ET ( )Tj /P <>BDC ( )Tj 7 0 0 7 554.7883 298.7654 Tm 7 0 0 7 193.1059 485.9528 Tm ET 9 0 0 9 531.902 467.8898 Tm 0 Tc 9 0 0 9 368.7299 346.8898 Tm /P <>BDC EMC (5,096)Tj BT -.02 Tc 9 0 0 9 211.8361 577.8898 Tm /P <>BDC -.02 Tc ( )Tj 10 0 0 10 425.05 814.1973 Tm (31,416lbs)Tj ( A)Tj /P <>BDC BT ET -.02 Tc ET 7 0 0 7 258.2805 727.7654 Tm BT BT 8 0 0 8 74.9636 717.9528 Tm 7 0 0 7 344.1175 595.7654 Tm 6 0 0 6 339.8239 673.9528 Tm EMC (977)Tj BT ET BT BT 9 0 0 9 53.8582 797.8898 Tm BT .023 .567 .626 rg BT ET /Artifact <>BDC BT BT (146,300)Tj 0 Tc (170)Tj [(S)8(eats)]TJ /P <>BDC ET /P <>BDC /P <>BDC /P <>BDC ( )Tj -.02 Tc EMC /P <>BDC (150)Tj /P <>BDC EMC /P <>BDC /P <>BDC ( )Tj 7 0 0 7 490.8321 265.7654 Tm /P <>BDC ET BT /F6 1 Tf BT Centre tank pumps should not be ET EMC 7 0 0 7 294.4014 419.7654 Tm ET -.02 Tc 9 0 0 9 229.6045 104.8898 Tm 7 0 0 7 71.6694 738.9528 Tm Do you have the estimated production material used for the 737 Next Gen? ET .151 .147 .15 rg EMC BT BT 7 0 0 7 491.4046 441.9528 Tm ET 7 0 0 7 363.2711 386.9528 Tm 9 0 0 9 408.1968 236.8898 Tm 8 0 0 8 365.7704 745.9528 Tm EMC 7 0 0 7 403.7368 705.7654 Tm EMC ET EMC (163 for the A321ceo & A321neo; and 152)Tj 7 0 0 7 82.2047 639.9528 Tm ET 0 Tc EMC ET EMC /P <>BDC ET BT ( )Tj Leaving a fuel pump on with a low pressure light 9 0 0 9 53.8582 192.8898 Tm BT /P <>BDC 9 0 0 9 232.438 192.8898 Tm 7 0 0 7 297.632 694.9528 Tm EMC BT ET BT EMC [(CFM L)17.1(E)-8.1(AP-1A26)]TJ 7 0 0 7 299.0601 408.9528 Tm EMC 9 0 0 9 570.805 49.8898 Tm /P <>BDC /P <>BDC BT /P <>BDC /P <>BDC /P <>BDC EMC EMC ( )Tj 7 0 0 7 59.2108 11.5129 Tm EMC EMC /P <>BDC 9 0 0 9 207.5518 588.8898 Tm BT BT /Artifact <>BDC ET ET ET BT ET (377,550)Tj BT (2,516)Tj BT 0 Tc EMC (improvement of 12.0% to 13.6% across)Tj 6 0 0 6 295.8268 673.9528 Tm ET (39,270)Tj EMC ET ( )Tj less heating from the smaller hydraulic system A. ET (283)Tj EMC [(737 M)-8.1(A)-24.9(X-8:)]TJ /F1 1 Tf /P <>BDC BT ET /P <>BDC /P <>BDC ( )Tj 8 0 0 8 105.6516 760.9528 Tm /P <>BDC 7 0 0 7 491.392 463.9528 Tm ET ET 6.5 0 0 6.5 500.4875 532.9529 Tm BT BT /P <>BDC BT For the purposes of)Tj ET 9 0 0 9 150.2504 434.8898 Tm ET BT ET BT ( )Tj 7 0 0 7 403.478 628.7654 Tm 9 0 0 9 215.433 93.8898 Tm 7 0 0 7 543.7693 11.5132 Tm [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ ET /P <>BDC 0 Tc EMC ET /P <>BDC EMC BT BT /P <>BDC /P <>BDC (CFM56-5B4/P)Tj ET BT EMC EMC 9 0 0 9 36.8504 280.8898 Tm /P <>BDC /P <>BDC (rules relating to the cruise altitudes and)Tj BT 9 0 0 9 75.3887 489.8898 Tm ( )Tj ET .151 .147 .15 rg /P <>BDC /P <>BDC EMC /P <>BDC 7 0 0 7 387.0159 617.9528 Tm ( )Tj /P <>BDC EMC 9 0 0 9 411.0181 346.8898 Tm The flight)Tj ( )Tj 0 Tc ET BT (170)Tj BT q EMC 0 Tc 6.5 0 0 6.5 346.9224 585.9529 Tm /P <>BDC /P <>BDC EMC 9 0 0 9 215.4409 247.8898 Tm BT /P <>BDC BT The classics have 5 dripsticks in each wing tank and none in the centre ( )Tj /P <>BDC EMC -.01 Tc 7 0 0 7 354.6933 474.7654 Tm BT EMC ( )Tj 7 0 0 7 82.8504 309.9528 Tm BT /P <>BDC