737 800 fuel capacity pounds
737 800 fuel capacity pounds
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BT 0 Tc -.02 Tc EMC 9 0 0 9 524.2249 478.8898 Tm (20)Tj )Tj BT /P <>BDC /P <>BDC ET -3.0537 -3.7076 -2.9805 -4.2115 -2.7872 -4.5727 c 9 0 0 9 372.2467 170.8898 Tm 137 )Tj BT -.02 Tc EMC /P <>BDC BT /P <>BDC ET ET /P <>BDC ( )Tj BT /P <>BDC 7 0 0 7 474.3564 485.9528 Tm EMC ET ET BT EMC ET BT EMC 36.85 824.882 572.599 17.008 re ET 9 0 0 9 232.438 192.8898 Tm 28.5749 0 TD ET 9 0 0 9 215.4313 214.8898 Tm ( )Tj /P <>BDC EMC BT /P <>BDC ET /P <>BDC EMC (some minor aerodynamic improvements)Tj (10)Tj the 737 but will require up to six on the 747. BT EMC /P <>BDC BT EMC 9 0 0 9 536.1277 247.8898 Tm ET BT 9 0 0 9 53.8578 456.8898 Tm EMC ET ET 9 0 0 9 545.0095 357.8898 Tm 8 0 0 8 85.4842 745.9528 Tm 9 0 0 9 229.6141 335.8898 Tm 9 0 0 9 186.5751 423.8898 Tm BT [(CFM L)17.1(E)-8.1(AP-1A32)]TJ BT BT /P <>BDC ET BT 9 0 0 9 53.8582 456.8898 Tm 0 Tc ET [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ 0 Tc BT 9 0 0 9 566.3417 423.8898 Tm BT 0 Tc 6.5 0 0 6.5 273.8079 702.9529 Tm 7 0 0 7 247.7395 441.7654 Tm -.02 Tc 0 Tc BT EMC EMC EMC ET ET (18)Tj ET ET ET ET ET ET BT -.02 Tc /P <>BDC EMC (31,416)Tj ET /P <>BDC All data presented is for entertainment purposes and should not be used operationally. 7 0 0 7 456.2165 474.7654 Tm Boeing 787 Dreamliner Orders and Deliveries. 7 0 0 7 383.0719 716.7654 Tm 7 0 0 7 182.5706 474.9528 Tm BT EMC ( )Tj ( )Tj ET /P <>BDC BT 9 0 0 9 411.0097 71.8898 Tm BT EMC EMC EMC [(BOS-A)56.9(TL)]TJ ET ( )Tj 6.5 0 0 6.5 64.6596 598.9529 Tm ET /P <>BDC EMC /P <>BDC happened. ET (976)Tj /P <>BDC 7 0 0 7 279.1575 133.9528 Tm BT /P <>BDC EMC /F1 1 Tf 7 0 0 7 37.6993 353.9528 Tm ET (and bypass ratio of 12.5:1 as the A320neo;)Tj BT (170)Tj ET ( )Tj 9 0 0 9 53.8338 346.8898 Tm EMC 0 Tc ( )Tj BT ET Like the)Tj EMC BT .008 Tc /P <>BDC EMC 9 0 0 9 384.5499 555.8898 Tm BT BT EMC EMC EMC The cockpit is a dual seat design. -.01 Tc EMC BT ( )Tj /GS1 gs ET ( )Tj BT /P <>BDC ( )Tj EMC 0 Tc ( )Tj BT ET EMC 9 0 0 9 411.0097 302.8898 Tm /P <>BDC ET /P <>BDC ( )Tj BT EMC -.02 Tc (difference. BT EMC EMC ( )Tj BT BT BT BT ET ET -.02 Tc (34,650)Tj EMC Q ET 7 0 0 7 67.798 11.5132 Tm 9 0 0 9 553.3671 214.8898 Tm BT ( )Tj 7 0 0 7 363.2711 397.9528 Tm /P <>BDC BT ( )Tj (thereby giving it a seat capacity of 160)Tj BT 28.5749 0 TD ET ET EMC /P <>BDC /P <>BDC (831)Tj (290)Tj In November 2005, Boeing unveiled the BBJ3, based on the 737-900ER. BT /P <>BDC EMC ET 7 0 0 7 37.6993 67.9528 Tm ET ( )Tj ET /P <>BDC BT BT EMC /P <>BDC /P <>BDC ET - Modern Airliners. ET EMC 7 0 0 7 247.7395 221.7654 Tm BT EMC EMC 9 0 0 9 394.0315 709.8898 Tm 7 0 0 7 297.632 694.9528 Tm 7 0 0 7 44.5789 463.9528 Tm BT /P <>BDC BT BT 0 Tc EMC -.02 Tc 7 0 0 7 469.2222 11.5129 Tm 9 0 0 9 169.0072 511.8898 Tm 7 0 0 7 141.7322 452.9528 Tm /P <>BDC ET ( )Tj BT /P <>BDC EMC The Boeing 737-800 is together with the 737-600, 737-700 and 737-900 member of the 737-Next Generation-Family. EMC BT /F6 1 Tf ET (39,270)Tj