/P <>BDC EMC 0 Tc EMC -.02 Tc ET 7 0 0 7 141.7322 485.9528 Tm EMC EMC 9 0 0 9 534.0193 390.8898 Tm /P <>BDC 9 0 0 9 196.8605 115.8898 Tm ET EMC 7 0 0 7 314.6398 727.7654 Tm BT BT 9 0 0 9 536.0613 49.8898 Tm ET If AC power is available, select 7 0 0 7 294.4014 584.7654 Tm /P <>BDC /P <>BDC EMC 9 0 0 9 394.0237 247.8898 Tm (typically based on the aircrafts certified)Tj (1B engine as the 737-8. They were solenoid held and BT BT (283)Tj BT /P <>BDC ET 9 0 0 9 178.1318 71.8898 Tm ( )Tj ET 0 Tc 9 0 0 9 232.438 49.8898 Tm -.01 Tc ET S 9 0 0 9 394.0315 412.8898 Tm EMC 9 0 0 9 557.8457 225.8898 Tm 9 0 0 9 421.0664 401.8898 Tm S /P <>BDC EMC /P <>BDC EMC EMC /P <>BDC EMC ET ET 0 Tc ( )Tj 6.5 0 0 6.5 375.6529 663.9529 Tm -.02 Tc 6 0 0 6 61.517 757.9528 Tm /P <>BDC EMC ET 7 0 0 7 258.2805 716.7654 Tm BT 5.25 0 0 5.25 123.5367 11.5132 Tm 9 0 0 9 36.8504 38.8898 Tm EMC ( )Tj /P <>BDC )Tj EMC (A321neo)Tj -.02 Tc (the 14 sectors with the 85% passenger)Tj W n EMC /P <>BDC ( )Tj ET 7 0 0 7 439.9995 661.9528 Tm /P <>BDC ET ( )Tj 7 0 0 7 440.0906 166.9528 Tm ET /P <>BDC ET ET /P <>BDC /P <>BDC ( )Tj EMC /P <>BDC ET 7 0 0 7 363.2711 67.9528 Tm EMC EMC BT 9 0 0 9 557.1673 794.1039 Tm 9 0 0 9 386.3946 137.8898 Tm BT /GS1 gs BT /P <>BDC 0 Tc EMC /P <>BDC 7 0 0 7 362.3891 342.9528 Tm BT 7 0 0 7 279.1575 507.9528 Tm ET (36,960)Tj (0.0177)Tj ET on 5 Nov 1990 have been destroyed on the ground due to explosions in the empty 7 0 0 7 54.5916 540.7654 Tm ET EMC ET [(AS)29(M)21(s)]TJ ET BT ET (A321ceo)Tj (136)Tj /P <>BDC /P <>BDC 7 0 0 7 456.2165 265.7654 Tm ET EMC EMC ET BT 0 Tc /P <>BDC /P <>BDC (977)Tj ( )Tj 7 0 0 7 457.0984 232.7654 Tm ( )Tj ET 6.5 0 0 6.5 222.7786 676.9529 Tm 9 0 0 9 36.8504 126.8898 Tm 9 0 0 9 232.4217 335.8898 Tm EMC endobj ( )Tj /P <>BDC /P <>BDC EMC BT BT EMC (cost and performance differences between)Tj 9 0 0 9 361.7 456.8898 Tm 0 Tc /P <>BDC 7 0 0 7 158.74 188.7654 Tm Happy Flying. BT -.01 Tc ET 7 0 0 7 204.0935 89.7654 Tm 10 0 0 10 417.91 814.1973 Tm ET BT Is the Range with Max Payload NM(Km) wrong? ET ( )Tj ET BT )Tj )Tj BT EMC /P <>BDC BT ET ET (generation aircraft continues to grow at a)Tj 7 0 0 7 321.6356 166.9528 Tm BT [(R)13.9(OUT)10(E CHARA)16.1(CT)10(ERIS)8.1(T)-8.1(I)0(C)-17.1(S)0( F)8.1(OR ANAL)86.9(YSIS OF AIR)7.1(CRAF)-12.9(T)18.1( PERF)8.1(ORMANCE )]TJ 9 0 0 9 68.3339 478.8898 Tm ET EMC ET EMC (482)Tj 6 0 0 6 507.2798 715.9528 Tm /P <>BDC ET ( )Tj /P <>BDC ET BT EMC (The in-service fleet of the newer)Tj BT EMC -.02 Tc ET ET /P <>BDC ET 0 Tc (As with the rest of the Airbus aircraft,)Tj 9 0 0 9 181.0402 335.8898 Tm BT /P <>BDC ( )Tj 7 0 0 7 141.7322 265.9528 Tm ( )Tj 0 Tc ET -.02 Tc ET EMC ET BT ( )Tj BT 7 0 0 7 247.7395 540.7654 Tm BT /P <>BDC 7 0 0 7 247.7395 265.7654 Tm 9 0 0 9 211.7668 225.8898 Tm EMC EMC BT /P <>BDC thanks for stopping by. EMC BT BT BT /P <>BDC ET -.02 Tc EMC [(BOS-Y)-49.1(VR)]TJ Q 9 0 0 9 36.8504 236.8898 Tm /P <>BDC BT ET /P <>BDC ET EMC /P <>BDC 0 Tc 9 0 0 9 53.8338 38.8898 Tm 7 0 0 7 491.4046 397.9528 Tm BT BT ET 0 Tc BT /GS2 gs EMC EMC ( )Tj ET EMC -.02 Tc ET EMC /P <>BDC (9.0:1)Tj 9 0 0 9 36.8504 412.8898 Tm ET EMC -.02 Tc ET EMC /Artifact <>BDC BT (the 14 routes in the evaluation. 