/P <>BDC BT (ASM benefit over the A320ceo for the)Tj /P <>BDC EMC EMC .023 .567 .626 rg ET (The main operating parameters are: )Tj q 1 0 0 1 394.024 91.644 cm 0 0 m BT EMC /P <>BDC EMC The)Tj /P <>BDC EMC ( )Tj BT ET ( )Tj BT (scheduled times planned by the carrier may)Tj /P <>BDC ET (1,823)Tj warmer air or accelerate to increase the kinetic heating. EMC BT 0 Tc EMC 7 0 0 7 355.3163 133.7654 Tm BT /P <>BDC /P <>BDC EMC ET (test programme is well underway for entry)Tj 7 0 0 7 494.3672 661.7654 Tm ( )Tj 9 0 0 9 36.8504 258.8898 Tm provision for a ferry kit. EMC /P <>BDC 7 0 0 7 554.7883 705.7654 Tm -.02 Tc .41 .161 .508 rg ( )Tj BT ( )Tj ET ET EMC ET ( )Tj ET /P <>BDC ET ET /P <>BDC ET /P <>BDC 8 0 0 8 43.6039 591.9528 Tm 7 0 0 7 210.1137 661.7654 Tm ( )Tj EMC EMC (original equipment manufacturer \(OEM\))Tj EMC 7 0 0 7 430.039 639.9528 Tm 7 0 0 7 386.3929 628.9528 Tm /P <>BDC EMC 9 0 0 9 341.891 335.8898 Tm 9 0 0 9 215.433 214.8898 Tm EMC EMC ( )Tj BT /P <>BDC /P <>BDC (might have over an older aircraft would)Tj EMC 9 0 0 9 411.0097 181.8898 Tm ( )Tj EMC ET A nitrogen-enriched air ( )Tj 7 0 0 7 379.3969 89.7654 Tm 6 0 0 6 553.1396 687.9528 Tm EMC ( )Tj BT EMC 9 0 0 9 394.0237 214.8898 Tm EMC 7 0 0 7 519.3773 221.9528 Tm BT ET ET 7 0 0 7 487.0872 11.5129 Tm 7 0 0 7 321.6356 364.9528 Tm 0 Tc (410,271)Tj /P <>BDC BT ET 9 0 0 9 394.0315 247.8898 Tm BT ( 2021)Tj /P <>BDC /P <>BDC /P <>BDC ( )Tj BT -.02 Tc EMC 0 Tc 9 0 0 9 542.6167 159.8898 Tm (0.0129)Tj ET EMC /P <>BDC ( )Tj ET 6.5 0 0 6.5 499.1812 663.9529 Tm ET ( )Tj /P <>BDC ET Bombardier CRJ 700/CRJ 900/CRJ 1000 Series. 9 0 0 9 53.8582 214.8898 Tm 7 0 0 7 337.6855 67.9528 Tm EMC The seat configuration used in)Tj BT /P <>BDC ( )Tj BT ET ET (the flight profile based on the cruise speed)Tj /P <>BDC /P <>BDC BT .0081 Tc /P <>BDC 0 Tc ET f /P <>BDC Follow this link to see the "Quick Change" Aux fuel system offered by Long Range, expected 2015. -.01 Tc EMC /P <>BDC ET -.02 Tc BT Flight crew can select fwd or aft tanks but normal practice is to use both /P <>BDC ET EMC BT EMC BT BT /P <>BDC EMC 7 0 0 7 364.1531 133.9528 Tm /P <>BDC EMC EMC ET ET EMC /P <>BDC EMC /P <>BDC 7 0 0 7 490.8321 540.7654 Tm ET BT ( )Tj ( )Tj 7 0 0 7 473.8245 287.9528 Tm BT EMC It is the CFM LEAP-)Tj /P <>BDC BT -.02 Tc /P <>BDC EMC BT 7 0 0 7 521.4928 573.9528 Tm (. BT 36.85 824.882 572.599 17.008 re /P <>BDC 9 0 0 9 215.4409 280.8898 Tm /P <>BDC W n /P <>BDC 7 0 0 7 230.7317 683.9528 Tm (831)Tj -.02 Tc BT (159,251)Tj The)Tj BT BT BT 9 0 0 9 411.0097 588.8898 Tm ( )Tj BT 5 0 0 5 484.5872 11.5129 Tm /P <>BDC (same passenger payload. ET EMC BT (403)Tj 0 Tc ET EMC (0.0154)Tj /P <>BDC 7 0 0 7 338.6433 298.7654 Tm ET EMC EMC EMC -.02 Tc 9 0 0 9 532.3544 214.8898 Tm ET /P <>BDC EMC /P <>BDC ( )Tj BT ET EMC BT (737-9 compared to the 737-900ER\(W\) is)Tj BT ET -.01 Tc ET 9 0 0 9 568.555 82.8898 Tm 0 Tc 6 0 0 6 433.7788 729.9528 Tm EMC 9 0 0 9 536.6833 500.8898 Tm S /P <>BDC EMC 9 0 0 9 171.8783 434.8898 Tm 7 0 0 7 554.7883 386.7654 Tm BT ET BT 6 0 0 6 527.3577 771.9528 Tm /P <>BDC BT )Tj ET /P <>BDC ET BT BT BT EMC (900ER\(W\). EMC (294)Tj ( )Tj BT ET BT ( )Tj EMC BT /P <>BDC 9 0 0 9 382.3068 489.8898 Tm EMC The)Tj /P <>BDC ET EMC /P <>BDC /P <>BDC BT (152)Tj ET 6 0 0 6 444.4713 715.9528 Tm ( )Tj 0 Tc EMC ET BT BT EMC Aux fuel tank in aft hold of a BBJ2 (-800 fuselage). BT EMC /P <>BDC BT /P <>BDC /P <>BDC 9 0 0 9 215.4313 82.8898 Tm ET /P <>BDC 5.25 0 0 5.25 492.6848 11.5129 Tm /P <>BDC (0.0113)Tj ET [(CFM L)17.1(E)-8.1(AP-1A32)]TJ /P <>BDC 9 0 0 9 208.0289 632.8898 Tm ( )Tj (158)Tj ET 859 0 obj (Airlines, Delta and United. EMC ET (Top), Specification Table Boeing 737 Next Gen and Max.