BT 7 0 0 7 404.101 133.7654 Tm EMC BT ( )Tj ET ET /P <>BDC EMC (404)Tj /P <>BDC ET 0 Tc (11.0:1)Tj EMC /P <>BDC ET BT /P <>BDC ET BT EMC BT 7 0 0 7 487.0872 11.5129 Tm /P <>BDC -.02 Tc /P <>BDC EMC ET EMC EMC /P <>BDC 7 0 0 7 95.225 11.5132 Tm /P <>BDC BT q 1 0 0 1 36.85 425.878 cm 0 0 m /P <>BDC 0 Tc BT ET 9 0 0 9 525.2239 324.8898 Tm EMC BT /OC /MC860 BDC /P <>BDC BT ( )Tj /P <>BDC /P <>BDC -.02 Tc BT Hi. BT EMC ( )Tj 7 0 0 7 298.3957 430.9528 Tm ( )Tj BT /P <>BDC EMC (0.0183)Tj EMC EMC ET 7 0 0 7 241.5317 485.9528 Tm /P <>BDC EMC (136)Tj -.01 Tc /P <>BDC ET ET BT EMC 9 0 0 9 408.1854 60.8898 Tm (190,800)Tj ( )Tj ET Q ET /P <>BDC /P <>BDC ( )Tj BT BT BT /P <>BDC (603)Tj )Tj BT ET ( )Tj 6 0 0 6 153.0397 715.9528 Tm 6 0 0 6 308.6461 743.9528 Tm EMC -.02 Tc (1,272)Tj /P <>BDC /P <>BDC 9 0 0 9 53.8582 709.8898 Tm BT 9 0 0 9 184.4215 434.8898 Tm ET /P <>BDC 9 0 0 9 77.618 82.8898 Tm ET ( )Tj ET What was the Super Sonic Transport (SST) Concorde plane?? ET EMC (178)Tj ET 7 0 0 7 294.4014 727.7654 Tm 7 0 0 7 354.6933 408.7654 Tm ET EMC ( )Tj In the cargo configuration, The 737-700C can carry up to 18,780 kg (41,420 pounds) of cargo on eight . EMC (T)Tj 7 0 0 7 241.5317 111.9528 Tm EMC 9 0 0 9 204.06 742.8898 Tm 7 0 0 7 37.5838 441.9528 Tm /P <>BDC -.02 Tc 9 0 0 9 394.0315 456.8898 Tm EMC 7 0 0 7 294.4014 430.7654 Tm /P <>BDC /P <>BDC /P <>BDC /P <>BDC ( )Tj BT 7 0 0 7 474.3564 738.9528 Tm (\(see table, page 19\))Tj EMC ET ( )Tj ET 6.5 0 0 6.5 528.5291 676.9529 Tm EMC ( )Tj ET EMC -.02 Tc ET EMC 9 0 0 9 232.4217 511.8898 Tm -.02 Tc EMC EMC 5 0 0 5 484.5872 11.5129 Tm ( )Tj 0 Tc EMC /P <>BDC -.02 Tc /P <>BDC ET 0 Tw EMC 9 0 0 9 541.0405 621.8898 Tm ( )Tj ( )Tj EMC EMC S 9 0 0 9 36.8504 489.8898 Tm /P <>BDC 7 0 0 7 247.7395 441.7654 Tm /P <>BDC ( )Tj /P <>BDC (1,114)Tj /P <>BDC EMC /P <>BDC (CFM56-5B3/P)Tj EMC ET ( )Tj ET EMC 7 0 0 7 99.8582 595.7654 Tm BT /P <>BDC The payload weights for)Tj 9 0 0 9 232.4217 577.8898 Tm ET BT BT /P <>BDC EMC ET /P <>BDC ET ET /P <>BDC ET ET BT /P <>BDC ET EMC /P <>BDC EMC (5.7:1)Tj ( )Tj BT ET (7,390)Tj 13 0 0 13 215.433 137.8898 Tm BT ET ET -.02 Tc EMC ( )Tj BT ET (of 170 passengers, the A321neo burns an)Tj ( )Tj 0 Tc ET /P <>BDC /P <>BDC .008 Tc ET (A321neo)Tj (1,272)Tj ET BT ET BT /P <>BDC ( )Tj /F1 1 Tf EMC EMC 0 Tc 7 0 0 7 158.74 144.7654 Tm ( )Tj (CFM56-5B4/P)Tj /P <>BDC 7 0 0 7 508.2252 11.5129 Tm /P <>BDC ET 9 0 0 9 232.4217 412.8898 Tm BT 0 Tc /P <>BDC )Tj EMC /P <>BDC /P <>BDC 0 Tc 9 0 0 9 232.4217 478.8898 Tm BT (0.0120)Tj ( )Tj BT /P <>BDC ET ET BT EMC EMC EMC EMC BT /P <>BDC ( )Tj ET EMC Pisquali 19/05/2018 at 16:07 Reply. EMC EMC BT EMC 9 0 0 9 361.016 49.8898 Tm (31,416)Tj (31,416)Tj EMC BT BT /P <>BDC 7 0 0 7 279.1575 221.9528 Tm 7 0 0 7 125.6292 89.7654 Tm 0 Tc 9 0 0 9 548.2598 489.8898 Tm EMC EMC BT ET ( )Tj BT 9 0 0 9 411.0234 687.8898 Tm BT -.02 Tc (fuel burn evaluation compares the selected)Tj ET ET EMC 9 0 0 9 553.0217 93.8898 Tm 7 0 0 7 537.7804 243.9528 Tm /P <>BDC /P <>BDC Specification Table Boeing 737 Original and Boeing 737 Classic. /P <>BDC /P <>BDC /P <>BDC (flight levels. 