ET EMC EMC BT 8 0 0 8 332.978 577.9528 Tm ET /P <>BDC ET BT 9 0 0 9 376.7938 500.8898 Tm 6 0 0 6 269.4048 687.9528 Tm (35,112)Tj EMC ET ( )Tj ( )Tj -.01 Tc EMC EMC -.02 Tc ET /OC /MC5078 BDC 9 0 0 9 215.4409 489.8898 Tm BT 0 Tc EMC /P <>BDC 0 Tc ET 0 Tc 7 0 0 7 141.7322 408.9528 Tm /P <>BDC ET /P <>BDC EMC 7 0 0 7 338.6433 342.7654 Tm BT /P <>BDC BT (A321ceo)Tj (2,517)Tj (\(see table, page 19\))Tj EMC EMC 7 0 0 7 474.7064 276.9528 Tm /P <>BDC 7 0 0 7 247.7395 628.7654 Tm BT BT 5.25 0 0 5.25 40.8474 11.5129 Tm ( )Tj 7 0 0 7 279.1575 331.9528 Tm . -.02 Tc ET (Flight time - mins)Tj EMC 7 0 0 7 230.7317 397.9528 Tm ( )Tj ET EMC 9 0 0 9 394.0123 324.8898 Tm 7 0 0 7 141.7322 364.9528 Tm BT BT BT 7 0 0 7 338.6433 199.7654 Tm /P <>BDC /GS2 gs 0 Tc EMC EMC BT ET BT BT EMC EMC EMC 7 0 0 7 444.737 232.7654 Tm ET BT ( )Tj EMC 7 0 0 7 337.6855 221.9528 Tm (compare the aircraft types on a fair or)Tj /P <>BDC ( )Tj EMC EMC ( )Tj /P <>BDC 9 0 0 9 394.0237 335.8898 Tm ( )Tj EMC ET ( )Tj /P <>BDC Even an empty tank has some unusable fuel ( )Tj /P <>BDC EMC /Artifact <>BDC EMC /P <>BDC ET 9 0 0 9 215.4409 192.8898 Tm 7 0 0 7 99.8582 309.7654 Tm BT (39,270lbs)Tj 0 Tc 7 0 0 7 366.0641 705.9528 Tm 0 Tc /P <>BDC ET BT ( )Tj ET (737-9)Tj ( )Tj The engine option used in this)Tj [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ EMC 0 Tc ( )Tj 7 0 0 7 337.9444 639.9528 Tm 8 0 0 8 551.3604 71.8898 Tm /P <>BDC The APU uses fuel from the number 1 tank. EMC /P <>BDC 7 0 0 7 491.7142 628.7654 Tm /GS2 gs ET BT 7 0 0 7 99.8582 276.7654 Tm ET BT ET EMC /P <>BDC EMC /P <>BDC 9 0 0 9 53.8582 60.8898 Tm (CFM56-)Tj 0 Tc -.01 Tc /P <>BDC /P <>BDC BT /P <>BDC EMC It is understood)Tj /P <>BDC /P <>BDC ET BT /P <>BDC EMC ET ET ET /P <>BDC 7 0 0 7 337.4684 661.9528 Tm /P <>BDC BT ET (with 2,000 feet separation. 0 Tc /P <>BDC (financing. ET /P <>BDC BT BT /P <>BDC EMC 7 0 0 7 86.3128 540.7654 Tm BT BT ET /P <>BDC /P <>BDC (comparison of the performance of the eight)Tj EMC 0 Tc ( )Tj /P <>BDC ( )Tj ( )Tj 9 0 0 9 381.9109 456.8898 Tm ( )Tj (34,650)Tj ET EMC ET The 800 is mainly used for passenger transport with its 526 seating capacity. BT EMC ET (150)Tj 7 0 0 7 82.2047 694.9528 Tm EMC 6.5 0 0 6.5 448.4195 722.9529 Tm ET (737-800W)Tj ET ET ET ET ET ET BT -.02 Tc )Tj BT ET [(CFM L)17.1(E)-8.1(AP-1A26)]TJ EMC /P <>BDC EMC )Tj BT 0 Tc BT ( )Tj ET BT [(trip fuel burn compar)10(ed to the 737-800. ( )Tj 7 