/P <>BDC ( )Tj 0 Tc /F4 1 Tf BT 9 0 0 9 53.8338 93.8898 Tm (sectors where a 170-passenger payload is)Tj BT ET EMC 9 0 0 9 166.1068 313.8898 Tm 6 0 0 6 357.8844 673.9528 Tm 9 0 0 9 372.0688 324.8898 Tm 7 0 0 7 459.6601 11.5129 Tm BT ET BT BT (737-800W)Tj ( )Tj ET 9 0 0 9 532.5876 137.8898 Tm EMC EMC ( )Tj 7 0 0 7 344.1175 573.7654 Tm endstream /P <>BDC (156,500)Tj /P <>BDC 7 0 0 7 314.6398 672.7654 Tm EMC /P <>BDC -.02 Tc ET ET ( )Tj /P <>BDC 7 0 0 7 141.7322 496.9528 Tm 9 0 0 9 215.433 236.8898 Tm [(v)21(ariant)]TJ 10 0 0 10 407.56 814.1973 Tm /P <>BDC EMC EMC ET (sectors, particularly the shorter ones,)Tj 13 0 0 13 340.4557 467.8898 Tm (It was assumed that all flights would)Tj /P <>BDC EMC EMC /P <>BDC 9 0 0 9 215.4409 38.8898 Tm ET EMC BT EMC -.02 Tc ET ET ( )Tj 7 0 0 7 82.8504 221.9528 Tm 0 Tc ET ET EMC BT ET (1A26-powered aircraft that is used in this)Tj (difference to an average of 2.1% over the)Tj 6.5 0 0 6.5 296.4841 689.9529 Tm BT 7 0 0 7 99.8582 309.7654 Tm EMC ET EMC 7 0 0 7 71.6694 738.9528 Tm ET EMC BT EMC ET BT EMC /P <>BDC BT /P <>BDC -.02 Tc BT 7 0 0 7 337.4684 738.9528 Tm /GS1 gs 6 0 0 6 236.6735 673.9528 Tm (2,731)Tj ET /P <>BDC 7 0 0 7 99.8582 518.7654 Tm 0 Tc 7 0 0 7 230.7317 188.9528 Tm BT BT ( )Tj /P <>BDC 7 0 0 7 491.392 573.9528 Tm 7 0 0 7 380.2788 518.7654 Tm -.02 Tc BT /P <>BDC 7 0 0 7 37.0536 485.9528 Tm -.02 Tc W n BT [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ ( )Tj /P <>BDC EMC 10 0 0 10 137.0323 771.9528 Tm BT EMC /P <>BDC BT EMC BT BT ( )Tj ET /P <>BDC /P <>BDC ( )Tj 7 0 0 7 554.7883 210.7654 Tm BT /P <>BDC 13 0 0 13 118.3688 390.8898 Tm 9 0 0 9 190.8846 379.8898 Tm (ratio of 11.0:1. ( )Tj ( )Tj ET 7 0 0 7 338.3085 320.9528 Tm EMC (737-8)Tj Just wondering, where did you get the information about what specific aluminium alloys are used on different parts of the aircraft? BT BT EMC ( )Tj EMC BT EMC ET 7 0 0 7 354.7351 694.7654 Tm 7 0 0 7 440.6226 683.9528 Tm In the cargo configuration, The 737-700C can carry up to 18,780 kg (41,420 pounds) of cargo on eight . Since development and production Boeing has built 10,574 737-800s. 0 Tc ( )Tj BT ET A nitrogen-enriched air 6.5 0 0 6.5 191.63 624.9529 Tm ( )Tj 7 0 0 7 518.4953 144.9528 Tm BT (1,272)Tj ET EMC (capacity of 6,353USG, giving it a range of)Tj /P <>BDC [(CFM L)17.1(E)-8.1(AP-1B27)]TJ (737-900ER\(W\) rather than the 737-900,)Tj ET EMC EMC /P <>BDC /P <>BDC (989)Tj ET 0 Tc 0 Tc EMC 7 0 0 7 476.1204 694.9528 Tm BT ET ( )Tj 6 0 0 6 381.7993 715.9528 Tm ET BT EMC ET BT 7 0 0 7 403.478 485.7654 Tm /P <>BDC EMC /F6 1 