BT BT ( )Tj ET ET 7 0 0 7 386.4701 397.9528 Tm EMC EMC Maximum zero fuel weight (kg) 70 990: Standard fuel capacity (litres) 25 800: Performance; Range with max payload (km) 6 500: Cruise speed (km/h) 840: Maximum operating altitude (m) 12 000: Engines: CFMI LEAP-1B, 2 x 26790-29310 lb: BT BT ( )Tj ET /P <>BDC BT BT ET ET BT ( )Tj 7 0 0 7 490.5101 496.9528 Tm BT ET /P <>BDC 0 Tc EMC ( )Tj BT BT /P <>BDC /P <>BDC 7 0 0 7 355.3163 166.7654 Tm 7 0 0 7 337.6855 529.9528 Tm ET ( )Tj EMC /P <>BDC /P <>BDC ET BT 8 0 0 8 72.3645 771.9528 Tm /P <>BDC ET BT (A321ceo)Tj ET which in hot conditions will evaporate and create an explosive mixture with the ( 2021)Tj EMC EMC ET ET ET EMC BT ( )Tj (fuel capacity of 6,303USG )Tj ET ( )Tj EMC 7 0 0 7 508.4124 320.7654 Tm /P <>BDC 9 0 0 9 455.0733 60.8898 Tm 7 0 0 7 362.3891 199.9528 Tm ( )Tj 7 0 0 7 82.8504 144.9528 Tm ET ET /GS1 gs ET -.02 Tc EMC EMC ET 6.5 0 0 6.5 244.0438 722.9529 Tm BT 7 0 0 7 404.101 232.7654 Tm 7 0 0 7 314.6398 661.7654 Tm /P <>BDC /P <>BDC 9 0 0 9 394.0315 368.8898 Tm ET 9 0 0 9 215.4313 247.8898 Tm 0 Tc ( )Tj /P <>BDC (A potential operator would need to)Tj ET ET (31,416)Tj 9 0 0 9 390.5438 566.8898 Tm (which has the lowest fuel burn rate per)Tj 9 0 0 9 392.5128 236.8898 Tm [(Summar)-33(y )]TJ EMC BT EMC /P <>BDC EMC /P <>BDC EMC BT [(v)21(ariant)]TJ Well, the fuel capacity of this airplane varies depending on the specific model and generation. 9 0 0 9 518.0203 170.8898 Tm ET EMC EMC ET 0 Tc EMC ET EMC 7 0 0 7 507.7893 507.7654 Tm EMC ( )Tj BT ET -.02 Tc BT /P <>BDC ET BT (minutes between aircraft types or 3.7% on)Tj -.02 Tc -.02 Tc (travelled for the aircraft on each route is)Tj Until its launch on September 5, 1994 the 737-800 was known as the 737-400X Stretch. BT ( )Tj ( )Tj 0 Tc /P <>BDC 7 0 0 7 427.7291 232.9528 Tm /P <>BDC EMC 6 0 0 6 465.8383 673.9528 Tm ET /P <>BDC EMC EMC ET EMC BT BT /P <>BDC 6 0 0 6 513.0339 701.9528 Tm EMC ( )Tj 7 0 0 7 386.3929 573.9528 Tm /P <>BDC (. /P <>BDC EMC BT EMC ET /P <>BDC ( )Tj ( )Tj /P <>BDC BT EMC EMC 7 0 0 7 141.7322 111.9528 Tm 6.5 0 0 6.5 54.877 598.9529 Tm BT EMC /OC /MC21 BDC ( )Tj BT 7 0 0 7 241.5317 320.9528 Tm /P <>BDC endobj EMC BT EMC BT 7 0 0 7 294.4014 397.7654 Tm EMC EMC 0 Tc /P <>BDC 9 0 0 9 177.8457 82.8898 Tm ET ( )Tj EMC /P <>BDC ( )Tj EMC EMC /P <>BDC BT BT /P <>BDC ( )Tj 0 Tc )Tj ET /P <>BDC /P <>BDC 5.25 0 0 5.25 549.1047 11.5132 Tm EMC ( )Tj ET -.02 Tc BT EMC ( )Tj EMC EMC 7 0 0 7 457.0984 463.7654 Tm 7 0 0 7 381.1608 584.7654 Tm 13 0 0 13 202.8899 533.8898 Tm ET ( )Tj -.02 Tc /P <>BDC BT EMC Maybe there is