737 800 fuel capacity pounds

EMC ET ET ( )Tj 9 0 0 9 508.4714 38.8898 Tm BT BT )Tj ( )Tj ET EMC EMC /P <>BDC -.02 Tc /P <>BDC 0 Tc EMC 7 0 0 7 158.74 331.7654 Tm EMC /P <>BDC BT ET This includes the weight of the plane, which is about 41,000 kg (90,000 lbs), and the weight of the fuel which is about 18,000 kg (40,000 lbs). 7 0 0 7 554.7883 166.7654 Tm 0 Tc higher. [(BOS-DF)-13.9(W)]TJ 10 0 0 10 47.7404 814.1973 Tm Some accidents involving the Boeing 737-800 have resulted in the death or injury of passengers aboard. BT BT ET /P <>BDC ET 9 0 0 9 68.0071 423.8898 Tm ( )Tj ( )Tj EMC (evaluated for both types, the 737-)Tj (\(see tables,)Tj BT ET 7 0 0 7 554.7883 408.7654 Tm BT BT ET Airbus seals the deal to reinvigorate the QANTAS Fleet. /P <>BDC EMC (0.0126)Tj /P <>BDC EMC ET ( )Tj EMC /P <>BDC .151 .147 .15 RG BT 6.5 0 0 6.5 244.2974 545.9529 Tm !! EMC 0 Tc ET BT ET EMC /GS2 gs EMC ET ( )Tj 7 0 0 7 54.7071 595.7654 Tm exacerbating the imbalance. ET /P <>BDC EMC ( )Tj /P <>BDC S EMC (cost index calculated by the airline to the)Tj -.02 Tc (38,168)Tj ET EMC 9 0 0 9 53.8582 214.8898 Tm 7 0 0 7 403.478 617.7654 Tm /Artifact <>BDC 9 0 0 9 54.9417 794.1039 Tm ET (when using a cost index. ET 7 0 0 7 445.619 375.7654 Tm /P <>BDC 9 0 0 9 566.3776 192.8898 Tm /P <>BDC /P <>BDC (82,110)Tj EMC BT BT EMC BT /P <>BDC ( )Tj /F4 1 Tf 0 Tc 7 0 0 7 125.6292 584.7654 Tm BT ET 6.5 0 0 6.5 499.22 598.9529 Tm BT 9 0 0 9 53.8338 390.8898 Tm (47,000)Tj ET ( )Tj ET /P <>BDC BT BT ET /P <>BDC BT ( )Tj EMC ET ET )Tj BT BT ET ET In payload scenario 1 the)Tj ET ET ET 9 0 0 9 360.9639 192.8898 Tm BT EMC -.01 Tc EMC EMC ( )Tj q (they are replacing. 7 0 0 7 247.7395 705.7654 Tm (A US domestic reserve policy was)Tj ( )Tj ET 7 0 0 7 82.8504 221.9528 Tm -.02 Tc ( )Tj ET EMC /P <>BDC BT ET 9 0 0 9 394.0237 467.8898 Tm 0 841.89 609.449 -841.89 re EMC ET 6.5 0 0 6.5 378.2463 637.9529 Tm 0 Tc ET (1.5 mm) thick, the extent of the frost is similar on both wings, the frost is on or between the black lines defining /P <>BDC If a fuel gauge is u/s the quantity /P <>BDC EMC EMC 0 Tc /P <>BDC (170)Tj BT /P <>BDC (comparison focused on the fuel burn)Tj /P <>BDC 0 Tc ET 7 0 0 7 474.7064 100.9528 Tm 0 Tc (passenger payload. ET EMC -.02 Tc EMC BT Specification Table Boeing 737 Original and Boeing 737 Classic. /P <>BDC BT ( )Tj BT 9 0 0 9 294.2183 346.8898 Tm ( )Tj ( )Tj ET /P <>BDC 9 0 0 9 423.3885 401.8898 Tm /P <>BDC BT ( )Tj EMC Max. ET 9 0 0 9 53.8582 423.8898 Tm /P <>BDC ET EMC -.02 Tc -.02 Tc ( )Tj ( )Tj EMC (A320neo:)Tj 56 0 0 56 447.1169 682.1944 Tm BT 9 0 0 9 53.8582 764.8898 Tm ET BT ET ET BT EMC /P <>BDC ( )Tj ET ET (35,112)Tj 7 0 0 7 37.5838 441.9528 Tm BT /P <>BDC EMC ( )Tj -.02 Tc EMC /P <>BDC /P <>BDC ( )Tj BT EMC ET ET ET ET /P <>BDC EMC ET 7 0 0 7 141.7322 188.9528 Tm 7 0 0 7 125.6292 232.7654 Tm ET ET 9 0 0 9 215.433 445.8898 Tm EMC BT /P <>BDC (Block time - mins)Tj /P <>BDC /F6 1 Tf ET EMC /P <>BDC /F1 1 Tf /OC /MC1346 BDC BT ET ( )Tj EMC ET 9 0 0 9 232.4217 412.8898 Tm ( )Tj BT BT BT BT /P <>BDC BT 9 0 0 9 232.438 434.8898 Tm ET /P <>BDC ET ET (weight variants for this aircraft. ET 7 0 0 7 343.2355 518.7654 Tm EMC BT 7 0 0 7 365.035 617.9528 Tm EMC ( )Tj ET -.02 Tc /P <>BDC -.005 Tc /P <>BDC -.02 Tc /P <>BDC BT (longest sector. ( )Tj EMC EMC 9 0 0 9 533.9409 390.8898 Tm ET (choice of engine variant. 