(Top). EMC ET ET /Figure <>BDC BT BT EMC EMC The design of the 737-800 lends itself to the sleek size and prowess of this aircraft. /P <>BDC /P <>BDC ET BT 9 0 0 9 53.8582 599.8898 Tm (the defined LRC speed, this has resulted in)Tj -.02 Tc unit, Open or short in BT EMC BT 0 Tc ET BT 0 Tc EMC 9 0 0 9 563.0415 775.8898 Tm EMC /P <>BDC BT BT 6.5 0 0 6.5 448.4585 702.9529 Tm /P <>BDC /P <>BDC ET (\(see table,)Tj EMC -.02 Tc ()Tj -.02 Tc ( )Tj 7 0 0 7 241.5317 287.9528 Tm /GS1 gs BT 9 0 0 9 215.4313 291.8898 Tm ( )Tj ET 7 0 0 7 355.3163 221.7654 Tm especially during start. /P <>BDC (6,303)Tj ET EMC BT EMC /P <>BDC ( )Tj 9 0 0 9 216.03 687.8898 Tm 7 0 0 7 187.0858 628.9528 Tm (23)Tj /GS2 gs EMC ET /P <>BDC ET BT BT /P <>BDC 7 0 0 7 187.0858 100.9528 Tm BT BT /P <>BDC 0 Tc ET 0 Tc BT EMC EMC EMC ( )Tj /P <>BDC BT EMC 0 Tc ( )Tj (124,650)Tj -.02 Tc (150)Tj 0 Tc 7 0 0 7 101.0963 210.9528 Tm /P <>BDC EMC /P <>BDC ET 7 0 0 7 279.1575 287.9528 Tm BT 8 0 0 8 365.7704 633.9528 Tm 9 0 0 9 232.4217 104.8898 Tm EMC Q -.02 Tc BT EMC ET ET EMC -.02 Tc BT 0 Tc ( )Tj 7 0 0 7 141.7322 133.9528 Tm ( )Tj ET 6.5 0 0 6.5 192.5726 722.9529 Tm ( )Tj (157)Tj /P <>BDC EMC ( )Tj EMC EMC ET (Under payload scenario 1, where the)Tj EMC BT EMC 7 0 0 7 387.0932 188.9528 Tm ( )Tj ET EMC BT BT EMC ET 6.5 0 0 6.5 182.0193 611.9529 Tm ( )Tj 0 Tc ET EMC EMC /P <>BDC EMC ET /P <>BDC ET /P <>BDC ET ET ET .014984 841.89 609.45 -841.89 re /P <>BDC ( )Tj ( )Tj EMC BT BT BT ( )Tj ( )Tj 9 0 0 9 394.0237 445.8898 Tm ET -.02 Tc [(OM)8.1(M)-12.9(E)-24.9(R)7.1(C)8.1(E)]TJ EMC 0 Tw BT 7 0 0 7 258.2805 331.7654 Tm BT /F4 1 Tf ET EMC 7 0 0 7 277.3936 265.9528 Tm EMC BT 9 0 0 9 229.6064 49.8898 Tm EMC ET BT 7 0 0 7 492.5963 639.7654 Tm ET /F4 1 Tf /P <>BDC BT EMC ( )Tj next aircraft ET )Tj 6 0 0 6 247.3662 673.9528 Tm ET EMC ET EMC ET ET /P <>BDC ( )Tj BT (ratio of 12.5:1; and the CFM LEAP-1A26)Tj 7 0 0 7 387.0159 595.9528 Tm 6 0 0 6 61.517 645.9528 Tm )Tj /P <>BDC ET 9 0 0 9 531.7939 104.8898 Tm EMC 8 0 0 8 153.6923 633.9528 Tm /P <>BDC EMC EMC BT 6.5 0 0 6.5 430.0114 565.9529 Tm EMC EMC ( )Tj ET 7 0 0 7 258.2805 144.7654 Tm (127)Tj BT (213)Tj BT /P <>BDC ET BT /P <>BDC BT What are the Boeing 787 Dreamliner Specs? (178)Tj ( )Tj EMC ET 9 0 0 9 246.6113 401.8898 Tm /P <>BDC ET EMC /Artifact <>BDC (5.7:1)Tj /P <>BDC /F4 1 Tf (performance )Tj EMC EMC /P <>BDC ( )Tj BT /P <>BDC /P <>BDC /P <>BDC endobj ET BT EMC ( )Tj The NGS is an onboard inert gas system that uses an EMC 7 0 0 7 355.3163 210.7654 Tm BT 8 0 0 8 542.9269 786.8898 Tm ( )Tj EMC ET /P <>BDC ET /P <>BDC ET BT BT 7 0 0 7 77.36 11.5132 Tm /P <>BDC ( )Tj EMC EMC EMC 6 0 0 6 238.0716 687.9528 Tm /GS2 gs 9 0 0 9 53.8578 104.8898 Tm /P <>BDC EMC ( )Tj EMC EMC /P <>BDC 7 0 0 7 473.8245 122.9528 Tm 0 Tc /P <>BDC EMC /P <>BDC BT EMC /P <>BDC ( )Tj 7 0 0 7 53.8582 11.5132 Tm -.02 Tc BT ET EMC BT /P <>BDC EMC /P <>BDC /P <>BDC ET ET (150)Tj /P <>BDC BT 9 0 0 9 215.4313 456.8898 Tm EMC (economy cabin, but some airlines can)Tj /P <>BDC /P <>BDC ET /P <>BDC BT ET 7 0 0 7 116.3631 11.5132 Tm BT BT /P <>BDC /P <>BDC 9 0 0 9 542.2986 192.8898 Tm 0 Tc ET EMC For the purposes of)Tj EMC BT EMC ET BT ( )Tj /P <>BDC BT ET ET 9 0 0 9 553.6047 423.8898 Tm EMC ET BT 9 0 0 9 232.4217 203.8898 Tm BT EMC -.02 Tc /P <>BDC ET /P <>BDC BT ( A)Tj ET EMC EMC ET /P <>BDC Supports 737-600, 737-700, 737-800 and 737-900. 