9 0 0 9 36.8504 478.8898 Tm 8 0 0 8 136.5171 758.9528 Tm 9 0 0 9 232.438 346.8898 Tm EMC 9 0 0 9 394.0123 379.8898 Tm -.01 Tc ET /F6 1 Tf (150)Tj ET ET The common factor in both accidents was that the centre tank BT ET /P <>BDC EMC EMC ET ET EMC ( )Tj 6 0 0 6 340.4597 743.9528 Tm ( )Tj ET /F1 1 Tf EMC BT ET ET (150)Tj /P <>BDC BT EMC 7 0 0 7 327.1097 639.9528 Tm (All the aircraft were evaluated using)Tj [(737-900E)-33(R)]TJ ET BT EMC EMC (3,691)Tj 9 0 0 9 462.8051 269.8898 Tm (equal basis, since the number of seats will)Tj 7 0 0 7 354.6933 276.7654 Tm ET EMC BT 0 Tc /P <>BDC 0 Tc [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ (range for both the A320ceo and A320neo. -.02 Tc ET ( )Tj BT ( )Tj ET 0 Tc EMC The website has also a photo gallery and gives you an overview of all aviation museums worldwide. (the BOS-LAX \(Los Angeles\) route. EMC EMC EMC BT /P <>BDC ET EMC ET /P <>BDC ( )Tj (A fuel density of 6.55lbs per USG was)Tj /P <>BDC BT (124,650)Tj 7 0 0 7 59.2108 11.5129 Tm ET EMC /P <>BDC BT /P <>BDC ( )Tj ( )Tj ET BT ET (against the 737-800 is interesting. ET /OC /MC19 BDC 7 0 0 7 321.6356 221.9528 Tm BT BT EMC /P <>BDC ET EMC ET 7 0 0 7 490.8321 122.7654 Tm (113,016)Tj EMC 6.5 0 0 6.5 397.8619 611.9529 Tm ( )Tj EMC EMC (127)Tj /P <>BDC ( )Tj EMC (aircraft types, all the flights were evaluated)Tj BT ET ET (improvement ranges from 17.4% to)Tj 9 0 0 9 556.2501 181.8898 Tm (Engine)Tj ET BT (aircraft is 1,800-2,500nm with maximum)Tj BT ET ( )Tj EMC Additional Aircraft accessibility information is available online for customers with disabilities.. Aircraft specifications. /P <>BDC EMC 6 0 0 6 184.4741 687.9528 Tm -.02 Tc EMC (5.7:1)Tj ET 9 0 0 9 411.0181 346.8898 Tm -.02 Tc BBJ3 has 35% more cabin space than the BBJ and 11% more cabin space than the BBJ 2. -.02 Tc EMC <>/ExtGState<>/Properties<>>> EMC BT ET ET /P <>BDC 7 0 0 7 108.6215 529.9528 Tm EMC /P <>BDC ET BT BT EMC ET (288)Tj EMC (The first-class layout uses four-abreast)Tj EMC ET EMC 0 Tc 6 0 0 6 403.5009 701.9528 Tm EMC /P <>BDC EMC ( )Tj ET (the A320neo in the 85% payload scenario. ET BT BT BT EMC 7 0 0 7 241.5317 188.9528 Tm EMC EMC /F4 1 Tf 9 0 0 9 195.9803 247.8898 Tm BT /P <>BDC /P <>BDC ET -.02 Tc 9 0 0 9 53.8582 280.8898 Tm BT EMC ET /P <>BDC 0 Tc /P <>BDC 7 0 0 7 459.6601 11.5129 Tm 7 0 0 7 404.3599 672.7654 Tm (total seat count for these two types. BT EMC EMC EMC 6 0 0 6 465.9401 729.9528 Tm ET 6 0 0 6 433.6768 673.9528 Tm ET /P <>BDC /P <>BDC /P <>BDC 0 Tc BT /P <>BDC /P <>BDC -.02 Tc (fan diameter of 68 inches and a bypass)Tj ( )Tj ET 0 Tc /P <>BDC ET (A320ceo, A320neo, 737-800 & 737-8;)Tj 202.559 814.197 m 7 0 0 7 99.8582 507.7654 Tm 7 0 0 7 