8 0 0 8 38.4438 731.9528 Tm ET (similar rate, with Boeing having delivered)Tj EMC EMC ET (and the A321ceo and A321neo. EMC ( )Tj ET (170)Tj 9 0 0 9 213.7241 467.8898 Tm ET 7 0 0 7 403.478 419.7654 Tm EMC /P <>BDC EMC sectors to ensure an even fuel balance. ( )Tj ET ET EMC -.02 Tc ( )Tj EMC BT EMC BT 9 0 0 9 229.6064 456.8898 Tm This study uses a)Tj 137 )Tj EMC 6.5 0 0 6.5 346.3049 676.9529 Tm 7 0 0 7 315.5217 562.7654 Tm 7 0 0 7 141.7322 89.9528 Tm 9 0 0 9 215.4409 357.8898 Tm 28.5749 0 TD BT 0 Tc -.02 Tc 9 0 0 9 232.4217 203.8898 Tm ET /P <>BDC BT ET 9 0 0 9 381.3998 126.8898 Tm ET /P <>BDC 8 0 0 8 38.4438 745.9528 Tm -.02 Tc 0 Tc EMC BT BT 7 0 0 7 457.0984 133.7654 Tm /P <>BDC /P <>BDC 0 Tc BT 0 Tc 0 Tc /P <>BDC 361 0 obj -.02 Tc ( )Tj FQIS accuracy: +/- 3.0% 0 Tc ( )Tj 0 Tc (163)Tj 8 0 0 8 480.7187 771.9529 Tm (assumes that an equal number of)Tj BT (includes checked and carry-on luggage. ( )Tj 0 Tc /P <>BDC ET (37,653lbs )Tj 9 0 0 9 215.4409 148.8898 Tm BT ( )Tj ET ET 6.5 0 0 6.5 448.3675 532.9529 Tm Is the Range with Max Payload NM(Km) wrong? /P <>BDC BT EMC /P <>BDC /F1 1 Tf 7 0 0 7 491.7142 67.7654 Tm BT /P <>BDC BT /P <>BDC ( )Tj 7 0 0 7 298.1781 67.9528 Tm /P <>BDC -.02 Tc ET ET 0 Tc BT ET EMC ( )Tj BT 9 0 0 9 384.8177 445.8898 Tm 6.5 0 0 6.5 114.0477 545.9529 Tm ET 9 0 0 9 524.2249 478.8898 Tm (187,700)Tj (a cost index, which is a more cost-efficient)Tj BT 6.5 0 0 6.5 93.2476 702.9529 Tm BT EMC 9 0 0 9 389.0497 445.8898 Tm ET (4,863)Tj ( )Tj BT BT BT EMC EMC ( )Tj BT 0 Tc BT /P <>BDC (2,728)Tj BT ( )Tj EMC ( )Tj BT /P <>BDC ET -.02 Tc EMC EMC EMC /P <>BDC 19.841 0 l -.02 Tc ET EMC ET /P <>BDC /P <>BDC ( )Tj BT /P <>BDC EMC BT (65,688)Tj ( )Tj (A320neo, A321neo, 737-800, 737-)Tj BT /P <>BDC Q 0 Tc BT BT ET 9 0 0 9 194.5468 71.8898 Tm 5 0 0 5 484.5872 11.5129 Tm 9 0 0 9 68.3339 467.8898 Tm (the planned payload of 170. ( )Tj BT ET 7 0 0 7 364.1531 122.9528 Tm /P <>BDC EMC /P <>BDC ET ET EMC /P <>BDC ET 6.5 0 0 6.5 227.9655 565.9529 Tm (831)Tj 0 Tc /P <>BDC ( )Tj ET 0 Tc 7 0 0 7 204.0935 584.7654 Tm ( )Tj ET ( )Tj 0 Tc EMC 13 0 0 13 215.4313 115.8898 Tm /P <>BDC EMC 0 Tc /P <>BDC ET /Im2 Do ( )Tj ( )Tj ( )Tj EMC BT BT -.02 Tc 7 0 0 7 338.6433 320.7654 Tm ( )Tj -.02 Tc 7 0 0 7 99.8582 309.7654 Tm BT Q 9 0 0 9 530.624 269.8898 Tm BT /P <>BDC 0 Tc BT ( )Tj 0 Tc -.02 Tc ( )Tj 9 0 0 9 142.2128 335.8898 Tm EMC ET BT /P <>BDC ET ( )Tj /P <>BDC BT EMC ET -12.427 302.461 389.443 -271.279 re BT ET ET ( )Tj 10 0 0 10 52.6304 814.1973 Tm ET BT -.02 Tc BT /P <>BDC /P <>BDC (more seats. /P <>BDC (34,650)Tj 8 0 0 8 124.845 717.9528 Tm EMC 0 Tc EMC BT /P <>BDC EMC (The sectors are chosen to ensure a)Tj ( )Tj 7 0 0 7 321.6356 375.9528 Tm 0 J 0 j 5 w 10 M [] 0 d EMC EMC 0 Tc (178)Tj ( A)Tj ( )Tj ( )Tj ET It requires a 2316 meter or 7,598.33 feet of take off distance. BT /P <>BDC BT 9 0 0 9 367.2172 269.8898 Tm /P <>BDC EMC 9 0 0 9 529.0344 445.8898 Tm BT 9 0 0 9 518.9756 49.1073 Tm /P <>BDC ET 9 0 0 9 53.8578 357.8898 Tm -.02 Tc /P <>BDC BT BT (377,550)Tj y9ou may find what you are looking for by clicking here. EMC /P <>BDC /P <>BDC EMC BT EMC 6.5 0 0 6.5 284.897 532.9529 Tm EMC EMC 7 0 0 7 141.7322 210.9528 Tm EMC -.02 Tc /P <>BDC /P <>BDC BT ET 9 0 0 9 394.0315 522.8898 Tm ( )Tj BT EMC BT (3,300 - )Tj q ET EMC (ONT/73)Tj /P <>BDC BT 8 0 0 8 258.7094 760.9528 Tm 8 0 0 8 187.3427 661.9528 Tm (34,650)Tj /P <>BDC /P <>BDC 9 0 0 9 232.438 258.8898 Tm (between the aircraft types even greater. ET ET BT BT /P <>BDC (136)Tj [(OM)8(M)-13(E)-25(R)7(C)8(E)]TJ -.02 Tc BT BT /P <>BDC /P <>BDC 6.5 0 0 6.5 191.8316 637.9529 Tm /P <>BDC 8 0 0 8 394.0237 82.8898 Tm BT 6.5 0 0 6.5 399.2659 565.9529 