0 Tc BT BT 7 0 0 7 491.4046 199.9528 Tm /P <>BDC ( )Tj ET /P <>BDC BT /P <>BDC /P <>BDC 0 Tc 7 0 0 7 278.2756 78.9528 Tm BT ET 7 0 0 7 321.6356 243.9528 Tm BT tank. ET -.02 Tc BT 6.5 0 0 6.5 539.6182 532.9529 Tm 9 0 0 9 384.8988 225.8898 Tm ET /P <>BDC /P <>BDC BT EMC BT ET 56 0 obj BT /P <>BDC /P <>BDC ET BT 7 0 0 7 316.0679 298.7654 Tm [(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 EMC /P <>BDC 9 0 0 9 544.921 225.8898 Tm 9 0 0 9 215.4409 137.8898 Tm ET (737-800W)Tj ET (1,800 - )Tj /P <>BDC (37,653lbs )Tj /F1 1 Tf BT EMC ET BT ( )Tj BT /F1 1 Tf ET /F7 1 Tf BT ( )Tj BT 9 0 0 9 394.0123 247.8898 Tm ET Q ET EMC 8 0 0 8 397.6498 771.9529 Tm ET EMC BT ET /F1 1 Tf 6 0 0 6 496.2633 701.9528 Tm /P <>BDC EMC 7 0 0 7 118.104 562.7654 Tm BT BT /P <>BDC EMC EMC 9 0 0 9 184.2244 203.8898 Tm /OC /MC2278 BDC ET ET /P <>BDC (158)Tj ET ET Q EMC 7 0 0 7 82.8504 430.9528 Tm 9 0 0 9 551.0194 588.8898 Tm BT BT 9 0 0 9 408.1889 192.8898 Tm ET 7 0 0 7 294.4014 243.7654 Tm EMC EMC ET (0.0115)Tj ( )Tj /P <>BDC 9 0 0 9 538.8793 368.8898 Tm -.02 Tc ( )Tj /P <>BDC BT /P <>BDC ( )Tj /P <>BDC 7 0 0 7 386.4701 386.9528 Tm ( )Tj /F6 1 Tf ET The 737-900ER's successor is set to be the MAX 10, which will have a maximum capacity of 230 passengers and can fly 3,300 nautical miles (narrowly beating its predecessor). BT automatically moved back to OFF after one minute. 7 0 0 7 337.6855 507.9528 Tm EMC ET ( )Tj /P <>BDC BT EMC /P <>BDC 9 0 0 9 252.9543 170.8898 Tm 7 0 0 7 387.0159 584.9528 Tm /P <>BDC 7 0 0 7 141.7322 111.9528 Tm ET BT EMC EMC 7 0 0 7 141.7322 562.9528 Tm BT ET ( )Tj BT )Tj -.02 Tc ET 7 0 0 7 99.8582 573.7654 Tm /F7 1 Tf ET BT 0 Tc 7 0 0 7 554.7883 276.7654 Tm BT /P <>BDC EMC /P <>BDC ( )Tj ET /P <>BDC (to in-flight service levels will increase seat)Tj EMC ( )Tj ( )Tj 9 0 0 9 206.8767 148.8898 Tm /P <>BDC 7 0 0 7 187.0858 628.9528 Tm /P <>BDC 0 Tc 9 0 0 9 185.7888 489.8898 Tm EMC /P <>BDC ET 7 0 0 7 445.619 573.7654 Tm /P <>BDC /P <>BDC EMC (total seat count for these two types. ( )Tj EMC EMC 9 0 0 9 543.5425 522.8898 Tm BT BT /Artifact <>BDC /P <>BDC BT /P <>BDC 9 0 0 9 172.0312 357.8898 Tm BT 0 Tc (scenario, the difference in fuel burn)Tj EMC /P <>BDC ET BT EMC (average for the month of June, and the)Tj document.getElementById( "ak_js_1" ).setAttribute( "value", ( new Date() ).getTime() ); Airbus A320 Introduction The very popular short haul airliner. EMC BT (1,272)Tj 9 0 0 9 394.0123 555.8898 Tm EMC BT 8 0 0 8 524.1105 760.9528 Tm /P <>BDC 0 Tc EMC EMC EMC (174,200)Tj /P <>BDC EMC ET BT EMC /P <>BDC The APU uses fuel from the number 1 tank. /P <>BDC BT ( )Tj ET EMC 0 Tc /P <>BDC BT /P <>BDC ET BT EMC support combustion. on 5 Nov 1990 have been destroyed on the ground due to explosions in the empty ET /P <>BDC (performance )Tj 7 0 0 7 338.6433 210.7654 Tm 7 0 0 7 474.3564 716.9528 Tm EMC System Description. EMC EMC 9 0 0 9 425.1913 93.8898 Tm /F6 1 Tf (Using the evaluation payloads of 170)Tj /P <>BDC EMC /P <>BDC 13 0 0 13 179.2927 71.8898 Tm 1 i BT ET -.02 Tc EMC ( )Tj ( )Tj The fuel flow indication is integrated over time to calculate the fuel used for each engine. 