8 0 0 8 542.3528 764.8898 Tm BT ET 304.725 420.96 m ET ( )Tj EMC EMC 0 Tc /P <>BDC /P <>BDC (in engine cool-down times. /P <>BDC ET EMC ( )Tj ET 7 0 0 7 543.7693 11.5132 Tm -.02 Tc (A320ceo)Tj EMC This will)Tj (150)Tj BT ( )Tj EMC (to a larger increase when going from 5.7:1)Tj ( )Tj BT EMC EMC (passenger numbers are 136 for the)Tj ET ET /P <>BDC 0 Tc ( )Tj 6.5 0 0 6.5 528.5291 702.9529 Tm -.02 Tc BT ET /P <>BDC BT /P <>BDC ( )Tj ( )Tj BT -.02 Tc 7 0 0 7 354.6933 507.7654 Tm /P <>BDC 0 Tc BT 7 0 0 7 491.392 672.9528 Tm BT ET ( )Tj BT 7 0 0 7 440.0906 342.9528 Tm 7 0 0 7 492.5963 573.7654 Tm [(737-900E)-33(R)]TJ 7 0 0 7 314.6398 540.7654 Tm ET [(Seat configur)10(ation)]TJ /P <>BDC ( )Tj ET (The performance improvement in the)Tj (CFM56-5B4/P)Tj BT ET ET 7 0 0 7 387.0932 100.9528 Tm EMC 6.5 0 0 6.5 549.8557 585.9529 Tm 7 0 0 7 108.6215 441.9528 Tm /P <>BDC [(737-900E)-33(R)]TJ BT What makes the newest 747 Jumbo tick? ET ET BT ET /P <>BDC EMC EMC EMC (175,047)Tj 9 0 0 9 544.8128 412.8898 Tm EMC EMC 9 0 0 9 232.4408 687.8898 Tm /P <>BDC 7 0 0 7 141.7322 232.9528 Tm EMC ( )Tj BT 7 0 0 7 354.6933 441.7654 Tm EMC EMC 0 Tc ( )Tj BT EMC BT EMC BT /P <>BDC After /P <>BDC ET BT 9 0 0 9 53.8582 225.8898 Tm 7 0 0 7 338.3085 144.9528 Tm ET 8 0 0 8 366.8367 771.9528 Tm /P <>BDC EMC EMC ( )Tj BT EMC EMC EMC BT ( )Tj /P <>BDC BT EMC EMC 9 0 0 9 53.8338 258.8898 Tm /P <>BDC /P <>BDC BT /P <>BDC ( )Tj ET BT ET /P <>BDC EMC decrease the oxygen content to a level where the air volume (ullage) will not /P <>BDC (38,168)Tj /P <>BDC /P <>BDC (directly compare the fuel burn and)Tj 7 0 0 7 473.4744 518.9528 Tm EMC 9 0 0 9 215.4409 423.8898 Tm BT ET 7 0 0 7 247.7395 188.7654 Tm 6 0 0 6 506.5237 757.9528 Tm ET BT BT /P <>BDC EMC BT BT BT /P <>BDC 9 0 0 9 206.7178 181.8898 Tm (737-9)Tj BT ET BT 7 0 0 7 520.6108 617.9528 Tm BT EMC BT [(AIRL)8.1(INE & AIR)7.1(CRAF)-12.9(T)18.1( OPERA)56.9(T)-8.1(ION)-13.9(S)]TJ BT 0 Tc BT ( )Tj BT 7 0 0 7 247.7395 507.7654 Tm /P <>BDC 1 i ET S /P <>BDC EMC ( )Tj -.02 Tc EMC EMC )Tj ET ET ET BT 9 0 0 9 394.0315 82.8898 Tm ET (method of operation that balances the cost)Tj BT (analysis are: an MTOW of 213,848lbs; an)Tj /GS1 gs /P <>BDC EMC -.02 Tc q /P <>BDC EMC /P <>BDC ET 0 Tc 6.5 0 0 6.5 381.6589 624.9529 Tm /P <>BDC /F6 1 Tf 7 0 0 7 404.101 309.7654 Tm (at 27,000lbs thrust compared to the)Tj (2,313)Tj /P <>BDC ET ET /P <>BDC ( )Tj BT ET -.02 Tc 9 0 0 9 394.0315 346.8898 Tm 9 0 0 9 172.0312 357.8898 Tm BT BT EMC /P <>BDC BT ( )Tj BT 7 0 0 7 54.7071 716.7654 Tm /P <>BDC ET /P <>BDC BT 7 0 0 7 473.8245 177.9528 Tm 6 0 0 6 381.7993 757.9528 Tm BT BT BT 9 0 0 9 175.0911 269.8898 Tm ( )Tj ET ( )Tj /P <>BDC ET 7 0 0 7 241.2727 265.9528 Tm BT 9 0 0 9 368.9994 225.8898 Tm ET (CFM56-7B27B3)Tj Since development and production Boeing has built 10,574 737-800s. 9 0 0 9 51.0315 324.8898 Tm 9 0 0 9 36.8504 49.8898 Tm EMC (193,344)Tj 0 Tc ET 505.325 82.247 l BT There are many variants of the 737. BT ET ( )Tj /P <>BDC 0 Tc 7 0 0 7 279.1575 188.9528 Tm EMC BT 0 Tc 7 0 0 7 379.3969 166.7654 Tm ET EMC BT BT BT EMC ET 7 0 0 7 277.3936 364.9528 Tm BT EMC 7 0 0 7 125.6292 540.7654 Tm /P <>BDC /P <>BDC BT BT -.01 Tc EMC 0 Tc 8 0 0 8 355.1264 760.7654 Tm /P <>BDC 9 0 0 9 375.9258 49.8898 Tm 7 0 0 7 99.8582 166.7654 Tm 7 0 0 7 491.7142 463.7654 Tm BT 9 0 0 9 425.1967 720.8898 Tm EMC Boeing 797, MNA-6x and MNA-7x. EMC EMC ET /P <>BDC EMC /P <>BDC /P <>BDC BT 9 0 0 9 541.1655 478.8898 Tm ( )Tj 9 0 0 9 232.4217 390.8898 Tm EMC 9 0 0 9 418.1167 335.8898 Tm EMC EMC /P <>BDC /P <>BDC ET 0 Tc /P <>BDC EMC 7 0 0 7 354.6933 639.7654 Tm 7 0 0 7 430.039 705.9528 Tm BT (37,416)Tj (the CFM56-5B with thrust ratings of)Tj BT 0 Tc BT EMC ET (11,593)Tj BT [(AIRL)8.1(INE & AIR)7.1(CRAF)-12.9(T)18.1( OPERA)56.9(T)-8.1(ION)-13.9(S)]TJ 7 0 0 7 445.619 408.7654 Tm Perhaps somebody has experience in shipment of landing gear. ET EMC ET 8 0 0 8 275.1912 745.9528 Tm EMC /P <>BDC 7 0 0 7 490.5101 540.9528 Tm EMC /P <>BDC EMC 7 0 0 7 182.5706 672.9528 Tm ET -.02 Tc 6.5 0 0 6.5 276.4014 598.9529 Tm ET 9 0 0 9 365.7772 467.8898 Tm BT /Artifact <>BDC ET ( )Tj /P <>BDC EMC /P <>BDC ET 7 0 0 7 107.1165 474.9528 Tm ET /P <>BDC 9 0 0 9 373.1937 357.8898 Tm ( )Tj /P <>BDC (737-800:)Tj BT (170)Tj -.02 Tc .023 .567 .626 rg EMC ( A)Tj ET BT ET EMC (0.0140)Tj /P <>BDC ( )Tj EMC ET 7 0 0 7 457.0984 683.7654 Tm ET EMC EMC /P <>BDC EMC EMC ( )Tj -.02 Tc BT ( )Tj ( )Tj [(MR)32(TX - lbs)]TJ ET 0 Tc BT ET 9 0 0 9 505.9653 115.8898 Tm 0 Tc ( )Tj (-47)Tj BT 8 0 0 8 158.74 760.7654 Tm /P <>BDC /P <>BDC (block fuel burn performance of up to)Tj 0 Tc as shown at the top of the page. BT (powered by either the CFM56-5 series or)Tj /P <>BDC EMC /P <>BDC /P <>BDC BT /P <>BDC 0 Tc -.02 Tc ET /F7 1 Tf BT ET 6 0 0 6 340.4597 743.9528 Tm ET 9 0 0 9 179.7604 159.8898 Tm ET 9 0 0 9 408.1968 159.8898 Tm EMC 9 0 0 9 68.3339 500.8898 Tm EMC 9 0 0 9 369.892 412.8898 Tm 7 0 0 7 179.5605 518.9528 Tm ( )Tj ET (hour and per mile reduces . ET BT EMC BT ET ( )Tj ET 6 0 0 6 164.6501 715.9528 Tm ET /P <>BDC /P <>BDC ET BT /P <>BDC -.01 Tc (impact on the fuel cost per ASM. 0 Tc ( )Tj /P <>BDC /P <>BDC ET 7 0 0 7 247.7395 177.7654 Tm BT ( )Tj BT BT BT 8 0 0 8 394.0157 786.8898 Tm BT /P <>BDC BT 6.5 0 0 6.5 128.6016 558.9529 Tm /P <>BDC /P <>BDC ( )Tj ET 7 0 0 7 337.6855 529.9528 Tm -.02 Tc 0 Tc BT EMC ET ET BT -.02 Tc BT ( )Tj BT BT ( )Tj 7 0 0 7 54.5916 540.7654 Tm ET BT ET -.02 Tc BT BT EMC EMC ( )Tj ET ET ( )Tj BT 7 0 0 7 554.7883 342.7654 Tm BT BT ET 0 Tc EMC BT EMC ET 7 0 0 7 338.5674 133.9528 Tm ET /P <>BDC 9 0 0 9 36.8504 104.8898 Tm BT (or scenarios in this study. /P <>BDC BT 9 0 0 9 36.8583 335.8898 Tm EMC /P <>BDC 0 Tc -.02 Tc BT EMC -.02 Tc ET 9 0 0 9 194.061 324.8898 Tm /P <>BDC ( )Tj (31,416)Tj 6.5 0 0 6.5 398.3298 650.9529 Tm /P <>BDC BT ET ET EMC -.02 Tc EMC 6.5 0 0 6.5 181.2003 532.9529 Tm EMC /P <>BDC 9 0 0 9 526.8813 445.8898 Tm EMC /P <>BDC ( )Tj 6.5 0 0 6.5 324.4345 689.9529 Tm (ratio of 5.1:1. 9 0 0 9 213.7526 258.8898 Tm EMC cumulative errors it is recommended that the wings are filled once every few The Boeing 737-800 is a twin-engined short-to-medium-range narrowbody airliner with a capacity of maximum 189 passengers produced by the American manufacturer Boeing Commercial Airplanes. BFE; . 9 0 0 9 204.4018 665.8898 Tm EMC 7 0 0 7 320.7537 78.9528 Tm 9 0 0 9 430.7427 687.8898 Tm 7 0 0 7 125.6292 441.7654 Tm -.01 Tc BT EMC /P <>BDC /P <>BDC EMC (series of aircraft benefits from increased)Tj ET EMC /P <>BDC ( )Tj ET 300.229 562.194 m 8 0 0 8 225.1837 633.9528 Tm BT 9 0 0 9 565.9882 214.8898 Tm /P <>BDC 7 0 0 7 230.7317 419.9528 Tm EMC /P <>BDC (operations, the block times would be)Tj /Artifact <>BDC (0.0130)Tj EMC EMC (39,270)Tj 9 0 0 9 534.3536 577.8898 Tm ET EMC 9 0 0 9 215.4409 379.8898 Tm /F6 1 Tf BT BT ( )Tj EMC ET ET ( )Tj 7 0 0 7 82.8504 232.9528 Tm ET 8 0 0 8 365.7704 633.9528 Tm ( )Tj 6.5 0 0 6.5 347.0329 532.9529 Tm BT BT ( )Tj /P <>BDC 7 0 0 7 490.8321 386.7654 Tm 9 0 0 9 36.8504 467.8898 Tm 7 0 0 7 456.7412 661.7654 Tm /P <>BDC )Tj 0 Tc EMC (152)Tj BT .559 .331 .619 rg ( )Tj EMC ( )Tj EMC 10 0 0 10 49.3644 814.1973 Tm (economy-plus seats typically offer two to)Tj /P <>BDC /P <>BDC ET BT /TT2 1 Tf ET -.015 Tc BT /P <>BDC EMC /P <>BDC ( C)Tj /P <>BDC 9 0 0 9 515.9449 654.8898 Tm /P <>BDC (1,690)Tj /P <>BDC 0 Tc ET BT (aim was remove this variability from the)Tj (141,270)Tj 0 Tc BT ET BT (same passenger payload. [(R)13.9(ange with full)]TJ ET /P <>BDC ( )Tj BT ET BT ET (1,272)Tj BT tanks into the centre tank where it is then fed to the engines in the normal /P <>BDC 0 Tc 8 0 0 8 542.9269 786.8898 Tm 7 0 0 7 427.7291 320.9528 Tm 7 0 0 7 518.4953 100.9528 Tm (0.0111)Tj 9 0 0 9 170.626 357.8898 Tm /P <>BDC EMC ET BT ET EMC -.02 Tc /GS2 gs EMC /P <>BDC /P <>BDC BT BT /P <>BDC . -.02 Tc 5.25 0 0 5.25 73.853 11.5132 Tm EMC BT /P <>BDC EMC EMC EMC [(737-900E)-33(R)]TJ /P <>BDC 0 Tc (2,220)Tj /P <>BDC EMC BT EMC ET EMC 9 0 0 9 367.9911 71.8898 Tm (900ER and 737-9, A320ceo and A320neo,)Tj (34,650)Tj /P <>BDC BT must be determined by using the. ( )Tj (City-pair)Tj -.01 Tc 6 0 0 6 496.2034 757.9528 Tm EMC /P <>BDC BT ET EMC BT EMC [(BOS-SE)-13.9(A)]TJ /P <>BDC ( )Tj BT 7 0 0 7 387.0932 375.9528 Tm ( )Tj /P <>BDC 7 0 0 7 241.5317 584.9528 Tm ( )Tj [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ 7 0 0 7 187.0858 133.9528 Tm ( )Tj /P <>BDC ET /P <>BDC 7 0 0 7 440.3636 518.9528 Tm /P <>BDC EMC 7 0 0 7 131.6494 375.7654 Tm -.02 Tc 7 0 0 7 469.2222 11.5129 Tm ET 9 0 0 9 548.2598 489.8898 Tm ET EMC /P <>BDC BT BT EMC 7 0 0 7 179.5605 320.9528 Tm EMC Q /P <>BDC ET /P <>BDC Cheers Peter, Pingback:Is Covid-19 isolation an opportunity to learn to fly? BT BT (weights used are an MTOW of)Tj ET ET BT 9 0 0 9 232.438 126.8898 Tm /P <>BDC /P <>BDC ( )Tj /P <>BDC 0 Tc -.01 Tc BT 7 0 0 7 99.8582 683.7654 Tm -.02 Tc /P <>BDC EMC ET W* n /P <>BDC /GS1 gs 7 0 0 7 297.632 507.9528 Tm 7 0 0 7 380.2788 639.7654 Tm /P <>BDC (977)Tj EMC /P <>BDC The fuel flow indication is integrated over time to calculate the fuel used for each engine. ( )Tj ET ET EMC /P <>BDC -.01 Tc BT 9 0 0 9 394.0237 346.8898 Tm BT EMC must be determined by using the dripsticks (floatsticks 7 0 0 7 258.2805 111.7654 Tm (5,395)Tj EMC EMC 0 Tc 7 0 0 7 297.632 518.9528 Tm (0.0120)Tj -.02 Tc 7 0 0 7 439.2087 320.9528 Tm BT 9 0 0 9 205.7907 236.8898 Tm -.02 Tc 0 841.89 609.449 -841.89 re It sounds like you have a bit of a project on your hands. ( )Tj EMC EMC S 7 0 0 7 554.7883 375.7654 Tm 7 0 0 7 338.6433 166.7654 Tm EMC BT ET (other seven aircraft types. /P <>BDC ET -.02 Tc BT EMC /P <>BDC ET 0 Tc EMC ET ( )Tj /F1 1 Tf 0 Tc EMC /P <>BDC /P <>BDC EMC /P <>BDC ( )Tj ET EMC EMC this question can have so many answers depending on the conditions, such as weight, air density, required speed etc. 9 0 0 9 394.0315 786.8898 Tm ET ET ET BT EMC ( )Tj ET -.01 Tc 7 0 0 7 241.5317 243.9528 Tm -.02 Tc ET BT BT ( )Tj ( )Tj EMC /P <>BDC /P <>BDC EMC BT ET /P <>BDC ( )Tj ET (A320ceo, A320neo, 737-800 & 737-8;)Tj /P <>BDC /P <>BDC ( )Tj /P <>BDC /P <>BDC 7 0 0 7 491.7142 562.7654 Tm ( )Tj 0 Tc 9 0 0 9 232.438 324.8898 Tm /F1 1 Tf 9 0 0 9 532.5876 137.8898 Tm BT EMC BT /P <>BDC ET EMC -.02 Tc (310,080)Tj BT 7 0 0 7 158.74 496.7654 Tm 0 Tc 7 0 0 7 508.4124 221.7654 Tm BT ET 7 0 0 7 387.0932 221.9528 Tm ( )Tj EMC 6 0 0 6 246.6462 743.9528 Tm EMC 0 Tc ET EMC 6.5 0 0 6.5 379.0655 585.9529 Tm (This is chosen to represent a typical airline)Tj EMC EMC [(737-900E)-33(R)]TJ (CFM56-)Tj EMC re-primed. /P <>BDC BT ET (operationally safe to do so, in the)Tj EMC /P <>BDC BT EMC ET 7 0 0 7 294.4014 