[(A3)24.9(20ceo v)12.9(ersus A3)24.9(20neo )]TJ EMC (largest operating costs for any aircraft)Tj 0 Tc 9 0 0 9 379.7168 225.8898 Tm The -800 has sold strongly since its launch . (174,165)Tj 9 0 0 9 191.4329 786.8898 Tm BT BT /P <>BDC BT ET /P <>BDC EMC 7 0 0 7 508.4124 441.7654 Tm BT BT 161.574 0 l -.02 Tc (832)Tj ET 7 0 0 7 299.0601 100.9528 Tm BT /P <>BDC ET ( )Tj -.01 Tc 0 Tc ET ET 9 0 0 9 545.8785 489.8898 Tm BT BT (273,750)Tj (A)Tj 9 0 0 9 369.3136 698.8898 Tm 9 0 0 9 215.433 379.8898 Tm ( )Tj 7 0 0 7 487.0872 11.5129 Tm 0 Tc (scenario 2, which uses an 85% passenger)Tj EMC BT BT 0 Tc ET /F2 1 Tf BT (. ET 10 0 0 10 37.304 794.2914 Tm (generated per route. 9 0 0 9 53.8338 269.8898 Tm )Tj 9 0 0 9 215.4409 500.8898 Tm ( )Tj /P <>BDC ET 7 0 0 7 537.7804 67.9528 Tm -.02 Tc 9 0 0 9 380.2477 247.8898 Tm EMC 7 0 0 7 54.7071 694.7654 Tm EMC ( )Tj BT ET EMC In addition, with many airlines)Tj [(v)21(ariant)]TJ EMC BT ( )Tj ET /P <>BDC 7 0 0 7 258.2805 133.7654 Tm /P <>BDC /F6 1 Tf /P <>BDC (39,270)Tj ET (fuel burn than the 737-8. -.02 Tc EMC /P <>BDC EMC BT S BT (484)Tj [(OM)8(M)-13(E)-25(R)7(C)8(E)]TJ EMC 8 0 0 8 43.6039 731.9528 Tm /GS1 gs ET /P <>BDC 9 0 0 9 195.5727 104.8898 Tm ET ( )Tj 6.5 0 0 6.5 531.2397 565.9529 Tm /P <>BDC ET ET EMC .0081 Tc 9 0 0 9 53.8582 192.8898 Tm ET EMC BT /P <>BDC )Tj 9 0 0 9 425.183 258.8898 Tm ET /P <>BDC ET 6.5 0 0 6.5 64.6596 650.9529 Tm BT (35,112)Tj 0 Tc (0.0177)Tj -.02 Tc BT /P <>BDC )Tj BT /P <>BDC BT [(BOS-C)-8.1(V)18.1(G)]TJ -.02 Tc 9 0 0 9 411.0097 313.8898 Tm /P <>BDC BT BT how can i know the material of 737NGs nose landing gear lower drag strut?thank you. ET /P <>BDC 0 Tc (performance )Tj ET ET EMC /P <>BDC /P <>BDC ET BT 0 Tc BT -.02 Tc EMC EMC ( )Tj 8 0 0 8 136.4919 577.9528 Tm /P <>BDC /P <>BDC (CFM56-5B4/P)Tj (2,218)Tj /P <>BDC BT EMC (0.0123)Tj 8 0 0 8 124.845 633.9528 Tm EMC Boeing 737 History, the story behind this hugely successful City Jet. EMC 7 0 0 7 82.2047 639.9528 Tm /P <>BDC ET 0 Tc .023 .567 .626 rg (bypass ratio than the A320/321neo. EMC Boeing 737 800 Hainan Airlines Alan Wilson. /P <>BDC ET 7 0 0 7 258.2805 617.7654 Tm ET (146,550)Tj ET EMC /P <>BDC EMC ( )Tj ET 7 0 0 7 294.4014 672.7654 Tm ( )Tj ET /P <>BDC 7 0 0 7 321.6356 166.9528 Tm .151 .147 .15 rg EMC /P <>BDC EMC ET /P <>BDC ET 7 0 0 7 297.632 518.9528 Tm BT 9 0 0 9 542.2986 192.8898 Tm 9 0 0 9 549.8977 313.8898 Tm 9 0 0 9 232.4217 368.8898 Tm -.02 Tc 0 Tc /P <>BDC ET ET EMC ET ET 9 0 0 9 53.8582 786.8898 Tm BT ET ET EMC /P <>BDC ET /P <>BDC EMC /P <>BDC BT ET -.02 Tc 8 0 0 8 187.3427 661.9528 Tm ET EMC /P <>BDC 17 0 0 17 550.9253 758.6944 Tm ET 9 0 0 9 53.8338 346.8898 Tm BT ET 7 0 0 7 279.1575 210.9528 Tm ET ET /P <>BDC - Smiths. 