737 800 fuel capacity pounds737 800 fuel capacity pounds

-.02 Tc 0 Tc 0 Tc 7 0 0 7 343.2355 694.7654 Tm ET EMC ( )Tj -.02 Tc /P <>BDC EMC /P <>BDC BT 9 0 0 9 36.8504 456.8898 Tm EMC 9 0 0 9 232.4217 104.8898 Tm EMC BT ( )Tj BT ET EMC ( )Tj 7 0 0 7 99.8582 232.7654 Tm EMC /P <>BDC 7 0 0 7 247.7395 496.7654 Tm (1,800 - )Tj (172,992)Tj 9 0 0 9 408.1854 423.8898 Tm BT ET -.02 Tc ET BT (/S)Tj ( )Tj /P <>BDC ET EMC ( )Tj ET 7 0 0 7 338.3085 298.9528 Tm EMC ET ( )Tj ( )Tj BT EMC 9 0 0 9 394.0157 390.8898 Tm (376)Tj -.02 Tc (1,272)Tj /P <>BDC /P <>BDC ET EMC ( )Tj /P <>BDC ET /P <>BDC /P <>BDC 7 0 0 7 536.3849 639.7654 Tm /P <>BDC The B737-800SF Cargo Conversion consists of the installation of a 86x137 cargo door on the left side of the fuselage, and modification of the main deck to a Class E cargo compartment. /P <>BDC 9 0 0 9 411.0097 148.8898 Tm ( )Tj EMC BT /F6 1 Tf ET EMC BT ET ( )Tj EMC 0 Tc ET 7 0 0 7 141.7322 78.9528 Tm /P <>BDC 26.0355 0 TD 9 0 0 9 348.3267 324.8898 Tm /P <>BDC (464,440)Tj /P <>BDC 7 0 0 7 299.0601 298.9528 Tm /P <>BDC /P <>BDC BT /P <>BDC EMC BT 7 0 0 7 444.737 276.7654 Tm 9 0 0 9 232.4217 247.8898 Tm ET 6 0 0 6 138.6506 757.9528 Tm 10 0 0 10 47.1144 814.1973 Tm /P <>BDC -.6563 -2.3409 l ET /P <>BDC EMC EMC BT 7 0 0 7 99.8582 89.7654 Tm 9 0 0 9 53.8582 753.8898 Tm It is produced in the Renton plant in Washington by Boeing Commercial Airplanes. /P <>BDC 9 0 0 9 543.0273 192.8898 Tm 7 0 0 7 279.1575 485.9528 Tm ET BT 8 0 0 8 275.7172 760.7654 Tm ET BT 9 0 0 9 386.3946 137.8898 Tm the most hazardous condition-an empty center wing tank-that GBI would remain /P <>BDC 6 0 0 6 527.699 701.9528 Tm EMC /P <>BDC 9 0 0 9 212.7029 390.8898 Tm (831)Tj BT (-54)Tj BT (151)Tj (0.0110)Tj 0 Tc EMC ET 9 0 0 9 541.3533 522.8898 Tm (297,312)Tj ET ( )Tj EMC 7 0 0 7 491.7142 628.7654 Tm ( )Tj [(CFM L)17.1(E)-8.1(AP-1B27)]TJ ( )Tj ET EMC BT 7 0 0 7 279.1575 89.9528 Tm /P <>BDC EMC BT 9 0 0 9 215.4409 93.8898 Tm aux tanks to push the aux fuel into the centre tank. 0 Tc ( )Tj EMC /P <>BDC 8 0 0 8 336.1225 771.7654 Tm 7 0 0 7 37.0536 606.9528 Tm EMC ET The Boeing 737 is designed to fill the smaller jet airliners space over a given range of seats. BT 0 Tc BT EMC 6.5 0 0 6.5 528.5291 663.9529 Tm 8 0 0 8 490.9813 771.9528 Tm 8 0 0 8 38.4438 703.9528 Tm (344-358)Tj /P <>BDC BT The westerly)Tj (1,938)Tj 9 0 0 9 186.9983 500.8898 Tm 6.5 0 0 6.5 191.942 532.9529 Tm ET ET EMC 7 0 0 7 474.3564 716.9528 Tm 7 0 0 7 294.4014 122.7654 Tm EMC -.02 Tc /P <>BDC BT ( )Tj ET /P <>BDC /P <>BDC BT /P <>BDC I am looking for the radius of the fuselage specifically the cargo door. 7 0 0 7 278.9827 430.9528 Tm ET (156)Tj ET 9 0 0 9 532.8774 346.8898 Tm 7 0 0 7 439.7405 529.9528 Tm BT /P <>BDC 6 0 0 6 295.8268 673.9528 Tm BT EMC BT /P <>BDC S (146,550)Tj 9 0 0 9 394.0123 258.8898 Tm BT ( )Tj /P <>BDC ( )Tj BT ( )Tj 0 Tc ( )Tj EMC BT BT 7 0 0 7 182.5706 375.9528 Tm BT /P <>BDC (216,240)Tj /P <>BDC