ET 0 Tw BT /P <>BDC /P <>BDC (0.0137)Tj ET BT EMC q (CFM LEAP-1B28B1 rated at 28,000lbs)Tj BT ET 6.5 0 0 6.5 232.6392 735.9529 Tm 7 0 0 7 316.0679 232.7654 Tm ET 9 0 0 9 394.0237 401.8898 Tm ET EMC 7 0 0 7 518.4953 320.9528 Tm hi! /P <>BDC allowed for deposit of the ground-based NEA into the center wing tank (CWT). BT BT endstream .014984 841.89 609.45 -841.89 re ET ET -.02 Tc /P <>BDC BT BT EMC 6.5 0 0 6.5 181.2003 532.9529 Tm /P <>BDC (Under payload scenario 1, where the)Tj BT 0 Tc EMC ET ET (170)Tj /P <>BDC EMC EMC ET EMC BT /P <>BDC safest way forward, but is very expensive and possibly impractical. 9 0 0 9 372.3347 412.8898 Tm ( )Tj /P <>BDC BT 9 0 0 9 543.4875 456.8898 Tm /P <>BDC Main tanks < 50%, -1 to 5 deg pitch, +/- 1 deg roll: +/- 2.0 9 0 0 9 53.8582 324.8898 Tm /GS2 gs ET ( )Tj BT EMC ET ET (\(see table, page 21\))Tj The FILTER BYPASS BT )Tj BT -.02 Tc EMC ( )Tj ET 7 0 0 7 53.8582 551.7654 Tm ET /F6 1 Tf ET BT ET /P <>BDC ( )Tj /P <>BDC 9 0 0 9 211.8218 533.8898 Tm BT Cheers Peter. 7 0 0 7 490.5101 639.9528 Tm 0 Tw (10)Tj BT (distance flown increases, the fuel burn)Tj 10 0 0 10 407.41 814.1973 Tm ET /P <>BDC -.02 Tc /P <>BDC /P <>BDC -.02 Tc 7 0 0 7 187.5417 430.9528 Tm 7 0 0 7 490.8321 397.7654 Tm -.02 Tc BT BT /P <>BDC BT .151 .147 .15 rg ET EMC EMC /P <>BDC 7 0 0 7 365.035 628.9528 Tm ( )Tj EMC BT 9 0 0 9 375.9258 49.8898 Tm EMC /GS2 gs BT EMC [(BOS-SE)-13.9(A)]TJ ET ( )Tj BT 9 0 0 9 394.0237 467.8898 Tm EMC 378 0 0 271.8 -.30716 30.902 cm BT EMC 9 0 0 9 505.9653 115.8898 Tm BT -.02 Tc BT ( )Tj 7 0 0 7 321.6356 298.9528 Tm /P <>BDC ET [(F)11(uel capacity - U)-8.1(S)0(G)]TJ ET -.01 Tc BT cell which attached to the seat tracks of the passenger cabin. BT /P <>BDC EMC f /P <>BDC BT ET /P <>BDC BT 9 0 0 9 184.2804 148.8898 Tm 9 0 0 9 229.6141 302.8898 Tm EMC ( )Tj BT BT BT EMC ET ET ( )Tj ( )Tj BT EMC ET It sounds like you have a bit of a project on your hands. 