/P <>BDC /P <>BDC EMC ( )Tj 7 0 0 7 456.4753 716.7654 Tm 7 0 0 7 535.5029 606.7654 Tm 9 0 0 9 394.0157 632.8898 Tm BT EMC EMC ( )Tj BT (- mins)Tj /P <>BDC ( )Tj -.02 Tc 7 0 0 7 108.6215 342.9528 Tm EMC ET EMC EMC /P <>BDC ET EMC 0 Tc /P <>BDC ET /P <>BDC BT ET (113,016)Tj ET 9 0 0 9 232.4217 445.8898 Tm 0 Tc BT 7 0 0 7 475.2383 639.9528 Tm ( )Tj 9 0 0 9 232.438 357.8898 Tm BT 9 0 0 9 545.3896 302.8898 Tm 7 0 0 7 233.5248 78.9528 Tm ( )Tj 737-600/-700/-800/-900 without densitometer: 7 0 0 7 445.619 507.7654 Tm ET /P <>BDC EMC EMC 8 0 0 8 365.7704 745.9528 Tm /P <>BDC /P <>BDC ( )Tj -.02 Tc /P <>BDC ( )Tj ( )Tj 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 /P <>BDC BT /P <>BDC /P <>BDC (20)Tj ET 7 0 0 7 487.0872 11.5129 Tm EMC EMC 6.5 0 0 6.5 295.7432 545.9529 Tm ET BT EMC /P <>BDC -.02 Tc BT ET 0 Tc EMC ET 0 Tc ET BT /P <>BDC ET EMC BT /P <>BDC ( )Tj 73 0 obj /Artifact <>BDC )Tj /P <>BDC 9 0 0 9 390.5438 566.8898 Tm EMC endobj (The A321ceo is equipped with either:)Tj ( )Tj BT 7 0 0 7 520.6108 683.9528 Tm 7 0 0 7 519.3773 67.9528 Tm 9 0 0 9 362.6813 357.8898 Tm /P <>BDC ET BT ( )Tj 7 0 0 7 247.7395 111.7654 Tm /P <>BDC BT (190,800)Tj EMC EMC EMC EMC -.02 Tc ET /P <>BDC I will be very happy to share with you once I get decent results. /P <>BDC BT BT /P <>BDC ET EMC 9 0 0 9 232.4217 181.8898 Tm (configurations for these aircraft types. /P <>BDC [(CFM L)17.1(E)-8.1(AP-)]TJ ET ET S ET ET /P <>BDC BT (135,453)Tj /P <>BDC Economy-plus is also)Tj 9 0 0 9 394.0315 181.8898 Tm /P <>BDC /GS1 gs 0 Tc /P <>BDC 7 0 0 7 99.8582 386.7654 Tm 7 0 0 7 520.6108 606.9528 Tm )]TJ BT 9 0 0 9 464.9339 577.8898 Tm ET /P <>BDC 9 0 0 9 194.7718 456.8898 Tm BT (382,280)Tj 9 0 0 9 373.9458 159.8898 Tm BT /P <>BDC .023 .567 .626 RG ( )Tj ( )Tj 7 0 0 7 383.0719 716.7654 Tm ET ET In real)Tj /P <>BDC EMC BT 6 0 0 6 246.7063 757.9528 Tm ET /P <>BDC 9 0 0 9 384.7818 137.8898 Tm ET ET EMC /P <>BDC BT /P <>BDC ( )Tj 6.5 0 0 6.5 499.4541 735.9529 Tm /P <>BDC [(AIRL)8.1(INE & AIR)7.1(CRAF)-12.9(T)18.1( OPERA)56.9(T)-8.1(ION)-13.9(S)]TJ 7 0 0 7 125.6292 441.7654 Tm (34,650lbs)Tj 9 0 0 9 232.4217 214.8898 Tm ET EMC ET .151 .147 .15 rg [(UG)-17.1(U)-8(S)8.1(T)]TJ 9 0 0 9 68.3339 478.8898 Tm EMC -.02 Tc BT EMC 6 0 0 6 277.7064 757.9528 Tm /P <>BDC /P <>BDC ET BT 9 0 0 9 394.0123 280.8898 Tm EMC -.01 Tc BT /P <>BDC BT ET -.02 Tc ET ( )Tj BT ET /P <>BDC EMC ET 9 0 0 9 166.7302 126.8898 Tm ( )Tj /P <>BDC EMC ET 9 0 0 9 394.0123 489.8898 Tm 6 0 0 6 434.3127 743.9528 Tm 9 0 0 9 252.9543 170.8898 Tm (415,112)Tj EMC (alternates used and their distance from the)Tj 0 Tc EMC (2,517)Tj ET 0 Tc ( )Tj 9 0 0 9 544.5291 665.8898 Tm ( )Tj (payload is carried. EMC EMC -.02 Tc BT BT )Tj ET 9 0 0 9 229.6141 335.8898 Tm ET BT (82,110)Tj /P <>BDC 7 0 0 7 247.7395 474.7654 Tm ( )Tj 9 0 0 9 200.4401 258.8898 Tm ET BT ( )Tj /P <>BDC EMC 0 J 0 j 5 w 10 M [] 0 d (used is 16/30/114, giving a seat count of)Tj /P <>BDC (. endobj BT 9 0 0 9 394.0237 225.8898 Tm 304.725 420.96 m ET