BT ET EMC /P <>BDC (283)Tj 7 0 0 7 247.7395 199.7654 Tm BT 7 0 0 7 99.8582 78.7654 Tm .151 .147 .15 rg 7 0 0 7 366.0641 661.9528 Tm -.02 Tc ET /P <>BDC EMC -.005 Tc ET 7 0 0 7 404.3599 716.7654 Tm ET /P <>BDC 9 0 0 9 347.4891 203.8898 Tm /P <>BDC EMC EMC ET EMC ( )Tj EMC ET /P <>BDC 0 Tc 7 0 0 7 82.8504 78.9528 Tm ( )Tj ( )Tj EMC ET (216)Tj /P <>BDC ET 8 0 0 8 216.3261 771.9529 Tm /P <>BDC 9 0 0 9 215.433 401.8898 Tm (216,240)Tj BT EMC 7 0 0 7 141.7322 518.9528 Tm If you look at your favourite model of car, you would see that they have also evolved over time to be something unrecognisable from their ancestors. BT EMC ( )Tj ET 0 Tc EMC EMC BT /P <>BDC BT BT ET 7 0 0 7 158.74 430.7654 Tm -.02 Tc -.02 Tc BT 7 0 0 7 36.8504 155.9528 Tm Therefore,)Tj Pingback:Council Post: Aviation Is The Driving Force Of Hydrogen | QNewsHub, Pingback:When will the Boeing 737 MAX fly again? BT EMC ET -.02 Tc (31,416)Tj (longer routes. 9 0 0 9 186.0353 291.8898 Tm ET BT ( )Tj 0 Tc /P <>BDC BT /P <>BDC 6.5 0 0 6.5 227.9655 624.9529 Tm q 1 0 0 1 36.85 469.878 cm 0 0 m /GS1 gs ET 6 0 0 6 496.2034 757.9528 Tm -.02 Tc The New Midsized Airplane. BT 0 Tc 36.85 824.882 572.599 17.008 re /P <>BDC ET 0 Tc EMC ( )Tj EMC EMC 9 0 0 9 555.2855 478.8898 Tm 7 0 0 7 491.7142 133.7654 Tm /P <>BDC /P <>BDC (573)Tj EMC -.02 Tc BT ( )Tj EMC /P <>BDC 7 0 0 7 355.3163 210.7654 Tm 7 0 0 7 199.5784 298.7654 Tm BT EMC /P <>BDC ET EMC /P <>BDC 8 0 0 8 225.1837 591.9528 Tm ET ET /P <>BDC ET -.01 Tc EMC /P <>BDC /P <>BDC ET 7 0 0 7 439.8175 727.9528 Tm 7 0 0 7 427.7291 331.9528 Tm /P <>BDC BT ET ( )Tj EMC ET /P <>BDC BT ET (2,517)Tj 6.5 0 0 6.5 171.7493 689.9529 Tm (374-388)Tj 6 0 0 6 561.1317 771.9528 Tm /P <>BDC ET EMC /P <>BDC BT 0 Tc 9 0 0 9 36.8504 49.8898 Tm ET There was no additional)Tj 7 0 0 7 131.6494 309.7654 Tm The CFM56-5B4/P is rated)Tj 9 0 0 9 394.0315 698.8898 Tm ( )Tj BT BT ET EMC BT (831)Tj BT Cheers Peter. ( )Tj (170)Tj (airport charges, while the time-dependent)Tj /P <>BDC 7 0 0 7 141.7322 661.9528 Tm The airliner was attempting to land at Amsterdams Schiphol Airport. /P <>BDC /P <>BDC EMC EMC /P <>BDC BT ET ET -.02 Tc /P <>BDC /P <>BDC /P <>BDC ET BT EMC ( )Tj 9 0 0 9 411.0181 467.8898 Tm 7 0 0 7 53.8582 11.5132 Tm EMC 8 0 0 8 435.4879 760.7654 Tm ET /P <>BDC BT 17 0 0 17 36.8606 758.6944 Tm ET (5,338)Tj ET 7 0 0 7 355.3163 67.7654 Tm BT ( )Tj 7 0 0 7 490.8321 100.7654 Tm BT [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ EMC 0 Tc -.02 Tc 201.803 814.197 m /P <>BDC /P <>BDC 7 0 0 7 158.74 716.7654 Tm /P <>BDC (. 