0 0 7 204.0935 408.7654 Tm BT (with a thrust rating of 27,000lbs, an intake)Tj EMC 0 Tc ( )Tj ( )Tj ( )Tj 0 Tc EMC BT ET BT -.02 Tc BT BT /P <>BDC /P <>BDC EMC ( )Tj ( )Tj ( )Tj EMC ET BT 7 0 0 7 383.0719 672.7654 Tm BT BT /P <>BDC ET BT /P <>BDC /P <>BDC 7 0 0 7 338.5674 133.9528 Tm /P <>BDC EMC 9 0 0 9 516.4593 412.8898 Tm 9 0 0 9 445.6725 302.8898 Tm /P <>BDC ET /P <>BDC ET EMC ET /P <>BDC You could support me with that. /P <>BDC /P <>BDC ET 9 0 0 9 53.8338 60.8898 Tm ET EMC 9 0 0 9 348.3267 324.8898 Tm ( )Tj 7 0 0 7 230.7317 331.9528 Tm BT 6 0 0 6 403.6028 743.9528 Tm /P <>BDC /P <>BDC ET 9 0 0 9 394.0237 511.8898 Tm ET 9 0 0 9 362.3229 313.8898 Tm 7 0 0 7 321.6356 243.9528 Tm ( )Tj ET /P <>BDC /P <>BDC 7 0 0 7 241.5317 210.9528 Tm ET ( )Tj 7 0 0 7 321.6356 287.9528 Tm 9 0 0 9 215.4409 456.8898 Tm 0 Tc ( )Tj endobj BT ET /P <>BDC EMC BT /P <>BDC ( 2021)Tj BT (. 0 Tc /P <>BDC ET 9 0 0 9 206.8767 148.8898 Tm ET 0 Tc BT /P <>BDC /P <>BDC -.02 Tc ( )Tj BT (68.3 inches and a bypass ratio of up to)Tj ET ET 9 0 0 9 542.2972 203.8898 Tm /P <>BDC /P <>BDC 9 0 0 9 215.4313 148.8898 Tm BT ET BT ET ET EMC EMC /P <>BDC BT [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ Q 0 Tc /P <>BDC EMC 9 0 0 9 53.8582 654.8898 Tm 9 0 0 9 232.438 456.8898 Tm 13 0 0 13 127.1464 456.8898 Tm -.02 Tc ( )Tj next aircraft -.01 Tc ( )Tj ET BT 6 0 0 6 277.7064 715.9528 Tm ( )Tj How an instrument landing system(ILS) can autoland aircraft. /P <>BDC -.01 Tc BT (483)Tj ET 6.5 0 0 6.5 121.1068 532.9529 Tm /P <>BDC ( )Tj Hi Jeffrey, ET EMC BT BT EMC ( )Tj 6.5 0 0 6.5 192.5726 722.9529 Tm /GS1 gs EMC The NGS is an onboard inert gas system that uses an 9 0 0 9 370.7977 236.8898 Tm ET 9 0 0 9 36.8504 126.8898 Tm -.02 Tc EMC ( )Tj ET 7 0 0 7 187.0858 661.9528 Tm ET ET ET 0 Tc /P <>BDC ET EMC 7 0 0 7 444.737 89.7654 Tm 19.843 0 l q /P <>BDC BT EMC BT BT /P <>BDC EMC -.02 Tc ET How much fuel do planes burn? EMC -.015 Tc (0.0123)Tj 0 Tc /P <>BDC 7 0 0 7 101.0963 408.9528 Tm ( )Tj BT EMC EMC EMC BT ET 9 0 0 9 345.8168 445.8898 Tm ET /P <>BDC ET 9 0 0 9 425.1913 214.8898 Tm EMC BT 6.5 0 0 6.5 397.7514 598.9529 Tm 8 0 0 8 275.1912 745.9528 Tm BT /P <>BDC 503.534 80.74 l ET EMC -.02 Tc 9 0 0 9 466.0881 203.8898 Tm 9 0 0 9 411.0181 456.8898 Tm 9 0 0 9 394.0123 203.8898 Tm BT BT /P <>BDC ET https://simpleflying.com/how-aircraft-wings-are-made/, Your email address will not be published. EMC ET BT ( )Tj