Tf EMC EMC (passenger load factor based on each types)Tj (class cabin configuration used in this study)Tj /F6 1 Tf q 1 0 0 1 505.328 82.247 cm 0 0 m EMC EMC BT (aircraft types; and with no additional cargo)Tj ET 7 0 0 7 316.0679 133.7654 Tm /P <>BDC 9 0 0 9 232.438 302.8898 Tm (176)Tj EMC 9 0 0 9 215.4313 335.8898 Tm 9 0 0 9 36.8504 434.8898 Tm EMC In this scenario, the calculated)Tj 9 0 0 9 53.8582 412.8898 Tm BT 7 0 0 7 456.4753 738.7654 Tm 6.5 0 0 6.5 477.8064 676.9529 Tm 9 0 0 9 534.0193 390.8898 Tm /P <>BDC EMC ( )Tj /P <>BDC ET /P <>BDC 6.5 0 0 6.5 54.877 650.9529 Tm EMC BT EMC 0 841.89 609.449 -841.89 re 9 0 0 9 532.3544 214.8898 Tm BT BT BT BT ( )Tj EMC EMC ( )Tj ET 0 Tc /P <>BDC (39,270)Tj (assume that the optimum flight level could)Tj 9 0 0 9 51.0236 445.8898 Tm /P <>BDC ( )Tj ( )Tj ET 7 0 0 7 354.6933 496.7654 Tm ET (10)Tj ( )Tj EMC BT EMC .151 .147 .15 rg (. -.02 Tc BT -.02 Tc [(BOS-D)17.1(T)-11(W)]TJ BT BT 0 Tc /P <>BDC [(CFM L)17.1(E)-8.1(AP-1B27)]TJ 7 0 0 7 297.632 606.9528 Tm EMC EMC ( )Tj ET /P <>BDC BT 7 0 0 7 199.5784 595.7654 Tm EMC EMC ET EMC BT ET EMC ( )Tj 9 0 0 9 53.8582 203.8898 Tm -.02 Tc /P <>BDC 0 Tc /P <>BDC 7 0 0 7 381.1608 562.7654 Tm 6.5 0 0 6.5 64.6596 558.9529 Tm EMC 13 0 0 13 186.9936 588.8898 Tm ET (39,270lbs)Tj EMC ET ( )Tj 9 0 0 9 394.0123 225.8898 Tm BT ET /P <>BDC BT (31,416)Tj BT (0.0119)Tj And I hope I will get some good stuff to post it to you. ()Tj EMC BT BT /P <>BDC EMC BT /P <>BDC EMC /P <>BDC ( )Tj ET /P <>BDC BT 6.5 0 0 6.5 435.6469 722.9529 Tm BT EMC EMC ET /P <>BDC EMC EMC 7 0 0 7 475.2383 683.9528 Tm EMC -.02 Tc EMC 0 Tc ET ET 9 0 0 9 394.0157 159.8898 Tm /P <>BDC ET In which manual could you find the cross-sectional dimensions of the wing spars and stabilizer (737-300) EMC EMC (The main operating parameters are: )Tj EMC 9 0 0 9 211.0829 379.8898 Tm BT ( )Tj BT (403)Tj /GS1 gs EMC ET EMC ET EMC EMC ET BT ET (for the 737-900ER\(W\) and 737-9. /P <>BDC BT EMC 9 0 0 9 36.8583 445.8898 Tm 0 Tc /P <>BDC EMC 7 0 0 7 277.3936 166.9528 Tm ( )Tj BT 9 0 0 9 215.4313 203.8898 Tm ET /P <>BDC 8 0 0 8 243.3422 771.9529 Tm /P <>BDC EMC EMC BT ET ET EMC /P <>BDC BT -.02 Tc /P <>BDC (-58)Tj 7 0 0 7 54.7071 364.7654 Tm ET (using the same payload and seat)Tj ( )Tj (408)Tj ( )Tj /P <>BDC /P <>BDC (12,549)Tj (2,060)Tj 7 0 0 7 429.157 617.9528 Tm ( )Tj EMC [(the A320neo)16.1(. ( )Tj 7 0 0 7 179.5605 221.9528 Tm 8 0 0 8 256.0704 577.9528 Tm 7 0 0 7 380.2788 606.7654 Tm ET BT 6jf/+6*Pe/[LeaVSjtLZ6*vXQ9b;(P+L(vV^V;,]2^JsGHqp]]&MDK1B39?ZVM,9P=2/ Zz>\\.. 