8 0 0 8 124.845 675.9528 Tm W n /P <>BDC (CFM56-7B26)Tj (98,500)Tj 9 0 0 9 215.433 247.8898 Tm /P <>BDC EMC -.02 Tc 7 0 0 7 82.8504 309.9528 Tm EMC EMC ( )Tj ET BT .151 .147 .15 rg BT ET ET EMC BT 505.331 89.873 m (146,550)Tj ET (170)Tj ET /P <>BDC EMC 6.5 0 0 6.5 324.4345 663.9529 Tm (flight and block time, wind components,)Tj ET ( )Tj (\(see table, this page\))Tj (In this comparison, the A321neo)Tj ( )Tj BT 6 0 0 6 195.3167 715.9528 Tm BT ET 6.5 0 0 6.5 64.6596 624.9529 Tm ET ET /P <>BDC ET ET 7 0 0 7 99.8582 309.7654 Tm ET 0 Tc 0 Tc ( )Tj /P <>BDC (weights used are an MTOW of)Tj 6.5 0 0 6.5 375.6529 676.9529 Tm ET ( )Tj ET EMC ET (I)Tj 261 0 obj ET 9 0 0 9 394.0315 126.8898 Tm ET 6 0 0 6 154.1438 757.9528 Tm EMC ET BT ( )Tj BT /F4 1 Tf 7 0 0 7 474.3564 606.9528 Tm /P <>BDC /P <>BDC BT EMC ( )Tj 9 0 0 9 523.7694 214.8898 Tm ( )Tj EMC ET (have taken advantage of lighter composite)Tj ( )Tj ET BT ( )Tj ET ( )Tj EMC BT (/S)Tj ET 9 0 0 9 367.2442 379.8898 Tm ( )Tj 9 0 0 9 369.2608 38.8898 Tm /P <>BDC ET EMC EMC ET 7 0 0 7 363.2711 210.9528 Tm Boeing supplied 10,574 since initial development as of 2020. 9 0 0 9 212.5107 313.8898 Tm 7 0 0 7 247.7395 573.7654 Tm BT ( )Tj BT /P <>BDC (405)Tj BT /P <>BDC BT 8 0 0 8 74.9636 591.9528 Tm (The fuel burn difference is greater on)Tj EMC /P <>BDC BT 9 0 0 9 411.0181 489.8898 Tm EMC 0 Tc EMC 7 0 0 7 88.196 11.5129 Tm ET ET EMC /P <>BDC ET ET 304.725 420.96 m 9 0 0 9 516.3894 247.8898 Tm 0 Tc BT ET (the equivalent aircraft types, the lowest fuel)Tj ( )Tj /P <>BDC BT ET (passenger payload. 9 0 0 9 546.9046 423.8898 Tm 7 0 0 7 187.0858 694.9528 Tm 0 Tc BT /P <>BDC ET EMC EMC Main tanks > 50%, -1 to 5 deg pitch, +/- 1 deg roll: +/- 1.5% 0 Tc /P <>BDC 7 0 0 7 354.6933 507.7654 Tm /P <>BDC thanks for stopping by. ( )Tj Maybe there is someone out there who can give you a better answer. (192 seats versus 179 on the 737-9. 6 0 0 6 195.6824 659.9528 Tm 7 0 0 7 354.6933 639.7654 Tm ( )Tj (20)Tj EMC EMC /P <>BDC ( )Tj EMC /P <>BDC ( )Tj ( )Tj 7 0 0 7 338.6433 386.7654 Tm ET EMC ET EMC ( )Tj ET Refuelling of the aux tanks is done by moving the guarded switch in the 7 0 0 7 37.6993 386.9528 Tm 9 0 0 9 215.4409 335.8898 Tm EMC /P <>BDC /P <>BDC /F6 1 Tf /P <>BDC 6 0 0 6 184.0127 771.9528 Tm ET ET 9 0 0 9 394.0315 720.8898 Tm 7 0 0 7 141.7322 89.9528 Tm BT BT .023 .567 .626 RG EMC ( )Tj EMC ET (382,280)Tj EMC 7 0 0 7 326.2278 694.9528 Tm BT 6 0 0 6 184.072 659.9528 Tm (1A26)Tj BT ET /P <>BDC EMC ET EMC BT /P <>BDC q ET BT EMC EMC /P <>BDC I already checked in the AMM, SRM. EMC /P <>BDC 7 0 0 7 474.7064 408.9528 Tm /P <>BDC ET -.02 Tc ( )Tj BT (0.0113)Tj ET ET EMC Airbus A320 History a new player in the short-haul market. /P <>BDC BT 9 0 0 9 192.0203 313.8898 Tm EMC ( )Tj ET /P <>BDC /P <>BDC /P <>BDC ( )Tj EMC ET ET EMC (have been optimised by the PPS flight)Tj ET ( )Tj ET BT ET EMC .41 .161 .508 RG (because the 737-900 is limited to the same)Tj ET ET ET /P <>BDC BT 9 0 0 9 53.8578 236.8898 Tm BT BT BT 6.5 0 0 6.5 244.2585 598.9529 Tm 7 0 0 7 338.3085 188.9528 Tm /P <>BDC ( )Tj BT ET (I)Tj ET BT BT EMC ( )Tj ET EMC ET 7 0 0 7 230.7317 441.9528 Tm /P <>BDC BT EMC BT ( )Tj ( )Tj -.02 Tc BT EMC EMC /P <>BDC /P <>BDC Because of 7 0 0 7 508.4124 298.7654 Tm 7 0 0 7 294.4014 507.7654 Tm ET ( )Tj 0 Tc EMC BT BT ET 9 0 0 9 215.433 