BT ET 6 0 0 6 371.6408 743.9528 Tm 9 0 0 9 53.8582 236.8898 Tm ET 0 Tc ( )Tj ET /P <>BDC EMC (170)Tj ET BT EMC /P <>BDC 9 0 0 9 170.6722 104.8898 Tm -.02 Tc BT ET 9 0 0 9 411.0097 555.8898 Tm ( )Tj 0 Tc BT (. BT ET 7 0 0 7 337.7614 111.7654 Tm ( )Tj EMC BT /P <>BDC /P <>BDC EMC -.02 Tc ( )Tj ET ET EMC ET 0 Tc /P <>BDC /P <>BDC BT 0 Tc .151 .147 .15 rg ET BT (737-8)Tj 7 0 0 7 141.7322 243.9528 Tm Just wondering, where did you get the information about what specific aluminium alloys are used on different parts of the aircraft? 7 0 0 7 326.2278 595.9528 Tm ET ET EMC 9 0 0 9 551.8838 324.8898 Tm %PDF-1.4 BT EMC ET ( )Tj BT W n /P <>BDC BT EMC 0 Tc BT ET EMC (CFM56-7B26 engine on the heavier weight)Tj ET EMC EMC ET 0 Tc /P <>BDC /F4 1 Tf 9 0 0 9 394.0157 82.8898 Tm EMC ( )Tj ET /P <>BDC 6 0 0 6 174.3402 701.9528 Tm EMC ( )Tj EMC (CFM56-7B27B3)Tj 9 0 0 9 568.6457 357.8898 Tm ( )Tj BT /P <>BDC ET -.02 Tc 0 Tc ET EMC EMC ( )Tj (977)Tj BT Thank you for your reply. EMC ET BT 8 0 0 8 554.6981 771.7654 Tm (three inches more legroom than the)Tj /P <>BDC ET BT 7 0 0 7 439.2087 177.9528 Tm (CFM56-7B26)Tj /P <>BDC /P <>BDC ET EMC BT ET BT 9 0 0 9 411.0234 753.8898 Tm ET /P <>BDC BT EMC /P <>BDC 7 0 0 7 182.5706 540.9528 Tm EMC 7 0 0 7 315.5217 573.7654 Tm /P <>BDC /P <>BDC ET BT ( )Tj BT ET /P <>BDC EMC ( )Tj 9 0 0 9 199.3017 401.8898 Tm EMC The aux fuel 0 Tc 0 Tc \p+\rWef6lfL6;U1E5/6lUYyVebaHfQM]$q|L>_ SO9_sXa 3@"G;C=zlPY[?B 8 0 0 8 164.9203 771.9528 Tm 9 0 0 9 53.8338 82.8898 Tm ( )Tj ET BT -.02 Tc ET 5 0 0 5 484.5872 11.5129 Tm ( )Tj !! (CFM56-5B3/P)Tj ET BT 7 0 0 7 107.1165 78.9528 Tm ET /P <>BDC EMC ( )Tj BT (Top), Specification Table Boeing 737 Next Gen and Max.(Top). EMC ( )Tj BT BT 0 Tc BT BT 6.5 0 0 6.5 549.8557 598.9529 Tm Blended Winglets provide a simple and elegant solution to measurably improving aircraft fuel burn, managing operating costs and extending the economic life of an aircraft. BT 7 0 0 7 258.2805 144.7654 Tm 8 0 0 8 315.034 760.7654 Tm 6 0 0 6 277.6461 743.9528 Tm 5.25 0 0 5.25 465.7151 11.5129 Tm /P <>BDC ( )Tj (network used in this study, due to fuel tank)Tj ET /F6 1 Tf EMC BT BT EMC ET ( )Tj ( )Tj ET EMC EMC ET BT ET 9 0 0 9 138.3634 544.8898 Tm /P <>BDC 7 0 0 7 326.2278 474.9528 Tm 7 0 0 7 141.7322 595.9528 Tm EMC ET EMC /P <>BDC ( )Tj EMC /P <>BDC ET BT /P <>BDC 7 0 0 7 337.6855 177.9528 Tm ET /P <>BDC <>stream /P <>BDC 8 0 0 8 302.5117 633.9528 Tm EMC /GS2 gs 6.5 0 0 6.5 244.2585 637.9529 Tm -.02 Tc /P <>BDC /P <>BDC EMC 6 0 0 6 380.7199 659.9528 Tm BT ET EMC 9 0 0 9 36.8504 368.8898 Tm 0 Tc EMC 9 0 0 9 394.0237 192.8898 Tm 7 0 0 7 99.8582 298.7654 Tm 9 0 0 9 270.3219 720.8898 Tm ( )Tj EMC EMC /P <>BDC 8 0 0 8 314.3535 619.9528 Tm The controls for main tanks 1 and 2 change to aft 9 0 0 9 534.3536 577.8898 Tm ET /P <>BDC More Economical Dash Speed Capacity; Lower Landing . 