9 0 0 9 548.4937 71.8898 Tm BT BT 7 0 0 7 386.3929 683.9528 Tm /GS2 gs q 1 0 0 1 53.858 546.878 cm 0 0 m -.005 Tc (34,650)Tj BT 6 0 0 6 146.7028 743.9528 Tm EMC -.02 Tc BT (36,960)Tj 7 0 0 7 539.8962 628.9528 Tm 7 0 0 7 299.0601 331.9528 Tm BT BT EMC Over the nine)Tj BT BT ET 9 0 0 9 373.9277 478.8898 Tm /P <>BDC 9 0 0 9 51.0236 401.8898 Tm /P <>BDC (have won more than 5,600. ET ( )Tj ET 0 Tc f 7 0 0 7 54.7071 463.7654 Tm 56.25 0 0 56.25 36.8583 489.8898 Tm 6 0 0 6 143.5527 701.9528 Tm 9 0 0 9 411.0097 148.8898 Tm EMC -.02 Tc 7 0 0 7 82.8504 265.9528 Tm Any help would be greatly appreciated and thank you for all your work its extremely helpful! /P <>BDC 7 0 0 7 294.4014 474.7654 Tm EMC ET The cause of the accident was determined to be a malfunctioning left radar altimeter. ET 9 0 0 9 215.4313 170.8898 Tm -.02 Tc /P <>BDC EMC /P <>BDC ( )Tj ET ET ( )Tj BT EMC EMC EMC EMC /P <>BDC ( )Tj /P <>BDC ET ET BT 7 0 0 7 204.0935 232.7654 Tm ET ET 9 0 0 9 369.892 412.8898 Tm (mainline US carriers like Alaska, American)Tj 0 Tc (Engine)Tj ET 6.5 0 0 6.5 375.6529 689.9529 Tm /P <>BDC 9 0 0 9 53.8578 258.8898 Tm 7 0 0 7 456.2165 375.7654 Tm ET [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ BT EMC ET BT EMC 7 0 0 7 326.2278 518.9528 Tm -.02 Tc /P <>BDC EMC 13 0 0 13 355.5757 115.8898 Tm ET /P <>BDC 9 0 0 9 53.8338 82.8898 Tm EMC 9 0 0 9 535.0095 423.8898 Tm BT /P <>BDC 0 Tc EMC ET EMC /P <>BDC 8 0 0 8 60.6117 771.7654 Tm /P <>BDC 9 0 0 9 550.3666 247.8898 Tm ET The NG/MAX's have separate ENG VALVE CLOSED & SPAR VALVE CLOSED lights in -.02 Tc 9 0 0 9 36.8504 302.8898 Tm (16,170)Tj EMC .151 .147 .15 rg BT /P <>BDC /P <>BDC EMC ( )Tj )Tj ( )Tj 0 Tc The A321ceo is restricted on four)Tj BT BT ( )Tj /P <>BDC EMC ET 6 0 0 6 195.3167 715.9528 Tm 6.5 0 0 6.5 54.877 585.9529 Tm 0 Tc EMC BT 6 0 0 6 425.0715 687.9528 Tm 9 0 0 9 373.87 258.8898 Tm BT I am looking forward to your responses. /P <>BDC EMC /P <>BDC )Tj BT EMC -.005 Tc ET ET EMC -.02 Tc BT 9 0 0 9 348.0922 511.8898 Tm -.02 Tc (A320neo has no reduction in passenger)Tj ET /P <>BDC 9 0 0 9 36.8504 170.8898 Tm /P <>BDC 7 0 0 7 82.2047 661.9528 Tm (A320ceo)Tj ET BT EMC 7 0 0 7 258.2805 661.7654 Tm /P <>BDC EMC EMC /P <>BDC (34,650)Tj /P <>BDC (I)Tj ET EMC BT EMC BT ET BT ET 7 0 0 7 241.5317 584.9528 Tm /P <>BDC BT /P <>BDC ET BT /P <>BDC -.02 Tc ET (2,748)Tj ( )Tj 7 0 0 7 204.0935 606.7654 Tm ET [(CFM L)17.1(E)-8.1(AP-1B27)]TJ (by the CFM LEAP-1A26. 