Tm -.02 Tc BT 7 0 0 7 404.101 298.7654 Tm (superior fuel burn per seat-mile of all)Tj /P <>BDC ET ET EMC ( )Tj ET 9 0 0 9 376.2498 478.8898 Tm 9 0 0 9 53.8582 203.8898 Tm EMC BT ET 9 0 0 9 187.3661 445.8898 Tm 9 0 0 9 215.4313 511.8898 Tm 137 )Tj ET (orders, while the 737-800 and 737-900ER)Tj BT EMC BT BT /P <>BDC EMC (/S)Tj (The specifications and weights of all)Tj /P <>BDC ( )Tj 7 0 0 7 456.2165 144.7654 Tm ET ET ET /P <>BDC /P <>BDC ET 7 0 0 7 113.1366 320.9528 Tm -.02 Tc ( )Tj (114)Tj 7 0 0 7 537.7804 232.9528 Tm ET BT EMC EMC EMC ET /P <>BDC /P <>BDC BT ET 7 0 0 7 141.7322 595.9528 Tm EMC (248,064)Tj 7 0 0 7 355.3163 166.7654 Tm BT 9 0 0 9 215.4313 280.8898 Tm /P <>BDC ET EMC ET EMC EMC [(Aircr)10(aft)]TJ /P <>BDC ET These are: Below is a table of the main features and specifications for the Boeing 737 family of aircraft. Q EMC /P <>BDC 6.5 0 0 6.5 54.877 598.9529 Tm 8 0 0 8 153.6923 591.9528 Tm EMC (5,791)Tj EMC ET /P <>BDC /P <>BDC BT 7 0 0 7 158.74 661.7654 Tm ( )Tj 7 0 0 7 298.1781 111.9528 Tm EMC ( )Tj 7 0 0 7 182.5706 177.9528 Tm EMC ET BT BT ET ( )Tj EMC (482)Tj 7 0 0 7 427.7291 188.9528 Tm /P <>BDC EMC -.02 Tc ET EMC BT ( )Tj 7 0 0 7 429.157 595.9528 Tm BT /P <>BDC (CFM56-5B3/P)Tj ET -.01 Tc ET ET /P <>BDC /P <>BDC ET -.02 Tc 0 Tc 0 Tc 15 w BT EMC BT ET ET 7 0 0 7 107.1165 276.9528 Tm 0 Tc ET EMC 9 0 0 9 215.4409 434.8898 Tm EMC BT EMC ( )Tj EMC BT ET EMC 431 0 obj ET (282)Tj (configurations used for these aircraft types)Tj EMC /P <>BDC 8 0 0 8 64.6596 760.9529 Tm /P <>BDC -.02 Tc -.02 Tc 7 0 0 7 279.1575 595.9528 Tm EMC EMC /P <>BDC -.01 Tc (weight penalty in its OEW compared to its)Tj 0 Tc 6.5 0 0 6.5 485.8925 735.9529 Tm 7 0 0 7 67.798 11.5132 Tm )Tj /P <>BDC ET ET ET /P <>BDC ET /P <>BDC (2,517)Tj EMC 9 0 0 9 146.3 346.8898 Tm ET ET BT BT -.02 Tc BT ET q 1 0 0 1 505.328 82.247 cm 0 0 m BT BT EMC /P <>BDC EMC EMC 6 0 0 6 539.8061 760.9528 Tm BT /P <>BDC W n BT 0 Tc EMC ET (thereby giving it a seat capacity of 160)Tj ( )Tj BT 0 Tc EMC -.01 Tc /P <>BDC ( )Tj BT 9 0 0 9 545.1909 346.8898 Tm ET This would make)Tj BT ( )Tj ET ET /P <>BDC 9 0 0 9 394.0157 93.8898 Tm ( )Tj EMC /P <>BDC (282)Tj ET 304.725 420.96 m ET (ESAD)Tj BT .41 .161 .508 RG BT ET Hi Jeffrey, ET BT /P <>BDC 7 0 0 7 508.4124 716.7654 Tm BT 0 Tc 7 0 0 7 60.6117 243.7654 Tm EMC /P <>BDC BT EMC 8 0 0 8 187.3427 591.9528 Tm BT EMC ET ( )Tj ET EMC /P <>BDC 7 0 0 7 518.4953 210.9528 Tm EMC ( )Tj 7 0 0 7 314.6398 716.7654 Tm (CFM56-7B26)Tj 9 0 0 9 36.8504 456.8898 Tm BT /P <>BDC (571)Tj ET 7 0 0 7 386.4701 419.9528 Tm ET EMC EMC BT ET /P <>BDC 0 Tc EMC ET ET 9 0 0 9 215.433 93.8898 Tm EMC ET EMC EMC EMC ET 0 Tc 9 0 0 9 550.3917 456.8898 Tm EMC /P <>BDC ET ( )Tj ET EMC EMC BT 9 0 0 9 186.3413 291.8898 Tm ET 0 Tc /P <>BDC 8 0 0 8 302.5117 591.9528 Tm ET 0 Tc 518.723 0 l BT EMC ET 8 0 0 8 43.6039 633.9528 Tm BT /P <>BDC -.02 Tc /P <>BDC ET 9 0 0 9 425.1913 214.8898 Tm /P <>BDC ET 0 Tc BT BT ( )Tj ET 7 0 0 7 554.7883 716.7654 Tm 9 0 0 9 342.0176 126.8898 Tm BT 9 0 0 9 53.8338 60.8898 Tm 7 0 0 7 230.7317 694.9528 Tm 0 Tc EMC 9 0 0 9 211.7668 225.8898 Tm EMC /P <>BDC (1,825)Tj EMC /P <>BDC -.01 Tc /P <>BDC 7 0 0 7 247.7395 364.7654 Tm ET ET 9 0 0 9 215.433 291.8898 Tm ( )Tj ET /P <>BDC EMC These improvements include the redesign of fuel pumps, FQIS, any 9 0 0 9 360.0909 115.8898 Tm ET BT ET BT BT (Federal Aviation Administration) have cleaned up their act and made the MAX as safe an airliner as its predecessors. 