7 0 0 7 277.3936 177.9528 Tm 7 0 0 7 383.0719 738.7654 Tm -.02 Tc /P <>BDC ( )Tj (lower than the difference on the smaller)Tj EMC EMC 0 Tc ( )Tj 7 0 0 7 124.1242 694.7654 Tm /OC /MC854 BDC -.02 Tc 8 0 0 8 539.8061 771.9528 Tm ET (388)Tj EMC 7 0 0 7 54.5916 639.7654 Tm EMC /P <>BDC ET EMC ( )Tj ET 9 0 0 9 547.562 126.8898 Tm BT (O)Tj ET ET BT (1,272)Tj /P <>BDC ( )Tj f BT 9 0 0 9 368.2867 357.8898 Tm (In the payload 2 scenario, the fuel burn)Tj 304.725 420.96 m EMC EMC [(CFM L)17.1(E)-8.1(AP-1A26)]TJ [(T)92(axi out time - mins)]TJ BT /P <>BDC Boeings main competitor is with Airbus. ( )Tj BT /F6 1 Tf ( N)Tj ET exacerbating the imbalance. ET ET 7 0 0 7 241.5317 408.9528 Tm ( )Tj ET (the 14 sectors with the 85% passenger)Tj 7 0 0 7 537.267 232.7654 Tm 6 0 0 6 403.4411 715.9528 Tm ( )Tj /P <>BDC W n 7 0 0 7 363.2711 562.9528 Tm -.02 Tc /P <>BDC 7 0 0 7 445.619 540.7654 Tm ( )Tj ET ( )Tj ET q 9 0 0 9 539.8684 280.8898 Tm (passengers on BOS-LAX, whereas the)Tj ET (2,800 -)Tj 7 0 0 7 491.4046 386.9528 Tm ( )Tj BT ET BT ET BT BT ( )Tj ET BT BT EMC 7 0 0 7 445.619 573.7654 Tm (travelled for the aircraft on each route is)Tj 7 0 0 7 379.3969 166.7654 Tm EMC /P <>BDC /GS2 gs (A321neo carry the same passenger)Tj BT EMC /P <>BDC ( )Tj 9 0 0 9 394.0315 126.8898 Tm BT BT (150)Tj EMC ET ( )Tj ( )Tj ( )Tj /F6 1 Tf BT 0 Tc BT /P <>BDC BT [(ar)-22.9(ticles like this, visit: )]TJ 9 0 0 9 411.0181 302.8898 Tm BT ET (157,300)Tj -.02 Tc ET ( )Tj BT ET /P <>BDC (/S)Tj EMC /P <>BDC ( )Tj BT BT /P <>BDC EMC EMC 7 0 0 7 354.6933 529.7654 Tm 7 0 0 7 187.0858 309.9528 Tm ET /P <>BDC /P <>BDC BT EMC ET ET 8 0 0 8 85.4269 760.9529 Tm /P <>BDC EMC 28.5749 0 TD EMC /P <>BDC /P <>BDC [(P)11(ayload)]TJ 6.5 0 0 6.5 500.4875 532.9529 Tm 7 0 0 7 387.0932 298.9528 Tm (163)Tj EMC EMC /P <>BDC 9 0 0 9 536.5664 269.8898 Tm ET EMC BT ET 7 0 0 7 403.478 617.7654 Tm ET Centre tank pumps ET The fuel tank was instrumented with gas sample tubing and thermocouples to BT /P <>BDC ( )Tj EMC /P <>BDC EMC 9 0 0 9 394.0315 500.8898 Tm /P <>BDC ET ET BT EMC 0 Tc (1,272)Tj ET ( )Tj ( )Tj ET ET (the aircraft types. -.01 Tc ( )Tj 9 0 0 9 181.0402 335.8898 Tm ( )Tj BT EMC BT ET ET /GS2 gs 0 Tc /P <>BDC /P <>BDC EMC ET ET BT /P <>BDC BT 7 0 0 7 520.6108 562.9528 Tm ( )Tj ( )Tj BT 0 Tc 9 0 0 9 369.4947 357.8898 Tm (104-112)Tj EMC (11,593)Tj 6.5 0 0 6.5 93.2476 702.9529 Tm (CFM56-5B3/P)Tj /P <>BDC /P <>BDC /P <>BDC ET /P <>BDC (831)Tj /P <>BDC -.02 Tc ET BT 10 0 0 10 43.6039 794.2914 Tm .559 .331 .619 rg (number of seats and ASMs will give an)Tj ET ET ET 7 0 0 7 403.478 562.7654 Tm 0 Tc EMC 7 0 0 7 535.5029 705.7654 Tm (improvement ranges from 17.4% to)Tj .023 .567 .626 rg BT EMC EMC 9 0 0 9 379.3098 269.8898 Tm EMC /P <>BDC ( )Tj -.02 Tc EMC 0 Tc ET ( )Tj /P <>BDC ET BT /P <>BDC EMC 7 0 0 7 386.4701 397.9528 Tm ET EMC BT -2.5295 -5.0573 -2.1058 -5.3146 -1.5527 -5.3151 c /P <>BDC EMC EMC ( )Tj ( A)Tj EMC 6 0 0 6 316.5908 771.9528 Tm BT /P <>BDC /P <>BDC BT EMC BT ( )Tj ( )Tj BT (passengers fewer than the A321ceo )Tj EMC /P <>BDC ET ET BT EMC EMC ET /P <>BDC ET /P <>BDC ET BT ( )Tj /P <>BDC The aircraft broke into 3 pieces after crashing. BT /P <>BDC /P <>BDC 9 0 0 9 178.8353 478.8898 Tm ( )Tj /P <>BDC BT EMC /P <>BDC 9 0 0 9 215.4313 170.8898 Tm -.01 Tc BT 9 0 0 9 215.4409 324.8898 Tm ( )Tj EMC ( )Tj ET (CFM56-5B4/P)Tj ET 0 Tc 7 0 0 7 440.3636 518.9528 