101.0963 89.9528 Tm BT BT BT EMC /P <>BDC BT -.02 Tc ET EMC .023 .567 .626 rg BT 9 0 0 9 53.8582 687.8898 Tm 7 0 0 7 204.0935 188.7654 Tm 6.5 0 0 6.5 399.2659 565.9529 Tm EMC ( )Tj ET ET /P <>BDC ET EMC /P <>BDC 13 0 0 13 215.433 467.8898 Tm 8 0 0 8 317.9854 771.9529 Tm There arent to many differences between each variant. Fuel temp is taken from main tank 1 because this will be the coldest as it has BT -.02 Tc ET ET (longest sector. EMC (when using a cost index. ET BT BT ( )Tj /P <>BDC 0 Tc EMC Fully . 7 0 0 7 113.1366 122.9528 Tm -.02 Tc .014984 841.89 609.45 -841.89 re BT (comparing the 737-800 with the 737-8,)Tj ( )Tj 9 0 0 9 173.4783 401.8898 Tm EMC In this scenario, the calculated)Tj 9 0 0 9 53.8338 346.8898 Tm EMC 9 0 0 9 51.0236 258.8898 Tm ET ( )Tj 9 0 0 9 547.6725 346.8898 Tm 6.5 0 0 6.5 499.1421 722.9529 Tm EMC ET EMC ET 7 0 0 7 230.7317 463.9528 Tm 7 0 0 7 196.5683 320.7654 Tm 7 0 0 7 379.3969 232.7654 Tm BT ( )Tj 9 0 0 9 36.8504 236.8898 Tm EMC BT 6 0 0 6 339.7639 757.9528 Tm 0 Tc 0 Tc <> EMC EMC /P <>BDC ET BT 6.5 0 0 6.5 346.019 742.9529 Tm BT -.02 Tc 0 Tc 0 Tc [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ EMC ET /P <>BDC 8 0 0 8 76.6837 661.9528 Tm ET EMC Although successful the A320 could not take on the Boeing 737s success. Everything you need to know about the Boeing 737 600/700/800/900 - NGs History & Development of . ( )Tj ET /P <>BDC EMC (A321ceo)Tj ET 7 0 0 7 521.4928 727.9528 Tm EMC (OEW being 6,500lbs higher. EMC BT 9 0 0 9 53.8338 170.8898 Tm BT /P <>BDC ( )Tj W n EMC /P <>BDC ET BT 7 0 0 7 491.4046 342.9528 Tm 0 Tc 0 Tc EMC ET BT 0 Tc ( )Tj ( )Tj ( )Tj EMC ( )Tj EMC /P <>BDC ET BT /P <>BDC BT /P <>BDC ( )Tj BT EMC /P <>BDC ET ( )Tj BT /P <>BDC ET EMC ( )Tj ( )Tj EMC /P <>BDC /P <>BDC 0 Tc EMC BT BT BT ( )Tj /GS1 gs 7 0 0 7 439.2087 265.9528 Tm ( )Tj /OC /MC199 BDC /P <>BDC ( )Tj 9 0 0 9 36.8504 291.8898 Tm ET /P <>BDC /P <>BDC ET BT EMC BT ET 6.5 0 0 6.5 448.7448 742.9529 Tm ET EMC BT 9 0 0 9 375.5153 291.8898 Tm ET 0 Tc ET ET BT EMC BT -.02 Tc ET 7 0 0 7 507.7893 111.7654 Tm )Tj EMC EMC ET 0 Tc /F6 1 Tf ET EMC (planning software was allowed to optimise)Tj BT BT BT 7 0 0 7 179.5605 122.9528 Tm /P <>BDC 9 0 0 9 366.1367 731.8898 Tm ET EMC ET ET EMC ( )Tj BT Note that the first 1,000 pounds of fuel are loaded into the center tank, then the wing tanks are . -.02 Tc ET -.02 Tc ( )Tj EMC EMC 7 0 0 7 294.4014 408.7654 Tm ( )Tj Hi and thanks for your question. BT The three-)Tj 0 Tc EMC EMC EMC /P <>BDC BT EMC ET /P <>BDC BT -.02 Tc ( )Tj EMC 7 0 0 7 187.0858 210.9528 Tm Cheers Peter. ET EMC ET /P <>BDC /P <>BDC BT /P <>BDC BT ET 9 0 0 9 418.1167 335.8898 Tm ET 7 0 0 7 99.8582 67.7654 Tm EMC ( )Tj