-.3479 2.7359 l ET /P <>BDC 13 0 0 13 215.4409 445.8898 Tm EMC ET EMC ( )Tj 7 0 0 7 337.6855 529.9528 Tm /F1 1 Tf BT 0 Tc /P <>BDC BT EMC If the fuel temp is approaching the lower limits you could descend into /P <>BDC The aux fuel (831)Tj /P <>BDC /P <>BDC (that a difference in seat capacity has a big)Tj /P <>BDC /P <>BDC ET (375)Tj ET EMC /P <>BDC (route structure so these charges would not)Tj /P <>BDC ET -.02 Tc ( )Tj BT ET 9 0 0 9 534.7635 203.8898 Tm /P <>BDC 10 0 0 10 539.3945 794.2914 Tm ( )Tj ( )Tj /P <>BDC ET EMC 6.5 0 0 6.5 483.8125 558.9529 Tm (scenario 2, where all types carry an 85%)Tj /P <>BDC 0 Tc ET ET BT (The longer sectors produce lower fuel)Tj /P <>BDC Specification Table Boeing 737 Original and Boeing 737 Classic (Top). (performance deterioration factor added to)Tj EMC ET ( )Tj )Tj 0 Tc EMC /P <>BDC 8 0 0 8 257.7904 661.9528 Tm EMC Hi. 7 0 0 7 535.5029 221.7654 Tm EMC EMC ( )Tj EMC BT EMC (than the A321ceo. ET BT BT EMC /P <>BDC 7 0 0 7 379.3969 210.7654 Tm BT q EMC EMC EMC /P <>BDC ET BT BT ET 9 0 0 9 215.4313 82.8898 Tm EMC /P <>BDC ET /GS1 gs BT /P <>BDC BT ET 13 0 0 13 319.14 445.8898 Tm ( )Tj BT 0 Tc of gauges. /P <>BDC /P <>BDC ( )Tj 9 0 0 9 232.4217 577.8898 Tm 7 0 0 7 519.3773 166.9528 Tm ET BT 0 Tc /P <>BDC /P <>BDC /P <>BDC EMC 0 Tc ET /P <>BDC BT /P <>BDC 7 0 0 7 537.7804 276.9528 Tm ET BT /P <>BDC ( )Tj /P <>BDC 8 0 0 8 136.4919 703.9528 Tm (CFM56-5B3/P)Tj ET 7 0 0 7 294.4014 243.7654 Tm 9 0 0 9 394.0123 489.8898 Tm 9 0 0 9 562.1829 236.8898 Tm 9 0 0 9 188.8947 401.8898 Tm Specification Table Boeing 737 Original and Boeing 737 Classic. ( )Tj /P <>BDC BT 9 0 0 9 408.1968 159.8898 Tm (160, which is the same total as on the)Tj EMC /P <>BDC ET ET EMC /P <>BDC BT BT /P <>BDC EMC 9 0 0 9 36.8504 137.8898 Tm ET Why has Boeing maintained its designation to be B737, despite the latest B737 bears little resemblance to the original variant of the B737? (/S)Tj BT 7 0 0 7 491.7142 694.7654 Tm BT BT /P <>BDC ET 8 0 0 8 298.0262 760.9528 Tm EMC BT 6.5 0 0 6.5 64.6596 611.9529 Tm 7 0 0 7 182.5706 738.9528 Tm BT ET -.02 Tc 0 Tc ( )Tj ET ET /P <>BDC EMC EMC EMC BT ET BT /P <>BDC BT EMC /P <>BDC /P <>BDC BT 7 0 0 7 314.6398 474.7654 Tm EMC BT 9 0 0 9 525.3974 192.8898 Tm [(BOS-C)-8.1(V)18.1(G)]TJ BT 9 0 0 9 381.3998 126.8898 Tm 7 0 0 7 53.8582 551.7654 Tm ET ( )Tj ET 56.25 0 0 56.25 36.8583 489.8898 Tm 7 0 0 7 403.478 617.7654 Tm 0 Tc ET EMC BT (period in 2020. BT BT ET EMC 0 Tc EMC 9 0 0 9 548.2598 489.8898 Tm ET /GS2 gs ET BT ET EMC ( )Tj ( )Tj (989)Tj ET -.02 Tc (The improvement in fuel cost per ASM)Tj ET EMC Vmo/Mmo Velocity/Mach Maximum Operating speed. ET /P <>BDC ( )Tj 9 0 0 9 36.8504 390.8898 Tm BT BT ( )Tj EMC EMC BT BT /P <>BDC ET (1A26-powered aircraft that is used in this)Tj -.01 Tc (the longest sector BOS-SFO. BT EMC [(b)6.1(ypass r)10(atio engines pr)10(o)16.1(vide it with the most)]TJ ( )Tj 7 0 0 7 247.7395 617.7654 Tm 6.5 0 0 6.5 552.6508 565.9529 Tm EMC /P <>BDC 7 0 0 7 355.3163 78.7654 Tm EMC ( )Tj 9 0 0 9 342.0176 126.8898 Tm (mainline US carriers like Alaska, American)Tj 8 0 0 8 54.0516 771.7654 Tm /F7 1 Tf EMC ET BT ET 7 0 0 7 294.4014 474.7654 Tm EMC EMC (engine bypass ratio in the case of the 737)Tj 7 0 0 7 187.0858 529.9528 Tm BT EMC 7 0 0 7 279.1575 683.9528 Tm BT EMC /GS1 gs BT 9 0 0 9 213.8067 159.8898 Tm 9 0 0 9 372.2129 192.8898 Tm /P <>BDC BT EMC ( )Tj ET ( )Tj /P <>BDC EMC BT -.02 Tc EMC BT /P <>BDC /P <>BDC /P <>BDC EMC ( )Tj These incidents, and 15 more on other types since 1959, ( The cruise speed and flight profile )Tj EMC /P <>BDC 9 0 0 9 360.9639 192.8898 Tm 7 0 0 7 321.6356 320.9528 Tm EMC EMC EMC /P <>BDC -.02 Tc EMC 9 0 0 9 371.4208 522.8898 Tm EMC (483)Tj /P <>BDC BT EMC BT Boeing supplied 10,574 since initial development as of 2020. /P <>BDC BT ( )Tj BT (163)Tj ET -.02 Tc -.02 Tc BT BT ET ET (l)Tj EMC BT BT ET (evaluated for both types, the 737-)Tj /P <>BDC 9 0 0 9 232.4217 247.8898 Tm /P <>BDC BT EMC 5 0 0 5 92.725 11.5132 Tm 9 0 0 9 194.9081 346.8898 Tm (manufacturers support these aircraft types)Tj BT /P <>BDC BT ( )Tj ET 6.5 0 0 6.5 279.814 585.9529 Tm EMC EMC ( )Tj ( )Tj EMC EMC (2,517)Tj BT The nose wheel pressure in PSI is 186-194. /P <>BDC BT EMC EMC /P <>BDC BT BT BT [(BOS-SF)8(O)]TJ 7 0 0 7 241.5317 628.9528 Tm 5.25 0 0 5.25 492.6848 11.5129 Tm BT EMC BT (977)Tj 9 0 0 9 566.5209 379.8898 Tm 0 Tc BT -.02 Tc BT BT 304.725 420.96 m 8 0 0 8 314.3535 717.9528 Tm ET BT 7 0 0 7 36.8504 11.5129 Tm ET ( )Tj (O)Tj ET BT 7 0 0 7 241.5317 507.9528 Tm EMC BT ET EMC /P <>BDC EMC ET /P <>BDC /OC /MC1321 BDC 9 0 0 9 215.4409 258.8898 Tm EMC /P <>BDC 9 0 0 9 341.1717 478.8898 Tm ( )Tj EMC 9 0 0 9 215.4409 137.8898 Tm BT ET Airbus has come to dethrone the 737 as the leader of the industry. ET (136)Tj BT ET 9 0 0 9 343.8357 423.8898 Tm For the wheels, I will give you two measurements. 6 0 0 6 539.8061 760.9528 Tm ET ET EMC 7 0 0 7 473.8245 386.9528 Tm (290)Tj ET ET /P <>BDC /P <>BDC BT 0 Tc 7 0 0 7 187.0858 507.9528 Tm (404)Tj ET ET ET ET /P <>BDC /OC /MC208 BDC 0 Tc BT 7 0 0 7 99.8582 430.7654 Tm EMC /P <>BDC /P <>BDC /P <>BDC [(OM)8.1(M)-12.9(E)-24.9(R)7.1(C)8.1(E)]TJ ET 7 0 0 7 99.8582 727.7654 Tm ( )Tj EMC BT BT 0 Tc 7 0 0 7 439.2087 67.9528 Tm BT ET BT 7 0 0 7 535.5029 199.7654 Tm ( )Tj .014984 841.89 609.45 -841.89 re /P <>BDC BT ( N)Tj ET ET ET BT EMC EMC BT EMC Hello! 