6 0 0 6 333.1569 743.9528 Tm EMC ( )Tj /P <>BDC 7 0 0 7 379.3969 309.7654 Tm EMC /P <>BDC 9 0 0 9 53.8582 786.8898 Tm BT ET ET /P <>BDC ET BT 8 0 0 8 124.845 633.9528 Tm BT 7 0 0 7 535.5029 496.7654 Tm 7 0 0 7 427.7291 309.9528 Tm BT 9 0 0 9 566.3417 423.8898 Tm (216,240)Tj /GS2 gs ( )Tj ET BT EMC ET (It was assumed that all flights would)Tj ( )Tj EMC ( )Tj BT EMC .023 .567 .626 rg ET /P <>BDC -.02 Tc ET BT BT BT ( )Tj EMC 8 0 0 8 394.0237 71.8898 Tm ET 7 0 0 7 543.7693 11.5132 Tm ET -.02 Tc BT EMC ET ET ( )Tj (-47)Tj /P <>BDC EMC EMC EMC EMC ( )Tj 9 0 0 9 36.8583 368.8898 Tm 0 Tc EMC BT ( )Tj ET 7 0 0 7 314.6398 463.7654 Tm (165)Tj ET ET /P <>BDC ET EMC ET (72% of the NG fleet in service. Q 377.677 0 0 271.254 -.32779 534.078 cm EMC ET EMC BT 8 0 0 8 38.4438 605.9528 Tm /P <>BDC BT /P <>BDC BT BT 0 Tc ET /P <>BDC EMC /P <>BDC EMC 9 0 0 9 394.0123 412.8898 Tm (have been optimised by the PPS flight)Tj BT ( )Tj /P <>BDC ET ET 9 0 0 9 386.2848 170.8898 Tm 7 0 0 7 507.7893 331.7654 Tm BT ET 7 0 0 7 316.0679 375.7654 Tm BT ( )Tj ET EMC ( )Tj 9 0 0 9 511.9579 335.8898 Tm 7 0 0 7 299.0601 100.9528 Tm As an Amazon Associate I earn from qualifying purchases. /P <>BDC (The cost index used is heavily)Tj ET EMC 13 0 0 13 177.4468 500.8898 Tm W* n ( )Tj EMC EMC - Smiths. 6 0 0 6 527.699 701.9528 Tm ET -.02 Tc /P <>BDC BT capacitors in the tanks with fuel acting as the dielectric. BT -.02 Tc EMC BT /P <>BDC upon how many tanks the customer has specified (max 12). ET EMC BT 7 0 0 7 535.5029 320.7654 Tm /P <>BDC 0 Tc EMC -.02 Tc /P <>BDC EMC /P <>BDC EMC /P <>BDC BT BT 0 Tc /P <>BDC (in engine cool-down times. BT BT EMC 13 0 0 13 319.14 445.8898 Tm BT /P <>BDC 9 0 0 9 536.1277 247.8898 Tm /P <>BDC EMC ET 9 0 0 9 394.0315 720.8898 Tm /P <>BDC 6 0 0 6 184.9964 757.9528 Tm ET ET (0.0109)Tj (170)Tj BT ( )Tj EMC /P <>BDC BT BT 7 0 0 7 338.3085 199.9528 Tm ET /P <>BDC /P <>BDC ET 9 0 0 9 53.8578 346.8898 Tm compensator BT ET ( )Tj -.02 Tc 9 0 0 9 53.8582 324.8898 Tm ET BT ( )Tj BT /P <>BDC 9 0 0 9 198.2937 126.8898 Tm ( )Tj EMC 0 Tc EMC 7 0 0 7 536.3849 364.7654 Tm EMC (37,653)Tj 7 0 0 7 536.3849 463.7654 Tm 9 0 0 9 379.0889 291.8898 Tm EMC /P <>BDC -.02 Tc ET ET ET BT 6.5 0 0 6.5 225.3721 637.9529 Tm EMC -.01 Tc BT /P <>BDC ( )Tj /P <>BDC ET 7 0 0 7 520.6108 738.9528 Tm ET BT /P <>BDC /P <>BDC (2,349)Tj /P <>BDC BT BT ( )Tj /P <>BDC BT EMC ( )Tj ( )Tj EMC BT BT /P <>BDC 0 841.89 609.449 -841.89 re .41 .161 .508 rg -.02 Tc 9 0 0 9 518.0203 170.8898 Tm 0 Tc /P <>BDC ( )Tj /P <>BDC ET BT EMC ET ET ET ET -.02 Tc /P <>BDC (4,329)Tj ET EMC BT 0 Tc BT 9 0 0 9 408.1968 324.8898 Tm /P <>BDC ET ET (900ER\(W\) due to the heavier payload. /P <>BDC BT EMC (1,581)Tj /P <>BDC EMC (0.0112)Tj BT /P <>BDC 6 0 0 6 184.072 659.9528 Tm 7 0 0 7 37.6993 408.9528 Tm Due to the aircraft types and)Tj (170)Tj /P <>BDC BT EMC -.02 Tc BT /P <>BDC EMC /P <>BDC /P <>BDC .151 .147 .15 rg BT BT /P <>BDC 0 Tc (39,270lbs)Tj EMC EMC BT ET EMC ET /P <>BDC /P <>BDC (0.0113)Tj /P <>BDC -.02 Tc ET 7 0 0 7 247.7395 661.7654 Tm ET (160)Tj BT EMC ( )Tj 19.847 0 l BT (table, page 19\))Tj 0 J 0 j .5 w 10 M [] 0 d -.02 Tc ET BT ET /P <>BDC -.02 Tc ( )Tj However, it was also shown that the dual venting configuration of some EMC ( )Tj EMC 7 0 0 7 469.2222 11.5129 Tm (146,550)Tj ET ( )Tj BT BT ( )Tj /P <>BDC 0 841.89 609.449 -841.89 re 7 0 0 7 196.5683 221.7654 Tm BT /P <>BDC ( )Tj ET /P <>BDC [(Y)-7.1(XX/104)]TJ ET EMC /P <>BDC 7 0 0 7 70.8101 243.9528 Tm 7 0 0 7 37.6993 199.9528 Tm BT 7 0 0 7 354.6933 386.7654 Tm ( )Tj -.02 Tc ET /P <>BDC ET ( )Tj 7 0 0 7 440.3636 474.9528 Tm 9 0 0 9 535.2501 522.8898 Tm EMC 7 0 0 7 107.1165 573.9528 Tm EMC BT 0 841.89 609.449 -841.89 re BT ET ( )Tj ( )Tj /P <>BDC ET (31,416)Tj ( )Tj EMC ET ET ( )Tj ( )Tj /P <>BDC ET BT -.02 Tc BT EMC /P <>BDC 7 0 0 7 539.8962 727.9528 Tm EMC 9 0 0 9 73.1083 511.8898 Tm (977)Tj 9 0 0 9 147.641 236.8898 Tm EMC EMC 7 0 0 7 507.7893 562.7654 Tm BT -.02 Tc ET ( )Tj BT /P <>BDC 9 0 0 9 555.1066 434.8898 Tm Is the same happening with the 737? EMC BT 7 0 0 7 37.6993 111.9528 Tm [(7)-33(3)8.1(7-800 & 7)-33(3)8.1(7-8 )]TJ -.02 Tc ET ET BT 9 0 0 9 215.4313 379.8898 Tm ET EMC 7 0 0 7 247.7395 430.7654 Tm (aircraft in terms of engine rating, operating)Tj 7 0 0 7 429.157 606.9528 Tm ET ET EMC 0 Tc BT BT EMC 0 Tc ET ET /P <>BDC /P <>BDC ET EMC 7 0 0 7 444.737 342.7654 Tm 7 0 0 7 508.2252 11.5129 Tm /P <>BDC BT ET 9 0 0 9 549.0056 412.8898 Tm EMC EMC EMC /P <>BDC 7 0 0 7 230.7317 287.9528 Tm -.02 Tc ( )Tj (be charged the same in operation for this)Tj (0.0149)Tj ET EMC ( )Tj ET 7 0 0 7 247.7395 584.7654 Tm BT EMC 9 0 0 9 377.4586 676.8898 Tm ET ( )Tj 9 0 0 9 394.0123 401.8898 Tm 7 0 0 7 354.4763 661.7654 Tm BT /P <>BDC /Artifact <>BDC BT ET EMC /P <>BDC (1,272)Tj /P <>BDC ET 9 0 0 9 370.6339 302.8898 Tm /P <>BDC BT 7 0 0 7 439.2087 375.9528 Tm My Dad was a captain and I am curious if he flew the Flt 800 aircraft or not. BT ( )Tj ( )Tj EMC 9 0 0 9 232.4217 269.8898 Tm ET BT /P <>BDC ( )Tj EMC 9 0 0 9 375.8752 258.8898 Tm each engine. ET BT (150)Tj ET ET ET 9 0 0 9 51.0236 115.8898 Tm /P <>BDC BT BT 7 0 0 7 82.8504 210.9528 Tm 7 0 0 7 37.0536 694.9528 Tm /OC /MC5095 BDC ET 6.5 0 0 6.5 296.2827 637.9529 Tm 6 0 0 6 365.7265 729.9528 Tm /P <>BDC EMC ( )Tj 7 0 0 7 141.7322 419.9528 Tm BT 9 0 0 9 212.1598 302.8898 Tm ( )Tj 0 Tc /P <>BDC /P <>BDC (-59)Tj /P <>BDC EMC /P <>BDC 7 0 0 7 404.101 276.7654 Tm ET EMC -.02 Tc BT ( )Tj EMC 6.5 0 0 6.5 54.877 715.9529 Tm (2,518)Tj /P <>BDC 9 0 0 9 68.3339 511.8898 Tm EMC ET /F1 1 Tf /F7 1 Tf -.02 Tc /P <>BDC ( )Tj EMC EMC BT ET ET ET BT (37,653)Tj ( )Tj 0 Tc ET BT BT EMC /P <>BDC EMC /P <>BDC BT ( )Tj ET BT ET ET EMC BT 7 0 0 7 37.6993 122.9528 Tm /P <>BDC ET /P <>BDC 0 Tc (31,416)Tj BT (because the 737-900 is limited to the same)Tj /P <>BDC (increase in seat numbers a newer type)Tj ( )Tj ET 7 0 0 7 439.2087 78.9528 Tm BT (capacity would further increase the)Tj 9 0 0 9 394.0123 489.8898 Tm 7 0 0 7 343.2355 463.7654 Tm BT BT EMC /P <>BDC ET EMC EMC (2,115)Tj ( )Tj EMC [(OM)8.1(M)-12.9(E)-24.9(R)7.1(C)8.1(E)]TJ ( )Tj EMC 0 Tc 8 0 0 8 243.3422 771.9529 Tm ( )Tj EMC ET /P <>BDC BT EMC Q /P <>BDC BT ET 7 0 0 7 457.0984 672.7654 Tm -.02 Tc BT ET ET 7 0 0 7 475.2383 672.9528 Tm EMC ET EMC FQIS accuracy: +/- 2.0% overall 9 0 0 9 68.0314 258.8898 Tm /P <>BDC ET ET ET 9 0 0 9 411.0097 104.8898 Tm 7 0 0 7 536.3849 408.7654 Tm ( )Tj EMC 7 0 0 7 82.2047 540.9528 Tm (136)Tj 9 0 0 9 191.0032 225.8898 Tm 7 0 0 7 204.0935 573.7654 Tm ( )Tj ET BT ( )Tj [(CFM L)17.1(E)-8.1(AP-1B27)]TJ /P <>BDC ET 9 0 0 9 51.0236 379.8898 Tm -.02 Tc 7 0 0 7 490.5101 606.9528 Tm ( )Tj EMC EMC -.01 Tc /P <>BDC EMC ET BT ( )Tj (CFM56-5B3/P)Tj /P <>BDC 9 0 0 9 215.4313 346.8898 Tm ( )Tj - Modern Airliners, Pingback:A New Opportunity For Hydrogen is Aviation Aeronautics, Pingback:A New Opportunity For Hydrogen is Aviation - Revolution-Green, Pingback:Southwest CEO Says It's Safe to Fly Again. /P <>BDC ET BT -.01 Tc EMC BT 0 Tc ( )Tj 0 Tc (is 0.01 to 0.15 cents better than the)Tj ( )Tj EMC EMC BT BT 0 Tc 9 0 0 9 232.4217 335.8898 Tm BT BT EMC (\(see table, page 19\))Tj ET /P <>BDC BT 7 0 0 7 459.6601 11.5129 Tm (342,312)Tj EMC ( )Tj .001 Tc BT ET ( )Tj /GS2 gs 7 0 0 7 343.2355 683.7654 Tm 9 0 0 9 36.8504 115.8898 Tm (3,300 -)Tj -.02 Tc -.02 Tc 0 Tc ( )Tj /F7 1 Tf (96,500)Tj -.02 Tc EMC ET BT EMC 5.25 0 0 5.25 447.6106 11.5129 Tm /P <>BDC 0 Tc EMC /P <>BDC 7 0 0 7 37.0536 529.9528 Tm BT /P <>BDC /P <>BDC /P <>BDC ET 0 Tc 6.5 0 0 6.5 182.0193 611.9529 Tm ET 6.5 0 0 6.5 280.3794 722.9529 Tm /P <>BDC /P <>BDC /P <>BDC EMC EMC ( )Tj EMC BT EMC ET BT ET (2,481)Tj EMC 9 0 0 9 411.0097 269.8898 Tm ( )Tj EMC 7 0 0 7 36.8504 749.9528 Tm (156)Tj ( )Tj 7 0 0 7 179.5605 419.9528 Tm /P <>BDC ET EMC 9 0 0 9 213.7241 467.8898 Tm EMC BT ET 7 0 0 7 141.7322 166.9528 Tm ET /P <>BDC 0 Tc EMC /P <>BDC /P <>BDC ET 9 0 0 9 394.0237 456.8898 Tm BT (operating performance of the more)Tj /P <>BDC 7 0 0 7 230.7317 166.9528 Tm /P <>BDC What is the History behind the Airbus A380 Super Jumbo? ET (0.0146)Tj ( )Tj EMC (166,090)Tj /P <>BDC /P <>BDC /P <>BDC /P <>BDC 7 0 0 7 354.6933 199.7654 Tm EMC EMC ( )Tj (4,000)Tj /P <>BDC EMC (A320neo)Tj EMC EMC ET concentration at eight different locations. EMC (150)Tj /P <>BDC 0 Tc BT ET ( )Tj /P <>BDC (39,270)Tj -.02 Tc 0 Tc ET EMC )21(The r)10(elativ)12.9(e)]TJ EMC BT f /P <>BDC EMC EMC EMC (powered by either the CFM56-5 series or)Tj BT )Tj 9 0 0 9 346.8148 104.8898 Tm warmer air or accelerate to increase the kinetic heating. 6.5 0 0 6.5 448.257 637.9529 Tm BT ( )Tj BT 9 0 0 9 394.0237 379.8898 Tm 6 0 0 6 339.6853 659.9528 Tm /P <>BDC EMC BT -.02 Tc 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. ET EMC [(CFM L)17.1(E)-8.1(AP-1A26)]TJ ET EMC (34,650)Tj BT ET EMC ( )Tj ( )Tj ( )Tj 9 0 0 9 411.0234 709.8898 Tm ET EMC EMC ET 9 0 0 9 439.4008 324.8898 Tm -.02 Tc 9 0 0 9 53.8578 214.8898 Tm The three-)Tj EMC BT 9 0 0 9 351.8271 203.8898 Tm ( )Tj ( )Tj (The sectors are chosen to ensure a)Tj (l)Tj EMC ET ET 0 Tc 9 0 0 9 36.8504 225.8898 Tm /P <>BDC BT [(Summar)-33(y )]TJ /P <>BDC EMC EMC 7 0 0 7 101.0963 111.9528 Tm 9 0 0 9 51.0236 401.8898 Tm BT ( )Tj ET 137 )Tj ( )Tj BT BT /P <>BDC Well, the fuel capacity of this airplane varies depending on the specific model and generation. BT ET -.01 Tc 9 0 0 9 372.2467 170.8898 Tm BT 0 Tc 6.5 0 0 6.5 448.7448 742.9529 Tm ( )Tj ( )Tj BT ET ET ( )Tj /P <>BDC (2,517)Tj ( )Tj EMC /P <>BDC EMC ( )Tj /P <>BDC ET ET -.02 Tc ET EMC Thanks. 