7 0 0 7 37.6993 100.9528 Tm ET (the opposite to the Airbus aircraft. ET ET 9 0 0 9 198.3567 335.8898 Tm 8 0 0 8 471.0755 760.9528 Tm -2.5295 -5.0573 -2.1058 -5.3146 -1.5527 -5.3151 c 0 Tc BT EMC 7 0 0 7 230.7317 386.9528 Tm /P <>BDC 7 0 0 7 490.8321 375.7654 Tm ( )Tj ( )Tj (151)Tj ( )Tj EMC ( )Tj /P <>BDC ET 7 0 0 7 355.3163 89.7654 Tm ET BT )Tj ( )Tj EMC BT (72% of the NG fleet in service. BT BT EMC /P <>BDC BT 848 0 obj allow for a measurement of fuel tank inerting and heating during the ET 9 0 0 9 36.8583 335.8898 Tm EMC This would make)Tj 0 Tc 9 0 0 9 366.7762 390.8898 Tm /P <>BDC BT ( )Tj ET /P <>BDC 9 0 0 9 215.4409 379.8898 Tm BT BT BT It is)Tj 0 Tc /P <>BDC 9 0 0 9 408.1854 511.8898 Tm The advanced wing airfoil design provides an economical cruise speed of .789 Mach (530 mph) - compared to .745 Mach for earlier 737 models. EMC /P <>BDC 7 0 0 7 37.0536 595.9528 Tm ET EMC 6 0 0 6 504.5564 771.9528 Tm EMC BT -.02 Tc -.02 Tc /P <>BDC EMC BT )Tj BT 7 0 0 7 187.0858 661.9528 Tm ( )Tj -.02 Tc ( )Tj Q 3.0566 -3.9073 l I found this image that might have some of the answers you need. 378 0 0 303.84 -.19113 501.447 cm ( )Tj BT 6.5 0 0 6.5 397.5498 624.9529 Tm EMC /P <>BDC ET BT Other data such as fuel load, ET EMC 1 i /P <>BDC /P <>BDC /P <>BDC BT Thanks, Hi Henna, -.02 Tc As stated, this makes a fair)Tj BT /P <>BDC /P <>BDC ET 9 0 0 9 411.0181 346.8898 Tm Hi and thanks for your question. /P <>BDC /P <>BDC (The fourth generation 737-8 is)Tj ET 9 0 0 9 411.0181 467.8898 Tm BT /P <>BDC ( )Tj EMC BT 7 0 0 7 230.7317 705.9528 Tm 0 Tw 9 0 0 9 53.8582 588.8898 Tm ET ET BT ET /P <>BDC EMC EMC /P <>BDC 7 0 0 7 158.74 705.7654 Tm 8 0 0 8 153.6923 675.9528 Tm 7 0 0 7 380.2788 408.7654 Tm 9 0 0 9 197.0674 258.8898 Tm Im not sure I understand the question. /P <>BDC EMC ET ET 7 0 0 7 456.2165 342.7654 Tm /F1 1 Tf /P <>BDC BT -.02 Tc /P <>BDC 7 0 0 7 536.3849 529.7654 Tm EMC ( )Tj ET BT EMC EMC ( )Tj BT EMC BT 7 0 0 7 295.2833 199.7654 Tm -.02 Tc ET )Tj /P <>BDC 7 0 0 7 321.6356 276.9528 Tm /P <>BDC ET ( )Tj /P <>BDC 7 0 0 7 473.8245 221.9528 Tm q BT [(CFM L)17.1(E)-8.1(AP-1B27)]TJ 7 0 0 7 380.2788 430.7654 Tm 9 0 0 9 75.273 445.8898 Tm 9 0 0 9 544.934 49.8898 Tm /P <>BDC 7 0 0 7 337.6855 507.9528 Tm /P <>BDC 0 Tc BT 6 0 0 6 444.3028 659.9528 Tm EMC BT ( )Tj -.02 Tc EMC ( )Tj 7 0 0 7 543.7693 11.5132 Tm BT EMC EMC BT -.02 Tc (176)Tj /P <>BDC ( )Tj BT BT /P <>BDC ( )Tj ET EMC BT BT ( )Tj EMC ET BT /P <>BDC ET 6 0 0 6 205.0069 701.9528 Tm /P <>BDC 7 0 0 7 491.7142 529.7654 Tm BT EMC (0.0129)Tj /P <>BDC /P <>BDC ( )Tj ET BT ET EMC 9 0 0 9 539.8684 280.8898 Tm EMC EMC /GS1 gs 5 0 0 5 484.5872 11.5129 Tm ( )Tj ET /P <>BDC BT (34,650)Tj 7 0 0 7 77.36 11.5132 Tm 36.85 824.882 572.599 17.008 re ( )Tj /P <>BDC BT ET /P <>BDC EMC /P <>BDC 9 0 0 9 206.8496 346.8898 Tm ET 0 Tc 7 0 0 7 158.74 111.7654 Tm /P <>BDC )Tj BT - Modern Airliners. BT BT ( )Tj /P <>BDC ( )Tj EMC 9 0 0 9 232.4217 203.8898 Tm 7 0 0 7 187.0858 397.9528 Tm /P <>BDC 7 0 0 7 337.9444 639.9528 Tm 7 0 0 7 362.3891 287.9528 Tm ET -.01 Tc 6 0 0 6 61.517 701.9528 Tm ET BT (discussions in the industry to potentially)Tj EMC ET /P <>BDC /P <>BDC 9 0 0 9 215.433 192.8898 Tm ET /P <>BDC BT -.02 Tc 7 0 0 7 230.7317 683.9528 Tm EMC BT BT BT EMC /P <>BDC 7 0 0 7 380.2788 496.7654 Tm /P <>BDC BT BT (977)Tj EMC ET /P <>BDC ()Tj (comparison. /P <>BDC ET (37,416)Tj /P <>BDC BT (CFM56-5B3/P)Tj ( )Tj ET (159,251)Tj -.02 Tc ( )Tj /P <>BDC EMC /P <>BDC ET (575)Tj ET ET ( )Tj EMC /OC /MC186 BDC /P <>BDC 9 0 0 9 215.4313 49.8898 Tm BT EMC -.02 Tc 7 0 0 7 490.5101 705.9528 Tm 7 0 0 7 535.5029 122.7654 Tm /P <>BDC Can you confirm if Im right or wrong? 