someone out there who can give you a better answer. /P <>BDC (737-8)Tj /P <>BDC ET ET ET ET EMC BT ET (170)Tj /P <>BDC EMC ( )Tj ET ET )Tj re-primed. -.02 Tc 9 0 0 9 553.6047 423.8898 Tm The 737-800 has a maximum fuel capacity of 6,875 gallons, which it carries in fuel tanks in its wings, as seen here, and in a fuel tank located underneath the passenger cabin's midsection. ET 0 Tc EMC BT ET -.02 Tc BT ET BT /P <>BDC -.02 Tc Aluminium alloys are still the mainstay of the construction materials used with various blends used according to the strength required for the particular component. (with a thrust rating of 26,000lbs, an intake)Tj BT ( 2021)Tj 0 Tc ET ( )Tj .014984 841.89 609.45 -841.89 re BT /P <>BDC EMC 0 Tc ( )Tj /P <>BDC EMC EMC BT 7 0 0 7 491.7142 485.7654 Tm BT 851 0 obj /P <>BDC 6.5 0 0 6.5 64.6596 558.9529 Tm (0.0120)Tj (1,272)Tj 7 0 0 7 163.8846 11.5132 Tm /P <>BDC 7 0 0 7 258.2805 727.7654 Tm BT /P <>BDC EMC EMC (BOS-PHX \(Phoenix\); 133 on BOS-YVR;)Tj BT /P <>BDC 9 0 0 9 408.1854 676.8898 Tm 7 0 0 7 187.0858 100.9528 Tm 5.25 0 0 5.25 40.8474 11.5129 Tm BT BT BT EMC BT /P <>BDC /P <>BDC 9 0 0 9 36.8504 115.8898 Tm /P <>BDC /P <>BDC 6.5 0 0 6.5 64.6596 663.9529 Tm EMC BT 7 0 0 7 279.1575 683.9528 Tm (I)Tj /P <>BDC 7 0 0 7 158.74 639.7654 Tm ( )Tj EMC /P <>BDC 0 Tc 9 0 0 9 567.1517 49.8898 Tm BT /P <>BDC EMC BT 9 0 0 9 36.8583 423.8898 Tm (of aircraft types that are of equal size. BT /P <>BDC 9 0 0 9 207.5339 280.8898 Tm EMC 7 0 0 7 321.6356 133.9528 Tm BT ( )Tj BT ( )Tj /P <>BDC -.02 Tc (900ER\(W\) across the 14 routes with the)Tj ET EMC /P <>BDC BT /P <>BDC EMC 9 0 0 9 411.0097 269.8898 Tm 7 0 0 7 37.0536 584.9528 Tm /P <>BDC BT (1,019)Tj EMC ET ET ( )Tj BT ET -.01 Tc EMC EMC ET /P <>BDC EMC BT 28.5749 0 TD (The 737NG family has a single engine)Tj 7 0 0 7 379.3969 144.7654 Tm EMC ( )Tj .534 .14 .504 RG ( )Tj /P <>BDC 9 0 0 9 392.5848 346.8898 Tm BT BT ET 7 0 0 7 535.5029 474.7654 Tm /P <>BDC ET 0 Tc EMC /P <>BDC -.02 Tc EMC ( )Tj EMC ET Usually, you can find technical manuals, sometimes in PDF form which are full of information. ET Q -.02 Tc 0 Tc BT -.02 Tc /P <>BDC ET ( )Tj -.02 Tc ( )Tj /P <>BDC ET [(Engine b)6.1(ypass)]TJ /P <>BDC 7 0 0 7 404.101 144.7654 Tm BT air speed, altitude, and similar flight parameters were made available from (ranges from 0.47 to 0.33 cents, and is)Tj BT (974)Tj ET BT ET ET EMC ET EMC BT 7 0 0 7 314.6398 485.7654 Tm (31,416)Tj ET ET ( )Tj ET EMC EMC /P <>BDC (1,913)Tj /P <>BDC BT 0 Tc ( )Tj EMC ET BT ET ET ET ET ET EMC EMC ET ET BT /P <>BDC BT It has a maximum takeoff weight of