71.8898 Tm [(BL)32(OCK F)8.1(UEL)31( PERF)8.1(ORMANCE OF A3)24.9(20CEO, A3)24.9(20NEO, A3)24.9(21CEO, A3)24.9(21NEO, 7)-33(3)8.1(7-800, 7)-33(3)8(7-900ER, 7)-33(3)8(7-8 & 7)-33(3)8.1(7-9 - P)30(A)52(YL)32(O)6.1(AD SCENARIO 2 )]TJ BT EMC BT EMC ( )Tj ET ET 28.5749 0 TD 7 0 0 7 107.1165 474.9528 Tm BT 7 0 0 7 124.1242 199.7654 Tm ET ( )Tj 7 0 0 7 277.3936 265.9528 Tm /P <>BDC EMC ET ( )Tj 0 Tc 7 0 0 7 403.478 408.7654 Tm EMC ET 9 0 0 9 522.7491 280.8898 Tm ( )Tj EMC 7 0 0 7 114.6416 397.9528 Tm EMC /P <>BDC 9 0 0 9 372.8879 412.8898 Tm BT /P <>BDC /P <>BDC 9 0 0 9 425.183 159.8898 Tm (equivalent engine thrust ratings for the neo)Tj They are quite easy to find. 0 Tc .014984 824.882 572.583 17.008 re /P <>BDC /P <>BDC EMC /P <>BDC 7 0 0 7 241.5317 243.9528 Tm /P <>BDC ET BT /P <>BDC EMC ( )Tj 6 0 0 6 144.9509 687.9528 Tm -.02 Tc EMC (CFM56-)Tj 7 0 0 7 457.0984 628.7654 Tm ET BT 7 0 0 7 539.9176 11.5129 Tm EMC BT BT /P <>BDC 7 0 0 7 490.5101 617.9528 Tm 7 0 0 7 491.4046 287.9528 Tm EMC ( )Tj (/S)Tj BT 28.5749 0 TD BT Aircraft must carry enough fuel to taxi, climb, cruise, descent, and mutliple reserves. [(v)21(ariant)]TJ EMC )Tj ( )Tj ( )Tj ( )Tj ET BT BT (different available options, and gives the)Tj BT EMC 786 0 obj BT BT EMC ( )Tj ET (1,272)Tj 9 0 0 9 208.0289 632.8898 Tm EMC 7 0 0 7 440.6226 639.9528 Tm 0 Tc /P <>BDC 7 0 0 7 379.3969 144.7654 Tm 9 0 0 9 169.0521 368.8898 Tm 0 Tc ( )Tj 7 0 0 7 210.1137 463.7654 Tm EMC BT ( )Tj (all eight aircraft types. 7 0 0 7 403.478 617.7654 Tm BT (10)Tj ( )Tj 7 0 0 7 258.2805 331.7654 Tm 7 0 0 7 430.039 639.9528 Tm BT /P <>BDC (20)Tj /P <>BDC EMC /P <>BDC 7 0 0 7 118.104 507.7654 Tm 7 0 0 7 457.0984 672.7654 Tm BT 6.5 0 0 6.5 381.6589 558.9529 Tm EMC EMC -.01 Tc BT /P <>BDC 9 0 0 9 394.0157 280.8898 Tm /P <>BDC BT 19.843 0 l /P <>BDC /P <>BDC ET /P <>BDC EMC EMC /P <>BDC 9 0 0 9 362.0968 324.8898 Tm 9 0 0 9 215.4313 203.8898 Tm ( )Tj EMC /P <>BDC 7 0 0 7 459.6601 11.5129 Tm 6.5 0 0 6.5 500.4941 565.9529 Tm ET (on these flights. ET ET 7 0 0 7 297.632 463.9528 Tm BT BT There seem to be a lot of answers that come up, some of which might be what youre looking for. 7 0 0 7 427.7291 177.9528 Tm /P <>BDC ET ET 6 0 0 6 465.8383 673.9528 Tm 7 0 0 7 326.2278 705.9528 Tm ET EMC /P <>BDC ET ET /P <>BDC -.02 Tc 7 0 0 7 141.7322 177.9528 Tm (410)Tj 7 0 0 7 327.1097 617.9528 Tm /P <>BDC (the aircraft operator, but in this evaluation)Tj auxiliary tank at the forward end of the aft hold; these were available in ET ET ( )Tj ET ET EMC /P <>BDC /P <>BDC ET 7 0 0 7 456.2165 265.7654 Tm 7 0 0 7 386.3929 683.9528 Tm /P <>BDC EMC EMC 0 Tc 9 0 0 9 361.7 456.8898 Tm 9 0 0 9 394.0157 456.8898 Tm /Figure <>BDC 9 0 0 9 525.9757 60.8898 Tm (have payload restrictions on the evaluation)Tj /P <>BDC EMC ET (1,144)Tj EMC BT EMC /P <>BDC ET -.02 Tc /P <>BDC EMC EMC BT /P <>BDC ( )Tj 9 0 0 9 374.2211 379.8898 Tm BT ET 6 0 0 6 55.0668 701.9528 Tm 6 0 0 6 195.3167 757.9528 