.014984 824.882 572.583 17.008 re (analysis is for the A320neo on BOS-SFO,)Tj EMC (427,890)Tj /GS1 gs 7 0 0 7 387.0159 474.9528 Tm 9 0 0 9 522.5095 181.8898 Tm EMC 8 0 0 8 38.4438 577.9528 Tm [(CFM L)17.1(E)-8.1(AP-1A26)]TJ /P <>BDC ( )Tj ET /P <>BDC BT ET 7 0 0 7 113.1366 419.9528 Tm 9 0 0 9 394.0123 104.8898 Tm 0 Tc BT EMC EMC To allow a fair)Tj ET ( )Tj 6.5 0 0 6.5 435.6469 722.9529 Tm 7 0 0 7 337.4684 694.9528 Tm EMC BT BT /P <>BDC (1,824)Tj 0 Tc 7 0 0 7 355.3163 210.7654 Tm EMC /P <>BDC EMC ET /P <>BDC BT 0 Tc ET BT ET BT EMC 0 Tc /P <>BDC ET BT 0 Tc EMC 9 0 0 9 382.6146 368.8898 Tm 9 0 0 9 215.4409 159.8898 Tm the rear of the fwd hold and the front of the aft hold, this reduces the C of G EMC BT (sharklets. ( )Tj /P <>BDC /P <>BDC EMC /P <>BDC ET 9 0 0 9 53.8582 291.8898 Tm EMC ET 9 0 0 9 204.4018 665.8898 Tm BT 0 Tc /P <>BDC EMC ET ( )Tj BT /P <>BDC BT (difference in fuel cost per ASM, however,)Tj -.02 Tc -.02 Tc BT ( )Tj The fwd and aft tanks are switched off when the /P <>BDC BT 9 0 0 9 564.8379 269.8898 Tm (7,168)Tj EMC ET 6 0 0 6 322.3867 659.9528 Tm 7 0 0 7 490.8321 474.7654 Tm BT BT ET /P <>BDC EMC -.02 Tc BT ET 6.5 0 0 6.5 192.0331 676.9529 Tm BT EMC (737-9)Tj ET ET -.02 Tc BT EMC 0 Tc [(AIRL)8.1(INE & AIR)7.1(CRAF)-12.9(T)18.1( OPERA)56.9(T)-8.1(ION)-13.9(S)]TJ [(A3)24.9(20ceo v)12.9(ersus 7)-33(3)8.1(7-800 )]TJ BT BT Calculates enroute fuel burn based on cruise altitude and trip distance. ( )Tj ET safest way forward, but is very expensive and possibly impractical. ET BT ET EMC EMC ET BT (208)Tj EMC /P <>BDC EMC ET .023 .567 .626 rg 7 0 0 7 141.7322 375.9528 Tm 0 Tc /P <>BDC /P <>BDC /P <>BDC /P <>BDC -.02 Tc 7 0 0 7 337.6855 529.9528 Tm 0 Tc 9 0 0 9 369.4048 467.8898 Tm (seat capacity as the 737-800 due to the exit)Tj BT EMC EMC BT ( )Tj Wing provisioning for the 737-800 adds approx. EMC EMC ET EMC (comparison. (ESAD)Tj ( )Tj (scenario, the difference in fuel burn)Tj EMC /P <>BDC /P <>BDC ( )Tj 0 Tc BT 6 0 0 6 154.1438 757.9528 Tm ( )Tj 6.5 0 0 6.5 381.6589 558.9529 Tm ET ET ET (average improvement in trip fuel burn. ET BT /P <>BDC 7 0 0 7 491.7142 529.7654 Tm ET BT BT /P <>BDC EMC EMC 7 0 0 7 337.4684 661.9528 Tm ( )Tj 9 0 0 9 550.1644 170.8898 Tm EMC EMC BT ( )Tj /P <>BDC EMC 7 0 0 7 299.0601 122.9528 Tm /P <>BDC EMC BT EMC /P <>BDC EMC /P <>BDC q BT ET -.015 Tc BT (and their operational use by mainline)Tj ( )Tj /P <>BDC ET EMC /P <>BDC -.02 Tc EMC 0 Tc (0.0135)Tj 0 Tc 7 0 0 7 338.3085 309.9528 Tm BT /P <>BDC EMC [(OM)8.1(M)-12.9(E)-24.9(R)7.1(C)8.1(E)]TJ ET BT BT 0 Tc ET ET /P <>BDC -.02 Tc EMC ET ET ( )Tj (9,451)Tj BT ET .41 .161 .508 rg (1,058)Tj EMC 7 0 0 7 316.0679 309.7654 Tm EMC (4,836)Tj -.02 Tc 9 0 0 9 548.3115 412.8898 Tm BT 9 0 0 9 53.8582 93.8898 Tm EMC /P <>BDC /P <>BDC /OC /MC5061 BDC ET 9 0 0 9 216.03 687.8898 Tm -.02 Tc EMC ( )Tj ET /P <>BDC 7 0 0 7 99.8582 540.7654 Tm ( )Tj ( The wind component and)Tj ( )Tj (remain key aircraft for many operators)Tj BT ET ( )Tj ET BT ET 0 Tc 7 0 0 7 53.8582 551.7654 Tm BT /P <>BDC ET (- nm)Tj /P <>BDC