about 80,000 kg (175,000 lbs). EMC (0.0123)Tj (2,748)Tj EMC (900ER\(W\) due to the heavier payload. EMC ( )Tj 7 0 0 7 247.7395 232.7654 Tm ( )Tj EMC EMC (0.0177)Tj BT 7 0 0 7 141.7322 705.9528 Tm 6.5 0 0 6.5 477.8064 702.9529 Tm ET BT ( )Tj (172,992)Tj EMC BT -.02 Tc /P <>BDC ET /P <>BDC ( )Tj ( )Tj BT (380-396)Tj (The A321ceo is equipped with either:)Tj 304.725 420.96 m compensator EMC BT ET /P <>BDC BT 7 0 0 7 82.8504 408.9528 Tm /P <>BDC 7 0 0 7 554.7883 705.7654 Tm ( )Tj 0 Tc Jump to Specification Table Boeing 737 Next Gen and Max. EMC 0 Tc BT /P <>BDC BT [(CFM L)17.1(E)-8.1(AP-1A26)]TJ -.02 Tc 0 Tc 9 0 0 9 369.4947 357.8898 Tm The average fuel cost per)Tj 7 0 0 7 518.4953 122.9528 Tm EMC EMC /P <>BDC ( )Tj ( )Tj /P <>BDC Boeing 737 Interior. ET ( )Tj (737-800W)Tj ( )Tj BT 0 Tc /OC /MC2287 BDC ( )Tj /P <>BDC ET ( )Tj ( )Tj BT BT q 1 0 0 1 36.85 797.54 cm 0 0 m /P <>BDC 5.25 0 0 5.25 64.5461 11.5129 Tm 7 0 0 7 456.2165 100.7654 Tm BT ET /P <>BDC Q EMC /P <>BDC ET /P <>BDC (737-9)Tj BT (payload in scenario 1. BT /P <>BDC /P <>BDC /P <>BDC EMC /P <>BDC ( )Tj EMC 9 0 0 9 552.2312 676.8898 Tm 9 0 0 9 232.438 335.8898 Tm (39,270)Tj 9 0 0 9 232.4217 225.8898 Tm /P <>BDC BT /P <>BDC EMC /P <>BDC ( )Tj ET ( )Tj /P <>BDC [(Aircr)10(aft types )]TJ /P <>BDC EMC 6.5 0 0 6.5 129.3816 598.9529 Tm /P <>BDC 9 0 0 9 411.0097 115.8898 Tm ET /P <>BDC EMC ET (and the 737 MAX family with the CFM)Tj 9 0 0 9 36.8504 357.8898 Tm Of course, we know that there have been major hiccups in the introduction of the new 737 MAX with the tragic loss of life as a result. ET 7 0 0 7 537.7804 199.9528 Tm /P <>BDC 7 0 0 7 429.157 738.9528 Tm EMC 8 0 0 8 122.6593 760.7654 Tm EMC 7 0 0 7 299.0601 188.9528 Tm 9 0 0 9 185.7888 489.8898 Tm BT EMC 7 0 0 7 439.7405 606.9528 Tm EMC /F1 1 Tf BT /P <>BDC EMC EMC BT ET ET (74-82)Tj 9 0 0 9 165.1286 137.8898 Tm ET -.02 Tc 7 0 0 7 337.6855 562.9528 Tm 9 0 0 9 194.5468 71.8898 Tm (/S)Tj ET 13 0 0 13 53.8338 588.8898 Tm 7 0 0 7 354.6933 430.7654 Tm /P <>BDC BT 7 0 0 7 456.2165 397.7654 Tm ( )Tj ( )Tj -.342 -1.2294 l (improvement in fuel burn compared with)Tj BT ( )Tj EMC ET /P <>BDC ET /P <>BDC 6.5 0 0 6.5 375.6529 689.9529 Tm 0 Tc 9 0 0 9 411.0234 731.8898 Tm ET ET 9 0 0 9 411.0097 214.8898 Tm ( )Tj 6 0 0 6 340.4597 743.9528 Tm EMC /P <>BDC BT 7 0 0 7 537.7804 67.9528 Tm BT 9 0 0 9 394.0315 654.8898 Tm 0 Tc 6.5 0 0 6.5 346.3049 689.9529 Tm 0 Tc /P <>BDC BT 0 Tc /P <>BDC -.02 Tc EMC (737-800W)Tj (46,900)Tj EMC ET ET BT This)Tj /P <>BDC BT (The 737-9 has an 11.2% to 12.7%)Tj -.02 Tc BT BT 9 0 0 9 394.0237 390.8898 Tm 9 0 0 