9 0 0 9 215.433 379.8898 Tm EMC /P <>BDC (bypass ratio of 5.7:1, and is rated at)Tj 0 Tc ET -.02 Tc ET BT 9 0 0 9 215.4409 500.8898 Tm BT /P <>BDC EMC 7 0 0 7 37.0536 595.9528 Tm BT /P <>BDC /P <>BDC 6 0 0 6 527.8009 743.9528 Tm /P <>BDC EMC EMC Can you please tell me where to look for the cabin height,width, seat height, width and door to door length. ET BT ( )Tj -.01 Tc ( )Tj EMC 9 0 0 9 360.5848 104.8898 Tm /P <>BDC /P <>BDC EMC ET ET 7 0 0 7 440.0906 276.9528 Tm Since no two)Tj BT ( )Tj EMC /P <>BDC (5,350)Tj (170)Tj BT 7 0 0 7 536.3849 408.7654 Tm (170)Tj /P <>BDC (or scenarios in this study. (PPS flight planning software is used to)Tj /P <>BDC S (170)Tj ET BT EMC BT -.02 Tc ( )Tj 8 0 0 8 187.3427 577.9528 Tm This is despite the 737-8s)Tj BT EMC The typical range for this)Tj 9 0 0 9 385.653 71.8898 Tm /P <>BDC ( )Tj 7 0 0 7 141.7322 122.9528 Tm /P <>BDC ET /P <>BDC ET 6.5 0 0 6.5 282.0695 735.9529 Tm ET BT 0 Tc (ASM of 0.55 to 0.88 cents per ASM)Tj EMC ET ( )Tj /P <>BDC ( )Tj ET caused the FAA to issue SFAR88 in June 2001 which mandates improvements to the 7 0 0 7 230.7317 397.9528 Tm /P <>BDC 0 Tc 7 0 0 7 490.5101 716.9528 Tm ( )Tj 7 0 0 7 490.5101 540.9528 Tm 6 0 0 6 309.2107 771.9528 Tm EMC 6.5 0 0 6.5 64.6596 558.9529 Tm ET ( )Tj ( )Tj EMC EMC ET EMC ( )Tj /P <>BDC ET ET BT /P <>BDC 7 0 0 7 366.0641 694.9528 Tm 517.244 80.729 l BT -2.0374 -.5351 -2.4615 -.7535 -2.6921 -1.1048 c 9 0 0 9 355.7787 379.8898 Tm ET -.02 Tc EMC EMC /P <>BDC EMC (The spot fuel price for the US aviation)Tj -.02 Tc /P <>BDC /P <>BDC 9 0 0 9 563.4796 324.8898 Tm 0 Tc EMC /P <>BDC EMC -.02 Tc EMC 0 Tc ET EMC EMC /P <>BDC ET BT EMC EMC 7 0 0 7 99.8582 320.7654 Tm ET EMC EMC 7 0 0 7 519.3773 166.9528 Tm EMC EMC 7 0 0 7 258.2805 463.7654 Tm ET ( )Tj ET 9 0 0 9 215.4409 203.8898 Tm BT 9 0 0 9 215.4313 412.8898 Tm ET /P <>BDC ET /P <>BDC /P <>BDC In-flight, the GW must be periodically ET -.02 Tc 6 0 0 6 372.295 673.9528 Tm 0 Tc BT EMC ET (The comparison will be for eight)Tj 6.5 0 0 6.5 397.1664 735.9529 Tm /P <>BDC 9 0 0 9 390.5438 566.8898 Tm ( )Tj 7 0 0 7 158.74 606.7654 Tm /F4 1 Tf BT ( )Tj 6.5 0 0 6.5 398.3298 637.9529 Tm EMC /P <>BDC (20)Tj ET EMC /P <>BDC BT 0 Tc 9 0 0 9 394.0237 170.8898 Tm 9 0 0 9 192.1373 401.8898 Tm /P <>BDC 7 0 0 7 539.8962 727.9528 Tm /P <>BDC The aircraft look like standard -800s, so why the difference? BT EMC BT EMC /P <>BDC -.3738 -6.1596 -.9177 -6.351 -1.6458 -6.3504 c EMC EMC EMC BT (191,100)Tj BT ( )Tj /GS1 gs BT ET /P <>BDC /P <>BDC 9 0 0 9 36.8504 467.8898 Tm /P <>BDC ET /P <>BDC ET ET 9 0 0 9 376.7938 500.8898 Tm -.02 Tc /P <>BDC 8 0 0 8 365.7704 619.9528 Tm BT ET (2,207)Tj /P <>BDC (and fuel burn per ASM for the four pairs)Tj [(T)53.9(r)10(acked distance - nm)]TJ EMC q 1 0 0 1 215.441 458.878 cm 0 0 m In this scenario, the calculated)Tj -.02 Tc /P <>BDC 7 0 0 7 520.6108 606.9528 Tm 7 0 0 7 294.4014 738.7654 Tm BT ( )Tj /P <>BDC (977)Tj /P <>BDC BT EMC BT /P <>BDC 9 0 0 9 552.6886 533.8898 Tm ( )Tj ( )Tj (performance, it was also assumed there)Tj /F5 1 Tf EMC ( )Tj /P <>BDC EMC 9 0 0 9 53.8582 731.8898 Tm BT 8 0 0 8 394.0237 71.8898 Tm -.02 Tc ET [(A3)24.9(20ceo v)12.9(ersus A3)24.9(20neo )]TJ EMC ET BT 7 0 0 7 535.5029 683.7654 Tm 7 0 0 7 363.2711 540.9528 Tm ( )Tj ET 7 0 0 7 381.1608 573.7654 Tm ET (passenger payload - nm)Tj 7 0 0 7 321.6356 232.9528 Tm BT (31,416)Tj (176)Tj /P <>BDC EMC EMC 0 Tc ET 7 0 0 7 344.1175 639.7654 Tm (163,900)Tj EMC 9 0 0 9 515.9449 654.8898 Tm -.02 Tc This is universally considered to be the BT EMC 9 0 0 9 571.3269 38.8898 Tm /P <>BDC ET /GS1 gs (airport charges, while the time-dependent)Tj EMC BT ET EMC (. EMC BT 7 0 0 7 99.8582 683.7654 Tm 7 0 0 7 54.5916 254.7654 Tm Waking the giant, the return of the Airbus A380. ET ( )Tj The -1/200 panel also has EMC EMC (4,716)Tj 6 0 0 6 289.3167 757.9528 Tm EMC ET (34,650)Tj 9 0 0 9 203.511 621.8898 Tm endobj ( )Tj EMC ET 7 0 0 7 456.4753 716.7654 Tm (. 