9 0 0 9 232.4217 247.8898 Tm /P <>BDC /P <>BDC /P <>BDC BT /P <>BDC EMC EMC (2,516)Tj 9 0 0 9 212.2888 93.8898 Tm 0 Tc BT /P <>BDC /P <>BDC [(A3)24.9(20ceo v)12.9(ersus 7)-33(3)8.1(7-800 )]TJ BT EMC 786 0 obj (. EMC 9 0 0 9 411.0181 456.8898 Tm EMC 9 0 0 9 411.0181 412.8898 Tm (cents, with a network average)Tj 7 0 0 7 131.6494 177.7654 Tm /P <>BDC EMC BT EMC EMC BT ET EMC /P <>BDC 0 Tc BT ET ET /P <>BDC /P <>BDC /P <>BDC ( )Tj -.02 Tc ET ( )Tj 7 0 0 7 204.0935 210.7654 Tm 7 0 0 7 490.5101 716.9528 Tm 9 0 0 9 201.162 500.8898 Tm EMC EMC BT /P <>BDC 6.5 0 0 6.5 296.2827 598.9529 Tm EMC EMC 9 0 0 9 572.0386 115.8898 Tm (10)Tj EMC (5,121)Tj EMC ET /P <>BDC ET (34,650)Tj ET /P <>BDC The APU uses fuel from the number 1 tank. 19.843 0 l 0 Tc ( )Tj EMC Boeing 797, MNA-6x and MNA-7x. ET either 3,065 or 1,421 litre capacities. (176)Tj .151 .147 .15 rg EMC /P <>BDC /P <>BDC EMC /P <>BDC BT BT /Figure <>BDC /P <>BDC BT BT BT 9 0 0 9 213.1228 368.8898 Tm BT ET EMC /P <>BDC ET EMC EMC ( )Tj /P <>BDC 7 0 0 7 491.4046 100.9528 Tm ET EMC 8 0 0 8 187.3427 591.9528 Tm /P <>BDC /P <>BDC 0 Tc /P <>BDC EMC /P <>BDC (A321ceo was payload-limited on the route)Tj BT EMC ET (of the Boeing aircraft, with the A321ceo)Tj (170)Tj 7 0 0 7 230.7317 485.9528 Tm 0 Tc ET BT EMC ( )Tj EMC EMC /P <>BDC /P <>BDC ET 9 0 0 9 394.0123 115.8898 Tm 0 Tc ET /P <>BDC 6.5 0 0 6.5 346.7208 624.9529 Tm BT 0 Tc BT -.01 Tc ET BT ( )Tj ET EMC q 6.5 0 0 6.5 397.7514 598.9529 Tm (171,520)Tj EMC ( )Tj ET (table, page 19\))Tj /P <>BDC EMC (31,416)Tj BT EMC BT /P <>BDC /P <>BDC EMC -.02 Tc ET Do you have the estimated production material used for the 737 Next Gen? BT ( )Tj ET ( )Tj 7 0 0 7 141.7322 188.9528 Tm 7 0 0 7 297.632 683.9528 Tm BT ET ET /P <>BDC /P <>BDC 9 0 0 9 386.9059 280.8898 Tm /P <>BDC BT EMC EMC EMC EMC EMC (sectors, particularly the shorter ones,)Tj BT ET /P <>BDC EMC ET ( )Tj )Tj EMC ET (70)Tj ET 6 0 0 6 555.6477 729.9528 Tm endobj 7 0 0 7 439.2087 67.9528 Tm (The main operating parameters are: )Tj ET 7 0 0 7 294.4014 727.7654 Tm EMC ET (0.0149)Tj /P <>BDC ET BT 0 Tc 7 0 0 7 82.2047 661.9528 Tm ET 7 0 0 7 430.039 694.9528 Tm /P <>BDC BT 7 0 0 7 141.7322 210.9528 Tm -.02 Tc (2,518)Tj BT /P <>BDC 7 0 0 7 507.7893 639.7654 Tm BT 6.5 0 0 6.5 448.2959 585.9529 Tm /P <>BDC It rolled out of the productionhangar on June 30th, 1997 and made her maiden flight on the 31st of July. EMC 6.5 0 0 6.5 64.6596 545.9529 Tm ( )Tj EMC 9 0 0 9 207.4166 137.8898 Tm EMC ( )Tj EMC ET BT BT 0 Tc EMC 8 0 0 8 386.5214 771.9528 Tm 0 Tc 9 0 0 9 214.7728 247.8898 Tm BT EMC 6 0 0 6 