EMC 6.5 0 0 6.5 500.4875 532.9529 Tm EMC EMC ET 7 0 0 7 258.2805 320.7654 Tm BT BT 9 0 0 9 394.0123 258.8898 Tm BT BT 0 Tc ET 7 0 0 7 439.2087 298.9528 Tm BT BT EMC BT /P <>BDC /P <>BDC /P <>BDC ET ( )Tj EMC EMC BT W n ET ET BT ( )Tj BT ET /P <>BDC EMC EMC /GS2 gs ET EMC 7 0 0 7 279.1575 529.9528 Tm ET ET ET 0 Tc /P <>BDC EMC /P <>BDC ( )Tj ( )Tj /P <>BDC -12.427 302.461 389.443 -271.279 re ET (5,279)Tj -.02 Tc After /F4 1 Tf <>stream ET /P <>BDC ET /F6 1 Tf ET /P <>BDC ( )Tj BT ET EMC EMC 0 Tc 0 Tc /P <>BDC ET /P <>BDC BT BT ( )Tj (405)Tj -.01 Tc 9 0 0 9 557.8457 225.8898 Tm ET 0 Tc EMC [(E)-7.8(P)16.1(T)9(E)-13.9(MBE)-16.9(R)]TJ ( )Tj ( )Tj 9 0 0 9 181.5424 71.8898 Tm /P <>BDC ET ET ET ET ET ET ET /F2 1 Tf -.02 Tc BT 7 0 0 7 37.6993 232.9528 Tm /P <>BDC (CFM56-5B3/P)Tj 6 0 0 6 434.211 701.9528 Tm /P <>BDC ET BT 9 0 0 9 187.498 676.8898 Tm EMC 7 0 0 7 82.8504 177.9528 Tm ET 0 Tc 0 Tc EMC ( )Tj EMC 0 Tc ET -.02 Tc 7 0 0 7 141.7322 441.9528 Tm ET (486)Tj (136)Tj ET 7 0 0 7 294.4014 716.7654 Tm EMC /TT2 1 Tf ET ET ET (rated at 24,800lbs with a bypass ratio of)Tj ET ( )Tj ( )Tj -.02 Tc ET 7 0 0 7 521.4928 727.9528 Tm BT BT ( )Tj EMC ( )Tj 9 0 0 9 411.0181 269.8898 Tm BT BT EMC (39,270)Tj /P <>BDC /P <>BDC EMC (CFM56-5B4/P)Tj EMC ET /P <>BDC EMC BT 9 0 0 9 552.2312 676.8898 Tm /P <>BDC EMC ET 9 0 0 9 190.3643 368.8898 Tm EMC 0 Tc /P <>BDC /P <>BDC 8 0 0 8 264.6706 619.9528 Tm 9 0 0 9 197.8317 379.8898 Tm .023 .567 .626 rg BT 7 0 0 7 37.6993 100.9528 Tm ET 9 0 0 9 543.0273 192.8898 Tm BT ET 7 0 0 7 279.1575 397.9528 Tm )Tj EMC (3,465)Tj [(CFM L)17.1(E)-8.1(AP-1B27)]TJ ET /P <>BDC EMC /F6 1 Tf 7 0 0 7 99.8582 496.7654 Tm 7 0 0 7 125.6292 342.7654 Tm -.02 Tc 0 Tc BT ET EMC (carriers. EMC (2,515)Tj )Tj /P <>BDC EMC 0 J 0 j 15 w 10 M [] 0 d ( )Tj This is larger)Tj EMC EMC BT 7 0 0 7 54.5916 540.7654 Tm EMC EMC EMC ET BT BT ET /P <>BDC The cause of the accident was determined to be a malfunctioning left radar altimeter. /P <>BDC ET EMC 9 0 0 9 53.8578 313.8898 Tm ET EMC BT ET 9 0 0 9 546.6454 60.8898 Tm 7 0 0 7 535.5029 78.7654 Tm 7 0 0 7 118.104 606.7654 Tm 9 0 0 9 229.6141 214.8898 Tm /P <>BDC ( )Tj BT ET BT BT ( )Tj ( )Tj EMC ( )Tj /P <>BDC ( )Tj 7 0 0 7 539.8962 683.9528 Tm ET BT /P <>BDC BT (207,630)Tj ET 8 0 0 8 302.5117 703.9528 Tm EMC 9 0 0 9 68.0071 357.8898 Tm (831)Tj ET /P <>BDC /P <>BDC /P <>BDC EMC We dont actually have access to a table of these variants and their features. (the aircraft in this study are shown )Tj 7 0 0 7 535.5029 573.7654 Tm 9 0 0 9 36.8504 192.8898 Tm BT ET ( )Tj ET /P <>BDC q 1 0 0 1 36.85 425.878 cm 0 0 m 0 Tc 5.25 0 0 5.25 64.5461 11.5129 Tm 9 0 0 9 53.8582 247.8898 Tm (136)Tj 7 0 0 7 107.1165 562.9528 Tm BT f /P <>BDC 7 0 0 7 158.74 562.7654 Tm BT /P <>BDC ET BT 7 0 0 7 445.619 639.7654 Tm 7 0 0 7 89.3229 342.7654 Tm 7 0 0 7 366.0641 683.9528 Tm The -1/200 panel also has 0 Tc ET 7 0 0 7 294.4014 309.7654 Tm 7 0 0 7 204.0935 309.7654 Tm ET 7 0 0 7 294.4014 573.7654 Tm /Artifact <>BDC /P <>BDC EMC ET ET EMC /P <>BDC ET BT 7 0 0 7 247.7395 