7 0 0 7 474.7064 188.9528 Tm ET BT /P <>BDC ET (1,138)Tj BT EMC EMC BT 9 0 0 9 215.433 214.8898 Tm BT BT 7 0 0 7 247.7395 540.7654 Tm BT -.02 Tc EMC EMC 7 0 0 7 299.0601 265.9528 Tm ET /P <>BDC /P <>BDC (5,448)Tj BT )Tj ( )Tj 0 Tc EMC BT ET ET 9 0 0 9 361.2861 181.8898 Tm ( )Tj /P <>BDC (737-8)Tj BT EMC ( )Tj EMC ET BT ( )Tj ET BT 9 0 0 9 366.6417 137.8898 Tm 9 0 0 9 206.8407 412.8898 Tm BT -.02 Tc EMC BT (The Sky interior means the MAX)Tj ET EMC /P <>BDC BT (. ET ET 7 0 0 7 366.0641 738.9528 Tm ET ET BT ET 9 0 0 9 215.4409 170.8898 Tm 9 0 0 9 196.4663 137.8898 Tm 7 0 0 7 82.2047 529.9528 Tm EMC EMC ET ET /OC /MC852 BDC /P <>BDC /P <>BDC ( )Tj ET ET Do you have a reference please? BT (into service in 2023. -.02 Tc ET 0 Tc BT EMC (31,416)Tj EMC -.02 Tc BT /F6 1 Tf /P <>BDC /GS2 gs /P <>BDC ET /P <>BDC /P <>BDC /P <>BDC BT ET ( )Tj BT EMC 7 0 0 7 354.4763 661.7654 Tm EMC ET BT ET EMC /P <>BDC BT ET /P <>BDC 9 0 0 9 53.8338 335.8898 Tm BT Leaving a fuel pump on with a low pressure light ( )Tj ( )Tj (831)Tj EMC BT 7 0 0 7 440.0906 133.9528 Tm /P <>BDC 7 0 0 7 440.0906 232.9528 Tm .023 .567 .626 rg /P <>BDC 7 0 0 7 490.7815 375.9528 Tm ET 6.5 0 0 6.5 532.7606 598.9529 Tm ( A)Tj BT 7 0 0 7 490.8321 375.7654 Tm -.02 Tc ET EMC BT -.02 Tc /P <>BDC ET /P <>BDC q 1 0 0 1 215.441 73.878 cm 0 0 m ( )Tj /P <>BDC ET /P <>BDC BT 9 0 0 9 232.438 324.8898 Tm 0 Tc q 1 0 0 1 36.85 425.878 cm 0 0 m (0.0112)Tj BT BT 7 0 0 7 86.3128 540.7654 Tm BT BT (737-8)Tj EMC ET ET ET /P <>BDC 9 0 0 9 200.4401 258.8898 Tm ET /P <>BDC /P <>BDC EMC /P <>BDC EMC ET (403-418)Tj ET EMC EMC ( )Tj EMC (98,500)Tj ET ET ET EMC BT ( )Tj -.01 Tc /P <>BDC (575)Tj EMC 8 0 0 8 136.4919 619.9528 Tm ET ET BT 0 Tc /P <>BDC 0 Tc /P <>BDC BT BT BT 7 0 0 7 428.6112 386.9528 Tm ET /P <>BDC 10 0 0 10 55.0104 814.1973 Tm (operation. EMC EMC [(E)-7.8(P)16.1(T)9(E)-13.9(MBE)-16.9(R)]TJ /P <>BDC ET 137 )Tj ET .151 .147 .15 rg EMC /P <>BDC (with 2,000 feet separation. ( )Tj EMC /P <>BDC -.02 Tc ET EMC ET EMC EMC BT EMC 9 0 0 9 411.0097 148.8898 Tm /F6 1 Tf 7 0 0 7 459.6601 11.5129 Tm ET /P <>BDC EMC EMC (distance - nm )Tj EMC /P <>BDC BT /P <>BDC ET BT EMC 7 0 0 7 297.632 595.9528 Tm EMC BT BT ET EMC 7 0 0 7 250.5326 100.7654 Tm ET EMC /P <>BDC 6.5 0 0 6.5 426.4819 676.9529 Tm 9 0 0 9 205.7907 236.8898 Tm ET ET ET ET EMC 6 0 0 6 61.517 743.9528 Tm EMC BT (The A321neo is offered to airlines with)Tj 340.159 0 l ET ET BT 7 0 0 7 445.7203 11.5129 Tm /P <>BDC 7 0 0 7 338.3085 188.9528 Tm /P <>BDC 6.5 0 0 6.5 549.8557 624.9529 Tm In contrast, Boeing has)Tj /P <>BDC -.01 Tc (. -.01 Tc (portion of the flight in the cruise phase,)Tj EMC ET ( )Tj EMC BT 7 0 0 7 456.2165 111.7654 Tm EMC (A321ceo was payload-limited on the route)Tj BT /P <>BDC ET BT EMC [(BOS-SE)-13.9(A)]TJ /F4 1 Tf 7 0 0 7 258.2805 573.7654 Tm ET (737-800:)Tj ( )Tj BT /P <>BDC 0 Tc 0 Tc /P <>BDC ET ET EMC -.02 Tc ( )Tj ET ( )Tj 9 0 0 9 553.6047 423.8898 Tm ET ET ET What are the Boeing 787 Dreamliner Specs? BT EMC EMC 0 Tc EMC /P <>BDC 9 0 0 9 215.4313 478.8898 Tm /P <>BDC /P <>BDC ET ET 13 0 0 13 205.5668 412.8898 Tm 7 0 0 7 429.157 562.9528 