BT /P <>BDC EMC (37,653)Tj (BOS-MIA)Tj (additional benefit in this comparison. BT 7 0 0 7 554.7883 540.7654 Tm -.02 Tc -.02 Tc /P <>BDC EMC EMC /P <>BDC 7 0 0 7 54.7071 232.7654 Tm (1,824)Tj /P <>BDC (37,653lbs)Tj ET ET 9 0 0 9 36.8504 258.8898 Tm ET . EMC 9 0 0 9 534.7515 599.8898 Tm ET BT /P <>BDC EMC /P <>BDC Q ( )Tj EMC BT EMC BT ET ET ET BT /P <>BDC [(BOS-SE)-13.9(A)]TJ EMC /F6 1 Tf (0.0112)Tj /P <>BDC ( )Tj /P <>BDC EMC 7 0 0 7 554.7883 221.7654 Tm ET EMC BT BT /P <>BDC /P <>BDC 7 0 0 7 141.7322 276.9528 Tm (5,126)Tj ( )Tj .001 Tc /P <>BDC BT (the fuel consumption for each type over)Tj BT (\(see table, this)Tj (fuel capacity of 6,303USG )Tj 7 0 0 7 54.5916 144.7654 Tm /P <>BDC 6.5 0 0 6.5 121.1068 532.9529 Tm EMC BT (series has a weight penalty because of its)Tj ET /P <>BDC The PPS flight)Tj (BOS-MIA)Tj EMC EMC EMC -.02 Tc BT BT /P <>BDC ( A)Tj EMC ET ET -.02 Tc ET 9 0 0 9 394.0315 786.8898 Tm 6 0 0 6 258.3167 715.9528 Tm 6 0 0 6 320.3167 757.9528 Tm .0161 Tc 0 Tc W n EMC EMC ET ( )Tj /P <>BDC EMC /P <>BDC ( )Tj ( )Tj (comparison of the fuel burn performance. ET BT EMC ET /P <>BDC ( )Tj EMC ET /P <>BDC ET 7 0 0 7 316.0679 342.7654 Tm body angle so number 2 engine fuel is drawn from main tank 2, while engine 1 is EMC BT EMC /OC /MC852 BDC BT 0 Tc 0 Tc EMC ET ET BT BT I started of using with this image. ( )Tj BT ET /P <>BDC ET -.01 Tc ET EMC /P <>BDC BT ET EMC /P <>BDC 7 0 0 7 386.3929 716.9528 Tm BT 7 0 0 7 295.2833 199.7654 Tm [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ ET EMC 9 0 0 9 366.6417 137.8898 Tm ( )Tj ET /P <>BDC EMC /P <>BDC BT /F1 1 Tf /P <>BDC 8 0 0 8 276.7109 633.9528 Tm [(TU)-8.1(S/101)]TJ ( )Tj /P <>BDC ET 7 0 0 7 439.2087 298.9528 Tm (payload 1 and payload 2 scenarios, the)Tj 19.843 0 l EMC BT ( )Tj EMC BT 8 0 0 8 225.1837 675.9528 Tm EMC -.02 Tc BT /P <>BDC ET /P <>BDC /P <>BDC EMC 7 0 0 7 204.0935 573.7654 Tm BT ET ET /P <>BDC EMC ET /P <>BDC 0 Tc 6.5 0 0 6.5 332.6961 735.9529 Tm EMC ET ( )Tj /P <>BDC ET EMC 6 0 0 6 184.3662 701.9528 Tm EMC /P <>BDC BT BT BT EMC 7 0 0 7 380.2788 463.7654 Tm -.02 Tc 6.5 0 0 6.5 64.6596 545.9529 Tm ( )Tj ET EMC BT 7 0 0 7 230.7317 166.9528 Tm -.01 Tc -.01 Tc BT /P <>BDC 0 Tc EMC 7 0 0 7 427.7291 287.9528 Tm -.02 Tc /P <>BDC -.02 Tc 9 0 0 9 568.024 148.8898 Tm BT ET 9 0 0 9 369.7648 346.8898 Tm BT ET ET ET 9 0 0 9 215.4409 335.8898 Tm ( )Tj EMC -.02 Tc ( )Tj BT /P <>BDC (192 seats. EMC EMC EMC /P <>BDC -.02 Tc -.02 Tc ( )Tj BT /P <>BDC (145,505lbs, and a fuel capacity of 6,303)Tj EMC /P <>BDC 518.723 0 l (0.0142)Tj -.02 Tc 7 0 0 7 476.1204 661.9528 Tm EMC ( )Tj 7 0 0 7 95.225 11.5132 Tm -.02 Tc 9 0 0 9 36.8504 368.8898 Tm BT 9 0 0 9 36.8504 335.8898 Tm EMC ( )Tj EMC BT ( )Tj ET ( )Tj /P <>BDC /P <>BDC A series of ten tests were performed (five flight, BT /P <>BDC ( )Tj BT /P <>BDC ET (109)Tj BT EMC ET BT /P <>BDC /P <>BDC EMC ( )Tj ET ( )Tj ( )Tj /P <>BDC (136)Tj 261 0 obj ( )Tj EMC EMC /P <>BDC BT ET /P <>BDC (this page\))Tj [(F)43(uel burn/)]TJ 6 0 0 6 539.8061 760.9528 Tm ET ( )Tj EMC EMC 9 0 0 9 455.0733 60.8898 Tm 0 Tc 8 0 0 8 322.6267 760.9528 Tm BT .151 .147 .15 rg 9 0 0 9 563.6848 401.8898 Tm /P <>BDC ET /P <>BDC (A320neo)Tj ( )Tj ET BT /P <>BDC EMC /P <>BDC 9 0 0 9 232.4217 82.8898 Tm /Artifact <>BDC /P <>BDC BT 9 0 0 9 232.4217 522.8898 Tm (A320ceo and A320neo in this study. -.02 Tc /P <>BDC BT /P <>BDC EMC ( )Tj ( )Tj (The cost index used is heavily)Tj BT EMC ( )Tj ability of GBI to reduce fuel tank flammability. 