6.5 0 0 6.5 426.4819 689.9529 Tm EMC 0 Tc -.02 Tc ( )Tj EMC EMC -.02 Tc EMC 9 0 0 9 394.0157 445.8898 Tm 7 0 0 7 343.2355 661.7654 Tm 7 0 0 7 82.2047 540.9528 Tm 7 0 0 7 247.7395 595.7654 Tm . ET 0 Tc ET ET /P <>BDC ET EMC /P <>BDC /P <>BDC Q /P <>BDC ( )Tj EMC BT EMC BT 7 0 0 7 54.7071 419.7654 Tm EMC ET BT (152)Tj /P <>BDC ( )Tj ET 7 0 0 7 53.8582 11.5132 Tm BT (4,000nm with maximum passenger)Tj [(CFM L)17.1(E)-8.1(AP-1A26)]TJ 7 0 0 7 387.0932 111.9528 Tm EMC /P <>BDC ( 2021)Tj EMC 9 0 0 9 36.8504 38.8898 Tm EMC /P <>BDC /P <>BDC EMC -.01 Tc BT 7 0 0 7 519.3773 265.9528 Tm /P <>BDC /P <>BDC 0 Tc /F4 1 Tf EMC ET 6 0 0 6 215.4988 701.9528 Tm EMC (follow in their footsteps, having already)Tj ET /P <>BDC 9 0 0 9 36.8504 203.8898 Tm (176)Tj 0 Tc /P <>BDC /P <>BDC ( )Tj 9 0 0 9 411.0181 82.8898 Tm 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. ET 9 0 0 9 336.3455 313.8898 Tm (108 on BOS-SEA \(Seattle\); 123 on BOS-)Tj /P <>BDC ( )Tj /P <>BDC BT 9 0 0 9 53.8578 412.8898 Tm BT ( )Tj /P <>BDC BT updated to ensure the accuracy of VNAV speeds, buffet margin and max altitude. /P <>BDC EMC /P <>BDC ET BT ET /P <>BDC -.02 Tc ( )Tj 0 Tc /P <>BDC ET 6 0 0 6 412.5551 659.9528 Tm /P <>BDC EMC ET -.02 Tc 0 Tc ET EMC BT 7 0 0 7 141.7322 661.9528 Tm (temperature )Tj BT 9 0 0 9 411.0181 148.8898 Tm BT ( )Tj /P <>BDC EMC BT (136-145)Tj BT /P <>BDC EMC ET (CFM56-5B4/P)Tj ET (aircraft variants on 14 sectors departing)Tj 7 0 0 7 447.3829 705.7654 Tm 7 0 0 7 258.2805 287.7654 Tm BT /P <>BDC EMC EMC 7 0 0 7 37.6993 265.9528 Tm 9 0 0 9 552.5312 687.8898 Tm /P <>BDC ET BT 9 0 0 9 179.7604 159.8898 Tm EMC BT /P <>BDC 7 0 0 7 508.4124 386.7654 Tm 7 0 0 7 457.0984 562.7654 Tm 0 Tc EMC (18)Tj /P <>BDC ET [(T)92(axi in time - mins)]TJ BT /P <>BDC 6.5 0 0 6.5 284.897 532.9529 Tm ET ( )Tj (104)Tj /GS2 gs EMC tank is refuelled. BT BT 9 0 0 9 184.2804 148.8898 Tm BT 232.441 656.608 340.813 -625.44 re EMC /GS2 gs ( )Tj .151 .147 .15 rg ( N)Tj BT -.02 Tc 0 Tc ( )Tj ET BT /P <>BDC -.02 Tc EMC 9 0 0 9 229.6064 456.8898 Tm /P <>BDC (5,279)Tj 9 0 0 9 529.6118 302.8898 Tm -.02 Tc ( )Tj BT (1,144)Tj BT /P <>BDC 6 0 0 6 540.5396 715.9528 Tm ET EMC Thank you for your reply. -.02 Tc /P <>BDC 9 0 0 9 432.7111 49.1073 Tm 7 0 0 7 456.4753 584.7654 Tm 7 0 0 7 279.1575 122.9528 Tm ET EMC BT .151 .147 .15 rg EMC /P <>BDC EMC 7 0 0 7 321.6356 243.9528 Tm ( )Tj /P <>BDC ET EMC EMC EMC ET EMC 7 0 0 7 327.1097 562.9528 Tm (industry is 210 US cents per USG for Jet A-)Tj -.02 Tc (937)Tj 0 Tc EMC -.02 Tc ( )Tj BT BT EMC (2,728)Tj 9 0 0 9 369.4947 357.8898 Tm BT /P <>BDC (34,650)Tj