6 0 0 6 184.3662 673.9528 Tm 0 Tc 7 0 0 7 230.7317 276.9528 Tm 7 0 0 7 241.5317 111.9528 Tm 0 Tc -.02 Tc /P <>BDC BT ET ET 9 0 0 9 408.1854 676.8898 Tm EMC (831)Tj /P <>BDC ET ET (A321neo)Tj (273,917)Tj BT 7 0 0 7 158.74 100.7654 Tm EMC 9 0 0 9 215.433 38.8898 Tm ET EMC 7 0 0 7 496.3063 705.7654 Tm ( )Tj EMC EMC 201.803 814.197 m /P <>BDC 7 0 0 7 99.8582 210.7654 Tm ET /Artifact <>BDC 7 0 0 7 363.2711 562.9528 Tm /F4 1 Tf /GS2 gs EMC /P <>BDC -.02 Tc EMC .559 .331 .619 rg 7 0 0 7 457.0984 595.7654 Tm ET ET EMC EMC (\(ATC\) charges. ET ET ET EMC (182,700)Tj q The)Tj Well, what do you know?! ET /P <>BDC /OC /MC1346 BDC /P <>BDC (4,863)Tj 7 0 0 7 366.0641 661.9528 Tm EMC 7 0 0 7 404.101 309.7654 Tm ET 7 0 0 7 518.4953 397.9528 Tm 0 Tc (the A320ceo. ET BT /P <>BDC 7 0 0 7 141.7322 276.9528 Tm EMC 0 Tc 0 Tc EMC 7 0 0 7 298.1781 144.9528 Tm BT 9 0 0 9 202.0349 753.8898 Tm ET EMC ET -.02 Tc /P <>BDC ET EMC BT ( )Tj -.02 Tc EMC BT EMC EMC /P <>BDC BT EMC BT 9 0 0 9 36.8504 478.8898 Tm EMC 7 0 0 7 99.8582 606.7654 Tm BT EMC EMC 0 Tc You can see the location of the centre tank 6 0 0 6 403.0689 729.9528 Tm EMC 9 0 0 9 551.4784 797.8898 Tm ET /P <>BDC BT /P <>BDC 7 0 0 7 241.5317 397.9528 Tm ET -.01 Tc BT /P <>BDC -.02 Tc ( )Tj -.02 Tc BT ET (31,416)Tj )Tj EMC ET ET EMC 7 0 0 7 54.7071 67.7654 Tm BT 9 0 0 9 361.1316 214.8898 Tm ET (MLW of 163,900lbs, and an OEW of)Tj EMC q 1 0 0 1 36.858 403.878 cm 0 0 m BT BT Main tanks smaller at 3900kg each but centre tank much larger giving total fuel capacity of 20,800kg. EMC -.02 Tc BT ET 7 0 0 7 54.7071 617.7654 Tm 9 0 0 9 53.8338 60.8898 Tm [(737-900E)-33(R)]TJ EMC EMC ET BT ET 9 0 0 9 411.0097 38.8898 Tm /P <>BDC EMC 0 Tc BT EMC BT -.01 Tc /P <>BDC BT BT -.02 Tc ( )Tj BT /P <>BDC ET ( )Tj BT EMC /P <>BDC /P <>BDC While the MAX 10 is still yet to be certified, the legacy of the -900ER lives on, and the type will likely continue to fly for many more years before retirement. BT EMC EMC (403-418)Tj EMC BT .534 .14 .504 RG (178)Tj EMC ET 9 0 0 9 394.0157 302.8898 Tm ET ET EMC ( )Tj /P <>BDC 9 0 0 9 562.1829 236.8898 Tm 6 0 0 6 394.3996 687.9528 Tm Q BT 7 0 0 7 404.101 133.7654 Tm 7 0 0 7 199.5784 199.7654 Tm BT BT BT /P <>BDC 9 0 0 9 68.0071 577.8898 Tm 9 0 0 9 215.4313 346.8898 Tm EMC EMC -.02 Tc 9 0 0 9 382.4508 159.8898 Tm 7 0 0 7 82.2047 683.9528 Tm 0 Tc ( C)Tj /P <>BDC ET /P <>BDC /P <>BDC 0 Tc 7 0 0 7 141.7322 100.9528 Tm /P <>BDC /P <>BDC BT ( )Tj BT [(CFM L)17.1(E)-8.1(AP-1B27)]TJ ET 7 0 0 7 187.0858 661.9528 Tm EMC ET /P <>BDC (346,456)Tj (166,090)Tj BT 7 0 0 7 316.0679 408.7654 Tm EMC EMC ET ( )Tj /P <>BDC (seats. EMC 9 0 0 9 534.7635 203.8898 Tm ( )Tj each engine. 9 0 0 9 411.0097 280.8898 Tm 9 0 0 9 552.2133 291.8898 Tm 6.5 0 0 6.5 273.8079 702.9529 Tm (table, page 19\))Tj ET BT /P <>BDC /P <>BDC .151 .147 .15 rg BT EMC ET /P <>BDC BT ET (188,400)Tj 9 0 0 9 343.5117 489.8898 Tm BT BT 0 Tc EMC (0.0108)Tj 7 0 0 7 490.5101 738.9528 Tm BT EMC ET BT (172,992)Tj (A)Tj ET BT 0 Tc -.02 Tc /P <>BDC ( )Tj EMC BT 9 0 0 9 411.0181 236.8898 Tm (seat capacity, with no additional cargo. /P <>BDC 7 0 0 7 387.0159 606.9528 