ET (163)Tj EMC EMC EMC /P <>BDC -.02 Tc BT ( )Tj EMC /P <>BDC 9 0 0 9 53.8578 324.8898 Tm /P <>BDC 9 0 0 9 342.6025 368.8898 Tm (follow in their footsteps, having already)Tj 1 i 7 0 0 7 258.2805 419.7654 Tm BT The fuel flow indication is integrated over time to calculate the fuel used for each engine. EMC ( )Tj BT -.02 Tc BT EMC BT ET 7 0 0 7 37.0536 507.9528 Tm EMC (In this comparison the passenger seat)Tj /P <>BDC EMC [(Alternate airpor)-23(t &)]TJ 7 0 0 7 518.4953 320.9528 Tm ET EMC /P <>BDC EMC ET 7 0 0 7 326.2278 595.9528 Tm .534 .14 .504 RG -.02 Tc EMC 0 Tc ( )Tj ET BT EMC -.02 Tc BT BT BT ET /P <>BDC /P <>BDC [(A3)24.9(21ceo v)12.9(ersus A3)24.9(21neo )]TJ BT BT (original equipment manufacturer \(OEM\))Tj ET ET BT EMC BT /P <>BDC EMC ET BT ( )Tj ET /P <>BDC ( )Tj The westerly)Tj ( )Tj ( )Tj (273,600)Tj (737-8)Tj .151 .147 .15 rg EMC (A)Tj 0 Tc )Tj /P <>BDC BT BT BT 7 0 0 7 491.7142 595.7654 Tm ( )Tj 7 0 0 7 241.5317 639.9528 Tm BT ( )Tj ET ET EMC ET EMC EMC 7 0 0 7 487.0872 11.5129 Tm BT /P <>BDC 6 0 0 6 521.632 729.9528 Tm ( )Tj (stated maximum still air passenger range of)Tj ET (31,416)Tj BT /P <>BDC ET ( )Tj 8 0 0 8 107.2917 771.9528 Tm BT EMC (number of seats and ASMs will give an)Tj 9 0 0 9 394.0123 588.8898 Tm ( )Tj Cheers Peter. BT EMC Boeing uses Rockwell Collins avionics for the 737-800. 9 0 0 9 411.0181 357.8898 Tm 10 0 0 10 425.05 814.1973 Tm EMC EMC ET In comparison, the fuel cost per)Tj ET BT ( )Tj EMC ( )Tj ( )Tj EMC ( )Tj (1,060)Tj ( )Tj BT (capacity with slimmer seats, and cabin)Tj 9 0 0 9 196.1514 390.8898 Tm EMC /P <>BDC BT ET /P <>BDC EMC BT 9 0 0 9 408.1854 511.8898 Tm ET 9 0 0 9 411.0097 291.8898 Tm safer place! -.005 Tc 6.5 0 0 6.5 64.6596 637.9529 Tm ET /F6 1 Tf 7 0 0 7 554.7883 661.7654 Tm ET (variant used in this study is the CFM)Tj /P <>BDC ( )Tj BT ET /P <>BDC ET ET /P <>BDC 7 0 0 7 362.3891 331.9528 Tm /P <>BDC (158)Tj ( )Tj /P <>BDC (37,653)Tj 0 Tc ( )Tj (difference. /P <>BDC ET EMC 7 0 0 7 520.6108 540.9528 Tm BT EMC BT EMC ( )Tj /P <>BDC BT EMC 304.725 420.96 m ( )Tj ( )Tj -.02 Tc ET 7 0 0 7 99.8582 122.7654 Tm BT ET ET 7 0 0 7 338.6433 309.7654 Tm 7 0 0 7 362.3891 144.9528 Tm 7 0 0 7 99.8582 705.7654 Tm BT /P <>BDC BT EMC BT The controls for main tanks 1 and 2 change to aft -.02 Tc BT 0 Tc /P <>BDC 7 0 0 7 247.7395 232.7654 Tm 9 0 0 9 336.3455 313.8898 Tm /P <>BDC 9 0 0 9 194.7833 236.8898 Tm ET BT 6.5 0 0 6.5 244.3689 