5.25 0 0 5.25 492.6848 11.5129 Tm BT ET /P <>BDC EMC ET /P <>BDC (209)Tj BT BT /P <>BDC 7 0 0 7 403.478 221.7654 Tm /P <>BDC EMC vlXf6.vlWfvlXyeb/k/+6**]CR$2T*+-t=* (&g@a};z53I$]I\+eSE_ >YXKt87^-+ L%!'W+6Q8P8s' 0 Tc 7 0 0 7 362.3891 375.9528 Tm BT (variant offers 26,000lbs of thrust, with a)Tj 7 0 0 7 294.4014 243.7654 Tm 0 Tc (achieve five inches extra legroom. BT BT EMC ( )Tj EMC (CFM56-5B3/P)Tj BT 9 0 0 9 229.6141 434.8898 Tm BT 7 0 0 7 444.737 78.7654 Tm 7 0 0 7 535.5029 342.7654 Tm /P <>BDC ET ET (-54)Tj ( )Tj ET ( )Tj ET BT 9 0 0 9 196.1514 390.8898 Tm /P <>BDC 9 0 0 9 36.8504 280.8898 Tm -.02 Tc EMC allowed for deposit of the ground-based NEA into the center wing tank (CWT). 6.5 0 0 6.5 549.8557 598.9529 Tm BT (35,112)Tj BT Neither the 737-800 nor the 737-8)Tj BT EMC ET EMC ET 9 0 0 9 411.0097 533.8898 Tm (176)Tj ( )Tj ( )Tj 0 Tc EMC EMC ( )Tj -.01 Tc /P <>BDC /P <>BDC /P <>BDC ET ET /Artifact <>BDC -.01 Tc ET EMC 6.5 0 0 6.5 173.5238 637.9529 Tm BT ET EMC /P <>BDC 9 0 0 9 53.8338 214.8898 Tm BT /P <>BDC /P <>BDC EMC ET 0 Tc (150-158)Tj 9 0 0 9 367.0732 423.8898 Tm BT ET 7 0 0 7 354.6933 298.7654 Tm 6.5 0 0 6.5 243.7903 611.9529 Tm ET 9 0 0 9 546.9046 423.8898 Tm ET BT BT ET ET ( )Tj 9 0 0 9 394.0157 346.8898 Tm /P <>BDC 9 0 0 9 270.2513 313.8898 Tm 6.5 0 0 6.5 432.488 558.9529 Tm EMC BT EMC (0.0155)Tj 8 0 0 8 334.994 661.9528 Tm BT EMC 6.5 0 0 6.5 346.5844 735.9529 Tm ET ET (31,416)Tj BT 0 Tc ET /P <>BDC BT 0 Tc BT BT .151 .147 .15 rg 9 0 0 9 394.0123 236.8898 Tm BT BT 0 Tc EMC EMC /P <>BDC endobj ET EMC BT /P <>BDC ET (1,272)Tj EMC EMC 0 Tc ( )Tj BT 9 0 0 9 394.0315 148.8898 Tm (0.0158)Tj ( )Tj /P <>BDC BT endstream 0 Tc 9 0 0 9 361.9529 159.8898 Tm (162,701)Tj BT /P <>BDC 7 0 0 7 508.4124 122.7654 Tm 9 0 0 9 36.8504 225.8898 Tm 7 0 0 7 99.8582 441.7654 Tm ET BT /P <>BDC 6.5 0 0 6.5 296.2827 637.9529 Tm 7 0 0 7 316.0679 408.7654 Tm /P <>BDC EMC /P <>BDC ( )Tj endobj BT /P <>BDC f ET -.01 Tc EMC /P <>BDC BT /P <>BDC EMC ET BT 9 0 0 9 36.8504 115.8898 Tm 0 Tc BT BT ET /P <>BDC ( )Tj 0 Tc EMC (4,716)Tj 7 0 0 7 403.478 727.7654 Tm 7 0 0 7 326.2278 738.9528 Tm ( )Tj /P <>BDC (City-pair)Tj (136)Tj (31,416)Tj 7 0 0 7 518.4953 320.9528 Tm These incidents, and 15 more on other types since 1959, ET /F1 1 Tf (737-800W)Tj 6.5 0 0 6.5 227.9655 565.9529 Tm ET (tracked distance, ESAD, and the difference)Tj ET /P <>BDC (on the longest sector. 