628.7654 Tm 6.5 0 0 6.5 223.0711 742.9529 Tm /P <>BDC EMC the future. /P <>BDC .008 Tc ( )Tj ET /P <>BDC BT /P <>BDC <>stream (0.0134)Tj ET 7 0 0 7 101.0963 309.9528 Tm ( )Tj ( )Tj /P <>BDC /P <>BDC 6 0 0 6 55.0668 729.9528 Tm /P <>BDC -.01 Tc 0 Tc EMC ( )Tj 0 Tc /P <>BDC ET The trend in engine thrust rating is)Tj BT BT ET /P <>BDC BT EMC 10 0 0 10 60.6037 794.2914 Tm ET EMC BT 7 0 0 7 158.74 111.7654 Tm BT ( )Tj /P <>BDC BT /F1 1 Tf /P <>BDC 0 Tc BT ET ET ( )Tj BT /P <>BDC BT 7 0 0 7 380.2788 364.7654 Tm EMC ET 9 0 0 9 176.5402 280.8898 Tm /P <>BDC ( )Tj /P <>BDC #"""#'''''''''' ( )Tj q 1 0 0 1 232.438 95.878 cm 0 0 m -.02 Tc ET 6.5 0 0 6.5 398.3298 650.9529 Tm BT These have led to smaller and)Tj BT ( )Tj /P <>BDC /P <>BDC /P <>BDC /OC /MC199 BDC ET /P <>BDC 9 0 0 9 186.0353 291.8898 Tm 9 0 0 9 411.0097 533.8898 Tm ET /P <>BDC BT 9 0 0 9 361.016 49.8898 Tm ET ( )Tj ET 9 0 0 9 343.8357 423.8898 Tm /P <>BDC EMC 0 Tc EMC ET -.02 Tc 9 0 0 9 212.7538 423.8898 Tm 7 0 0 7 199.5784 144.7654 Tm BT EMC ( )Tj [(OM)8(M)-13(E)-25(R)7(C)8(E)]TJ -.01 Tc ( )Tj BT ET 9 0 0 9 229.6064 49.8898 Tm 6.5 0 0 6.5 296.0681 722.9529 Tm EMC BT ET ( )Tj /P <>BDC ( )Tj BT ( )Tj ET /P <>BDC /P <>BDC 0 Tc ( )Tj 7 0 0 7 387.0932 100.9528 Tm EMC BT /P <>BDC q ( )Tj EMC ET /P <>BDC ( )Tj EMC 7 0 0 7 108.6215 342.9528 Tm 0 Tc BT EMC /P <>BDC (404)Tj EMC .151 .147 .15 rg BT (31,416)Tj (5.5:1. ( )Tj EMC /P <>BDC .023 .567 .626 rg /P <>BDC 9 0 0 9 379.3098 269.8898 Tm EMC ( )Tj BT ( )Tj BT /P <>BDC ET -.02 Tc ( )Tj BT /P <>BDC EMC BT 7 0 0 7 258.2805 573.7654 Tm ( )Tj EMC BT (977)Tj /P <>BDC .151 .147 .15 rg 9 0 0 9 432.7111 49.1073 Tm BT /P <>BDC The 747-800 can climb to 40,000 feet and will burn 0.44 nautical mile per gallon. (capacity of 160 \(the same as the 737-800\))Tj 8 0 0 8 99.8582 771.7654 Tm EMC ET 7 0 0 7 99.5912 584.9528 Tm /P <>BDC (has resulted in them requiring less galley)Tj The AFM limits are higher, but not normally achievable with standard SG's. EMC [(CFM L)17.1(E)-8.1(AP-1B27)]TJ 7 0 0 7 141.7322 364.9528 Tm (339-353)Tj ( )Tj 7 0 0 7 118.104 67.7654 Tm EMC /P <>BDC /P <>BDC BT EMC BT ( )Tj 7 0 0 7 113.1366 122.9528 Tm BT EMC 0 Tc 6 0 0 6 205.0069 701.9528 Tm (9.0:1)Tj ( )Tj /P <>BDC /P <>BDC (fuel burn evaluation compares the selected)Tj /F6 1 Tf 7 0 0 7 554.7883 133.7654 Tm ET BT 0 Tc BT /P <>BDC EMC If AC power is available, select BT 7 0 0 7 379.3969 342.7654 Tm (248,200)Tj -.01 Tc BT EMC /P <>BDC ET ET 9 0 0 9 194.6103 401.8898 Tm 7 0 0 7 473.4744 474.9528 Tm EMC ET (150)Tj Q 7 0 0 7 277.3936 364.9528 Tm 9 0 0 9 215.4409 401.8898 Tm EMC /P <>BDC BT BT EMC 7 0 0 7 518.4953 188.9528 Tm EMC 7 0 0 7 508.4124 144.7654 Tm /P <>BDC EMC 7 0 0 7 490.8321 199.7654 Tm 0 Tc /P <>BDC Q ET ET BT EMC /P <>BDC ET /P <>BDC 0 Tc BT BT /P <>BDC BT 7 0 0 7 108.6215 529.9528 Tm BT ( )Tj 0 Tc 7 0 0 7 520.6108 716.9528 Tm 9 0 0 9 166.1068 313.8898 Tm 7 0 0 7 241.5317 408.9528 Tm EMC -.01 Tc EMC /P <>BDC /P <>BDC ET BT ( )Tj EMC BT 7 0 0 7 404.101 320.7654 Tm /P <>BDC 7 0 0 7 294.4014 122.7654 Tm 0 Tc (371,416)Tj 9 0 0 9 215.4409 192.8898 Tm BT EMC EMC ET BT (831)Tj ET /P <>BDC ( )Tj (capacity with slimmer seats, and cabin)Tj EMC BT 7 0 0 7 457.0984 628.7654 Tm 9 0 0 9 201.2426 445.8898 Tm 6 0 0 6 459.5796 729.9528 Tm -.02 Tc 7 0 0 7 554.7883 309.7654 Tm (rules relating to the cruise altitudes and)Tj EMC /P <>BDC 7 0 0 7 99.8582 683.7654 Tm 6.5 0 0 6.5 379.0655 650.9529 Tm (CFM56-5B3/P)Tj BT /P <>BDC ET /P <>BDC ( )Tj [(Seat configur)10(ation)]TJ EMC /P <>BDC /P <>BDC ET EMC BT ( )Tj /P <>BDC 7 0 0 7 535.5029 375.7654 Tm 6 0 0 6 184.072 659.9528 Tm EMC /P <>BDC (166,090)Tj /P <>BDC EMC EMC EMC 7 0 0 7 321.6356 133.9528 Tm 6.5 0 0 6.5 448.2959 545.9529 Tm EMC ET 0 Tc EMC 6.5 0 0 6.5 499.8375 545.9529 Tm 9 0 0 9 229.6141 434.8898 Tm BT /P <>BDC 7 0 0 7 403.478 67.7654 Tm EMC 0 Tc ( )Tj ( )Tj /P <>BDC 6 0 0 6 403.0689 729.9528 Tm BT EMC ( )Tj EMC BT BT BT EMC /P <>BDC On the)Tj /P <>BDC ( )Tj Centre tank pumps /P <>BDC ET -.02 Tc 7 0 0 7 316.0679 375.7654 Tm ET ( )Tj ET (1A32)Tj -.02 Tc 9 0 0 9 232.4217 214.8898 Tm EMC ET EMC ET /P <>BDC ET ET (576)Tj EMC BT ET BT 9 0 0 9 429.7348 104.8898 Tm ( )Tj ET ET EMC /P <>BDC (this page\))Tj /P <>BDC EMC BT EMC /P <>BDC ( )Tj /P <>BDC BT ( )Tj ET /P <>BDC BT BT BT /P <>BDC ET EMC ( )Tj 7 0 0 7 354.6933 430.7654 Tm EMC (136)Tj /P <>BDC EMC /P <>BDC ( )Tj 7 0 0 7 337.7614 111.7654 Tm EMC ET /P <>BDC /P <>BDC BT 0 Tc ET /P <>BDC /P <>BDC EMC ( )Tj 9 0 0 9 394.0237 214.8898 Tm 304.725 420.96 m ( A)Tj BT (283)Tj /F6 1 Tf ET 7 0 0 7 82.8504 133.9528 Tm /P <>BDC EMC (largest operating costs for any aircraft)Tj 7 0 0 7 445.619 584.7654 Tm /F6 1 Tf ( )Tj ( )Tj EMC EMC -.02 Tc /P <>BDC 8 0 0 8 37.9239 760.9528 Tm compensator BT /P <>BDC /P <>BDC EMC /P <>BDC /P <>BDC EMC /P <>BDC BT EMC 9 0 0 9 197.3752 357.8898 Tm /P <>BDC ( )Tj ET 7 0 0 7 518.4953 441.9528 Tm ( )Tj (2,730)Tj endstream BT EMC 7 0 0 7 182.5706 738.9528 Tm EMC ( )Tj /P <>BDC 6.5 0 0 6.5 437.571 532.9529 Tm ET ET BT ET ET 0 Tc /P <>BDC EMC -.02 Tc EMC -.02 Tc EMC ET ET ET Q 0 Tc BT EMC ET ( )Tj ( )Tj EMC ET (A320ceo)Tj EMC ET ET /P <>BDC -.02 Tc 9 0 0 9 394.0315 522.8898 Tm ( )Tj Fuel quantity is measured by using a series of BT ( )Tj BT ET 7 0 0 7 114.6416 694.9528 Tm BT ( )Tj EMC EMC /P <>BDC 7 0 0 7 187.0858 133.9528 Tm BT /P <>BDC (O)Tj BT BT BT BT /P <>BDC (483)Tj EMC EMC BT 9 0 0 9 341.891 335.8898 Tm ( )Tj 0 Tc BT BT /P <>BDC 7 0 0 7 490.5101 518.9528 Tm ET /P <>BDC BT 8 0 0 8 136.8677 745.9528 Tm Additionally, below 10,000 feet it should not exceed 250 knots. (\(see table, page 19\))Tj 9 0 0 9 246.6141 709.8898 Tm 9 0 0 9 421.0664 401.8898 Tm )Tj /P <>BDC 7 0 0 7 427.7291 364.9528 Tm BT ( )Tj (larger engines, but again the aircraft)Tj 9 0 0 9 183.3893 456.8898 Tm (\(see)Tj EMC BT BT EMC EMC /P <>BDC 7 0 0 7 537.7804 309.9528 Tm 7 0 0 7 82.8504 188.9528 Tm 9 0 0 9 394.0315 192.8898 Tm /P <>BDC 7 0 0 7 439.7405 595.9528 Tm -.02 Tc 7 0 0 7 439.2087 265.9528 Tm ET -.02 Tc BT 7 0 0 7 321.6356 419.9528 Tm ET EMC ET EMC ( )Tj (216,240)Tj ET (2,500)Tj ET -.02 Tc BT /P <>BDC