532.9529 Tm 7 0 0 7 343.2355 672.7654 Tm 7 0 0 7 71.6694 639.9528 Tm /P <>BDC ( )Tj /P <>BDC (2,728)Tj 7 0 0 7 298.1781 144.9528 Tm ET EMC ( )Tj EMC (l)Tj ET 6 0 0 6 278.7028 659.9528 Tm 8 0 0 8 419.0258 760.9528 Tm BT 5.25 0 0 5.25 55.7484 11.5132 Tm /P <>BDC /P <>BDC ( )Tj (inches and a bypass ratio of 11.0:1. (178)Tj /P <>BDC 0 Tc BT ET ( )Tj EMC EMC 7 0 0 7 537.7804 441.9528 Tm BT 0 Tc 7 0 0 7 491.4046 133.9528 Tm /P <>BDC ET ( )Tj /P <>BDC 9 0 0 9 232.4408 698.8898 Tm EMC /P <>BDC 7 0 0 7 554.7883 287.7654 Tm BT 7 0 0 7 210.1137 562.7654 Tm EMC (major airports, which could lead to the)Tj BT BT EMC 9 0 0 9 393.4057 379.8898 Tm ET 9 0 0 9 366.7762 390.8898 Tm 7 0 0 7 387.0159 529.9528 Tm ( )Tj 9 0 0 9 550.8315 247.8898 Tm EMC BT EMC BT 9 0 0 9 366.6417 137.8898 Tm /P <>BDC EMC /P <>BDC BT EMC ( )Tj ET /Im1 Do EMC BT -.01 Tc ( )Tj 0 Tc BT ET /P <>BDC 6jf/+6*Pe/[LeaVSjtLZ6*vXQ9b;(P+L(vV^V;,]2^JsGHqp]]&MDK1B39?ZVM,9P=2/ Zz>\\.. BT 7 0 0 7 474.3564 507.9528 Tm 0 Tc ET 7 0 0 7 387.0159 540.9528 Tm (period in 2020. /P <>BDC EMC ( )Tj 7 0 0 7 490.5101 485.9528 Tm EMC /P <>BDC ET 0 Tc EMC (34,650)Tj 8 0 0 8 153.6923 675.9528 Tm BT ( )Tj EMC BT BT 0 Tc 0 Tc 9 0 0 9 53.8582 786.8898 Tm 6.5 0 0 6.5 449.7715 565.9529 Tm /P <>BDC EMC (Boeing aircraft, the 737-800 has a 2.5%)Tj ET EMC (same 85% passenger payload of 136. EMC These have led to smaller and)Tj /P <>BDC /F6 1 Tf EMC )Tj 7 0 0 7 536.3849 639.7654 Tm 7 0 0 7 107.1165 661.9528 Tm EMC 0 Tc (at 27,000lbs thrust compared to the)Tj 0 Tc EMC 9 0 0 9 535.511 379.8898 Tm /P <>BDC /P <>BDC EMC ET EMC EMC /P <>BDC on the Simmonds gauges or error codes 1,3 and 6 on the Smiths gauges. 7 0 0 7 82.8504 122.9528 Tm BT 9 0 0 9 79.8339 522.8898 Tm -.02 Tc EMC /P <>BDC /P <>BDC ( )Tj EMC Calculates enroute fuel burn based on cruise altitude and trip distance. 0 Tc /P <>BDC ET EMC ( )Tj /P <>BDC -.02 Tc BT /P <>BDC ET EMC /P <>BDC 0 Tc ET BT BT EMC (0.0124)Tj /P <>BDC EMC ( )Tj must be determined by using the. (192 seats versus 179 on the 737-9. EMC /P <>BDC EMC EMC EMC /P <>BDC ( )Tj -2.5295 -5.0573 -2.1058 -5.3146 -1.5527 -5.3151 c BT /OC /MC2279 BDC 9 0 0 9 542.4784 115.8898 Tm (1,272)Tj .151 .147 .15 rg -.02 Tc (\(ATC\) charges. 