737 800 fuel capacity pounds737 800 fuel capacity pounds

304.725 420.96 m /P <>BDC There was no additional)Tj EMC -.02 Tc 9 0 0 9 53.8338 192.8898 Tm ET 7 0 0 7 536.3849 111.7654 Tm ET BT (the 14 sectors with the 85% passenger)Tj -.02 Tc EMC BT /Artifact <>BDC EMC EMC /P <>BDC ET EMC ET BT As a result of its lower fuel burn,)Tj ET BT ET 0 Tc -.02 Tc ET BT (CFM56-5B4/P)Tj 7 0 0 7 99.8582 100.7654 Tm ET EMC /P <>BDC ET /P <>BDC )Tj /P <>BDC 0 Tc /P <>BDC )21(The r)10(elativ)12.9(e)]TJ ET 9 0 0 9 385.5399 115.8898 Tm 7 0 0 7 508.4124 727.7654 Tm EMC BT ET (18.3% on the sectors where an equivalent)Tj ( )Tj (the 14 routes in the evaluation. BT (A321neo)Tj -.01 Tc BT BT EMC 0 Tc BT ET BT /P <>BDC /P <>BDC BT 0 Tc /P <>BDC -.02 Tc EMC /P <>BDC 9 0 0 9 385.6838 346.8898 Tm ET (. EMC EMC /P <>BDC (I)Tj ET ET 7 0 0 7 210.1137 562.7654 Tm BT ET ET ET EMC 9 0 0 9 36.8504 280.8898 Tm 7 0 0 7 247.7395 397.7654 Tm ET /P <>BDC (39,732)Tj ET 9 0 0 9 170.626 357.8898 Tm ET 7 0 0 7 279.1575 738.9528 Tm 7 0 0 7 338.5674 122.9528 Tm BT /P <>BDC BT /P <>BDC 0 Tc 10 0 0 10 49.9904 814.1973 Tm ET /F4 1 Tf BT (carriers. BT Airbus A320 Assembly A truly international effort. [(AIRL)8.1(INE & AIR)7.1(CRAF)-12.9(T)18.1( OPERA)56.9(T)-8.1(ION)-13.9(S)]TJ BT ET /P <>BDC ( )Tj ( )Tj BT ET 7 0 0 7 554.7883 474.7654 Tm ET ET (342,312)Tj ET BT EMC BT EMC BT BT BT /P <>BDC 9 0 0 9 246.595 159.8898 Tm /F4 1 Tf (The wider intake fan diameters leading)Tj ET BT 6.5 0 0 6.5 276.4014 650.9529 Tm (The A320 and 737 families have been)Tj EMC /P <>BDC ( )Tj EMC ET ( )Tj [(AS)29.1(M)21(s)]TJ EMC /P <>BDC BT /P <>BDC (31,416)Tj (The fuel cost per ASM difference)Tj ET BT 7 0 0 7 125.6292 144.7654 Tm BT 9 0 0 9 190.4723 71.8898 Tm (ASM. ET /P <>BDC EMC ( )Tj BT BT BT ET BT 9 0 0 9 185.3513 159.8898 Tm -.02 Tc EMC 6 0 0 6 246.7063 757.9528 Tm BT /P <>BDC 7 0 0 7 299.0601 342.9528 Tm 6 0 0 6 154.2695 743.9528 Tm BT BT EMC BT (The aircraft are examined on the basis)Tj BT ET /P <>BDC /P <>BDC EMC (1,824)Tj ET ET EMC /P <>BDC /P <>BDC BT ET BT BT It is)Tj Hi Andrey, BT (188,400)Tj 9 0 0 9 196.725 654.8898 Tm BT -4.2575 -4.8278 -4.5158 -4.0295 -4.515 -3.0604 c ET /P <>BDC EMC /P <>BDC EMC /P <>BDC BT (30,000lbs to 33,000lbs, a fan diameter of)Tj /P <>BDC BT /P <>BDC EMC ( )Tj EMC 9 0 0 9 51.0236 302.8898 Tm /P <>BDC /P <>BDC 7 0 0 7 430.039 639.9528 Tm (than the 737-9. ( )Tj ET /P <>BDC 7 0 0 7 337.6855 485.9528 Tm ( )Tj EMC /P <>BDC 0 Tc ( )Tj 7 0 0 7 158.74 606.7654 Tm (831)Tj ET 9 0 0 9 232.4408 720.8898 Tm /P <>BDC The use of composite materials in the 737 Next Gen or even the 737 Max is quite conservative. -.02 Tc BT 