Tm (39,270)Tj EMC EMC ET ( )Tj 0 Tc /P <>BDC ( )Tj [(CFM L)17.1(E)-8.1(AP-1B27)]TJ 9 0 0 9 53.8582 390.8898 Tm ( )Tj 7 0 0 7 99.8582 639.7654 Tm EMC - Non Perele - News Online, Council Post: Aviation Is The Driving Force Of Hydrogen | QNewsHub, When will the Boeing 737 MAX fly again? ( )Tj EMC 0 Tc /P <>BDC ET EMC ET /P <>BDC BT BT ET /P <>BDC /F4 1 Tf (have payload restrictions on the evaluation)Tj BT EMC /P <>BDC 7 0 0 7 258.2805 595.7654 Tm 0 Tc I started of using with this image. BT BT 8 0 0 8 53.9373 760.7654 Tm EMC ET ET 7 0 0 7 344.1175 584.7654 Tm 9 0 0 9 394.0157 555.8898 Tm 7 0 0 7 444.737 265.7654 Tm /P <>BDC 7 0 0 7 108.6215 243.9528 Tm ET ET /P <>BDC BT 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 (6,303)Tj EMC 9 0 0 9 75.273 544.8898 Tm /P <>BDC ET EMC EMC -.01 Tc 9 0 0 9 552.2312 676.8898 Tm 7 0 0 7 258.2805 67.7654 Tm 7 0 0 7 258.2805 507.7654 Tm /P <>BDC EMC /P <>BDC ET BT Q /P <>BDC EMC ET /P <>BDC EMC (comparison of the fuel burn performance. [(CFM L)17.1(E)-8.1(AP-1A26)]TJ -.02 Tc BT 0 Tc ET /P <>BDC ET 7 0 0 7 279.1575 606.9528 Tm EMC (A)Tj ET /P <>BDC ( )Tj EMC /P <>BDC 7 0 0 7 107.1165 375.9528 Tm /P <>BDC 7 0 0 7 404.101 397.7654 Tm /P <>BDC ( )Tj /P <>BDC /P <>BDC 0 Tc /P <>BDC /P <>BDC (by the CFM LEAP-1A26. ET Cheers Peter. 9 0 0 9 411.0097 390.8898 Tm ( )Tj 6.5 0 0 6.5 192.6116 650.9529 Tm EMC BT 7 0 0 7 99.8582 177.7654 Tm BT EMC BT 6.5 0 0 6.5 227.9655 565.9529 Tm EMC ( )Tj 7 0 0 7 124.1242 199.7654 Tm EMC BT ET ET /P <>BDC 7 0 0 7 294.4014 375.7654 Tm 6 0 0 6 527.5437 659.9528 Tm EMC EMC ET Aircraft must carry enough fuel to taxi, climb, cruise, descent, and mutliple reserves. EMC (0.0122)Tj -.02 Tc EMC EMC EMC /P <>BDC ET EMC 7 0 0 7 187.0858 705.9528 Tm BT BT .151 .147 .15 rg 9 0 0 9 374.4497 214.8898 Tm ET EMC 6.5 0 0 6.5 536.1732 545.9529 Tm BT 0 Tc BT BT EMC 7 0 0 7 387.0932 276.9528 Tm ET EMC /P <>BDC BT EMC EMC EMC EMC -.02 Tc EMC ET ET 0 Tc 7 0 0 7 230.7317 386.9528 Tm /P <>BDC EMC ET /P <>BDC EMC EMC 13 0 0 13 162.9571 181.8898 Tm 7 0 0 7 363.2711 540.9528 Tm (10,040)Tj ET /Artifact <>BDC 7 0 0 7 535.5029 518.7654 Tm ( )Tj 9 0 0 9 394.0315 599.8898 Tm (29,359)Tj (3,535)Tj EMC -.02 Tc 9 0 0 9 199.0091 401.8898 Tm I already checked in the AMM, SRM. EMC ET [(www)60.7(.aircr)9.7(aft-commerce.com)]TJ /P <>BDC ( )Tj 0 Tc /P <>BDC 7 0 0 7 141.7322 122.9528 Tm /OC /MC835 BDC ( )Tj /P <>BDC ET /P <>BDC 9 0 0 9 505.9653 115.8898 Tm 0 Tc ET /P <>BDC (performance deterioration factor added to)Tj ET 9 0 0 9 112.3045 346.8898 Tm EMC EMC 9 0 0 9 394.0157 577.8898 Tm Follow this link to see the "Quick Change" Aux fuel system offered by Long Range, expected 2015. /P <>BDC 7 0 0 7 539.8962 474.9528 Tm /F6 1 Tf (1,782)Tj (The A320 and 737 families have been)Tj ET 7 0 0 7 316.0679 331.7654 Tm For example, if the fuel tank maximum capacity is 10,000 KG, then the tolerance of the gauging is 0.02 (airplane without a densitometer) * 10000 = 200 KG. 0 Tc 7 0 0 7 554.7883 507.7654 Tm /P <>BDC /P <>BDC 9 0 0 9 394.0157 566.8898 Tm BT /P <>BDC BT BT 6.5 0 0 6.5 295.8145 611.9529 Tm (483)Tj 7 0 0 7 37.6993 276.9528 Tm /F6 1 Tf BT ET EMC ( )Tj 9 0 0 9 368.9994 456.8898 Tm 304.725 420.96 m x&o[v?vr&D6oi#9v I7JW\'18pLq2qN8hbeebfvlV7pr ET 0 Tc (179)Tj 0 Tc 9 0 0 9 215.4313 478.8898 Tm EMC -.02 Tc 7 0 0 7 355.3163 133.7654 Tm BT 7 0 0 7 247.7395 342.7654 Tm ET ( )Tj BT /P <>BDC 7 0 0 7 158.74 518.7654 Tm BT 7 0 0 7 403.478 694.7654 Tm /Artifact <>BDC EMC EMC BT EMC ET EMC 6.5 0 0 6.5 93.2476 702.9529 Tm ET ( )Tj ( )Tj EMC ET BT EMC Boeing 737-800 GSSI 2021-07-28T14:13:10-07:00 With a larger area, wide wingspan and greater fuel capacity, the Boeing 737-800 from KF is ready for lease. /P <>BDC ( )Tj (737-9)Tj ET -.02 Tc BT EMC BT /P <>BDC EMC 7 0 0 7 297.632 595.9528 Tm ( )Tj EMC 5.25 0 0 5.25 100.8225 11.5132 Tm (0.0140)Tj ET 9 0 0 9 229.6064 456.8898 Tm 9 0 0 9 394.0123 599.8898 Tm EMC (271,728)Tj ( )Tj 7 0 0 7 141.7322 78.9528 Tm [(Y)-7.1(XX/104)]TJ 0 Tc 0 Tc /P <>BDC ( )Tj /P <>BDC -.02 Tc ET 6.5 0 0 6.5 273.8079 676.9529 Tm /P <>BDC (1,351)Tj (the flight profile based on the cruise speed)Tj 7 0 0 7 536.3849 331.7654 Tm ( )Tj EMC (payload on any sector in this evaluation. 56 0 obj /P <>BDC 7 0 0 7 337.4684 705.9528 Tm ( )Tj EMC /P <>BDC (6,875)Tj (service in late 2020 with many)Tj EMC BT 8 0 0 8 38.4438 745.9528 Tm EMC ET ( )Tj BT /P <>BDC EMC BT BT ( )Tj .7 -.5345 .9114 -1.2305 y ET BT 9 0 0 9 342.0176 126.8898 Tm ET 0 Tc -.01 Tc ET ( )Tj 9 0 0 9 547.6725 346.8898 Tm ET 7 0 0 7 337.9444 89.9528 Tm ET /P <>BDC EMC ET ( )Tj BT 7 0 0 7 554.7883 122.7654 Tm EMC ET 0 Tc ( )Tj /P <>BDC /P <>BDC -.02 Tc EMC 10 0 0 10 312.5146 771.9528 Tm BT 9 0 0 9 408.2047 203.8898 Tm /P <>BDC ( )Tj ET EMC 0 Tc 0 Tc 6.5 0 0 6.5 324.4345 702.9529 Tm /P <>BDC EMC (uses one of the 11 certified weight variants. BT /P <>BDC BT ( )Tj .151 .147 .15 rg ( )Tj 9 0 0 9 232.4217 456.8898 Tm EMC BT (Engine)Tj 9 0 0 9 372.6154 236.8898 Tm ET BT 7 0 0 7 439.7405 628.9528 Tm 7 0 0 7 444.737 78.7654 Tm BT 9 0 0 9 246.595 302.8898 Tm BT 9 0 0 9 215.433 434.8898 Tm 6.5 0 0 6.5 295.5027 565.9529 Tm (CFM56-7B27B3)Tj 7 0 0 7 230.7317 375.9528 Tm 7 0 0 7 543.7693 11.5132 Tm /P <>BDC BT BT BT /P <>BDC BT BT -.02 Tc 6 0 0 6 191.3929 771.9528 Tm )Tj q 1 0 0 1 53.858 150.878 cm 0 0 m Values can be entered and displayed in pounds or kilograms. (A321neo)Tj 8 0 0 8 275.7172 760.7654 Tm EMC BT 7 0 0 7 387.0159 507.9528 Tm ET ET ( )Tj 8 0 0 8 339.6345 760.7654 Tm 0 Tc /P <>BDC BT ET /P <>BDC -.02 Tc way. /OC /MC3431 BDC /F6 1 Tf 9 0 0 9 341.891 335.8898 Tm BT 0 Tc BT BT ( )Tj /P <>BDC -.02 Tc ( )Tj You were right, there were some discrepancies around the range. (planned 170 passengers as follows: 145 on)Tj (- nm)Tj ET (20)Tj EMC (maintenance. BT ET EMC ( )Tj EMC ET ET -.02 Tc 9 0 0 9 36.8504 181.8898 Tm 10 0 0 10 422.8 814.1973 Tm EMC EMC BT ET 9 0 0 9 53.8338 137.8898 Tm 7 0 0 7 99.8582 595.7654 Tm ET ET /P <>BDC /P <>BDC ( )Tj -.02 Tc BT /F1 1 Tf ET EMC waiting