BT BT ET (distances, and alternate airports are shown)Tj BT BT /P <>BDC BT ( )Tj EMC &6E'dtU7()euFVfvGWgw8HXhx9IYiy*:JZjz ? ET ( )Tj BT EMC EMC (34,650)Tj [(7)-33(3)8.1(7-800 & 7)-33(3)8.1(7-8 )]TJ /P <>BDC 9 0 0 9 232.438 181.8898 Tm 9 0 0 9 36.8504 181.8898 Tm In payload scenario 1 the)Tj EMC /P <>BDC ( )Tj /P <>BDC /P <>BDC BT ET 7 0 0 7 101.0963 111.9528 Tm 7 0 0 7 99.5912 485.9528 Tm BT 7 0 0 7 429.157 496.9528 Tm ET (0.0109)Tj These transfer fuel from the centre tank into tank 1 at a minimum rate of 100kg/hr, although usually nearer 200kg/hr. In contrast, Boeing has)Tj BT BT 9 0 0 9 258.18 60.8898 Tm ET BT /P <>BDC EMC EMC /P <>BDC ( )Tj ET 7 0 0 7 131.6494 474.7654 Tm 7 0 0 7 258.2805 210.7654 Tm /P <>BDC BT 9 0 0 9 565.9277 60.8898 Tm /P <>BDC (covers a 3,300-3,400nm range with a full)Tj 7 0 0 7 366.0641 716.9528 Tm 0 Tc BT BT ET 9 0 0 9 36.8504 379.8898 Tm ET 9 0 0 9 388.0328 467.8898 Tm ( )Tj BT /P <>BDC EMC ET /P <>BDC ET /P <>BDC /P <>BDC /P <>BDC ( )Tj EMC EMC ET (temperature )Tj /F1 1 Tf ET 6.5 0 0 6.5 64.6596 532.9529 Tm 7 0 0 7 344.1175 573.7654 Tm -.015 Tc /P <>BDC BT EMC 9 0 0 9 213.7526 258.8898 Tm BT BT EMC /P <>BDC BT (The A320ceo is payload-restricted to)Tj EMC EMC /P <>BDC ET ET BT EMC ( )Tj EMC (0.0115)Tj ET EMC ( )Tj 9 0 0 9 36.8504 49.8898 Tm EMC ( )Tj ( )Tj (346,456)Tj /P <>BDC ET 8 0 0 8 365.7704 745.9528 Tm ET EMC ( )Tj ET 7 0 0 7 299.0601 441.9528 Tm 7 0 0 7 387.0159 661.9528 Tm BT ( )Tj ET EMC 7 0 0 7 299.0601 265.9528 Tm /P <>BDC (give the A321neo a range of up to)Tj /P <>BDC ET ET EMC ET EMC ( )Tj .151 .147 .15 rg 6 0 0 6 226.9834 715.9528 Tm BT ( )Tj 0 Tc /P <>BDC ( )Tj EMC BT EMC EMC BT EMC /P <>BDC 6.5 0 0 6.5 107.0213 650.9529 Tm 9 0 0 9 53.8582 104.8898 Tm EMC BT 7 0 0 7 387.0932 210.9528 Tm 9 0 0 9 36.8504 313.8898 Tm 7 0 0 7 54.7071 419.7654 Tm ET ET (3,300 -)Tj ( )Tj ( )Tj BT /P <>BDC EMC /P <>BDC EMC EMC EMC EMC 6.5 0 0 6.5 426.4819 676.9529 Tm 9 0 0 9 528.0345 511.8898 Tm ET EMC (A320ceo)Tj ET -.02 Tc 7 0 0 7 298.1781 67.9528 Tm 7 0 0 7 279.1575 738.9528 Tm 9 0 0 9 215.4313 357.8898 Tm EMC 7 0 0 7 490.8321 221.7654 Tm /P <>BDC EMC -.02 Tc [(BOS-SE)-13.9(A)]TJ ( )Tj BT 9 0 0 9 36.8504 280.8898 Tm 7 0 0 7 294.4014 177.7654 Tm 9 0 0 9 215.4313 49.8898 Tm BT The analysis, however,)Tj /P <>BDC EMC EMC BT BT 9 0 0 9 356.7322 159.8898 Tm ET EMC ET 9 0 0 9 215.4409 357.8898 Tm 9 0 0 9 354.463 49.8898 Tm 9 0 0 9 383.3617 346.8898 Tm /P <>BDC (34,650lbs)Tj BT BT EMC BT 7 0 0 7 440.0906 342.9528 Tm ET ( )Tj ET ( )Tj BT BT ET BT 7 0 0 7 294.4014 408.7654 Tm BT EMC ( )Tj BT 7 0 0 7 114.6416 496.9528 Tm ET /P <>BDC ET /P <>BDC /P <>BDC ET ET 7 0 0 7 37.6993 199.9528 Tm -.02 Tc 7 0 0 7 43.6039 254.9528 Tm ET BT The Boeing 737-800 is an example of an average sized airplane. ET BT ET 7 0 0 7 387.0159 485.9528 Tm 0 Tc BT BT 7 0 0 7 316.0679 199.7654 Tm (174,606)Tj (26,000lbs thrust on the A320neo powered)Tj /P <>BDC /P <>BDC ET It has a maximum range of 10,140km. (sectors, particularly the shorter ones,)Tj 0 Tc EMC 9 0 0 