137 )Tj 9 0 0 9 215.4313 71.8898 Tm EMC 7 0 0 7 490.8321 540.7654 Tm 0 Tc EMC .014984 841.89 609.45 -841.89 re ET /P <>BDC 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 BT BT EMC ET 7 0 0 7 67.798 11.5132 Tm 7 0 0 7 82.2047 705.9528 Tm BT 9 0 0 9 542.4332 335.8898 Tm -.02 Tc ET -.02 Tc ET 7 0 0 7 457.0984 67.7654 Tm EMC ( )Tj ( )Tj )Tj ET EMC 7 0 0 7 230.7317 474.9528 Tm BT 7 0 0 7 118.104 67.7654 Tm /P <>BDC -.02 Tc /P <>BDC BT ET 9 0 0 9 36.8504 357.8898 Tm BT EMC .151 .147 .15 rg ET /P <>BDC 7 0 0 7 113.1366 320.9528 Tm BT 0 Tc (CFM56-5B3/P)Tj EMC /P <>BDC (166,090)Tj -.005 Tc 9 0 0 9 232.4217 357.8898 Tm ET 7 0 0 7 445.619 628.7654 Tm 0 Tc /P <>BDC EMC /GS2 gs ET EMC BT /GS2 gs /F6 1 Tf /P <>BDC 9 0 0 9 194.7833 236.8898 Tm (2,745)Tj /P <>BDC BT EMC /P <>BDC ( )Tj EMC /P <>BDC EMC EMC EMC -.02 Tc /P <>BDC /P <>BDC ET BT -.02 Tc 7 0 0 7 508.4124 397.7654 Tm ET BT EMC 9 0 0 9 198.5183 445.8898 Tm 680kg; All other series: 453kg, Main tanks to be full if centre contains over 453kg, If a fuel gauge is u/s the quantity 9 0 0 9 411.0097 434.8898 Tm ET 7 0 0 7 439.1464 430.9528 Tm 9 0 0 9 53.8582 489.8898 Tm -.02 Tc 10 0 0 10 49.2604 814.1973 Tm ET ET /P <>BDC EMC /P <>BDC W n 7 0 0 7 247.7395 232.7654 Tm ( )Tj /P <>BDC EMC 6 0 0 6 527.3389 687.9528 Tm (163)Tj 7 0 0 7 427.7291 276.9528 Tm ET -.02 Tc /P <>BDC /F6 1 Tf ET /P <>BDC BT 6.5 0 0 6.5 296.3931 532.9529 Tm BT (table, page 19\))Tj ET /P <>BDC 7 0 0 7 338.3085 265.9528 Tm ET BT ( )Tj )21(This ar)-23(ticle)]TJ )]TJ ( )Tj (heavier than the A320ceo. EMC ( )Tj 8 0 0 8 187.3427 633.9528 Tm 8 0 0 8 296.665 771.9529 Tm /P <>BDC 0 Tc /P <>BDC EMC .023 .567 .626 rg EMC 9 0 0 9 232.4217 214.8898 Tm /P <>BDC /P <>BDC ET BT EMC BT EMC /P <>BDC 8 0 0 8 225.1837 619.9528 Tm EMC 7 0 0 7 535.5029 540.7654 Tm ET ET BT EMC /P <>BDC EMC (344-358)Tj EMC EMC 6.5 0 0 6.5 176.9362 545.9529 Tm ( )Tj ( )Tj 7 0 0 7 99.8582 408.7654 Tm EMC /P <>BDC BT 6 0 0 6 132.3631 659.9528 Tm BT EMC 9 0 0 9 548.1057 610.8898 Tm Bombardier CRJ 700/CRJ 900/CRJ 1000 Series. 9 0 0 9 394.0157 368.8898 Tm 7 0 0 7 355.3163 122.7654 Tm ET 788 0 obj EMC 7 0 0 7 99.8582 287.7654 Tm 6.5 0 0 6.5 112.0328 637.9529 Tm BT ( )Tj EMC 19.841 0 l EMC BT ET (2,517)Tj ET BT ( )Tj 7 0 0 7 54.7071 100.7654 Tm 7 0 0 7 507.7893 331.7654 Tm /GS1 gs /P <>BDC /P <>BDC /P <>BDC BT ET 6.5 0 0 6.5 484.6315 545.9529 Tm -.02 Tc (economy cabin, but some airlines can)Tj EMC 9 0 0 9 379.0889 291.8898 Tm ET ET 6.5 0 0 6.5 64.6596 558.9529 Tm (1,945)Tj EMC (379)Tj 0 Tc 9 0 0 9 411.0097 555.8898 Tm EMC BT /P <>BDC 0 Tc (132,872)Tj /P <>BDC BT /P <>BDC BT /P <>BDC BT EMC EMC ( )Tj (shorter sectors. (aircraft in terms of engine rating, operating)Tj (equal basis, since the number of seats will)Tj (65,552)Tj BT 7 0 0 7 380.2788 507.7654 Tm ( )Tj ET BT 9 0 0 9 411.0097 423.8898 Tm 0 Tc (cabin interior enhancements and changes)Tj EMC . /P <>BDC BT ET ( )Tj ET ( )Tj BT EMC /P <>BDC ET (total cost for fuel burn, time-related costs,)Tj 0 Tc BT 0 Tc /P <>BDC ET EMC 0 Tc /P <>BDC ET EMC EMC (1,668)Tj BT -.005 Tc EMC ET EMC (1,272)Tj /P <>BDC /P <>BDC ET ( )Tj EMC BT ET EMC /P <>BDC .41 .161 .508 RG ( )Tj BT BT 9 0 0 9 391.7137 104.8898 Tm ET 7 0 0 7 314.6398 738.7654 Tm 7 0 0 7 321.6356 199.9528 Tm BT 7 0 0 7 386.3929 705.9528 Tm ( )Tj EMC ET 7 0 0 7 182.5706 639.9528 Tm ( )Tj 9 0 0 9 194.061 324.8898 Tm ( )Tj BT BT ET BT BT (190-199)Tj EMC /P <>BDC /P <>BDC ET ET ET BT 137 )Tj EMC BT ET BT BT 0 Tc /P <>BDC ET 7 0 0 7 82.2047 496.9528 Tm /P <>BDC ( )Tj 7 0 0 7 490.5101 529.9528 Tm error codes 1, 3, 5 or 7 /P <>BDC 0 841.89 609.449 -841.89 re These carriers)Tj EMC BT EMC /P <>BDC -.02 Tc EMC ( )Tj (ratio of 5.1:1. EMC /P <>BDC Since development and production Boeing has built 10,574 737-800s. (. 7 0 0 7 230.7317 397.9528 Tm )Tj EMC EMC BT 7 0 0 7 279.1575 694.9528 Tm /P <>BDC EMC /P <>BDC /P <>BDC BT EMC 7 0 0 7 445.619 375.7654 Tm EMC ET EMC EMC ( )Tj EMC ( )Tj EMC /P <>BDC EMC ( )Tj ET ET /P <>BDC 9 0 0 9 371.6638 247.8898 Tm BT EMC /GS1 gs 9 0 0 9 197.3752 357.8898 Tm 7 0 0 7 258.2805 221.7654 Tm 0 Tc 9 0 0 9 374.3633 401.8898 Tm 9 0 0 9 571.3269 38.8898 Tm ET /P <>BDC /P <>BDC 8 0 0 8 339.6345 760.7654 Tm (financing. BT (136)Tj 7 0 0 7 258.2805 331.7654 Tm ET ( )Tj EMC ET Cheers Peter. EMC 6 0 0 6 333.9129 729.9528 Tm 7 0 0 7 54.7071 496.7654 Tm ET ( )Tj ET ( )Tj EMC ( )Tj 7 0 0 7 158.74 133.7654 Tm BT BT /P <>BDC 7 0 0 7 387.0932 144.9528 Tm BT 9 0 0 9 229.6141 390.8898 Tm EMC BT 5.25 0 0 5.25 55.7484 11.5132 Tm (A321ceo)Tj BT 9 0 0 9 544.9208 280.8898 Tm 9 0 0 9 368.7299 346.8898 Tm /P <>BDC ET BT EMC [(SS)-9.1(U)8(E)]TJ /P <>BDC 9 0 0 9 208.354 291.8898 Tm ET 0 Tc EMC EMC (7,390)Tj -.02 Tc BT ET 7 0 0 7 321.6356 100.9528 Tm BT 0 J 0 j 5 w 10 M [] 0 d ET EMC 9 0 0 9 215.4409 423.8898 Tm BT EMC )Tj BT ET BT BT 9 0 0 9 215.4313 