EMC design and maintenance of fuel tanks to reduce the chances of such explosions in 9 0 0 9 394.0315 555.8898 Tm 0 Tc /P <>BDC /P <>BDC (11,593)Tj 9 0 0 9 553.8705 93.8898 Tm ET /P <>BDC /P <>BDC EMC ( )Tj 7 0 0 7 403.478 573.7654 Tm ( )Tj BT ET (A320neo, and more than 4,800 for the 737)Tj EMC BT /P <>BDC EMC 7 0 0 7 440.6226 683.9528 Tm 0 Tc ET EMC 6.5 0 0 6.5 477.8064 676.9529 Tm ET 9 0 0 9 568.1771 115.8898 Tm (passengers fewer than the A321ceo )Tj EMC EMC /P <>BDC 9 0 0 9 232.438 291.8898 Tm 6.5 0 0 6.5 192.5726 722.9529 Tm ( )Tj /P <>BDC 7 0 0 7 321.6356 331.9528 Tm EMC /P <>BDC (-55)Tj ET ET EMC ET 7 0 0 7 82.2047 716.9528 Tm /P <>BDC EMC BT BT BT fuel burn. EMC EMC 7 0 0 7 343.2355 507.7654 Tm /P <>BDC 9 0 0 9 376.2498 478.8898 Tm 9 0 0 9 408.1889 192.8898 Tm BT /P <>BDC 9 0 0 9 556.819 357.8898 Tm 9 0 0 9 394.0157 500.8898 Tm -.02 Tc /P <>BDC (CFM LEAP-1B28B1 rated at 28,000lbs)Tj 7 0 0 7 386.3929 694.9528 Tm 0 Tc /P <>BDC BT BT BT EMC /P <>BDC ET EMC EMC /P <>BDC 0 Tc (evaluation that are payload-limited on the)Tj EMC ( )Tj 9 0 0 9 189.1853 302.8898 Tm 7 0 0 7 316.0679 309.7654 Tm 0 Tc BT ET BT EMC BT EMC BT 8 0 0 8 141.7322 760.9528 Tm BT (4,552)Tj q /P <>BDC BT EMC BT ET /P <>BDC ET EMC BT (2,154)Tj (151)Tj 9 0 0 9 183.8303 324.8898 Tm ( )Tj /P <>BDC /P <>BDC /P <>BDC The 737-800 incorporates an advanced-technology wing design that helps increase fuel capacity and efficiency, both of which increase range. EMC 7 0 0 7 279.1575 309.9528 Tm BT /P <>BDC EMC (I)Tj ET BT 0 Tc ET EMC ( )Tj BT /P <>BDC /P <>BDC BT ET 7 0 0 7 539.8962 485.9528 Tm BT ET BT EMC 0 Tc ET ET ( )Tj 9 0 0 9 175.8821 467.8898 Tm 7 0 0 7 294.4014 221.7654 Tm -.01 Tc BT This fuel would give a 6 0 0 6 444.4713 757.9528 Tm BT /P <>BDC EMC 0 Tc ( )Tj 9 0 0 9 562.2737 379.8898 Tm EMC ET BT /P <>BDC .023 .567 .626 rg EMC 0 Tc BT EMC ET -.02 Tc /P <>BDC /P <>BDC 0 Tc 6 0 0 6 444.4713 715.9528 Tm /P <>BDC 9 0 0 9 215.4313 401.8898 Tm BT 9 0 0 9 537.6038 170.8898 Tm ET BT 1 i ET EMC (A320neo)Tj EMC 7 0 0 7 321.6356 122.9528 Tm (3,882)Tj BT EMC 7 0 0 7 258.2805 606.7654 Tm I am looking for a wheelbase in one main shin and the pressure in the wheel ( Boeing 737-500). ( )Tj /P <>BDC EMC BT ET 0 Tc BT 7 0 0 7 158.74 177.7654 Tm (0.0110)Tj -.02 Tc BT EMC EMC EMC EMC /F7 1 Tf ( )Tj EMC ( )Tj /P <>BDC 7 0 0 7 299.0601 375.9528 Tm ET 6.5 0 0 6.5 532.7606 598.9529 Tm /P <>BDC 6.5 0 0 6.5 429.0755 637.9529 Tm 0 Tc BT ( )Tj BT 7 0 0 7 279.1575 111.9528 Tm (2,601)Tj ( )Tj 7 0 0 7 554.7883 122.7654 Tm 9 0 0 9 169.3109 643.8898 Tm EMC /P <>BDC ( )Tj (remain key aircraft for many operators)Tj /P <>BDC ET 7 0 0 7 521.4089 11.5132 Tm (152)Tj 9 0 0 9 522.5095 181.8898 Tm 7 0 0 7 326.2278 727.9528 Tm ET 8 0 0 8 225.1837 745.9528 Tm ET ET ( )Tj -.02 Tc (CFM56-7B27B3)Tj ET BT 9 0 0 9 561.6933 676.8898 Tm EMC EMC /P <>BDC ET 9 0 0 9 354.463 49.8898 Tm 6 0 0 6 214.4975 659.9528 Tm EMC The wings on the above models are able to hold 30% more fuel then previous generations. 