7 0 0 7 387.0159 540.9528 Tm /P <>BDC 9 0 0 9 193.7007 236.8898 Tm /P <>BDC 7 0 0 7 101.0963 309.9528 Tm /GS1 gs /P <>BDC 7 0 0 7 537.7804 221.9528 Tm ET ET ET 0 Tc ET 9 0 0 9 53.8338 368.8898 Tm /P <>BDC BT /P <>BDC ET ET /P <>BDC /P <>BDC ()Tj EMC (even though the two have the same)Tj ET ET 7 0 0 7 279.1575 221.9528 Tm ET BT /P <>BDC For land the 800 needs 1372 meters or 4,501.26 feet. /P <>BDC 0 Tc 9 0 0 9 215.4313 181.8898 Tm 7 0 0 7 199.5784 144.7654 Tm ET 10.479 -.009 l 7 0 0 7 37.5838 144.9528 Tm /P <>BDC /P <>BDC 6.5 0 0 6.5 332.0787 545.9529 Tm 7 0 0 7 60.6117 540.7654 Tm /P <>BDC BT EMC ET EMC /P <>BDC /OC /MC2269 BDC 0 Tc (0.0131)Tj ( )Tj Jump to Specification Table Boeing 737 Next Gen and Max. 7 0 0 7 535.5029 199.7654 Tm /P <>BDC /P <>BDC 9 0 0 9 408.1854 676.8898 Tm ET (146,550)Tj ET 7 0 0 7 131.6494 474.7654 Tm BT BT 9 0 0 9 215.4313 159.8898 Tm (\(see table, this page\))Tj Do you have the estimated production material used for the 737 Next Gen? /P <>BDC Note: Specifications are listed as standard and may vary slightly. EMC EMC EMC BT BT 7 0 0 7 320.7537 144.9528 Tm /P <>BDC ET /P <>BDC BT -3.5781 -.0449 -2.6539 .5294 -1.6216 .5285 c /P <>BDC 0 Tc BT ET EMC (405)Tj BT ET Boeings main competitor is with Airbus. ET 7 0 0 7 230.7317 595.9528 Tm BT 9 0 0 9 36.8504 423.8898 Tm /P <>BDC ET EMC ET )Tj ( )Tj q BT ( )Tj ET ET ( )Tj (170)Tj (CFM56-7B26)Tj EMC 6 0 0 6 363.2184 687.9528 Tm EMC EMC /P <>BDC [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ ET (0.0123)Tj 5.25 0 0 5.25 73.853 11.5132 Tm /P <>BDC EMC /P <>BDC BT 6.5 0 0 6.5 426.4819 702.9529 Tm -.02 Tc [(MR)32(TX - lbs)]TJ BT 1 w 9 0 0 9 418.9315 59.9073 Tm BT operation, centre tank pumps must be not be positioned to ON, unless ET /P <>BDC BT 0 Tc /F6 1 Tf (A320neos cost per ASM advantage. ( )Tj /P <>BDC BT BT 0 Tc BT BT /P <>BDC 7 0 0 7 387.0932 100.9528 Tm ET EMC /P <>BDC 9 0 0 9 362.4471 82.8898 Tm EMC EMC (900ER\(W\) has a 4.3% lower fuel burn)Tj (passengers. BT ET /P <>BDC Q ( )Tj Digital Sunburst Fuel Gauges - Simmonds 4 Tank. 9 0 0 9 394.0123 599.8898 Tm BT 7 0 0 7 338.5674 133.9528 Tm -.02 Tc BT 9 0 0 9 170.626 357.8898 Tm ET (0.0108)Tj ( )Tj 7 0 0 7 444.737 133.7654 Tm EMC ET EMC /P <>BDC EMC /P <>BDC BT (0.0127)Tj 7 0 0 7 230.7317 507.9528 Tm 7 0 0 7 354.4763 661.7654 Tm ET ET BT /P <>BDC /P <>BDC ( )Tj BT /P <>BDC EMC 7 0 0 7 490.5101 529.9528 Tm <>/ExtGState<>/Properties<>>> /P <>BDC /P <>BDC EMC 9 0 0 9 374.0759 203.8898 Tm /P <>BDC ( )Tj /P <>BDC EMC ( )Tj BT BT ET 9 0 0 9 433.049 544.8898 Tm 7 0 0 7 326.2278 672.9528 Tm ET BT (The A320 and 737 families have been)Tj 0 Tc ( )Tj BT /P <>BDC EMC ( )Tj (158)Tj In the 90s Boeing produced 80% of components in house including the wings, fuselage and tall assemblies. (achieved more than 6,000 orders for the)Tj (404)Tj 7 0 0 7 536.3849 210.7654 Tm [(UG)-17.1(U)-8(S)8.1(T)]TJ 6 0 0 6 191.3929 771.9528 Tm /P <>BDC 7 0 0 7 387.0159 507.9528 Tm EMC ET EMC EMC BT EMC EMC ( )Tj /P <>BDC ( )Tj 9 0 0 9 51.0236 60.8898 Tm 0 Tc ( )Tj 377.677 0 0 271.254 -.32779 534.078 cm 6.5 0 0 6.5 381.6589 558.9529 Tm ET EMC (ratio of 11.0:1. 