6 0 0 6 527.699 701.9528 Tm ET ET /P <>BDC /P <>BDC BT (152)Tj EMC BT /P <>BDC /P <>BDC ET BT 7 0 0 7 315.5217 584.7654 Tm EMC (132,872)Tj )Tj EMC 9 0 0 9 146.3 346.8898 Tm supplied to the center wing tank and the oxygenenriched air (OEA) is vented ET /P <>BDC ET endobj ( )Tj (170)Tj /P <>BDC BT 7 0 0 7 403.478 485.7654 Tm 7 0 0 7 440.0906 166.9528 Tm -.02 Tc 9 0 0 9 197.3303 170.8898 Tm EMC /P <>BDC EMC ( )Tj /P <>BDC /P <>BDC [(737-900E)-33(R)]TJ BT BT ( )Tj 9 0 0 9 535.511 379.8898 Tm /P <>BDC /P <>BDC (135,453)Tj ET ET /P <>BDC ET (burn comparison. )Tj 9 0 0 9 525.6696 192.8898 Tm )21(The )]TJ /F6 1 Tf ( )Tj BT BT /P <>BDC BT /F1 1 Tf ET EMC ET (. ( )Tj EMC ET Boeing 737-800 Aircraft type: Commercial airplane Manufacturer: Boeing Maiden flight year: 1997 I have flown in this plane Reports (16) Reviews (2) Photos (333) Forum (8) List of aircraft operators Boeing 737-800 Specifications (2,054)Tj EMC ( )Tj EMC 9 0 0 9 53.8578 357.8898 Tm 9 0 0 9 361.9078 401.8898 Tm (revenue benefit of 11 passengers. BT /P <>BDC ET BT 7 0 0 7 204.0935 672.7654 Tm BT ET EMC ( )Tj ( )Tj /P <>BDC ET 7 0 0 7 554.7883 331.7654 Tm 6 0 0 6 527.6392 715.9528 Tm -.02 Tc EMC ( )Tj ET /P <>BDC ( )Tj -.02 Tc /P <>BDC /P <>BDC ET ( )Tj EMC EMC ET on 5 Nov 1990 have been destroyed on the ground due to explosions in the empty BT EMC /P <>BDC ET -.02 Tc 8 0 0 8 394.0157 753.8898 Tm 7 0 0 7 37.6993 89.9528 Tm 7 0 0 7 446.5009 661.7654 Tm -.02 Tc -.02 Tc BT ( )Tj /P <>BDC BT /P <>BDC /P <>BDC 9 0 0 9 411.0181 104.8898 Tm /P <>BDC EMC During cruise, the tolerance is less than 0.5%. ET EMC ET BT 7 0 0 7 490.7815 364.9528 Tm BT BT ET ( )Tj .661 .752 .896 rg BT ET )Tj (10)Tj 0 Tc ( )Tj [(E)-7.8(P)16.1(T)9(E)-13.9(MBE)-16.9(R)]TJ ET ET ET /P <>BDC ET /P <>BDC /OC /MC208 BDC 7 0 0 7 230.7317 529.9528 Tm /P <>BDC /P <>BDC /P <>BDC -.01 Tc -.02 Tc ( )Tj /P <>BDC EMC ( )Tj 7 0 0 7 456.4753 430.7654 Tm EMC 7 0 0 7 490.8321 122.7654 Tm (170)Tj EMC BT (Although there have recently been)Tj EMC ET /P <>BDC ( )Tj 7 0 0 7 247.7395 727.7654 Tm /P <>BDC 10 0 0 10 408.34 814.1973 Tm BT /P <>BDC EMC 6 0 0 6 365.7265 729.9528 Tm /P <>BDC (I)Tj 7 0 0 7 456.2165 309.7654 Tm 7 0 0 7 473.8245 298.9528 Tm ( )Tj 9 0 0 9 394.0315 280.8898 Tm 0 Tc ET /P <>BDC Our Math Says It Isn't. BT 0 Tc 6.5 0 0 6.5 276.5184 565.9529 Tm 9 0 0 9 197.3752 357.8898 Tm 7 0 0 7 125.6292 430.7654 Tm /P <>BDC Im not sure I understand the question. endobj (379)Tj ET (A321ceo)Tj ET EMC BT EMC 7 0 0 7 490.5101 683.9528 Tm EMC EMC EMC BT BT BT BT ET It also boasts a 3,060 Nautical Mile or 5,667 Kilometers travel range. EMC EMC EMC EMC -.02 Tc /P <>BDC