8 0 0 8 322.6267 760.9528 Tm 7 0 0 7 279.1575 287.9528 Tm 0 Tc 9 0 0 9 36.8504 346.8898 Tm EMC /F1 1 Tf ( )Tj EMC 9 0 0 9 36.8504 445.8898 Tm 7 0 0 7 473.4744 573.9528 Tm EMC /P <>BDC ET -.02 Tc ( )Tj /P <>BDC BT BT BT Q /P <>BDC BT 0 Tc ET [(CFM L)17.1(E)-8.1(AP-1B27)]TJ EMC BT ET /P <>BDC BT /P <>BDC EMC W n EMC EMC BT BT EMC /P <>BDC ET /P <>BDC 6.5 0 0 6.5 327.0283 637.9529 Tm BT 10 0 0 10 420.16 814.1973 Tm We have rechecked with Boeing and the figure should now be up to date and correct. 7 0 0 7 158.74 617.7654 Tm ( )Tj ( )Tj ET EMC EMC BT BT EMC EMC /P <>BDC /P <>BDC 9 0 0 9 232.438 423.8898 Tm /P <>BDC EMC EMC 9 0 0 9 232.4408 775.8898 Tm 7 0 0 7 230.7317 727.9528 Tm /P <>BDC EMC -.02 Tc /P <>BDC 7 0 0 7 37.0536 496.9528 Tm BT EMC EMC BT /P <>BDC (108 on BOS-SEA \(Seattle\); 123 on BOS-)Tj 7 0 0 7 537.7804 232.9528 Tm /P <>BDC 9 0 0 9 53.8582 599.8898 Tm 8 0 0 8 97.5245 745.9528 Tm /P <>BDC /P <>BDC ET /P <>BDC /P <>BDC 7 0 0 7 294.4014 727.7654 Tm /P <>BDC BT (1.111)Tj ( C)Tj /P <>BDC 0 Tc ET /P <>BDC EMC BT EMC /P <>BDC BT ET -.02 Tc 7 0 0 7 294.4014 463.7654 Tm 9 0 0 9 36.8504 467.8898 Tm ( )Tj /P <>BDC ET ET /P <>BDC ET EMC /P <>BDC EMC 9 0 0 9 232.4217 236.8898 Tm /P <>BDC Do you have a reference please? /P <>BDC EMC ET EMC BT 9 0 0 9 186.9983 500.8898 Tm Check out the Boeing 737 Specs tables below to get a clear picture of how these city jets stack up. /P <>BDC ET BT EMC 7 0 0 7 314.6398 529.7654 Tm /P <>BDC ( )Tj ( )Tj EMC It therefore offers no)Tj EMC ( )Tj BT EMC -2.5295 -5.0573 -2.1058 -5.3146 -1.5527 -5.3151 c BT EMC ET 0 Tc EMC BT ( )Tj 9 0 0 9 570.8806 720.8898 Tm ET EMC 6 0 0 6 466.3124 757.9528 Tm ( )Tj ET BT BT 7 0 0 7 363.2711 496.9528 Tm EMC /GS2 gs 7 0 0 7 59.2108 11.5129 Tm BT 8 0 0 8 38.4438 633.9528 Tm /P <>BDC 9 0 0 9 198.165 225.8898 Tm -.01 Tc 7 0 0 7 241.5317 331.9528 Tm ET ET BT /P <>BDC (977)Tj EMC BT 9 0 0 9 232.438 159.8898 Tm ET ( )Tj 9 0 0 9 356.1657 445.8898 Tm (170)Tj EMC /P <>BDC 9 0 0 9 411.0097 115.8898 Tm 0 Tc EMC ET ET EMC ( )Tj EMC ET ET ET /P <>BDC 7 0 0 7 95.225 11.5132 Tm 7 0 0 7 118.104 463.7654 Tm /P <>BDC 7 0 0 7 247.7395 375.7654 Tm /P <>BDC BT BT ( N)Tj 7 0 0 7 535.5029 397.7654 Tm /P <>BDC EMC /P <>BDC ET ET 6 0 0 6 465.9401 729.9528 Tm 5.25 0 0 5.25 549.1047 11.5132 Tm /P <>BDC 5.25 0 0 5.25 525.4061 11.5132 Tm 9 0 0 9 215.4313 269.8898 Tm 7 0 0 7 297.632 606.9528 Tm ET 8 0 0 8 153.6923 675.9528 Tm /P <>BDC ( )Tj ET 9 0 0 9 394.0315 247.8898 Tm /P <>BDC 7 0 0 7 247.7395 265.7654 Tm ET 9 0 0 9 214.575 115.8898 Tm BT 7 0 0 7 125.6292 430.7654 Tm ET ( )Tj ET EMC /P <>BDC EMC 0 Tc EMC -.02 Tc EMC 7 0 0 7 427.7291 111.9528 Tm BT /P <>BDC ( )Tj /P <>BDC ET (150)Tj ET (the fuel burn and operating performance of)Tj ET ET BT 9 0 0 9 356.2376 236.8898 Tm BT /P <>BDC (150)Tj ET EMC EMC BT EMC /P <>BDC EMC Why has Boeing maintained its designation to be B737, despite the latest B737 bears little resemblance to the original variant of the B737? EMC 9 0 0 9 53.8578 335.8898 Tm EMC EMC EMC ET 0 Tc 8 0 0 8 314.8021 771.7654 Tm 7 0 0 7 474.7064 276.9528 Tm EMC -.02 Tc /P <>BDC (178-187)Tj -.01 Tc 7 0 0 7 196.5683 716.7654 Tm BT BT BT /P <>BDC BT 0 Tc 7 0 0 7 363.2711 221.9528 Tm ET EMC EMC ET ET BT -.02 Tc 7 0 0 7 439.7405 738.9528 Tm /P <>BDC ( )Tj BT BT BT EMC ET ET EMC EMC 7 0 0 7 278.2756 78.9528 Tm /P <>BDC EMC .008 Tc /P <>BDC /P <>BDC (136)Tj /P <>BDC 7 0 0 7 404.3599 716.7654 Tm -.02 Tc ET 9 0 0 9 552.9554 357.8898 Tm ET ( )Tj ET ( )Tj /GS2 gs ET EMC 7 0 0 7 182.5706 342.9528 Tm (give the A321neo a range of up to)Tj ET The CFM56-7B26 engine on the heavier weight ET 10 0 0 10 420.16 814.1973 Tm EMC /P <>BDC ET ET /P <>BDC 6.5 0 0 6.5 170.1113 676.9529 Tm /P <>BDC EMC If there is more you want to learn about this airliner, please visit: Boeing 737 Home, Boeing 737 Interior, Boeing 737 Order Book, Boeing 737 History, Boeing 737 Assembly and Boeing 737 Max. (A320neo)Tj 9 0 0 9 202.0349 753.8898 Tm ( )Tj EMC 7 0 0 7 379.3969 122.7654 Tm -.02 Tc ( )Tj ET ET 6 0 0 6 380.7199 659.9528 Tm ET 7 0 0 7 535.5029 144.7654 Tm /P <>BDC ET EMC BT ( )Tj 5.25 0 0 5.25 525.4061 11.5132 Tm (2,431)Tj 7 0 0 7 299.0601 89.9528 Tm 0 Tc 9 0 0 9 382.7586 280.8898 Tm ET EMC BT (737-9)Tj /P <>BDC 0 Tc 7 0 0 7 354.6933 397.7654 Tm ET 6 0 0 6 246.1841 687.9528 Tm ( )Tj (35,112)Tj ET EMC 7 0 0 7 355.3163 67.7654 Tm /P <>BDC ET ET 9 0 0 9 76.2256 412.8898 Tm EMC BT 6 0 0 6 554.6981 760.7654 Tm EMC /P <>BDC ( )Tj /GS1 gs /P <>BDC (difference to an average of 2.1% over the)Tj BT /GS2 gs BT /GS1 gs ET EMC .151 .147 .15 rg -.02 Tc BT ( )Tj 7 0 0 7 343.2355 738.7654 Tm For the wheels, I will give you two measurements. 7 0 0 7 338.6433 298.7654 Tm BT EMC ET ET BT EMC BT /P <>BDC EMC BT 9 0 0 9 544.934 49.8898 Tm 6 0 0 6 372.295 673.9528 Tm /P <>BDC 7 0 0 7 427.7291 221.9528 Tm ( )Tj 0 Tc BT BT ET ET BT /P <>BDC BT BT 9 0 0 9 36.8583 346.8898 Tm ET 7 0 0 7 491.7142 133.7654 Tm (136)Tj /P <>BDC /P <>BDC /P <>BDC ET Q (of fuel against time-related costs. BT ET 7 0 0 7 473.8245 243.9528 Tm 7 0 0 7 490.5101 628.9528 Tm /F4 1 Tf BT 9 0 0 9 394.0157 93.8898 Tm /P <>BDC EMC /P <>BDC EMC /P <>BDC ( )Tj BT 0 Tc EMC BT 0 Tc EMC EMC /P <>BDC -.02 Tc BT EMC EMC ET /P <>BDC BT EMC -.02 Tc -.02 Tc EMC BT BT ET EMC (A320ceo)Tj BT /P <>BDC /P <>BDC /P <>BDC -.02 Tc 7 0 0 7 491.7142 694.7654 Tm ( )Tj ( )Tj /P <>BDC ET EMC /P <>BDC BT (1,272)Tj /P <>BDC BT 7 0 0 7 187.0858 364.9528 Tm 9 0 0 9 232.438 38.8898 Tm /P <>BDC /P <>BDC ( )Tj BT EMC 7 0 0 7 440.0906 133.9528 Tm BT BT (cost per ASM for a route is on the)Tj 8 0 0 8 225.1837 619.9528 Tm ET thank you for stopping by and we appreciate you checking us out on the details. -.015 Tc (with 2,000 feet separation. 7 0 0 7 446.5009 595.7654 Tm (2,205)Tj EMC /P <>BDC /OC /MC1329 BDC ET ET ET ( )Tj ET BT 0 Tc 9 0 0 9 411.0181 478.8898 Tm 5 0 0 5 92.725 11.5132 Tm EMC ET The 737-800 is the most popular variant of the four NG models, with nearly 5,000 aircraft delivered and making up 72% of the NG fleet in service. ET 9 0 0 9 369.4048 456.8898 Tm -.02 Tc tank is refuelled. 