61.517 743.9528 Tm 5 0 0 5 92.725 11.5132 Tm Wing provisioning for the 737-800 adds approx. /P <>BDC BT ( )Tj EMC /GS1 gs ET EMC ET /P <>BDC ET /P <>BDC ET 0 Tc /P <>BDC BT BT 10 0 0 10 37.304 794.2914 Tm BT ET BT EMC 0 Tc -.02 Tc BT ET ( )Tj ( )Tj ET 9 0 0 9 105.3138 82.8898 Tm EMC ( )Tj EMC ET BT /P <>BDC ET ( )Tj BT /GS1 gs EMC EMC (900ER\(W\) due to the heavier payload. ET /P <>BDC EMC (192 seats versus 179 on the 737-9. EMC BT BT ET /P <>BDC ET ET BT ( )Tj ET 7 0 0 7 247.7395 529.7654 Tm -.02 Tc ( )Tj ET BT /P <>BDC It is notably more stretched than and based off of the original 400. /P <>BDC ET EMC /P <>BDC -.02 Tc /P <>BDC EMC EMC EMC /P <>BDC 7 0 0 7 474.7064 276.9528 Tm EMC /P <>BDC EMC /P <>BDC 7 0 0 7 54.5916 144.7654 Tm /P <>BDC ( )Tj EMC /P <>BDC /P <>BDC ( The cruise speed and flight profile )Tj BT 19.843 0 l EMC /P <>BDC ET BT ET ET (CFM56-)Tj /P <>BDC 7 0 0 7 316.0679 309.7654 Tm Fuel remains one of the)Tj /P <>BDC EMC -.02 Tc EMC 6.5 0 0 6.5 54.877 545.9529 Tm [(CFM L)17.1(E)-8.1(AP-1A26)]TJ ET ( )Tj EMC (65,552)Tj -.02 Tc ET /P <>BDC /P <>BDC BT ET 0 Tc ET 9 0 0 9 232.4408 720.8898 Tm ( C)Tj ET ( )Tj 9 0 0 9 36.8504 192.8898 Tm Boeing has developed a Nitrogen Generating System (NGS) which decreases the EMC (1,162)Tj ET BT BT .023 .567 .626 rg -.02 Tc 518.735 0 l ( )Tj ET /P <>BDC BT BT ET (\(see table, this page\))Tj EMC EMC 9 0 0 9 394.0315 247.8898 Tm ET EMC EMC I not sure what you mean by a and b basis allowable. EMC BT EMC BT 6 0 0 6 371.6897 659.9528 Tm ET EMC Regarding winglets, I think Simple Flying explains it well. /P <>BDC ET /P <>BDC /P <>BDC EMC /P <>BDC 7 0 0 7 82.8504 276.9528 Tm [(CFM L)17.1(E)-8.1(AP-1B27)]TJ 7 0 0 7 338.3085 144.9528 Tm 7 0 0 7 141.7322 716.9528 Tm /P <>BDC ( )Tj 6.5 0 0 6.5 224.5532 598.9529 Tm /P <>BDC ET -.02 Tc BT /P <>BDC /P <>BDC 7 0 0 7 182.5706 441.9528 Tm EMC 8 0 0 8 302.5117 619.9528 Tm /P <>BDC ET 7 0 0 7 82.8504 386.9528 Tm EMC EMC BT /P <>BDC ( )Tj EMC 9 0 0 9 207.5518 588.8898 Tm EMC /P <>BDC 63 0 obj Aircraft must carry enough fuel to taxi, climb, cruise, descent, and mutliple reserves. /P <>BDC ET ET 7 0 0 7 554.7883 89.7654 Tm /P <>BDC ET ET /P <>BDC ( )Tj ET BT (603)Tj EMC EMC (distance - nm )Tj -.02 Tc /P <>BDC /P <>BDC EMC 9 0 0 9 215.4409 357.8898 Tm ET 7 0 0 7 37.5838 738.9528 Tm 7 0 0 7 279.1575 727.9528 Tm EMC BT BT ET EMC EMC BT 9 0 0 9 551.0194 588.8898 Tm /P <>BDC 0 Tc /P <>BDC ET /P <>BDC BT 0 Tc (A321ceo have had more than 6,500)Tj ( )Tj ET (35,112)Tj /P <>BDC ET /P <>BDC ET /P <>BDC (6,303)Tj 73 0 obj 7 0 0 7 362.3891 287.9528 Tm ( )Tj ET 0 Tc ( )Tj 0 Tc /P <>BDC EMC ET 0 Tc BT ET ET BT (11,593)Tj 7 0 