EMC ET 9 0 0 9 392.5848 346.8898 Tm BT 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. The 1/200's had heater switches; these used bleed air to heat the /P <>BDC EMC BT -.02 Tc (10,040)Tj ET 7 0 0 7 364.1531 463.9528 Tm 7 0 0 7 491.7142 133.7654 Tm 9 0 0 9 195.231 423.8898 Tm BT EMC .0161 Tc /P <>BDC EMC /P <>BDC /P <>BDC -.01 Tc 7 0 0 7 99.5912 606.9528 Tm /P <>BDC 9 0 0 9 215.433 258.8898 Tm ( )Tj ET BT BT /P <>BDC /P <>BDC /P <>BDC /GS2 gs (151)Tj BT 6.5 0 0 6.5 191.7701 558.9529 Tm (178-187)Tj EMC BT -.02 Tc (. ET ET EMC /P <>BDC /P <>BDC /P <>BDC /F7 1 Tf BT EMC EMC BT ET 7 0 0 7 299.0601 243.9528 Tm ( )Tj EMC ( )Tj (1,813)Tj ( )Tj /P <>BDC /P <>BDC ET ET )Tj Q (BOS-PHX \(Phoenix\); 133 on BOS-YVR;)Tj BT /P <>BDC 360 0 obj 7 0 0 7 445.619 221.7654 Tm (1,351)Tj 9 0 0 9 36.8504 49.8898 Tm (190,800)Tj ET 7 0 0 7 326.2278 540.9528 Tm ET (standard passenger weight of 231lbs that)Tj The Boeing 737-800 is a twin-engined short-to-medium-range narrowbody airliner with a capacity of maximum 189 passengers produced by the American manufacturer Boeing Commercial Airplanes. 0 Tc 8 0 0 8 90.0179 771.7654 Tm -.02 Tc /P <>BDC ET ET BT -.02 Tc BT /P <>BDC EMC EMC 9 0 0 9 336.3455 313.8898 Tm BT (performance of the two reduces to 0.8%)Tj ( )Tj The cause of the accident was determined to be a malfunctioning left radar altimeter. BT ET /F4 1 Tf ET ET EMC BT EMC (CFM56-7B27B3)Tj .151 .147 .15 rg (engine bypass ratio in the case of the 737)Tj /P <>BDC /P <>BDC 10 0 0 10 47.0104 814.1973 Tm EMC EMC 9 0 0 9 51.0236 401.8898 Tm ( )Tj 9 0 0 9 361.016 49.8898 Tm 6.5 0 0 6.5 433.3069 585.9529 Tm /P <>BDC ( )Tj BT ( )Tj BT 9 0 0 9 181.5981 280.8898 Tm EMC )Tj -.01 Tc BT EMC ET BT (the IAE V2533-A5 engine, rated at)Tj /P <>BDC EMC /P <>BDC EMC /P <>BDC ET EMC EMC ET ET ET ( )Tj ( )Tj lights were FILTER ICING on the 1/200. ( )Tj /P <>BDC (193,344)Tj ( )Tj ( )Tj 9 0 0 9 521.6329 137.8898 Tm /P <>BDC EMC EMC (2,731)Tj ET (737-8)Tj /P <>BDC -.02 Tc /P <>BDC ( )Tj /P <>BDC ET ET ET 7 0 0 7 158.74 199.7654 Tm ET ( )Tj ( )Tj BT EMC EMC BT /P <>BDC EMC ET EMC 7 0 0 7 37.0536 562.9528 Tm /P <>BDC ET BT EMC 9 0 0 9 545.0095 357.8898 Tm EMC /P <>BDC EMC ET BT (A321ceo)Tj ET 9 0 0 9 53.8582 643.8898 Tm EMC ET BT EMC EMC 9 0 0 9 408.1968 159.8898 Tm ET (150)Tj ( )Tj EMC /P <>BDC ET ET ( )Tj (burn difference is 2.2%, and results in an)Tj BT EMC (977)Tj 7 0 0 7 490.5101 507.9528 Tm BT 7 0 0 7 537.7804 287.9528 Tm EMC EMC ET (/S)Tj ET 7 0 0 7 141.7322 727.9528 Tm -.02 Tc 7 0 0 7 387.0932 144.9528 Tm (ESAD)Tj EMC 9 0 0 9 394.0123 269.8898 Tm ( )Tj /P <>BDC BT ( )Tj ET EMC ET BT BT BT BT ( )Tj ET EMC /P <>BDC /P <>BDC EMC BT ET The Boeing 737-800 to date has around 5000 units produced and 2019 saw 138 of the 800 roll of the production line. (of aircraft types that are of equal size. /P <>BDC 0 Tc 7 0 0 7 508.4124 298.7654 Tm 7 0 0 7 130.1443 419.7654 Tm 9 0 0 9 455.2971 478.8898 Tm (0.0127)Tj ( )Tj BT 7 0 0 7 457.0984 276.7654 Tm ET ET /P <>BDC BT ( )Tj ET (0.0124)Tj (34,650)Tj EMC BT 0 Tc The)Tj BT 7 0 0 7 491.7142 529.7654 Tm EMC ET ( )Tj 9 0 0 9 68.0314 335.8898 Tm /P <>BDC 0 Tc 9 0 0 9 548.5375 225.8898 Tm (powered by either the CFM56-5 series or)Tj 9 0 0 9 53.8338 225.8898 Tm 6.5 0 0 6.5 346.9224 650.9529 Tm 0 Tc 7 0 0 7 490.5101 595.9528 Tm ET (128-137)Tj 9 0 0 9 232.438 137.8898 Tm EMC (The performance improvement in the)Tj ET EMC ET /P <>BDC 7 0 0 7 196.5683 122.7654 Tm EMC EMC ( )Tj ET 0 Tc 0 Tc EMC BT EMC ET 8 0 0 8 225.1837 717.9528 Tm ET ET EMC /P <>BDC BT /P <>BDC EMC ET 7 0 0 7 338.6433 265.7654 Tm ET BT /P <>BDC EMC Centre tank pumps 0 Tc (CFM56-5B3/P)Tj ( )Tj /P <>BDC /P <>BDC EMC EMC ET /P <>BDC EMC (5,121)Tj ( )Tj )Tj ( )Tj 7 0 0 7 507.7893 628.7654 Tm ET 7 0 0 7 459.6601 11.5129 Tm ET (weight penalty in its OEW compared to its)Tj /P <>BDC BT /P <>BDC 0 Tc BT ET BT -.02 Tc ( )Tj EMC ET ET 0 Tc 7 0 0 7 518.4953 144.9528 Tm BT ET 6.5 0 0 6.5 499.1812 663.9529 Tm 10 0 0 10 49.3644 814.1973 Tm BT 9 0 0 9 558.7096 390.8898 Tm 6.5 0 0 6.5 534.5352 558.9529 Tm 7 0 0 7 554.7883 738.7654 Tm ET ( )Tj (passengers; thereby giving the A321ceo a)Tj 7 0 0 7 294.4014 364.7654 Tm /P <>BDC (than is possible in this article. /P <>BDC /P <>BDC 9 0 0 9 411.0097 214.8898 Tm ET BT ( )Tj 7 0 0 7 294.4014 738.7654 Tm /P <>BDC ( )Tj (variant offers 26,000lbs of thrust, with a)Tj ET /P <>BDC 7 0 0 7 518.4953 342.9528 Tm 7 0 0 7 508.4124 683.7654 Tm 0 Tc ET BT 6.5 0 0 6.5 296.3606 735.9529 Tm BT BT )Tj 8 0 0 8 43.6039 577.9528 Tm ( )Tj .014984 841.89 609.45 -841.89 re BT 0 Tc BT -.02 Tc ( )Tj (464,440)Tj 7 0 0 7 444.737 397.7654 Tm ( )Tj 7 0 0 7 82.8504 89.9528 Tm 0 Tc 7 0 0 7 54.7071 628.7654 Tm (/S)Tj EMC 7 0 0 7 204.0935 573.7654 Tm The aux tanks are located at BT /GS2 gs 0 Tc ( )Tj BT ET W n ET EMC BT EMC 6 0 0 6 372.4689 687.9528 Tm -.02 Tc /P <>BDC BT Q /P <>BDC ( )Tj 9 0 0 9 394.0315 390.8898 Tm 7 0 0 7 427.7291 177.9528 Tm -.02 Tc ET /P <>BDC /P <>BDC -.02 Tc BT 7 0 0 7 37.0536 716.9528 Tm BT EMC 7 0 0 7 37.5838 551.9528 Tm 0 Tc (150)Tj (typically based on the aircrafts certified)Tj (737 MAX 8 & 9 fuel)Tj 9 0 0 9 394.0315 445.8898 Tm /P <>BDC EMC I am looking forward to your responses. /F6 1 Tf /P <>BDC /P <>BDC 7 0 0 7 554.7883 342.7654 Tm /P <>BDC BT /P <>BDC ET /P <>BDC ET 9 0 0 9 545.7273 731.8898 Tm 0 Tc 8 0 0 8 314.3535 661.9528 Tm EMC 7 0 0 7 539.8962 672.9528 Tm EMC BT Aluminium alloys are still the mainstay of the construction materials used with various blends used according to the strength required for the particular component. ET ET BT ET 7 0 0 7 59.2108 11.5129 Tm EMC 7 0 0 7 54.7071 331.7654 Tm 7 0 0 7 158.74 67.7654 Tm 6 0 0 6 115.1719 701.9528 Tm /P <>BDC Wed love you to share what you build when youre done. ET 6 0 0 6 215.373 715.9528 Tm ET /P <>BDC 0 Tc BT ET ET ET ET /P <>BDC BT /P <>BDC /P <>BDC BT /P <>BDC [(M)-13.9(KE/84)]TJ (class cabin configuration used in this study)Tj 0 Tc (O)Tj ET (0.0149)Tj 0 Tc /P <>BDC /P <>BDC ( )Tj ET /P <>BDC BT 6 0 0 6 364.9705 743.9528 Tm 8 0 0 8 239.3289 771.7654 Tm ET EMC /P <>BDC EMC q /P <>BDC ET (159,251)Tj (table, page 19\))Tj BT 9 0 0 9 508.4714 38.8898 Tm EMC ET (20/29/143, giving a maximum capacity of)Tj ET BT /P <>BDC BT EMC BT ( )Tj BT /P <>BDC (163)Tj EMC 6.5 0 0 6.5 398.369 585.9529 Tm EMC 0 Tc BT ET EMC /F6 1 Tf ET (0.0115)Tj -.02 Tc ET /P <>BDC EMC 7 0 0 7 247.7395 210.7654 Tm BT (0.0194)Tj /P <>BDC EMC BT 9 0 0 9 411.0181 302.8898 Tm 7 0 0 7 294.4014 287.7654 Tm 0 Tc EMC BT /P <>BDC BT BT A previous model which had success was Airbuses A320. /P <>BDC ET (give the newer type a further advantage. ( )Tj ET /P <>BDC ( )Tj 7 0 0 7 247.7395 111.7654 Tm (A321neo)Tj BT 9 0 0 9 361.1316 214.8898 Tm 9 0 0 9 215.4409 181.8898 Tm 9 0 0 9 425.1913 291.8898 Tm -.02 Tc BT BT EMC BT (7,379)Tj 0 Tc ( )Tj (576)Tj I think in the table you are talking about the range where payload is limited by MTOW. ET ET ET ( )Tj ET EMC BT ( )Tj ET ( )Tj ET thank you for stopping by and we appreciate you checking us out on the details. 0 Tc ( )Tj 6.5 0 0 6.5 324.4345 650.9529 Tm /P <>BDC 9 0 0 9 68.3339 445.8898 Tm EMC ET 7 0 0 7 299.0601 122.9528 Tm EMC EMC 7 0 0 7 337.9444 100.9528 Tm 9 0 0 9 36.8504 38.8898 Tm /P <>BDC ( )Tj ( )Tj ( )Tj 9 0 0 9 215.4409 522.8898 Tm ET EMC ET 8 0 0 8 317.9854 771.9529 Tm (2,800 -)Tj .0161 Tc BT 6.5 0 0 6.5 176.1172 624.9529 Tm ( )Tj EMC EMC EMC ET BT .559 .331 .619 rg BT ET /P <>BDC 7 0 0 7 118.104 210.7654 Tm /P <>BDC /P <>BDC /P <>BDC -.02 Tc 7 0 0 7 258.2805 177.7654 Tm S EMC ET BT ( )Tj 7 0 0 7 230.7317 232.9528 Tm BT BT ET EMC 9 0 0 9 215.4313 159.8898 Tm ( )Tj 7 0 0 7 314.6398 474.7654 Tm BT /P <>BDC (temperature )Tj /P <>BDC .151 .147 .15 rg 7 0 0 7 158.74 584.7654 Tm ET BT 7 0 0 7 321.6356 177.9528 Tm ET ET ET ( )Tj -.2034 -.7911 -.1202 -.4766 0 0 c 9 0 0 9 193.0624 445.8898 Tm ET ( )Tj ( )Tj ET EMC BT BT q 1 0 0 1 36.85 84.878 cm 0 0 m 432 0 obj ET EMC (170)Tj (mainline carriers may in fact opt to use a)Tj (compared to the A320ceo. BT ( N)Tj EMC /P <>BDC -.01 Tc ET BT ET ET BT EMC /P <>BDC /P <>BDC /P <>BDC - Simmonds, Digital Fuel Quantity Indicator Error Codes 7 0 0 7 491.4046 144.9528 Tm ET BT 0 Tc ET maximum declarable fuel capacity for tech log, nav log, etc is 16,200kgs for .008 Tc ET BT 9 0 0 9 36.8504 148.8898 Tm BT f /OC /MC1957 BDC BT ( )Tj BT ET ET EMC 9 0 0 9 171.8783 434.8898 Tm EMC (the 737-9 reduces the block fuel burn)Tj 6.5 0 0 6.5 379.1824 565.9529 Tm ET 6.5 0 0 6.5 397.0428 532.9529 Tm 7 0 0 7 247.7395 705.7654 Tm ( )Tj BT 6 0 0 6 246.1841 687.9528 Tm ET /P <>BDC /P <>BDC BT /P <>BDC 7 0 0 7 337.6855 397.9528 Tm 0 Tc ( )Tj /P <>BDC BT ET BT /P <>BDC BT BT (3,691)Tj (the CFM LEAP-1A32 variant. BT ET ET (A321neo)Tj EMC BT (Block fuel)Tj ET EMC BT -.02 Tc 7 0 0 7 343.2355 716.7654 Tm ET EMC ( )Tj (152)Tj BT ( )Tj /P <>BDC 8 0 0 8 347.1567 771.9529 Tm 7 0 0 7 230.7317 474.9528 Tm ET ET ( )Tj The Boeing 737-800 has a maximum fuel capacity of 6,875 gallons or 26,020 liters. EMC (379)Tj BT ( )Tj EMC BT 0 Tc BT 0 Tc ET 7 0 0 7 536.3849 463.7654 Tm ET body angle so number 2 engine fuel is drawn from main tank 2, while engine 1 is /P <>BDC ET ET 7 0 0 7 344.1175 584.7654 Tm EMC 7 0 0 7 354.6933 386.7654 Tm ET EMC (0.0160)Tj ( )Tj BT 7 0 0 7 70.8101 144.9528 Tm /P <>BDC ET ( )Tj /P <>BDC ET EMC ( A)Tj BT ET ET /P <>BDC /P <>BDC BT /Artifact <>BDC 7 0 0 7 508.2252 11.5129 Tm EMC BT BT BT ( )Tj BT /P <>BDC ( )Tj 0 Tc /P <>BDC (for the purposes of this performance)Tj (831)Tj /P <>BDC )Tj 0 Tc 10 0 0 10 420.16 814.1973 Tm BT 7 0 0 7 343.2355 705.7654 Tm EMC /P <>BDC 7 0 0 7 337.4684 705.9528 Tm 6.5 0 0 6.5 176.1172 558.9529 Tm /P <>BDC /P <>BDC BT (is used on the CFM56-5B3/P, despite the)Tj ET (burn and operating)Tj BT ( )Tj /P <>BDC BT 6.5 0 0 6.5 170.1113 676.9529 Tm EMC EMC Our Math Says It Isn't. BT EMC /P <>BDC /P <>BDC ET 7 0 0 7 99.8582 672.7654 Tm /P <>BDC ( )Tj BT BT BT EMC EMC 8 0 0 8 225.1837 675.9528 Tm ( )Tj BT /P <>BDC /P <>BDC (aircraft operators plan and fly using the)Tj 7 0 0 7 141.7322 364.9528 Tm /P <>BDC ET 7 0 0 7 508.4124 518.7654 Tm 9 0 0 9 36.8504 49.8898 Tm (payload and route, and 16% higher than)Tj ( )Tj ( )Tj BT EMC -.01 Tc /P <>BDC /P <>BDC EMC BT ET 0 Tc EMC /P <>BDC 9 0 0 9 394.0123 313.8898 Tm (737-800W)Tj ET -.02 Tc EMC (2,517)Tj /P <>BDC EMC ET ET 6 0 0 6 513.0339 673.9528 Tm 7 0 0 7 116.3631 11.5132 Tm BT EMC /P <>BDC EMC ET BT 9 0 0 9 215.4409 489.8898 Tm ET /P <>BDC ( )Tj /OC /MC2279 BDC /P <>BDC BT ET /P <>BDC -.02 Tc /P <>BDC /P <>BDC EMC ET 9 0 0 9 53.8578 368.8898 Tm .008 