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. EMC /P <>BDC 9 0 0 9 232.4408 687.8898 Tm BT 7 0 0 7 247.7395 595.7654 Tm /P <>BDC EMC BT -.02 Tc .559 .331 .619 rg ET ( )Tj BT EMC /P <>BDC 9 0 0 9 199.3527 390.8898 Tm [(CFM L)17.1(E)-8.1(AP-1A32)]TJ 9 0 0 9 232.438 445.8898 Tm EMC 0 Tc The NG has 6 dripsticks in each wing tank and 4 in the centre BT ET (105)Tj ET /P <>BDC ( )Tj BT (2,376)Tj BT ( )Tj ( )Tj BT BT ( )Tj [(CFM L)17.1(E)-8.1(AP-1B27)]TJ 0 Tc EMC BT <>stream BT EMC /P <>BDC Q 7 0 0 7 230.7317 738.9528 Tm BT levels in the center fuel tanks. -.02 Tc /P <>BDC /P <>BDC 7 0 0 7 158.74 298.7654 Tm /P <>BDC /P <>BDC EMC 9 0 0 9 562.4354 137.8898 Tm /P <>BDC BT W n (scenario 2, where all types carry an 85%)Tj BT BT ET 7 0 0 7 54.7071 463.7654 Tm 9 0 0 9 374.3633 401.8898 Tm aux tanks to push the aux fuel into the centre tank. ( )Tj (difference. /P <>BDC f BT ET BT EMC ( )Tj 7 0 0 7 204.0935 331.7654 Tm BT 0 Tc 6.5 0 0 6.5 244.3364 735.9529 Tm BT EMC /P <>BDC EMC 9 0 0 9 36.8504 368.8898 Tm 9 0 0 9 68.3339 445.8898 Tm BT BT ET /P <>BDC ( )Tj EMC ET /P <>BDC /P <>BDC ( )Tj /P <>BDC ( )Tj ( )Tj More Economical Dash Speed Capacity; Lower Landing . /P <>BDC /P <>BDC ET 7 0 0 7 87.8179 243.7654 Tm EMC ET (132,872)Tj EMC /P <>BDC 7 0 0 7 343.2355 661.7654 Tm EMC BT 9 0 0 9 540.3891 544.8898 Tm ET 0 Tc /P <>BDC -.02 Tc ET ET /P <>BDC ET 7 0 0 7 473.4744 518.9528 Tm Classics could (31,416)Tj ET EMC ( )Tj ET ( )Tj EMC (5,279)Tj (operator. 7 0 0 7 241.2727 144.9528 Tm 0 Tc ET BT ET EMC EMC /P <>BDC ET EMC 0 Tc BT 6 0 0 6 497.1933 687.9528 Tm BT EMC BT BT /P <>BDC EMC ET 6.5 0 0 6.5 399.2659 565.9529 Tm 7 0 0 7 386.3929 573.9528 Tm ET BT /F6 1 Tf EMC ET 9 0 0 9 105.3138 82.8898 Tm (10)Tj 9 0 0 9 554.3696 269.8898 Tm EMC BT EMC /P <>BDC 7 0 0 7 316.0679 232.7654 Tm 7 0 0 7 457.0984 408.7654 Tm Digital Fuel Quantity Indicator Error Codes, Missing or disconnected tank /P <>BDC BT ( )Tj 6.5 0 0 6.5 296.2827 637.9529 Tm EMC (0.0133)Tj EMC 7 0 0 7 233.5248 78.9528 Tm BT 9 0 0 9 232.4408 753.8898 Tm /P <>BDC BT /P <>BDC ET 56.25 0 0 56.25 36.8583 489.8898 Tm BT (service in late 2020 with many)Tj BT 7 0 0 7 491.7142 133.7654 Tm EMC 7 0 0 7 490.8321 375.7654 Tm ( )Tj EMC 9 0 0 9 518.9185 401.8898 Tm ET ET ( )Tj /P <>BDC 6.5 0 0 6.5 324.4345 702.9529 Tm ET ET EMC ET 6.5 0 0 6.5 447.8411 663.9529 Tm BT (35,112)Tj BT 7 0 0 7 158.74 67.7654 Tm /P <>BDC EMC EMC EMC /P <>BDC ET EMC BT ET ET EMC BT BT BT 9 0 0 9 36.8504 159.8898 Tm Cheers Peter. BT BT ET /P <>BDC /P <>BDC 9 0 0 9 232.438 434.8898 Tm (152)Tj [(CFM L)17.1(E)-8.1(AP-1A32)]TJ (277,248)Tj ET BT /OC /MC1956 BDC BT /P <>BDC ( )Tj ( )Tj 0 Tc 7 0 0 7 158.74 331.7654 Tm /P <>BDC /P <>BDC BT EMC EMC /P <>BDC EMC EMC 7 0 0 7 196.5683 419.7654 Tm EMC ET (in this analysis is one of the 12 certified)Tj 9 0 0 9 53.8582 577.8898 Tm BT ET BT EMC 6.5 0 0 6.5 222.7786 676.9529 Tm 1 i BT BT BT ET ET BT warmer air or accelerate to increase the kinetic heating. BT ET /P <>BDC .023 .567 .626 rg (number of seats and ASMs will give an)Tj /P <>BDC /P <>BDC 7 0 0 7 537.8154 430.9528 Tm /P <>BDC /F2 1 Tf BT 9 0 0 9 408.1889 533.8898 Tm /P <>BDC 7 0 0 7 67.798 11.5132 Tm ( )Tj ET ( )Tj 9 0 0 9 362.0968 324.8898 Tm -.02 Tc /P <>BDC ( )Tj BT 9 0 0 9 207.867 368.8898 Tm BT ( )Tj ET 5.25 0 0 5.25 492.6848 11.5129 Tm EMC 7 0 0 7 247.7395 166.7654 Tm /P <>BDC EMC ( )Tj EMC BT EMC EMC (2,517)Tj ET /P <>BDC EMC BT ( )Tj /P <>BDC 7 0 0 7 380.2788 298.7654 Tm ET The weight configuration used)Tj /P <>BDC EMC EMC 9 0 0 9 121.2888 38.8898 Tm ET 0 Tc ( )Tj /P <>BDC /P <>BDC BT ET 9 0 0 9 232.4217 599.8898 Tm ET EMC -.02 Tc (affect the comparison of ASM versus cost. 6.5 0 0 6.5 429.0755 637.9529 Tm EMC ( )Tj ET (282)Tj 6.5 0 0 6.5 429.0755 650.9529 Tm /P <>BDC BT ET ( )Tj EMC BT BT EMC (152)Tj EMC BT EMC EMC ET (150)Tj EMC BT 0 Tc /P <>BDC /P <>BDC 9 0 0 9 53.8582 665.8898 Tm ET ET EMC /P <>BDC EMC 7 0 0 7 362.3891 287.9528 Tm EMC EMC BT ( )Tj 7 0 0 7 204.0935 111.7654 Tm It is produced in the Renton plant in Washington by Boeing Commercial Airplanes. /P <>BDC 7 0 0 7 125.6292 144.7654 Tm BT /OC /MC27 BDC Regarding winglets, I think Simple Flying explains it well. The 800 being based of the 400 is designed for short routes. ( )Tj (The A321ceo has a maximum fuel)Tj (0.0109)Tj /P <>BDC ET EMC /P <>BDC BT BT 13 0 0 13 202.8899 533.8898 Tm BT /OC /MC854 BDC EMC /P <>BDC 0 Tc -.02 Tc 0 Tc ( )Tj EMC BT EMC ET -.02 Tc EMC 7 0 0 7 36.8504 11.5129 Tm /P <>BDC 10 0 0 10 51.9004 814.1973 Tm BT EMC (1,074)Tj EMC (2,748)Tj (major airports, which could lead to the)Tj BT ET BT ( )Tj EMC EMC /P <>BDC 6 0 0 6 236.6735 673.9528 Tm EMC BT /P <>BDC ET EMC /P <>BDC /P <>BDC ET EMC (aircraft operators fly their aircraft based on)Tj 9 0 0 9 550.1644 170.8898 Tm /P <>BDC EMC ET /P <>BDC /P <>BDC ( )Tj /P <>BDC ET (CFM56-7B27B3)Tj ET 0 Tc BT ET /P <>BDC 9 0 0 9 544.5056 302.8898 Tm ET (CFM56-7B26)Tj ET EMC /P <>BDC ET BT ( )Tj 9 0 0 9 215.4409 203.8898 Tm (CFM56-7B27B3)Tj BT 8 0 0 8 314.8021 771.7654 Tm 7 0 0 7 403.478 683.7654 Tm 9 0 0 9 392.5848 346.8898 Tm BT (of each aircrafts ASMs. BT 0 841.89 609.449 -841.89 re ET ( )Tj 9 0 0 9 411.0181 335.8898 Tm (31,416)Tj EMC ET -.02 Tc ( )Tj EMC (CFM56-7B26)Tj 7 0 0 7 158.74 441.7654 Tm 7 0 0 7 518.4953 100.9528 Tm 9 0 0 9 543.1342 192.8898 Tm /P <>BDC /P <>BDC In this case I believe TUI fly is the main customer. EMC /P <>BDC 8 0 0 8 394.0157 775.8898 Tm /P <>BDC /P <>BDC EMC EMC ET BT BT ET ( )Tj ( )Tj /P <>BDC BT [(T)92(axi out time - mins)]TJ 6 0 0 6 55.0668 659.9528 Tm ( )Tj /P <>BDC (l)Tj /P <>BDC /Artifact <>BDC EMC 7 0 0 7 444.737 100.7654 Tm /P <>BDC EMC EMC 10 0 0 10 49.2604 814.1973 Tm ET 7 0 0 7 539.8962 628.9528 Tm /P <>BDC (346,583)Tj EMC /P <>BDC 7 0 0 7 43.6039 144.9528 Tm /P <>BDC -.02 Tc BT 0 Tc /P <>BDC /F4 1 Tf /P <>BDC BT ( )Tj ( )Tj BT (The A320ceo is payload-limited to 127)Tj ET /P <>BDC BT (/S)Tj tank. /OC /MC4769 BDC ET 6.5 0 0 6.5 448.4195 722.9529 Tm ET ( )Tj ET BT EMC (improved engine efficiency and offer)Tj -.02 Tc ET /P <>BDC ( )Tj -.02 Tc BT /P <>BDC ET EMC ET ( )Tj ET 5.25 0 0 5.25 64.5461 11.5129 Tm 9 0 0 9 186.1613 49.8898 Tm /P <>BDC (1,272)Tj 9 0 0 9 191.9099 93.8898 Tm 6 0 0 6 434.3127 743.9528 Tm BT 0 J 0 j 15 w 10 M [] 0 d (category. ( )Tj BT ( )Tj /P <>BDC ET EMC BT ET /P <>BDC (performance )Tj EMC 9 0 0 9 394.0123 225.8898 Tm ET ET /P <>BDC BT EMC BT 10 0 0 10 417.91 814.1973 Tm 7 0 0 7 258.2805 67.7654 Tm /P <>BDC EMC [(AIR)7.1(CRAF)-12.9(T)18.1( P)30(A)52(YL)32(O)6.1(ADS IN )21(T)-11(W)25.9(O C)13.9(OMP)30(ARISON SCENARIOS )]TJ EMC f (2,349)Tj /P <>BDC 6 0 0 6 247.27 771.9528 Tm -.01 Tc /P <>BDC BT EMC ( )Tj 6 0 0 6 513.0339 673.9528 Tm BT /P <>BDC /P <>BDC