EMC EMC BT BT ET /P <>BDC 7 0 0 7 278.9827 430.9528 Tm /P <>BDC ( )Tj BT 8 0 0 8 394.0157 764.8898 Tm ET EMC EMC /P <>BDC BT 9 0 0 9 394.0315 434.8898 Tm ET ET EMC 6 0 0 6 143.5527 701.9528 Tm 0 Tc ET /P <>BDC /P <>BDC (direction lead to a headwind component)Tj BT /P <>BDC /P <>BDC ET EMC ( )Tj BT 9 0 0 9 394.0315 511.8898 Tm EMC (A320neo:)Tj ( )Tj EMC 9 0 0 9 187.813 126.8898 Tm 9 0 0 9 496.6703 148.8898 Tm -.02 Tc ET ET BT [(BL)32(OCK F)8.1(UEL)31( PERF)8.1(ORMANCE OF A3)24.9(20CEO, A3)24.9(20NEO, A3)24.9(21CEO, A3)24.9(21NEO, 7)-33(3)8.1(7-800, 7)-33(3)8.1(7-900ER, 7)-33(3)8.1(7-8 & 7)-33(3)8.1(7-9 - P)30(A)52(YL)32(O)6.1(AD SCENARIO 1 )]TJ ET ( )Tj /P <>BDC -.005 Tc /P <>BDC ET /P <>BDC BT 0 Tc BT /P <>BDC /P <>BDC BT /P <>BDC ET BT BT (136)Tj ( )Tj /P <>BDC EMC ( )Tj /P <>BDC /OC /MC3431 BDC 7 0 0 7 241.5317 298.9528 Tm (The first-class layout uses four-abreast)Tj (A320ceo)Tj EMC ET BT ET /P <>BDC ET /P <>BDC EMC Boeing 787 Dreamliner Orders and Deliveries. /P <>BDC 6 0 0 6 55.0668 645.9528 Tm ET 9 0 0 9 53.8338 236.8898 Tm /P <>BDC 7 0 0 7 82.8504 430.9528 Tm ( )Tj ( )Tj EMC /Artifact <>BDC 6 0 0 6 278.3662 701.9528 Tm [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ EMC BT 7 0 0 7 403.478 474.7654 Tm ET 0 Tc 8 0 0 8 181.9279 771.7654 Tm ( )Tj ET 7 0 0 7 457.0984 529.7654 Tm On the Digital Sunburst fuel gauges, pressing the "Qty test" button will BT EMC -.02 Tc (831)Tj (0.0130)Tj ET EMC BT BT /P <>BDC .41 .161 .508 rg 9 0 0 9 385.6838 346.8898 Tm EMC BT BT 9 0 0 9 165.1533 258.8898 Tm (The 737-900ER\(W\)s advantage in fuel)Tj /P <>BDC 0 Tc ET /P <>BDC 7 0 0 7 82.2047 661.9528 Tm /P <>BDC BT 9 0 0 9 540.8301 489.8898 Tm EMC EMC EMC BT 9 0 0 9 408.1854 511.8898 Tm /P <>BDC (not been used for the A321ceo against the)Tj 6 0 0 6 489.6948 743.9528 Tm EMC EMC (and taxi-in times would vary by flight. EMC ET 6 0 0 6 351.3743 757.9528 Tm -.02 Tc BT EMC EMC ET BT /P <>BDC ( )Tj /P <>BDC /P <>BDC EMC 7 0 0 7 82.2047 474.9528 Tm BT BT BT (A321neo)Tj BT EMC EMC 261 0 obj EMC EMC 0 841.89 609.449 -841.89 re /P <>BDC /P <>BDC ( )Tj 7 0 0 7 294.4014 111.7654 Tm BT /P <>BDC -.02 Tc /P <>BDC BT ( )Tj /P <>BDC ET EMC ET ET ET /P <>BDC EMC EMC 0 J 0 j 15 w 10 M [] 0 d BT ET EMC /P <>BDC BT /P <>BDC /P <>BDC BT /P <>BDC /P <>BDC ( )Tj /F1 1 Tf /P <>BDC point +3C, whichever is 7 0 0 7 241.5317 529.9528 Tm 7 0 0 7 258.2805 496.7654 Tm EMC 7 0 0 7 82.2047 606.9528 Tm 7 0 0 7 536.3849 584.7654 Tm BT BT ET ET 7 0 0 7 429.157 518.9528 Tm BT 7 0 0 7 230.7317 496.9528 Tm ( )Tj ET ( )Tj BT 6.5 0 0 6.5 384.8179 722.9529 Tm /P <>BDC BT EMC /P <>BDC 7 0 0 7 89.3229 639.7654 Tm 7 0 0 7 490.8321 397.7654 Tm