Tm BT BT EMC 7 0 0 7 338.5674 133.9528 Tm ET EMC (powered by either the CFM56-5 series or)Tj /P <>BDC permissible, provided the following are met: The standard number of fuel tanks is three. ET 0 Tc BT 0 Tc ( )Tj 7 0 0 7 113.1366 419.9528 Tm /P <>BDC EMC ET 7 0 0 7 337.4684 694.9528 Tm BT EMC -.02 Tc BT ET ( )Tj EMC EMC W n 7 0 0 7 490.8321 265.7654 Tm ( )Tj ET /P <>BDC (1,059)Tj 7 0 0 7 54.7071 287.7654 Tm 7 0 0 7 474.3564 562.9528 Tm EMC BT /P <>BDC -.02 Tc EMC (26,000lbs thrust on the A320neo powered)Tj ET ET EMC 9 0 0 9 386.3946 137.8898 Tm (208)Tj BT EMC -.02 Tc BT BT /P <>BDC EMC BT -.02 Tc BT BT BT ET EMC ET BT 6 0 0 6 214.7788 729.9528 Tm EMC -.02 Tc BT /P <>BDC BT BT /P <>BDC 7 0 0 7 384.8358 683.7654 Tm /P <>BDC EMC It is simply an 800 with certain modifications that might have been stipulated by the customer airliner. /P <>BDC /P <>BDC EMC (The A320neo has a 0.55-0.69 cents per)Tj 0 Tc EMC /P <>BDC 0 Tc 7 0 0 7 387.0159 485.9528 Tm BT ET ( )Tj EMC 7 0 0 7 37.5838 463.9528 Tm 9 0 0 9 394.0237 247.8898 Tm -.02 Tc .41 .161 .508 RG (16,170)Tj /P <>BDC /F1 1 Tf 7 0 0 7 386.3929 573.9528 Tm EMC ( )Tj (A)Tj /P <>BDC 6.5 0 0 6.5 426.4819 689.9529 Tm ( )Tj /P <>BDC BT (scheduled times planned by the carrier may)Tj -.02 Tc (39,270)Tj BT [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ 9 0 0 9 229.6064 390.8898 Tm 9 0 0 9 411.0181 203.8898 Tm /P <>BDC BT /P <>BDC 8 0 0 8 54.0516 771.7654 Tm EMC (3,069)Tj EMC (operation the overflight and airport)Tj 9 0 0 9 206.7178 181.8898 Tm (that in real airline operations the taxi-out)Tj 0 Tc 6.5 0 0 6.5 295.7432 545.9529 Tm BT f -.02 Tc /P <>BDC must be switched OFF when both LP lights illuminate. ( )Tj 0 Tc 9 0 0 9 341.891 335.8898 Tm EMC 7 0 0 7 43.6039 243.9528 Tm 8 0 0 8 365.7704 717.9528 Tm The 737-800 is used in airlines such as Aircal, Delta Air Lines, New York Air and United Airlines just to name a few. (1,272)Tj -.02 Tc EMC /P <>BDC ET ET (0.0149)Tj ET ET BT ( )Tj EMC ET ( )Tj /P <>BDC 0 Tc /P <>BDC /P <>BDC 5 0 0 5 92.725 11.5132 Tm /P <>BDC ( )Tj BT (977)Tj BT BT ET ( )Tj 7 0 0 7 258.2805 419.7654 Tm /P <>BDC -.01 Tc ET EMC BT ET EMC BT -2.5295 -5.0573 -2.1058 -5.3146 -1.5527 -5.3151 c 7 0 0 7 37.6993 276.9528 Tm ET BT BT EMC EMC EMC ( )Tj -.02 Tc ET 9 0 0 9 377.4586 676.8898 Tm EMC BT 9 0 0 9 232.4217 225.8898 Tm /P <>BDC BT 8 0 0 8 338.514 745.9528 Tm EMC 9 0 0 9 394.0315 60.8898 Tm (737-8)Tj ( )Tj ET ET 7 0 0 7 37.6993 177.9528 Tm /P <>BDC /P <>BDC EMC 6 0 0 6 278.3662 701.9528 Tm ET ( )Tj EMC 6 0 0 6 301.1609 687.9528 Tm /P <>BDC ET 6 0 0 6 277.7064 715.9528 Tm /P <>BDC 13 0 0 13 411.0097 467.8898 Tm /P <>BDC ET EMC EMC ( )Tj ET -.01 Tc ET ET 7 0 0 7 116.3631 11.5132 Tm EMC ET BT BT 7 0 0 7 364.1531 166.9528 Tm /P <>BDC EMC /P <>BDC (passengers and the 737-900ER\(W\) 152)Tj 7 0 0 7 158.74 397.7654 Tm 0 Tc EMC BT -.02 Tc ( )Tj EMC However, it was also shown that the dual venting configuration of some ET 0 Tc BT EMC /P <>BDC BT ET /P <>BDC EMC 8 0 0 8 315.7776 591.9528 Tm EMC BT ( )Tj BT 9 0 0 9 411.0097 423.8898 Tm ET BT ( )Tj EMC (2,731)Tj EMC BT (0.0151)Tj ET BT BT 0 Tc 432 0 obj EMC ET EMC (0.0149)Tj BT 7 0 0 7 314.6398 496.7654 Tm 9 0 0 9 53.8578 412.8898 Tm /P <>BDC 0 Tc (34,650)Tj ET ( )Tj 9 0 0 9 207.8168 445.8898 Tm 13 0 0 13 118.3688 390.8898 Tm EMC 7 0 0 7 82.8504 133.9528 Tm /P <>BDC /P <>BDC ( )Tj BT ( )Tj (737-9)Tj EMC EMC BT S EMC 9 0 0 9 543.4875 456.8898 Tm BT ET /P <>BDC /P <>BDC W n ET BT BT ET panels. ET EMC 0 Tc BT EMC BT EMC /P <>BDC (weather, traffic and ATC constraints, all of)Tj ET /P <>BDC ( )Tj ET /P <>BDC EMC EMC 9 0 0 9 408.1889 467.8898 Tm - Non Perele - News Online, Hi, 0 Tc 7 0 0 7 473.4744 518.9528 Tm ( )Tj ET ET 6.5 0 0 6.5 54.877 715.9529 Tm /P <>BDC 6 0 0 6 519.1239 687.9528 Tm ET ET 9 0 0 9 267.0826 500.8898 Tm EMC /P <>BDC BT BT 6.5 0 0 6.5 297.8076 558.9529 Tm /P <>BDC ( )Tj BT 7 0 0 7 469.2222 11.5129 Tm 0 Tc Can you confirm if Im right or wrong? 