159.8898 Tm 0 Tc 7 0 0 7 366.0641 661.9528 Tm /P <>BDC 7 0 0 7 193.1059 287.9528 Tm BT ET BT /P <>BDC EMC 7 0 0 7 404.101 320.7654 Tm /GS2 gs EMC EMC 0 Tc S /P <>BDC /F4 1 Tf -.01 Tc 0 Tc 6 0 0 6 412.5551 659.9528 Tm ET BT /P <>BDC (404)Tj -.02 Tc ET (1A26-powered aircraft that is used in this)Tj EMC 0 Tc /P <>BDC EMC (payload, the A321neo has an 18.9%)Tj BT /P <>BDC EMC EMC /P <>BDC ET -.01 Tc /P <>BDC EMC EMC ( )Tj BT ET Hi Anna-Maria, /P <>BDC EMC /P <>BDC 6 0 0 6 143.5527 701.9528 Tm (170)Tj ET 6.5 0 0 6.5 480.4 637.9529 Tm EMC ( )Tj /P <>BDC (955)Tj EMC BT /F6 1 Tf BT EMC 7 0 0 7 299.0601 221.9528 Tm /P <>BDC 17 0 0 17 560.3929 742.1944 Tm EMC 7 0 0 7 158.74 331.7654 Tm BT The weight increase in)Tj 0 Tc BT 0 Tc EMC BT -.02 Tc BT 5 0 0 5 92.725 11.5132 Tm ( )Tj BT /F1 1 Tf 7 0 0 7 82.2047 672.9528 Tm ( )Tj /P <>BDC /P <>BDC ET ET EMC ET 0 Tc [(A3)24.9(21neo v)12.9(ersus 7)-33(3)8.1(7-9 )]TJ EMC must be determined by using the dripsticks (floatsticks (2,732)Tj EMC ET 0 Tc EMC 8 0 0 8 85.4842 745.9528 Tm BT (capacity would further increase the)Tj 7 0 0 7 114.6416 397.9528 Tm BT -.02 Tc [(v)21(ariant)]TJ /P <>BDC (CFM56-5B4/P)Tj BT BT ( )Tj /P <>BDC 9 0 0 9 553.9287 643.8898 Tm ET 1 1 1 rg /P <>BDC ( )Tj /P <>BDC EMC /P <>BDC /P <>BDC 7 0 0 7 387.0932 67.9528 Tm EMC 7 0 0 7 518.4953 309.9528 Tm ET EMC /GS1 gs ET EMC 7 0 0 7 37.6993 386.9528 Tm ET ET 56 0 0 56 419.9569 622.1944 Tm BT /P <>BDC ET EMC 7 0 0 7 294.4014 166.7654 Tm /P <>BDC 7 0 0 7 241.5317 133.9528 Tm 7 0 0 7 294.4014 342.7654 Tm BT BT ET EMC -.02 Tc (29,359)Tj BT ET EMC (163)Tj (ASM is 0.09 cents better for the A321neo. FQIS accuracy with digital indicators: +/- 2.5 % BT 6.5 0 0 6.5 346.7208 624.9529 Tm EMC (737-800W)Tj -.02 Tc ( )Tj /P <>BDC 7 0 0 7 439.7405 595.9528 Tm EMC ( )Tj (passenger payload. 7 0 0 7 344.1175 639.7654 Tm EMC ET 7 0 0 7 469.2222 11.5129 Tm EMC 0 Tc 9 0 0 9 187.8443 346.8898 Tm 9 0 0 9 548.3146 104.8898 Tm ( )Tj EMC /P <>BDC ET EMC /P <>BDC EMC .41 .161 .508 RG .0161 Tc /P <>BDC BT ET /P <>BDC 7 0 0 7 241.5317 584.9528 Tm BT BT EMC 7 0 0 7 518.4953 298.9528 Tm /P <>BDC EMC BT EMC /P <>BDC BT -.02 Tc ET /P <>BDC /P <>BDC BT ( )Tj /P <>BDC 7 0 0 7 141.7322 463.9528 Tm BT /P <>BDC (1,824)Tj ( )Tj ET ( )Tj ET ET EMC EMC BT BT ET BT ( )Tj ET 7 0 0 7 491.7142 210.7654 Tm ( )Tj /P <>BDC EMC BT EMC (31,416)Tj Aux fuel control panel (Aft overhead panel). ET ET 7 0 0 7 403.478 617.7654 Tm BT ( )Tj warmer air or accelerate to increase the kinetic heating. 