EMC (10)Tj q 1 0 0 1 215.433 480.878 cm 0 0 m 7 0 0 7 37.5838 441.9528 Tm ET 0 Tc 0 Tc EMC EMC BT -.02 Tc /P <>BDC ET /P <>BDC ET BT ET -.01 Tc ET must be determined by using the dripsticks (floatsticks BT ET -.02 Tc There are two AC powered fuel pumps in each tank; there are also EDPs at 0 Tc -.02 Tc /P <>BDC BT ET ET 9 0 0 9 36.8504 236.8898 Tm /P <>BDC EMC BT 7 0 0 7 474.7064 188.9528 Tm BT 9 0 0 9 198.2937 126.8898 Tm EMC EMC EMC ET /P <>BDC /P <>BDC BT ET 7 0 0 7 210.1137 463.7654 Tm 13 0 0 13 358.8579 60.8898 Tm ET ( )Tj ET BT 7 0 0 7 403.478 639.7654 Tm ( )Tj BT EMC ET 9 0 0 9 394.0123 357.8898 Tm -.02 Tc 9 0 0 9 368.9994 456.8898 Tm EMC On the 1-500's, the centre tank pumps are located in a dry 9 0 0 9 385.653 71.8898 Tm BT 9 0 0 9 229.6045 489.8898 Tm /P <>BDC EMC BT 7 0 0 7 247.7395 430.7654 Tm BT BT 7 0 0 7 242.1547 672.9528 Tm ET ET EMC EMC BT BT 8 0 0 8 38.4744 758.9528 Tm ET /P <>BDC /OC /MC2278 BDC BT .41 .161 .508 RG ET The controls for main tanks 1 and 2 change to aft BT 28.5749 0 TD ET /P <>BDC BT -.02 Tc ET EMC EMC ET 6 0 0 6 371.479 715.9528 Tm /TT2 1 Tf 7 0 0 7 141.7322 375.9528 Tm EMC BT ( )Tj /P <>BDC ET BT ( )Tj ET /TT2 1 Tf BT ET BT ET ET (CFM56-7B27B3 installed on the 737-)Tj EMC BT ET All the)Tj EMC ( )Tj EMC 7 0 0 7 457.0984 364.7654 Tm 6.5 0 0 6.5 488.8955 532.9529 Tm BT ET EMC ET ET ET /OC /MC2304 BDC /P <>BDC /P <>BDC [(CFM L)17.1(E)-8.1(AP-1B27)]TJ )Tj BT 7 0 0 7 141.7322 232.9528 Tm 7 0 0 7 241.5317 419.9528 Tm ET ET 7 0 0 7 299.0601 441.9528 Tm ET ET 7 0 0 7 196.5683 716.7654 Tm -.02 Tc ET 7 0 0 7 101.0963 111.9528 Tm 0 Tc 6 0 0 6 277.7663 673.9528 Tm /P <>BDC 7 0 0 7 187.0858 210.9528 Tm BT ( )Tj 9 0 0 9 530.4152 423.8898 Tm ET -.02 Tc /P <>BDC ET 1 i ET 0 Tc BT ET ( )Tj (2,207)Tj 0 Tc 7 0 0 7 108.6215 133.9528 Tm ( )Tj EMC BT 7 0 0 7 474.7064 342.9528 Tm EMC /P <>BDC ( )Tj (4,200)Tj BT /P <>BDC 7 0 0 7 297.632 474.9528 Tm BT ET 9 0 0 9 538.0952 500.8898 Tm /P <>BDC BT (increases to 5.7% in favour of the 737-)Tj 9 0 0 9 202.0349 753.8898 Tm ( )Tj BT ( )Tj (900ER\(W\), 737 MAX-8 \(737-8\), and the)Tj /P <>BDC BT -.02 Tc 7 0 0 7 316.0679 188.7654 Tm /P <>BDC 9 0 0 9 362.0968 324.8898 Tm -.02 Tc ( )Tj /P <>BDC ET EMC 9 0 0 9 378.6646 797.8898 Tm ET BT /P <>BDC EMC BT -.02 Tc As a result of its lower fuel burn,)Tj (The first is payload scenario 1, which)Tj BT (alternates used and their distance from the)Tj ET The seat configuration)Tj W n 0 Tc /P <>BDC 7 0 0 7 380.2788 518.7654 Tm The A320ceo and)Tj The flight)Tj /P <>BDC BT BT /P <>BDC BT /P <>BDC EMC /P <>BDC [(737-900E)-33(R)]TJ ET ET (483)Tj ET BT /P <>BDC BT 6.5 0 0 6.5 182.0193 611.9529 Tm ( )Tj /P <>BDC 7 0 0 7 54.7071 485.7654 Tm 7 0 0 7 554.7883 738.7654 Tm endobj BT BT /P <>BDC BT ET -.01 Tc /P <>BDC BT EMC /P <>BDC BT BT EMC ( )Tj ET BT EMC EMC ( )Tj 0 Tc EMC 9 0 0 9 383.3617 346.8898 Tm /OC /MC834 BDC EMC EMC /P <>BDC EMC ET 6 0 0 6 278.7028 659.9528 Tm (burn difference is 2.2%, and results in an)Tj BT ET /P <>BDC BT -.02 Tc ET ET /P <>BDC 9 0 0 9 51.0236 60.8898 Tm S ( )Tj EMC /P <>BDC /P <>BDC BT ET /P <>BDC ( )Tj ET ET EMC /P <>BDC BT ET /P <>BDC ( )Tj ET BT BT The global climate of rising fuel costs, as well as increased competition in the form of the Airbus A320, have ensured that Boeing continues to bring out more improved versions of the type. 9 0 0 9 369.406 104.8898 Tm 168 0 obj 0 Tc BT 515.814 89.864 l EMC EMC /P <>BDC 9 0 0 9 408.2047 676.8898 Tm 8 0 0 8 412.41 771.9529 Tm BT 7 0 0 7 445.619 584.7654 Tm EMC BT 0 Tc ET 10 0 0 10 38.6761 771.9528 Tm 6 0 0 6 402.4813 771.9528 Tm EMC /P <>BDC (A321ceo)Tj (In the same trend as on the A320)Tj /P <>BDC ( )Tj ( )Tj (alternate and 45 minutes continued cruise. BT EMC /P <>BDC /P <>BDC BT ET /P <>BDC ( )Tj EMC EMC 7 0 0 7 338.5674 78.9528 Tm BT The Honeywell NGS was certified by the FAA on 21 Feb 2006 after over 1000hrs flight testing on two 737-NGs. ET ( )Tj It is recognised that most)Tj BT BT /P <>BDC ET /P <>BDC ET (150 passengers on the A320ceo, A320neo,)Tj /P <>BDC 7 0 0 7 258.2805 595.7654 Tm 0 Tc ET BT ET ET BT EMC 0 Tc 304.725 420.96 m 9 0 0 9 207.5339 280.8898 Tm ET (1,683)Tj BT ( )Tj EMC /P <>BDC /P <>BDC ( )Tj ( )Tj EMC BT 9 0 0 9 215.4409 335.8898 Tm ET aux (AA) and fwd aux (FA) respectively. BT EMC /P <>BDC BT /P <>BDC BT /P <>BDC 7 0 0 7 491.4046 320.9528 Tm EMC /P <>BDC EMC /P <>BDC /P <>BDC BT ( )Tj /P <>BDC ( )Tj /P <>BDC 9 0 0 9 411.0181 203.8898 Tm ET (3,882)Tj ( )Tj /P <>BDC ET EMC 9 0 0 9 36.8583 445.8898 Tm (5.1:1)Tj (2,731)Tj <>stream /P <>BDC EMC .0081 Tc 9 0 0 9 215.4409 500.8898 Tm (214,730)Tj BT ( )Tj S /P <>BDC BT BT ET (the shorter sectors at 4.6%, and reduces to)Tj 7 0 0 7 89.3229 342.7654 Tm EMC EMC ET BT /P <>BDC 9 0 0 9 411.0181 489.8898 Tm ( )Tj EMC BT ( )Tj /P <>BDC -.02 Tc /P <>BDC EMC /P <>BDC ( )Tj EMC [(CFM L)17.1(E)-8.1(AP-1A32)]TJ (same cost index, and the method that each)Tj EMC /P <>BDC <>stream ( )Tj BT ET )Tj /P <>BDC - Modern Airliners, Pingback:A New Opportunity For Hydrogen is Aviation Aeronautics, Pingback:A New Opportunity For Hydrogen is Aviation - Revolution-Green, Pingback:Southwest CEO Says It's Safe to Fly Again. -.02 Tc BT 9 0 0 9 547.9346 93.8898 Tm cell which attached to the seat tracks of the passenger cabin. 