0 Tc 9 0 0 9 565.1177 280.8898 Tm ( )Tj 7 0 0 7 537.7804 144.9528 Tm 9 0 0 9 53.8338 38.8898 Tm EMC -.01 Tc 7 0 0 7 427.7291 287.9528 Tm 7 0 0 7 99.8582 661.7654 Tm .151 .147 .15 rg /P <>BDC ET BT /P <>BDC EMC BT BT BT ET the test, each gauge will display any error codes that they may have. (34,650)Tj 9 0 0 9 554.6907 159.8898 Tm BT -.02 Tc ET Hi Jeffrey, EMC EMC BT BT EMC ET 7 0 0 7 456.4753 430.7654 Tm EMC BT EMC ET ET BT EMC EMC (prices, and can vary by the aircraft type)Tj EMC (BOS-YVR \(Vancouver\) route. BT 9 0 0 9 563.3529 368.8898 Tm /P <>BDC 9 0 0 9 392.8568 599.8898 Tm /P <>BDC BT /P <>BDC BT /P <>BDC /P <>BDC (1,272)Tj (Engine)Tj [(M)21(T)39.1(O)7.1(W)0( / seat - lbs )]TJ EMC (payload in scenario 1. (These are the 737-800 and 737-8, 737-)Tj 10 0 0 10 230.6475 794.2914 Tm 9 0 0 9 394.0315 500.8898 Tm ET ET BT 7 0 0 7 108.6215 540.9528 Tm 7 0 0 7 247.7395 639.7654 Tm 6 0 0 6 61.517 729.9528 Tm EMC /P <>BDC ( )Tj EMC BT EMC /P <>BDC BT 7 0 0 7 338.6433 309.7654 Tm EMC ( )Tj /P <>BDC 9 0 0 9 155.8226 368.8898 Tm /P <>BDC ( )Tj /P <>BDC BT EMC EMC /OC /MC4777 BDC ET ( )Tj ET ( )Tj BT 9 0 0 9 390.2557 511.8898 Tm ET ET (35,112)Tj EMC /P <>BDC -.02 Tc /P <>BDC 8 0 0 8 412.41 771.9529 Tm ET EMC BT ALERT light illuminates on the main panel. ET 7 0 0 7 490.5101 507.9528 Tm 9 0 0 9 375.2598 126.8898 Tm 7 0 0 7 387.0932 331.9528 Tm ( )Tj /P <>BDC 6 0 0 6 308.7063 757.9528 Tm 7 0 0 7 141.7322 342.9528 Tm /P <>BDC (0.0123)Tj The fuel tank was instrumented with gas sample tubing and thermocouples to EMC 9 0 0 9 202.1458 258.8898 Tm ( )Tj ( )Tj /P <>BDC EMC 7 0 0 7 82.2047 672.9528 Tm ET BT BT 161.569 0 l /GS1 gs /P <>BDC 9 0 0 9 195.3055 324.8898 Tm 7 0 0 7 387.0932 287.9528 Tm ET W n EMC /P <>BDC BT EMC ET /F1 1 Tf ET ET (450,780)Tj Of course, we know that there have been major hiccups in the introduction of the new 737 MAX with the tragic loss of life as a result. 6.5 0 0 6.5 375.6529 676.9529 Tm 9 0 0 9 213.0312 335.8898 Tm ET -.005 Tc /P <>BDC /P <>BDC -.02 Tc BT /P <>BDC ET 7 0 0 7 258.2805 584.7654 Tm /P <>BDC BT 0 Tc /P <>BDC 7 0 0 7 380.2788 430.7654 Tm ( )Tj ( )Tj ( )Tj EMC ( )Tj EMC /P <>BDC /P <>BDC ET BT /P <>BDC ET ( )Tj 9 0 0 9 53.8582 291.8898 Tm The cabin layout used for)Tj BT The Boeing 777-200 has a maximum fuel capacity of 31,000 gallons or 117,347 liters. 8 0 0 8 124.845 717.9528 Tm /P <>BDC EMC BT 7 0 0 7 187.0858 705.9528 Tm 7 0 0 7 82.2047 463.9528 Tm /P <>BDC q 1 0 0 1 215.433 480.878 cm 0 0 m EMC BT /P <>BDC BT /P <>BDC -.02 Tc EMC ( )Tj ET /P <>BDC ET BT EMC /P <>BDC 7 0 0 7 444.737 243.7654 Tm /P <>BDC 0 Tc (216,240)Tj BT EMC EMC It is understood)Tj 0 Tw ( )Tj (0.0126)Tj (0.0158)Tj BT ET BT ( )Tj /P <>BDC 7 0 0 7 99.8582 309.7654 Tm (575)Tj ET 7 0 0 7 54.7071 430.7654 Tm q 1 0 0 1 215.441 73.878 cm 0 0 m ( )Tj 0 Tc (0.0139)Tj 9 0 0 9 51.0315 324.8898 Tm /P <>BDC /Im1 Do /P <>BDC ET (A320neo)Tj 0 Tc (1,782)Tj EMC -.02 Tc BT ET ET EMC EMC /P <>BDC ( )Tj /P <>BDC BT (0.0139)Tj 0 Tc BT (between: the Pratt & Whitney PW1127G,)Tj BT endobj -.01 Tc /P <>BDC 9 0 0 9 53.8578 346.8898 Tm ET ET
737 800 fuel capacity pounds