Tm ET EMC (- USG)Tj BT EMC BT -.02 Tc automatically moved back to OFF after one minute. /P <>BDC ( )Tj (1,707)Tj BT EMC ET ET BT ( )Tj (The Sky interior means the MAX)Tj ET ( )Tj ET 9 0 0 9 394.0237 478.8898 Tm 7 0 0 7 37.6993 210.9528 Tm ET 7 0 0 7 321.6356 122.9528 Tm -.005 Tc ET The total tolerance for the FQIS system is based on a full tank. BT 9 0 0 9 394.0157 214.8898 Tm BT (65,552)Tj 7 0 0 7 554.7883 331.7654 Tm EMC (operating the 737 has increased its)Tj EMC ET ET The A320ceos are)Tj BT 9 0 0 9 411.0181 412.8898 Tm ET ET /P <>BDC BT ET ET 7 0 0 7 158.74 419.7654 Tm BT 9 0 0 9 544.5291 665.8898 Tm EMC EMC 9 0 0 9 165.0289 60.8898 Tm /P <>BDC BT 0 Tc /P <>BDC 9 0 0 9 140.333 313.8898 Tm EMC .023 .567 .626 RG BT 9 0 0 9 36.8504 291.8898 Tm ET ET ( )Tj /P <>BDC 7 0 0 7 490.5101 639.9528 Tm EMC /F7 1 Tf /P <>BDC .023 .567 .626 rg 7 0 0 7 247.7395 661.7654 Tm ET BT Each version in the 737 family fills a differ role. BT EMC EMC ET BT 9 0 0 9 195.6833 115.8898 Tm /P <>BDC [(O)7.1(W)-2(E/DO)7.1(W/seat - lbs)]TJ ET EMC /GS1 gs The)Tj ET EMC 7 0 0 7 141.7322 287.9528 Tm /P <>BDC ET BT -.02 Tc EMC 7 0 0 7 364.1531 463.9528 Tm (207,336)Tj BT BT EMC (39,270lbs)Tj ET 0 Tc /P <>BDC /P <>BDC BT /P <>BDC EMC BT /P <>BDC 6.5 0 0 6.5 549.8557 735.9529 Tm EMC ET BT 6 0 0 6 495.9463 771.9528 Tm BT 9 0 0 9 232.4217 445.8898 Tm 0 Tc ET EMC re-primed. BT BT ET ET ( )Tj ET 9 0 0 9 541.8752 775.8898 Tm 7 0 0 7 158.74 342.7654 Tm /P <>BDC 9 0 0 9 362.2746 489.8898 Tm BT /P <>BDC (404)Tj BT EMC EMC /P <>BDC ET BT ( )Tj EMC /P <>BDC /P <>BDC (371,416)Tj 7 0 0 7 386.4701 419.9528 Tm /P <>BDC (CFM56-5B4/P)Tj (5,279)Tj /P <>BDC EMC 9 0 0 9 371.6638 247.8898 Tm BT ( )Tj BT 9 0 0 9 53.8338 269.8898 Tm EMC EMC ( )Tj the 737 but will require up to six on the 747. ( )Tj EMC EMC 7 0 0 7 554.7883 133.7654 Tm (analysis are: an MTOW of 213,848lbs; an)Tj ( )Tj /P <>BDC ET 7 0 0 7 131.6494 78.7654 Tm BT ( )Tj ET ET 0 Tc /P <>BDC If anyone does, please feel free to share with us all. EMC BT (\(see)Tj BT BT ( )Tj EMC Its sales cant be matched. /P <>BDC BT /P <>BDC (and airframe modifications. ET BT ET /P <>BDC 0 Tc 7 0 0 7 403.478 727.7654 Tm BT ( )Tj /P <>BDC f *PUUqUef\r+vl BT EMC EMC Q /P <>BDC ET 7 0 0 7 490.8321 419.7654 Tm BT EMC /P <>BDC 6.5 0 0 6.5 499.1812 689.9529 Tm ( 2021)Tj 0 Tc EMC The engine option used in this)Tj BT ET (1,272)Tj BT 7 0 0 7 355.3163 67.7654 Tm ( )Tj EMC 7 0 0 7 490.8321 144.7654 Tm EMC /P <>BDC BT /P <>BDC EMC ET BT 0 Tc BT /P <>BDC EMC -.02 Tc EMC BT ET W n BT ET 0 Tc /P <>BDC [(E)-7.8(P)16.1(T)9(E)-13.9(MBE)-16.9(R)]TJ ET EMC ( )Tj 7 0 0 7 427.7291 166.9528 Tm 10 0 0 10 425.05 814.1973 Tm ET /P <>BDC BT Max. (referred to as premium, main cabin extra)Tj BT EMC EMC /P <>BDC (2,189)Tj -.02 Tc (operate with first, economy-plus and)Tj EMC ET -.02 Tc /P <>BDC 7 0 0 7 456.7412 661.7654 Tm 7 0 0 7 141.7322 221.9528 Tm decrease the oxygen content to a level where the air volume (ullage) will not EMC -.02 Tc ET /P <>BDC 0 Tc EMC 6 0 0 6 309.4021 729.9528 Tm BT BT EMC /P <>BDC 7 0 0 7 518.4953 408.9528 Tm BT BT /P <>BDC 9 0 0 9 464.9339 577.8898 Tm BT BT BT ET ET BT BT ET (are taxi fuel burn, flight fuel burn, the)Tj 9 0 0 9 202.1458 258.8898 Tm BT EMC 9 0 0 9 543.1342 192.8898 Tm 6.5 0 0 6.5 474.3939 663.9529 Tm EMC /P <>BDC ET EMC 0 Tc /P <>BDC (A320ceo)Tj BT /P <>BDC BT EMC /P <>BDC EMC -.02 Tc 6.5 0 0 6.5 448.8744 624.9529 Tm Compared with the -400 the -800 is 3.02m (9ft 9in) longer, taking typical two class seating from 146 to 162, while range is significantly increased. 