with pax /P <>BDC /P <>BDC ( )Tj ET /P <>BDC 6.5 0 0 6.5 448.8744 624.9529 Tm ET /P <>BDC EMC /P <>BDC BT BT ET EMC 7 0 0 7 428.6112 386.9528 Tm EMC 9 0 0 9 53.8582 709.8898 Tm -.01 Tc /P <>BDC BT /P <>BDC BT BT 0 Tc 7 0 0 7 338.3085 265.9528 Tm EMC ET 9 0 0 9 229.6141 434.8898 Tm ET 7 0 0 7 491.7142 232.7654 Tm ET 8 0 0 8 38.4438 577.9528 Tm ( )Tj ET 7 0 0 7 230.7317 397.9528 Tm 7 0 0 7 520.6108 507.9528 Tm 9 0 0 9 53.8578 302.8898 Tm EMC BT 9 0 0 9 53.8578 434.8898 Tm EMC /P <>BDC When this runs dry the scavenge the 737 but will require up to six on the 747. /P <>BDC EMC EMC 6.5 0 0 6.5 499.597 585.9529 Tm ET BT 9 0 0 9 411.0181 401.8898 Tm ET 7 0 0 7 429.4931 122.9528 Tm 7 0 0 7 429.157 738.9528 Tm ET BT /P <>BDC EMC EMC EMC (31,416)Tj 9 0 0 9 372.2467 170.8898 Tm (136)Tj ( )Tj BT BT 7 0 0 7 99.8582 716.7654 Tm EMC EMC 9 0 0 9 535.0095 423.8898 Tm /P <>BDC EMC (72,450)Tj EMC EMC EMC EMC 6.5 0 0 6.5 499.8375 545.9529 Tm EMC EMC EMC BT ET BT /P <>BDC ET BT 0 Tc ET ET ( )Tj ET 13 0 0 13 202.8899 533.8898 Tm BT /P <>BDC (CFM56-5B4/P)Tj BT (104-112)Tj /P <>BDC BT ET /P <>BDC EMC BT ET BT /P <>BDC BT 7 0 0 7 539.8962 507.9528 Tm ET ( )Tj /F4 1 Tf -.02 Tc .014984 841.89 609.45 -841.89 re 9 0 0 9 192.0203 313.8898 Tm /P <>BDC BT EMC /P <>BDC 7 0 0 7 258.2805 386.7654 Tm 7 0 0 7 230.7317 166.9528 Tm ET ET EMC I found this image that might have some of the answers you need. EMC ( )Tj BT BT ET -.01 Tc ET ET BT EMC EMC EMC BT ET BT 7 0 0 7 354.6933 364.7654 Tm /P <>BDC /P <>BDC BT (39,270)Tj /P <>BDC ET BT ( )Tj EMC EMC /P <>BDC EMC 7 0 0 7 338.3085 309.9528 Tm ET ET /P <>BDC 0 Tc ( )Tj ET (4,615)Tj /P <>BDC /P <>BDC 7 0 0 7 196.5683 320.7654 Tm (170)Tj BT ET EMC EMC ET ET EMC BT EMC (5.7:1)Tj EMC 7 0 0 7 354.4763 705.7654 Tm ( )Tj EMC 9 0 0 9 394.0157 335.8898 Tm EMC ( )Tj EMC ET ET (737-9)Tj EMC 6.5 0 0 6.5 296.4841 702.9529 Tm EMC /F4 1 Tf EMC BT /P <>BDC EMC ( )Tj ET ET /P <>BDC EMC 7 0 0 7 279.1575 221.9528 Tm ET ET 7 0 0 7 492.5963 584.7654 Tm ET /P <>BDC -.02 Tc EMC /P <>BDC ET ET (All the flights were in a westerly)Tj 0 Tc EMC 26.0355 0 TD ET design and maintenance of fuel tanks to reduce the chances of such explosions in (destination airport are listed )Tj -.01 Tc 7 0 0 7 230.7317 738.9528 Tm 7 0 0 7 131.6494 276.7654 Tm 9 0 0 9 378.9498 368.8898 Tm EMC The AFM limits are higher, but not normally achievable with standard SG's. BT BT BT /P <>BDC BT /P <>BDC ET 7 0 0 7 520.6108 628.9528 Tm /P <>BDC EMC safer place! EMC ( )Tj ( )Tj BT BT 9 0 0 9 375.2598 126.8898 Tm Due to the additional structural)Tj .1334 -5.7288 l )Tj /P <>BDC /P <>BDC EMC (and 737-9. 