6 0 0 6 239.8235 743.9528 Tm 0 Tc 9 0 0 9 541.1655 478.8898 Tm /P <>BDC .151 .147 .15 rg EMC .001 Tc ( )Tj EMC BT BT EMC ( )Tj Hello! 9 0 0 9 175.8821 467.8898 Tm /P <>BDC S ET (418)Tj /P <>BDC BT BT 9 0 0 9 411.0181 115.8898 Tm /P <>BDC -.02 Tc /P <>BDC /P <>BDC ET BT /P <>BDC (371,416)Tj It has a maximum range of 10,140km. EMC BT EMC (152)Tj /P <>BDC (capacity, so that payload is reduced to)Tj 7 0 0 7 187.0858 408.9528 Tm (CFM LEAP-1B28B1s thrust rating to)Tj 7 0 0 7 366.0641 727.9528 Tm ( )Tj ( )Tj ( )Tj (A321neo)Tj ET ET ET ET BT ET (170)Tj 0 Tc 8 0 0 8 187.3427 661.9528 Tm EMC ET 0 Tc 7 0 0 7 158.74 639.7654 Tm BT -.02 Tc ET EMC 9 0 0 9 197.9514 148.8898 Tm BT /P <>BDC ET ( )Tj /P <>BDC BT /P <>BDC BT EMC /P <>BDC ET 17 0 0 17 36.8606 775.1944 Tm 503.542 90.794 m 7 0 0 7 475.2383 672.9528 Tm /P <>BDC ( )Tj ET (3,400 )Tj .023 .567 .626 rg 9 0 0 9 53.8582 687.8898 Tm ET ( )Tj 9 0 0 9 53.8582 742.8898 Tm EMC /P <>BDC tank is refuelled. ( )Tj ET /P <>BDC ( )Tj (have therefore been removed from the)Tj ( )Tj EMC ET ( )Tj /P <>BDC BT /P <>BDC 8 0 0 8 394.0157 786.8898 Tm ( )Tj /P <>BDC BT 6 0 0 6 271.9128 729.9528 Tm /P <>BDC BT -.02 Tc (109,800lbs )Tj EMC ET 0 Tc ET ET EMC EMC Boeing 737 MAX 9 pictures, specifications, cabin configuration. (Most mainline US carriers are using the)Tj BT /P <>BDC EMC Q ET ( )Tj /P <>BDC BT ( )Tj ( )Tj BT ET BT ET @import url(http://www.google.com/cse/api/branding.css); All of the information, photographs & schematics from this website and much more is now available in a 374 page printed book or in electronic format. ( )Tj /P <>BDC BT -.02 Tc ET EMC ET /P <>BDC /P <>BDC 7 0 0 7 338.5674 133.9528 Tm 9 0 0 9 541.5243 720.8898 Tm 0 Tc EMC BT 7 0 0 7 199.5784 540.7654 Tm BT EMC (load factor, the A321neo carries a heavier)Tj BT EMC 6.5 0 0 6.5 331.0061 722.9529 Tm ET BT ET BT ET 10 0 0 10 37.304 794.2914 Tm 7 0 0 7 387.0159 595.9528 Tm All information is given in good faith and for information purposes only. ET EMC EMC ET ET (A320neo:)Tj EMC EMC BT Q BT /P <>BDC /P <>BDC BT 9 0 0 9 77.618 82.8898 Tm 7 0 0 7 490.5101 507.9528 Tm /P <>BDC ET EMC ( )Tj /P <>BDC EMC ET 786 0 obj EMC /F1 1 Tf /P <>BDC /P <>BDC -.02 Tc EMC 7 0 0 7 539.8962 595.9528 Tm ( )Tj ET (1,351)Tj BT 0 Tc EMC /P <>BDC EMC ( )Tj BT 9 0 0 9 36.8504 137.8898 Tm ET (2,115)Tj /P <>BDC ET BT /P <>BDC 9 0 0 9 382.9368 148.8898 Tm ET /P <>BDC ET /P <>BDC /P <>BDC (0.0134)Tj 0 Tc BT BT (materials. ET /P <>BDC ( )Tj /P <>BDC EMC /F1 1 Tf /OC /MC2261 BDC ( )Tj 0 Tc 0 Tc 7 0 0 7 404.101 166.7654 Tm EMC ( )Tj ( )Tj BT BT W n BT BT EMC ET ET q /P <>BDC BT 0 Tc ET 7 0 0 7 193.1059 683.9528 Tm /P <>BDC /P <>BDC ET ET (uses one of the 11 certified weight variants. 