7 0 0 7 279.1575 540.9528 Tm /P <>BDC /P <>BDC BT 6 0 0 6 277.7064 757.9528 Tm ET ET The Boeing 737-800 has a maximum fuel capacity of 6,875 gallons or 26,020 liters. ET EMC /P <>BDC 7 0 0 7 54.7071 617.7654 Tm 0 Tc EMC BT BT EMC ET EMC S 7 0 0 7 474.3564 562.9528 Tm 7 0 0 7 294.4014 166.7654 Tm /P <>BDC 9 0 0 9 53.8582 478.8898 Tm ET 6 0 0 6 339.6853 659.9528 Tm ET (and considered against the A320 current)Tj ( )Tj 0 Tc 8 0 0 8 187.3427 633.9528 Tm /P <>BDC /P <>BDC ET EMC ET /P <>BDC BT ( )Tj /P <>BDC EMC (offering: the 737NG with the CFM56-7B;)Tj BT BT EMC 5 0 0 5 92.725 11.5132 Tm EMC /P <>BDC 7 0 0 7 491.7142 89.7654 Tm BT BT 9 0 0 9 215.433 225.8898 Tm BT /P <>BDC BT /P <>BDC BT BT ET BT S BT BT 9 0 0 9 411.0181 38.8898 Tm ET 9 0 0 9 215.4409 357.8898 Tm /P <>BDC .023 .567 .626 rg (374-388)Tj 9 0 0 9 411.0097 302.8898 Tm ET ( )Tj 7 0 0 7 279.1575 595.9528 Tm ( )Tj ET EMC 7 0 0 7 99.8582 518.7654 Tm ET ET ET -.02 Tc 0 Tc ET (170)Tj ET (\(Miami\) sector, to 299 degrees on the)Tj 9 0 0 9 358.1891 434.8898 Tm ET [(CFM L)17.1(E)-8.1(AP-1A32)]TJ 7 0 0 7 141.7322 430.9528 Tm 9 0 0 9 563.4796 324.8898 Tm ET 9 0 0 9 550.4974 599.8898 Tm EMC /P <>BDC /P <>BDC EMC (performance on this sector is 2.19 cents per)Tj EMC BT BT 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 EMC ( )Tj (170)Tj ET https://www.markuspilot.com/download/BOEING%20737%20MEASUREMENTS.pdf, Perhaps you will build a cockpit and use it with the new Flight Sim 2020. /P <>BDC BT The world's largest commercial airplane the Antanov AN-225 can carry over 98,000Gal/375,000 liters of fuel compared to a Beechcraft 1900D commuter airplane which carries 665Gal/2,520 liters. BT BT 7 0 0 7 537.7804 265.9528 Tm BT ( )Tj ()Tj EMC (A321ceo:)Tj /P <>BDC EMC 7 0 0 7 326.2278 738.9528 Tm ( )Tj BT ET 7 0 0 7 554.7883 221.7654 Tm 5.25 0 0 5.25 465.7151 11.5129 Tm 8 0 0 8 38.4438 745.9528 Tm EMC 9 0 0 9 411.0097 126.8898 Tm 9 0 0 9 554.0057 566.8898 Tm /P <>BDC 0 Tc EMC /P <>BDC /P <>BDC NEA is produced in sufficient quantities, during most conditions, to 7 0 0 7 518.4953 441.9528 Tm ET ET ET ET EMC ( )Tj EMC battery bus but have a dedicated battery to ensure that there is always EMC ET 7 0 0 7 490.7815 166.9528 Tm /P <>BDC ( )Tj /P <>BDC ( )Tj /P <>BDC 9 0 0 9 554.9974 456.8898 Tm (176)Tj BT BT /P <>BDC BT /P <>BDC ( )Tj ( )Tj )21(The )]TJ ( )Tj EMC -.02 Tc BT EMC (4,514)Tj 7 0 0 7 187.0858 232.9528 Tm EMC ( )Tj BT EMC BT (350-365)Tj ( )Tj ( )Tj EMC 7 0 0 7 54.7071 573.7654 Tm 9 0 0 9 203.511 621.8898 Tm BT ET EMC EMC BT -.02 Tc ET /P <>BDC /GS2 gs ET ( )Tj ET 7 0 0 7 82.8504 342.9528 Tm ET /P <>BDC 9 0 0 9 232.4217 390.8898 Tm (US airspace can be congested near the)Tj (comparison of the performance of the eight)Tj ET (sectors, particularly the shorter ones,)Tj /P <>BDC ( The taxi-in and taxi-out times and)Tj /P <>BDC (27,000lbs, a fan diameter of 69 inches and)Tj endobj (would be no additional holding required,)Tj ET /P <>BDC /P <>BDC BT /P <>BDC (0.0119)Tj ET BT 7 0 0 7 379.3969 78.7654 Tm EMC ET EMC ET EMC BT -.02 Tc /P <>BDC EMC /P <>BDC -.02 Tc ( )Tj EMC /P <>BDC ET ET /P <>BDC /P <>BDC ET (152)Tj EMC (382,736)Tj (0.0134)Tj BT BT EMC ET Note: The gauges are still considered to be operating normally with ET EMC EMC BT /GS1 gs BT ET ( )Tj 9 0 0 9 103.7478 390.8898 Tm /F2 1 Tf EMC -.02 Tc ET /P <>BDC (performance deterioration factor added to)Tj 9 0 0 9 36.8504 467.8898 