0 Tc BT BT ( )Tj /P <>BDC (applied to all flights. EMC 0 Tc 6 0 0 6 55.0668 757.9528 Tm EMC /P <>BDC EMC BT EMC /P <>BDC -.02 Tc BT /P <>BDC 9 0 0 9 411.0097 500.8898 Tm EMC /P <>BDC ( )Tj ( )Tj 7 0 0 7 278.9827 430.9528 Tm EMC (fuel capacity of 6,303USG )Tj /P <>BDC BT EMC BT ET BT 8 0 0 8 136.4919 717.9528 Tm 8 0 0 8 404.5618 771.9528 Tm For instance, What is the Aluminium alloy 7055 basis values ? /F6 1 Tf EMC ( )Tj -.2034 -.7911 -.1202 -.4766 0 0 c 5.25 0 0 5.25 40.8474 11.5129 Tm ET BT /P <>BDC /P <>BDC (payload 1 and payload 2 scenarios, the)Tj BT ET 7 0 0 7 125.6292 584.7654 Tm BT (1,824)Tj BT EMC (payload, the A321neo has an 18.9%)Tj 0 Tc BT BT EMC /P <>BDC /P <>BDC BT EMC (34,650lbs )Tj /P <>BDC ( )Tj ET EMC -.01 Tc 0 Tc 0 Tc 9 0 0 9 366.6417 137.8898 Tm (0.0160)Tj BT pump will also transfer any remaining centre tank fuel into main tank 1, thereby [(v)21(ariant)]TJ 0 Tc EMC /P <>BDC BT /P <>BDC EMC ET /P <>BDC 9 0 0 9 142.2128 335.8898 Tm BT ET ( )Tj 7 0 0 7 456.2165 419.7654 Tm EMC /P <>BDC ET ET EMC /P <>BDC 7 0 0 7 537.7804 287.9528 Tm This is due to cold -.02 Tc /P <>BDC 7 0 0 7 445.619 375.7654 Tm BT 9 0 0 9 79.8339 522.8898 Tm (-62)Tj 6.5 0 0 6.5 346.1424 545.9529 Tm ET /P <>BDC 6.5 0 0 6.5 347.0329 532.9529 Tm BT EMC 9 0 0 9 186.1613 49.8898 Tm BT /GS2 gs 6 0 0 6 418.9814 701.9528 Tm /P <>BDC 7 0 0 7 141.7322 562.9528 Tm ( )Tj BT BT ( )Tj EMC /P <>BDC 6.5 0 0 6.5 114.9382 611.9529 Tm (the CFM56-5B with thrust ratings of)Tj ET BT 10 0 0 10 49.2604 814.1973 Tm /P <>BDC ( )Tj EMC /P <>BDC ( )Tj (150)Tj EMC 7 0 0 7 490.5101 562.9528 Tm ET ET ( )Tj [(CFM L)17.1(E)-8.1(AP-1B27)]TJ EMC 7 0 0 7 445.619 628.7654 Tm BT BT ET Hi there.. is anyone able to tell me the radius of the arc of the L1 and L2 doors as they are being opened? BT ( )Tj /P <>BDC 6.5 0 0 6.5 549.8557 611.9529 Tm EMC ( )Tj ( )Tj EMC BT -.02 Tc BT EMC /P <>BDC /P <>BDC 7 0 0 7 427.7291 210.9528 Tm EMC /P <>BDC ET 7 0 0 7 535.5029 661.7654 Tm 9 0 0 9 53.8578 214.8898 Tm BT EMC EMC EMC BT ( )Tj 9 0 0 9 369.0641 225.8898 Tm ET ET ( )Tj ET (4,552)Tj BT 10 0 0 10 52.0044 814.1973 Tm 7 0 0 7 278.2756 672.9528 Tm /P <>BDC ET 6.5 0 0 6.5 397.9138 722.9529 Tm ET 9 0 0 9 551.0194 588.8898 Tm 1 i /P <>BDC ET ( )Tj ( )Tj BT (A321ceo)Tj 9 0 0 9 359.1448 181.8898 Tm /P <>BDC 7 0 0 7 337.7614 89.7654 Tm ET 9 0 0 9 394.0315 456.8898 Tm /P <>BDC ( )Tj ET EMC ET EMC ET EMC (The later generation aircraft are set to)Tj BT ( )Tj BT /P <>BDC ( )Tj -.02 Tc 0 841.89 609.449 -841.89 re EMC /P <>BDC /P <>BDC EMC ET 6 0 0 6 208.1569 743.9528 Tm EMC ( )Tj ET -.02 Tc 9 0 0 9 533.576 236.8898 Tm EMC EMC /P <>BDC ( )Tj EMC ET ET ET ( )Tj /F1 1 Tf (CFM56-7B27B3)Tj EMC /GS1 gs EMC /P <>BDC BT BT 9 0 0 9 212.1598 302.8898 Tm 9 0 0 9 202.1458 258.8898 Tm ET (0.0142)Tj BT (total seat count for these two types. BT (2,729)Tj (832)Tj (ESAD)Tj (same passenger payload. BT -.02 Tc BT ET BT 9 0 0 9 548.3146 104.8898 Tm EMC ET BT 9 0 0 9 566.4993 698.8898 Tm 7 0 0 7 387.0932 177.9528 Tm fuel pumps will automatically shut off when they detect a low output pressure. 6 0 0 6 277.7064 715.9528 Tm (20)Tj EMC BT ET (152)Tj ET (calculate the fuel burns and times. 6.5 0 0 6.5 225.3721 585.9529 Tm 9 0 0 9 424.4247 764.8898 Tm ET /P <>BDC 7 0 0 7 491.7142 133.7654 Tm BT /P <>BDC the most hazardous condition-an empty center wing tank-that GBI would remain BT Vmo/Mmo Velocity/Mach Maximum Operating speed. 