7 0 0 7 316.0679 342.7654 Tm ET ET BT ET 8 0 0 8 153.6923 661.9528 Tm [(737-900E)-33(R)]TJ BT BT ET EMC 7 0 0 7 204.0935 111.7654 Tm EMC /P <>BDC EMC /OC /MC2287 BDC (The first is payload scenario 1, which)Tj ( )Tj ET ET BT EMC /P <>BDC /P <>BDC 7 0 0 7 338.6433 309.7654 Tm 9 0 0 9 361.007 126.8898 Tm EMC 9 0 0 9 53.8338 148.8898 Tm /P <>BDC BT EMC (831)Tj /P <>BDC BT ET 7 0 0 7 430.039 683.9528 Tm ET BT EMC /P <>BDC ( )Tj EMC EMC /P <>BDC /P <>BDC ET /P <>BDC 8 0 0 8 187.3427 619.9528 Tm . /P <>BDC (fixed speed of LRC can be applied to all)Tj 0 Tc 9 0 0 9 53.8582 566.8898 Tm 7 0 0 7 456.4753 430.7654 Tm /P <>BDC BT ET EMC 7 0 0 7 445.619 694.7654 Tm ( )Tj BT BT 6.5 0 0 6.5 192.0331 663.9529 Tm /P <>BDC /P <>BDC ( )Tj (37,653)Tj BT 7 0 0 7 439.2087 199.9528 Tm 7 0 0 7 491.4046 100.9528 Tm 7 0 0 7 363.0612 430.9528 Tm . (1,272)Tj BT 7 0 0 7 279.1575 441.9528 Tm BT /P <>BDC ( )Tj (maintenance costs. ET /P <>BDC ET ( )Tj -.02 Tc ET /P <>BDC /GS2 gs EMC ( )Tj EMC (follow in their footsteps, having already)Tj /OC /MC5097 BDC ET -.02 Tc ( )Tj 7 0 0 7 298.514 562.9528 Tm BT EMC /P <>BDC /P <>BDC ( )Tj 9 0 0 9 343.6557 148.8898 Tm -.02 Tc /P <>BDC ( )Tj EMC 9 0 0 9 36.8583 467.8898 Tm EMC ET ( )Tj ET -.07 Tc 7 0 0 7 131.6494 265.7654 Tm /P <>BDC ET ( )Tj /P <>BDC EMC ET BT The cause of the accident was determined to be a malfunctioning left radar altimeter. /P <>BDC 5.25 0 0 5.25 73.853 11.5132 Tm ( )Tj BT EMC EMC EMC EMC ET /P <>BDC EMC 7 0 0 7 82.8504 419.9528 Tm /GS2 gs 7 0 0 7 508.4124 496.7654 Tm /P <>BDC ET 8 0 0 8 38.4438 661.9528 Tm ( )Tj ET -.01 Tc /P <>BDC ET 9 0 0 9 540.3891 544.8898 Tm ( )Tj BT ET 8 0 0 8 474.6331 771.7654 Tm /F1 1 Tf BT BT EMC ET 0 J 0 j .5 w 10 M [] 0 d /GS2 gs /P <>BDC 0 Tc /P <>BDC 9 0 0 9 411.0097 49.8898 Tm EMC 9 0 0 9 381.9109 456.8898 Tm 9 0 0 9 390.2557 511.8898 Tm EMC (206,132lbs, an MLW of 171,500lbs, and)Tj ET BT /P <>BDC 735 0 obj ( )Tj ET /P <>BDC ( )Tj 7 0 0 7 187.0858 265.9528 Tm BT 9 0 0 9 394.0315 159.8898 Tm ( )Tj ( )Tj ( )Tj EMC 7 0 0 7 491.7142 606.7654 Tm 7 0 0 7 82.8504 78.9528 Tm endobj /P <>BDC 6 0 0 6 222.2255 771.9528 Tm BT BT ET /P <>BDC the No 1 tank pumps ON for APU operation to assist the fuel control unit, .0161 Tc 9 0 0 9 542.5887 159.8898 Tm ET /P <>BDC ET 7 0 0 7 141.7322 177.9528 Tm caused the FAA to issue SFAR88 in June 2001 which mandates improvements to the ET BT ET 5 0 0 5 484.5872 11.5129 Tm ET 0 Tc 7 0 0 7 508.2252 11.5129 Tm (273,600)Tj 7 0 0 7 54.7071 716.7654 Tm ET EMC 0 Tc Typical freezing point of Jet A1 is -47C. ET BT (CFM56-7B26)Tj 7 0 0 7 338.3085 287.9528 Tm /P <>BDC /P <>BDC /P <>BDC /P <>BDC ET 9 0 0 9 232.4217 236.8898 Tm (0.0110)Tj 7 0 0 7 365.035 639.9528 Tm 7 0 0 7 439.2087 375.9528 Tm 6 0 0 6 434.151 757.9528 Tm ( )Tj BT BT EMC 6 0 0 6 77.6053 771.9528 Tm BT ET 0 Tc (A320neo)Tj ( )Tj (192)Tj 9 0 0 9 232.4217 258.8898 Tm ( )Tj BT /P <>BDC BT 7 0 0 7 380.2788 419.7654 Tm BT ( )Tj /P <>BDC BT /P <>BDC (A321neo)Tj ( )Tj 9 0 0 9 232.438 225.8898 Tm BT ET BT EMC EMC /P <>BDC 9 0 0 9 68.0314 126.8898 Tm EMC EMC BT EMC ( )Tj EMC ( )Tj EMC BT EMC 7 0 0 7 490.7815 221.9528 Tm 9 0 0 9 369.406 104.8898 Tm (CFM56-7B27B3)Tj /P <>BDC ET Share Improve this answer Follow answered Aug 12, 2019 at 15:48 user14897 These variables are also important because there's an assumption that if you're riding a 737, certain load factors and distances are more likely. ( )Tj ET EMC EMC 7 0 0 7 125.6292 133.7654 Tm -.02 Tc 7 0 0 7 316.0679 287.7654 Tm BT 0 Tc The)Tj ET 6 0 