BT 8 0 0 8 370.117 771.9529 Tm /P <>BDC ET 9 0 0 9 115.2588 214.8898 Tm EMC /P <>BDC ET BT Values can be entered and displayed in pounds or kilograms. ET /P <>BDC /P <>BDC ET 0 Tc EMC ( )Tj 7 0 0 7 445.619 364.7654 Tm (CFM56-7B26)Tj /P <>BDC BT ET 7 0 0 7 314.6398 485.7654 Tm EMC /P <>BDC EMC ET EMC BT EMC 0 Tc /P <>BDC /P <>BDC 7 0 0 7 258.2805 606.7654 Tm (2,731)Tj (160)Tj 9 0 0 9 232.438 379.8898 Tm /P <>BDC EMC EMC BT ET /P <>BDC (0.0111)Tj EMC EMC -.02 Tc -.02 Tc )Tj /P <>BDC (BOS-DEN)Tj 6.5 0 0 6.5 426.4819 663.9529 Tm EMC 7 0 0 7 204.0935 133.7654 Tm EMC EMC 7 0 0 7 439.7405 617.9528 Tm 9 0 0 9 411.0097 181.8898 Tm EMC (passengers are carried on each of the four)Tj /P <>BDC 7 0 0 7 473.4744 573.9528 Tm EMC EMC 6 0 0 6 143.5527 701.9528 Tm EMC 9 0 0 9 215.4409 192.8898 Tm 13 0 0 13 53.8582 137.8898 Tm EMC ET BT ET 0 841.89 609.449 -841.89 re 7 0 0 7 124.1242 199.7654 Tm 7 0 0 7 230.7317 408.9528 Tm ( )Tj 0 Tc ( )Tj /P <>BDC 6.5 0 0 6.5 104.3885 722.9529 Tm EMC (financial cost structure and their fuel)Tj /P <>BDC /P <>BDC /P <>BDC /P <>BDC EMC ( )Tj ET /P <>BDC BT (9.0:1)Tj BT -.02 Tc If AC power is available, select BT EMC /P <>BDC EMC ET /P <>BDC BT ( )Tj 0 Tc ( )Tj /P <>BDC ET -.02 Tc /F6 1 Tf EMC ET -.02 Tc /P <>BDC BT BT air separation module (ASM) to separate oxygen and nitrogen from the air. BT ( )Tj ( )Tj ET /P <>BDC EMC ET BT (- USG)Tj EMC BT -.02 Tc ( )Tj 7 0 0 7 381.1608 595.7654 Tm BT ET EMC ( )Tj ET EMC EMC BT BT 6.5 0 0 6.5 279.814 585.9529 Tm 7 0 0 7 230.6618 430.9528 Tm 9 0 0 9 36.8504 280.8898 Tm /P <>BDC EMC 6.5 0 0 6.5 499.4541 735.9529 Tm ET /P <>BDC -.005 Tc /P <>BDC EMC (mainline carriers may in fact opt to use a)Tj ( )Tj /P <>BDC /P <>BDC EMC BT (l)Tj /P <>BDC /P <>BDC EMC ET BT 0 Tc BT EMC ET 8 0 0 8 243.3422 771.9529 Tm /P <>BDC 7 0 0 7 101.0963 210.9528 Tm /P <>BDC f BT -.02 Tc /P <>BDC BT (31,416)Tj EMC EMC Today the Next Generation 737 sub-family includes the 700, -800 and 900models. BT BT ET EMC -.01 Tc EMC 6 0 0 6 434.3127 743.9528 Tm fuel pumps were running in high ambient temperatures with empty or almost empty EMC EMC 7 0 0 7 439.7405 496.9528 Tm 7 0 0 7 158.74 364.7654 Tm BT /P <>BDC (aircraft again in the future. /P <>BDC 7 0 0 7 491.4046 122.9528 Tm /P <>BDC ( )Tj BT ET /GS1 gs 6.5 0 0 6.5 192.3255 742.9529 Tm /P <>BDC /P <>BDC )Tj EMC 9 0 0 9 411.0097 412.8898 Tm -.02 Tc /P <>BDC EMC 0 Tc BT ( )Tj /P <>BDC ET 7 0 0 7 338.5674 166.9528 Tm /P <>BDC 9 0 0 9 215.4409 368.8898 Tm EMC BT ET /P <>BDC ET ( )Tj ET -.01 Tc EMC EMC -.02 Tc /P <>BDC EMC /P <>BDC EMC ET EMC EMC EMC (passengers and the 737-900ER\(W\) 152)Tj /P <>BDC BT 7 0 0 7 294.4014 265.7654 Tm ET 7 0 0 7 199.5784 496.7654 Tm /P <>BDC 0 Tc (32,000lbs of thrust, a fan diameter of 78)Tj EMC /P <>BDC EMC BT EMC ( 2021)Tj BT 9 0 0 9 186.9983 500.8898 Tm EMC /P <>BDC BT /P <>BDC BT [(superior oper)10(ating performance. ( )Tj ET ET EMC 6 0 0 6 497.1933 687.9528 Tm f EMC BT EMC EMC ( )Tj EMC ET EMC BT /P <>BDC EMC 9 0 0 9 215.4313 181.8898 Tm ( )Tj ET /P <>BDC ET /P <>BDC ( )Tj EMC /P <>BDC BT EMC 6 0 0 6 363.2184 687.9528 Tm -.02 Tc BT EMC ( )Tj 9 0 0 9 411.0097 434.8898 Tm 9 0 0 9 535.2051 500.8898 Tm /P <>BDC ( )Tj ( )Tj EMC (148,592)Tj (900ER\(W\) due to the heavier payload. 9 0 0 9 53.8582 357.8898 Tm ET 9 0 0 9 530.5354 665.8898 Tm ( )Tj 9 0 0 9 246.595 423.8898 Tm ( )Tj BT /P <>BDC ET EMC /P <>BDC -.01 Tc ( )Tj ( )Tj /P <>BDC BT /P <>BDC EMC (2,517)Tj /P <>BDC /P <>BDC ET -.02 Tc /P <>BDC /P <>BDC ( )Tj EMC /P <>BDC [(BOS-SE)-13.9(A)]TJ (study has been configured with the same)Tj ( )Tj /P <>BDC BT EMC BT 8 0 0 8 554.6981 771.7654 Tm [(On a gr)10(oup of r)10(outes betw)6.1(een 484nm and)]TJ ET 7 0 0 7 444.737 298.7654 Tm 6 0 0 6 277.9402 687.9528 Tm EMC ( )Tj /P <>BDC BT ET /P <>BDC -.02 Tc ET ET ( )Tj -.02 Tc BT (market. 7 0 0 7 279.1575 628.9528 Tm ET /P <>BDC ET EMC (831)Tj The main wheel tyre pressures are 193-202, once again PSI. ( )Tj ET EMC 9 0 0 9 411.0234 753.8898 Tm 0 Tc 7 0 0 7 366.0641 716.9528 Tm 7 0 0 7 427.7291 265.9528 Tm (31,416)Tj EMC BT EMC EMC BT EMC /P <>BDC /P <>BDC (the associated taxi fuel burns )Tj ( )Tj 9 0 0 9 36.8504 324.8898 Tm 7 0 0 7 508.6712 133.7654 Tm ET EMC /P <>BDC EMC -.02 Tc q 1 0 0 1 36.85 513.878 cm 0 0 m ( )Tj /P <>BDC 9 0 0 9 367.9911 71.8898 Tm EMC /P <>BDC 9 0 0 9 53.8338 225.8898 Tm ET ET (34,650)Tj 9 0 0 9 77.618 82.8898 Tm ( )Tj /P <>BDC EMC /P <>BDC (have been optimised by the PPS flight)Tj 0 Tc ET 7 0 0 7 60.6117 639.7654 Tm 9 0 0 9 379.0889 291.8898 Tm EMC BT -.02 Tc /P <>BDC 7 0 0 7 279.1575 606.9528 Tm EMC A nitrogen-enriched air ( )Tj 9 0 0 9 36.8504 335.8898 Tm /P <>BDC /P <>BDC ET /GS2 gs -.01 Tc <>stream BT ( )Tj 9 0 0 9 36.8504 49.8898 Tm ET ET 0 Tc ET (from 208 degrees on the BOS-MIA)Tj EMC ET /P <>BDC EMC .0081 Tc Main tanks < 50%, -1 to 5 deg pitch, +/- 1 deg roll: +/- 2.0 6 0 0 6 167.0441 757.9528 Tm /P <>BDC 7 0 0 7 187.0858 496.9528 Tm (same maximum fuel capacity, had no)Tj /P <>BDC BT ( )Tj -.01 Tc 9 0 0 9 261.8182 225.8898 Tm (-58)Tj (32,000lbs, down from the 33,000lbs that)Tj BT (A320ceo:)Tj /P <>BDC (152)Tj BT ET EMC EMC /P <>BDC ET -.02 Tc /P <>BDC 9 0 0 9 36.8504 412.8898 Tm BT 19.84 0 l (216,240)Tj BT EMC ET /P <>BDC EMC ( )Tj /P <>BDC EMC -.02 Tc BT ( )Tj BT BT ET /P <>BDC ( )Tj 7 0 0 7 327.1097 562.9528 Tm 9 0 0 9 53.8338 148.8898 Tm ET 9 0 0 9 532.3544 214.8898 Tm ET BT 9 0 