EMC ET EMC ET ET BT /P <>BDC EMC EMC endobj (150)Tj 0 Tc (component is stated )Tj EMC 7 0 0 7 355.3163 331.7654 Tm BT ( )Tj ET /P <>BDC BT EMC ( )Tj BT -.02 Tc /P <>BDC /P <>BDC ET /P <>BDC Cheers Peter. ( )Tj 6.5 0 0 6.5 499.9091 611.9529 Tm 0 Tc 13 0 0 13 394.0123 434.8898 Tm BT EMC EMC EMC ET -.01 Tc 0 Tc ET /P <>BDC 6.5 0 0 6.5 174.4663 735.9529 Tm /P <>BDC (112)Tj EMC [(737-900E)-33(R)]TJ EMC EMC ET EMC 7 0 0 7 247.7395 232.7654 Tm (136)Tj -.02 Tc /P <>BDC 7 0 0 7 440.0906 276.9528 Tm BT EMC ET /P <>BDC ET /P <>BDC ET /P <>BDC BT (The fuel tank capacity means the)Tj /P <>BDC ( )Tj BT BT 1 w -.01 Tc 9 0 0 9 68.3339 500.8898 Tm BT ET 8 0 0 8 38.4438 591.9528 Tm /P <>BDC ( )Tj ET EMC [(7)-33(3)8(7-8)]TJ EMC /P <>BDC 7 0 0 7 535.5029 474.7654 Tm ET ET ET BT 9 0 0 9 197.3303 170.8898 Tm EMC (direction, with an initial heading ranging)Tj ET How much fuel do planes burn? EMC BT 7 0 0 7 387.0159 507.9528 Tm ET BT /P <>BDC BT 0 Tc /P <>BDC 518.735 0 l BT /P <>BDC EMC BT /P <>BDC ET 0 Tc BT ( )Tj ( )Tj EMC (5,395)Tj ET ET 0 Tc -.07 Tc EMC EMC 9 0 0 9 169.0072 511.8898 Tm 9 0 0 9 36.8504 456.8898 Tm 0 Tc EMC EMC ET EMC BT 9 0 0 9 214.7728 247.8898 Tm /P <>BDC EMC 6 0 0 6 247.4022 729.9528 Tm BT 169 0 obj 6.5 0 0 6.5 346.019 742.9529 Tm This makes it more challenging to)Tj ET /P <>BDC BT 7 0 0 7 99.8582 144.7654 Tm BT BT ET ET 9 0 0 9 36.8504 104.8898 Tm (1,058)Tj ( )Tj /P <>BDC /P <>BDC (industry is 210 US cents per USG for Jet A-)Tj ET EMC /P <>BDC /P <>BDC 9 0 0 9 538.7331 225.8898 Tm EMC EMC The 737 fuel quantity indication system has the following accuracy tolerances: 737-100/-200: 9 0 0 9 411.0097 555.8898 Tm /P <>BDC /P <>BDC ( )Tj (CFM56-5B4/P)Tj BT 6 0 0 6 246.7063 757.9528 Tm /P <>BDC ET I think in the table you are talking about the range where payload is limited by MTOW. [(R)30(elativ)12.9(e fuel consumption )]TJ 9 0 0 9 394.0157 544.8898 Tm ET ( )Tj 9 0 0 9 215.4313 368.8898 Tm 0 Tc BT /P <>BDC /P <>BDC BT 0 Tc ET (increase in engine efficiency to offer)Tj (dependent on the operators internal)Tj -.02 Tc ET /P <>BDC /P <>BDC /P <>BDC ( )Tj ET (I)Tj (977)Tj EMC ET 6.5 0 0 6.5 54.877 545.9529 Tm EMC (1,351)Tj ( )Tj ET (136)Tj BT BT /P <>BDC 9 0 0 9 378.9498 335.8898 Tm BT BT Since no two)Tj 7 0 0 7 82.2047 661.9528 Tm EMC /P <>BDC 6.5 0 0 6.5 280.3794 722.9529 Tm ( )Tj /P <>BDC BT ET BT /P <>BDC /P <>BDC BT EMC ET ET /P <>BDC ET ET ET 7 0 0 7 37.6993 353.9528 Tm ( )Tj 9 0 0 9 381.3998 126.8898 Tm BT EMC /P <>BDC ET BT ET ET EMC /P <>BDC 6 0 0 6 434.151 715.9528 Tm (737-800 results in a fuel cost per ASM that)Tj 7 0 0 7 517.6133 78.9528 Tm BT 7 0 0 7 365.035 606.9528 Tm BT (maximum passenger payload of 160. ET EMC ET EMC EMC BT 7 0 0 7 363.0612 430.9528 Tm 7 0 0 7 444.737 188.7654 Tm EMC ET (5,183)Tj ET EMC ( )Tj EMC /P <>BDC BT /P <>BDC ( )Tj BT (1,813)Tj ET BT EMC EMC EMC /P <>BDC /P <>BDC EMC 0 Tc ET 7 0 0 7 343.2355 496.7654 Tm 7 0 0 7 492.5963 716.7654 Tm 9 0 0 9 215.4313 291.8898 Tm f BT ( )Tj /P <>BDC BT /P <>BDC /P <>BDC 9 0 0 9 368.3979 38.8898 Tm 9 0 0 9 548.5375 225.8898 Tm ET 0 Tc /P <>BDC BT EMC EMC Pingback:Council Post: Aviation Is The Driving Force Of Hydrogen | QNewsHub, Pingback:When will the Boeing 737 MAX fly again? /F1 1 Tf EMC 0 Tc 7 0 0 7 520.6108 716.9528 Tm BT ET /F7 1 Tf /P <>BDC /P <>BDC /P <>BDC (136-145)Tj 7 0 0 7 508.2252 11.5129 