9 215.4313 159.8898 Tm /P <>BDC /F1 1 Tf EMC EMC BT ET BT /P <>BDC (737-8)Tj ET /F6 1 Tf BT ( )Tj 9 0 0 9 544.5056 302.8898 Tm BT 6.5 0 0 6.5 397.7514 598.9529 Tm EMC BT -.02 Tc EMC EMC /P <>BDC EMC (In the 85% passenger payload)Tj BT BT EMC BT 9 0 0 9 394.0157 280.8898 Tm ( )Tj EMC ( )Tj ET /P <>BDC 7 0 0 7 187.0858 496.9528 Tm The weight increase in)Tj BT ET BT /P <>BDC EMC ( )Tj [(BOS-D)17.1(T)-11(W)]TJ -.02 Tc )Tj I already checked in the AMM, SRM. ET EMC ET BT ( )Tj /P <>BDC EMC 7 0 0 7 294.4014 419.7654 Tm /P <>BDC 9 0 0 9 198.192 599.8898 Tm Q ( )Tj ET 0 Tc 6.5 0 0 6.5 488.8955 532.9529 Tm EMC -.02 Tc (the CFM56-5B4/P with a maximum take-)Tj ET 6.5 0 0 6.5 552.6508 565.9529 Tm /P <>BDC (34,650)Tj EMC /OC /MC5080 BDC 0 J 0 j 5 w 10 M [] 0 d BT 0 Tc /P <>BDC BT S (CFM56-7B26)Tj ET -.02 Tc 6 0 0 6 444.4713 757.9528 Tm ET BT /P <>BDC [(SS)-9.1(U)8(E)]TJ EMC ( )Tj 0 Tc ET (pages 23 & 24\))Tj BT /P <>BDC BT BT EMC (5.1:1)Tj ET ET ( )Tj BT 7 0 0 7 179.5605 617.9528 Tm EMC /P <>BDC ( )Tj EMC /P <>BDC (217)Tj ( )Tj (0.0122)Tj ET BT EMC /P <>BDC 7 0 0 7 387.0932 210.9528 Tm BT BT /P <>BDC ( )Tj EMC ET ET /P <>BDC EMC 7 0 0 7 457.0984 210.7654 Tm EMC 304.725 420.96 m EMC ET BT (route structure so these charges would not)Tj (33,000lbs, the same 81-inch fan diameter)Tj ( )Tj BT BT /P <>BDC BT EMC ET (379)Tj ET 8 0 0 8 64.6596 760.9529 Tm ET BT EMC ET EMC ET /P <>BDC /P <>BDC EMC ET /P <>BDC EMC EMC /P <>BDC ( )Tj EMC EMC BT A previous model which had success was Airbuses A320. EMC endobj ET /P <>BDC ( )Tj BT 7 0 0 7 163.8846 11.5132 Tm /P <>BDC /P <>BDC 9 0 0 9 117.7519 170.8898 Tm ET EMC ET EMC BT BT EMC ( )Tj ET EMC 0 Tc (150)Tj (inches and a bypass ratio of 11.0:1. (3,369)Tj ET EMC 8 0 0 8 124.845 577.9528 Tm 0 Tc 9 0 0 9 194.9081 346.8898 Tm ( )Tj BT sectors to ensure an even fuel balance. ( )Tj /P <>BDC /GS1 gs [(CFM L)17.1(E)-8.1(AP-1A26)]TJ sorry that is way out of our knowledge here. 7 0 0 7 404.101 243.7654 Tm EMC ET /P <>BDC [(Oper)10(ating Assumptions )]TJ /P <>BDC BT ( )Tj EMC BT ET EMC /P <>BDC /P <>BDC /P <>BDC ( )Tj (10)Tj ( The time spent in potential holding)Tj BT ( )Tj EMC ET EMC EMC -.02 Tc ET /P <>BDC 10 0 0 10 50.1204 814.1973 Tm EMC 8 0 0 8 394.0157 786.8898 Tm BT -.02 Tc EMC /P <>BDC EMC /P <>BDC (seat count as the 737-900ER\(W\). EMC ET (72,450)Tj BT There seem to be a lot of answers that come up, some of which might be what youre looking for. ET 6 0 0 6 496.3652 743.9528 Tm BT as shown at the top of the page. EMC EMC BT ( )Tj ( )Tj EMC /P <>BDC (179)Tj BT 7 0 0 7 70.8101 243.9528 Tm ( )Tj -.02 Tc BT (even