0 7 187.0858 100.9528 Tm EMC EMC BT EMC ET ET /P <>BDC The analysis, however,)Tj ET /OC /MC835 BDC (178)Tj ( )Tj 0 Tc ET /P <>BDC (further improve the fuel cost per ASM)Tj ET EMC (5,243)Tj Q 9 0 0 9 516.3894 247.8898 Tm ( )Tj BT /P <>BDC ET ( )Tj BT 9 0 0 9 372.2129 192.8898 Tm ( )Tj ( )Tj /P <>BDC 7 0 0 7 82.2047 474.9528 Tm EMC EMC 0 Tc ET ET (1,824)Tj BT 7 0 0 7 125.6292 331.7654 Tm BT (by the CFM LEAP-1A26. .498 .4095 .5623 .1043 v ET (shorter sectors. 9 0 0 9 394.0123 225.8898 Tm BT /P <>BDC BT 7 0 0 7 258.2805 67.7654 Tm .023 .567 .626 rg BT EMC 19.84 0 l BT 8 0 0 8 520.6337 771.7654 Tm /P <>BDC W* n (2,365)Tj 7 0 0 7 298.1781 67.9528 Tm EMC ET ET 7 0 0 7 518.4953 199.9528 Tm BT ( )Tj 9 0 0 9 190.2715 38.8898 Tm ET EMC BT ( )Tj 7 0 0 7 158.74 562.7654 Tm EMC ET 7 0 0 7 54.5916 738.7654 Tm /P <>BDC ET -.02 Tc ET /P <>BDC ( )Tj ET 7 0 0 7 490.5101 694.9528 Tm 6 0 0 6 418.9814 701.9528 Tm ET 9 0 0 9 129.4781 489.8898 Tm EMC EMC BT 7 0 0 7 519.3773 276.9528 Tm /P <>BDC 7 0 0 7 338.6433 122.7654 Tm 0 Tc -.01 Tc EMC 6.5 0 0 6.5 433.3069 585.9529 Tm BT -12.427 302.461 389.443 -271.279 re ET -.02 Tc ( )Tj EMC BT 0 Tc BT EMC EMC BT /P <>BDC /P <>BDC BT ( )Tj EMC BT /P <>BDC ( )Tj BT 0 Tc Why has Boeing maintained its designation to be B737, despite the latest B737 bears little resemblance to the original variant of the B737? (1B28B1)Tj ET /P <>BDC ET ET 6 0 0 6 412.5551 659.9528 Tm /P <>BDC /P <>BDC [(YH)-23.9(M/58)]TJ EMC EMC ET /P <>BDC /P <>BDC 0 Tc BT ET 7 0 0 7 474.5665 430.9528 Tm 9 0 0 9 408.2047 423.8898 Tm /P <>BDC (As with the rest of the Airbus aircraft,)Tj BT (26)Tj /P <>BDC ET BT /P <>BDC 6.5 0 0 6.5 536.1732 545.9529 Tm BT BT BT /P <>BDC ET /P <>BDC )Tj 7 0 0 7 354.4763 672.7654 Tm ET 13 0 0 13 162.9571 181.8898 Tm /P <>BDC ET 19.843 0 l ET ET 0 Tc BT ET EMC EMC 8 0 0 8 90.0179 771.7654 Tm 0 Tc 0 Tc EMC 0 Tc 7 0 0 7 141.7322 309.9528 Tm BT 0 Tc EMC ET ET BT ET BT ET ET /P <>BDC [(E)-7.8(P)16.1(T)9(E)-13.9(MBE)-16.9(R)]TJ ( )Tj (20)Tj The Boeing 777-200 has a maximum fuel capacity of 31,000 gallons or 117,347 liters. EMC BT BT EMC ET EMC 0 Tc ET ET 7 0 0 7 363.2711 210.9528 Tm -.02 Tc 8 0 0 8 216.3261 771.9529 Tm 7 0 0 7 491.7142 133.7654 Tm 9 0 0 9 186.5212 225.8898 Tm BT /P <>BDC (428,060)Tj -.02 Tc EMC 7 0 0 7 141.7322 683.9528 Tm /P <>BDC (other seven aircraft types. EMC ET /P <>BDC BT /P <>BDC /P <>BDC BT (0.0129)Tj 0 Tc /P <>BDC 9 0 0 9 193.4848 280.8898 Tm ET The typical range for this)Tj ET EMC /P <>BDC EMC /P <>BDC EMC /P <>BDC EMC 9 0 0 9 411.0234 709.8898 Tm Just not sure how to access these. 