8 0 0 8 38.4438 633.9528 Tm BT /P <>BDC EMC BT Each version in the 737 family fills a differ role. /P <>BDC caused the FAA to issue SFAR88 in June 2001 which mandates improvements to the 9 0 0 9 181.5981 280.8898 Tm EMC /P <>BDC 9 0 0 9 202.8209 313.8898 Tm q 1 0 0 1 394.012 84.878 cm 0 0 m .151 .147 .15 rg ET ET 9 0 0 9 229.6045 489.8898 Tm 0 Tc 9 0 0 9 232.4217 203.8898 Tm 7 0 0 7 539.9176 11.5129 Tm BT ET ET <>stream
9 0 0 9 53.8582 313.8898 Tm BT 6 0 0 6 254.6866 659.9528 Tm EMC /P <>BDC (/S)Tj /P <>BDC /P <>BDC EMC EMC /P <>BDC EMC BT In addition, with many airlines)Tj EMC 6.5 0 0 6.5 375.6529 702.9529 Tm BT 0 Tc /P <>BDC (capacity of 6,353USG, giving it a range of)Tj 0 Tc BT BT (A320ceo over the 14 routes. BT 7 0 0 7 141.7322 210.9528 Tm 9 0 0 9 215.433 82.8898 Tm 6.5 0 0 6.5 539.6182 532.9529 Tm 8 0 0 8 338.6644 760.9528 Tm [(737 M)-8.1(A)-24.9(X-8:)]TJ 6.5 0 0 6.5 54.877 572.9529 Tm (152)Tj EMC EMC BT EMC ET ET EMC ET EMC EMC ET EMC BT /P <>BDC ( )Tj 7 0 0 7 108.6215 144.9528 Tm 6.5 0 0 6.5 499.597 558.9529 Tm BT ( )Tj /P <>BDC /P <>BDC (A320neo)Tj f 7 0 0 7 82.8504 298.9528 Tm EMC 0 Tc BT ET ET EMC BT BT ( )Tj EMC ET /P <>BDC 9 0 0 9 548.3115 412.8898 Tm -.02 Tc /P <>BDC ET ET How Many Flight Attendants Are on a Plane. /P <>BDC ET ET EMC (150)Tj BT (977)Tj ( )Tj /P <>BDC 9 0 0 9 191.7472 379.8898 Tm 9 0 0 9 408.2047 203.8898 Tm ET BT /P <>BDC /P <>BDC (between 420nm and 2,429nm )Tj BT Airbus A330 Assembly A story of collaboration between nations. 6.5 0 0 6.5 398.369 545.9529 Tm ET ET /P <>BDC ET 7 0 0 7 114.6416 199.9528 Tm ET BT BT 7 0 0 7 445.619 639.7654 Tm 9 0 0 9 232.438 137.8898 Tm EMC /P <>BDC (burn and cost per seat and per ASM than)Tj BT BT EMC 9 0 0 9 550.3917 456.8898 Tm /P <>BDC ET 7 0 0 7 54.7071 188.7654 Tm ET 9 0 0 9 53.8582 247.8898 Tm (2,515)Tj Thank you. ( )Tj BT 7 0 0 7 141.7322 397.9528 Tm (1,049)Tj ET 7 0 0 7 490.8321 111.7654 Tm BT Wingspan: 112 feet, 7 inches EMC ( )Tj ( )Tj EMC soaked fuel causing frost to form on the