0 6 554.6981 760.7654 Tm EMC /P <>BDC EMC ET 7 0 0 7 199.5784 639.7654 Tm (113,016)Tj /P <>BDC 0 Tc EMC ET 8 0 0 8 457.2727 760.7654 Tm BT ( )Tj EMC BT EMC EMC Can you please tell me where to look for the cabin height,width, seat height, width and door to door length. BT EMC /P <>BDC (ratio of 5.1:1. /P <>BDC ( )Tj )21(The r)10(elativ)12.9(e)]TJ BT 7 0 0 7 315.1859 144.7654 Tm EMC -.02 Tc ET 199,158 Litres: . EMC ( )Tj 6.5 0 0 6.5 176.9362 545.9529 Tm 0 Tc )Tj Hi Anna-Maria, ET /P <>BDC 7 0 0 7 337.6855 595.9528 Tm -.02 Tc ET 13 0 0 13 532.9001 786.8898 Tm /P <>BDC ET -.02 Tc less heating from the smaller hydraulic system A. EMC ET - Smiths. /P <>BDC -.02 Tc 5.25 0 0 5.25 515.3989 11.5129 Tm /P <>BDC 7 0 0 7 491.7142 364.7654 Tm EMC BT ET ET EMC BT EMC Q ET [(AIRL)8.1(INE & AIR)7.1(CRAF)-12.9(T)18.1( OPERA)56.9(T)-8.1(ION)-13.9(S)]TJ /P <>BDC 7 0 0 7 387.0932 210.9528 Tm BT /P <>BDC EMC 7 0 0 7 429.157 738.9528 Tm 6.5 0 0 6.5 346.3049 663.9529 Tm EMC 9 0 0 9 394.0157 500.8898 Tm ET 7 0 0 7 521.4089 11.5132 Tm ( )Tj EMC ET ET ET ( )Tj ET /P <>BDC 7 0 0 7 294.4014 188.7654 Tm 9 0 0 9 505.9653 115.8898 Tm ET 7 0 0 7 403.478 694.7654 Tm 9 0 0 9 60.6117 794.1039 Tm .014984 841.89 609.45 -841.89 re /P <>BDC -.02 Tc EMC ( )Tj EMC 9 0 0 9 36.8504 478.8898 Tm (operational factors that also have to be)Tj ( )Tj 7 0 0 7 141.7322 430.9528 Tm ( )Tj EMC ( )Tj ( )Tj 9 0 0 9 185.7888 489.8898 Tm ET (same cost index, and the method that each)Tj ET 7 0 0 7 337.6855 540.9528 Tm EMC Calibration ( )Tj 9 0 0 9 36.8504 214.8898 Tm ET BT ET ( )Tj (\(Toronto Pearson\) sector, to 2,730nm for)Tj EMC ET ET EMC EMC document.getElementById( "ak_js_1" ).setAttribute( "value", ( new Date() ).getTime() ); Airbus A320 Introduction The very popular short haul airliner. 0 Tc 0 Tc /P <>BDC EMC BT ET EMC EMC BT ET EMC ( )Tj ET ET 9 0 0 9 375.0299 434.8898 Tm EMC [(CFM L)17.1(E)-8.1(AP-1A26)]TJ 0 Tc ( )Tj 7 0 0 7 520.6108 485.9528 Tm ( )Tj (-62)Tj EMC ( )Tj -.02 Tc EMC -.02 Tc [(7)-33(3)8(7-900ER)]TJ /P <>BDC /GS1 gs BT /P <>BDC /P <>BDC ET -.02 Tc BT (- mins)Tj 9 0 0 9 213.294 489.8898 Tm 7 0 0 7 241.5317 485.9528 Tm -.02 Tc /P <>BDC ET ET 7 0 0 7 107.1165 661.9528 Tm ET 7 0 0 7 158.74 122.7654 Tm 7 0 0 7 99.8582 188.7654 Tm /P <>BDC BT ( )Tj ET 5 0 obj .151 .147 .15 rg ET (O)Tj ET BT EMC /P <>BDC /GS1 gs ET EMC .151 .147 .15 rg ( )Tj -.02 Tc 19.85 0 l 6 0 0 6 301.1609 687.9528 Tm EMC BT (CFM56-7B26)Tj -.02 Tc 0 Tc 6.5 0 0 6.5 500.4941 565.9529 Tm ET endobj /P <>BDC (component is stated )Tj EMC ET ET [(BOS-C)-8.1(V)18.1(G)]TJ 9 0 0 9 36.8504 313.8898 Tm ( )Tj W n ET (hour and per mile reduces . BT ET ET BT BT ET Aircraft have been NGS provisioned since l/n 1935 and it has been installed since l/n 2620 onwards. BT 7 0 0 7 518.4953 441.9528 Tm ( )Tj ET 9 0 0 9 394.0315 456.8898 Tm EMC ET /F6 1 Tf EMC ( )Tj 9 0 0 9 53.8338 60.8898 Tm [(SS)-9(U)8.1(E)]TJ EMC /P <>BDC 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 ET 0 Tc (603)Tj 8 0 0 8 397.6498 771.9529 Tm ET 9 0 0 9 215.433 412.8898 Tm BT ET 0 Tc BT /P <>BDC ( )Tj ET 0 Tc EMC BT 0 Tc -.02 Tc -.02 Tc ET /P <>BDC EMC 7 0 0 7 182.3536 78.9528 Tm BT 8 0 0 8 365.7704 675.9528 Tm 9 0 0 9 394.0315 709.8898 Tm /P <>BDC EMC ET ET /P <>BDC BT BT ( )Tj 9 0 0 9 538.0952 500.8898 