0 Tc /P <>BDC /P <>BDC ET ET ( )Tj The A320neo in this study)Tj ET ET EMC ( )Tj (5,279)Tj 7 0 0 7 337.6855 67.9528 Tm -.2034 -.7911 -.1202 -.4766 0 0 c BT /P <>BDC EMC 0 Tc /P <>BDC W n . -.02 Tc 8 0 0 8 302.5117 633.9528 Tm /OC /MC4794 BDC /P <>BDC /P <>BDC 7 0 0 7 326.2278 529.9528 Tm BT (weight penalty in its OEW compared to its)Tj EMC especially during start. 0 J 0 j 5 w 10 M [] 0 d /P <>BDC EMC (The comparison will be for eight)Tj ( )Tj ET ET 0 Tc EMC EMC /P <>BDC BT 13 0 0 13 36.8583 390.8898 Tm EMC ( )Tj /P <>BDC BT 6.5 0 0 6.5 426.4819 663.9529 Tm (CFM56-7B26)Tj /OC /MC2 BDC [(CFM L)17.1(E)-8.1(AP-1B27)]TJ ( )Tj BT (136)Tj BT 0 Tc EMC BT (CFM56-7B27B3)Tj /P <>BDC 7 0 0 7 43.6039 738.9528 Tm (airport charges, while the time-dependent)Tj -.02 Tc ET -.02 Tc /P <>BDC 6 0 0 6 380.7199 659.9528 Tm .023 .567 .626 rg /P <>BDC (capacity of 6,353USG, giving it a range of)Tj /P <>BDC BT ET BT EMC EMC /P <>BDC 0 Tc BT ET /P <>BDC /P <>BDC BT EMC This leaves about 20,000 kg (45,000 lbs) for passengers, cargo, and crew. /P <>BDC (0.0126)Tj (capacity of 160 \(the same as the 737-800\))Tj 0 Tc 6 0 0 6 55.0668 715.9528 Tm BT -.02 Tc All the aircraft would therefore)Tj -.02 Tc ET [(CFM L)17.1(E)-8.1(AP-1A26)]TJ BT BT 0 Tc /P <>BDC /P <>BDC -9.719 805.04 386.723 -270.624 re /P <>BDC EMC BT 9 0 0 9 394.0157 159.8898 Tm /P <>BDC BT (CFM56-5B3/P)Tj ( )Tj EMC ET /P <>BDC ET 10 0 0 10 425.05 814.1973 Tm EMC EMC 0 Tc BT (inches and a bypass ratio of 11.0:1. The nose wheel pressure in PSI is 186-194. /GS2 gs (achieve five inches extra legroom. /P <>BDC ET BT /P <>BDC FQIS accuracy with analog indicators: +/- 3.0% /P <>BDC /P <>BDC 6.5 0 0 6.5 244.2974 545.9529 Tm BT 9 0 0 9 187.8443 346.8898 Tm ( )Tj /P <>BDC /P <>BDC /P <>BDC BT BT BT 7 0 0 7 354.6933 463.7654 Tm EMC BT ET /P <>BDC 7 0 0 7 387.0159 672.9528 Tm BT EMC (158)Tj 7 0 0 7 366.0641 694.9528 Tm ET BT 7 0 0 7 37.6993 100.9528 Tm /P <>BDC ET /P <>BDC EMC (18)Tj EMC (174,200)Tj /P <>BDC ( )Tj /P <>BDC 9 0 0 9 369.4048 467.8898 Tm EMC BT BT ET (32,000lbs, down from the 33,000lbs that)Tj BT ET BT /P <>BDC /P <>BDC ET 6 0 0 6 195.3167 757.9528 Tm BT BT 9 0 0 9 554.3696 269.8898 Tm /P <>BDC EMC 9 0 0 9 354.313 236.8898 Tm -.02 Tc ( )Tj 8 0 0 8 136.4919 675.9528 Tm /OC /MC188 BDC 7 0 0 7 554.7883 463.7654 Tm 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? /P <>BDC ET /P <>BDC 5.25 0 0 5.25 64.5461 11.5129 Tm BT ET /P <>BDC BT ET ET BT BT q 1 0 0 1 36.85 513.878 cm 0 0 m (CFM56-5B4/P)Tj BT EMC EMC -.02 Tc BT ET 6.5 0 0 6.5 176.1172 558.9529 Tm EMC 0 Tc (464,440)Tj 56 0 obj [(7)-33(3)8.1(7-900ER\(W)-19(\) v)12.9(ersus 7)-33(3)8.1(7-9 )]TJ ( )Tj /P <>BDC -.02 Tc /P <>BDC ET /P <>BDC (The aircraft weights used