9 0 0 9 195.4853 126.8898 Tm ET /P <>BDC BT BT ( )Tj -.02 Tc BT 9 0 0 9 361.7 456.8898 Tm 7 0 0 7 490.5101 617.9528 Tm i.e..what is the maximum lateral distance the doors swing away from the aircraft, before they get to rest in the fully open position? EMC 9 0 0 9 68.0314 522.8898 Tm 9 0 0 9 190.2832 49.8898 Tm EMC ET ET EMC 7 0 0 7 141.7322 133.9528 Tm BT BT 7 0 0 7 383.0719 705.7654 Tm Boeing 737 Interior. 7 0 0 7 354.7351 694.7654 Tm 361 0 obj ET EMC /P <>BDC /P <>BDC 9 0 0 9 215.4409 236.8898 Tm /P <>BDC 0 Tc EMC BT EMC /P <>BDC 7 0 0 7 247.7395 67.7654 Tm EMC EMC -.02 Tc /P <>BDC ( )Tj BT 7 0 0 7 241.5317 199.9528 Tm ET EMC EMC /P <>BDC ( )Tj (bypass ratio than the A320/321neo. either 3,065 or 1,421 litre capacities. 9 0 0 9 426.0987 687.8898 Tm EMC (the destination airports. 9 0 0 9 215.4313 192.8898 Tm (engine bypass ratio in the case of the 737)Tj EMC BT [(SS)-9.1(U)8(E)]TJ (- mins)Tj 0 Tc /P <>BDC 7 0 0 7 457.0984 463.7654 Tm /P <>BDC /P <>BDC -.02 Tc /P <>BDC ET /P <>BDC BT -.02 Tc -.02 Tc 9 0 0 9 53.8338 335.8898 Tm ET ET BT ET 10 0 0 10 47.7404 814.1973 Tm ET 7 0 0 7 440.0906 133.9528 Tm (A)Tj /P <>BDC 9 0 0 9 205.6978 291.8898 Tm 7 0 0 7 537.7804 265.9528 Tm EMC /P <>BDC EMC /P <>BDC EMC /P <>BDC ( )Tj ET 7 0 0 7 108.6215 232.9528 Tm ET (63.5 inches and a bypass ratio of 4.5:1; or)Tj ET EMC /P <>BDC EMC BT ET (483)Tj BT /P <>BDC (0.0158)Tj BT ET /P <>BDC -.02 Tc EMC BT /GS1 gs (efficiency and so lower fuel burn. BT ET /P <>BDC /P <>BDC 8 0 0 8 54.8194 760.9529 Tm EMC EMC /P <>BDC /P <>BDC EMC 7 0 0 7 314.6398 474.7654 Tm 9 0 0 9 516.3894 247.8898 Tm ET EMC EMC BT 9 0 0 9 394.0157 456.8898 Tm BT BT -.02 Tc (39,270)Tj ET ET (375)Tj /P <>BDC ET 0 Tc /P <>BDC (Since both the aircraft and engine)Tj /P <>BDC 6.5 0 0 6.5 430.0114 565.9529 Tm /F5 1 Tf /P <>BDC EMC ET EMC /P <>BDC ET BT ET 9 0 0 9 349.1631 60.8898 Tm 9 0 0 9 75.273 478.8898 Tm 0 Tc EMC EMC 0 Tc 7 0 0 7 294.4014 67.7654 Tm ET BT BT EMC (difference in fuel cost per ASM, however,)Tj 9 0 0 9 177.8457 82.8898 Tm Seating in the 737 was a result of the design when moving the engines underneath the wings. EMC EMC ET BT (The fuel tank capacity means the)Tj /P <>BDC ( )Tj ET 10 0 0 10 55.0104 814.1973 Tm EMC /P <>BDC /P <>BDC EMC EMC ( )Tj /P <>BDC ET ET EMC EMC /P <>BDC BT (the flight profile based on the cruise speed)Tj ET ( )Tj 7 0 0 7 520.6108 716.9528 Tm EMC EMC 7 0 0 7 490.8321 122.7654 Tm ET 8 0 0 8 38.4438 731.9528 Tm [(R)13.9(ange with full)]TJ BT (163)Tj 0 Tc 7 0 0 7 337.6855 485.9528 Tm ET 9 0 0 9 162.5427 412.8898 Tm EMC BT /P <>BDC ET EMC 7 0 0 7 337.4684 683.9528 Tm EMC /P <>BDC