Tm /OC /MC854 BDC BT ( )Tj /P <>BDC ( )Tj (number of available seat-miles \(ASM\))Tj ( )Tj BT EMC EMC 0 Tc BT /P <>BDC ET BT /P <>BDC ( )Tj ET /P <>BDC EMC EMC 7 0 0 7 299.0601 210.9528 Tm ET 8 0 0 8 187.3427 577.9528 Tm 7 0 0 7 82.2047 694.9528 Tm (4,787)Tj BT /P <>BDC (The average over the 14 sectors is a)Tj ( )Tj 0 Tc ET ET 9 0 0 9 232.4217 544.8898 Tm EMC 0 Tc BT 13 0 0 13 202.8899 533.8898 Tm ( )Tj BT ET ( )Tj EMC ET /P <>BDC /P <>BDC ET 7 0 0 7 294.4014 716.7654 Tm ET BT ET EMC ET /P <>BDC /Artifact <>BDC EMC /P <>BDC '''''''''' z" ET (737-800W)Tj EMC EMC /P <>BDC EMC ( )Tj 9 0 0 9 411.0181 159.8898 Tm BT 9 0 0 9 68.0314 401.8898 Tm 7 0 0 7 344.1175 617.7654 Tm /F1 1 Tf BT /F6 1 Tf EMC -.02 Tc /P <>BDC BT (3,882)Tj ET BT /P <>BDC 0 Tc /P <>BDC EMC (1,272)Tj EMC /P <>BDC 7 0 0 7 427.7291 177.9528 Tm /P <>BDC BT Although successful the A320 could not take on the Boeing 737s success. ET 7 0 0 7 118.104 661.7654 Tm ET (297,312)Tj /F1 1 Tf the permissible CSFF area, the outside air temperature is above freezing(0 C, 32 BT /P <>BDC BT BT ET /P <>BDC BT EMC 7 0 0 7 459.6601 11.5129 Tm 7 0 0 7 520.6108 584.9528 Tm BT The)Tj BT ( )Tj (would need to consider many more factors)Tj EMC /P <>BDC 7 0 0 7 473.8245 111.9528 Tm BT /P <>BDC ET ( )Tj 9 0 0 9 394.0123 280.8898 Tm -.02 Tc /GS2 gs EMC BT ( )Tj ET -.02 Tc ( )Tj /P <>BDC 9 0 0 9 565.2708 313.8898 Tm EMC ET 7 0 0 7 314.6398 606.7654 Tm EMC (1,091)Tj EMC -2.0374 -.5351 -2.4615 -.7535 -2.6921 -1.1048 c EMC ( )Tj BT (The performance improvement in the)Tj EMC -.02 Tc 7 0 0 7 37.6993 177.9528 Tm (126,312)Tj ET (0.0121)Tj ( )Tj /P <>BDC This narrow body jet airliner had first rolled out on June 30, 1997 and shortly after was had its first test flight with he pilot Jim McRoberts in the cockpit. BT 9 0 0 9 142.2128 335.8898 Tm ET 0 Tc [(BOS-A)56.9(TL)]TJ /P <>BDC BT 7 0 0 7 204.0935 430.7654 Tm EMC /P <>BDC EMC /P <>BDC /P <>BDC ET 9 0 0 9 542.2972 203.8898 Tm BT 9 0 0 9 204.9867 214.8898 Tm /P <>BDC ET EMC EMC There arent to many differences between each variant. ET 7 0 0 7 537.7804 188.9528 Tm ( )Tj 9 0 0 9 53.8582 753.8898 Tm Q ET /P <>BDC EMC ( )Tj ET BT ( )Tj All the aircraft would therefore)Tj EMC /P <>BDC -.02 Tc 7 0 0 7 535.5029 661.7654 Tm 9 0 0 9 36.8504 291.8898 Tm 0 Tc 9 0 0 9 215.4313 478.8898 Tm (174,900)Tj ( )Tj EMC ( )Tj /F6 1 Tf EMC /P <>BDC BT ET 0 Tc (. EMC ET EMC ( )Tj ( )Tj S /P <>BDC ET EMC BT EMC /P <>BDC BT EMC ET -.02 Tc /P <>BDC 8 0 0 8 181.9279 771.7654 Tm /P <>BDC 7 0 0 7 99.8582 397.7654 Tm 7 0 0 7 82.8504 89.9528 Tm (140-148)Tj [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ /P <>BDC /P <>BDC 9 0 0 9 53.8338 269.8898 Tm 7 0 0 7 298.514 584.9528 Tm EMC 6 0 0 6 527.8009 743.9528 Tm EMC ET EMC ET 6.5 0 0 6.5 276.4014 650.9529 Tm 6.5 0 0 6.5 174.4663 735.9529 Tm /P <>BDC EMC EMC 7 0 0 7 403.478 639.7654 Tm 7 0 0 7 316.0679 243.7654 Tm /F7 1 Tf ( )Tj BT 7 0 0 7 82.2047 507.9528 Tm /P <>BDC 7 0 0 7 387.0159 727.9528 Tm EMC /P <>BDC .176 .307 .621 rg ET EMC 0 Tc BT ET BT 0 Tc EMC ( )Tj EMC ET (2,731)Tj EMC 7 0 0 7 187.0858 100.9528 Tm BT ET (which is BOS-LAX, whereas the 737-800)Tj BT (5,025)Tj 0 Tc /P <>BDC ET /P <>BDC (37,653)Tj (choice of engine variant. EMC ET /P <>BDC ET ET /Artifact <>BDC /P <>BDC 7 0 0 7 158.74 232.7654 Tm EMC BT /P <>BDC EMC (carriers. /P <>BDC BT (0.0134)Tj EMC 9 0 0 9 372.0688 324.8898 Tm /P <>BDC EMC .0161 Tc ET 7 0 0 7 457.0984 507.7654 Tm ( )Tj 9 0 0 9 215.433 71.8898 Tm EMC -.02 Tc EMC (differences in the flight times. 