in this)Tj EMC ET ET BT /P <>BDC ET 9 0 0 9 79.8339 489.8898 Tm BT 7 0 0 7 344.1175 595.7654 Tm EMC ET EMC -.02 Tc 7 0 0 7 182.5706 474.9528 Tm ( )Tj EMC BT EMC EMC -.02 Tc BT BT ET (1,498)Tj ( )Tj /P <>BDC EMC BT BT EMC BT 0 Tc BT ET -.02 Tc ET endobj /P <>BDC EMC 0 Tc 9 0 0 9 53.8578 38.8898 Tm (737-9)Tj BT ( )Tj 7 0 0 7 182.5706 177.9528 Tm EMC ET 9 0 0 9 36.8504 126.8898 Tm ET BT ( )Tj /P <>BDC /P <>BDC ( )Tj 6.5 0 0 6.5 243.3486 742.9529 Tm /P <>BDC ET 7 0 0 7 337.7614 144.7654 Tm ( )Tj ( )Tj EMC ET -.02 Tc /P <>BDC EMC -.02 Tc (orders, while the 737-800 and 737-900ER)Tj ET /P <>BDC BT EMC ( )Tj BT 7 0 0 7 316.0679 122.7654 Tm ET 7 0 0 7 131.6494 672.7654 Tm EMC BT BT ET EMC /P <>BDC BT (288)Tj BT ET 7 0 0 7 99.8582 672.7654 Tm 1 w (CFM56-7B26)Tj ET BT /P <>BDC BT BT EMC BT EMC BT -.02 Tc ET EMC EMC /P <>BDC 7 0 0 7 131.6494 474.7654 Tm /P <>BDC EMC 0 Tc ET 6 0 0 6 286.5632 771.9528 Tm -.01 Tc 6.5 0 0 6.5 332.6961 735.9529 Tm BT 7 0 0 7 439.2087 199.9528 Tm 7 0 0 7 99.8582 287.7654 Tm 0 Tc 9 0 0 9 36.8504 390.8898 Tm (direction, with an initial heading ranging)Tj 7 0 0 7 141.7322 628.9528 Tm (A321neo)Tj /P <>BDC BT BT EMC )Tj BT 6 0 0 6 153.7355 729.9528 Tm ET EMC /P <>BDC EMC 6.5 0 0 6.5 530.1996 735.9529 Tm /P <>BDC /P <>BDC 7 0 0 7 387.0932 320.9528 Tm ( )Tj BT (I)Tj 7 0 0 7 54.7071 210.7654 Tm ET BT 1 i ET /P <>BDC (this analysis is 20/42/117, giving a total)Tj /P <>BDC ( )Tj ET ( )Tj BT 7 0 0 7 187.0858 232.9528 Tm (31,416lbs)Tj /P <>BDC unit, Open or short in 0 Tc ET ( )Tj EMC 304.725 420.96 m /P <>BDC 0 Tc ET /P <>BDC /P <>BDC BT /P <>BDC 9 0 0 9 53.8578 280.8898 Tm (BOS-MIA)Tj BT EMC (277,248)Tj /P <>BDC 10 0 0 10 47.8705 814.1973 Tm ET BT 7 0 0 7 539.8962 694.9528 Tm 7 0 0 7 279.1575 100.9528 Tm EMC /P <>BDC /P <>BDC /OC /MC854 BDC 7 0 0 7 294.4014 144.7654 Tm BT ET EMC BT EMC BT EMC ( )Tj -.02 Tc ET EMC ( )Tj EMC ET ET EMC (payload, the A321neo has an 18.9%)Tj 7 0 0 7 242.1547 672.9528 Tm /P <>BDC BT ET ET 7 0 0 7 537.7804 287.9528 Tm ( )Tj ET BT ( )Tj EMC 7 0 0 7 439.7405 463.9528 Tm Can we suggest copying and pasteing Aluminium alloy 7055 basis value into your search engine of choice? ( )Tj 7 0 0 7 114.6416 694.9528 Tm EMC EMC 7 0 0 7 70.8101 243.9528 Tm EMC BT BT (A321ceo)Tj BT ET .0081 Tc EMC EMC EMC 0 Tc 9 0 0 9 215.433 280.8898 Tm ( )Tj EMC 9 0 0 9 36.8504 511.8898 Tm BT BT EMC ( )Tj The 800 is mainly used for passenger transport with its 526 seating capacity. BT (CFM56-5B4/P)Tj ET /P <>BDC EMC ( )Tj 7 0 0 7 536.3849 639.7654 Tm EMC (157,300)Tj ( )Tj ( )Tj BT ( )Tj (A320neo will be evaluated with the same)Tj EMC EMC BT 6.5 0 0 6.5 54.877 742.9529 Tm (operating