMC BT (not been used for the A321ceo against the)Tj BT EMC (significant enough that operating the)Tj 6.5 0 0 6.5 484.6315 585.9529 Tm BT BT BT The average headwind)Tj (0.0140)Tj EMC BT BT differential pressure (and bleed air as a backup) is used to maintain a head of pressure in the 7 0 0 7 508.4124 716.7654 Tm 9 0 0 9 544.921 225.8898 Tm /P <>BDC BT ET 8 0 0 8 43.6039 717.9528 Tm BT ET 0 Tc ET EMC 9 0 0 9 381.9109 456.8898 Tm BT ( )Tj 6 0 0 6 308.6461 743.9528 Tm /P <>BDC -.02 Tc 7 0 0 7 108.6215 232.9528 Tm ( )Tj 0 Tc BT 9 0 0 9 195.6833 115.8898 Tm ET -.02 Tc 7 0 0 7 321.6356 320.9528 Tm 0 Tc /P <>BDC ET 9 0 0 9 551.0015 291.8898 Tm EMC /P <>BDC BT /P <>BDC /P <>BDC (157,300)Tj (and fuel burn per ASM for the four pairs)Tj BT EMC BT ET EMC ET 9 0 0 9 36.8504 368.8898 Tm (l)Tj ( )Tj /P <>BDC /P <>BDC ET 0 Tc BT -.02 Tc /P <>BDC Note: for aircraft delivered after May 2004, centre tank ( )Tj EMC BT BT EMC /P <>BDC ET BT EMC EMC ET In the)Tj ET ( )Tj .008 Tc /P <>BDC 6 0 0 6 351.3743 715.9528 Tm BT (404)Tj 6 0 0 6 425.0715 687.9528 Tm EMC BT ET ET ET EMC ET S -.02 Tc ( )Tj -.02 Tc BT /P <>BDC BT (0.0132)Tj EMC (0.0129)Tj ( )Tj EMC ( )Tj In contrast, Boeing has)Tj EMC -.02 Tc BT Just not sure how to access these. 9 0 0 9 209.6398 489.8898 Tm 9 0 0 9 378.6646 797.8898 Tm (The sectors are chosen to ensure a)Tj ET EMC 7 0 0 7 241.5317 298.9528 Tm EMC ET 9 0 0 9 53.8578 456.8898 Tm /P <>BDC (179)Tj ET EMC 6 0 0 6 326.0708 673.9528 Tm ET ET /P <>BDC BT [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ (compared to 16,200kg on classics). 7 0 0 7 82.8504 408.9528 Tm 9 0 0 9 363.3015 775.8898 Tm 9 0 0 9 534.0193 390.8898 Tm 8 0 0 8 43.6039 731.9528 Tm EMC 0 Tc ET 9 0 0 9 198.8517 280.8898 Tm ET EMC ET ET /P <>BDC /P <>BDC BT /P <>BDC ET /P <>BDC The Honeywell NGS was certified by the FAA on 21 Feb 2006 after over 1000hrs flight testing on two 737-NGs. /P <>BDC BT (136)Tj EMC /P <>BDC 0 Tc BT /P <>BDC 7 0 0 7 386.4701 89.9528 Tm /P <>BDC BT (5,126)Tj BT /P <>BDC BT ( )Tj ET ET /P <>BDC ET BT 9 0 0 9 196.1514 390.8898 Tm 7 0 0 7 338.3085 375.9528 Tm BT EMC /P <>BDC 9 0 0 9 199.3527 390.8898 Tm ( )Tj BT In real)Tj /P <>BDC /P <>BDC ET ( )Tj BT EMC ET 7 0 0 7 158.74 617.7654 Tm /P <>BDC ( )Tj /P <>BDC ET (Using the evaluation payloads of 170)Tj ( )Tj ET /P <>BDC 7 0 0 7 314.6398 738.7654 Tm /P <>BDC EMC 7 0 0 7 204.0935 78.7654 Tm 7 0 0 7 315.5217 562.7654 Tm ET /P <>BDC /P <>BDC EMC 0 841.89 609.449 -841.89 re /P <>BDC EMC (737-8)Tj EMC BT 7 0 0 7 535.5029 716.7654 Tm ( )Tj EMC 7 0 0 7 99.8582 606.7654 Tm (dependent on the operators internal)Tj endobj It works by transferring fuel from the aux BT /P <>BDC 9 0 0 9 411.0181 313.8898 Tm

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