0 Tw ET 7 0 0 7 101.0963 386.9528 Tm (ASM is 0.09 cents better for the A321neo. BT /P <>BDC 7 0 0 7 404.101 265.7654 Tm /P <>BDC /P <>BDC /P <>BDC ET 0 Tc EMC ET ET EMC /F6 1 Tf /P <>BDC 6 0 0 6 561.1317 771.9528 Tm [(CFM L)17.1(E)-8.1(AP-1A32)]TJ BT /P <>BDC ET /P <>BDC (to allow a clearer performance and fuel)Tj EMC (989)Tj -.9038 -.6598 -1.2447 -.5357 -1.6041 -.5355 c (667)Tj ET /P <>BDC (\(see table, this)Tj ET EMC 7 0 0 7 37.0536 661.9528 Tm ET EMC 7 0 0 7 125.6292 738.7654 Tm 13 0 0 13 355.5757 115.8898 Tm 9 0 0 9 411.0181 313.8898 Tm 9 0 0 9 385.5399 115.8898 Tm ET BT ( )Tj ET /P <>BDC BT EMC 9 0 0 9 394.0123 522.8898 Tm EMC BT ( )Tj 7 0 0 7 387.0159 540.9528 Tm BT BT 6.5 0 0 6.5 64.6596 742.9529 Tm /P <>BDC 7 0 0 7 354.6933 628.7654 Tm 8 0 0 8 315.034 760.7654 Tm BT EMC 9 0 0 9 36.8504 522.8898 Tm EMC ET ET 0 Tc ET /P <>BDC /P <>BDC EMC BT -.02 Tc -.02 Tc /P <>BDC BT EMC ET /P <>BDC ( )Tj /P <>BDC 0 Tc [(CFM L)17.1(E)-8.1(AP-1A26)]TJ 1 i ET ( )Tj 8 0 0 8 124.845 619.9528 Tm BT /P <>BDC BT EMC 9 0 0 9 53.8582 742.8898 Tm /P <>BDC -.01 Tc -.02 Tc BT 0 Tc W n [(7)-33(3)8.1(7-800 & 7)-33(3)8.1(7-8 )]TJ ( )Tj ( )Tj /P <>BDC ( )Tj ET ( )Tj .41 .161 .508 RG -.02 Tc /P <>BDC BT EMC EMC ( )Tj (includes checked and carry-on luggage. /P <>BDC 9 0 0 9 378.9498 368.8898 Tm EMC /P <>BDC /P <>BDC EMC EMC BT ET [(M)-9(L)51(W - lbs)]TJ /P <>BDC BT (-62)Tj /P <>BDC EMC /P <>BDC EMC 7 0 0 7 445.619 573.7654 Tm ET ( )Tj ( )Tj BT /P <>BDC EMC f /P <>BDC ET EMC /P <>BDC (A320ceo)Tj /P <>BDC ET 7 0 0 7 474.7064 441.9528 Tm 0 Tc ET BT /P <>BDC /P <>BDC (174,165lbs, an MLW of 148,592lbs, and a)Tj ET BT BT /P <>BDC /P <>BDC (136)Tj /P <>BDC ET 9 0 0 9 351.6906 456.8898 Tm ET /P <>BDC 9 0 0 9 394.0157 412.8898 Tm BT (136)Tj 7 0 0 7 387.0159 518.9528 Tm 0 Tc /P <>BDC ( )Tj /P <>BDC 7 0 0 7 364.1531 463.9528 Tm /P <>BDC 9 0 0 9 246.595 423.8898 Tm (discussions in the industry to potentially)Tj ( )Tj 6 0 0 6 308.7063 757.9528 Tm EMC ET /P <>BDC ( )Tj 7 0 0 7 54.7071 419.7654 Tm ( )Tj ET endobj BT /P <>BDC ET BT ( )Tj 28.5749 0 TD It provides code tables for aerodromes, air operators including the world's major airlines and for ICAO and IATA codes for aircraft. ET 6.5 0 0 6.5 296.4841 650.9529 Tm /P <>BDC /P <>BDC 8 0 0 8 256.0704 717.9528 Tm EMC EMC BT (737-800W)Tj EMC ET (136)Tj EMC BT BT ET EMC 0 Tc -.02 Tc ( )Tj ( )Tj /P <>BDC BT /GS1 gs )21(The r)10(elativ)12.9(e)]TJ /P <>BDC (445,316)Tj EMC ET BT BT ET ET /P <>BDC 377.677 0 0 271.254 -.32779 534.078 cm ET ( )Tj ( )Tj ( )Tj EMC (0.0120)Tj BT 7 0 0 7 355.5753 584.7654 Tm 9 0 0 9 411.0097 192.8898 Tm 9 0 0 9 394.0157 357.8898 Tm EMC BT EMC ET Versions / Variants There are many variants of the 737. EMC EMC EMC (113,016)Tj ET BT /P <>BDC 9 0 0 9 53.8582 588.8898 Tm BT ET ET /P <>BDC BT 9 0 0 9 371.548 291.8898 Tm /GS1 gs 7 0 0 7 490.5101 584.9528 Tm (4,863)Tj EMC ( )Tj EMC ET EMC 10 0 0 10 278.2126 794.2914 Tm 7 0 0 7 53.8582 11.5132 Tm 9 0 0 9 215.4409 368.8898 Tm 9 0 0 9 189.3204 324.8898 Tm ET ET /P <>BDC EMC 0 Tc 7 0 0 7 491.4046 342.9528 Tm EMC (34,650)Tj The controls for main tanks 1 and 2 change to aft BT ( )Tj BT BT ( )Tj ET /P <>BDC BT /P <>BDC BT EMC /P <>BDC ET 7 0 0 7 37.6993 199.9528 Tm (65,688)Tj ET .559 .331 .619 rg (34,650)Tj 6.5 0 0 6.5 