7 0 0 7 343.2355 507.7654 Tm Everything you need to know about the Boeing 737 600/700/800/900 - NGs History & Development of . EMC 7 0 0 7 60.6117 441.7654 Tm /P <>BDC /P <>BDC ET EMC 9 0 0 9 548.5375 225.8898 Tm ET EMC 9 0 0 9 394.0157 126.8898 Tm 7 0 0 7 354.4763 705.7654 Tm /P <>BDC EMC /P <>BDC EMC EMC /P <>BDC q BT /GS2 gs ET EMC BT [(OM)8.1(M)-12.9(E)-24.9(R)7.1(C)8.1(E)]TJ /P <>BDC BT (150)Tj BT 9 0 0 9 373.2203 368.8898 Tm [(CFM L)17.1(E)-8.1(AP-1A26)]TJ (2,498)Tj BT EMC BT 9 0 0 9 182.8403 93.8898 Tm (A321ceo versus the 737-900ER\(W\), in the)Tj endobj ET -.02 Tc 6 0 0 6 381.7993 757.9528 Tm BT EMC BT 9 0 0 9 36.8583 346.8898 Tm 9 0 0 9 492.5143 500.8898 Tm ET 9 0 0 9 207.9609 511.8898 Tm EMC BT ET BT [(Aircr)10(aft type)]TJ ET - Non Perele - News Online, Council Post: Aviation Is The Driving Force Of Hydrogen | QNewsHub, When will the Boeing 737 MAX fly again? BT ( )Tj EMC 5.25 0 0 5.25 73.853 11.5132 Tm /P <>BDC BT 9 0 0 9 36.8583 423.8898 Tm EMC (0.0115)Tj 0 Tc BT 0 Tc -.005 Tc ET /P <>BDC /P <>BDC (5,000 aircraft delivered and making up)Tj BT (\(see table, this page\))Tj EMC 7 0 0 7 403.478 639.7654 Tm EMC /P <>BDC ET /P <>BDC ET /P <>BDC ET <> /P <>BDC BT /P <>BDC EMC 9 0 0 9 51.0236 335.8898 Tm 7 0 0 7 537.7804 419.9528 Tm EMC 7 0 0 7 344.1175 584.7654 Tm /P <>BDC EMC /P <>BDC 0 Tc 7 0 0 7 363.2711 441.9528 Tm BT BT 7 0 0 7 338.6433 67.7654 Tm 9 0 0 9 411.0181 456.8898 Tm 7 0 0 7 277.3936 573.9528 Tm BT /F4 1 Tf BT ET EMC EMC ET EMC BT (4,000)Tj ( )Tj /P <>BDC ET (170)Tj EMC ET ET -.02 Tc EMC ET ( )Tj 7 0 0 7 491.7142 595.7654 Tm EMC 9 0 0 9 572.0386 115.8898 Tm 9 0 0 9 215.4409 324.8898 Tm BT EMC BT BT /P <>BDC EMC ( )Tj There are many variants of the 737. (283)Tj BT -.02 Tc /Figure <>BDC EMC 7 0 0 7 316.0679 386.7654 Tm ET EMC ET /P <>BDC -.02 Tc ET /P <>BDC -.02 Tc ( )Tj ET EMC ET BT (0.0149)Tj allow for a measurement of fuel tank inerting and heating during the The NG series are prone to "Upper Wing Surface 0 Tc (compared to the A320ceo. (248,200)Tj 9 0 0 9 425.1967 775.8898 Tm EMC /P <>BDC /P <>BDC 544,000 lbs 246,754 Kg: Maximum Fuel Capacity: 48,445 US Gal. EMC (0.0134)Tj (have any payload limitations on the routes)Tj ( )Tj /P <>BDC 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 BT Greetings. ()Tj My simulation is focused on postcrash fires. EMC 0 J 0 j 15 w 10 M [] 0 d BT 6.5 0 0 6.5 54.877 637.9529 Tm ET [(E)-7.8(P)16.1(T)9(E)-13.9(MBE)-16.9(R)]TJ ( )Tj BT EMC .023 .567 .626 rg EMC /P <>BDC ET Your email address will not be published. 9 0 0 9 232.4408 797.8898 Tm BT EMC 0 Tc /P <>BDC ET ( )Tj ET BT EMC ET BT EMC BT ( )Tj ( )Tj EMC 1 i ET ET (5,243)Tj ( )Tj ( )Tj EMC ET 8 0 0 8 276.7109 633.9528 Tm EMC 7 0 0 7 77.36 11.5132 Tm ET EMC ET /P <>BDC ET ET BT ( )Tj 7 0 0 7 490.5101 518.9528 Tm ET ET /P <>BDC ET (737-9)Tj /P <>BDC EMC ET 3.0566 -3.9073 l /P <>BDC /P <>BDC /P <>BDC ET EMC BT 6 0 0 6 246.6462 743.9528 Tm 9 0 0 9 215.433 401.8898 Tm EMC ET EMC BT 7 0 0 7 99.5912 507.9528 Tm ET /P <>BDC 7 0 0 7 199.5784 397.7654 Tm /P <>BDC EMC BT (Using the evaluation