9 0 0 9 193.0624 445.8898 Tm 7 0 0 7 158.74 584.7654 Tm /P <>BDC EMC ( )Tj (271,728)Tj ( )Tj EMC [(CFM L)17.1(E)-8.1(AP-1B27)]TJ ET /P <>BDC 9 0 0 9 425.183 544.8898 Tm 8 0 0 8 347.1567 771.9529 Tm ( )Tj /P <>BDC 7 0 0 7 444.737 100.7654 Tm (capacity would further increase the)Tj 6.5 0 0 6.5 347.0849 722.9529 Tm /P <>BDC EMC 7 0 0 7 54.7071 529.7654 Tm /P <>BDC .014984 841.89 609.45 -841.89 re /P <>BDC 9 0 0 9 229.6045 104.8898 Tm [(R)13.9(ange with full)]TJ ET The)Tj 8 0 0 8 287.7892 771.7654 Tm BT (192)Tj ( )Tj EMC ET EMC /P <>BDC BT EMC Hello, do you know the meaning of the 737-8K5 designation and its background? 6 0 0 6 346.935 771.9528 Tm ET ( )Tj BT 137 )Tj EMC ( )Tj /P <>BDC EMC /P <>BDC 0 Tc EMC ( )Tj EMC ET ET BT (1,311)Tj BT EMC .964 .834 .406 rg /P <>BDC 9 0 0 9 200.4401 258.8898 Tm 7 0 0 7 314.6398 518.7654 Tm ET 9 0 0 9 541.0135 159.8898 Tm The 737-9 has a)Tj ET /P <>BDC 8 0 0 8 187.3427 591.9528 Tm ET BT BT ET /P <>BDC BT /P <>BDC ET ( )Tj ET /P <>BDC EMC 13 0 0 13 215.433 137.8898 Tm f BT /P <>BDC ET /P <>BDC 8 0 0 8 95.6042 633.9528 Tm 9 0 0 9 68.0314 38.8898 Tm ET BT BT 6.5 0 0 6.5 295.5027 565.9529 Tm EMC 9 0 0 9 68.0314 522.8898 Tm /P <>BDC 0 Tc /P <>BDC Jump to Specification Table Boeing 737 Original and Boeing 737 Classic. EMC EMC ET [(Y)-7.1(XX/64)]TJ BT EMC 8 0 0 8 334.994 633.9528 Tm BT EMC /Artifact <>BDC 7 0 0 7 187.0858 364.9528 Tm EMC ET BT Fuel temp is taken from main tank 1 because this will be the coldest as it has BT /P <>BDC ET 0 Tw 7 0 0 7 404.101 199.7654 Tm 7 0 0 7 354.9521 100.7654 Tm 7 0 0 7 491.7142 210.7654 Tm EMC /P <>BDC EMC EMC ET /P <>BDC BT Any help would be greatly appreciated and thank you for all your work its extremely helpful! (The aircraft weights used in this)Tj /F7 1 Tf 6.5 0 0 6.5 499.1812 702.9529 Tm 7 0 0 7 362.3891 309.9528 Tm EMC -.02 Tc Tweet !function(d,s,id){var js,fjs=d.getElementsByTagName(s)[0],p=/^http:/.test(d.location)? 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. BT 7 0 0 7 490.8321 265.7654 Tm ( )Tj ET 0 Tc Q ET /P <>BDC 6 0 0 6 214.8454 771.9528 Tm (A320neo, A321neo, 737-800, 737-)Tj BT EMC 6.5 0 0 6.5 244.0438 722.9529 Tm ET ET /P <>BDC EMC EMC caused the FAA to issue SFAR88 in June 2001 which mandates improvements to the BT /P <>BDC We dont actually have access to a table of these variants and their features. -.02 Tc ET ET ( )Tj BT BT (132,872)Tj 0 Tc ( )Tj )Tj ( )Tj EMC BT /P <>BDC 7 0 0 7 429.157 562.9528 Tm /P <>BDC /P <>BDC /P <>BDC /P <>BDC /P <>BDC /P <>BDC 7 0 0 7 539.8962 683.9528 Tm ET /P <>BDC ( 2021)Tj EMC ET ( )Tj /P <>BDC /P <>BDC W n ET EMC EMC EMC ET BT 7 0 0 7 37.0536 595.9528 Tm ET ET (Airlines, Delta and United. 