7 0 0 7 158.74 100.7654 Tm ( )Tj EMC (937)Tj ET (1,823)Tj /P <>BDC /P <>BDC ( )Tj /P <>BDC (CFM56-7B27B3 installed on the 737-)Tj EMC /P <>BDC 9 0 0 9 232.4217 500.8898 Tm -.02 Tc 0 Tc ET /P <>BDC ( )Tj 7 0 0 7 554.7883 705.7654 Tm EMC EMC ( )Tj ET /GS1 gs 9 0 0 9 53.8582 71.8898 Tm BT 7 0 0 7 82.2047 573.9528 Tm 9 0 0 9 394.0157 434.8898 Tm ( )Tj (182,700)Tj ( )Tj -.02 Tc 6.5 0 0 6.5 448.2959 545.9529 Tm ( )Tj /P <>BDC -.02 Tc 9 0 0 9 544.6834 126.8898 Tm EMC (576)Tj 7 0 0 7 107.1165 661.9528 Tm (737 MAX-9 \(737-9\) )Tj -.02 Tc ( )Tj The flight)Tj ET /P <>BDC .41 .161 .508 rg BT ( )Tj blue VALVE OPEN lights similar to that on the crossfeed valve. BT 6.5 0 0 6.5 227.9655 565.9529 Tm EMC /P <>BDC EMC EMC BT 7 0 0 7 507.7893 595.7654 Tm ET EMC /P <>BDC 8 0 0 8 275.1912 745.9528 Tm (16,170)Tj ( )Tj ( )Tj /P <>BDC Can you confirm if Im right or wrong? ET concentration at eight different locations. ET 7 0 0 7 338.6433 364.7654 Tm (performance of the two reduces to 0.8%)Tj /Artifact <>BDC 7 0 0 7 354.6933 298.7654 Tm EMC ET /P <>BDC [(SS)-9(U)8.1(E)]TJ Their version of the Boeing 737-800 is the Airbus A220. ET /P <>BDC ET EMC /P <>BDC 7 0 0 7 537.7804 166.9528 Tm ET ET -.02 Tc ET fuel burn. /P <>BDC 9 0 0 9 548.4937 71.8898 Tm ( )Tj (170)Tj ( )Tj /P <>BDC ( )Tj -.02 Tc (373-388)Tj ( )Tj ET ET ET /P <>BDC /P <>BDC ET ET ET 0 Tc ET /P <>BDC BT ( )Tj EMC EMC EMC 9 0 0 9 408.1854 610.8898 Tm 7 0 0 7 131.6494 375.7654 Tm 9 0 0 9 232.4217 412.8898 Tm BT 6.5 0 0 6.5 64.6596 742.9529 Tm 7 0 0 7 520.6108 683.9528 Tm EMC EMC EMC 9 0 0 9 182.2339 500.8898 Tm BT 0 Tc /P <>BDC ET EMC 9 0 0 9 186.3413 291.8898 Tm /P <>BDC EMC 7 0 0 7 99.8582 705.7654 Tm ( )Tj EMC /P <>BDC /P <>BDC /P <>BDC BT EMC BT EMC /F1 1 Tf BT BT 9 0 0 9 464.4377 621.8898 Tm (127)Tj BT EMC EMC 7 0 0 7 508.6712 430.7654 Tm EMC /P <>BDC /P <>BDC ( )Tj BT EMC /P <>BDC ET been many other improvements to wiring and FQIS. BT BT BT /P <>BDC 7 0 0 7 456.2165 441.7654 Tm -.02 Tc /P <>BDC /P <>BDC ( )Tj ( )Tj -.01 Tc -.02 Tc ET /P <>BDC ET ( )Tj (737-9)Tj 7 0 0 7 536.3849 364.7654 Tm BT /P <>BDC /P <>BDC EMC BT /P <>BDC ET ET ET EMC (CFM56-7B26)Tj (compares to a tracked distance of)Tj /P <>BDC EMC ET /P <>BDC 9 0 0 9 232.4217 104.8898 Tm ( )Tj ET BT ( )Tj (124,650)Tj ET ( )Tj 7 0 0 7 141.7322 540.9528 Tm (112)Tj EMC -.02 Tc 9 0 0 9 411.0181 60.8898 Tm BT /P <>BDC 8 0 0 8 474.6331 771.7654 Tm 7 0 0 7 82.2047 716.9528 Tm -.02 Tc BT /P <>BDC ET .661 .752 .896 rg 10 0 0 10 230.6475 794.2914 Tm ET 8 0 0 8 542.9269 786.8898 Tm BT ( )Tj EMC EMC (66,096)Tj 9 0 0 9 561.5176 522.8898 Tm ET Aircraft have been NGS provisioned since l/n 1935 and it has been installed since l/n 2620 onwards. 