EMC /P <>BDC [(E)-24.9(SAD - nm )]TJ ET ( )Tj 7 0 0 7 279.1575 584.9528 Tm 7 0 0 7 326.2278 694.9528 Tm /F4 1 Tf /P <>BDC BT BT EMC (1,059)Tj BT ET EMC EMC ( )Tj BT (LEAP-1B. /P <>BDC EMC BT BT /P <>BDC BT ET /P <>BDC ET ( )Tj BT ET 7 0 0 7 535.5029 144.7654 Tm BT EMC EMC (1,272)Tj EMC /P <>BDC EMC (test programme is well underway for entry)Tj ( )Tj BT BT BT 7 0 0 7 187.0858 694.9528 Tm /P <>BDC BT The A320neo in this study)Tj EMC ET (industry is 210 US cents per USG for Jet A-)Tj 7 0 0 7 439.7405 507.9528 Tm ET EMC ET ( )Tj EMC The 737-)Tj 7 0 0 7 82.8504 89.9528 Tm /P <>BDC ( )Tj ET EMC ET /P <>BDC ET /P <>BDC 9 0 0 9 232.4217 170.8898 Tm BT BT Q EMC BT ET 9 0 0 9 394.0157 632.8898 Tm 9 0 0 9 343.5117 489.8898 Tm /P <>BDC EMC BT EMC 7 0 0 7 179.5605 221.9528 Tm ET ET ( )Tj ET 9 0 0 9 382.3068 489.8898 Tm EMC 19.841 0 l 0 Tc ET ( )Tj (MLW of 163,900lbs, and an OEW of)Tj BT ET BT ET EMC BT BT ET -.02 Tc Production has run from 1998 to present day. BT ET EMC ET 9 0 0 9 532.082 247.8898 Tm 7 0 0 7 314.6398 661.7654 Tm (136)Tj 7 0 0 7 158.74 243.7654 Tm Airbus A340, history of a long haul airliner. 0 Tc EMC 7 0 0 7 457.1753 705.7654 Tm Boeing 737-800 commercial aircraft. EMC ( )Tj 9 0 0 9 411.0097 522.8898 Tm ET ET EMC EMC 7 0 0 7 447.3829 705.7654 Tm ET BT ET EMC ET /P <>BDC ET (3,069)Tj ET ( )Tj EMC /P <>BDC EMC EMC EMC 7 0 0 7 518.4953 243.9528 Tm /P <>BDC BT EMC ( )Tj 6.5 0 0 6.5 375.6529 663.9529 Tm ( )Tj EMC BT 7 0 0 7 298.514 639.9528 Tm EMC 6 0 0 6 130.4965 771.9528 Tm (39,270)Tj /P <>BDC ET BT EMC ET /P <>BDC BT \p+\rWef6lfL6;U1E5/6lUYyVebaHfQM]$q|L>_ SO9_sXa 3@"G;C=zlPY[?B ET (cost compared to fuel. /P <>BDC 9 0 0 9 411.0181 258.8898 Tm 0 Tc (2,800 -)Tj ET (31,416)Tj /P <>BDC ( )Tj 7 0 0 7 258.2805 122.7654 Tm 0 Tc [(CFM L)17.1(E)-8.1(AP-1A32)]TJ 7 0 0 7 314.6398 463.7654 Tm 9 0 0 9 411.0097 533.8898 Tm 1 i 7 0 0 7 294.4014 639.7654 Tm 6.5 0 0 6.5 170.1113 702.9529 Tm ET BT 7 0 0 7 508.2252 11.5129 Tm /P <>BDC ET .023 .567 .626 rg ( )Tj BT EMC 7 0 0 7 508.4124 606.7654 Tm EMC ET 7 0 0 7 54.7071 562.7654 Tm EMC BT /P <>BDC /P <>BDC ET (using the same payload and seat)Tj ( )Tj ET 7 0 0 7 54.7071 606.7654 Tm ( )Tj (. BT EMC (1,074)Tj 0 Tc ( )Tj EMC (409,650)Tj -.01 Tc 7 0 0 7 445.7203 11.5129 Tm ET EMC /P <>BDC 7 0 0 7 99.8582 606.7654 Tm 0 Tc Since no two)Tj ET /P <>BDC /P <>BDC /P <>BDC BT ET (-58)Tj

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