Tm (the aircraft types. /P <>BDC ( )Tj 9 0 0 9 246.6113 247.8898 Tm -.02 Tc 7 0 0 7 141.7322 474.9528 Tm 7 0 0 7 539.8962 683.9528 Tm ET ( )Tj EMC 7 0 0 7 490.8321 166.7654 Tm ( )Tj -.02 Tc BT 0 Tc ( )Tj BT EMC ET BT EMC EMC /P <>BDC ET ( )Tj BT 9 0 0 9 181.0402 335.8898 Tm EMC 0 Tc ET ( )Tj ET ET EMC BT ET ET ( )Tj BT BT /F1 1 Tf BT ET EMC (series of aircraft benefits from increased)Tj /P <>BDC (37,416)Tj /P <>BDC 0 841.89 609.449 -841.89 re ( )Tj EMC 0 Tc 7 0 0 7 521.4089 11.5132 Tm ET (160)Tj ( )Tj ( )Tj /P <>BDC ET /P <>BDC ET ET ET ET EMC /Artifact <>BDC EMC ET EMC 9 0 0 9 190.3643 368.8898 Tm -.02 Tc EMC ET 6.5 0 0 6.5 477.8064 702.9529 Tm EMC (39,270)Tj EMC 0 Tc /P <>BDC -.02 Tc EMC ( )Tj BT /P <>BDC BT 7 0 0 7 537.267 133.7654 Tm /P <>BDC ( )Tj EMC 7 0 0 7 258.2805 364.7654 Tm 9 0 0 9 547.3802 566.8898 Tm endstream BT (4,158)Tj EMC ET EMC EMC ET EMC EMC ( )Tj EMC ET EMC ET EMC 6.5 0 0 6.5 398.2453 742.9529 Tm BT EMC ET 7 0 0 7 363.2711 441.9528 Tm BT /P <>BDC 7 0 0 7 77.36 11.5132 Tm EMC 9 0 0 9 53.8582 214.8898 Tm The aircraft look like standard -800s, so why the difference? ( )Tj /GS1 gs -.02 Tc /GS2 gs BT BT ( )Tj ( )Tj /P <>BDC 8 0 0 8 314.3535 633.9528 Tm 6.5 0 0 6.5 528.5291 676.9529 Tm EMC ( )Tj 7 0 0 7 258.2805 188.7654 Tm ( )Tj /OC /MC835 BDC ET /P <>BDC EMC ET 7 0 0 7 70.8101 243.9528 Tm ET 6.5 0 0 6.5 192.5726 722.9529 Tm ET 0 Tc BT /P <>BDC [(superior oper)10(ating performance. BT EMC EMC EMC 7 0 0 7 241.5317 595.9528 Tm (sectors where a 170-passenger payload is)Tj -.02 Tc BT /P <>BDC -.02 Tc EMC 394.516 71.673 160.63 -39.992 re BT /P <>BDC ET /F6 1 Tf BT EMC BT ( )Tj EMC ET ET 7 0 0 7 508.4124 375.7654 Tm (19)Tj ( )Tj (356-369)Tj -.02 Tc ET (2,388)Tj ET 9 0 0 9 53.8582 478.8898 Tm 7 0 0 7 294.4014 628.7654 Tm [(CFM L)17.1(E)-8.1(AP-1A32)]TJ ET BT 9 0 0 9 53.8338 82.8898 Tm (31,416)Tj EMC BT ET ( )Tj (A320neo)Tj ET ( )Tj ET 7 0 0 7 54.7071 287.7654 Tm -.02 Tc The trigger for the scavenge pump is different for the series as follows: NB On the classics, when departing with less than 1,000kg of fuel in the centre tank, an imbalance may occur during 0 Tc EMC ET EMC EMC ( )Tj BT ET 10 0 0 10 420.16 814.1973 Tm EMC endobj ( )Tj ( )Tj EMC (282-294)Tj BT EMC EMC 0 Tw BT ET 0 Tc ET EMC 9 0 0 9 512.8093 434.8898 Tm 9 0 0 9 385.653 71.8898 Tm 9 0 0 9 565.1979 478.8898 Tm 7 0 0 7 298.514 628.9528 Tm BT 7 0 0 7 118.104 210.7654 Tm ( )Tj ET ( )Tj ET BT 6 0 0 6 214.8509 687.9528 Tm 9 0 0 9 53.8582 379.8898 Tm BT 9 0 0 9 68.0071 566.8898 Tm 9 0 0 9 206.6251 236.8898 Tm ET BT EMC ( )Tj &6E'dtU7()euFVfvGWgw8HXhx9IYiy*:JZjz ? EMC ET BT ET 6.5 0 0 6.5 430.0114 565.9529 Tm ET BT /F4 1 Tf BT ET ( )Tj EMC /P <>BDC ET EMC ET 8 0 0 8 276.7109 633.9528 Tm BT ET EMC 7 0 0 7 72.3151 342.9528 Tm levels in the center fuel tanks. BT 7 0 0 7 88.196 11.5129 Tm ET 5 0 0 5 484.5872 11.5129 Tm BT 7 0 0 7 187.0858 199.9528 Tm BT 0 Tc ET BT EMC ET /P <>BDC 8 0 0 8 539.8061 771.9528 