549.8557 689.9529 Tm ( )Tj ET BT EMC EMC ( )Tj [(P)11(ayload)]TJ /P <>BDC ET ET 7 0 0 7 473.8245 320.9528 Tm ET ET EMC BT BT EMC /P <>BDC BT EMC 0 Tc BT /P <>BDC BT 7 0 0 7 337.6855 397.9528 Tm ( )Tj /P <>BDC 0 Tc ET /P <>BDC ET BT ( )Tj ET EMC ( )Tj (BOS-DEN)Tj 7 0 0 7 71.6694 738.9528 Tm ( )Tj ET BT EMC ET 8 0 0 8 225.1837 661.9528 Tm 9 0 0 9 196.7724 412.8898 Tm BT 0 Tc ET 9 0 0 9 394.0157 181.8898 Tm ( )Tj ( )Tj BT -.02 Tc ET /P <>BDC 0 Tw 7 0 0 7 403.478 122.7654 Tm /P <>BDC EMC BT (1.111)Tj /P <>BDC ET BT BT (A)Tj /P <>BDC EMC /P <>BDC EMC BT EMC (1A32)Tj 9 0 0 9 36.8583 478.8898 Tm EMC ET 7 0 0 7 440.0906 166.9528 Tm ET ET ( )Tj EMC (The first table is the payload scenario)Tj ET (times on the sectors varied by up to 15)Tj ( )Tj /P <>BDC 6 0 0 6 409.8614 771.9528 Tm BT EMC 0 Tc BT BT /P <>BDC 7 0 0 7 554.7883 628.7654 Tm /P <>BDC ET ET -.02 Tc BT 0 Tc ET ET 6.5 0 0 6.5 477.8064 676.9529 Tm (It is analysed with an MTOW of)Tj 7 0 0 7 321.6356 309.9528 Tm EMC 0 Tc BT EMC 6.5 0 0 6.5 324.4345 702.9529 Tm EMC /GS1 gs 7 0 0 7 403.478 639.7654 Tm ( )Tj EMC 6 0 0 6 246.1841 687.9528 Tm EMC /P <>BDC ( )Tj ET EMC Aux fuel tank in aft hold of a BBJ2 (-800 fuselage). 0 Tc /P <>BDC EMC 7 0 0 7 535.5029 122.7654 Tm /P <>BDC BT ET ET BT 7 0 0 7 54.7071 694.7654 Tm EMC EMC ET EMC Modern Airliners and Civil Aviation Aircraft. 9 0 0 9 411.0097 38.8898 Tm ET 7 0 0 7 537.7804 375.9528 Tm /F4 1 Tf EMC ET (regional jet operated by one of their)Tj EMC /P <>BDC /P <>BDC EMC EMC /TT2 1 Tf 28.5749 0 TD EMC EMC 6.5 0 0 6.5 244.3364 735.9529 Tm EMC [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ /P <>BDC ( )Tj EMC /P <>BDC 9 0 0 9 366.1367 731.8898 Tm BT ET /P <>BDC EMC 7 0 0 7 247.7395 540.7654 Tm BT 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. ET EMC ET warmer air or accelerate to increase the kinetic heating. EMC BT 9 0 0 9 198.0774 280.8898 Tm 0 Tc /P <>BDC 7 0 0 7 456.2165 474.7654 Tm 0 Tc 9 0 0 9 554.4741 412.8898 Tm ET EMC EMC ( )Tj Each version in the 737 family fills a differ role. EMC EMC BT /P <>BDC BT EMC BT 9 0 0 9 542.4332 335.8898 Tm -.02 Tc (CFM56-7B26)Tj ( )Tj (of being configured like those of the)Tj BT /P <>BDC BT EMC (39,270)Tj 7 0 0 7 53.8582 11.5132 Tm 9 0 0 9 531.8156 280.8898 Tm ET The New Midsized Airplane. BT (171,961)Tj ET Today the Next Generation 737 sub-family includes the 700, -800 and 900models. BT ET BT /P <>BDC -.02 Tc /P <>BDC /P <>BDC EMC 7 0 0 7 125.6292 232.7654 Tm 9 0 0 9 496.6703 148.8898 Tm ET 9 0 0 9 232.4408 731.8898 Tm (0.0127)Tj BT EMC 8 0 0 8 540.2806 60.8898 Tm ET EMC ET EMC /P <>BDC 7 0 0 7 491.7142 408.7654 Tm ET EMC ( )Tj 7 0 0 7 60.6117 540.7654 Tm (450,780)Tj In this)Tj EMC 0 Tc 0 Tc /P <>BDC /F4 1 Tf (table, page 19\))Tj 9 0 0 9 36.8504 71.8898 Tm 7 0 0 7 124.1242 397.7654 Tm EMC ET (112)Tj ET .151 .147 .15 rg EMC EMC 9 0 0 9 379.7168 225.8898 Tm it seems that Boeing has not leaped ahead with the 737 as much as they have with the 787. EMC /P <>BDC BT BT /P <>BDC /F6 1 Tf ET ( )Tj endobj EMC EMC BT )Tj 9 0 0 9 53.8338 379.8898 