though the two have the same)Tj EMC (These are the 737-800 and 737-8, 737-)Tj BT -.02 Tc 8 0 0 8 394.0157 764.8898 Tm ET EMC ET 8 0 0 8 317.9854 771.9529 Tm BT EMC ET EMC -.02 Tc 6.5 0 0 6.5 499.7986 637.9529 Tm /P <>BDC ET ( )Tj 8 0 0 8 542.3528 764.8898 Tm BT EMC ET BT ET BT BT EMC EMC /P <>BDC (166,090)Tj /P <>BDC /P <>BDC /P <>BDC ET (A320ceo: )Tj ( )Tj EMC 9 0 0 9 511.9579 335.8898 Tm EMC /P <>BDC )Tj /P <>BDC /P <>BDC EMC 7 0 0 7 380.2788 298.7654 Tm BT ET BT /P <>BDC 9 0 0 9 343.5117 489.8898 Tm /P <>BDC 9 0 0 9 360.9639 192.8898 Tm q 1 0 0 1 505.328 82.247 cm 0 0 m 9 0 0 9 550.4974 599.8898 Tm EMC EMC ET ET BT /P <>BDC 0 Tc BT A Boeing 737-800 NG with all seats removed can not carry more than 24 000 kg of payload and the maximum volume transported can not surpass 184 m3, no matter what you do, as long as, according to the article B737-800BDSF Passenger to Cargo Conversion, "the 737-800BDSF [a factory modified 737-800 NG] is the second B737 New Generation converted ET EMC 9 0 0 9 36.8504 302.8898 Tm ( )Tj EMC must not be left ON unless personnel are available in the flight deck (1465,400)Tj 848 0 obj ( )Tj 9 0 0 9 36.8504 137.8898 Tm /P <>BDC BT /P <>BDC EMC (capacity. 9 0 0 9 535.2051 500.8898 Tm BT ET BT /P <>BDC (LRC; the same as the primary sector. (1,272)Tj BT 0 Tc 7 0 0 7 387.0159 529.9528 Tm /P <>BDC BT (be charged the same in operation for this)Tj /P <>BDC -.01 Tc (other seven aircraft types. /P <>BDC BT (34,650)Tj BT BT /P <>BDC 7 0 0 7 294.4014 276.7654 Tm 9 0 0 9 411.0181 38.8898 Tm Hi Peter, EMC ET ET (Like the A321neo, the 737-9 has a)Tj BT ( )Tj BT BT /P <>BDC EMC 9 0 0 9 542.5887 159.8898 Tm EMC BT /P <>BDC /P <>BDC Adobe d (41,289)Tj The)Tj /P <>BDC EMC (170)Tj ET ET /P <>BDC -.01 Tc ET ET EMC EMC ET /P <>BDC ( )Tj BT ET /P <>BDC 6 0 0 6 363.2184 687.9528 Tm (0.0113)Tj ( )Tj ET EMC 7 0 0 7 299.0601 309.9528 Tm -.02 Tc 9 0 0 9 246.6113 71.8898 Tm ET EMC /P <>BDC (thrust. EMC EMC /P <>BDC BT EMC (this page\))Tj BT 9 0 0 9 53.8582 324.8898 Tm BT /P <>BDC ET /P <>BDC ET EMC ET (have any payload limitations on the routes)Tj ET ( )Tj EMC (against the 737-800 is interesting. -.02 Tc 9 0 0 9 408.1854 159.8898 Tm /P <>BDC EMC EMC EMC ( )Tj /P <>BDC ET BT ( )Tj -.02 Tc 8 0 0 8 258.2687 771.7654 Tm ET ( )Tj EMC ET ET /P <>BDC EMC (table, page 19\))Tj 0 Tc 9 0 0 9 36.8504 434.8898 Tm 7 0 0 7 444.737 331.7654 Tm /P <>BDC /P <>BDC I found this image that might have some of the answers you need. (0.0154)Tj 8 0 0 8 43.6039 661.9528 Tm -.02 Tc ET 6 0 0 6 547.0496 673.9528 Tm 788 0 obj /P <>BDC ET -.02 Tc 7 0 0 7 