639.7654 Tm ET EMC EMC /P <>BDC EMC 7 0 0 7 387.0932 111.9528 Tm EMC 0 Tc BT ( )Tj ET /P <>BDC 9 0 0 9 36.8504 159.8898 Tm ET ( )Tj BT 0 Tc EMC ET BT (fuel consumption and cost per seat or per)Tj BT (I)Tj 7 0 0 7 446.5009 672.7654 Tm ( )Tj 7 0 0 7 279.1575 298.9528 Tm EMC -.01 Tc ET .0081 Tc EMC EMC BT ET (Boeing aircraft, the 737-800 has a 2.5%)Tj 8 0 0 8 365.7704 675.9528 Tm 9 0 0 9 232.4217 93.8898 Tm (737-800W)Tj EMC EMC BT EMC 7 0 0 7 241.5317 188.9528 Tm /P <>BDC ET ( )Tj ET BT ET /P <>BDC BT 7 0 0 7 491.7142 276.7654 Tm 7 0 0 7 490.5101 716.9528 Tm BT EMC W* n 9 0 0 9 369.406 104.8898 Tm (166-175)Tj (156)Tj EMC (achieved more than 6,000 orders for the)Tj EMC /P <>BDC W n 9 0 0 9 212.5107 313.8898 Tm ET ET ( )Tj 544,000 lbs 246,754 Kg: Maximum Fuel Capacity: 48,445 US Gal. BT /P <>BDC ET /F6 1 Tf EMC ET 7 0 0 7 279.1575 232.9528 Tm 7 0 0 7 107.1165 463.9528 Tm (aircraft types: the A320ceo, A321ceo,)Tj 6 0 0 6 459.5796 729.9528 Tm EMC 0 Tc EMC BT ET /P <>BDC upon how many tanks the customer has specified (max 12). /P <>BDC EMC /Artifact <>BDC BT (1,824)Tj EMC 9 0 0 9 365.1022 170.8898 Tm BT EMC EMC /P <>BDC /F7 1 Tf EMC 0 Tc /P <>BDC EMC EMC ( )Tj /GS1 gs ET 7 0 0 7 294.4014 331.7654 Tm ET /P <>BDC EMC ET ET BT BT EMC 9 0 0 9 408.1854 346.8898 Tm EMC EMC EMC 8 0 0 8 471.0755 760.9528 Tm BT (737-9)Tj EMC /P <>BDC /P <>BDC BT ET ET ( )Tj BT EMC ET -.02 Tc ( )Tj ( )Tj ( )Tj /P <>BDC BT (superior fuel burn per seat-mile of all)Tj ET 7 0 0 7 131.6494 276.7654 Tm 7 0 0 7 491.7142 529.7654 Tm [(AS)29(M)]TJ 9 0 0 9 563.0415 775.8898 Tm /F6 1 Tf 0 Tc -.02 Tc /P <>BDC 9 0 0 9 213.7241 467.8898 Tm ET EMC BT 0 Tc W n ET EMC 9 0 0 9 203.1969 566.8898 Tm [(737 M)-8.1(A)-24.9(X-9:)]TJ ( )Tj BT 7 0 0 7 519.3773 265.9528 Tm 6 0 0 6 215.4988 701.9528 Tm BT 9 0 0 9 232.4408 731.8898 Tm 7 0 0 7 141.7322 474.9528 Tm 7 0 0 7 37.0536 507.9528 Tm ET BT EMC q /P <>BDC BT My Dad was a captain and I am curious if he flew the Flt 800 aircraft or not. EMC EMC EMC ( )Tj BT ET -.02 Tc ET 7 0 0 7 230.7317 584.9528 Tm 7 0 0 7 404.101 342.7654 Tm /P <>BDC ( )Tj /P <>BDC -.01 Tc EMC (1,089)Tj And I hope I will get some good stuff to post it to you. /P <>BDC BT BT ET EMC EMC /P <>BDC BT ( )Tj 7 0 0 7 158.74 485.7654 Tm EMC EMC BT 0 Tc 6 0 0 6 61.517 687.9528 Tm ET /P <>BDC 9 0 0 9 394.0315 170.8898 Tm EMC EMC -.02 Tc 0 Tc following conditions: Takeoff with CSFF on the upper wing surfaces is EMC ET BT EMC BT (number of seats as the A320ceo; and the)Tj /P <>BDC /P <>BDC (190-199)Tj 0 Tc BT /P <>BDC EMC ET BT ( )Tj /P <>BDC /P <>BDC /P <>BDC ET (737-800W)Tj ( )Tj /P <>BDC EMC ET 7 0 0 7 294.4014 727.7654 Tm 0 Tc 6 0 0 6 246.7063 757.9528 Tm EMC /P <>BDC /P <>BDC BT BT /P <>BDC /P <>BDC 0 Tc BT BT BT ET In the 90s Boeing produced 80% of components in house including the wings, fuselage and tall assemblies. BT BT 9 0 0 9 36.8504 236.8898 Tm For the wheels, I will give you two measurements. ET (the A321neo offers a better fuel cost per)Tj EMC 7 0 0 7 518.4953 287.9528 Tm /P <>BDC (same cost index, and the method that each)Tj EMC BT (50,800)Tj 9 0 0 9 53.8578 148.8898 Tm ( )Tj (a 3.3% advantage for the A321neo on the)Tj 9 0 0 9 213.294 489.8898 Tm /P <>BDC /P <>BDC ET /P <>BDC ET (0.0134)Tj EMC BT ( )Tj BT (between 420nm and 2,429nm )Tj 0 Tc -.02 Tc -.5815 -.9071 l BT /P <>BDC ET 7 0 0 7 403.478 463.7654 Tm ET 9 0 0 9 394.0237 192.8898 Tm (The comparison of the two aircraft)Tj During cruise, the tolerance is less than 0.5%. ET EMC /P <>BDC Airbus A320 Assembly A truly international