10 0 0 10 230.6475 794.2914 Tm /P <>BDC BT (0.0137)Tj 0 Tc EMC ET EMC EMC ET ET 8 0 0 8 136.4919 703.9528 Tm 7 0 0 7 384.8358 683.7654 Tm EMC 9 0 0 9 566.4993 698.8898 Tm ET 7 0 0 7 429.157 529.9528 Tm BT BT (282-294)Tj BT (these aircraft, two different payload)Tj -.02 Tc BT /P <>BDC 0 Tc ET BT ET 7 0 0 7 440.0906 133.9528 Tm ET EMC EMC (for seats. 7 0 0 7 241.5317 518.9528 Tm 0 Tc ET 7 0 0 7 520.6108 529.9528 Tm 7 0 0 7 230.7317 166.9528 Tm [(A3)24.9(20ceo & A3)24.9(20neo )]TJ 9 0 0 9 556.2501 181.8898 Tm We have rechecked with Boeing and the figure should now be up to date and correct. 9 0 0 9 191.7774 423.8898 Tm ET /P <>BDC EMC BT /P <>BDC /P <>BDC BT EMC EMC BT BT ET BT /P <>BDC All the flights are in a westerly)Tj /P <>BDC /P <>BDC BT ET 7 0 0 7 383.0719 716.7654 Tm 0 Tc /P <>BDC 7 0 0 7 444.737 309.7654 Tm /P <>BDC [(P)11(ayload)]TJ Q /P <>BDC [(P)11(assenger payload - lbs )]TJ must not be left ON unless personnel are available in the flight deck ET 0 Tc ( )Tj /P <>BDC /P <>BDC ( )Tj (same cost index, and the method that each)Tj EMC EMC ( )Tj 7 0 0 7 326.2278 661.9528 Tm ( )Tj ET ET (5B4/P)Tj ( )Tj (compared to the CFM56-7B-powered 737-)Tj 7 0 0 7 36.8504 11.5129 Tm (136)Tj ( )Tj EMC ET (7B27B3)Tj ET 7 0 0 7 297.632 661.9528 Tm -.02 Tc EMC (rules relating to the cruise altitudes and)Tj ( )Tj /P <>BDC ( )Tj /P <>BDC BT BT 7 0 0 7 379.3969 232.7654 Tm 9 0 0 9 394.0123 588.8898 Tm ( )Tj EMC BT ET 0 Tc 9 0 0 9 411.0234 698.8898 Tm BT 8 0 0 8 539.0026 760.7654 Tm EMC BT ( )Tj 7 0 0 7 99.8582 419.7654 Tm ET 9 0 0 9 546.4149 456.8898 Tm EMC 0 Tc /P <>BDC ( )Tj BT 0 Tc wiring in tanks, proximity to hot air-conditioning or pneumatic systems, etc. /P <>BDC 6 0 0 6 527.8009 743.9528 Tm ( )Tj 9 0 0 9 191.9099 93.8898 Tm ( )Tj 137 )Tj 7 0 0 7 54.7071 100.7654 Tm ET BT (420)Tj (-58)Tj 0 Tc The NTSB EMC BT EMC ET /P <>BDC .001 Tc EMC 7 0 0 7 490.8321 199.7654 Tm The Honeywell NGS was certified by the FAA on 21 Feb 2006 after over 1000hrs flight testing on two 737-NGs. The aircraft also features)Tj EMC -.02 Tc BT /P <>BDC BT /P <>BDC 8 0 0 8 225.1837 577.9528 Tm 7 0 0 7 387.0932 342.9528 Tm ET ( )Tj EMC (A320ceo and A320neo in this study. ET ( )Tj ET /P <>BDC ET 9 0 0 9 411.0181 302.8898 Tm /P <>BDC 7 0 0 7 439.2087 320.9528 Tm [(CFM L)17.1(E)-8.1(AP-1A26)]TJ EMC /P <>BDC ET /P <>BDC (analysis are: an MTOW of 213,848lbs; an)Tj ET 7 0 0 7 297.632 694.9528 Tm tank. EMC 7 0 0 7 403.478 683.7654 Tm endobj [(A3)24.9(21ceo & A3)24.9(21neo )]TJ (westerly direction so that all operate)Tj BT /P <>BDC ET EMC /P <>BDC ET 6 0 0 6 352.5857 659.9528 Tm ( )Tj ET ET ( )Tj EMC /P <>BDC 0 Tc /P <>BDC 10 0 0 10 422.8 814.1973 Tm ET 10 0 0 10 52.6304 814.1973 Tm 6 0 0 6 561.1918 687.9528 Tm )Tj EMC /P <>BDC ( )Tj EMC /P <>BDC q 1 0 0 1 394.016 758.971 cm 0 0 m 7 0 0 7 258.2805 144.7654 Tm 1 i /P <>BDC ( )Tj EMC (against the 737-800 is interesting. ET ET 9 0 0 9 545.3896 302.8898 Tm 0 Tc ET ( )Tj ET /P <>BDC 7 0 0 7 490.7815 221.9528 Tm ( )Tj ET EMC -.02 Tc ( )Tj -.02 Tc ET q 1 0 0 1 215.431 128.878 cm 0 0 m ( )Tj EMC 7 0 0 7 99.8582 386.7654 Tm ( )Tj /P <>BDC BT 9 0 0 9 379.0889 291.8898 Tm BT /P <>BDC 7 0 0 7 316.0679 320.7654 Tm ( )Tj EMC (mainline carriers may in fact opt to use a)Tj ET ET ( )Tj /P <>BDC BT /GS2 gs BT /Artifact <>BDC EMC BT ET BT 9 0 0 9 555.1324 148.8898 Tm ET -.02 Tc EMC EMC 7 0 0 7 70.8101 441.9528 Tm BT -.02 Tc 9 0 0 9 68.0071 71.8898 Tm 9 0 0 9 354.313 236.8898 Tm BT ET ET -.02 Tc /F6 1 Tf EMC ET /P <>BDC ( )Tj ET BT EMC /P <>BDC /P <>BDC BT BT BT BT (5.7:1)Tj BT EMC /P <>BDC EMC BT /P <>BDC /P <>BDC 7 0 0 7 386.4701 397.9528 Tm /P <>BDC BT 0 Tc /F6 1 Tf EMC 7 0 0 7 141.7322 716.9528 Tm BT /P <>BDC 0 Tc (1B27)Tj 7 0 0 7 279.1575 331.9528 Tm /P <>BDC BT BT ET EMC /P <>BDC /P <>BDC 9 0 0 9 107.6178 269.8898 Tm /P <>BDC EMC EMC ET ET (22)Tj EMC ( )Tj ET ET ( )Tj EMC EMC EMC EMC /P <>BDC BT ET ( )Tj EMC /F1 1 Tf BT (cost per ASM ranges from 0.06 to 0.16)Tj 6.5 0 0 6.5 432.488 624.9529 Tm /P <>BDC /P <>BDC /GS1 gs /P <>BDC BT BT ET /P <>BDC /P <>BDC EMC ( )Tj EMC EMC ET ET BT /P <>BDC /P <>BDC EMC /P <>BDC (977)Tj endobj EMC -.02 Tc 0 Tc EMC /P <>BDC EMC This is equivalent to)Tj /P <>BDC /P <>BDC EMC ET /P <>BDC BT /P <>BDC -.01 Tc /P <>BDC ( )Tj 0 Tc BT BT EMC EMC /GS2 gs /P <>BDC 7 0 0 7 241.5317 606.9528 Tm ET 7 0 0 7 491.7142 463.7654 Tm 7 0 0 7 199.5784 540.7654 Tm (1,825)Tj ET ( )Tj /P <>BDC /Artifact <>BDC EMC EMC /GS1 gs ( )Tj EMC 0 Tc EMC BT 7 0 0 7 230.7317 342.9528 Tm /P <>BDC BT 0 Tc BT ET ( )Tj BT BT EMC BT BT (37,653)Tj BT ET /OC /MC5061 BDC BT -.02 Tc EMC 9 0 0 9 394.0315 60.8898 Tm BT ET 7 0 0 7 386.3929 628.9528 Tm /P <>BDC ET BT 6.5 0 0 6.5 284.897 532.9529 Tm BT 6.5 0 0 6.5 471.1051 742.9529 Tm ET 9 0 0 9 394.0123 665.8898 Tm ( )Tj /P <>BDC ( )Tj Their version of the Boeing 737-800 is the Airbus A220. BT 10 0 0 10 55.0104 814.1973 Tm /P <>BDC /P <>BDC Boeing 737 Assembly, the building of this popular City Jet. ET BT ET -.02 Tc EMC /P <>BDC BT BT ET 6.5 0 0 6.5 397.0428 532.9529 Tm BT 7 0 0 7 366.0641 727.9528 Tm [(CFM L)17.1(E)-8.1(AP-1A26)]TJ BT ET 5.25 0 0 5.25 123.5367 11.5132 Tm EMC (3,400 )Tj (1,547)Tj EMC BT ET EMC ( )Tj ( )Tj /P <>BDC EMC ET 7 0 0 7 241.5317 419.9528 Tm ET EMC ET ET 9 0 0 9 53.8582 478.8898 Tm ET BT ET EMC /P <>BDC /P <>BDC ET -.02 Tc BT 7 0 0 7 114.6416 298.9528 Tm /P <>BDC The A320neo in this study)Tj 9 0 0 9 555.0639 467.8898 Tm 9 0 0 9 425.1967 775.8898 Tm BT /P <>BDC EMC ET ET BT BT 7 0 0 7 490.5101 485.9528 Tm /P <>BDC ( )Tj BT 7 0 0 7 491.4046 199.9528 Tm 7 0 0 7 294.4014 639.7654 Tm 7 0 0 7 427.7291 276.9528 Tm 9 0 0 9 537.9817 445.8898 Tm 9 0 0 9 232.438 412.8898 Tm EMC EMC EMC (0.0141)Tj -.02 Tc /P <>BDC EMC 0 Tc /P <>BDC ET ET 0 Tc ET 9 0 0 9 393.5047 181.8898 Tm /P <>BDC 6.5 0 0 6.5 448.257 650.9529 Tm BT EMC /P <>BDC /P <>BDC BT 7 0 0 7 387.0932 276.9528 Tm ET /P <>BDC 9 0 0 9 232.4217 203.8898 Tm -.02 Tc ( )Tj -.02 Tc 0 Tc 9 0 0 9 190.0677 203.8898 Tm /P <>BDC ET /P <>BDC ( )Tj BT 9 0 0 9 411.0181 236.8898 Tm EMC ( )Tj EMC 7 0 0 7 445.619 738.7654 Tm /P <>BDC 10 0 0 10 54.1504 814.1973 Tm /P <>BDC ET ET ET EMC BT on the Simmonds gauges or error codes 1,3 and 6 on the Smiths gauges. EMC 0 J 0 j 15 w 10 M [] 0 d BT ET endstream ET EMC ET /P <>BDC 6 0 0 6 357.8844 701.9528 Tm /P <>BDC ( )Tj BT ET ( )Tj ET ET ET ET /P <>BDC EMC 7 0 0 7 158.74 595.7654 Tm 7 0 0 7 535.5029 78.7654 Tm BT q 1 0 0 1 53.858 546.878 cm 0 0 m /P <>BDC BT ( )Tj (be achieved. BT ET 7 0 0 7 37.8848 452.9528 Tm 9 0 0 9 361.1316 214.8898 Tm /P <>BDC ET BT EMC EMC ( )Tj /P <>BDC EMC ET 0 Tc EMC /P <>BDC BT BT BT BT /P <>BDC BT 0 Tc EMC ET ET 9 0 0 9 53.8582 654.8898 Tm ET .151 .147 .15 rg This is because the RH centre tank pump will stop feeding due to the 6.5 0 0 6.5 499.1812 650.9529 Tm 9 0 0 9 548.3146 104.8898 Tm BT BT (44,121)Tj EMC 9 0 0 9 372.4479 368.8898 Tm EMC 9 0 0 9 53.8578 434.8898 Tm /F6 1 Tf /P <>BDC BT /P <>BDC -.01 Tc BT /P <>BDC ET EMC 7 0 0 7 490.8321 122.7654 Tm 7 0 0 7 447.3829 705.7654 Tm (831)Tj BT ET ET BT (445,316)Tj ET 9 0 0 9 215.433 357.8898 Tm 9 0 0 9 560.68 60.8898 Tm 0 Tc EMC ( )Tj 0 Tc EMC 9 0 0 9 532.5876 137.8898 Tm ET ( The flight rules )Tj 7 0 0 7 297.632 595.9528 Tm /P <>BDC (150)Tj EMC ET BT 0 J 0 j 5 w 10 M [] 0 d EMC /Artifact <>BDC EMC ET BT 6 0 0 6 472.7745 771.9528 Tm ( )Tj ET -.02 Tc EMC 9 0 0 9 529.3116 533.8898 Tm EMC BT EMC /P <>BDC ( )Tj 7 0 0 7 457.0984 518.7654 Tm 7 0 0 7 536.3849 507.7654 Tm ET EMC EMC 7 0 0 7 279.1575 199.9528 Tm EMC 0 Tc /P <>BDC 10 0 0 10 52.6304 814.1973 Tm I already checked in the AMM, SRM. EMC BT BT /P <>BDC ET /P <>BDC EMC BT EMC 7 0 0 7 386.3929 716.9528 Tm /P <>BDC (136)Tj EMC /P <>BDC /P <>BDC ET BT BT EMC 8 0 0 8 394.0237 82.8898 Tm BT EMC 9 0 0 9 195.4853 126.8898 Tm /P <>BDC ( )Tj (discussions in the industry to potentially)Tj (105,800lbs )Tj ET ET 6 0 0 6 195.6824 659.9528 Tm EMC ET BT 9 0 0 9 394.0123 621.8898 Tm 9 0 0 9 411.0097 357.8898 Tm BT ET /P <>BDC BT (and 737-9. ET 9 0 0 9 545.8646 522.8898 Tm 9 0 0 9 394.0157 456.8898 Tm BT /P <>BDC BT ( )Tj (1,202)Tj ET EMC /P <>BDC /P <>BDC 9 0 0 9 552.5356 445.8898 Tm ET ( )Tj EMC ET EMC BT /P <>BDC BT ( )Tj EMC EMC BT ET ( )Tj /P <>BDC ET -.02 Tc 9 0 0 9 555.4203 346.8898 Tm EMC 9 0 0 9 204.9907 467.8898 Tm 7 0 0 7 327.1097 628.9528 Tm BT BT BT BT ET 7 0 0 7 537.7804 408.9528 Tm 9 0 0 9 421.0664 401.8898 Tm ( )Tj 7 0 0 7 321.6356 199.9528 Tm (0.0129)Tj BT [(Summar)-33(y )]TJ BT EMC BT /P <>BDC -.02 Tc ET EMC BT /OC /MC2279 BDC 7 0 0 7 428.6112 89.9528 Tm (I)Tj /P <>BDC EMC /GS2 gs EMC Are there any useful sources where I might find the exact materials used in other aircraft? The A321neo takes advantage of)Tj EMC EMC EMC /P <>BDC EMC 9 0 0 9 535.511 379.8898 Tm (Improvements introduced to the)Tj ET ( )Tj EMC ( )Tj ET /P <>BDC BT EMC ET EMC from cockpit door to the kitchen alley . 9 0 0 9 186.0514 60.8898 Tm 6.5 0 0 6.5 276.4014 598.9529 Tm ( )Tj EMC 7 0 0 7 337.6855 595.9528 Tm ET 7 0 0 7 444.737 166.7654 Tm /P <>BDC ( )Tj ET EMC EMC /P <>BDC 8 0 0 8 54.0516 771.7654 Tm (impact on the fuel cost per ASM. ET 9 0 0 9 369.7648 346.8898 Tm BT -.02 Tc A series of ten tests were performed (five flight, ET 0 Tc /P <>BDC BT 5.25 0 0 5.25 515.3989 11.5129 Tm EMC 10 0 0 10 417.91 814.1973 Tm /P <>BDC BT ET ( )Tj /P <>BDC ( )Tj EMC ET (1,019)Tj /P <>BDC ET ( )Tj ET 7 0 0 7 491.4046 298.9528 Tm BT BT 9 0 0 9 215.4313 511.8898 Tm EMC ET 9 0 0 9 173.4783 401.8898 Tm 5 0 0 5 484.5872 11.5129 Tm 6.5 0 0 6.5 549.8557 722.9529 Tm Q /P <>BDC BT Im glad you got something out of our site that was helpful. EMC [(BOS-D)17.1(T)-11(W)]TJ ET EMC ET EMC 7 0 0 7 518.4953 122.9528 Tm ET 0 Tc ( )Tj EMC (and the 737 MAX family with the CFM)Tj ( )Tj (282)Tj BT 9 0 0 9 68.0314 126.8898 Tm EMC (considers these routes to give a more)Tj EMC 0 Tc 9 0 0 9 385.6838 346.8898 Tm .661 .752 .896 rg ( )Tj 9 0 0 9 374.4497 214.8898 Tm ET EMC /F4 1 Tf 7 0 0 7 507.7893 463.7654 Tm 7 0 0 7 554.7883 727.7654 Tm /P <>BDC BT ET 9 0 0 9 232.438 115.8898 Tm BT 0 Tc ( )Tj /P <>BDC ( )Tj BT BT BT 7 0 0 7 543.7693 11.5132 Tm BT ET 0 Tc 7 0 0 7 297.632 672.9528 Tm ET BT 9 0 0 9 554.6907 159.8898 Tm -.02 Tc EMC BT BT BT ( N)Tj 9 0 0 9 190.8846 379.8898 Tm BT BT BT ( )Tj ET EMC EMC BT ( )Tj EMC EMC 9 0 0 9 411.0181 357.8898 Tm /P <>BDC f /P <>BDC 9 0 0 9 368.9994 225.8898 Tm 0 Tc /P <>BDC The cockpit is a dual seat design. /Artifact <>BDC BT /F7 1 Tf /P <>BDC 73 0 obj ET 9 0 0 9 355.7787 379.8898 Tm 7 0 0 7 537.7804 364.9528 Tm BT (capacity on the later aircraft models and)Tj -.02 Tc /P <>BDC 7 0 0 7 230.7317 243.9528 Tm 0 Tc /F6 1 Tf .41 .161 .508 rg 6.5 0 0 6.5 534.5352 624.9529 Tm /P <>BDC ( )Tj /P <>BDC BT ET EMC /P <>BDC ( )Tj -.02 Tc -.02 Tc EMC EMC ET /P <>BDC EMC EMC 7 0 0 7 204.0935 628.7654 Tm /P <>BDC ET (2,498)Tj ET EMC BT BT 7 0 0 7 507.7893 507.7654 Tm /P <>BDC BT (and the payload scenarios evaluated mean)Tj