Tm ET BT ET /F4 1 Tf EMC 7 0 0 7 363.2711 67.9528 Tm BT /P <>BDC 7 0 0 7 456.2165 199.7654 Tm ET EMC BT ( )Tj /P <>BDC ( )Tj /F6 1 Tf ET BT 7 0 0 7 520.6108 496.9528 Tm ET /P <>BDC EMC 6.5 0 0 6.5 64.6596 742.9529 Tm BT ET ET /P <>BDC 6.5 0 0 6.5 549.8557 702.9529 Tm EMC EMC BT -.01 Tc ET /P <>BDC Boeings main competitor is with Airbus. /P <>BDC 0 Tc BT ET ET /P <>BDC /P <>BDC BT EMC /P <>BDC 9 0 0 9 411.0181 104.8898 Tm BT 17 0 0 17 36.8606 758.6944 Tm 7 0 0 7 337.6855 67.9528 Tm /P <>BDC -.01 Tc ET ET 7 0 0 7 474.7064 342.9528 Tm /P <>BDC /GS2 gs BT 9 0 0 9 386.9059 280.8898 Tm EMC (ASM is 0.09 cents better for the A321neo. EMC ET BT EMC [(Engine b)6.1(ypass)]TJ -.02 Tc BT -.02 Tc ( )Tj 6.5 0 0 6.5 244.3754 565.9529 Tm ( )Tj /P <>BDC BT /P <>BDC 0 Tc ET EMC The Boeing 737-800 is a twin-engined short-to-medium-range narrowbody airliner with a capacity of maximum 189 passengers produced by the American manufacturer Boeing Commercial Airplanes. EMC /OC /MC5086 BDC ET EMC -.02 Tc ET /P <>BDC ET /P <>BDC BT ET ET EMC EMC BT ET /P <>BDC ET BT 7 0 0 7 37.0536 507.9528 Tm 7 0 0 7 380.2788 606.7654 Tm 13 0 0 13 53.8582 533.8898 Tm /GS2 gs /P <>BDC EMC BT [(R)30(elativ)12.9(e fuel burn )]TJ BT ET BT /P <>BDC 9 0 0 9 197.8317 379.8898 Tm 7 0 0 7 187.0858 111.9528 Tm (420)Tj -2.4549 -3.9026 l 7 0 0 7 537.7804 320.9528 Tm /P <>BDC EMC ET BT ( )Tj ET [(BOS-A)56.9(TL)]TJ 7 0 0 7 473.8245 265.9528 Tm The AFM limits are higher, but not normally achievable with standard SG's. EMC ( )Tj EMC /P <>BDC BT 7 0 0 7 518.4953 199.9528 Tm EMC EMC 9 0 0 9 203.5468 379.8898 Tm 7 0 0 7 474.3564 529.9528 Tm EMC ET )Tj EMC /P <>BDC BT of gauges. EMC ET BT 7 0 0 7 54.5916 144.7654 Tm /P <>BDC /P <>BDC .151 .147 .15 rg ET EMC -.02 Tc ( )Tj /P <>BDC 0 Tc ET 7 0 0 7 473.8245 309.9528 Tm /P <>BDC 5 0 0 5 484.5872 11.5129 Tm EMC ET /P <>BDC 7 0 0 7 554.7883 122.7654 Tm BT /P <>BDC ( )Tj 9 0 0 9 362.6813 357.8898 Tm /P <>BDC ET EMC (types, but it is worth noting that in)Tj BT BT BT 7 0 0 7 491.7142 331.7654 Tm EMC EMC 6.5 0 0 6.5 448.4585 689.9529 Tm 7 0 0 7 37.6993 375.9528 Tm BT (distance - nm )Tj ( )Tj BT ET /P <>BDC BT BT 9 0 0 9 360.9261 280.8898 Tm BT ET EMC /P <>BDC .008 Tc (scenarios have been run. BT /P <>BDC 7 0 0 7 490.5101 716.9528 Tm -.02 Tc ET EMC BT ( )Tj 7 0 0 7 131.6494 672.7654 Tm EMC EMC EMC 6 0 0 6 539.8061 760.9528 Tm /P <>BDC 9 0 0 9 252.5189 181.8898 Tm EMC /P <>BDC ( )Tj /P <>BDC BT ( )Tj 9 0 0 9 411.0181 192.8898 Tm -.02 Tc /F1 1 Tf BT EMC EMC ( )Tj ET BT (108)Tj 7 0 0 7 258.5394 100.7654 Tm BT /P <>BDC ( )Tj /P <>BDC /P <>BDC The 737-8 offers)Tj EMC 7 0 0 7 294.4014 573.7654 Tm 6.5 0 0 6.5 382.478 545.9529 Tm ET /P <>BDC /P <>BDC .151 .147 .15 rg (The wind speed was based on an 85%)Tj 7 0 0 7 404.101 210.7654 Tm This is the same)Tj -.02 Tc BT /P <>BDC 7 0 0 7 258.2805 210.7654 Tm ET (20)Tj -.02 Tc BT 0 Tc EMC BT -.02 Tc EMC 9 0 0 9 394.0237 335.8898 Tm BT BT BT BT /P <>BDC BT 8 0 0 8 314.4333 745.9528 Tm ET ( )Tj EMC ET 7 0 0 7 338.3085 199.9528 Tm /P <>BDC 7 0 0 7 380.2788 199.7654 Tm /P <>BDC /P <>BDC /OC /MC828 BDC 9 0 0 9 383.9197 412.8898 Tm /P <>BDC BT ( )Tj (14 the sectors in this study. 