Tc /P <>BDC /P <>BDC Fully loaded, the jet can fly up to 3,159 miles without refueling. /P <>BDC /F4 1 Tf /P <>BDC ET 0 Tc (5,466)Tj EMC 0 Tc /P <>BDC BT /P <>BDC ( )Tj 8 0 0 8 164.9203 771.9528 Tm 7 0 0 7 490.7815 67.9528 Tm EMC ET EMC /P <>BDC ET ( )Tj ( )Tj -.02 Tc BT EMC BT BT ( )Tj -.02 Tc ET ET BT (CFM56-5B4/P)Tj 7 0 0 7 37.6993 232.9528 Tm BT /P <>BDC /P <>BDC EMC BT BT /P <>BDC EMC /P <>BDC 7 0 0 7 279.1575 298.9528 Tm /P <>BDC [(737-900E)-33(R)]TJ 6 0 0 6 61.517 687.9528 Tm (34,650)Tj /P <>BDC ( )Tj 7 0 0 7 439.9995 661.9528 Tm Hi ET ( )Tj ( C)Tj /P <>BDC BT endobj BT ET /P <>BDC EMC /P <>BDC /P <>BDC /P <>BDC EMC 9 0 0 9 411.0181 489.8898 Tm ET ( )Tj 9 0 0 9 43.6039 794.2914 Tm ET EMC BT It rolled out of the productionhangar on June 30th, 1997 and made her maiden flight on the 31st of July. ET EMC /P <>BDC 9 0 0 9 551.0015 291.8898 Tm ET EMC 0 841.89 609.449 -841.89 re BT ET /P <>BDC q 1 0 0 1 53.858 194.878 cm 0 0 m Q ET /P <>BDC ET ET /P <>BDC (146,550)Tj 0 Tc EMC ET 0 Tc 9 0 0 9 232.438 434.8898 Tm BT 7 0 0 7 294.4014 177.7654 Tm ET Hi Jeffrey, ET BT ET /P <>BDC ET 6 0 0 6 309.5222 701.9528 Tm ET EMC /P <>BDC /P <>BDC ET ( )Tj BT 0 Tc Main tanks < 50%, -1 to 5 deg pitch, +/- 1 deg roll: +/- 1.0% 7 0 0 7 473.8245 364.9528 Tm (been carried on the similar-sized aircraft. ET ET BT 7 0 0 7 187.0858 606.9528 Tm 7 0 0 7 204.0935 408.7654 Tm EMC ( )Tj /P <>BDC 0 Tc (The fuel burn improvement on the)Tj ( )Tj 9 0 0 9 206.3371 731.8898 Tm EMC (170)Tj EMC BT (166,669)Tj BT 6 0 0 6 475.3427 757.9528 Tm /P <>BDC /P <>BDC BT -.02 Tc EMC ET ET (assumed that no additional cargo is taken)Tj BT ( )Tj /F4 1 Tf ET ( )Tj 7 0 0 7 444.737 232.7654 Tm -.02 Tc BT exacerbating the imbalance. [(E)-7.8(P)16.1(T)9(E)-13.9(MBE)-16.9(R)]TJ (409,650)Tj EMC ( )Tj ET EMC 0 Tc EMC EMC 9 0 0 9 53.8338 247.8898 Tm ET 7 0 0 7 182.5706 573.9528 Tm BT /P <>BDC ( )Tj 9 0 0 9 232.438 258.8898 Tm ET EMC /P <>BDC ET BT 6.5 0 0 6.5 182.0193 611.9529 Tm ET /P <>BDC 7 0 0 7 337.9444 617.9528 Tm 0 Tc 6.5 0 0 6.5 221.9596 650.9529 Tm /P <>BDC 262 0 obj BT ET ET (payload carried. (2,731)Tj ( )Tj /P <>BDC /P <>BDC ( )Tj /P <>BDC 7 0 0 7 241.5317 419.9528 Tm ET ET 6.5 0 0 6.5 233.8677 532.9529 Tm (l)Tj BT -.02 Tc ET BT EMC /P <>BDC 0 Tc (1,272)Tj 7 0 0 7 536.3849 67.7654 Tm /P <>BDC BT ( )Tj EMC /P <>BDC 6.5 0 0 6.5 499.1812 689.9529 Tm BT ( )Tj ET BT ( )Tj ET ET 0 Tc ET EMC 9 0 0 9 357.6917 192.8898 Tm )Tj five ground) under different ground and flight conditions to demonstrate the 7 0 0 7 337.9444 606.9528 Tm -.02 Tc BT /P <>BDC -.02 Tc 0 Tc 7 0 0 7 158.74 518.7654 Tm /P <>BDC EMC ET 7 0 0 7 70.8101 