0 Tc EMC 9 0 0 9 202.684 357.8898 Tm /P <>BDC EMC BT BT 9 0 0 9 411.0181 126.8898 Tm 9 0 0 9 181.8233 49.8898 Tm 6 0 0 6 418.9814 701.9528 Tm ( )Tj EMC /P <>BDC EMC EMC /P <>BDC /P <>BDC ET 8 0 0 8 38.4438 689.9528 Tm /P <>BDC (1,025)Tj EMC -.02 Tc ( )Tj BT ( )Tj (covers a 3,300-3,400nm range with a full)Tj EMC EMC 7 0 0 7 258.2805 672.7654 Tm EMC 9 0 0 9 212.7538 423.8898 Tm EMC ET BT 9 0 0 9 51.0236 71.8898 Tm EMC /Artifact <>BDC /P <>BDC ET 7 0 0 7 37.0536 705.9528 Tm 7 0 0 7 537.7804 364.9528 Tm /F7 1 Tf ( )Tj /P <>BDC /P <>BDC (20)Tj EMC 8 0 0 8 99.8582 771.7654 Tm EMC EMC EMC 0 Tc EMC /F6 1 Tf BT EMC BT ET BT /P <>BDC BT BT EMC 8 0 0 8 507.842 760.7654 Tm [(7)-33(3)8(7-8)]TJ 7 0 0 7 241.5317 342.9528 Tm 9 0 0 9 180.5261 423.8898 Tm ET 9 0 0 9 394.0237 313.8898 Tm ( )Tj 7 0 0 7 124.1242 298.7654 Tm ET /P <>BDC (150)Tj /P <>BDC /P <>BDC EMC (A)Tj EMC EMC ( )Tj /P <>BDC (26,000lbs thrust on the A320neo powered)Tj ET (5,394)Tj EMC BT 9 0 0 9 408.1854 346.8898 Tm BT 9 0 0 9 215.433 412.8898 Tm /P <>BDC /P <>BDC ET 0 Tc 9 0 0 9 36.8504 379.8898 Tm EMC <>stream EMC EMC 0 Tc ET ET /GS2 gs (900ER\(W\) across the 14 routes with the)Tj /P <>BDC BT /P <>BDC 7 0 0 7 131.6494 672.7654 Tm /P <>BDC ( )Tj ( )Tj BT BT /P <>BDC 9 0 0 9 548.3146 104.8898 Tm ( )Tj /P <>BDC /P <>BDC ET (31,416)Tj 6 0 0 6 497.1212 729.9528 Tm ET 17 0 0 17 36.8606 791.6944 Tm /P <>BDC ET ( )Tj ( )Tj 9 0 0 9 383.6398 709.8898 Tm )Tj EMC BT BT 7 0 0 7 404.101 287.7654 Tm 0 Tc /P <>BDC /P <>BDC 9 0 0 9 68.0071 412.8898 Tm EMC ET The 737-800 project began in 1994, with Hapag-Lloyd Airlines ofGermany placing the first order for this aircraft. ET ET EMC BT EMC EMC 0 Tc 6.5 0 0 6.5 192.6116 689.9529 Tm 6 0 0 6 513.0339 673.9528 Tm 0 Tc /GS2 gs 7 0 0 7 354.6933 540.7654 Tm EMC EMC ( )Tj BT (scheduled times planned by the carrier may)Tj EMC -.01 Tc 0 Tc [(F)-21(LL/47)]TJ (187,700lbs, an MLW of 157,300lbs and a)Tj -.02 Tc ET 6 0 0 6 255.8802 771.9528 Tm ET ET /P <>BDC ET EMC -.02 Tc ET ( )Tj /P <>BDC /P <>BDC EMC Aircraft must carry enough fuel to taxi, climb, cruise, descent, and mutliple reserves. /P <>BDC (0.0124)Tj 8 0 0 8 165.2278 