Tm 7 0 0 7 554.7883 661.7654 Tm the test, each gauge will display any error codes that they may have. 8 0 0 8 74.9636 577.9528 Tm EMC ( )Tj BT 7 0 0 7 279.1575 441.9528 Tm /P <>BDC ET /P <>BDC 7 0 0 7 258.2805 364.7654 Tm ( )Tj EMC ( )Tj ET EMC -.02 Tc BT ET EMC ET ET BT /P <>BDC EMC ET (\(see table,)Tj EMC BT 9 0 0 9 554.3696 269.8898 Tm (0.0137)Tj BT 0 Tc EMC BT BT EMC ( )Tj 9 0 0 9 361.1316 214.8898 Tm 7 0 0 7 279.1575 188.9528 Tm 7 0 0 7 344.1175 584.7654 Tm 0 Tc .559 .331 .619 rg BT ( )Tj (at 27,000lbs thrust compared to the)Tj )Tj ET /P <>BDC BT BT EMC ET (or comfort plus, depending on the airline. BT ET ( )Tj (150)Tj BT BT 7 0 0 7 381.1608 584.7654 Tm /P <>BDC BT ( )Tj BT ET 7 0 0 7 445.7203 11.5129 Tm (150)Tj EMC ET 7 0 0 7 362.3891 298.9528 Tm BT /P <>BDC 7 0 0 7 387.0159 661.9528 Tm BT ET ET /P <>BDC /P <>BDC 8 0 0 8 163.4218 771.9529 Tm 6.5 0 0 6.5 297.8076 558.9529 Tm 9 0 0 9 394.0237 412.8898 Tm 7 0 0 7 294.4014 727.7654 Tm ( )Tj EMC 7 0 0 7 125.6292 683.7654 Tm /P <>BDC EMC (0.0183)Tj (3,031)Tj 0 Tc The NGS requires no flight or ground crew action for normal system operation and is not dispatch critical. ET This airliner can hold either 162 first class seats, 175 business class or 189 economy seats in total. (configuration as the 737-900ER\(W\), but)Tj BT /P <>BDC /P <>BDC BT (486)Tj BT BT EMC ET ET /P <>BDC EMC 9 0 0 9 381.9109 456.8898 Tm BT ( )Tj ET -.01 Tc ET /P <>BDC ET EMC /P <>BDC /P <>BDC 7 0 0 7 54.7071 100.7654 Tm (CFM56-7B27B3)Tj 137 )Tj /P <>BDC ( )Tj (170)Tj ET ET ET BT EMC BT BT EMC /P <>BDC ( )Tj /P <>BDC BT BT ( )Tj BT 0 Tc ET /F1 1 Tf BT /P <>BDC EMC BT -.02 Tc 9 0 0 9 53.8578 280.8898 Tm BT )Tj ( )Tj EMC /P <>BDC ET EMC ( )Tj 8 0 0 8 43.6039 771.9528 Tm EMC BT 0 Tc 7 0 0 7 383.0719 705.7654 Tm ET 0 Tc BT 9 0 0 9 545.0725 434.8898 Tm BT EMC 9 0 0 9 553.4085 203.8898 Tm BT EMC EMC 7 0 0 7 258.2805 441.7654 Tm EMC -.02 Tc BT BT 7 0 0 7 445.619 364.7654 Tm /P <>BDC (3,850)Tj BT ET BT 7 0 0 7 101.0963 386.9528 Tm (0.0115)Tj (165)Tj 9 0 0 9 367.9911 71.8898 Tm EMC /P <>BDC /P <>BDC /P <>BDC <>/XObject<>/ExtGState<>/Properties<>>> 6.5 0 0 6.5 64.6596 585.9529 Tm BT EMC /P <>BDC 9 0 0 9 522.5613 38.8898 Tm BT 9 0 0 9 395.1859 258.8898 Tm BT /P <>BDC ET (CFM56-5B4/P)Tj -.02 Tc EMC (273,600)Tj /P <>BDC /P <>BDC (A320neo)Tj /P <>BDC BT 6 0 0 6 434.151 715.9528 Tm /P <>BDC 0 Tc /P <>BDC /P <>BDC /GS2 gs /P <>BDC EMC ET 6.5 0 0 6.5 64.6596 572.9529 Tm ( )Tj (all eight aircraft types. ( )Tj EMC (1.111)Tj x&o[v?vr&D6oi#9v I7JW\'18pLq2qN8hbeebfvlV7pr ET For ground It provides code tables for aerodromes, air operators including the world's major airlines and for ICAO and IATA codes for aircraft. 9 0 0 9 36.8504 181.8898 Tm BT -.02 Tc /P <>BDC /P <>BDC EMC ET 7 0 0 7 403.478 122.7654 Tm 7 0 0 7 247.7395 705.7654 Tm [(737-900E)-33(R)]TJ ( )Tj (737-8)Tj 7 0 0 7 537.7804 221.9528 Tm /P <>BDC ET EMC /P <>BDC /P <>BDC EMC EMC 7 0 0 7 99.8582 221.7654 Tm ET ET EMC 9 0 0 9 394.0315 610.8898 Tm BT EMC EMC ET EMC EMC EMC EMC ET (/S)Tj BT BT ET /P <>BDC ET 7 0 0 7 338.3085 364.9528 Tm -.02 Tc ET 9 0 0 9 173.6527 500.8898 Tm /P <>BDC (Block fuel)Tj 0 Tc ( )Tj ( )Tj 0 Tc BT ( )Tj 7 0 0 7 491.4046 100.9528 Tm ( )Tj 0 Tc EMC ET 7 0 0 7 314.6398 716.7654 Tm ET (1B engine as the 737-8. ET -.02 Tc ET ET BT ET EMC /P <>BDC ( )Tj /P <>BDC ET /P <>BDC /P <>BDC /P <>BDC EMC ( )Tj 7 0 0 7 187.0858 199.9528 Tm 7 0 0 7 427.7291 133.9528 Tm q 1 0 0 1 36.85 84.878 cm 0 0 m ET /P <>BDC 9 0 0 9 411.0097 