9 68.0071 412.8898 Tm /P <>BDC 7 0 0 7 537.7804 309.9528 Tm /P <>BDC EMC BT ET BT 10 0 0 10 49.9904 814.1973 Tm /Artifact <>BDC [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ .008 Tc 9 0 0 9 199.3017 401.8898 Tm BT 7 0 0 7 457.1753 705.7654 Tm BT ET 503.534 80.74 l (388)Tj EMC BT ET BT EMC ET EMC EMC ET 7 0 0 7 404.101 430.7654 Tm 7 0 0 7 315.1859 144.7654 Tm 7 0 0 7 247.7395 364.7654 Tm /P <>BDC 6 0 0 6 372.295 673.9528 Tm ET 7 0 0 7 163.8846 11.5132 Tm -.02 Tc )Tj BT /P <>BDC ( )Tj EMC /P <>BDC ET ET BT EMC 7 0 0 7 444.737 144.7654 Tm /P <>BDC BT (6,303)Tj 7 0 0 7 490.8321 397.7654 Tm ET ET ( )Tj -.02 Tc BT Q (. ET ET ET 9 0 0 9 377.8897 291.8898 Tm EMC ( )Tj 9 0 0 9 394.0123 522.8898 Tm 7 0 0 7 508.4124 694.7654 Tm ( )Tj EMC 8 0 0 8 64.6596 760.9529 Tm ( )Tj ( )Tj 9 0 0 9 371.7696 390.8898 Tm BT ( )Tj ( )Tj EMC -.02 Tc The payload weights for)Tj 7 0 0 7 536.3849 309.7654 Tm ET 10 0 0 10 425.05 814.1973 Tm 0 Tc BT 9 0 0 9 215.4409 192.8898 Tm ET 0 Tc ET (method of operation that balances the cost)Tj ( )Tj 7 0 0 7 354.6933 430.7654 Tm ET EMC 9 0 0 9 394.0157 181.8898 Tm system is essentially automatic. BT BT BT BT ET EMC BT (34,650)Tj EMC 7 0 0 7 277.3936 144.9528 Tm EMC (34,650lbs)Tj ET 9 0 0 9 232.4217 533.8898 Tm BT /P <>BDC (evaluation, the 737-8 and 737-9 are 2.2%)Tj BT EMC 7 0 0 7 54.7071 694.7654 Tm (I)Tj BT BT (150)Tj EMC ET 9 0 0 9 232.438 115.8898 Tm -.02 Tc <> (20)Tj BT BT /P <>BDC This is because the RH centre tank pump will stop feeding due to the ET EMC Download the Final EMC ET EMC 9 0 0 9 394.0123 478.8898 Tm EMC 7 0 0 7 427.7291 166.9528 Tm 9 0 0 9 36.8504 258.8898 Tm /P <>BDC ET /P <>BDC ET /P <>BDC EMC BT ( )Tj ET /P <>BDC 7 0 0 7 518.4953 331.9528 Tm EMC EMC The Boeing 737-800 variant has as mentioned 27300 pound-force delivered by two turbo fans. BT ET -.02 Tc /P <>BDC BT /P <>BDC ET BT /P <>BDC EMC ( )Tj ET ET 0 Tc BT /P <>BDC ET /P <>BDC /P <>BDC (2,900)Tj EMC 7 0 0 7 535.5029 606.7654 Tm EMC EMC BT 7 0 0 7 230.7317 694.9528 Tm 9 0 0 9 53.8582 665.8898 Tm 9 0 0 9 542.2972 203.8898 Tm (342,312)Tj 8 0 0 8 53.9012 749.9529 Tm /P <>BDC BT ET /P <>BDC EMC [(Seat configur)10(ation)]TJ BT /P <>BDC 9 0 0 9 53.8578 346.8898 Tm ET BT -.02 Tc /P <>BDC 9 0 0 9 425.183 456.8898 Tm EMC /P <>BDC ET (used is 16/30/114, giving a seat count of)Tj ET /P <>BDC BT /P <>BDC 7 0 0 7 299.0601 232.9528 Tm 0 Tc /P <>BDC EMC BT Cheers Peter. ( )Tj EMC /GS2 gs (equivalent NG family members. BT 7 0 0 7 125.6292 243.7654 Tm ET EMC BT ET /P <>BDC BT BT ET (132,872)Tj (in a more efficient engine. ET BT 9 0 0 9 394.0237 214.8898 Tm EMC .964 .834 .406 rg 7 0 0 7 314.6398 738.7654 Tm (31,416)Tj BT ( )Tj EMC /P <>BDC 9 0 0 9 521.6329 137.8898 Tm BT (10)Tj ET ET EMC /P <>BDC In scenario 2, the 85% payload)Tj EMC BT EMC 7 0 0 7 230.7317 518.9528 Tm /P <>BDC ET 7 0 0 7 429.157 727.9528 Tm ET .0081 Tc (1,668)Tj (174,165)Tj (977)Tj 8 0 0 8 334.994 703.9528 Tm EMC 7 0 0 7 439.2087 111.9528 Tm ET EMC S BT BT /P <>BDC BT EMC /P <>BDC (capacity. ET ET BT /P <>BDC BT ET BT /Artifact <>BDC BT (178-187)Tj EMC BT BT 9 0 0 9 215.4409 346.8898 Tm BT 9 0 0 9 211.0829 379.8898 Tm Thank you. 7 0 0 7 230.7317 408.9528 Tm -.02 Tc EMC /P <>BDC EMC 7 0 0 7 518.4953 144.9528 Tm /F6 1 Tf ( )Tj ( )Tj BT ( )Tj EMC 9 0 0 9 68.3339 467.8898 Tm 8 0 0 8 225.1837 591.9528 Tm BT BT 7 0 0 7 381.1608 562.7654 Tm <>stream BT EMC (170)Tj BT /P <>BDC BT EMC /P <>BDC ET 7 0 0 7 473.8245 320.9528 Tm EMC EMC ET 9 0 0 9 537.6038 170.8898 Tm (this page\))Tj /GS1 gs BT /F6 1 Tf (1,392)Tj BT 6.5 0 0 6.5 474.3939 663.9529 Tm 7 0 0 7 294.4014 496.7654 Tm (/S)Tj ( )Tj ET ET ET 7 0 0 7 457.0984 507.7654 Tm 9 0 0 9 232.4217 104.8898 Tm 137 )Tj EMC 6 0 0 6 154.2695 743.9528 Tm BT ET 7 0 0 7 53.8582 11.5132 Tm (2,732)Tj /P <>BDC ET ( )Tj ET EMC /P <>BDC ET (207,336)Tj BT ET ( )Tj ( )Tj ET 6.5 0 0 6.5 432.488 558.9529 Tm ( )Tj 7 0 0 7 338.6433 276.7654 Tm BT ( )Tj BT /P <>BDC EMC ET ET ( )Tj ET 7 0 0 7 387.0932 441.9528 Tm (ratio of 12.5:1; and the CFM LEAP-1A26)Tj ET 9 0 0 9 53.8578 478.8898 Tm EMC EMC ET BT ( )Tj BT .151 .147 .15 rg BT /P <>BDC 7 0 0 7 554.7883 507.7654 Tm <> BT (20)Tj /P <>BDC BT 7 0 0 7 141.7322 441.9528 Tm ET (39,270)Tj ET ET ET ( )Tj 7 0 0 7 99.8582 243.7654 Tm BT BT 9 0 0 9 542.2986 192.8898 Tm EMC ET BT ( )Tj /P <>BDC (fuselage length. 7 0 0 7 337.7614 144.7654 Tm ET /GS2 gs /P <>BDC EMC (252-264)Tj BT BT ( )Tj 9 0 0 9 411.0097 115.8898 Tm EMC EMC ET 7 0 0 7 508.4124 287.7654 Tm This is due to cold ( )Tj Happy Flying. 7 0 0 7 536.3849 485.7654 Tm BT 13 0 0 13 53.8582 137.8898 Tm [(D)12.9(A)-8.1(L/36)]TJ EMC (163)Tj /P <>BDC ( )Tj BT (improvement ranges from 17.4% to)Tj ET EMC EMC /P <>BDC BT -.02 Tc BT ( )Tj 7 0 0 7 37.6993 298.9528 Tm 0 Tc (737-800W)Tj ET /P <>BDC 7 0 0 7 187.0858 298.9528 Tm BT BT (passenger load factor based on each types)Tj 8 0 0 8 421.0237 771.7654 Tm ET 0 Tc of 12% is sufficient to prevent ignition, this is achievable with one module on /P <>BDC /P <>BDC ET 0 Tc .014984 824.882 572.583 17.008 re BT 0 Tc ET ET /P <>BDC EMC 0 Tc EMC 9 0 0 9 53.8338 247.8898 Tm /P <>BDC 6.5 0 0 6.5 64.6596 624.9529 Tm EMC EMC /P <>BDC EMC 6.5 0 0 6.5 347.0329 611.9529 Tm /P <>BDC )]TJ EMC 7 0 0 7 204.0935 430.7654 Tm 10 0 0 10 36.8504 814.1973 Tm BT 7 0 0 7 354.6933 265.7654 Tm ( )Tj EMC 0 Tc 7 0 0 7 54.7071 298.7654 Tm (equipped with the more fuel-efficient CFM)Tj 6.5 0 0 6.5 382.9199 735.9529 Tm ET ET 5.25 0 0 5.25 492.6848 11.5129 Tm EMC BT BT 0 Tc /P <>BDC ET 9 0 0 9 173.7412 203.8898 Tm EMC 7 0 0 7 520.6108 639.9528 Tm 13 0 0 13 53.8338 588.8898 Tm 7 0 0 7 456.2165 122.7654 Tm (between the A320ceo and A320neo. EMC ( )Tj 9 0 0 9 411.0097 599.8898 Tm ET (737-9)Tj 8 0 0 8 159.2283 745.9528 Tm 7 0 0 7 337.7614 111.7654 Tm /P <>BDC /P <>BDC EMC EMC /P <>BDC 6 0 0 6 268.0069 701.9528 Tm EMC /P <>BDC ET 9 0 0 9 360.9639 192.8898 Tm 9 0 0 9 68.0071 159.8898 Tm 0 Tc /P <>BDC BT ( )Tj BT BT 6 0 0 6 153.6996 701.9528 Tm ( )Tj BT BT EMC ( )Tj EMC (152)Tj BT /Artifact <>BDC ET EMC ET EMC /P <>BDC 7 0 0 7 474.3564 606.9528 