760.9528 Tm /OC /MC2278 BDC /P <>BDC ET ( )Tj (\(see table,)Tj BT ( )Tj ET /P <>BDC 7 0 0 7 258.2805 639.7654 Tm EMC BT /P <>BDC -.02 Tc EMC BT ET ET ( )Tj BT EMC 7 0 0 7 125.6292 738.7654 Tm 9 0 0 9 367.2172 269.8898 Tm 7 0 0 7 354.6933 474.7654 Tm /P <>BDC ET BT ET /P <>BDC supplied to the center wing tank and the oxygenenriched air (OEA) is vented 7 0 0 7 108.6215 331.9528 Tm ( )Tj /P <>BDC (37,653)Tj ET 0 Tc ET ET 7 0 0 7 37.5838 243.9528 Tm -.01 Tc BT -.02 Tc (be charged the same in operation for this)Tj (37,653lbs )Tj ET 7 0 0 7 294.4014 738.7654 Tm )Tj /P <>BDC EMC EMC ET ( )Tj 7 0 0 7 241.5317 738.9528 Tm EMC BT /P <>BDC BT 9 0 0 9 229.6064 126.8898 Tm 9 0 0 9 53.8338 214.8898 Tm EMC BT EMC 7 0 0 7 387.0932 144.9528 Tm ( )Tj EMC 0 Tc BT /P <>BDC /Artifact <>BDC EMC 7 0 0 7 54.7071 419.7654 Tm BT EMC /P <>BDC EMC ET BT 9 0 0 9 411.0097 533.8898 Tm BT ET BT 0 Tc ( )Tj ET EMC EMC EMC 7 0 0 7 554.7883 265.7654 Tm /P <>BDC 0 Tc ET ET EMC The NGS is an onboard inert gas system that uses an (152)Tj ET (31,416)Tj /P <>BDC EMC ET ( )Tj BT /P <>BDC 0 Tc 5.25 0 0 5.25 447.6106 11.5129 Tm BT BT BT endobj EMC ( )Tj [(R)13.9(OUT)10(E CHARA)16.1(CT)10(ERIS)8.1(T)-8.1(I)0(C)-17.1(S)0( F)8.1(OR ANAL)86.9(YSIS OF AIR)7.1(CRAF)-12.9(T)18.1( PERF)8.1(ORMANCE )]TJ ( )Tj ( )Tj /P <>BDC 7 0 0 7 537.7804 298.9528 Tm /P <>BDC ET EMC EMC EMC EMC 0 Tc BT /P <>BDC /P <>BDC 7 0 0 7 508.4124 375.7654 Tm EMC ( )Tj -.01 Tc EMC /P <>BDC EMC BT EMC 7 0 0 7 343.2355 661.7654 Tm /P <>BDC EMC ET 9 0 0 9 560.5186 214.8898 Tm ET EMC EMC EMC ( )Tj EMC (The wind speed was based on an 85%)Tj ET (2,748)Tj ET ( )Tj ( )Tj ET EMC BT ( )Tj ( )Tj EMC BT EMC 6.5 0 0 6.5 430.0114 565.9529 Tm ET 0 Tc 7 0 0 7 182.5706 276.9528 Tm /P <>BDC BT EMC EMC EMC 7 0 0 7 230.6618 430.9528 Tm ET EMC /P <>BDC ET ET In contrast, Boeing has)Tj 7 0 0 7 297.632 595.9528 Tm /P <>BDC EMC ET (31,416)Tj 5.25 0 0 5.25 515.3989 11.5129 Tm 7 0 0 7 387.0932 331.9528 Tm 9 0 0 9 232.4217 577.8898 Tm /P <>BDC 9 0 0 9 566.9979 423.8898 Tm -.02 Tc The service ceiling is 41,000 feet. BT ET -.02 Tc ( )Tj ( )Tj ET /P <>BDC ( )Tj The weight increase in)Tj ET /P <>BDC /P <>BDC EMC /P <>BDC ET 9 0 0 9 394.0157 621.8898 Tm -.02 Tc (0.0135)Tj /F6 1 Tf (CFM56-5B4/P)Tj -.02 Tc 9 0 0 9 394.0237 467.8898 Tm BT BT (-58)Tj EMC 10.486 7.6165 l BT 7 0 0 7 108.6215 738.9528 Tm BT EMC (\(see table, this)Tj 7 0 0 7 99.8582 166.7654 Tm /P <>BDC