357.8898 Tm ET ( )Tj )Tj ET /P <>BDC /P <>BDC BT BT 7 0 0 7 99.8582 738.7654 Tm /P <>BDC 7 0 0 7 384.8358 683.7654 Tm ET ET BT EMC /P <>BDC BT /P <>BDC ( )Tj 0 Tc 7 0 0 7 247.7395 177.7654 Tm (7B26)Tj ( )Tj Aux fuel control panel (Aft overhead panel). BT EMC /P <>BDC ET ( )Tj BT ET 9 0 0 9 425.183 346.8898 Tm ET /P <>BDC EMC ( )Tj 0 Tc BT 7 0 0 7 230.7317 320.9528 Tm 0 Tc (20)Tj BT 7 0 0 7 158.74 529.7654 Tm BT (141,270)Tj ( )Tj (483)Tj /P <>BDC /P <>BDC ET ET ET EMC /P <>BDC EMC 7 0 0 7 445.619 617.7654 Tm (O)Tj /P <>BDC /P <>BDC ( )Tj EMC /P <>BDC EMC S EMC ET EMC ( 2021)Tj 8 0 0 8 124.845 591.9528 Tm -.02 Tc 1 i BT 9 0 0 9 53.8578 390.8898 Tm ET EMC endobj ET (The A320neo has an average fuel burn)Tj 10 0 0 10 47.1144 814.1973 Tm /P <>BDC /P <>BDC BT EMC 9 0 0 9 232.4217 236.8898 Tm EMC (170)Tj (10)Tj /P <>BDC ( )Tj BT 0 Tc EMC ET For Example: (variants increases from 5.1:1 on the 737-)Tj EMC The New Midsized Airplane. EMC /P <>BDC ET EMC The A320neo in this study)Tj ET /P <>BDC 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. EMC 7 0 0 7 258.2805 716.7654 Tm ET ( )Tj )Tj ( )Tj 7 0 0 7 230.7317 518.9528 Tm 0 Tc /P <>BDC EMC /Artifact <>BDC ( )Tj 7 0 0 7 379.3969 67.7654 Tm 0 Tc Therefore, the Boeing 777-200 can carry 24,125 more gallons of fuel than the Boeing 737-800. 6 0 0 6 433.7979 771.9528 Tm -.02 Tc 7 0 0 7 473.4744 518.9528 Tm -.02 Tc )Tj ET (0.0112)Tj ( )Tj BT ( )Tj ET EMC BT (CFM56-7B26)Tj [(R)11(emaining car)13.9(go - lbs )]TJ /P <>BDC ( )Tj BT EMC ET BT (/S)Tj EMC BT 9 0 0 9 394.0157 511.8898 Tm ET 0 841.89 609.449 -841.89 re /P <>BDC EMC 8 0 0 8 43.6039 703.9528 Tm 7 0 0 7 241.5317 705.9528 Tm /P <>BDC EMC 19.843 0 l ET ET [(P)11(assenger payload - lbs )]TJ /P <>BDC EMC EMC EMC /P <>BDC ET 0 Tc BT ET EMC EMC 7 0 0 7 387.0932 232.9528 Tm BT -.02 Tc BT 9 0 0 9 569.5997 566.8898 Tm ( )Tj /GS2 gs ET ET BT ET EMC BT 7 0 0 7 337.6855 397.9528 Tm -.02 Tc EMC (737-800W)Tj BT (408)Tj BT BT BT ( )Tj /P <>BDC 7 0 0 7 344.1175 617.7654 Tm 7 0 0 7 141.7322 507.9528 Tm 9 0 0 9 394.0123 324.8898 Tm EMC [(D)12.9(A)-8.1(L/36)]TJ 9 0 0 9 198.2937 126.8898 Tm /P <>BDC 7 0 0 7 141.7322 177.9528 Tm /P <>BDC The B737-800SF Cargo Conversion consists of the installation of a 86x137 cargo door on the left side of the fuselage, and modification of the main deck to a Class E cargo compartment. EMC 6.5 0 0 6.5 296.4841 663.9529 Tm ( )Tj EMC EMC [(AIRL)8.1(INE & AIR)7.1(CRAF)-12.9(T)18.1( OPERA)56.9(T)-8.1(ION)-13.9(S)]TJ ET 0 Tc 7 0 0 7 241.5317 628.9528 Tm 0 Tc /P <>BDC (the CFM56-5B with thrust ratings of)Tj /P <>BDC 9 0 0 9 370.8228 302.8898 Tm EMC (equipped with the more fuel-efficient CFM)Tj /P <>BDC EMC /P <>BDC BT /F4 1 Tf ET (\(see table, this page\))Tj 7 0 0 7 108.6215 67.9528 Tm BT ( )Tj 7 0 0 7 259.1625 78.7654 Tm ( )Tj EMC EMC BT /P <>BDC 7 0 0 7 404.101 78.7654 Tm ET This maybe? ET EMC /P <>BDC BT BT 6 0 0 6 309.5222 701.9528 Tm -.02 Tc 7 0 0 7 130.1443 518.7654 Tm /P <>BDC ( )Tj BT BT BT EMC ET EMC BT ET /P <>BDC 0 Tc BT ET (831)Tj BT EMC BT BT 0 Tc /P <>BDC EMC BT ET BT /P <>BDC 7 0 0 7 37.6993 232.9528 Tm EMC 9 0 0 9 215.4409 148.8898 Tm 9 0 0 9 121.2888 38.8898 Tm EMC /P <>BDC ET -.02 Tc /P <>BDC ( )Tj ( )Tj ET EMC 7 0 0 7 294.4014 111.7654 Tm EMC (31,416)Tj /P <>BDC EMC EMC EMC -.02 Tc 6.5 0 0 6.5 221.9596 650.9529 Tm EMC ( )Tj 0 Tc 7 0 0 7 88.196 11.5129 Tm [(T)39.1(OL/57)]TJ 7 0 0 7 491.7142 364.7654 Tm EMC /P <>BDC BT EMC BT /P <>BDC 9 0 0 9 36.8504 390.8898 Tm 0 Tc ( )Tj