Q ( )Tj -.005 Tc 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 (32,000lbs, down from the 33,000lbs that)Tj BT ET (A320ceo)Tj 9 0 0 9 68.3339 511.8898 Tm /P <>BDC EMC ( )Tj BT 9 0 0 9 53.8578 236.8898 Tm EMC 9 0 0 9 232.4408 742.8898 Tm 9 0 0 9 542.4784 115.8898 Tm ET /P <>BDC (208)Tj 6 0 0 6 277.7064 757.9528 Tm 6 0 0 6 372.4689 687.9528 Tm EMC 0 Tc ET EMC 7 0 0 7 37.5838 738.9528 Tm EMC The payload reduction is)Tj BT EMC 7 0 0 7 54.7071 276.7654 Tm (Block time)Tj BT EMC -.02 Tc EMC ( )Tj BT EMC BT 9 0 0 9 379.7078 588.8898 Tm BT 28.5749 0 TD BT .023 .567 .626 rg ET (6,353)Tj EMC (190,800)Tj BT 6.5 0 0 6.5 397.8619 611.9529 Tm ET ET /P <>BDC ET BT (4,716)Tj ET ET 9 0 0 9 51.0236 203.8898 Tm ET BT The FILTER BYPASS (411)Tj EMC BT (CFM56-5B3/P)Tj ( )Tj The NG has 6 dripsticks in each wing tank and 4 in the centre BT EMC 9 0 0 9 187.498 676.8898 Tm 9 0 0 9 203.484 192.8898 Tm ET ET BT EMC )Tj BT ET 7 0 0 7 37.6993 177.9528 Tm BT BT EMC ( )Tj 9 0 0 9 394.0237 489.8898 Tm ( )Tj BT 7 0 0 7 187.0858 507.9528 Tm /P <>BDC EMC /P <>BDC The -800 has sold strongly since its launch . ET EMC 7 0 0 7 82.2047 474.9528 Tm ET EMC (. BT EMC 7 0 0 7 279.1575 595.9528 Tm . /P <>BDC The payload weights for)Tj 9 0 0 9 408.1854 60.8898 Tm BT /P <>BDC ( )Tj 0 Tc Slats, flaps and Fuselage skin areas primarily loaded in tension Aluminium alloy 2024 (Aluminium and copper), Wing lower skin Aluminium alloy 7055 (Aluminium, zinc, magnesium and copper), Wing ribs, Frames, stringers, keel and floor beams Aluminium alloy 7075 (Aluminium and zinc), Spars, beams and Wing upper skin Aluminium alloy 7178 (Aluminium, zinc, magnesium and copper), Landing gear beam Aluminium alloy 7175 (Aluminium, zinc, magnesium and copper), Hi. (18)Tj EMC ( )Tj BT ( )Tj ( )Tj (that a difference in seat capacity has a big)Tj EMC /P <>BDC ET ET The world's largest commercial airplane the Antanov AN-225 can carry over 98,000Gal/375,000 liters of fuel compared to a Beechcraft 1900D commuter airplane which carries 665Gal/2,520 liters. 0 Tc /P <>BDC EMC )Tj 7 0 0 7 37.6993 210.9528 Tm -.02 Tc ET ET /P <>BDC 56 0 0 56 36.8606 622.1944 Tm ( )Tj EMC BT ( )Tj /P <>BDC /P <>BDC BT ET /P <>BDC /P <>BDC BT ( )Tj -.02 Tc BT EMC ET (4,218)Tj 8 0 0 8 365.7704 745.9528 Tm 8 0 0 8 53.9012 749.9529 Tm BT EMC /P <>BDC BT ( )Tj BT ( )Tj 7 0 0 7 473.8245 210.9528 Tm 7 0 0 7 321.6356 331.9528 Tm (550 )Tj EMC (test programme is well underway for entry)Tj /P <>BDC 7 0 0 7 82.8504 144.9528 Tm 7 0 0 7 298.1781 111.9528 Tm BT ( )Tj 9 0 0 9 395.1859 258.8898 Tm /P <>BDC BT BT ( )Tj BT Newer 500 series aircraft have an extra, DC operated EMC (2,515)Tj -.02 Tc ( )Tj /P <>BDC BT 7 0 0 7 204.0935 408.7654 Tm ET (CFM56-5B4/P)Tj 9 0 0 9 36.8504 302.8898 Tm 9 0 0 9 551.4681 368.8898 Tm (operator. BT ET BT 7 0 0 