Tm BT ( )Tj ( )Tj 7 0 0 7 116.3631 11.5132 Tm 9 0 0 9 417.7488 511.8898 Tm Max T/O Weight: 174200 Lb Max Landing Weight: 146300 Lb Operating Weight: 102100 Lb Fuel Capacity: 69982 lbs Lb Payload W/Full Fuel: 2618 Lb Max Payload: 36200 Lb Range Normal Range: 5644 nm Max Range: 5673 nm Service Ceiling: 41000 ft Distances Balanced Field Length: 7210 ft Landing Distance: 4117 ft Performance Rate of Climb: 3100 fpm 0 Tc ( )Tj 7 0 0 7 536.3849 408.7654 Tm BT (alternates used and their distance from the)Tj EMC BT ET ( )Tj /P <>BDC ET /P <>BDC BT 9 0 0 9 36.8504 247.8898 Tm EMC BT /P <>BDC BT EMC 6 0 0 6 55.0668 659.9528 Tm 9 0 0 9 553.6047 423.8898 Tm (10)Tj BT (0.0135)Tj BT (passengers and 163 passengers on the)Tj EMC /P <>BDC /P <>BDC Digital Sunburst Fuel Gauges - Simmonds 4 Tank. EMC ET Boeing Information on Coronavirus (COVID-19) The safety of Boeing employees, their dependents and visitors to our sites is a top priority. ET EMC ET /P <>BDC EMC ET /P <>BDC ET /P <>BDC ET /P <>BDC ET ET q BT /P <>BDC 0 Tc ( )Tj ET ET ( )Tj ( )Tj 7 0 0 7 241.5317 705.9528 Tm /P <>BDC 9 0 0 9 544.5056 302.8898 Tm /P <>BDC 7 0 0 7 241.5317 122.9528 Tm BT ET 0 Tc /OC /MC2279 BDC 7 0 0 7 444.737 133.7654 Tm EMC 7 0 0 7 82.8504 100.9528 Tm ET ET EMC 9 0 0 9 562.2737 379.8898 Tm EMC BT (34,650lbs)Tj movement as fuel is loaded and used. BT (City-pair)Tj BT /P <>BDC BT EMC ET 7 0 0 7 403.478 221.7654 Tm ET EMC BT EMC /P <>BDC 0 Tc (251-267)Tj /P <>BDC /P <>BDC EMC ET 7 0 0 7 337.7614 144.7654 Tm BT -.02 Tc /P <>BDC The Boeing 737-800 to date has around 5000 units produced and 2019 saw 138 of the 800 roll of the production line. 0 Tc EMC 9 0 0 9 394.0315 60.8898 Tm /P <>BDC (average 3.6% less fuel over the 14 sectors)Tj EMC /Artifact <>BDC 0 Tc ( )Tj ET BT /P <>BDC BT Q 0 Tc 7 0 0 7 99.8582 276.7654 Tm BT EMC (. BT 6.5 0 0 6.5 335.5237 532.9529 Tm /P <>BDC ET EMC /P <>BDC 9 0 0 9 541.1665 599.8898 Tm BT ( )Tj (128-137)Tj 7 0 0 7 387.0159 485.9528 Tm ET /P <>BDC 9 0 0 9 163.2471 269.8898 Tm BT 2002-19-52 which requires the crew to maintain certain minimum fuel 6.5 0 0 6.5 116.0238 624.9529 Tm 6 0 0 6 174.3402 701.9528 Tm (CFM56-)Tj 6 0 0 6 403.4411 757.9528 Tm ET BT /GS1 gs .41 .161 .508 RG BT ( )Tj -.02 Tc BT 0 Tc 7 0 0 7 247.7395 705.7654 Tm /P <>BDC 9 0 0 9 411.0097 412.8898 Tm /P <>BDC /P <>BDC BT ET ET Thanks for stopping by. BT ( )Tj especially during start. /P <>BDC /P <>BDC thank you for stopping by. ET EMC ET 0 Tc BT (34,650)Tj BT BT EMC (737-8)Tj EMC BT /P <>BDC /P <>BDC EMC ET /P <>BDC 9 0 0 9 394.0157 258.8898 Tm ( )Tj 7 0 0 7 299.0601 232.9528 Tm ( )Tj ( )Tj BT BT S -.01 Tc ET 9 0 0 9 368.9649 423.8898 Tm BT q 1 0 0 1 394.012 84.878 cm 0 0 m BT -.02 Tc EMC -.02 Tc (In this comparison the passenger seat)Tj 7 0 0 7 37.6993 111.9528 Tm (136)Tj EMC 9 0 0 9 373.2203 368.8898 Tm 9 0 0 9 36.8504 423.8898 Tm EMC 7 0 0 7 321.6356 320.9528 Tm ( )Tj (0.0134)Tj BT 9 0 0 9 112.3045 346.8898 Tm 9 