0 Tc ET /P <>BDC BT /P <>BDC EMC 0 Tc ET ET 7 0 0 7 297.632 485.9528 Tm 9 0 0 9 411.0097 192.8898 Tm ( )Tj /P <>BDC 7 0 0 7 158.74 562.7654 Tm .559 .331 .619 rg ET /P <>BDC BT BT Irkut MC-21, Russias homegrown modern airliner. -.01 Tc BT 0 Tc BT ( )Tj EMC ( )Tj .964 .834 .406 rg (150)Tj Boeing 737 MAX 9 reviews and traveller comments. /P <>BDC /P <>BDC EMC 7 0 0 7 158.74 584.7654 Tm 7 0 0 7 314.6398 727.7654 Tm BT (5B4/P)Tj (45,276)Tj -.02 Tc EMC /P <>BDC 0 Tc BT .41 .161 .508 rg BT 9 0 0 9 527.5473 390.8898 Tm 8 0 0 8 421.0237 771.7654 Tm BT -.02 Tc /P <>BDC /P <>BDC /P <>BDC BT BT ( )Tj 7 0 0 7 439.2087 320.9528 Tm EMC -.01 Tc ET /P <>BDC BT ( )Tj ET 7 0 0 7 363.2711 540.9528 Tm EMC /F4 1 Tf EMC ( )Tj ET EMC ET ET ( )Tj 7 0 0 7 338.3085 144.9528 Tm BT ET EMC (1,272)Tj /Artifact <>BDC /P <>BDC /P <>BDC ( )Tj /P <>BDC 7 0 0 7 299.0601 166.9528 Tm /P <>BDC /P <>BDC BT EMC 9 0 0 9 215.4409 489.8898 Tm /P <>BDC ( )Tj 6.5 0 0 6.5 243.7903 611.9529 Tm EMC 0 Tc EMC (0.0121)Tj BT The A320neo in this study)Tj 8 0 0 8 136.4919 591.9528 Tm EMC -.02 Tc ET ET EMC ( )Tj /P <>BDC (BOS-MIA)Tj 0 Tc -.07 Tc EMC BT /P <>BDC Hiya, 7 0 0 7 363.2711 210.9528 Tm 10 0 0 10 52.6304 814.1973 Tm ( )Tj /P <>BDC (passenger numbers are 136 for the)Tj 9 0 0 9 555.1324 148.8898 Tm /P <>BDC EMC (has resulted in them requiring less galley)Tj EMC EMC [(737-900E)-33(R)]TJ ( )Tj ( )Tj ( )Tj 9 0 0 9 197.9514 148.8898 Tm /P <>BDC 7 0 0 7 247.7395 144.7654 Tm BT /P <>BDC EMC /P <>BDC BT ET BT ET 8 0 0 8 302.5117 619.9528 Tm EMC /P <>BDC (2,731)Tj (0.0112)Tj EMC BT /P <>BDC ET /P <>BDC EMC (170)Tj /P <>BDC BT EMC /P <>BDC ET ET 6.5 0 0 6.5 398.3298 650.9529 Tm EMC -.02 Tc (CFM56-5B4/P)Tj /P <>BDC EMC ( )Tj ET BT 7 0 0 7 337.6855 562.9528 Tm ( )Tj ET /Artifact <>BDC https://www.researchgate.net/publication/302903333_On_Boeing_737_-_300_Wing_Aerodynamics_Calculations_Based_on_VLM_Theory. ET ET /P <>BDC BT ET BT ET EMC )Tj 7 0 0 7 131.6494 276.7654 Tm 0 Tc EMC EMC /P <>BDC EMC EMC /P <>BDC /P <>BDC 9 0 0 9 565.9882 214.8898 Tm 6 0 0 6 450.9814 701.9528 Tm ET EMC -.01 Tc EMC (0.0139)Tj BT EMC ET (289)Tj EMC BT (288)Tj EMC /P <>BDC BT BT EMC ET BT 0 Tc /P <>BDC ET 9 0 0 9 372.4479 368.8898 Tm 6.5 0 0 6.5 244.4599 702.9529 Tm EMC ET /P <>BDC ET [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ [(equal-siz)6.1(ed 737NG counterpar)-23(ts and A320ceo)]TJ [(W)7.1(ind component - kts)]TJ 7 0 0 7 444.737 133.7654 Tm BT BT 9 0 0 9 554.6907 159.8898 Tm EMC /P <>BDC ( )Tj 9 0 0 9 51.0236 445.8898 Tm )Tj 10 0 0 10 422.8 814.1973 Tm ( )Tj EMC EMC 9 0 0 9 197.3398 214.8898 Tm EMC EMC Boeing made BT 9 0 0 9 394.0315 720.8898 Tm ET EMC Q EMC ( )Tj EMC BT (hugely successful. (104)Tj 9 0 0 9 186.3413 291.8898 Tm 0 Tc 9 0 0 9 418.9315 59.9073 Tm EMC BT /P <>BDC /P <>BDC BT 9 0 0 9 215.4409 258.8898 Tm EMC EMC /P <>BDC ET These are: Below is a table of the main features and specifications for the Boeing 737 family of aircraft. ( )Tj 7 0 0 7 380.2788 518.7654 Tm BT (and in fuel burn per ASM. EMC ET 9 0 0 9 195.4763 258.8898 Tm BT EMC EMC ET ET BT ET BT ( )Tj /P <>BDC /P <>BDC EMC BT 7 0 0 7 53.8582 452.7654 Tm ( )Tj BT EMC could you point me in the right direction or tell me what the weight of the landing gear would be on a 737? system is essentially automatic. (22)Tj EMC EMC -.02 Tc BT ET ET EMC BT BT /P <>BDC BT /F6 1 Tf 0 Tc ET ( )Tj On the longer sectors, however, the)Tj ET EMC /P <>BDC /P <>BDC must be switched OFF when both LP lights illuminate. BT ET /TT2 1 Tf BT /P <>BDC ( )Tj BT BT ( )Tj ET EMC