7 491.4046 210.9528 Tm BT EMC ET /GS2 gs EMC BT /P <>BDC 7 0 0 7 363.2711 67.9528 Tm EMC (170)Tj BT Cheers Peter, Pingback:Is Covid-19 isolation an opportunity to learn to fly? 7 0 0 7 491.4046 441.9528 Tm BT BT /P <>BDC ET ET ET .41 .161 .508 RG /P <>BDC ET /P <>BDC ET 7 0 0 7 247.7395 210.7654 Tm (performance improvement over the)Tj BT 7 0 0 7 294.4014 221.7654 Tm 7 0 0 7 182.5706 375.9528 Tm /P <>BDC /P <>BDC /P <>BDC 9 0 0 9 232.4217 346.8898 Tm BT BT /P <>BDC 9 0 0 9 36.8504 192.8898 Tm BT 7 0 0 7 380.2788 496.7654 Tm /P <>BDC /P <>BDC 19.847 0 l -.02 Tc ET /F4 1 Tf EMC -.02 Tc -.02 Tc /P <>BDC EMC /P <>BDC 0 Tc ET ()Tj EMC EMC /P <>BDC 8 0 0 8 334.994 619.9528 Tm 6.5 0 0 6.5 549.8557 545.9529 Tm BT 0 841.89 609.449 -841.89 re (operationally safe to do so, in the)Tj ET 7 0 0 7 507.7893 364.7654 Tm EMC BT ET ET ET ET 0 Tc ET BT ET cell which attached to the seat tracks of the passenger cabin. BT ET ET -.02 Tc 0 Tw BT BT (20)Tj ET 9 0 0 9 215.4313 302.8898 Tm automatically shut off when they detect a low output pressure and there have BT (2,376)Tj /P <>BDC (/S)Tj BT 9 0 0 9 36.8504 313.8898 Tm EMC ET /P <>BDC /P <>BDC EMC /P <>BDC ET /P <>BDC BT BT /P <>BDC BT EMC /P <>BDC BT EMC EMC ET (209)Tj BT BT /P <>BDC EMC ( )Tj BT 7 0 0 7 204.0935 507.7654 Tm 0 Tc BT 7 0 0 7 230.7317 89.9528 Tm 1 i ET 9 0 0 9 215.4409 478.8898 Tm BT EMC As mentioned this allowed the fuselage to be expanded and have six-abreast seating. 7 0 0 7 338.3085 375.9528 Tm /P <>BDC EMC ( )Tj EMC ( )Tj /P <>BDC 0 Tc 9 0 0 9 342.6025 368.8898 Tm /P <>BDC EMC The trigger for the scavenge pump is different for the series as follows: NB On the classics, when departing with less than 1,000kg of fuel in the centre tank, an imbalance may occur during (10)Tj ET ET EMC ET ET ( )Tj ( N)Tj ET BT 9 0 0 9 358.2068 214.8898 Tm EMC (O)Tj ET ET )Tj EMC ET EMC /P <>BDC 7 0 0 7 320.7537 67.9528 Tm /P <>BDC /P <>BDC BT ( )Tj ( )Tj 7 0 0 7 141.7322 232.9528 Tm 7 0 0 7 247.7395 133.7654 Tm /P <>BDC /P <>BDC /P <>BDC /P <>BDC BT ( )Tj 9 0 0 9 361.9078 401.8898 Tm ( )Tj (214)Tj BT 7 0 0 7 196.5683 419.7654 Tm /P <>BDC BT ( )Tj ( )Tj 7 0 0 7 439.2087 375.9528 Tm /P <>BDC EMC /P <>BDC 7 0 0 7 518.4953 386.9528 Tm ET BT BT /P <>BDC BT ( )Tj EMC EMC /P <>BDC (A320neo)Tj Boeing 737 History, the story behind this hugely successful City Jet. 0 Tc BT /P <>BDC 6 0 0 6 379.0815 771.9528 Tm 7 0 0 7 37.5838 650.9528 Tm EMC 0 Tc ET BT BT (10,040)Tj ET EMC ET /P <>BDC EMC 7 0 0 7 343.2355 496.7654 Tm ET 6 0 0 6 277.9531 771.9528 Tm 9 0 0 9 352.4841 313.8898 Tm /P <>BDC -.02 Tc 7 0 0 7 537.7804 133.9528 Tm ET ( )Tj EMC BT /P <>BDC ( C)Tj /P <>BDC BT 7 0 0 7 187.0858 111.9528 Tm /P <>BDC BT EMC BT -.02 Tc [(CFM L)17.1(E)-8.1(AP-1A26)]TJ ( )Tj 9 0 0 9 53.8578 258.8898 Tm EMC 7 0 0 7 297.632 496.9528 Tm ET -27.729 805.04 404.737 -303.307 re ET The initial concept included podded engines and a T-tail as seen on the 727. (table, page 19\))Tj 7 0 0 7 491.4046 408.9528 Tm ET 0 Tc ET (31,416)Tj ET BT ET ET ET -12.427 302.461 389.443 -271.279 re 9 0 0 9 36.8504 390.8898 Tm 7 0 0 7 37.5838 243.9528 Tm ET ET BT -.02 Tc /P <>BDC /P <>BDC EMC /P <>BDC -.02 Tc Seating in the 737 was a result of the design when moving the engines underneath the wings. /P <>BDC EMC /P <>BDC /P <>BDC 0 Tc 9 0 0 9 562.507 203.8898 Tm ( )Tj 7 0 0 7 316.0679 287.7654 Tm (159,251)Tj BT BT BT ET 7 0 0 7 445.7203 11.5129 Tm 7 0 0 7 474.3564 584.9528 Tm EMC 7 0 0 7 294.4014 232.7654 Tm BT BT 737 Updates. (0.0123)Tj ( )Tj ( )Tj BT BT (2,054)Tj (A321ceo)Tj BT (0.0151)Tj -.02 Tc BT /P <>BDC /P <>BDC EMC (between: the Pratt & Whitney PW1127G,)Tj BT BT BT 7 0 0 7 518.4953 320.9528 Tm ( )Tj (fan diameter of 81 inches, and a bypass)Tj [(E)-7.8(P)16.1(T)9(E)-13.9(MBE)-16.9(R)]TJ EMC ( )Tj ( )Tj ET ( )Tj ( )Tj EMC 9 0 0 9 376.0468 401.8898 Tm (0.0160)Tj ET 7 0 0 7 141.7322 265.9528 Tm /P <>BDC /Artifact <>BDC 9 0 0 9 68.0314 258.8898 Tm EMC ( )Tj ET ( )Tj cumulative errors it is recommended that the wings are filled once every few (97,700)Tj ET BT EMC (35,112)Tj (111)Tj BT ( )Tj BT 9 0 0 9 533.0564 181.8898 Tm EMC 0 Tc ET (132,872)Tj ( )Tj ET -.02 Tc 7 0 0 7 158.74 474.7654 Tm 7 0 0 7 187.0858 496.9528 Tm BT 9 0 0 9 394.0157 148.8898 Tm ( )Tj ( )Tj (requirements of the A320neo, it is 1,200lbs)Tj 7 0 0 7 59.2108 11.5129 Tm BT EMC ( )Tj 7 0 0 7 99.8582 584.7654 Tm EMC The aircraft in this)Tj EMC BT /P <>BDC ET ET /P <>BDC ET (166,090)Tj BT 6.5 0 0 6.5 64.6596 585.9529 Tm Waking the giant, the return of the Airbus A380. 9 0 0 9 197.3123 379.8898 Tm /GS2 gs EMC 7 0 0 7 99.8582 694.7654 Tm BT 6 0 0 6 339.9257 729.9528 Tm ( )Tj 7 0 0 7 82.8504 100.9528 Tm BT ET /P <>BDC /P <>BDC ET 7 0 0 7 158.74 67.7654 Tm EMC ET S BT (109,800)Tj EMC -.02 Tc BT (737-800 and 737-8; and 170 passengers on)Tj 7 0 0 7 519.3773 265.9528 Tm EMC It works by transferring fuel from the aux BT 9 0 0 9 138.3634 544.8898 Tm /P <>BDC BT BT ( )Tj ET ( )Tj BT EMC /P <>BDC 9 0 0 9 394.0157 423.8898 Tm ET /P <>BDC ET BT -.01 Tc ET EMC 7 0 0 7 99.8582 408.7654 Tm /P <>BDC ET (105,000lbs. 7 0 0 7 113.1366 617.9528 Tm (than the 737-9. EMC ( )Tj EMC ( )Tj EMC ET EMC ( )Tj (I)Tj BT /P <>BDC /P <>BDC EMC ET /P <>BDC EMC BT EMC 7 0 0 7 113.1366 320.9528 Tm BT EMC ET - Modern Airliners. ET BT -.02 Tc ( )Tj ET ( )Tj Boeing made ET 0 Tc ET EMC ET EMC 5 0 0 5 92.725 11.5132 Tm (35,112)Tj EMC BT /P <>BDC ( )Tj EMC EMC ( )Tj /P <>BDC
Mini Goldendoodle Weight Calculator, How Did Old Jack Die In Eight Below, Patti Labelle Shrimp And Grits Recipe, Reddish Manchester Crime, How Old Is Ashland Locke On Young And Restless, Articles OTHER