EMC 9 0 0 9 36.8504 137.8898 Tm ( )Tj BT ET EMC BT ( )Tj EMC 6.5 0 0 6.5 191.8316 637.9529 Tm EMC /P <>BDC EMC ET EMC ( )Tj ET /P <>BDC ET EMC EMC 9 0 0 9 394.0237 170.8898 Tm [(SS)-9(U)8.1(E)]TJ EMC /P <>BDC /P <>BDC /P <>BDC EMC ( The flight rules )Tj 7 0 0 7 118.104 661.7654 Tm EMC BT Q BT /P <>BDC 7 0 0 7 354.6933 507.7654 Tm /F1 1 Tf EMC ( )Tj /P <>BDC /P <>BDC ET 0 Tc EMC 7 0 0 7 298.514 562.9528 Tm ET 0 Tc ET ET ET ET .964 .834 .406 rg EMC /P <>BDC /P <>BDC 9 0 0 9 229.6141 434.8898 Tm BT 0 Tc -.02 Tc 7 0 0 7 539.9176 11.5129 Tm 9 0 0 9 544.5056 302.8898 Tm EMC EMC BT 0 Tc EMC 9 0 0 9 547.3802 566.8898 Tm ( )Tj BT /F6 1 Tf ( N)Tj 0 Tc EMC EMC .41 .161 .508 RG ET 7 0 0 7 158.74 111.7654 Tm ET EMC /P <>BDC /P <>BDC EMC ET EMC BT ET /P <>BDC ET EMC 6.5 0 0 6.5 178.4573 722.9529 Tm EMC ( )Tj (0.0126)Tj EMC BT ET BT -.02 Tc EMC ET EMC 9 0 0 9 546.5092 577.8898 Tm BT (I)Tj 9 0 0 9 215.4409 434.8898 Tm ET /P <>BDC ET 7 0 0 7 241.5317 518.9528 Tm (1,668)Tj ET 0 Tc ET /P <>BDC EMC BT BT 9 0 0 9 53.8582 236.8898 Tm ( )Tj EMC ET (5,126)Tj EMC ET EMC ET 7 0 0 7 158.74 661.7654 Tm /P <>BDC EMC ET ( )Tj ET 9 0 0 9 394.0237 335.8898 Tm 6.5 0 0 6.5 448.8744 558.9529 Tm ( )Tj 7 0 0 7 537.7804 188.9528 Tm 7 0 0 7 54.7071 672.7654 Tm EMC (377,550)Tj EMC BT /P <>BDC EMC (sectors where a 170-passenger payload is)Tj /P <>BDC ET ( )Tj 7 0 0 7 258.2805 298.7654 Tm /P <>BDC Boeings 737-800 isnt called the most popular airliner for no reason. BT (payload 1 and payload 2 scenarios, the)Tj /P <>BDC ET 5 0 0 5 484.5872 11.5129 Tm /P <>BDC ( )Tj (163)Tj /OC /MC1974 BDC EMC EMC -.02 Tc ( )Tj 0 Tc 7 0 0 7 241.2727 276.9528 Tm EMC 7 0 0 7 204.0935 188.7654 Tm BT 0 Tc BT ( )Tj ET /P <>BDC EMC /P <>BDC BT ET ET ET /P <>BDC -.02 Tc EMC EMC EMC ET EMC 7 0 0 7 314.6398 518.7654 Tm BT 7 0 0 7 316.0679 133.7654 Tm 7 0 0 7 54.7071 111.7654 Tm /P <>BDC 9 0 0 9 232.4217 434.8898 Tm 7 0 0 7 386.4701 386.9528 Tm 7 0 0 7 279.1575 529.9528 Tm /P <>BDC /P <>BDC BT ET ET BT BT -.02 Tc /P <>BDC 9 0 0 9 53.8578 423.8898 Tm EMC 56 0 0 56 36.8606 562.1944 Tm -.02 Tc .023 .567 .626 rg ET BT -.02 Tc ET [(superior oper)10(ating performance. (payload, due to its higher seat capacity, of)Tj EMC /P <>BDC /P <>BDC 6.5 0 0 6.5 528.5291 689.9529 Tm -.01 Tc ( )Tj 7 0 0 7 294.4014 122.7654 Tm 9 0 0 9 163.2471 269.8898 Tm BT ET -.02 Tc 7 0 0 7 247.7395 474.7654 Tm /P <>BDC BT ET EMC ( )Tj /GS2 gs ET BT 10 0 0 10 312.5146 771.9528 Tm ( )Tj 9 0 0 9 383.9197 412.8898 Tm 7 0 0 7 445.619 529.7654 Tm BT (performance improvement over the)Tj ET (1,272)Tj 7 0 0 7 43.6039 540.9528 Tm ET EMC BT ET -.02 Tc 7 0 0 7 36.8504 749.9528 Tm 7 0 0 7 491.4046 188.9528 Tm 9 0 0 9 184.2804 148.8898 Tm /P <>BDC EMC q BT ET .559 .331 .619 rg /P <>BDC /P <>BDC 7 0 0 7 54.7071 694.7654 Tm ET EMC ET ( )Tj -.01 Tc 9 0 0 9 469.5781 577.8898 Tm 7 0 0 7 88.196 11.5129 Tm 7 0 0 7 338.6433 166.7654 Tm /P <>BDC 9 0 0 9 232.438 170.8898 Tm The average fuel)Tj /P <>BDC S ET EMC (largest operating costs for any aircraft)Tj BT BT 0 Tc ET ( )Tj 9 0 0 9 156.9898 269.8898 Tm EMC cumulative errors it is recommended that the wings are filled once every few EMC BT EMC ET ( )Tj ( )Tj EMC &6E'dtU7()euFVfvGWgw8HXhx9IYiy*:JZjz ? BT 7 0 0 7 508.4124 89.7654 Tm 9 0 0 9 189.8423 467.8898 Tm ( )Tj EMC EMC BT EMC As stated, this makes a fair)Tj /P <>BDC BT BT 6 0 0 6 554.8917 743.9528 Tm EMC EMC /Artifact <>BDC ( )Tj BT 9 0 0 9 531.8156 280.8898 Tm
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