EMC BT /P <>BDC I am looking for the radius of the fuselage specifically the cargo door. /P <>BDC EMC 8 0 0 8 43.6039 661.9528 Tm -.02 Tc BT ET 6.5 0 0 6.5 397.1339 689.9529 Tm ET 9 0 0 9 529.6118 302.8898 Tm BT ET EMC ET 9 0 0 9 433.049 544.8898 Tm EMC ET ( )Tj EMC EMC EMC Q EMC (737-8)Tj support combustion. (fuel consumption and cost per seat or per)Tj (\(see table, this)Tj EMC /OC /MC199 BDC /P <>BDC 9 0 0 9 79.8339 456.8898 Tm endobj 9 0 0 9 36.8583 368.8898 Tm ET BT EMC ET BT ET BT 13 0 0 13 205.5668 412.8898 Tm ET ( )Tj ( )Tj ( )Tj 7 0 0 7 491.392 727.9528 Tm /P <>BDC /P <>BDC BT /P <>BDC BT ET ( )Tj 9 0 0 9 528.0345 511.8898 Tm ET BT Airbus A320 Interior Inside the cabin of this city hopper. [(737-900E)-33(R)]TJ 9 0 0 9 563.0415 775.8898 Tm ET EMC ET /P <>BDC /P <>BDC 9 0 0 9 36.8504 126.8898 Tm 9 0 0 9 36.8504 170.8898 Tm EMC EMC BT EMC /P <>BDC /P <>BDC EMC BT EMC /P <>BDC BT 7 0 0 7 210.1137 67.7654 Tm EMC 5.25 0 0 5.25 525.4061 11.5132 Tm ET 6.5 0 0 6.5 276.4014 650.9529 Tm EMC EMC EMC EMC ET ET EMC 9 0 0 9 185.7888 489.8898 Tm BT (compare the aircraft types on a fair or)Tj /P <>BDC 9 0 0 9 53.8338 82.8898 Tm ( )Tj EMC 9 0 0 9 187.2749 610.8898 Tm ET BT ( )Tj EMC BT BT (179)Tj 9 0 0 9 204.3477 335.8898 Tm EMC 9 0 0 9 394.0315 225.8898 Tm /P <>BDC ET /P <>BDC 8 0 0 8 439.9149 760.9528 Tm 9 0 0 9 373.2203 368.8898 Tm ET EMC (Block time)Tj /P <>BDC /P <>BDC /P <>BDC BT 0 Tc ET EMC EMC 7 0 0 7 403.7368 705.7654 Tm BT EMC ET EMC 7 0 0 7 440.6226 683.9528 Tm /P <>BDC EMC (105,000lbs. -2.9413 -1.4846 -3.0524 -2.0356 -3.053 -2.8052 c /P <>BDC BT ET 10 0 0 10 52.7604 814.1973 Tm BT 7 0 0 7 141.7322 67.9528 Tm /P <>BDC 9 0 0 9 383.0289 544.8898 Tm /P <>BDC EMC EMC BT (72% of the NG fleet in service. /Artifact <>BDC /P <>BDC ET /P <>BDC EMC 9 0 0 9 540.3981 588.8898 Tm BT ( )Tj .964 .834 .406 rg EMC ET ET refuelling panel to AUX TANKS. These have led to smaller and)Tj ( )Tj ET EMC EMC EMC EMC (when using a cost index. EMC ( )Tj /P <>BDC 0 Tw /P <>BDC ( )Tj BT 0 Tc 7 0 0 7 277.3936 265.9528 Tm All the flights are in a westerly)Tj 9 0 0 9 53.8582 390.8898 Tm /P <>BDC ET BT (SEA, SFO, YVR and LAX. EMC EMC BT BT EMC 7 0 0 7 474.3564 606.9528 Tm ET /P <>BDC /P <>BDC /P <>BDC ( )Tj -.01 Tc /F6 1 Tf ( )Tj BT ET EMC BT /P <>BDC ET ET BT /P <>BDC BT .014984 841.89 609.45 -841.89 re /P <>BDC ET Q -.005 Tc BT /P <>BDC BT ( )Tj -.01 Tc BT /P <>BDC ET 7 0 0 7 204.0935 584.7654 Tm 0 Tc 7 0 0 7 258.2805 507.7654 Tm BT 7 0 0 7 518.4953 320.9528 Tm 53.858 511.715 518.74 293.325 re BT /P <>BDC BT ET EMC /P <>BDC /P <>BDC /P <>BDC /P <>BDC BT ( )Tj -.01 Tc The massive 800 variant is powered by two 2Snecma / CFM56-7B27 underwing turbofans putting out a respectable 27,300 pound-force. ET ET ET ET 7 0 0 7 141.7322 463.9528 Tm ()Tj ET EMC EMC 7 0 0 7 337.9444 617.9528 Tm BT ET Thank you. /P <>BDC ET ET EMC ( )Tj (150)Tj 9 0 0 9 229.6141 49.8898 Tm 8 0 0 8 256.0704 577.9528 Tm EMC 7 0 0 7 99.8582 661.7654 Tm /P <>BDC EMC EMC 7 0 0 7 337.6855 210.9528 Tm 9 0 0 9 546.6454 60.8898 Tm 9 0 0 9 68.3339 533.8898 Tm BT 0 Tc ET EMC BT EMC /P <>BDC (generated per route. 