0 0 9 391.278 313.8898 Tm EMC ( )Tj /P <>BDC EMC We dont actually have access to a table of these variants and their features. /P <>BDC ( )Tj 7 0 0 7 247.7395 133.7654 Tm 7 0 0 7 82.8504 166.9528 Tm ( )Tj 9 0 0 9 36.8504 478.8898 Tm ET /P <>BDC ET -.02 Tc 9 0 0 9 466.0881 203.8898 Tm /P <>BDC EMC ET ET BT ET EMC EMC EMC 7 0 0 7 363.2711 507.9528 Tm EMC 7 0 0 7 354.6933 430.7654 Tm -.02 Tc 9 0 0 9 394.0315 236.8898 Tm /P <>BDC /P <>BDC /P <>BDC BT EMC 7 0 0 7 199.5784 595.7654 Tm EMC ET /P <>BDC 9 0 0 9 531.902 467.8898 Tm EMC ET /P <>BDC ET ET /P <>BDC 9 0 0 9 215.433 214.8898 Tm 7 0 0 7 299.0601 199.9528 Tm ( )Tj 0 Tc 9 0 0 9 552.5493 357.8898 Tm ET ( )Tj /P <>BDC 9 0 0 9 408.2047 423.8898 Tm 0 Tc ET ( )Tj EMC ( )Tj /P <>BDC 0 Tc The BBJ can have up to 9 aux fuel tanks giving it a maximum fuel quantity of 37,712kgs (83,000lbs) although in practice this would EMC 7 0 0 7 507.7893 529.7654 Tm EMC 9 0 0 9 53.8582 269.8898 Tm ET ( )Tj -.02 Tc ( )Tj EMC EMC (152)Tj thanks for stopping by. EMC /P <>BDC Slats, flaps and Fuselage skin areas primarily loaded in tension Aluminium alloy 2024 (Aluminium and copper), Wing lower skin Aluminium alloy 7055 (Aluminium, zinc, magnesium and copper), Wing ribs, Frames, stringers, keel and floor beams Aluminium alloy 7075 (Aluminium and zinc), Spars, beams and Wing upper skin Aluminium alloy 7178 (Aluminium, zinc, magnesium and copper), Landing gear beam Aluminium alloy 7175 (Aluminium, zinc, magnesium and copper), Hi. 7 0 0 7 241.5317 386.9528 Tm BT ( )Tj ET EMC (289)Tj /P <>BDC 0 Tc EMC BT 0 Tc 9 0 0 9 571.0211 258.8898 Tm (CFM56-5B4/P)Tj /TT2 1 Tf (1,824)Tj EMC ET 7 0 0 7 54.7071 529.7654 Tm 9 0 0 9 200.7278 170.8898 Tm ET (Although it is most fuel-efficient to)Tj (full passenger payload. ET (172,842)Tj 9 0 0 9 215.4409 225.8898 Tm 6 0 0 6 433.8509 687.9528 Tm -.02 Tc -.02 Tc ET /P <>BDC 7 0 0 7 473.8245 287.9528 Tm /P <>BDC EMC BT ET In one insistence a 737-800 on a route from Istanbul crashing in a field near the Polderbaan. ET /P <>BDC 9 0 0 9 53.8578 269.8898 Tm BT 7 0 0 7 258.2805 496.7654 Tm (31,416lbs)Tj ET BT 7 0 0 7 99.8582 617.7654 Tm ( )Tj (737-9 compared to the 737-900ER\(W\) is)Tj /P <>BDC (150)Tj /P <>BDC 0 Tw ET ET ET ET BT /P <>BDC EMC ET BT -.01 Tc BT (CFM56-7B27B3)Tj EMC -.02 Tc ET 9 0 0 9 394.0237 412.8898 Tm ET BT /GS1 gs ET /P <>BDC ( )Tj 7 0 0 7 354.6933 518.7654 Tm BT BT 7 0 0 7 204.0935 628.7654 Tm BT /P <>BDC /P <>BDC ET ET Thanks. ET /P <>BDC EMC BT -.02 Tc BT 7 0 0 7 43.6039 639.9528 Tm /P <>BDC 7 0 0 7 508.4124 606.7654 Tm BT BT 0 Tc ET 9 0 0 9 501.24 731.8898 Tm EMC ET EMC /TT2 1 Tf /P <>BDC ( )Tj (A320ceo a range of 2,800-2,900nm with)Tj /P <>BDC 7 0 0 7 487.0872 11.5129 Tm EMC /P <>BDC ( )Tj 9 0 0 9 192.6957 346.8898 Tm /P <>BDC EMC 6.5 0 0 6.5 112.0328 637.9529 Tm 0 Tc ET fuel and de-ice the fuel filter. 