Tm /P <>BDC 0 Tc /P <>BDC One carrier)Tj ET 9 0 0 9 508.3771 698.8898 Tm /P <>BDC ET -.02 Tc BT 9 0 0 9 368.3979 38.8898 Tm 7 0 0 7 182.5706 573.9528 Tm 9 0 0 9 53.8582 500.8898 Tm BT 7 0 0 7 363.2711 67.9528 Tm ET /P <>BDC ET 9 0 0 9 394.0123 379.8898 Tm ET ET 7 0 0 7 429.4931 122.9528 Tm ET (104-112)Tj (1,824)Tj ( )Tj 0 Tc ET ET /P <>BDC <>/XObject<>/ExtGState<>/Properties<>>> 0 Tc /P <>BDC (reconfiguration to reposition toilets and)Tj ET ( )Tj -.02 Tc /P <>BDC (2,524)Tj ET ET 9 0 0 9 356.4538 258.8898 Tm EMC ( )Tj EMC ( )Tj BT (4,514)Tj (1,272)Tj -.02 Tc ET ET ET ( )Tj 0 Tc 7 0 0 7 473.8245 298.9528 Tm If you like us, please share with your followers. BT BT ET BT BT EMC ET BT /P <>BDC (larger engines, but again the aircraft)Tj BT 0 Tc ET 6.5 0 0 6.5 375.6529 676.9529 Tm 9 0 0 9 192.8213 60.8898 Tm EMC BT ( )Tj BT EMC These sectors)Tj EMC 7 0 0 7 457.0984 485.7654 Tm ET (longer routes. /P <>BDC /P <>BDC 7 0 0 7 316.0679 276.7654 Tm ( )Tj BT 9 0 0 9 526.8813 445.8898 Tm /P <>BDC ( )Tj probably take you over MTOW if any payload was carried. EMC 7 0 0 7 279.1575 419.9528 Tm /P <>BDC -.02 Tc EMC BT ET 0 Tc ( )Tj ET 0 Tc 8 0 0 8 141.7322 771.9528 Tm 6.5 0 0 6.5 328.6662 585.9529 Tm 7 0 0 7 321.6356 177.9528 Tm /P <>BDC The data for our pages are sourced from various locations, ranging from airliner manufacturer websites, technical airliner manuals etc. BT ET -.01 Tc BT ET BT 0 Tc ( )Tj /P <>BDC EMC EMC BT BT EMC /P <>BDC ( )Tj /TT2 1 Tf EMC ET BT BT EMC ET 9 0 0 9 394.0123 324.8898 Tm EMC ET (158)Tj BT BT ET EMC (31,416)Tj EMC ET EMC (average improvement in trip fuel burn. ET EMC 7 0 0 7 507.7893 67.7654 Tm BT ET ET ET -.02 Tc BT BT (test programme is well underway for entry)Tj BT ( A)Tj (170)Tj BT ET EMC ET ET 0 841.89 609.449 -841.89 re BT 7 0 0 7 539.8962 518.9528 Tm The NG has 6 dripsticks in each wing tank and 4 in the centre ET ( )Tj 7 0 0 7 354.6933 441.7654 Tm ( )Tj EMC ET ET ET 0 Tc 9 0 0 9 176.5402 280.8898 Tm BT EMC EMC 5.25 0 0 5.25 64.5461 11.5129 Tm EMC EMC 0 Tc /P <>BDC /P <>BDC 7 0 0 7 258.2805 298.7654 Tm BT /P <>BDC /P <>BDC )Tj ET ( )Tj /P <>BDC /P <>BDC All the aircraft would therefore)Tj ( )Tj ET ( )Tj BT /P <>BDC (38,168)Tj ET ET 9 0 0 9 204.9907 467.8898 Tm EMC -.02 Tc ET [(UG)-17.1(U)-8(S)8.1(T)]TJ /P <>BDC EMC /P <>BDC 7 0 0 7 439.9995 694.9528 Tm /P <>BDC ET EMC ET ET -.02 Tc 9 0 0 9 361.007 126.8898 Tm BT ET ( )Tj ET BT ET BT EMC ET BT EMC (A320neo)Tj /P <>BDC ( )Tj (37,653lbs )Tj 9 0 0 9 394.0315 302.8898 Tm 9 0 0 9 232.4408 687.8898 Tm BT EMC /GS1 gs /P <>BDC /P <>BDC (374)Tj thank you for stopping by and we appreciate you checking us out on the details. 