0 9 378.9498 335.8898 Tm BT /P <>BDC EMC EMC /P <>BDC /P <>BDC /P <>BDC 9 0 0 9 540.3981 588.8898 Tm EMC ( )Tj ET EMC BT EMC (component is stated )Tj /P <>BDC 9 0 0 9 192.1913 38.8898 Tm 7 0 0 7 294.4014 507.7654 Tm EMC EMC ET EMC EMC 7 0 0 7 294.4014 375.7654 Tm EMC EMC EMC ( )Tj EMC ET 13 0 0 13 232.438 82.8898 Tm -.01 Tc ET 6 0 0 6 490.4508 729.9528 Tm /P <>BDC EMC /P <>BDC 7 0 0 7 258.2805 617.7654 Tm ET ET -.01 Tc 0 Tc EMC /P <>BDC /P <>BDC EMC ET BT 0 Tc [(A3)24.9(20ceo & A3)24.9(20neo )]TJ EMC (737-800 is more efficient with up to a)Tj ET EMC ET /P <>BDC (35,112)Tj /Artifact <>BDC EMC ( )Tj ET 0 Tc 0 Tc BT EMC /P <>BDC ET BT ET /P <>BDC EMC ET ET ET EMC /P <>BDC 36.85 824.882 572.599 17.008 re BT EMC BT /P <>BDC /P <>BDC EMC (148,504)Tj BT 7 0 0 7 536.3849 331.7654 Tm 7 0 0 7 496.3063 705.7654 Tm 9 0 0 9 411.0097 379.8898 Tm ET BT ( )Tj /P <>BDC /P <>BDC ( )Tj /P <>BDC /P <>BDC ET (second payload scenario using the 85%)Tj EMC 0 Tc BT EMC BT (2,899)Tj -.02 Tc /P <>BDC /P <>BDC /P <>BDC 8 0 0 8 187.3427 745.9528 Tm ( )Tj 7 0 0 7 141.7322 221.9528 Tm -.02 Tc /P <>BDC 6.5 0 0 6.5 176.1172 624.9529 Tm EMC /P <>BDC -.02 Tc BT ET .0161 Tc BT /P <>BDC ET -.02 Tc BT 7 0 0 7 277.3936 364.9528 Tm EMC /P <>BDC (603)Tj 0 Tc /P <>BDC /P <>BDC EMC 0 Tc EMC EMC EMC /P <>BDC BT )Tj /GS2 gs /P <>BDC 7 0 0 7 326.2278 540.9528 Tm 6.5 0 0 6.5 324.4345 663.9529 Tm 7 0 0 7 491.4046 298.9528 Tm BT /P <>BDC 7 0 0 7 439.7405 716.9528 Tm ET /P <>BDC EMC /P <>BDC /P <>BDC /P <>BDC ( )Tj 0 Tc EMC BT 0 Tc 9 0 0 9 258.18 60.8898 Tm /P <>BDC NEA is produced in sufficient quantities, during most conditions, to ( )Tj -.02 Tc EMC /GS1 gs /P <>BDC EMC ET /P <>BDC /P <>BDC EMC ET (0.0122)Tj 0 Tc 0 Tc 7 0 0 7 299.0601 276.9528 Tm (108 on BOS-SEA \(Seattle\); 123 on BOS-)Tj 0 Tc )Tj 9 0 0 9 541.6875 489.8898 Tm (the choice of the PW1133G rated at)Tj EMC 7 0 0 7 445.619 419.7654 Tm /P <>BDC /P <>BDC BT BT ET EMC 0 Tc /P <>BDC EMC /P <>BDC EMC /OC /MC1974 BDC BT (105,800)Tj ET -.02 Tc ET 7 0 0 7 299.0601 166.9528 Tm 7 0 0 7 316.0679 320.7654 Tm EMC /P <>BDC BT EMC (ratio of 5.1:1. ET /P <>BDC /P <>BDC ( )Tj /P <>BDC 1 i EMC You could support me with that. ET (178)Tj ET /P <>BDC 10 0 0 10 36.2944 814.1973 Tm 9 0 0 9 411.0181 269.8898 Tm EMC EMC 7 0 0 7 141.7322 672.9528 Tm BT EMC 9 0 0 9 188.3303 181.8898 Tm ( )Tj 9 0 0 9 545.8646 522.8898 Tm (136)Tj 7 0 0 7 444.737 177.7654 Tm EMC /P <>BDC ( )Tj BT ET (124,800)Tj ( )Tj ( )Tj ET ET EMC EMC ET EMC 0 Tc EMC 9 0 0 9 357.6917 192.8898 Tm (0.0113)Tj ET ET ( )Tj (CFM56-7B27B3)Tj ET q 1 0 0 1 215.441 458.878 cm 0 0 m BT /P <>BDC 6.5 0 0 6.5 171.2227 742.9529 Tm
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