effort. )Tj EMC ET 7 0 0 7 521.4089 11.5132 Tm /P <>BDC EMC -.02 Tc ET EMC EMC ET ET ET ( )Tj EMC /P <>BDC BT 7 0 0 7 355.3163 188.7654 Tm ET BT ET 6 0 0 6 457.0716 687.9528 Tm ET 5.25 0 0 5.25 447.6106 11.5129 Tm ET 8 0 0 8 38.4438 745.9528 Tm EMC 9 0 0 9 566.9709 126.8898 Tm [(A3)24.9(21neo v)12.9(ersus 7)-33(3)8.1(7-9 )]TJ /P <>BDC ET BT As an Amazon Associate I earn from qualifying purchases. BT BT /P <>BDC BT (1,960)Tj (120-128)Tj EMC all the fuel required for priming which will render it inoperative even when the /P <>BDC Fuel Capacity 6,875 U.S. gal (26,020 L) Seat Pitch: 40 inches Premier World 32 inches Economy Max. EMC 0 Tc (number for the neo family. (152,800)Tj ET BT BT (The A320 and 737 families have been)Tj EMC 9 0 0 9 68.0071 566.8898 Tm EMC EMC ET /P <>BDC [(P)11(ayload)]TJ EMC /Artifact <>BDC (The fuel tank capacity means the)Tj /P <>BDC 7 0 0 7 365.035 628.9528 Tm EMC EMC ET BT ( )Tj BT (31,416)Tj BT ET EMC 9 0 0 9 568.555 82.8898 Tm 6 0 0 6 365.7265 729.9528 Tm EMC BT (149,300)Tj BT BT BT 9 0 0 9 394.0315 577.8898 Tm /P <>BDC ( )Tj 9 0 0 9 360.0909 115.8898 Tm BT (passenger payload - nm)Tj (minutes between aircraft types or 3.7% on)Tj ( )Tj /GS1 gs /P <>BDC ET /P <>BDC ET /P <>BDC -.02 Tc ET BT f /P <>BDC 7 0 0 7 82.2047 705.9528 Tm 9 0 0 9 36.8504 346.8898 Tm [(M)21(T)39.1(O)7.1(W)0( - lbs)]TJ 0 Tc ET 0 Tc permissible, provided the following are met: The standard number of fuel tanks is three. 8 0 0 8 64.6596 771.9529 Tm ( )Tj W n ET BT /P <>BDC ( )Tj 0 Tc ET (-62)Tj EMC /P <>BDC [(OM)8(M)-13(E)-25(R)7(C)8(E)]TJ 9 0 0 9 394.0315 357.8898 Tm 8 0 0 8 141.7322 760.9528 Tm /P <>BDC ET ET 9 0 0 9 534.0193 390.8898 Tm /P <>BDC /P <>BDC 0 Tc 7 0 0 7 95.225 11.5132 Tm -.02 Tc W n /P <>BDC ET ( )Tj (3,200)Tj (2,518)Tj /P <>BDC EMC /P <>BDC ET ET ET (the aircraft operator, but in this evaluation)Tj BT BT ( )Tj 9 0 0 9 358.9372 346.8898 Tm 7 0 0 7 199.5784 441.7654 Tm 9 0 0 9 393.5047 181.8898 Tm 7 0 0 7 37.6993 100.9528 Tm ( )Tj For this reason, a)Tj (- nm)Tj /P <>BDC EMC ET 9 0 0 9 53.8338 49.8898 Tm BT EMC 6 0 0 6 184.9964 757.9528 Tm EMC EMC 7 0 0 7 474.3564 617.9528 Tm -.02 Tc EMC /P <>BDC ET ET EMC The wheelbase which is the distance from the nosewheel to the line between the main wheels, which is 11.07 metres. BT /P <>BDC 7 0 0 7 196.5683 122.7654 Tm ET EMC [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ BT 7 0 0 7 279.1575 419.9528 Tm ET /P <>BDC ( )Tj /P <>BDC 304.725 420.96 m 7 0 0 7 387.0159 617.9528 Tm ( )Tj EMC ET /P <>BDC 7 0 0 7 387.0932 67.9528 Tm 9 0 0 9 232.438 445.8898 Tm 8 0 0 8 338.514 745.9528 Tm BT 0 Tc 0 Tc .406 .403 .405 rg -.02 Tc EMC BT 7 0 0 7 439.2087 364.9528 Tm EMC ET ( )Tj /P <>BDC ( )Tj ET EMC 8 0 0 8 158.74 771.7654 Tm EMC /P <>BDC /P <>BDC [(737 M)-8.1(A)-24.9(X-9:)]TJ BT Q /P <>BDC (1,824)Tj /P <>BDC EMC /P <>BDC ET 0 Tc FQIS accuracy: +/- 2.0% overall ET BT ET (A321neo)Tj -.02 Tc [(R)11(emaining car)13.9(go - lbs )]TJ BT BT ( )Tj /P <>BDC 0 Tc /P <>BDC (A higher engine bypass ratio will result)Tj EMC /P <>BDC /OC /MC4794 BDC 7 0 0 7 491.4046 309.9528 Tm 9 0 0 9 190.8053 247.8898 Tm ET [(B)-13.9(L)74(V/53)]TJ 9 0 0 9 388.0328 467.8898 Tm ( )Tj (ranges from 0.47 to 0.33 cents, and is)Tj 7 0 0 7 364.1531 584.9528 Tm BT EMC ET /F1 1 Tf ET -.02 Tc /P <>BDC /P <>BDC ET /P <>BDC EMC EMC ET ( )Tj ( )Tj /P <>BDC ET 8 0 0 8 365.7704 619.9528 Tm )Tj /P <>BDC BT BT BT /P <>BDC 6.5 0 0 6.5 549.8557 558.9529 Tm EMC 7 0 0 7 158.74 507.7654 Tm -.02 Tc EMC BT -.02 Tc ET ET EMC ET EMC ET 6.5 0 0 6.5 54.877 545.9529 Tm /P <>BDC EMC 6.5 0 0 6.5 244.2585 650.9529 Tm (table, page 19\))Tj (variant. 