9 0 0 9 341.891 335.8898 Tm ET 7 0 0 7 37.6993 265.9528 Tm 7 0 0 7 295.2833 78.7654 Tm /P <>BDC ( )Tj /P <>BDC EMC The system tolerance is then +/- 200 KG at any fuel level within the tank. /P <>BDC /P <>BDC BT [(OM)8.1(M)-12.9(E)-24.9(R)7.1(C)8.1(E)]TJ -.02 Tc EMC /P <>BDC ( )Tj 7 0 0 7 354.6933 364.7654 Tm ( )Tj BT 9 0 0 9 535.2501 522.8898 Tm (around the world. /P <>BDC 6 0 0 6 481.8528 701.9528 Tm ( )Tj 9 0 0 9 215.433 93.8898 Tm BT /P <>BDC ( )Tj [(OM)8.1(M)-12.9(E)-24.9(R)7.1(C)8.1(E)]TJ ( )Tj ET BT EMC ET -.02 Tc How much fuel does a A350 burn? /GS2 gs 9 0 0 9 171.8783 434.8898 Tm /P <>BDC EMC 10 0 0 10 51.9004 814.1973 Tm ET ET ( )Tj EMC ET ET (-62)Tj ( )Tj /P <>BDC 7 0 0 7 230.7317 122.9528 Tm 9 0 0 9 53.8582 764.8898 Tm /P <>BDC 7 0 0 7 491.7142 408.7654 Tm ET ET /P <>BDC 161.566 0 l ( )Tj EMC EMC 6 0 0 6 466.3723 701.9528 Tm 7 0 0 7 354.4763 716.7654 Tm (It is recognised that on some of the)Tj Note that the first 1,000 pounds of fuel are loaded into the center tank, then the wing tanks are . BT BT EMC /P <>BDC 7 0 0 7 337.6855 540.9528 Tm /P <>BDC BT BT EMC 6.5 0 0 6.5 295.373 742.9529 Tm 6.5 0 0 6.5 376.7644 742.9529 Tm ( )Tj /P <>BDC /P <>BDC ET /P <>BDC ( )Tj 6.5 0 0 6.5 531.2397 565.9529 Tm ( )Tj 0 Tc 9 0 0 9 394.0157 643.8898 Tm /P <>BDC 7 0 0 7 362.3891 309.9528 Tm (in engine cool-down times. ET BT (The evaluation uses US domestic flight)Tj -.02 Tc EMC 6.5 0 0 6.5 317.7333 742.9529 Tm 7 0 0 7 187.0858 210.9528 Tm ET EMC 7 0 0 7 82.8504 353.9528 Tm EMC /P <>BDC EMC BT /P <>BDC ( )Tj BT 0 Tc ( )Tj /P <>BDC /P <>BDC BT /P <>BDC [(A3)24.9(21ceo & A3)24.9(21neo )]TJ ET BT /P <>BDC /P <>BDC ( )Tj BT ET 7 0 0 7 337.6855 485.9528 Tm ET 0 Tc ET EMC BT EMC BT BT 0 Tc BT EMC safer place! BT (have therefore been removed from the)Tj ET /F2 1 Tf (A320neo, A321neo, 737-800, 737-)Tj ( )Tj BT (be charged the same in operation for this)Tj /P <>BDC BT /P <>BDC ( )Tj /P <>BDC EMC BT ( )Tj EMC BT BT 0 Tc BT ET q 1 0 0 1 215.441 73.878 cm 0 0 m ( )Tj 505.325 82.247 l BT BT EMC -.02 Tc 6 0 0 6 507.2798 715.9528 Tm (248,064)Tj 6 0 0 6 357.8844 701.9528 Tm )Tj BT BT ET /P <>BDC ( )Tj (manufacturers, with Airbus reducing the)Tj /P <>BDC ( )Tj BT (2.1%. 0 Tc ET (this evaluation. /P <>BDC 7 0 0 7 193.1059 188.9528 Tm EMC ET ET EMC BT 9 0 0 9 348.0922 511.8898 Tm /P <>BDC 8 0 0 8 435.4879 760.7654 Tm -2.4549 -3.9026 m 7 0 0 7 337.7614 100.7654 Tm EMC 9 0 0 9 418.9315 59.9073 Tm ET /P <>BDC ( )Tj BT ET BT 7 0 0 7 492.5963 716.7654 Tm (0.0112)Tj 7 0 0 7 537.7804 298.9528 Tm BT (uses one of the 11 certified weight variants. BT 7 0 0 7 355.3163 89.7654 Tm EMC 9 0 0 9 36.8504 280.8898 Tm 0 Tc EMC 7 0 0 7 490.5101 540.9528 Tm /GS2 gs 9 0 0 9 394.0237 269.8898 Tm EMC -.005 Tc These improvements include the redesign of fuel pumps, FQIS, any BT /P <>BDC design and maintenance of fuel tanks to reduce the chances of such explosions in ( )Tj /P <>BDC -.02 Tc BT ET (0.0124)Tj BT BT BT (427,890)Tj EMC /P <>BDC (the aircraft types. BT 9 0 0 9 202.0349 753.8898 Tm 7 0 0 7 362.3891 375.9528 Tm ET 9 0 0 9 394.0315 170.8898 Tm /P <>BDC ET ( )Tj /P <>BDC EMC 7 0 0 7 43.6039 342.9528 Tm ( )Tj BT (831)Tj (prices, and can vary by the aircraft type)Tj /P <>BDC 7 0 0 7 507.7893 639.7654 Tm (A321neo)Tj EMC ( )Tj ( )Tj /P <>BDC /P <>BDC (190,800)Tj ET What makes the newest 747 Jumbo tick? 56 0 0 56 36.8606 622.1944 Tm 9 0 0 9 73.1083 500.8898 Tm BT )Tj 7 0 0 7 444.737 199.7654 Tm /P <>BDC (39,270)Tj EMC ( )Tj [(P)11(ayload scenario one)]TJ ET ET /P <>BDC BT BT ( )Tj 7 0 0 7 54.7071 375.7654 Tm 9 0 0 9 551.4604 269.8898 Tm 7 0 0 7 518.4953 419.9528 Tm 0 Tc (A321ceo)Tj .151 .147 .15 rg -.01 Tc EMC BT EMC 6 0 0 6 240.5796 729.9528 Tm ET 7 0 0 7 337.6855 518.9528 Tm BT /P <>BDC BT [(737-900E)-33(R)]TJ 9 0 0 9 203.1969 566.8898 Tm /OC /MC5086 BDC EMC EMC ( )Tj /P <>BDC BT ( )Tj 7 0 0 7 82.8504 221.9528 Tm /P <>BDC (0.0122)Tj (A321neo)Tj If you switch on the centre tank pumps and the LP lights ( )Tj S BT (than the A321ceo. 0 Tc 0 Tc EMC ( )Tj /P <>BDC /P <>BDC EMC EMC Boeing 787 Dreamliner Orders and Deliveries. BT /P <>BDC (give the newer type a further advantage. BT ( )Tj 8 0 0 8 339.6345 760.7654 Tm BT ( )Tj 9 0 0 9 274.8953 93.8898 Tm 0 Tc ET ET 7 0 0 7 204.0935 683.7654 Tm ( )Tj 7 0 0 7 99.5912 507.9528 Tm /P <>BDC ET 7 0 0 7 326.2278 683.9528 Tm BT ( )Tj BT BT ( )Tj EMC -.02 Tc EMC /P <>BDC /P <>BDC (248,200)Tj EMC EMC BT ( )Tj ET -.02 Tc ET 9 0 0 9 53.8338 313.8898 Tm /P <>BDC EMC 1.6741 -3.9062 l EMC 7 0 0 7 88.196 11.5129 Tm [(M)-13.9(KE/84)]TJ ET 7 0 0 7 125.6292 529.7654 Tm /P <>BDC BT BT EMC ET 7 0 0 7 141.7322 683.9528 Tm 9 0 0 9 215.433 71.8898 Tm BT ET BT EMC 0 Tc EMC ET EMC (. ET /P <>BDC ET ET EMC Having a higher)Tj 9 0 0 9 361.1316 214.8898 Tm ( )Tj BT EMC /P <>BDC BT BT EMC ET ( )Tj EMC EMC ( )Tj ET /P <>BDC ET ET /P <>BDC (I)Tj ( )Tj EMC ET ET ET /P <>BDC BT )Tj ( )Tj /P <>BDC endobj -.02 Tc ( )Tj /P <>BDC (136)Tj BT EMC 7 0 0 7 37.0536 518.9528 Tm -.02 Tc /P <>BDC 10 0 0 10 64.6596 794.2914 Tm 9 0 0 9 394.0157 621.8898 Tm 9 0 0 9 53.8582 632.8898 Tm /P <>BDC /P <>BDC BT 7 0 0 7 279.1575 529.9528 Tm ( )Tj /P <>BDC ET ( )Tj BT ( )Tj ET 7 0 0 7 294.4014 540.7654 Tm ET (150)Tj ET /P <>BDC ( )Tj 5 0 0 5 92.725 11.5132 Tm 7 0 0 7 439.7405 705.9528 Tm (136)Tj 6.5 0 0 6.5 171.2227 742.9529 Tm /P <>BDC EMC ( )Tj ET ET 6 0 0 6 138.6506 757.9528 Tm /F6 1 Tf EMC BT ( )Tj /P <>BDC ET ( )Tj /P <>BDC ( )Tj /P <>BDC /P <>BDC BT BT BT (/S)Tj 7 0 0 7 403.478 474.7654 Tm ET /P <>BDC (the relative fuel costs between the aircraft)Tj ( )Tj BT ET 7 0 0 7 230.7317 485.9528 Tm /P <>BDC ( )Tj EMC EMC /P <>BDC ET -.02 Tc ET BT /P <>BDC ( )Tj 503.542 90.794 m ET ET (152)Tj /P <>BDC BT EMC (176)Tj BT /P <>BDC EMC 9 0 0 9 215.4313 159.8898 Tm (163)Tj 8 0 0 8 136.4919 661.9528 Tm EMC ET /P <>BDC EMC BT 9 0 0 9 206.6251 236.8898 Tm ET 9 0 0 9 232.4217 467.8898 Tm EMC 7 0 0 7 204.0935 606.7654 Tm ET ET /P <>BDC BT ET ET /P <>BDC ET ( )Tj /P <>BDC ET /P <>BDC 7 0 0 7 241.5317 529.9528 Tm BT 9 0 0 9 522.1112 247.8898 Tm ( )Tj (economy seating by 12 seats when)Tj BT ET /P <>BDC (157)Tj BT ( )Tj BT ET ET ET ET ET 7 0 0 7 363.2711 177.9528 Tm BT /P <>BDC ( )Tj EMC EMC EMC /P <>BDC /P <>BDC ( )Tj ( )Tj EMC ( )Tj ET /P <>BDC BT BT BT BT ( )Tj (0.0133)Tj ( )Tj /P <>BDC /P <>BDC ET /P <>BDC BT 6 0 0 6 255.8802 771.9528 Tm (1,019)Tj ( )Tj ( )Tj EMC /P <>BDC ET ( )Tj 7 0 0 7 338.3085 309.9528 Tm ET EMC /P <>BDC /P <>BDC