8 0 0 8 38.4438 619.9528 Tm ET 9 0 0 9 366.4417 533.8898 Tm EMC BT ET EMC 9 0 0 9 53.8578 478.8898 Tm 0 Tc EMC EMC /P <>BDC /P <>BDC BT 6.5 0 0 6.5 191.7701 558.9529 Tm EMC 63 0 obj ET 7 0 0 7 337.7614 100.7654 Tm BT BT ET /P <>BDC EMC EMC ET BT /P <>BDC /P <>BDC BT 9 0 0 9 79.8339 456.8898 Tm ET ( )Tj /F1 1 Tf (0.0160)Tj 8 0 0 8 264.6706 703.9528 Tm ET ( )Tj 7 0 0 7 279.1575 111.9528 Tm ET 7 0 0 7 230.7317 606.9528 Tm EMC .014984 841.89 609.45 -841.89 re 9 0 0 9 51.0236 379.8898 Tm ET EMC BT -.02 Tc BT /P <>BDC BT EMC EMC BT BT /P <>BDC 7 0 0 7 299.0601 166.9528 Tm EMC It rolled out of the productionhangar on June 30th, 1997 and made her maiden flight on the 31st of July. -.02 Tc /P <>BDC /GS1 gs EMC ( )Tj (136)Tj BT /P <>BDC /P <>BDC ( )Tj ET BT EMC /P <>BDC 9 0 0 9 68.0314 126.8898 Tm /P <>BDC EMC 6 0 0 6 138.6506 757.9528 Tm ET ET ET 9 0 0 9 546.5092 577.8898 Tm ( )Tj ( )Tj 9 0 0 9 548.2598 489.8898 Tm /GS2 gs ET ET 0 Tc 7 0 0 7 230.7317 221.9528 Tm -.01 Tc BT EMC EMC ( )Tj EMC ET (BOS-LAX due to the strong headwind)Tj EMC /P <>BDC EMC ET 6.5 0 0 6.5 346.1424 545.9529 Tm /P <>BDC EMC /P <>BDC EMC EMC ET ET (20)Tj 7 0 0 7 554.7883 584.7654 Tm 6 0 0 6 309.4742 687.9528 Tm 7 0 0 7 445.7203 11.5129 Tm 7 0 0 7 404.101 100.7654 Tm 9 0 0 9 394.0315 335.8898 Tm /P <>BDC ( )Tj ET ET ( )Tj /P <>BDC BT ET 0 Tc BT 7 0 0 7 519.3773 364.9528 Tm EMC 6.5 0 0 6.5 549.8557 598.9529 Tm /P <>BDC BT BT ( )Tj BT ET 7 0 0 7 82.2047 485.9528 Tm ET EMC 9 0 0 9 411.0097 269.8898 Tm ET -.02 Tc ( )Tj EMC ET BT BT EMC BT BT 9 0 0 9 36.8504 148.8898 Tm BT /P <>BDC -.02 Tc /P <>BDC ET 7 0 0 7 258.2805 628.7654 Tm BT EMC /P <>BDC BT (directly compare the fuel burn and)Tj -4.5143 -2.2339 -4.3751 -1.5784 -4.0786 -1.0086 c ET -.02 Tc EMC ( )Tj -.02 Tc 7 0 0 7 241.2727 166.9528 Tm ET ( )Tj -.01 Tc EMC ( )Tj 9 0 0 9 215.4409 346.8898 Tm /P <>BDC ET BT 8 0 0 8 124.845 577.9528 Tm ET EMC ( )Tj 7 0 0 7 37.0536 617.9528 Tm ( )Tj /P <>BDC BT (page 23\))Tj BT ET -.02 Tc ET ( )Tj ET ET ET -.3738 -6.1596 -.9177 -6.351 -1.6458 -6.3504 c 0 Tc -.02 Tc /P <>BDC 7 0 0 7 279.1575 342.9528 Tm ET /F4 1 Tf ET )Tj -.02 Tc ET /P <>BDC 7 0 0 7 508.4124 320.7654 Tm 7 0 0 7 247.7395 375.7654 Tm BT /P <>BDC BT ET /P <>BDC 7 0 0 7 554.7883 375.7654 Tm 13 0 0 13 532.9001 786.8898 Tm 0 Tc ET /P <>BDC BT 9 0 0 9 215.433 170.8898 Tm 0 Tc (financial cost structure and their fuel)Tj 8 0 0 8 531.1443 775.8898 Tm EMC 7 0 0 7 554.7883 243.7654 Tm EMC /P <>BDC ( )Tj 9 0 0 9 551.0557 467.8898 Tm EMC 7 0 0 7 141.7322 144.9528 Tm /P <>BDC /P <>BDC ET (A321neo)Tj EMC BT ET 7 0 0 7 250.5326 100.7654 