7 0 0 7 383.0719 672.7654 Tm BT 7 0 0 7 108.6215 144.9528 Tm EMC /P <>BDC EMC 7 0 0 7 82.8504 353.9528 Tm 7 0 0 7 403.478 617.7654 Tm 9 0 0 9 215.4313 335.8898 Tm EMC BT ET .001 Tc ( )Tj -.02 Tc 9 0 0 9 543.5425 522.8898 Tm BT /P <>BDC 6.5 0 0 6.5 531.9417 637.9529 Tm -.02 Tc ( )Tj 7 0 0 7 298.1781 67.9528 Tm 9 0 0 9 411.0097 379.8898 Tm /P <>BDC [(737-900E)-33(R)]TJ BT (performed with both engines operating to)Tj 7 0 0 7 95.225 11.5132 Tm 7 0 0 7 279.1575 507.9528 Tm /P <>BDC ET 7 0 0 7 315.5217 562.7654 Tm ET EMC BT 7 0 0 7 338.3085 320.9528 Tm BT /P <>BDC BT EMC (are taxi fuel burn, flight fuel burn, the)Tj -.02 Tc ET 0 Tc 9 0 0 9 232.438 456.8898 Tm ( )Tj 9 0 0 9 411.0181 71.8898 Tm EMC -.02 Tc ET (150)Tj (used for conversion to volume. EMC /P <>BDC -.02 Tc The fuel tank was instrumented with gas sample tubing and thermocouples to (All the aircraft were evaluated using)Tj )Tj 6 0 0 6 496.2633 701.9528 Tm EMC 0 Tc ( )Tj 9 0 0 9 36.8504 93.8898 Tm EMC ET This is equivalent to)Tj 0 Tc /P <>BDC ET BT EMC EMC 9 0 0 9 36.8504 170.8898 Tm 9 0 0 9 425.183 346.8898 Tm EMC ( )Tj /P <>BDC (1,272)Tj 0 Tc ET ( )Tj /P <>BDC ET 7 0 0 7 247.7395 628.7654 Tm EMC -.01 Tc EMC (0.0157)Tj 6 0 0 6 527.6392 757.9528 Tm 9 0 0 9 195.0251 434.8898 Tm 7 0 0 7 439.8175 727.9528 Tm (2,731)Tj BT /P <>BDC -.02 Tc BT BT (0.0140)Tj /P <>BDC EMC /P <>BDC (Although there have recently been)Tj 0 Tc ET /P <>BDC BT ET ( )Tj BT ET 7 0 0 7 343.2355 705.7654 Tm 9 0 0 9 192.5225 489.8898 Tm ET -.02 Tc BT 7 0 0 7 473.8245 320.9528 Tm EMC 7 0 0 7 37.6993 331.9528 Tm BT EMC ET /P <>BDC EMC EMC ( )Tj ET 7 0 0 7 429.157 617.9528 Tm 7 0 0 7 362.3891 364.9528 Tm /P <>BDC ET (737-9)Tj ET /OC /MC3432 BDC BT /P <>BDC BT ET BT ( )Tj BT /P <>BDC ( )Tj (and 4.3% better performance on the 737-)Tj ET /P <>BDC EMC 7 0 0 7 108.6215 265.9528 Tm ET 7 0 0 7 439.2087 364.9528 Tm BT EMC -.02 Tc BT .151 .147 .15 rg 9 0 0 9 75.273 445.8898 Tm /P <>BDC ( )Tj BT (increases to an average of 3.3% for the)Tj ET /P <>BDC ET EMC /P <>BDC 8 0 0 8 394.0157 753.8898 Tm ET 378 0 0 271.8 -.30716 30.902 cm BT BT /P <>BDC 6.5 0 0 6.5 448.257 598.9529 Tm EMC ET ( )Tj /P <>BDC BT [(F)-21(LL/47)]TJ /P <>BDC /P <>BDC 6 0 0 6 403.5248 659.9528 Tm 10 0 0 10 55.0104 814.1973 Tm BT (213,848)Tj /P <>BDC 9 0 0 9 394.0237 379.8898 Tm ( )Tj ][F$, c;9M$ C[\SU~s#4B#g"DH V6S[_t099J'Nbqur((h\Yf'urV(nYYW6V*f]+ 8 0 0 8 404.5618 771.9528 Tm /P <>BDC /P <>BDC 7 0 0 7 387.0159 727.9528 Tm /TT2 1 Tf EMC ET EMC -.01 Tc ET BT BT BT 0 Tc /P <>BDC /P <>BDC BT /P <>BDC ( )Tj EMC /P <>BDC (977)Tj (10)Tj /P <>BDC (737-8 has a 0.8-3.0% higher trip fuel burn than)Tj BT ET /GS2 gs 7 0 0 7 337.6855 221.9528 Tm (136)Tj EMC hello, i would like to know about the technology which applied on B737 NG flight cockpit lay out include its characteristics (advantages and disadvantages), especially on PFD and MFD, can you tell me or send me a link which discuss about that? -.02 Tc EMC BT /P <>BDC BT /P <>BDC EMC ( )Tj ( )Tj /P <>BDC BT 0 Tc /P <>BDC (l)Tj ET ( )Tj 7 0 0 7 230.7317 562.9528 Tm EMC BT On older aircraft the trimmers were accessible from the /P <>BDC BT 0 Tc EMC /P <>BDC BT 7 0 0 7 362.3891 320.9528 Tm /P <>BDC EMC BT -.005 Tc EMC ET ET BT ET 8 0 0 8 354.3239 771.7654 Tm 7 0 0 7 258.2805 705.7654 Tm [(R)30(elativ)12.9(e oper)10(ational cost )]TJ ET ( )Tj ET )Tj 9 0 0 9 496.6703 148.8898 Tm 9 0 0 9 211.0081 82.8898 Tm ET 7 0 0 7 554.7883 463.7654 Tm /P <>BDC (0.0140)Tj 9 0 0 9 394.0315 588.8898 Tm EMC ET 9 0 0 9 354.313 236.8898 Tm [(trip fuel burn compar)10(ed to the 737-800. EMC ( )Tj BT 7 0 0 