BT -.01 Tc EMC ET 8 0 0 8 43.6039 647.9528 Tm BT ET 9 0 0 9 188.8887 60.8898 Tm 9 0 0 9 68.0314 126.8898 Tm 6 0 0 6 55.0668 659.9528 Tm 0 Tc 7 0 0 7 247.7395 485.7654 Tm (direction lead to a headwind component)Tj 7 0 0 7 355.3163 177.7654 Tm BT BT BT ( )Tj /P <>BDC 7 0 0 7 404.101 78.7654 Tm 7 0 0 7 496.3063 727.7654 Tm ( )Tj -.02 Tc /P <>BDC 0 Tc EMC 7 0 0 7 77.36 11.5132 Tm ET -.02 Tc 6.5 0 0 6.5 382.478 545.9529 Tm (191,240)Tj EMC ( )Tj 7 0 0 7 241.5317 540.9528 Tm (is 0.01 to 0.15 cents better than the)Tj BT ET EMC ( )Tj BT EMC EMC 9 0 0 9 394.0315 533.8898 Tm /P <>BDC BT 7 0 0 7 473.8245 265.9528 Tm 7 0 0 7 241.5317 210.9528 Tm EMC BT EMC 7 0 0 7 491.4046 397.9528 Tm ( )Tj ET ET /OC /MC199 BDC ET )Tj 9 0 0 9 565.2708 313.8898 Tm ( )Tj EMC EMC BT fuel burn. ET (flight levels. BT 7 0 0 7 403.478 221.7654 Tm 7 0 0 7 439.7405 617.9528 Tm EMC .661 .752 .896 rg EMC BT EMC /P <>BDC BT /P <>BDC 7 0 0 7 473.8245 243.9528 Tm EMC ET -.01 Tc EMC EMC EMC EMC BT EMC EMC BT BT /P <>BDC 7 0 0 7 539.8962 727.9528 Tm /P <>BDC EMC Thai Airways on 3 Mar 2001 and 737-300 EI-BZG operated by Philippine Airlines ( )Tj 7 0 0 7 131.6494 265.7654 Tm /P <>BDC EMC 7 0 0 7 537.7804 210.9528 Tm ET BT EMC BT ET ( )Tj ( )Tj EMC /P <>BDC EMC ET ET /P <>BDC /P <>BDC BT 9 0 0 9 534.5925 753.8898 Tm 9 0 0 9 211.7668 225.8898 Tm 7 0 0 7 519.3773 67.9528 Tm (2,745)Tj BT 9 0 0 9 570.805 49.8898 Tm ET 5.25 0 0 5.25 73.853 11.5132 Tm BT BT ET /F1 1 Tf EMC ET 9 0 0 9 394.0315 159.8898 Tm ( )Tj /P <>BDC /P <>BDC /P <>BDC EMC /P <>BDC ET EMC [(AIR)7.2(CRAF)-12.8(T)18.2( SPECIF)7.2(IC)-32.9(A)57(T)-8(ION)-13.8(S & )22(WEIGHT)12.1(S )]TJ ( )Tj /P <>BDC EMC 7 0 0 7 54.7071 100.7654 Tm (-60)Tj ET /P <>BDC ET 9 0 0 9 394.0315 665.8898 Tm ET ET EMC ET BT BT (2,933)Tj EMC /P <>BDC EMC ET 7 0 0 7 187.0858 309.9528 Tm ET /P <>BDC ET EMC EMC /P <>BDC /P <>BDC ( )Tj 7 0 0 7 337.9444 617.9528 Tm As a result of its lower fuel burn,)Tj EMC ET /P <>BDC ET 7 0 0 7 196.5683 518.7654 Tm ET EMC EMC EMC 6.5 0 0 6.5 124.409 585.9529 Tm 7 0 0 7 141.7322 364.9528 Tm /P <>BDC /P <>BDC EMC EMC ET -.02 Tc /P <>BDC /P <>BDC ET /P <>BDC BT ET /P <>BDC ( )Tj EMC 7 0 0 7 326.2278 474.9528 Tm [(OEW/DO)7.1(W - lbs)]TJ How Many Flight Attendants Are on a Plane. BT 0 841.89 609.449 -841.89 re ET EMC EMC 0 J 0 j 5 w 10 M [] 0 d BT EMC /P <>BDC ( )Tj BT BT 7 0 0 7 387.0159 584.9528 Tm 9 0 0 9 53.8578 225.8898 Tm BT 0 Tc EMC 7 0 0 7 108.6215 243.9528 Tm ET BT ET -.02 Tc /P <>BDC ET BT EMC ET 9 0 0 9 232.4217 170.8898 Tm 9 0 0 9 380.2477 247.8898 Tm EMC -.02 Tc 304.725 420.96 m EMC /P <>BDC Centre tank pumps EMC EMC ET ( )Tj ET 9 0 0 9 528.7084 742.8898 Tm BT BT BT (0.0115)Tj 13 0 0 13 36.8504 71.8898 Tm ET ( )Tj ( )Tj /P <>BDC ( )Tj /P <>BDC /P <>BDC BT ( )Tj BT EMC EMC /P <>BDC /P <>BDC ET EMC /P <>BDC 9 0 0 9 36.8504 324.8898 Tm -.02 Tc EMC (CFM56-7B26)Tj EMC 7 0 0 7 320.7537 78.9528 Tm -.02 Tc BT BT EMC ET ET (380-396)Tj EMC EMC ET 0 Tc BT EMC ET -.02 Tc BT EMC (CFM56-5B3/P)Tj .41 .161 .508 rg 7 0 0 7 118.104 364.7654 