9 0 0 9 36.8504 247.8898 Tm ET -.02 Tc /P <>BDC BT (171,520)Tj ( )Tj EMC (150)Tj ET 7 0 0 7 518.4953 331.9528 Tm EMC BT 9 0 0 9 525.9757 60.8898 Tm ET 7 0 0 7 125.6292 342.7654 Tm ET EMC /P <>BDC ( )Tj /GS2 gs EMC /P <>BDC ( )Tj /P <>BDC /P <>BDC ( )Tj 6.5 0 0 6.5 244.4599 702.9529 Tm 9 0 0 9 394.0157 346.8898 Tm ( )Tj 7 0 0 7 124.1242 694.7654 Tm 10 0 0 10 60.6037 794.2914 Tm ( )Tj /P <>BDC 7 0 0 7 475.2383 683.9528 Tm ET ( )Tj 0 Tc /GS1 gs ET EMC ET BT /P <>BDC EMC ET (282)Tj BT EMC 0 Tc 7 0 0 7 404.101 166.7654 Tm BT 7 0 0 7 554.7883 298.7654 Tm 6.5 0 0 6.5 285.7159 611.9529 Tm ( )Tj BT ET 9 0 0 9 215.4409 412.8898 Tm BT EMC /P <>BDC ET 7 0 0 7 37.0536 727.9528 Tm ET 8 0 0 8 43.6039 771.9528 Tm ET BT ET EMC EMC (163)Tj /P <>BDC 7 0 0 7 469.2222 11.5129 Tm EMC BT ET BT ET ET ET ET 9 0 0 9 68.9175 247.8898 Tm EMC EMC 7 0 0 7 158.74 606.7654 Tm /P <>BDC EMC EMC 9 0 0 9 351.6906 456.8898 Tm BT /P <>BDC 9 0 0 9 389.1758 522.8898 Tm ET EMC 0 Tc (141,270)Tj 7 0 0 7 539.8962 661.9528 Tm tank. EMC /P <>BDC -.02 Tc (burn and cost per seat and per ASM than)Tj BT EMC BT EMC /P <>BDC (-58)Tj /P <>BDC /P <>BDC ET /P <>BDC /P <>BDC ET EMC (BOS-YVR \(Vancouver\) route. ET /P <>BDC /P <>BDC ET EMC EMC q 1 0 0 1 215.433 150.878 cm 0 0 m 0 Tc 9 0 0 9 566.3776 192.8898 Tm ET BT ET ( )Tj 0 Tc BT /P <>BDC BT BT 9 0 0 9 51.0236 401.8898 Tm ET /P <>BDC EMC ET ET EMC BT 0 J 0 j .5 w 10 M [] 0 d 7 0 0 7 294.4014 683.7654 Tm 7 0 0 7 54.5916 342.7654 Tm 7 0 0 7 321.6356 210.9528 Tm ( )Tj BT /P <>BDC EMC BT EMC EMC BT ( )Tj 7 0 0 7 314.6398 463.7654 Tm )Tj -.02 Tc BT EMC BT BT ( )Tj 9 0 0 9 36.8504 170.8898 Tm EMC BT BT EMC ET q 1 0 0 1 508.103 86.641 cm 0 0 m EMC 0 Tc EMC BT /P <>BDC ET Hi and thanks for stopping by. /OC /MC5095 BDC -.02 Tc /P <>BDC /P <>BDC BT /P <>BDC BT /P <>BDC BT re-primed. ( )Tj ET 9 0 0 9 232.4217 236.8898 Tm .41 .161 .508 rg /P <>BDC EMC 7 0 0 7 456.2165 78.7654 Tm ET EMC /P <>BDC ET (optimum cruise altitude. 0 Tc /P <>BDC /P <>BDC EMC /P <>BDC ET /P <>BDC ET BT ET EMC ET EMC BT ET 7 0 0 7 456.2165 397.7654 Tm 0 Tc (2,042)Tj ET f ET ET EMC (1,091)Tj These sectors)Tj ( )Tj EMC 9 0 0 9 394.0123 478.8898 Tm /P <>BDC Q ( )Tj /P <>BDC BT ( )Tj (174,165)Tj /P <>BDC /P <>BDC ET /P <>BDC /P <>BDC EMC ET ET 7 0 0 7 316.0679 188.7654 Tm BT /P <>BDC BT BT EMC ET 9 0 0 9 350.8719 390.8898 Tm BT /P <>BDC ET 0 Tc (209)Tj 9 0 0 9 411.0181 71.8898 Tm EMC EMC BT BT 9 0 0 9 538.7331 225.8898 Tm -.02 Tc 0 841.89 609.449 -841.89 re EMC EMC 9 0 0 9 394.0315 643.8898 Tm BT /P <>BDC BT (6,820)Tj EMC /P <>BDC /P <>BDC ( )Tj 7 0 0 7 54.7071 364.7654 Tm /GS1 gs EMC EMC ( )Tj BT 8 0 0 8 296.665 771.9529 Tm EMC ET (load factor, the A321neo carries a heavier)Tj EMC EMC EMC BT EMC EMC 0 Tc 0 J 0 j 15 w 10 M [] 0 d ET /P <>BDC (. BT ( )Tj ET /P <>BDC ( )Tj (174,900)Tj EMC /F1 1 Tf ( )Tj /P <>BDC /P <>BDC ET (A321ceo)Tj /P <>BDC BT ET /P <>BDC )Tj (support, operating procedures and)Tj ET 0 Tc (5,376)Tj