7 0 0 7 204.0935 628.7654 Tm BT BT EMC ET EMC /P <>BDC 9 0 0 9 375.2598 126.8898 Tm -.02 Tc BT 7 0 0 7 459.6601 11.5129 Tm 9 0 0 9 216.03 687.8898 Tm 0 Tc ET -.07 Tc 6.5 0 0 6.5 346.019 742.9529 Tm /P <>BDC EMC ( )Tj BT BT /P <>BDC EMC 7 0 0 7 473.8245 320.9528 Tm ET (1,683)Tj ET (A320ceo)Tj BT /P <>BDC (977)Tj ET /P <>BDC /P <>BDC ET ( )Tj centre fuel tank. EMC /P <>BDC BT ET ET (0.0149)Tj /P <>BDC ET BT /P <>BDC 9 0 0 9 394.0157 247.8898 Tm /P <>BDC (136)Tj , http://toulouse747.com/wp-content/uploads/2018/12/Boeing-B737-700-800-900-Operations-Manual.pdf. 9 0 0 9 232.4408 720.8898 Tm The fuel was fed BT W n 7 0 0 7 456.4753 716.7654 Tm ( )Tj BT BT BT The Boeing 737-800 is an example of an average sized airplane. 7 0 0 7 230.7317 628.9528 Tm ( )Tj EMC ( )Tj ET EMC /P <>BDC EMC /P <>BDC 7 0 0 7 316.0679 441.7654 Tm 10 0 0 10 47.8705 814.1973 Tm EMC 7 0 0 7 118.104 166.7654 Tm BT The)Tj /P <>BDC BT /P <>BDC -.02 Tc /P <>BDC /P <>BDC .0161 Tc BT 7 0 0 7 439.2087 210.9528 Tm BT (The A320ceo is payload-restricted to)Tj EMC ET EMC EMC -.02 Tc ( )Tj /P <>BDC -.02 Tc ( )Tj The flight)Tj ( )Tj /P <>BDC EMC ET EMC /P <>BDC ( )Tj EMC BT ( )Tj ET /P <>BDC 9 0 0 9 53.8582 643.8898 Tm 7 0 0 7 518.4953 408.9528 Tm BT EMC /GS2 gs ET (39,270)Tj EMC .014984 841.89 609.45 -841.89 re BT BT 7 0 0 7 490.5101 485.9528 Tm ET /P <>BDC 0 Tc BT 7 0 0 7 473.8245 265.9528 Tm ET 7 0 0 7 294.4014 276.7654 Tm EMC auxiliary tank at the forward end of the aft hold; these were available in ET ET ET 7 0 0 7 363.2711 573.9528 Tm EMC 7 0 0 7 294.4014 628.7654 Tm BT 6.5 0 0 6.5 224.5532 598.9529 Tm 0 Tc ET BT )Tj BT /P <>BDC BT ET 7 0 0 7 473.8245 243.9528 Tm 0 Tc 0 Tc ET EMC If you like us, please share with your followers. ( )Tj EMC EMC -.02 Tc Their version of the Boeing 737-800 is the Airbus A220. BT BT ( )Tj 8 0 0 8 122.6593 760.7654 Tm ET ET EMC /P <>BDC EMC /P <>BDC ET BT BT BT /P <>BDC 7 0 0 7 518.4953 188.9528 Tm BT BT ET 9 0 0 9 232.4217 489.8898 Tm (The A320neo offers a significant)Tj /P <>BDC EMC 9 0 0 9 215.4409 368.8898 Tm ( )Tj ( )Tj ( )Tj BT ( )Tj EMC 9 0 0 9 191.9099 93.8898 Tm BT 0 Tc BT ( )Tj ET EMC /P <>BDC ( )Tj -.02 Tc BT 7 0 0 7 518.4953 210.9528 Tm ET ET ET (have taken advantage of lighter composite)Tj ET BT EMC ET /P <>BDC BT /F4 1 Tf ET 7 0 0 7 182.5706 639.9528 Tm ( )Tj ET -.02 Tc 0 Tc /P <>BDC 6.5 0 0 6.5 64.6596 565.9529 Tm 7 0 0 7 54.7071 694.7654 Tm 7 0 0 7 116.3631 11.5132 Tm /P <>BDC (operate with first, economy-plus and)Tj 8 0 0 8 332.978 591.9528 Tm 7 0 0 7 37.0536 573.9528 Tm (CFM56-7B26)Tj ( )Tj /P <>BDC BT ET /P <>BDC /P <>BDC ET The 800 variant is the stretched version of the 737-700. /P <>BDC BT EMC (2,933)Tj -.02 Tc /P <>BDC BT BT /P <>BDC 9 0 0 9 198.5183 445.8898 Tm /P <>BDC 8 0 0 8 225.1837 619.9528 Tm (ONT/73)Tj 9 0 0 9 53.8582 346.8898 Tm BT ( )Tj EMC ET /P <>BDC EMC [(737-900E)-33(R)]TJ EMC ET BT (difference between the aircraft types)Tj (410,271)Tj ET for water. BT /GS1 gs ET EMC EMC BT /P <>BDC It therefore offers no)Tj 8 0 0 8 439.2348 