7 0 0 7 297.632 496.9528 Tm EMC 199,158 Litres: . 9 0 0 9 193.7007 236.8898 Tm ET ( )Tj EMC BT /P <>BDC ET BT 6 0 0 6 553.1396 687.9528 Tm (371,416)Tj ET EMC 7 0 0 7 179.5605 716.9528 Tm 9 0 0 9 376.7668 291.8898 Tm ET 7 0 0 7 508.4124 518.7654 Tm /P <>BDC EMC /P <>BDC BT BT BT EMC ( )Tj q 1 0 0 1 215.433 150.878 cm 0 0 m )Tj BT EMC EMC /P <>BDC /P <>BDC BT BT ET /P <>BDC /P <>BDC EMC ET ET ( )Tj 6.5 0 0 6.5 296.5232 585.9529 Tm 9 0 0 9 394.0315 302.8898 Tm fuel and de-ice the fuel filter. EMC BT /P <>BDC -.02 Tc ( )Tj ( )Tj /P <>BDC ET EMC )Tj /P <>BDC /P <>BDC (166,669)Tj BT BT /P <>BDC 0 Tc /P <>BDC /P <>BDC ET 6 0 0 6 138.6506 757.9528 Tm (2,040)Tj ET EMC EMC EMC ET /Artifact <>BDC /P <>BDC 7 0 0 7 387.0159 672.9528 Tm ET EMC BT 9 0 0 9 374.887 346.8898 Tm 9 0 0 9 369.4947 357.8898 Tm EMC BT -.02 Tc (191,240)Tj ET ET /P <>BDC 3.0566 -3.9073 l 7 0 0 7 520.6108 485.9528 Tm ET BT EMC EMC BT /P <>BDC (127 passengers on the longest sector,)Tj 7 0 0 7 54.7071 562.7654 Tm BT /P <>BDC ET 6.5 0 0 6.5 174.4663 735.9529 Tm EMC ( )Tj ET BT BT EMC BT ET (CFM56-5B3/P)Tj start a self test of the display and the fuel quantity indicating system. /P <>BDC 0 Tc ET 8 0 0 8 370.117 771.9529 Tm [(Aircr)10(aft types )]TJ -.02 Tc 9 0 0 9 411.0234 753.8898 Tm 0 Tc /P <>BDC 0 Tc ET 9 0 0 9 545.1909 346.8898 Tm /P <>BDC ET 0 Tc 7 0 0 7 520.6108 496.9528 Tm EMC /P <>BDC ( )Tj (A320ceo)Tj 7 0 0 7 456.2165 342.7654 Tm ET /P <>BDC BT ET BT BT BT ( )Tj EMC BT /P <>BDC BT BT ( )Tj EMC 0 Tc EMC 7 0 0 7 491.7142 518.7654 Tm ( )Tj Airbus A320 Specs What is behind one of the most popular short-haul airliners? 7 0 0 7 491.7142 694.7654 Tm EMC ( )Tj W n ET EMC (0.0137)Tj 7 0 0 7 554.7883 463.7654 Tm 9 0 0 9 51.0236 60.8898 Tm EMC (The A320ceo, A321ceo and 737-)Tj EMC 7 0 0 7 439.2087 397.9528 Tm -.01 Tc /P <>BDC EMC (1,581)Tj BT BT 7 0 0 7 124.1242 694.7654 Tm ET (178)Tj BT -.02 Tc /P <>BDC BT /P <>BDC BT BT ( )Tj EMC ET (450,780)Tj (PPS flight planning software is used to)Tj ET ET /P <>BDC /P <>BDC EMC ( )Tj /P <>BDC /P <>BDC BT /P <>BDC BT /P <>BDC 0 Tc 304.725 420.96 m EMC ( )Tj /P <>BDC ET /P <>BDC 6.5 0 0 6.5 243.4784 585.9529 Tm EMC ( )Tj BT BT 8 0 0 8 319.1147 771.9528 Tm 5.25 0 0 5.25 100.8225 11.5132 Tm EMC -.02 Tc ET 7 0 0 7 338.6433 408.7654 Tm ET (18.3% on the sectors where an equivalent)Tj EMC BT BT /P <>BDC BT (increases to an average of 3.3% for the)Tj /P <>BDC Q operation, centre tank pumps must be not be positioned to ON, unless BT (163)Tj BT ( )Tj ( )Tj Note: The gauges are still considered to be operating normally with 9 0 0 9 191.4329 786.8898 Tm 9 0 0 9 367.0732 423.8898 Tm EMC /P <>BDC BT /P <>BDC 6.5 0 0 6.5 54.877 637.9529 Tm EMC EMC EMC (1,825)Tj ( )Tj /F4 1 Tf ( )Tj BT BT EMC ET BT BT EMC ET 7 0 0 7 258.2805 243.7654 Tm Delta Air Lines received the first Next-Gen 737 model with this brake package, a . ET (158)Tj /P <>BDC BT 8 0 0 8 505.7415 771.9528 Tm 7 0 0 7 298.514 584.9528 Tm ( )Tj EMC ET EMC -.02 Tc 9 0 0 9 53.8578 126.8898 Tm EMC ( )Tj 9 0 0 9 172.5802 467.8898 Tm /P <>BDC /GS1 gs 6.5 0 0 6.5 477.8064 702.9529 Tm -.02 Tc 13 0 0 13 36.8504 71.8898 Tm /P <>BDC EMC ET 7 0 0 7 387.0932 232.9528 Tm 0 Tc (. BT EMC ET EMC ET ET BT /P <>BDC ET ( )Tj EMC BT 7 0 0 7 108.6215 232.9528 Tm (page\))Tj ( )Tj BT ET (294)Tj ET EMC -.02 Tc BT EMC BT /F7 1 Tf 9 0 0 9 538.8793 368.8898 Tm EMC ( )Tj /P <>BDC BT /P <>BDC EMC ET ET BT /P <>BDC EMC /P <>BDC EMC EMC thanks for stopping by. S EMC 