7 554.7883 265.7654 Tm /P <>BDC The fuel was fed -.02 Tc .014984 841.89 609.45 -841.89 re ET fuel pumps were running in high ambient temperatures with empty or almost empty 7 0 0 7 379.3969 188.7654 Tm BT 9 0 0 9 53.8582 434.8898 Tm /P <>BDC BT ( )Tj EMC EMC Thanks now. ET 7 0 0 7 338.6433 386.7654 Tm /P <>BDC BT ( )Tj 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. BT ET EMC 7 0 0 7 387.0159 595.9528 Tm /P <>BDC 0 Tc ET EMC /P <>BDC /P <>BDC ET EMC 0 Tc ET 6 0 0 6 115.2799 687.9528 Tm /Artifact <>BDC /P <>BDC ET /P <>BDC 6.5 0 0 6.5 375.6529 663.9529 Tm ET /P <>BDC EMC ( )Tj (higher OEW. 0 Tc (150)Tj BT ( )Tj (I)Tj BT EMC EMC All data presented is for entertainment purposes and should not be used operationally. ( )Tj 6.5 0 0 6.5 432.488 558.9529 Tm (148,592)Tj -.02 Tc .176 .307 .621 rg ( )Tj ET EMC BT 0 Tc BT EMC 6.5 0 0 6.5 499.1812 702.9529 Tm ( )Tj ( )Tj -.5815 -.9071 l 7 0 0 7 490.8321 166.7654 Tm (737-9)Tj /P <>BDC ET ET (test programme is well underway for entry)Tj EMC ( )Tj .151 .147 .15 rg 7 0 0 7 456.2165 265.7654 Tm (146,300)Tj ET /P <>BDC EMC 0 Tc BT 9 0 0 9 215.4313 423.8898 Tm /P <>BDC (0.0115)Tj ET EMC BT BT (A321neo)Tj ET 7 0 0 7 508.4124 496.7654 Tm /F7 1 Tf 6 0 0 6 379.0815 771.9528 Tm BT /P <>BDC ET BT BT 9 0 0 9 536.6833 500.8898 Tm 0 Tc 9 0 0 9 232.4217 192.8898 Tm 7 0 0 7 53.8582 11.5132 Tm EMC 9 0 0 9 394.0123 368.8898 Tm BT ET 9 0 0 9 195.3055 324.8898 Tm ( )Tj /GS2 gs BT ( N)Tj (13.1% to 18.9% improvements in block)Tj EMC BT ( )Tj -.02 Tc EMC (better for the A321neo due to its increased)Tj EMC EMC ET ET /P <>BDC /P <>BDC ( )Tj 7 0 0 7 82.8504 221.9528 Tm 9 0 0 9 206.8842 522.8898 Tm 0 Tc 737-600/-700/-800/-900 without densitometer: (thrust rating could provide the 737 MAX)Tj BT /P <>BDC BT BT /OC /MC5061 BDC /P <>BDC EMC (BOS-MIA)Tj ( )Tj /P <>BDC ET 6 0 0 6 308.6461 743.9528 Tm BT /P <>BDC BT ET 7 0 0 7 141.7322 408.9528 Tm 9 0 0 9 364.9498 511.8898 Tm /P <>BDC -.02 Tc BT BT ET ( )Tj BT EMC /P <>BDC 9 0 0 9 53.8338 60.8898 Tm 7 0 0 7 187.0858 606.9528 Tm /GS1 gs (that in scenario 1 both aircraft carry 170)Tj (977)Tj ET 9 0 0 9 53.8582 456.8898 Tm ( )Tj (0.0142)Tj ET 7 0 0 7 230.7317 320.9528 Tm ( )Tj BT (original equipment manufacturer \(OEM\))Tj 7 0 0 7 380.2788 408.7654 Tm 7 0 0 7 37.0536 716.9528 Tm 6.5 0 0 6.5 427.5934 742.9529 Tm ET /P <>BDC /P <>BDC (is 16/30/114, giving a maximum passenger)Tj /P <>BDC /P <>BDC ( )Tj EMC /P <>BDC ET /P <>BDC (configuration as the 737-900ER\(W\), but)Tj ET ET BT BT -.02 Tc ( )Tj Therefore, the Boeing 777-200 can carry 24,125 more gallons of fuel than the Boeing 737-800. EMC /P <>BDC /P <>BDC ET /P <>BDC EMC (manufacturers support these aircraft types)Tj /P <>BDC /P <>BDC 7 0 0 7 60.6117 540.7654 Tm ET ET ET (483)Tj ET -.01 Tc /P <>BDC EMC /P <>BDC /P <>BDC 8 0 0 8 54.8194 771.9529 Tm BT /P <>BDC 7 0 0 7 473.8245 122.9528 Tm .151 .147 .15 rg 0 Tc (0.0150)Tj BT EMC /P <>BDC (a 3.3% advantage for the A321neo on the)Tj BT /P <>BDC 7 0 0 7 298.3957 430.9528 Tm 7 0 0 7 554.7883 628.7654 Tm 7 0 0 7 445.619 529.7654 Tm BT 7 0 0 7 37.6993 386.9528 Tm EMC ET /P <>BDC EMC /P <>BDC BT BT EMC ET -.02 Tc BT 9 0 0 9 53.8578 434.8898 Tm BT -.02 Tc BT 0 Tc /P <>BDC ( )Tj BT BT ET BT 9 0 0 9 536.1277 247.8898 Tm

Jazmin Tyler Uc Berkeley, The Lincoln Highway Characters, Fred Street England Physio, Articles OTHER