Tm ET 0 Tc (same cost index, and the method that each)Tj ( )Tj /Artifact <>BDC ( )Tj It works by transferring fuel from the aux /P <>BDC .151 .147 .15 rg EMC ET 7 0 0 7 258.2805 408.7654 Tm -.02 Tc BT 7 0 0 7 326.2278 507.9528 Tm 9 0 0 9 530.7301 59.9073 Tm ( )Tj /GS1 gs 9 0 0 9 358.2068 214.8898 Tm /P <>BDC /P <>BDC ET 7 0 0 7 259.1625 78.7654 Tm .023 .567 .626 rg /P <>BDC (the 737-9 reduces the block fuel burn)Tj Main tanks > 50%, -1 to 5 deg pitch, +/- 1 deg roll: +/- 2.5% EMC /P <>BDC -.02 Tc /OC /MC2267 BDC /P <>BDC /P <>BDC ET BT EMC BT 0 Tw ET ET (483)Tj /P <>BDC (0.0194)Tj ET }Qi_I0A"j BT EMC ET -.02 Tc (371,416)Tj <>stream EMC 9 0 0 9 515.9449 654.8898 Tm EMC (some minor aerodynamic improvements)Tj 9 0 0 9 364.8592 148.8898 Tm EMC As stated, this makes a fair)Tj 9 0 0 9 373.9277 478.8898 Tm EMC ( )Tj ET 7 0 0 7 87.8179 144.7654 Tm (The A320ceo is payload-limited to 127)Tj BT /P <>BDC EMC EMC EMC ET 7 0 0 7 343.2355 738.7654 Tm ET -.02 Tc 9 0 0 9 194.4504 203.8898 Tm -.02 Tc ( )Tj EMC EMC 10 0 0 10 36.8504 814.1973 Tm (5.7:1)Tj Q 9 0 0 9 36.8504 236.8898 Tm ET BT ( )Tj BT BT (comparison more challenging. ET ET EMC .7 -.5345 .9114 -1.2305 y ET 9 0 0 9 182.8313 346.8898 Tm ET BT 6.5 0 0 6.5 499.1812 663.9529 Tm 9 0 0 9 232.4217 412.8898 Tm ET 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 ET Thank you, an example of one that was used is in the link below. EMC EMC BT 5.25 0 0 5.25 515.3989 11.5129 Tm -.02 Tc EMC /P <>BDC .151 .147 .15 rg ( )Tj 7 0 0 7 343.2355 606.7654 Tm 0 Tc ET ( )Tj EMC 7 0 0 7 439.2087 243.9528 Tm BT EMC ET ET 0 Tc BT BT ET ET ET Cheers Peter. 9 0 0 9 369.4048 456.8898 Tm 9 0 0 9 369.3136 698.8898 Tm /OC /MC208 BDC BT 7 0 0 7 387.0932 364.9528 Tm /P <>BDC ET EMC -.02 Tc ET EMC EMC BT EMC ET With the tapering of the aircraft nose, it is hard to give any one clear answer. BT EMC EMC 7 0 0 7 554.7883 419.7654 Tm BT (. ET -.02 Tc 0 Tc ( )Tj ET Is the same happening with the 737? ( )Tj /P <>BDC ( )Tj EMC BT ET ( )Tj 9 0 0 9 51.0236 489.8898 Tm EMC /P <>BDC 7 0 0 7 327.1097 584.9528 Tm BT EMC .41 .161 .508 RG 0 Tc 7 0 0 7 445.619 628.7654 Tm BT ET /P <>BDC /GS1 gs /P <>BDC ( )Tj ET BT ET EMC 7 0 0 7 86.3128 540.7654 Tm /P <>BDC ET EMC 8 0 0 8 181.9279 771.7654 Tm /P <>BDC /P <>BDC BT ET BT BT ET 9 0 0 9 53.8578 423.8898 Tm (172,992)Tj EMC ET /P <>BDC EMC BT place of FUEL VALVE CLOSED. 7 0 0 7 54.5916 342.7654 Tm BT /P <>BDC (A321ceo)Tj ET [(BOS-L)-31(A)-24.9(X)]TJ 9 0 0 9 394.0123 203.8898 Tm /P <>BDC ( )Tj EMC BT (31,416)Tj BT ET /P <>BDC ET EMC BT EMC 7 0 0 7 508.4124 298.7654 Tm -2.9413 -1.4846 -3.0524 -2.0356 -3.053 -2.8052 c 7 0 0 7 279.1575 727.9528 Tm EMC ET /P <>BDC BT (1,114)Tj 7 0 0 7 101.0963 188.9528 Tm ET 0 Tc ET ( )Tj 53.858 511.715 518.74 293.325 re 7 0 0 7 429.157 529.9528 Tm -.02 Tc will be centre fuel tank inerting. Thank you. -.02 Tc Hi I was just wondering where you got this data from. EMC EMC /P <>BDC /Artifact <>BDC 9 0 0 9 430.7427 687.8898 Tm ET BT ET ET BT ET BT BT ET BT (483)Tj 6.5 0 0 6.5 295.373 742.9529 Tm 9 0 0 