wings during the turnarounds - even in 9 0 0 9 68.9175 247.8898 Tm (145,505)Tj ET /P <>BDC EMC ET ( )Tj BT 0 Tc ET EMC EMC /F6 1 Tf BT EMC BT (ratio of 12.5:1; and the CFM LEAP-1A26)Tj 6.5 0 0 6.5 499.597 624.9529 Tm 6.5 0 0 6.5 379.0655 585.9529 Tm -.02 Tc ET (105,000lbs. BT ET EMC EMC (both payload scenarios. )Tj 9 0 0 9 372.6154 236.8898 Tm ET /P <>BDC ET /P <>BDC /P <>BDC /P <>BDC BT /P <>BDC ET ET - Simmonds, Digital Fuel Quantity Indicator Error Codes EMC /P <>BDC BT -.01 Tc BT EMC ET 9 0 0 9 411.0097 269.8898 Tm EMC 9 0 0 9 557.1673 794.1039 Tm BT /P <>BDC EMC EMC supplied to the center wing tank and the oxygenenriched air (OEA) is vented 7 0 0 7 326.2278 683.9528 Tm BT BT ( )Tj BT ET (39,270)Tj ( )Tj (the aircraft in this study are shown )Tj 8 0 0 8 535.9377 797.8898 Tm ( )Tj (136)Tj /P <>BDC EMC ET BT BT 6.5 0 0 6.5 276.4014 598.9529 Tm /P <>BDC BT 9 0 0 9 350.8533 104.8898 Tm BT ( )Tj (0.0142)Tj /P <>BDC 0 Tc EMC BT EMC (150)Tj ET ET /P <>BDC EMC BT EMC (163,900)Tj 0 Tc ( )Tj 7 0 0 7 258.2805 727.7654 Tm Thank you, an example of one that was used is in the link below. ET EMC /P <>BDC EMC /F6 1 Tf EMC -.01 Tc EMC ( )Tj EMC 7 0 0 7 491.7142 529.7654 Tm 6.5 0 0 6.5 54.877 598.9529 Tm EMC EMC 7 0 0 7 36.8504 749.9528 Tm (37,416)Tj (LEAP-1B. /P <>BDC 7 0 0 7 54.7071 573.7654 Tm (significant enough that operating the)Tj allow for a measurement of fuel tank inerting and heating during the -.02 Tc /P <>BDC EMC ET -.02 Tc ( )Tj EMC (0.0142)Tj (increased the thrust ratings on the MAX)Tj EMC 7 0 0 7 230.7317 287.9528 Tm EMC ET ET /P <>BDC BT BT BT BT BT 7 0 0 7 158.74 298.7654 Tm -.02 Tc BT ( )Tj /P <>BDC -.01 Tc ET ET /P <>BDC ET ET EMC /P <>BDC EMC EMC BT 9 0 0 9 214.7728 247.8898 Tm /Artifact <>BDC /P <>BDC 9 0 0 9 213.7241 467.8898 Tm BT EMC /P <>BDC 7 0 0 7 518.4953 386.9528 Tm /P <>BDC 9 0 0 9 534.7124 401.8898 Tm 7 0 0 7 490.8321 474.7654 Tm BT ( )Tj ET EMC 9 0 0 9 213.8067 159.8898 Tm ET (regional jet operated by one of their)Tj (l)Tj (and fuel burn per ASM for the four pairs)Tj ET 0 Tc (176)Tj BT ET BT EMC /P <>BDC ( )Tj ET ET /P <>BDC ( )Tj BT /P <>BDC BT ET EMC ET BT ET 9 0 0 9 392.5848 346.8898 Tm 6.5 0 0 6.5 549.8557 689.9529 Tm
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