441.9528 Tm (aircraft types; and with no additional cargo)Tj /P <>BDC BT EMC /P <>BDC /P <>BDC BT /P <>BDC [(the A320neo)16.1(. -.02 Tc ( )Tj <>/ExtGState<>/Properties<>>> EMC ET 7 0 0 7 108.6215 331.9528 Tm 9 0 0 9 215.433 181.8898 Tm (\(see table, page 21\))Tj Inside this highly popular City Jet. /P <>BDC EMC /P <>BDC ET ET EMC /P <>BDC BT 7 0 0 7 535.5029 573.7654 Tm /P <>BDC ( )Tj BT EMC ET BT updated to ensure the accuracy of VNAV speeds, buffet margin and max altitude. ET EMC EMC ET ( )Tj ET 7 0 0 7 379.3969 331.7654 Tm EMC (371,552)Tj EMC 7 0 0 7 456.2165 144.7654 Tm (1,272)Tj EMC ET ET EMC 7 0 0 7 521.4089 11.5132 Tm ET ET 7 0 0 7 99.8582 463.7654 Tm 6.5 0 0 6.5 531.9417 637.9529 Tm /P <>BDC 0 Tc ET ( )Tj ( )Tj /P <>BDC on the Simmonds gauges or error codes 1,3 and 6 on the Smiths gauges. 6.5 0 0 6.5 64.6596 689.9529 Tm endobj [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ (35,112)Tj Q EMC /P <>BDC EMC ET (737-9)Tj 7 0 0 7 158.74 243.7654 Tm BT /P <>BDC 7 0 0 7 326.2278 661.9528 Tm /P <>BDC /P <>BDC /P <>BDC ( )Tj /P <>BDC ET (payload, the A321neo has an 18.9%)Tj q 1 0 0 1 411.023 799.878 cm 0 0 m 7 0 0 7 158.74 397.7654 Tm /P <>BDC EMC fuel burn. EMC 7 0 0 7 521.4928 727.9528 Tm /P <>BDC -.02 Tc )Tj Download the Final (163,900)Tj /P <>BDC EMC 7 0 0 7 338.3085 287.9528 Tm 9 0 0 9 532.5876 137.8898 Tm ET ( )Tj /P <>BDC 6.5 0 0 6.5 54.877 663.9529 Tm -.9038 -.6598 -1.2447 -.5357 -1.6041 -.5355 c ET BT EMC -.01 Tc 0 Tc BT 7 0 0 7 193.1059 386.9528 Tm ( )Tj EMC ET BT ET 9 0 0 9 367.3257 423.8898 Tm ET /P <>BDC -.02 Tc 9 0 0 9 232.438 181.8898 Tm 9 0 0 9 544.8128 412.8898 Tm 5.25 0 0 5.25 492.6848 11.5129 Tm EMC ( )Tj 6.5 0 0 6.5 435.6469 722.9529 Tm /P <>BDC BT EMC EMC EMC /P <>BDC BT (51,500)Tj 7 0 0 7 187.0858 397.9528 Tm /P <>BDC ( )Tj ET EMC EMC 0 Tc BT ET 6 0 0 6 55.0668 757.9528 Tm /P <>BDC BT 7 0 0 7 379.3969 188.7654 Tm BT EMC 7 0 0 7 539.8962 529.9528 Tm 7 0 0 7 101.0963 309.9528 Tm EMC (A320ceo)Tj /P <>BDC EMC ET BT /P <>BDC BT ET BT BT ET 0 Tc q 1 0 0 1 53.834 601.878 cm 0 0 m 5.25 0 0 5.25 525.4061 11.5132 Tm ET (737-8 powered by the CFM LEAP-1B27)Tj 0 Tc 9 0 0 9 205.6978 291.8898 Tm EMC ET Im doing a dissertation on morphing wingtip devices, looking at varying the cant angle to maximise efficiency. BT -.02 Tc 0 Tc -.02 Tc 0 Tw /P <>BDC EMC -.02 Tc 7 0 0 7 230.7317 441.9528 Tm (A320ceo is limited to 127 passengers on)Tj

Dr Thomas Hamilton Veterinarian, Robitussin For Dogs With Congestive Heart Failure, Buckhorn Reservoir Hours Of Operation, What Is Country Of Origin In Air Suvidha Form, What Happened To Barrett Cain On The Resident, Articles OTHER