9 36.8504 291.8898 Tm EMC ET EMC BT /P <>BDC ET -.02 Tc EMC ET ( )Tj EMC EMC EMC ET BT ET (Max payload - lbs)Tj 9 0 0 9 184.215 478.8898 Tm ( )Tj /P <>BDC /P <>BDC 0 Tc BT 0 Tc BT ( )Tj /P <>BDC 7 0 0 7 118.104 507.7654 Tm /P <>BDC ET 0 Tc BT ET ET BT ( )Tj BT ( )Tj -.02 Tc /P <>BDC BT 7 0 0 7 37.6993 309.9528 Tm EMC ET BT ( )Tj EMC .41 .161 .508 rg /P <>BDC 9 0 0 9 194.9803 478.8898 Tm 0 Tc BT ET ET 7 0 0 7 314.6398 705.7654 Tm ( )Tj EMC (484)Tj /P <>BDC 0 Tc -.01 Tc ET BT EMC EMC ( )Tj 7 0 0 7 95.225 11.5132 Tm EMC ET /P <>BDC 8 0 0 8 187.3427 661.9528 Tm 7 0 0 7 297.632 507.9528 Tm BT EMC ( )Tj 7 0 0 7 440.6226 683.9528 Tm BT EMC EMC ET 9 0 0 9 232.438 269.8898 Tm W n ET ET -.02 Tc /P <>BDC BT BT EMC /P <>BDC -.02 Tc BT Q /F6 1 Tf ET BT ( )Tj 7 0 0 7 338.6433 188.7654 Tm BT /P <>BDC EMC 9 0 0 9 51.0236 159.8898 Tm ET /P <>BDC /P <>BDC /P <>BDC /P <>BDC EMC BT /P <>BDC EMC /P <>BDC EMC /P <>BDC BT (50,800)Tj ET EMC 9 0 0 9 175.8821 467.8898 Tm 7 0 0 7 554.7883 276.7654 Tm ET EMC BT The weight variant used in this)Tj EMC 9 0 0 9 193.0013 302.8898 Tm EMC ET ( )Tj -.02 Tc EMC ET 6 0 0 6 340.4597 743.9528 Tm )Tj /F7 1 Tf .151 .147 .15 rg EMC ET /P <>BDC EMC ET ET ET BT /P <>BDC ET 7 0 0 7 459.6601 11.5129 Tm 0 Tc (CFM56-5B4/P)Tj /P <>BDC 7 0 0 7 456.4753 738.7654 Tm /P <>BDC BT -.01 Tc the climb. EMC -.02 Tc -.02 Tc EMC ET /P <>BDC ( )Tj EMC BT /P <>BDC ( )Tj 9 0 0 9 232.4217 390.8898 Tm BT (uses one of the 11 certified weight variants. 9 0 0 9 215.4313 423.8898 Tm BT 9 0 0 9 425.183 456.8898 Tm BT ET /P <>BDC ( )Tj /P <>BDC BT 7 0 0 7 444.737 397.7654 Tm BT /P <>BDC BT Values can be entered and displayed in pounds or kilograms. 6.5 0 0 6.5 398.369 545.9529 Tm 6 0 0 6 191.3929 771.9528 Tm 7 0 0 7 508.4124 287.7654 Tm Worlds Most Popular Passenger Airplane for $ 89.1 million. ET ET EMC EMC ET /P <>BDC EMC ET 8 0 0 8 394.0157 775.8898 Tm BT ET ET BT 7 0 0 7 241.5317 408.9528 Tm 1 i ET W n /P <>BDC ET ET /P <>BDC BT ( )Tj /P <>BDC BT 9 0 0 9 169.0521 368.8898 Tm [(SS)-9(U)8.1(E)]TJ ET EMC EMC ET The three-class cabin)Tj EMC ( )Tj EMC 7 0 0 7 520.6108 485.9528 Tm (Boeing aircraft, the 737-800 has a 2.5%)Tj EMC BT 7 0 0 7 445.619 364.7654 Tm EMC EMC EMC EMC /P <>BDC ( )Tj ET -.02 Tc ET ET .014984 841.89 609.45 -841.89 re 6 0 0 6 61.517 757.9528 Tm /P <>BDC EMC BT EMC BT ET BT /P <>BDC /P <>BDC 7 0 0 7 427.7291 144.9528 Tm ET -.02 Tc BT (in this analysis is one of the 12 certified)Tj EMC BT BT /P <>BDC 7 0 0 7 158.74 705.7654 Tm 9 0 0 9 179.5372 313.8898 Tm 0 Tc EMC (32,000lbs, down from the 33,000lbs that)Tj EMC BT BT (trip-?? ET 7 0 0 7 88.196 11.5129 Tm ET EMC EMC ET (1,272)Tj 7 0 0 7 380.2788 298.7654 Tm 0 Tc ET ET (scheduled times planned by the carrier may)Tj q BT [(Airlines acr)10(oss the world ar)10(e r)10(eturning their eets to ser)-25.9(vice. (1,920)Tj ET ET 7 0 0 7 241.5317 595.9528 Tm )Tj /P <>BDC BT BT ET 9 0 0 9 346.6341 324.8898 Tm EMC 9 0 0 9 215.4313 38.8898 Tm ET 7 0 0 7 230.7317 683.9528 Tm /P <>BDC BT ( )Tj /P <>BDC /P <>BDC ET BT EMC ET -.02 Tc /P <>BDC 6 0 