0 Tc EMC BT ( )Tj ET ( )Tj EMC /P <>BDC 7 0 0 7 445.619 727.7654 Tm 0 Tc /OC /MC828 BDC EMC 0 Tc ET /P <>BDC EMC 0 Tc .014984 841.89 609.45 -841.89 re ET endobj BT -.02 Tc EMC (141,757)Tj 6.5 0 0 6.5 64.6596 742.9529 Tm BT 9 0 0 9 207.0841 203.8898 Tm EMC 0 Tc ( )Tj /P <>BDC BT (25,160)Tj ( )Tj /P <>BDC ( )Tj ET BT BT /P <>BDC BT /P <>BDC /P <>BDC 8 0 0 8 136.4919 717.9528 Tm EMC ( )Tj 7 0 0 7 294.4014 562.7654 Tm ET EMC BT 7 0 0 7 187.0858 496.9528 Tm BT 9 0 0 9 166.7302 126.8898 Tm ( )Tj /GS1 gs BT EMC ET ET BT .559 .331 .619 rg ( )Tj BT /P <>BDC [(7)-33(3)8.1(7-900ER & 7)-33(3)8.1(7-9 )]TJ (483)Tj ET Airbus seals the deal to reinvigorate the QANTAS Fleet. 0 Tc /P <>BDC BT EMC BT BT ( )Tj /P <>BDC /P <>BDC 9 0 0 9 53.8582 214.8898 Tm /P <>BDC 10 0 0 10 417.91 814.1973 Tm 5.25 0 0 5.25 549.1047 11.5132 Tm 6.5 0 0 6.5 285.7159 611.9529 Tm ( )Tj ET EMC ( )Tj /P <>BDC -.01 Tc 7 0 0 7 37.0536 727.9528 Tm ET ET 9 0 0 9 215.4409 478.8898 Tm ET ( )Tj ET ET EMC BT /P <>BDC ET This)Tj EMC /P <>BDC ET (150)Tj ET BT /P <>BDC ET 9 0 0 9 546.9705 291.8898 Tm EMC ET 0 Tc /P <>BDC BT /P <>BDC 9 0 0 9 394.0237 500.8898 Tm 6 0 0 6 55.0668 687.9528 Tm 0 Tc (2,498)Tj BT /P <>BDC /P <>BDC ET ET BT -.02 Tc /P <>BDC /P <>BDC EMC ET /P <>BDC 7 0 0 7 230.7317 463.9528 Tm ( )Tj -.01 Tc ( )Tj 0 Tc BT 9 0 0 9 75.273 478.8898 Tm 7 0 0 7 490.5101 496.9528 Tm BT ( )Tj BT ET BT ET /P <>BDC ( )Tj ET /P <>BDC ( )Tj BT 7 0 0 7 439.8175 727.9528 Tm /P <>BDC EMC ET BT EMC ET -.02 Tc ET (1,454)Tj EMC [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ 0 Tc Boeing 737 Max, a new generation of this highly successful City Jet. 9 0 0 9 374.4497 214.8898 Tm (adsbygoogle = window.adsbygoogle || []).push({}); The web portal flugzeuginfo.net includes a comprehensive civil and military aircraft encyclopedia. EMC ( )Tj ( )Tj BT 6 0 0 6 89.371 673.9528 Tm EMC BT ET (I)Tj BT BT (A321neo)Tj /P <>BDC BT ET EMC (carried - lbs)Tj BT ET 9 0 0 9 75.273 500.8898 Tm /P <>BDC 9 0 0 9 550.3341 313.8898 Tm /P <>BDC BT EMC /P <>BDC ( )Tj (The A320ceo is payload-restricted to)Tj EMC BT BT BT ( )Tj /P <>BDC EMC [(In addition to lo)12(w)6.1(er fuel burn compar)10(ed to its)]TJ BT /P <>BDC 6 0 0 6 147.4588 729.9528 Tm /P <>BDC /P <>BDC q 1 0 0 1 53.834 601.878 cm 0 0 m ( )Tj ( )Tj The aux fuel The world's largest commercial airplane the Antanov AN-225 can carry over 98,000Gal/375,000 liters of fuel compared to a Beechcraft 1900D commuter airplane which carries 665Gal/2,520 liters. BT BT EMC ( )Tj -.02 Tc ( )Tj EMC 7 0 0 7 277.3936 562.9528 Tm EMC EMC )Tj 7 0 0 7 403.478 694.7654 Tm BT BT 9 0 0 9 552.6886 533.8898 Tm -.01 Tc ( )Tj EMC /P <>BDC /P <>BDC BT ET /P <>BDC ET EMC EMC ( )Tj EMC EMC .0161 Tc /P <>BDC ET ET 0 Tc EMC EMC EMC (6,353)Tj BT ET EMC BT EMC EMC 7 0 0 7 241.2727 661.9528 Tm (20/29/143, giving a maximum capacity of)Tj /P <>BDC /P <>BDC 9 0 0 9 469.5781 577.8898 Tm -.005 Tc /P <>BDC The total tolerance for the FQIS system is based on a full tank. /P <>BDC /P <>BDC (5.1:1)Tj W n BT BT EMC 7 0 0 7 82.8504 243.9528 Tm BT BT 5.25 0 0 5.25 447.6106 11.5129 Tm BT ET BT ET (150)Tj BT /P <>BDC ET EMC EMC /P <>BDC EMC (150)Tj ( )Tj 10 0 0 10 37.304 794.2914 Tm /P <>BDC ( )Tj 7 0 0 7 326.2278 518.9528 Tm -.02 Tc If AC power is available, select 0 Tc /P <>BDC BT 7 0 0 7 101.0963 386.9528 Tm EMC /P <>BDC EMC EMC EMC /F4 1 Tf (1,138)Tj 7 0 0 7 36.8504 155.9528 Tm EMC ET 6 0 0 6 527.6392 715.9528 Tm ET EMC ( )Tj (performance deterioration factor added to)Tj BT BT ( )Tj ET 7 0 0 7 537.7804 375.9528 Tm 7 0 