0 J 0 j 5 w 10 M [] 0 d EMC EMC 7 0 0 7 539.8962 485.9528 Tm (482)Tj (136)Tj 7 0 0 7 554.7883 430.7654 Tm /P <>BDC -.02 Tc EMC 9 0 0 9 347.4891 203.8898 Tm BT -.02 Tc EMC 7 0 0 7 554.7883 529.7654 Tm ET 7 0 0 7 277.3936 265.9528 Tm BT BT ET (A320neos 7,000lbs higher MTOW. (310,080)Tj BT BT 6 0 0 6 237.4295 701.9528 Tm EMC .151 .147 .15 rg 7 0 0 7 294.4014 507.7654 Tm 9 0 0 9 523.7694 214.8898 Tm 9 0 0 9 204.5367 93.8898 Tm [(M)21(T)39.1(O)7.1(W)0( / seat - lbs )]TJ 858 0 obj /P <>BDC 7 0 0 7 521.4089 11.5132 Tm ( )Tj /P <>BDC BT BT BT -.02 Tc 6.5 0 0 6.5 296.4841 689.9529 Tm EMC ET ET -.01 Tc /P <>BDC 9 0 0 9 392.8568 599.8898 Tm ET BT /P <>BDC -.02 Tc BT 9 0 0 9 229.6064 390.8898 Tm /P <>BDC ET 7 0 0 7 403.478 419.7654 Tm My simulation is focused on postcrash fires. ET BT BT BT /P <>BDC /P <>BDC ET 7 0 0 7 37.6993 100.9528 Tm /P <>BDC /P <>BDC EMC BT -.02 Tc /P <>BDC BT 0 Tc ET 7 0 0 7 321.6356 188.9528 Tm ET BT /P <>BDC y9ou may find what you are looking for by clicking here. ET EMC BT 7 0 0 7 54.7071 408.7654 Tm 7 0 0 7 258.2805 518.7654 Tm ET EMC ET ET /P <>BDC BT /P <>BDC BT /P <>BDC /P <>BDC ET ( )Tj EMC EMC ( )Tj ( )Tj BT BT -.02 Tc /P <>BDC 9 0 0 9 53.8578 478.8898 Tm [(v)21(ariant)]TJ BT /P <>BDC 8 0 0 8 53.9012 749.9529 Tm ET 9 0 0 9 336.3455 313.8898 Tm BT /P <>BDC (achieved more than 6,000 orders for the)Tj ET EMC /P <>BDC /P <>BDC (114)Tj 6 0 0 6 176.4941 687.9528 Tm /P <>BDC /P <>BDC (977)Tj 8 0 0 8 225.1837 717.9528 Tm EMC 13 0 0 13 118.3688 390.8898 Tm what we have done is sourced a document that gives the various dimensions of a 737 cockpit with which you should be able to find your desired outcome. -.02 Tc 9 0 0 9 518.5923 511.8898 Tm BT 0 Tc EMC EMC 9 0 0 9 166.1068 313.8898 Tm 7 0 0 7 537.7804 397.9528 Tm The fuel was fed -.01 Tc ET EMC ET /P <>BDC q 1 0 0 1 508.103 86.641 cm 0 0 m This fuel would give a /GS2 gs BT EMC 0 Tc /P <>BDC -.02 Tc 36.85 824.882 572.599 17.008 re BT EMC 0 Tc EMC BT 0 Tc EMC EMC BT EMC /P <>BDC 7 0 0 7 279.1575 606.9528 Tm ET /P <>BDC EMC 9 0 0 9 550.8776 170.8898 Tm /F6 1 Tf ET /P <>BDC ET 7 0 0 7 403.478 738.7654 Tm /P <>BDC EMC 7 0 0 7 338.6433 188.7654 Tm 9 0 0 9 53.8338 313.8898 Tm EMC 6 0 0 6 195.3167 757.9528 Tm BT ET 9 0 0 9 345.8168 445.8898 Tm BT 6 0 0 6 496.2633 673.9528 Tm /P <>BDC 7 0 0 7 279.1575 419.9528 Tm -.02 Tc BT /OC /MC208 BDC ( )Tj EMC /P <>BDC (1,275)Tj EMC BT /P <>BDC BT 0 Tc /P <>BDC ET EMC (capacity on the later aircraft models and)Tj (payload reduction. BT ET /P <>BDC 7 0 0 7 338.6433 331.7654 Tm 9 0 0 9 553.7373 225.8898 Tm /P <>BDC (136)Tj ET BT BT ( )Tj /P <>BDC 9 0 0 9 508.4714 38.8898 Tm /P <>BDC 0 Tc BT 7 0 0 7 230.7317 496.9528 Tm ( )Tj /P <>BDC ET ET From July 2004 NGs have been delivered with markings on the