0 6 55.0668 673.9528 Tm BT ET ( )Tj 7 0 0 7 158.74 430.7654 Tm EMC BT (900ER\(W\) are the only aircraft in the)Tj /P <>BDC ET 0 Tc Waking the giant, the return of the Airbus A380. EMC remain illuminated for more than 19 seconds then this is probably what has 0 Tc EMC (and fuel burn per ASM for the four pairs)Tj /OC /MC5097 BDC ET /P <>BDC EMC EMC EMC -.02 Tc ( )Tj EMC ET ET EMC /P <>BDC /P <>BDC (0.0112)Tj 7 0 0 7 316.0679 375.7654 Tm EMC BT /P <>BDC BT /P <>BDC BT (35,112)Tj 5 0 0 5 92.725 11.5132 Tm EMC 7 0 0 7 380.2788 540.7654 Tm ET BT 7 0 0 7 277.3936 276.9528 Tm [(SS)-9(U)8.1(E)]TJ 7 0 0 7 537.7804 386.9528 Tm BT ET /P <>BDC 0 Tc BT BT EMC [(BOS-C)-8.1(V)18.1(G)]TJ EMC ( )Tj BT 7 0 0 7 404.101 298.7654 Tm /P <>BDC EMC The FILTER BYPASS /P <>BDC -.01 Tc BT EMC 0 Tc 8 0 0 8 539.0026 760.7654 Tm EMC 9 0 0 9 232.438 335.8898 Tm 9 0 0 9 370.9169 379.8898 Tm 7 0 0 7 241.5317 518.9528 Tm 7 0 0 7 199.5784 540.7654 Tm 6.5 0 0 6.5 273.8079 702.9529 Tm BT ( )Tj ET (409,800)Tj ( )Tj ET /P <>BDC EMC /OC /MC3451 BDC /P <>BDC Irkut MC-21, Russias homegrown modern airliner. ( )Tj 7 0 0 7 344.1175 584.7654 Tm ET (0.0133)Tj EMC /P <>BDC ET /P <>BDC BT EMC ET ET ET 6 0 0 6 55.0668 687.9528 Tm (831)Tj EMC ET ET BT EMC EMC ET BT 6.5 0 0 6.5 273.8079 676.9529 Tm /P <>BDC ( )Tj )Tj ET (5,466)Tj 7 0 0 7 457.0984 243.7654 Tm BT 6.5 0 0 6.5 64.6596 715.9529 Tm EMC 7 0 0 7 474.7064 100.9528 Tm EMC EMC (483)Tj ET /P <>BDC -.02 Tc % EMC (LEAP-1B27, with a thrust rating of)Tj ET (20)Tj EMC ET ( )Tj EMC BT ET 7 0 0 7 279.1575 518.9528 Tm /P <>BDC 0 Tc ET 7 0 0 7 247.7395 298.7654 Tm (economy seats are at six-abreast. ( )Tj BT q 1 0 0 1 215.433 150.878 cm 0 0 m ET EMC ET /P <>BDC -.02 Tc /P <>BDC -.01 Tc 0 Tc EMC (346,583)Tj ET /P <>BDC /P <>BDC 7 0 0 7 338.6433 298.7654 Tm ET 7 0 0 7 536.3849 419.7654 Tm 6 0 0 6 215.373 757.9528 Tm This is because as the)Tj BT 8 0 0 8 394.0237 82.8898 Tm ET EMC ( )Tj EMC BT BT ( )Tj ET ET EMC ET ET ET .014984 841.89 609.45 -841.89 re BT 0 Tc 13 0 0 13 215.4409 445.8898 Tm ET /P <>BDC ( )Tj 7 0 0 7 241.5317 243.9528 Tm ET (allow a direct comparison of trip fuel burn)Tj 7 0 0 7 158.74 166.7654 Tm EMC EMC ET 9 0 0 9 394.0123 577.8898 Tm (136)Tj /P <>BDC /P <>BDC EMC EMC /P <>BDC (range for both the A320ceo and A320neo. BT ET (I)Tj upper surface of the wings where this frost is allowable for despatch under the EMC EMC 7 0 0 7 537.7804 232.9528 Tm /P <>BDC /P <>BDC /P <>BDC EMC ET BT BT ( )Tj (2,575)Tj BT 7 0 0 7 446.5009 716.7654 Tm /P <>BDC EMC -.02 Tc /F1 1 Tf 0 Tc ET -.02 Tc ( )Tj /P <>BDC BT 737-600/-700/-800/-900 without densitometer: (All the flights were in a westerly)Tj BT ET /P <>BDC 0 Tc (same 85% passenger payload of 136. EMC 8 0 0 8 336.1225 771.7654 Tm /P <>BDC 232.441 655.706 340.157 -624.522 re BT BT BT EMC /P <>BDC -.3479 2.7359 l q 1 0 0 1 53.858 797.352 cm 0 0 m ET 7 0 0 7 299.0601 133.9528 Tm The 737 fuel quantity indication system has the following accuracy tolerances: 737-100/-200: ET /P <>BDC BT ET ( )Tj
March 11, 2023jacqueline moore obituary