490.5101 485.9528 Tm 8 0 0 8 302.5117 619.9528 Tm (310,080)Tj ET ()Tj -.02 Tc BT -.02 Tc /P <>BDC EMC EMC EMC Do you have a reference please? (full passenger payload. ET 7 0 0 7 456.4753 617.7654 Tm /P <>BDC 7 0 0 7 141.7322 683.9528 Tm ( )Tj s !1AQa"q2B#R3b$r%C4Scs5D'6Tdt& .151 .147 .15 rg BT BT 9 0 0 9 229.6141 49.8898 Tm EMC /P <>BDC ET 9 0 0 9 53.8578 467.8898 Tm ET ET BT EMC 7 0 0 7 37.0536 727.9528 Tm EMC 0 Tc /P <>BDC ET /P <>BDC BT ET /P <>BDC EMC (offering: the 737NG with the CFM56-7B;)Tj EMC BT /P <>BDC /P <>BDC EMC ET 6 0 0 6 425.0715 687.9528 Tm /P <>BDC ( )Tj EMC ET EMC ET 7 0 0 7 536.3849 210.7654 Tm /P <>BDC (of the Boeing aircraft, with the A321ceo)Tj 8 0 0 8 256.0704 591.9528 Tm ET BT [(7)-33(3)8(7-800)]TJ /Artifact <>BDC [(CFM L)17.1(E)-8.1(AP-1A26)]TJ 13 0 0 13 179.2927 71.8898 Tm BT /Artifact <>BDC BT 7 0 0 7 316.0679 375.7654 Tm ET ET (483)Tj EMC BT /P <>BDC EMC /P <>BDC ( )Tj BT (31,416)Tj BT BT /P <>BDC /P <>BDC /P <>BDC BT This will)Tj /P <>BDC EMC EMC At engine idle, the system tolerance can be 12%. ( )Tj <> ET EMC ET 6 0 0 6 153.9401 659.9528 Tm -.02 Tc BT 7 0 0 7 520.6108 628.9528 Tm 6.5 0 0 6.5 244.2585 650.9529 Tm W n (/S)Tj ET BT (HGW2 option with an MTOW of)Tj /P <>BDC 7 0 0 7 179.5605 122.9528 Tm BT 0 841.89 609.449 -841.89 re BT (2,149)Tj BT /P <>BDC ( )Tj /P <>BDC ( )Tj 7 0 0 7 321.6356 375.9528 Tm than the main wing tanks. BT 9 0 0 9 166.1068 313.8898 Tm /P <>BDC EMC ( )Tj 9 0 0 9 411.0097 379.8898 Tm /P <>BDC /P <>BDC BT 6.5 0 0 6.5 228.7846 545.9529 Tm BT EMC ( )Tj EMC ET ET BT ET /P <>BDC ( )Tj 9 0 0 9 215.4409 379.8898 Tm EMC (35,112)Tj /P <>BDC -.02 Tc BT /P <>BDC safest way forward, but is very expensive and possibly impractical. concentration at eight different locations. 7 0 0 7 36.8504 11.5129 Tm ET BT -.01 Tc The)Tj ET y9ou may find what you are looking for by clicking here. 7 0 0 7 445.619 617.7654 Tm 7 0 0 7 491.4046 298.9528 Tm /P <>BDC 9 0 0 9 215.4313 60.8898 Tm EMC /OC /MC1950 BDC This is the same)Tj ( )Tj BT (5,126)Tj EMC 9 0 0 9 367.2172 269.8898 Tm ET 0 Tc EMC /P <>BDC EMC BT ( )Tj 9 0 0 9 530.4152 423.8898 Tm /P <>BDC Q /P <>BDC ( )Tj /P <>BDC (This evaluation has been conducted)Tj -.02 Tc allow for a measurement of fuel tank inerting and heating during the 7 0 0 7 364.1531 463.9528 Tm BT 378 0 0 303.84 -.19113 501.447 cm ET ET ET BT BT /P <>BDC 6.5 0 0 6.5 327.0283 598.9529 Tm ET BT BT 9 0 0 9 192.5225 489.8898 Tm /P <>BDC ( )Tj EMC 6.5 0 0 6.5 172.8217 565.9529 Tm BT BT 7 0 0 7 230.7317 408.9528 Tm BT (166,090)Tj ET EMC EMC ET EMC EMC EMC BT [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ f (216,240)Tj 7 0 0 7 491.7142 287.7654 Tm ET BT BT (166,669)Tj 7 0 0 7 88.196 11.5129 Tm Well, what do you know?! 0 Tc ( N)Tj EMC 0 Tc ET 7 0 0 7 99.8582 386.7654 Tm EMC 7 0 0 7 204.0935 111.7654 Tm 0 Tc ET BT 7 0 0 7 54.7071 507.7654 Tm /P <>BDC /P <>BDC )Tj /P <>BDC 7 0 0 7 247.7395 89.7654 Tm BT EMC EMC How many square feet (or cubic feet) of space is in the 737 MAX flight deck? (\(see table, page 19\))Tj 0 Tc ET ET ( )Tj ET 161.569 0 l /P <>BDC (cost index calculated by the airline to the)Tj ET (170)Tj ( )Tj 7 0 0 7 327.1097 573.9528 Tm ET BT ( C)Tj BT ( )Tj ( )Tj ET EMC EMC BT BT BT ( )Tj 7 0 0 7 520.6108 529.9528 Tm 9 0 0 9 189.1673 137.8898 Tm 0 Tc (0.0135)Tj EMC BT -.015 Tc BT ( )Tj /P <>BDC 0 Tc EMC ET /P <>BDC 0 Tc BT ET EMC BT (uses one of the 11 certified weight variants. BT 9 0 0 9 545.0725 434.8898 Tm EMC !! BT BT EMC 7 0 0 7 258.2805 133.7654 Tm /P <>BDC 6.5 0 0 6.5 54.2794 735.9529 Tm ( )Tj BT Federal Aviation Administration and the Boeing Company to evaluate the ET BT 5.25 0 0 5.25 525.4061 11.5132 Tm /P <>BDC BBJ Aux fuel panel located on Capt's & F/O's main -.02 Tc ET BT .151 .147 .15 rg (payload and route, and 16% higher than)Tj EMC -.02 Tc .151 .147 .15 rg BT 0 Tc ET 0 Tc 8 0 0 8 91.2605 771.9529 Tm EMC BT 6.5 0 0 6.5 540.4371 611.9529 Tm ( )Tj (0.0113)Tj BT ET 7 0 0 7 518.4953 199.9528 Tm /P <>BDC EMC ET ET /P <>BDC (65,688)Tj ET /P <>BDC BT ET EMC 7 0 0 7 321.6356 243.9528 Tm /OC /MC1663 BDC (This comparison is made using the)Tj ( )Tj /P <>BDC (\(see table, this page\))Tj ET ET EMC ET 9 0 0 9 198.165 225.8898 Tm /P <>BDC ET BT ( )Tj 6 0 0 6 239.8235 743.9528 Tm EMC BT Economy-plus is also)Tj 9 0 0 9 544.0105 258.8898 Tm 9 0 0 9 421.0664 401.8898 Tm /P <>BDC BT /P <>BDC ET ET (375)Tj BT (1,876)Tj 7 0 0 7 279.1575 738.9528 Tm 7 0 0 7 474.3564 705.9528 Tm /P <>BDC BT 9 0 0 9 548.4937 71.8898 Tm ET 9 0 0 9 548.6884 137.8898 Tm ( )Tj BT [(A3)24.9(21neo v)12.9(ersus 7)-33(3)8.1(7-9 )]TJ EMC 7 0 0 7 125.6292 89.7654 Tm ET ET EMC EMC EMC 6.5 0 0 6.5 297.8076 558.9529 Tm BT (39,270)Tj ET 6.5 0 0 6.5 375.6529 702.9529 Tm BT EMC /P <>BDC ( )Tj ET EMC ET ET /P <>BDC BT /P <>BDC (The flight tracks and cruise altitudes)Tj 8 0 0 8 338.514 745.9528 Tm ET ET 9 0 0 9 545.546 115.8898 Tm BT ET ET to standardise the total tank capacitance and allows for the replacement /P <>BDC 7 0 0 7 337.6855 276.9528 Tm 9 0 0 9 568.1771 115.8898 Tm BT ( )Tj ( )Tj ( )Tj BT EMC 9 0 0 9 497.8043 313.8898 Tm 0 Tc /GS1 gs /P <>BDC EMC 7 0 0 7 210.1137 265.7654 Tm /P <>BDC /P <>BDC BT 7 0 0 7 491.4046 122.9528 Tm