Tm (improved engine efficiency and offer)Tj EMC /P <>BDC /F1 1 Tf -.02 Tc /P <>BDC BT EMC EMC EMC /F4 1 Tf 6 0 0 6 339.7639 757.9528 Tm BT Wing provisioning for the 737-800 adds approx. .559 .331 .619 rg 7 0 0 7 230.7317 683.9528 Tm BT BT The New Midsized Airplane. EMC 7 0 0 7 363.2711 507.9528 Tm /P <>BDC ET 9 0 0 9 209.838 60.8898 Tm BT ET BT /P <>BDC /P <>BDC 0 Tc )Tj (A320ceo)Tj -.02 Tc /P <>BDC 6 0 0 6 451.7374 673.9528 Tm 7 0 0 7 95.225 11.5132 Tm /P <>BDC ET (5.1:1)Tj 6.5 0 0 6.5 280.3794 722.9529 Tm BT EMC /P <>BDC BT EMC EMC The NG has 6 dripsticks in each wing tank and 4 in the centre /P <>BDC ET ET EMC EMC EMC ET EMC EMC (CFM56-5B4/P)Tj EMC 7 0 0 7 277.3936 144.9528 Tm (follow in their footsteps, having already)Tj BT EMC BT 7 0 0 7 297.632 518.9528 Tm (31,416)Tj EMC ET /P <>BDC ( )Tj ( )Tj .151 .147 .15 rg EMC ET EMC 6 0 0 6 286.5632 771.9528 Tm ET ET 7 0 0 7 439.2087 221.9528 Tm EMC W n BT EMC 0 Tc 6.5 0 0 6.5 335.5237 532.9529 Tm 7 0 0 7 492.5963 738.7654 Tm /P <>BDC (and in fuel burn per ASM. /GS2 gs BT ET EMC ET BT EMC /P <>BDC EMC 9 0 0 9 215.4409 357.8898 Tm <>stream /P <>BDC (on these flights. 7 0 0 7 404.101 309.7654 Tm BT 7 0 0 7 141.7322 243.9528 Tm 0 Tc /P <>BDC /P <>BDC /F4 1 Tf BT BT /P <>BDC .151 .147 .15 rg ET BT ET )Tj 0 Tc 0 Tc ET ET ET ( )Tj /F4 1 Tf 0 Tc . ET EMC EMC 6 0 0 6 277.6461 743.9528 Tm BT Additionally, below 10,000 feet it should not exceed 250 knots. BT EMC ET ( )Tj 7 0 0 7 386.4701 89.9528 Tm /P <>BDC 9 0 0 9 530.1182 346.8898 Tm ( )Tj /P <>BDC ( )Tj 0 Tc ET /P <>BDC BT BT 7 0 0 7 362.3891 331.9528 Tm /P <>BDC 0 Tc EMC 9 0 0 9 394.0315 192.8898 Tm ET ET /P <>BDC /P <>BDC 7 0 0 7 320.7537 111.9528 Tm ( )Tj EMC ET 9 0 0 9 383.0289 544.8898 Tm (737-800W)Tj 7 0 0 7 338.6433 122.7654 Tm ET (152)Tj /P <>BDC BT ( )Tj ( )Tj EMC 6 0 0 6 527.3389 687.9528 Tm ET ET ( )Tj ET 1 i BT EMC ( )Tj ET EMC EMC ET ET -.02 Tc BT BT ( )Tj /P <>BDC (The A321neo is offered to airlines with)Tj 9 0 0 9 371.4208 522.8898 Tm EMC /P <>BDC (A320ceo)Tj /P <>BDC EMC 9 0 0 9 207.0841 203.8898 Tm BT ET /P <>BDC 9 0 0 9 532.082 247.8898 Tm BT EMC ET EMC 0 841.89 609.449 -841.89 re EMC 7 0 0 7 363.2711 232.9528 Tm ( )Tj /P <>BDC (145,505lbs, and a fuel capacity of 6,303)Tj /TT2 1 Tf 6.5 0 0 6.5 176.1172 558.9529 Tm EMC 7 0 0 7 108.6215 727.9528 Tm 7 0 0 7 364.1531 133.9528 Tm ET EMC BT (0.0113)Tj /P <>BDC (11.0:1)Tj 9 0 0 9 229.6141 214.8898 Tm ( )Tj ET EMC ( )Tj BT 7 0 0 7 204.0935 628.7654 Tm BT -.02 Tc ET EMC ET BT refuelling panel to AUX TANKS. /P <>BDC /P <>BDC ET 9 0 0 9 394.0157 291.8898 