ET BT ( )Tj 6.5 0 0 6.5 397.1339 663.9529 Tm (configuration used in the study is)Tj 7 0 0 7 456.2165 177.7654 Tm ET BT ET /P <>BDC /P <>BDC 7 0 0 7 53.8582 353.7654 Tm 9 0 0 9 552.5312 687.8898 Tm ( )Tj EMC ET (854)Tj ( )Tj -2.4549 -3.9026 m ET (0.0112)Tj 7 0 0 7 297.632 518.9528 Tm 0 Tc ET ET ET 9 0 0 9 522.1112 247.8898 Tm ( )Tj ET 7 0 0 7 230.7317 628.9528 Tm /P <>BDC ET 0 Tc ET (maximum landing weight \(MLW\) of)Tj /P <>BDC (112)Tj /P <>BDC -.02 Tc ET EMC - Simmonds, Digital Fuel Quantity Indicator Error Codes /P <>BDC EMC (0.0141)Tj ( )Tj ( )Tj /P <>BDC ET BT 7 0 0 7 230.7317 276.9528 Tm /P <>BDC BT /F4 1 Tf 0 Tc (0.0108)Tj ET .151 .147 .15 rg EMC BT EMC 6.5 0 0 6.5 233.8677 532.9529 Tm 9 0 0 9 411.0181 467.8898 Tm 6.5 0 0 6.5 230.3055 722.9529 Tm (157,300)Tj oxygen in the air. /P <>BDC 9 0 0 9 436.7009 104.8898 Tm BT ( )Tj ET BT ( )Tj /Im2 Do /P <>BDC ET (737 MAX 8 & 9 fuel)Tj EMC /P <>BDC 6 0 0 6 237.4295 701.9528 Tm (the aircraft in this study are shown )Tj EMC EMC BT /P <>BDC /GS1 gs ET ET EMC ET /P <>BDC (rating on the CFM LEAP-1A32 to)Tj (150)Tj -.02 Tc /P <>BDC BT ET EMC The engine)Tj Q ( )Tj 9 0 0 9 215.4409 291.8898 Tm ET BT ( )Tj 0 Tc -.02 Tc 9 0 0 9 370.9169 379.8898 Tm /P <>BDC BT 6.5 0 0 6.5 276.5184 565.9529 Tm ET ( )Tj ( )Tj 7 0 0 7 337.4684 683.9528 Tm ET (capacity, whereas the A321neo, with the)Tj ( )Tj ET /F1 1 Tf BT The VNE or never exceed speed for the Boeing 737-800 is 340 KIAS(Knots indicated airspeed) or Mach 0.82. BT /P <>BDC 63 0 obj BT ET EMC BT ET ET EMC (170)Tj /P <>BDC BT ET EMC BT 9 0 0 9 394.0157 599.8898 Tm EMC /P <>BDC /P <>BDC ( )Tj 9 0 0 9 394.0123 533.8898 Tm EMC (A320neo:)Tj (29,359)Tj ET BT 0 Tc 9 0 0 9 53.8578 148.8898 Tm ET BT ( )Tj BT EMC ( )Tj BT /F4 1 Tf BT 9 0 0 9 394.0123 500.8898 Tm ET ( )Tj 9 0 0 9 215.4313 269.8898 Tm EMC ET EMC ET EMC /P <>BDC EMC /P <>BDC EMC (137,789)Tj /P <>BDC /GS1 gs 9 0 0 9 232.438 181.8898 Tm EMC /F6 1 Tf 7 0 0 7 315.1859 144.7654 Tm EMC ET 0 Tc 6.5 0 0 6.5 243.8814 689.9529 Tm EMC (172,992)Tj /P <>BDC 9 0 0 9 214.9959 159.8898 Tm BT 9 0 0 9 408.1854 511.8898 Tm /P <>BDC BT /P <>BDC /P <>BDC EMC EMC [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ 0 841.89 609.449 -841.89 re EMC /P <>BDC 7 0 0 7 507.7893 67.7654 Tm 9 0 0 9 526.8993 643.8898 Tm BT BT [(CFM L)17.1(E)-8.1(AP-1A32)]TJ 7 0 0 7 338.4211 430.9528 Tm BT BT ET EMC EMC /P <>BDC If a fuel gauge is u/s the quantity