payloads of 170)Tj 7 0 0 7 363.2711 386.9528 Tm ET BT ( )Tj BT 7 0 0 7 294.4014 540.7654 Tm /P <>BDC ET /P <>BDC ( )Tj All data presented is for entertainment purposes and should not be used operationally. EMC ( )Tj ET ET (160)Tj ET 10 0 0 10 47.8705 814.1973 Tm 8 0 0 8 314.3535 661.9528 Tm BT 0 Tc ET /P <>BDC 9 0 0 9 564.8379 269.8898 Tm ET /P <>BDC safer place! EMC ET /P <>BDC 9 0 0 9 202.0349 753.8898 Tm (The second comparison is payload)Tj 13 0 0 13 36.8504 71.8898 Tm 0 Tc ET /P <>BDC EMC BT EMC BT BT EMC 9 0 0 9 425.1913 93.8898 Tm ET 9 0 0 9 382.3068 489.8898 Tm ET (The first-class layout uses four-abreast)Tj ET /P <>BDC ( )Tj 0 Tc /P <>BDC ET ET ET /P <>BDC ET 6.5 0 0 6.5 296.3931 532.9529 Tm EMC BT 0 Tc EMC EMC (maximum passenger payload of 160. ET BT 9 0 0 9 181.0402 335.8898 Tm BT BT ET (30,000lbs to 33,000lbs, a fan diameter of)Tj The 800 variant is the stretched version of the 737-700. BT ET 7 0 0 7 279.1575 331.9528 Tm 0 Tc -.02 Tc (136)Tj /P <>BDC /P <>BDC BT (737-8)Tj -.02 Tc EMC (150)Tj BT BT /P <>BDC ET BT BT /P <>BDC /P <>BDC 6 0 0 6 561.1918 757.9528 Tm 9 0 0 9 394.0123 137.8898 Tm EMC /P <>BDC 9 0 0 9 371.6638 247.8898 Tm ET ( )Tj 7 0 0 7 380.2788 441.7654 Tm ET Although successful the A320 could not take on the Boeing 737s success. 6 0 0 6 451.7374 673.9528 Tm EMC (0.0111)Tj EMC ET EMC /P <>BDC /P <>BDC ET EMC BT BT 7 0 0 7 82.2047 672.9528 Tm /P <>BDC ET BT ET ET 15 w EMC -.02 Tc EMC ET ET )Tj ( )Tj BT EMC ( )Tj 7 0 0 7 204.0935 727.7654 Tm ET /P <>BDC ET /P <>BDC (operations, the block times would be)Tj /P <>BDC BT /P <>BDC EMC EMC EMC EMC EMC ET EMC 7 0 0 7 187.0858 298.9528 Tm 9 0 0 9 408.1968 236.8898 Tm BT ( )Tj (. 9 0 0 9 181.8233 49.8898 Tm ET 9 0 0 9 79.8339 522.8898 Tm /P <>BDC EMC ( )Tj (A321neo)Tj /P <>BDC EMC ( )Tj ET ( )Tj 7 0 0 7 537.267 133.7654 Tm ( )Tj ET BT ET EMC ET EMC BT ( )Tj EMC 9 0 0 9 215.4313 269.8898 Tm .014984 824.882 572.583 17.008 re EMC EMC ( )Tj /P <>BDC /P <>BDC ( )Tj /P <>BDC /P <>BDC ET EMC 680kg; All other series: 453kg, Main tanks to be full if centre contains over 453kg, If a fuel gauge is u/s the quantity ( )Tj /P <>BDC 7 0 0 7 316.0679 441.7654 Tm EMC EMC /P <>BDC EMC .0081 Tc ( )Tj ET EMC /P <>BDC ET -.02 Tc EMC ( )Tj ET ET -.02 Tc BT EMC ET -.02 Tc ( )Tj ET 0 Tc (Recent improvements in cabin design)Tj BT /P <>BDC -.02 Tc /P <>BDC BT fuel pumps were running in high ambient temperatures with empty or almost empty BT ET 9 0 0 9 186.5212 225.8898 Tm BT ET /P <>BDC ET /P <>BDC ET 7 0 0 7 297.632 496.9528 Tm ( )Tj 9 0 0 9 51.0236 71.8898 Tm BT 10 0 0 10 230.6475 794.2914 Tm -.02 Tc BT BT /P <>BDC 0 Tc (6,820)Tj ET ET -.02 Tc EMC EMC 7 0 0 7 230.7317 67.9528 Tm /P <>BDC 9 0 0 9 204.9907 467.8898 Tm ET BT 9 0 0 9 425.1913 291.8898 Tm /P <>BDC ( )Tj /P <>BDC BT EMC ET BT /P <>BDC BT EMC /P <>BDC BT ET 7 0 0 7 508.6712 133.7654 Tm EMC (aircraft types, all the flights were evaluated)Tj BT (20)Tj EMC ET -.02 Tc https://www.researchgate.net/publication/302903333_On_Boeing_737_-_300_Wing_Aerodynamics_Calculations_Based_on_VLM_Theory. BT EMC (35,112)Tj W n -.02 Tc 0 Tc EMC The A320ceos are)Tj /P <>BDC The weight configuration used)Tj EMC [(BOS-A)56.9(TL)]TJ EMC BT /P <>BDC 9 0 0 9 53.8582 621.8898 Tm BT ( )Tj ET ( )Tj BT BT ET 7 0 0 7 182.5706 573.9528 Tm 9 0 0 9 411.0097 104.8898 Tm BT Hi ET ( )Tj (2,748)Tj (10)Tj 5.25 0 0 5.25 64.5461 11.5129 Tm ( )Tj BT ET 9 0 0 9 195.3055 324.8898 Tm /P <>BDC BT ET ET /P <>BDC

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