0 7 491.7142 408.7654 Tm (170)Tj ET 6 0 0 6 254.6866 659.9528 Tm /P <>BDC -.02 Tc ET /P <>BDC /P <>BDC ET EMC /P <>BDC BT BT EMC ET /P <>BDC BT EMC EMC ET -.02 Tc 7 0 0 7 99.8582 628.7654 Tm EMC ET ET BT EMC EMC /P <>BDC EMC 7 0 0 7 258.2805 573.7654 Tm BT EMC ( )Tj ET EMC /P <>BDC ( )Tj ET BT 9 0 0 9 36.8504 170.8898 Tm EMC -.02 Tc ( )Tj ET ET 9 0 0 9 394.0123 621.8898 Tm /P <>BDC ET (same number of passengers is carried on)Tj /P <>BDC (Engine)Tj 7 0 0 7 82.2047 562.9528 Tm ET ET -.02 Tc [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ 9 0 0 9 530.4152 423.8898 Tm /P <>BDC .008 Tc /P <>BDC ET -.02 Tc ET BT These have led to smaller and)Tj https://simpleflying.com/how-aircraft-wings-are-made/, Your email address will not be published. ( )Tj 0 Tc ET ET EMC ( )Tj /P <>BDC /P <>BDC /P <>BDC ET /P <>BDC BT (166,090)Tj (150)Tj ET 7 0 0 7 230.7317 716.9528 Tm 9 0 0 9 215.4409 357.8898 Tm )Tj ET -.02 Tc EMC EMC EMC ( )Tj /P <>BDC /P <>BDC (CFM56-7B27B3)Tj EMC endstream BT 6 0 0 6 106.1775 729.9528 Tm /P <>BDC BT ET /P <>BDC BT EMC ET ET (alternates used and their distance from the)Tj ET (CFM56-5B4/P)Tj ET Best of luck. 0 Tc /P <>BDC /P <>BDC /P <>BDC ( )Tj ET BT EMC -.02 Tc /P <>BDC ( )Tj /P <>BDC EMC 7 0 0 7 456.2165 199.7654 Tm (170)Tj 7 0 0 7 297.632 694.9528 Tm (70)Tj ( )Tj EMC /P <>BDC EMC -.02 Tc ( )Tj /P <>BDC /P <>BDC EMC My simulation is focused on postcrash fires. 9 0 0 9 411.0097 170.8898 Tm EMC q ET ET EMC 9 0 0 9 368.3979 38.8898 Tm EMC ( )Tj 6 0 0 6 465.9579 659.9528 Tm ET /P <>BDC ET /F7 1 Tf (capacity, so that payload is reduced to)Tj /P <>BDC ( )Tj ( )Tj 9 0 0 9 377.4407 764.8898 Tm 0 Tc EMC 9 0 0 9 394.0315 599.8898 Tm EMC /P <>BDC ET /P <>BDC EMC ET BT ET BT 7 0 0 7 37.6993 265.9528 Tm BT 8 0 0 8 124.845 717.9528 Tm 0 Tc ( )Tj 7 0 0 7 445.619 628.7654 Tm (-55)Tj /P <>BDC .151 .147 .15 rg /P <>BDC ET EMC /GS2 gs 7 0 0 7 60.6117 540.7654 Tm 7 0 0 7 326.2278 507.9528 Tm /P <>BDC 7 0 0 7 241.5317 298.9528 Tm BT 7 0 0 7 354.6933 375.7654 Tm /P <>BDC -.01 Tc ( )Tj /P <>BDC EMC BT ( )Tj 9 0 0 9 411.0181 258.8898 Tm ET /P <>BDC EMC EMC BT (163)Tj BT BT ( )Tj ET EMC ( )Tj /F6 1 Tf EMC ET ET ET <>stream (0.0134)Tj 6.5 0 0 6.5 480.4 650.9529 Tm BT ( A)Tj 9 0 0 9 394.0123 181.8898 Tm EMC 0 Tc (comparison more challenging. BT ET 0 841.89 609.449 -841.89 re /P <>BDC BT 0 J 0 j .5 w 10 M [] 0 d /P <>BDC EMC 0 Tc BT ET EMC /P <>BDC EMC /P <>BDC EMC 9 0 0 9 374.3633 401.8898 Tm (31,416)Tj 7 0 0 7 204.0935 485.7654 Tm The A320ceo and)Tj ET ( )Tj ET BT EMC tank is refuelled. ET 7 0 0 7 490.8321 100.7654 Tm BT )Tj ET -4.2575 -4.8278 -4.5158 -4.0295 -4.515 -3.0604 c ET -.02 Tc ET ( )Tj ( )Tj ( )Tj BT (compared to the CFM56-7B-powered 737-)Tj 8 0 0 8 315.034 760.7654 Tm /P <>BDC 7 0 0 7 108.6215 67.9528 Tm /P <>BDC BT ET /P <>BDC 7 0 0 7 444.737 210.7654 Tm EMC ET (4,163)Tj EMC (CFM56-7B27B3)Tj BT /P <>BDC 7 0 0 7 82.2047 540.9528 Tm 7 0 0 7 82.2047 661.9528 Tm ET BT /P <>BDC EMC 7 0 0 7 554.7883 628.7654 Tm /P <>BDC /P <>BDC BT .014984 824.882 572.583 17.008 re 9 0 0 9 36.8583 456.8898 Tm EMC 9 0 0 9 181.5424 71.8898 Tm ET (216)Tj /P <>BDC ET EMC EMC 10 0 0 10 48.9263 771.9528 Tm EMC EMC EMC EMC BT 137 )Tj (832)Tj EMC 9 0 0 9 183.3893 456.8898 Tm EMC BT -.02 Tc 9 0 0 9 568.1771 115.8898 Tm (the engine option chosen for this study is)Tj EMC /P <>BDC -.02 Tc EMC EMC /P <>BDC ( )Tj /P <>BDC Q -.015 Tc 5.25 0 0 5.25 40.8474 11.5129 Tm 9 0 0 9 53.8582 709.8898 Tm /P <>BDC ET 9 0 0 9 566.5209 379.8898 Tm
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