Tm EMC EMC /P <>BDC ET (seat capacity over the NG series. /GS1 gs /P <>BDC [(AS)29(M)]TJ ET ET /P <>BDC (-61)Tj ET BT /P <>BDC (0.0194)Tj 8 0 0 8 259.5105 675.9528 Tm BT BT 7 0 0 7 82.8504 188.9528 Tm 7 0 0 7 258.2805 177.7654 Tm 6.5 0 0 6.5 448.257 598.9529 Tm /P <>BDC 9 0 0 9 232.4217 368.8898 Tm ET BT BT BT .964 .834 .406 rg ET 6.5 0 0 6.5 54.877 637.9529 Tm ET 9 0 0 9 232.4408 698.8898 Tm 6.5 0 0 6.5 222.7786 663.9529 Tm EMC - Modern Airliners. (800 is not as large as the difference)Tj EMC /P <>BDC /P <>BDC EMC /P <>BDC -2.4549 -3.9026 l BT ET ET 6.5 0 0 6.5 244.2974 545.9529 Tm f /P <>BDC (7,379)Tj 0 Tc EMC 9 0 0 9 53.8338 60.8898 Tm 7 0 0 7 457.0984 529.7654 Tm ET 7 0 0 7 456.7412 661.7654 Tm 7 0 0 7 355.5753 562.7654 Tm BT 7 0 0 7 230.7317 727.9528 Tm /P <>BDC 8 0 0 8 314.3535 717.9528 Tm ET (CFM56-7B26)Tj BT /P <>BDC (63.5 inches and a bypass ratio of 4.5:1; or)Tj ET /P <>BDC ET EMC EMC 7 0 0 7 543.7693 11.5132 Tm 7 0 0 7 247.7395 364.7654 Tm 7 0 0 7 82.2047 617.9528 Tm /P <>BDC ET EMC EMC ET ET 9 0 0 9 389.1758 522.8898 Tm BT 7 0 0 7 473.8245 375.9528 Tm /P <>BDC BT 0 Tc 8 0 0 8 95.6042 633.9528 Tm /P <>BDC /P <>BDC ET /P <>BDC 0 Tc 0 Tc /P <>BDC 7 0 0 7 457.1753 727.7654 Tm 0 Tc ET EMC ( )Tj /P <>BDC (capacity with slimmer seats, and cabin)Tj ET /Artifact <>BDC 9 0 0 9 370.2844 489.8898 Tm BT ET ET /P <>BDC EMC ET 7 0 0 7 316.0679 122.7654 Tm BT ( )Tj BT EMC EMC (20)Tj ET BT S 6.5 0 0 6.5 484.6315 545.9529 Tm EMC /P <>BDC EMC /P <>BDC EMC ET EMC EMC BT 7 0 0 7 247.7395 265.7654 Tm 9 0 0 9 344.8161 214.8898 Tm ET ( )Tj ET 7 0 0 7 141.7322 298.9528 Tm 9 0 0 9 193.6853 357.8898 Tm ET BT /P <>BDC /F6 1 Tf /P <>BDC EMC BT EMC ( )Tj ( )Tj EMC /P <>BDC EMC EMC BT /P <>BDC 7 0 0 7 520.6108 518.9528 Tm BT 304.725 420.96 m 7 0 0 7 43.6039 441.9528 Tm BT /Artifact <>BDC EMC BT ET 378 0 0 303.84 -.19113 501.447 cm EMC BT 7 0 0 7 355.3163 166.7654 Tm ( )Tj 9 0 0 9 349.6767 335.8898 Tm ET BT 0 Tc 7 0 0 7 141.7322 584.9528 Tm BT -.01 Tc The wheelbase which is the distance from the nosewheel to the line between the main wheels, which is 11.07 metres. ET EMC ET BT BT EMC BT 7 0 0 7 429.157 485.9528 Tm 0 Tc BT 7 0 0 7 299.0601 89.9528 Tm /P <>BDC 7 0 0 7 444.737 133.7654 Tm /P <>BDC 529.065 38.307 m 9 0 0 9 391.5788 478.8898 Tm 6.5 0 0 6.5 429.0755 650.9529 Tm BT ( )Tj (37,653)Tj ET ET /P <>BDC /P <>BDC ET BT EMC BT ET ET BT 9 0 0 9 215.433 401.8898 Tm BT 9 0 0 9 232.4217 93.8898 Tm 7 0 0 7 478.9484 727.9528 Tm 7 0 0 7 247.7395 716.7654 Tm (The A320ceo is payload-limited to 127)Tj 6 0 0 6 206.4048 687.9528 Tm