771.9528 Tm -.02 Tc 9 0 0 9 36.8504 280.8898 Tm 9 0 0 9 215.433 38.8898 Tm ET EMC EMC 7 0 0 7 404.101 100.7654 Tm BT EMC 7 0 0 7 379.3969 177.7654 Tm 7 0 0 7 258.2805 672.7654 Tm ET EMC /P <>BDC (against the 737-800 is interesting. EMC 9 0 0 9 373.9458 159.8898 Tm -.02 Tc BT 6.5 0 0 6.5 534.5352 624.9529 Tm EMC 9 0 0 9 394.0315 500.8898 Tm ( )Tj EMC /P <>BDC The -800 has sold strongly since its launch . ET EMC ( )Tj EMC Whilst bigger than the Embraer E-Jets, Boeing feels this is an optimum size range for a small city jet which can also be used for medium-haul international services. EMC EMC 9 0 0 9 53.8338 313.8898 Tm 6.5 0 0 6.5 54.877 689.9529 Tm EMC 9 0 0 9 426.0987 687.8898 Tm 7 0 0 7 204.0935 188.7654 Tm /P <>BDC (. /P <>BDC EMC /P <>BDC EMC (977)Tj ET BT ET 7 0 0 7 535.5029 221.7654 Tm ( )Tj /P <>BDC ET (maximise their service offering. .151 .147 .15 rg 7 0 0 7 316.0679 364.7654 Tm EMC ET 7 0 0 7 36.8504 749.9528 Tm /P <>BDC /P <>BDC ET 9 0 0 9 152.6787 566.8898 Tm /P <>BDC ( )Tj 6 0 0 6 309.2107 771.9528 Tm 7 0 0 7 354.6933 540.7654 Tm ( )Tj 7 0 0 7 543.7693 11.5132 Tm (1,272)Tj ET EMC /P <>BDC ET .12988 .27633 .58575 rg ET EMC 0 Tc (420)Tj /P <>BDC EMC 9 0 0 9 53.8582 390.8898 Tm ET EMC ET EMC BT /P <>BDC (family, Airbus has reduced the thrust)Tj /P <>BDC EMC )Tj (largest operating costs for any aircraft)Tj ET EMC [(SS)-9.1(U)8(E)]TJ 9 0 0 9 356.1657 445.8898 Tm BT /P <>BDC ET 7 0 0 7 355.5753 584.7654 Tm BT EMC BT 6.5 0 0 6.5 90.4525 663.9529 Tm ET /P <>BDC EMC .498 .4095 .5623 .1043 v ET EMC ET ET EMC EMC EMC /P <>BDC 7 0 0 7 439.2087 265.9528 Tm 9 0 0 9 215.4409 522.8898 Tm ( )Tj Because of BT 7 0 0 7 456.4753 639.7654 Tm BT /P <>BDC ET EMC -.02 Tc EMC /P <>BDC 9 0 0 9 182.0482 379.8898 Tm (1,761)Tj -.01 Tc ( )Tj ( )Tj /P <>BDC /P <>BDC ( )Tj EMC EMC ( )Tj -.01 Tc 9 0 0 9 181.3643 335.8898 Tm /P <>BDC System Description. EMC ET Greetings. ET 9 0 0 9 425.183 456.8898 Tm BT 19.843 0 l q /P <>BDC Economy-plus is also)Tj /P <>BDC 7 0 0 7 380.2788 463.7654 Tm -.02 Tc [(CFM L)17.1(E)-8.1(AP-1B27)]TJ ( )Tj /P <>BDC 7 0 0 7 316.0679 375.7654 Tm 8 0 0 8 225.1837 703.9528 Tm BT /P <>BDC )Tj ET 9 0 0 9 537.6801 258.8898 Tm 7 0 0 7 258.2805 628.7654 Tm EMC /P <>BDC ET 8 0 0 8 124.845 675.9528 Tm EMC 7 0 0 7 108.6215 232.9528 Tm BT /P <>BDC EMC BT EMC ( )Tj BT BT 9 0 0 9 411.0097 203.8898 Tm BT ET 8 0 0 8 394.0237 71.8898 Tm ET ET EMC EMC /P <>BDC 6 0 0 6 496.9595 715.9528 Tm In which manual could you find the cross-sectional dimensions of the wing spars and stabilizer (737-300) 7 0 0 7 366.0641 683.9528 Tm ET /P <>BDC EMC 9 0 0 9 215.4409 137.8898 Tm BT ET EMC BT (some minor aerodynamic improvements)Tj /P <>BDC ET /P <>BDC If you switch on the centre tank pumps and the LP lights ET 7 0 0 7 321.6356 397.9528 Tm BT BT [(D)12.9(A)42(Y/57)]TJ -.02 Tc .559 .331 .619 rg BT ( )Tj EMC /P <>BDC EMC 8 0 0 8 339.6345 760.7654 Tm EMC BT /P <>BDC /P <>BDC /P <>BDC The)Tj ET 9 0 0 9 232.4217 247.8898 Tm EMC -.02 Tc BT /P <>BDC BT EMC ET 0 Tc BT (series has a weight penalty because of its)Tj /P <>BDC <>/XObject<>/ExtGState<>/Properties<>>> EMC EMC [(BOS-A)56.9(TL)]TJ 0 Tc (0.0119)Tj ET EMC (1.5 mm) thick, the extent of the frost is similar on both wings, the frost is on or between the black lines defining