7 0 0 7 440.0906 166.9528 Tm ET /P <>BDC 0 Tc ET [(737-900E)-33(R)]TJ 6.5 0 0 6.5 192.4489 545.9529 Tm ET /F4 1 Tf 0 Tc [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ BT BT ET EMC ( )Tj ET 9 0 0 9 394.0123 225.8898 Tm /P <>BDC ET BT [(b)6.1(ypass r)10(atio engines pr)10(o)16.1(vide it with the most)]TJ /P <>BDC /P <>BDC 7 0 0 7 230.7317 562.9528 Tm BT /P <>BDC /P <>BDC EMC EMC (5.5:1. EMC BT 7 0 0 7 99.8582 364.7654 Tm 0 Tc EMC 6 0 0 6 372.295 673.9528 Tm ET (213)Tj EMC BT 7 0 0 7 279.1575 199.9528 Tm BT 7 0 0 7 241.5317 694.9528 Tm ( )Tj Any)Tj EMC 0 Tc /P <>BDC BT BT ET (374)Tj 9 0 0 9 68.031 170.8898 Tm The cruise speed to the alternate was)Tj ET /P <>BDC /P <>BDC BT /P <>BDC EMC 1.0437 2.7347 l BT BT 7 0 0 7 474.7064 441.9528 Tm 7 0 0 7 474.7064 166.9528 Tm EMC 7 0 0 7 338.6433 375.7654 Tm 7 0 0 7 141.7322 386.9528 Tm 5.25 0 0 5.25 123.5367 11.5132 Tm /Artifact <>BDC ET BT BT /P <>BDC ( )Tj 7 0 0 7 518.4953 287.9528 Tm ( )Tj ET BT ET BT /P <>BDC EMC ET BT EMC EMC ET 7 0 0 7 82.8504 320.9528 Tm EMC /P <>BDC /P <>BDC -.02 Tc BT ET /P <>BDC 7 0 0 7 508.4124 144.7654 Tm ( )Tj EMC q EMC /P <>BDC ET 7 0 0 7 158.74 375.7654 Tm EMC ( )Tj /P <>BDC 9 0 0 9 202.845 357.8898 Tm BT EMC (31,416)Tj ET (737-8)Tj /P <>BDC ( )Tj EMC ET ET ET ET /P <>BDC /P <>BDC BT /P <>BDC ET ET -.01 Tc ( )Tj -.02 Tc BT ( )Tj EMC BT ET /P <>BDC S /P <>BDC BT ET )Tj EMC EMC EMC ET /P <>BDC ET /P <>BDC [(Aircr)10(aft type)]TJ ( )Tj /P <>BDC EMC 7 0 0 7 539.8962 727.9528 Tm /P <>BDC BT /P <>BDC EMC EMC BT BT 7 0 0 7 508.4124 540.7654 Tm EMC 7 0 0 7 518.4953 122.9528 Tm ( )Tj EMC 7 0 0 7 445.619 529.7654 Tm EMC EMC ( )Tj -.02 Tc 9 0 0 9 541.6875 489.8898 Tm (. EMC ET 7 0 0 7 439.2087 78.9528 Tm [(CFM L)17.1(E)-8.1(AP-1A32)]TJ EMC /P <>BDC BT EMC /P <>BDC -.01 Tc ( )Tj Irkut MC-21, Russias homegrown modern airliner. ( )Tj ET 7 0 0 7 429.157 584.9528 Tm 9 0 0 9 232.438 236.8898 Tm /GS2 gs ET ET /P <>BDC 9 0 0 9 177.7731 181.8898 Tm EMC ET EMC BT /P <>BDC ET BT 7 0 0 7 474.7064 133.9528 Tm /P <>BDC BT 10 0 0 10 47.8705 814.1973 Tm ( )Tj EMC ET ET (The fuel cost per ASM difference)Tj 7 0 0 7 297.632 496.9528 Tm 9 0 0 9 53.8578 258.8898 Tm 0 Tc BT EMC ET /P <>BDC ET EMC ET BT 6.5 0 0 6.5 296.4841 663.9529 Tm [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ ET BT /P <>BDC BT 9 0 0 9 549.8405 632.8898 Tm /P <>BDC 7 0 0 7 230.7317 529.9528 Tm (172,992)Tj /P <>BDC ( )Tj EMC EMC /P <>BDC /GS1 gs (category. BT ( )Tj ET 9 0 0 9 73.1083 522.8898 Tm BT BT ET BT EMC BT /P <>BDC (off weight \(MTOW\) of 171,961lbs, a)Tj BT -.02 Tc BT ET 9 0 0 9 411.0234 742.8898 Tm EMC /P <>BDC 9 0 0 9 215.4313 214.8898 Tm ET ( )Tj /P <>BDC /P <>BDC EMC EMC ET (The A321ceo has a maximum fuel)Tj ( )Tj /P <>BDC ( )Tj EMC EMC BT /P <>BDC ( )Tj BT )Tj ( )Tj EMC ET ET /P <>BDC -.01 Tc /P <>BDC (35,112)Tj BT 6 0 0 6 222.2255 771.9528 Tm ( )Tj ET /P <>BDC 9 0 0 9 215.4409 500.8898 Tm /P <>BDC ET 7 0 0 7 491.4046 199.9528 Tm ET EMC 304.725 420.96 m /P <>BDC /P <>BDC ET

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