potential for these aircraft. (This evaluation has been conducted)Tj 8 0 0 8 158.74 760.7654 Tm ( )Tj ( )Tj /P <>BDC -.01 Tc ( )Tj (900ER and 737-9, A320ceo and A320neo,)Tj BT ET /P <>BDC /P <>BDC EMC ( )Tj 9 0 0 9 394.0315 280.8898 Tm 0 Tc ET BT BT ET BT EMC (thereby giving it a seat capacity of 160)Tj BT 0 Tc BT /P <>BDC ET 7 0 0 7 297.632 738.9528 Tm /GS2 gs 0 Tc /P <>BDC EMC (136)Tj ET /P <>BDC -.02 Tc This narrow body jet airliner had first rolled out on June 30, 1997 and shortly after was had its first test flight with he pilot Jim McRoberts in the cockpit. 9 0 0 9 361.7 456.8898 Tm BT EMC 7 0 0 7 297.632 705.9528 Tm 6 0 0 6 433.9826 659.9528 Tm 10 0 0 10 417.91 814.1973 Tm 7 0 0 7 539.8962 661.9528 Tm ET 9 0 0 9 36.8504 390.8898 Tm ET [(BOS-Y)-50(YZ)]TJ [(E)-7.8(P)16.1(T)9(E)-13.9(MBE)-16.9(R)]TJ 0 Tc 7 0 0 7 439.2087 364.9528 Tm 7 0 0 7 54.5916 254.7654 Tm 0 Tc Q /P <>BDC 0 Tc /TT2 1 Tf EMC 9 0 0 9 36.8504 313.8898 Tm 9 0 0 9 178.1318 71.8898 Tm BT BT /P <>BDC ET ( )Tj EMC ( )Tj BT BT EMC BT (Flight time - mins)Tj ET BT 8 0 0 8 122.6593 760.7654 Tm BT BT ( )Tj 7 0 0 7 491.4046 287.9528 Tm ET BT (into service in 2023. /P <>BDC ET 0 Tc ( )Tj BT ET /P <>BDC (20)Tj ET /P <>BDC -.02 Tc (170)Tj .559 .331 .619 rg ET /P <>BDC BT (3,443)Tj BT EMC EMC 7 0 0 7 338.4211 430.9528 Tm BT /P <>BDC ( )Tj (152)Tj EMC ET 0 Tc /P <>BDC BT /F1 1 Tf 7 0 0 7 125.6292 738.7654 Tm 10 0 0 10 54.2544 814.1973 Tm EMC EMC /P <>BDC Boeing 737Specs Tablefor Original and Classic. /P <>BDC /P <>BDC ( )Tj *PUUqUef\r+vl Hi I was just wondering where you got this data from. BT BT /P <>BDC Additionally, below 10,000 feet it should not exceed 250 knots. EMC /P <>BDC (A321ceo)Tj (146,300)Tj (and Boeing aircraft benefit from the)Tj -.01 Tc /P <>BDC (comprehensive comparison of the aircraft)Tj 0 Tc [(Y)-7.1(XX/104)]TJ 0 Tc ET BT ( )Tj 9 0 0 9 554.6907 159.8898 Tm /P <>BDC EMC EMC ET (737-9)Tj BT BT (136)Tj Thank you. EMC /P <>BDC ( )Tj ( )Tj BT 9 0 0 9 522.7491 280.8898 Tm ET 7 0 0 7 204.0935 628.7654 Tm 6 0 0 6 176.4941 687.9528 Tm 7 0 0 7 478.9484 727.9528 Tm ET EMC 7 0 0 7 294.4014 430.7654 Tm 0 Tc ( )Tj (1,825)Tj /P <>BDC /P <>BDC BT 9 0 0 9 546.3505 566.8898 Tm BT EMC ET 0 Tc /P <>BDC 6.5 0 0 6.5 346.3049 676.9529 Tm ET (31,416)Tj /P <>BDC BT ET EMC /P <>BDC 0 Tc BT 0 Tc ET [(CFM L)17.1(E)-8.1(AP-)]TJ 7 0 0 7 404.101 100.7654 Tm ET ET 0 Tc ET 9 0 0 9 53.8338 170.8898 Tm EMC ( )Tj /P <>BDC ET 9 0 0 9 215.4313 225.8898 Tm BT EMC Today the Next Generation 737 sub-family includes the 700, -800 and 900models. /P <>BDC ET 6.5 0 0 6.5 549.8557 722.9529 Tm BT ( )Tj /P <>BDC 0 Tc (36,960)Tj ET 0 Tc ET ( )Tj ( )Tj 7 0 