Tm 8 0 0 8 153.6923 633.9528 Tm EMC EMC EMC /P <>BDC Due to the additional structural)Tj EMC ET EMC (34,650)Tj ET 7 0 0 7 141.7322 507.9528 Tm ET ( )Tj 0 Tc BT The aircraft also features)Tj EMC Engine size 515.814 89.864 l /P <>BDC ( )Tj BT 7 0 0 7 158.74 683.7654 Tm /P <>BDC ET ET 7 0 0 7 535.5029 573.7654 Tm ( )Tj ET 9 0 0 9 215.433 357.8898 Tm EMC /P <>BDC ( )Tj 9 0 0 9 246.595 159.8898 Tm BT EMC BT /P <>BDC /P <>BDC 0 Tc 9 0 0 9 196.8605 115.8898 Tm BT /P <>BDC -.02 Tc /OC /MC186 BDC EMC BT 7 0 0 7 384.8358 683.7654 Tm -.02 Tc (294)Tj ET EMC 0 Tc (114)Tj 7 0 0 7 521.4089 11.5132 Tm 0 Tc 9 0 0 9 394.0315 247.8898 Tm (A320neo)Tj EMC EMC /P <>BDC /P <>BDC 0 Tc BT BT (3,443)Tj /P <>BDC /P <>BDC BT EMC ET EMC ET ET EMC (2,517)Tj BT /P <>BDC /P <>BDC /P <>BDC ( )Tj 36.85 824.882 572.599 17.008 re /P <>BDC 7 0 0 7 337.7614 78.7654 Tm EMC ET ET EMC 9 0 0 9 211.8218 533.8898 Tm Adobe d 0 Tc ET 7 0 0 7 321.6356 210.9528 Tm /P <>BDC 9 0 0 9 394.0237 368.8898 Tm 7 0 0 7 387.0159 617.9528 Tm ET BT 7 0 0 7 114.6416 298.9528 Tm EMC ( )Tj ( )Tj /P <>BDC (Top), Specification Table Boeing 737 Next Gen and Max.(Top). -.02 Tc 0 Tc BT refuelling panel to AUX TANKS. -.02 Tc BT BT /P <>BDC EMC EMC /P <>BDC 6.5 0 0 6.5 296.2827 637.9529 Tm EMC 7 0 0 7 99.8582 309.7654 Tm /P <>BDC 0 Tc EMC /P <>BDC /P <>BDC BT /P <>BDC (comparison of the performance of the eight)Tj /P <>BDC 0 Tc EMC (O)Tj 6 0 0 6 444.4713 757.9528 Tm BT ( )Tj The fuel tank was instrumented with gas sample tubing and thermocouples to BT BT ( )Tj BT ET /P <>BDC BT endstream 7 0 0 7 99.8582 705.7654 Tm /P <>BDC /P <>BDC f (217)Tj BT 7 0 0 7 535.5029 188.7654 Tm ET BT BT BT ET BT ( )Tj 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. 6 0 0 6 527.6392 757.9528 Tm ( )Tj ET EMC ( N)Tj ET 0 Tc 6 0 0 6 115.2799 687.9528 Tm -.02 Tc 6 0 0 6 490.4508 729.9528 Tm /P <>BDC -.07 Tc /P <>BDC ET EMC /P <>BDC ( )Tj ET ET ( N)Tj ET /P <>BDC 6.5 0 0 6.5 528.5291 650.9529 Tm 9 0 0 9 36.8504 181.8898 Tm /P <>BDC 0 Tc EMC ET 7 0 0 7 380.2788 265.7654 Tm -.02 Tc 8 0 0 8 302.5117 675.9528 Tm ET ET ET -.01 Tc BT A previous model which had success was Airbuses A320. ET /P <>BDC 7 0 0 7 54.7071 617.7654 Tm BT -.02 Tc ET 7 0 0 7 54.7071 716.7654 Tm -.02 Tc 7 0 0 7 456.7412 661.7654 Tm The use of composite materials in the 737 Next Gen or even the 737 Max is quite conservative. BT .964 .834 .406 rg EMC ( The reserve fuel policy )Tj -.02 Tc /P <>BDC -.02 Tc ET BT EMC -.02 Tc EMC BT EMC BT BT 9 0 0 9 173.6527 500.8898 Tm BT EMC -.02 Tc EMC EMC 0 Tc BT ( )Tj EMC 0 Tc 6.5 0 0 6.5 488.8955 532.9529 Tm ( )Tj 9 0 0 9 520.9143 511.8898 Tm /P <>BDC /P <>BDC /P <>BDC /P <>BDC ET /P <>BDC ET EMC /P <>BDC 0 Tc (14 sectors. 6 0 0 6 331.4048 687.9528 Tm ( )Tj EMC than the main wing tanks. 0 Tc EMC 7 0 0 7 362.3891 144.9528 Tm 7 0 0 7 355.5753 562.7654 Tm ET how can i know the material of 737NGs nose landing gear lower drag strut?thank you. (capacity has been configured as the same)Tj
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