0 7 36.8504 11.5129 Tm Wed love you to share what you build when youre done. /P <>BDC ( )Tj ET /GS1 gs 9 0 0 9 215.4409 104.8898 Tm 0 Tc ( )Tj ET ET ( )Tj 7 0 0 7 387.0932 221.9528 Tm EMC (1,272)Tj /F1 1 Tf BT (ASM benefit over the A320ceo for the)Tj ET /P <>BDC BT /P <>BDC (A320neo)Tj 0 Tc ( )Tj /P <>BDC ( )Tj BT ET /P <>BDC 0 Tc EMC ET EMC -.02 Tc EMC 7 0 0 7 141.7322 540.9528 Tm 9 0 0 9 194.9081 346.8898 Tm ET ET [(CFM L)17.1(E)-8.1(AP-1A32)]TJ EMC BT 6 0 0 6 372.3969 729.9528 Tm EMC 7 0 0 7 130.1443 320.7654 Tm ( )Tj ET 0 841.89 609.449 -841.89 re 9 0 0 9 546.4149 456.8898 Tm (mainline carriers may in fact opt to use a)Tj 9 0 0 9 394.0315 434.8898 Tm ET EMC ET ( )Tj EMC 9 0 0 9 544.0105 258.8898 Tm (is used on the CFM56-5B3/P, despite the)Tj 8 0 0 8 187.3427 619.9528 Tm ET /P <>BDC 5.25 0 0 5.25 549.1047 11.5132 Tm BT (CFM56-5B3/P)Tj BT (34,650)Tj EMC /P <>BDC -.02 Tc 6.5 0 0 6.5 397.1664 735.9529 Tm (0.0153)Tj (104-112)Tj [(AIRL)8.1(INE & AIR)7.1(CRAF)-12.9(T)18.1( OPERA)56.9(T)-8.1(ION)-13.9(S)]TJ [(CFM L)17.1(E)-8.1(AP-1A26)]TJ /P <>BDC /P <>BDC EMC 7 0 0 7 536.3849 529.7654 Tm 7 0 0 7 241.2727 573.9528 Tm -.02 Tc ET EMC EMC 0 Tc /P <>BDC ET (performance, it was also assumed there)Tj BT 9 0 0 9 394.0315 192.8898 Tm EMC ( )Tj /P <>BDC /P <>BDC /P <>BDC EMC 7 0 0 7 439.1464 430.9528 Tm BT /P <>BDC 8 0 0 8 257.7904 661.9528 Tm /F1 1 Tf /P <>BDC ET EMC /P <>BDC EMC ET .008 Tc BT EMC 7 0 0 7 404.3599 672.7654 Tm ET 5.25 0 0 5.25 73.853 11.5132 Tm /P <>BDC <>/ExtGState<>/Properties<>>> 7 0 0 7 182.5706 738.9528 Tm /F4 1 Tf ET BT 6 0 0 6 520.876 743.9528 Tm -.02 Tc EMC 9 0 0 9 232.438 368.8898 Tm EMC ( )Tj ET BT (0.0135)Tj 7 0 0 7 381.1608 584.7654 Tm ET EMC 0 Tc BT BT BT EMC ( )Tj ET EMC ET 9 0 0 9 173.2978 247.8898 Tm BT ET ET ET ET BT ET 9 0 0 9 531.8156 280.8898 Tm the future. (97,700)Tj /P <>BDC BT BT /GS2 gs ET 0 Tc ( )Tj EMC /P <>BDC ET /P <>BDC ET ET 0 Tc EMC ET ET EMC EMC ET BT BT EMC 7 0 0 7 496.3063 727.7654 Tm BT 6.5 0 0 6.5 534.5352 585.9529 Tm 7 0 0 7 258.2805 144.7654 Tm (from Boston \(BOS\) Logan International)Tj (The A320 analysed here is powered by)Tj Cruise Speed: 530 mph Propulsion: Two General Electric CFM56-7B24 High Bypass Ratio turbofan engines, rated at 24,200 pounds thrust each. BT (482)Tj 0 Tc /GS1 gs 9 0 0 9 541.8752 775.8898 Tm ( )Tj EMC 0 Tc 7 0 0 7 490.8321 78.7654 Tm BT (CFM56-7B26)Tj BT /P <>BDC 9 0 0 9 394.0157 126.8898 Tm ET 0 Tc ET /P <>BDC ET 0 Tc EMC ( )Tj EMC ET -.01 Tc Q ( )Tj (163)Tj ET /P <>BDC /P <>BDC /P <>BDC /P <>BDC BT /P <>BDC /P <>BDC
How Much Is A 14k Gold Herringbone Necklace Worth,
Post Box Near Me Collection Times,
Articles OTHER