9 0 0 9 373.4722 49.8898 Tm ET (The comparison of the A320ceo)Tj BT EMC (- USG)Tj 7 0 0 7 118.104 364.7654 Tm EMC ET /P <>BDC ET /P <>BDC 9 0 0 9 541.0405 621.8898 Tm /P <>BDC BT 7 0 0 7 338.6433 386.7654 Tm /P <>BDC 6 0 0 6 277.7064 757.9528 Tm BT /P <>BDC 7 0 0 7 337.4684 716.9528 Tm -.02 Tc ET 503.542 90.794 m -.02 Tc 8 0 0 8 302.5117 577.9528 Tm 9 0 0 9 394.0123 412.8898 Tm ET (an OEW of 98,500lbs )Tj EMC /P <>BDC 9 0 0 9 349.6767 335.8898 Tm 7 0 0 7 279.1575 485.9528 Tm 7 0 0 7 230.7317 529.9528 Tm /P <>BDC EMC 9 0 0 9 192.5225 489.8898 Tm /P <>BDC EMC From July 2004 NGs have been delivered with markings on the 9 0 0 9 36.8504 38.8898 Tm /P <>BDC ET EMC fuel pumps were running in high ambient temperatures with empty or almost empty ET 6.5 0 0 6.5 244.3364 735.9529 Tm (payload, the A321neo has an 18.9%)Tj (configuration, because this study shows)Tj /P <>BDC 7 0 0 7 439.7405 738.9528 Tm 7 0 0 7 204.0935 507.7654 Tm 9 0 0 9 215.4409 434.8898 Tm 0 Tc ET 0 Tc ET 7 0 0 7 37.6993 364.9528 Tm (136)Tj 7 0 0 7 158.74 221.7654 Tm /P <>BDC 9 0 0 9 376.579 434.8898 Tm 9 0 0 9 36.8504 170.8898 Tm BT BT 7 0 0 7 99.8582 463.7654 Tm EMC BT /P <>BDC 7 0 0 7 518.4953 441.9528 Tm -.02 Tc BT 8 0 0 8 332.978 591.9528 Tm /P <>BDC /P <>BDC BT EMC The wheelbase which is the distance from the nosewheel to the line between the main wheels, which is 11.07 metres. 7 0 0 7 536.3849 364.7654 Tm /P <>BDC /P <>BDC BT The cause of the accident was determined to be a malfunctioning left radar altimeter. /P <>BDC /P <>BDC BT ( )Tj 9 0 0 9 375.8752 258.8898 Tm BT BT /P <>BDC ET ET EMC 9 0 0 9 36.8504 412.8898 Tm EMC /P <>BDC EMC 7 0 0 7 204.0935 485.7654 Tm ( )Tj BT /P <>BDC BT (1,454)Tj /P <>BDC ( )Tj BT /P <>BDC ET Hi Mark, BT -.01 Tc ET EMC BT /P <>BDC EMC ET EMC /P <>BDC 0 Tc /P <>BDC 7 0 0 7 518.4953 408.9528 Tm BT /P <>BDC 9 0 0 9 394.0123 104.8898 Tm -.02 Tc ET BT (408)Tj 7 0 0 7 535.5029 705.7654 Tm .023 .567 .626 RG 7 0 0 7 338.6433 320.7654 Tm BT 9 0 0 9 546.3135 258.8898 Tm BT 0 Tc EMC (2,800 -)Tj ( )Tj 9 0 0 9 53.8582 588.8898 Tm ET /P <>BDC ET (31,416)Tj /P <>BDC (427,890)Tj (increase the passenger weight assumptions)Tj 10 0 0 10 37.304 794.2914 Tm (39,270lbs)Tj /P <>BDC 6.5 0 0 6.5 174.4663 735.9529 Tm 0 Tc As an Amazon Associate I earn from qualifying purchases. /P <>BDC 6 0 0 6 154.2695 743.9528 Tm 63 0 obj ET ( )Tj ET /P <>BDC 6.5 0 0 6.5 324.4345 650.9529 Tm BT /P <>BDC BT 6.5 0 0 6.5 64.6596 637.9529 Tm EMC /F6 1 Tf EMC BT 9 0 0 9 193.6853 357.8898 Tm (\(see table, page 19\))Tj ET .151 .147 .15 rg EMC 7 0 0 7 299.0601 89.9528 Tm ET (737-800 is more efficient with up to a)Tj ET ( )Tj -.01 Tc 6.5 0 0 6.5 296.3606 735.9529 Tm EMC &6E'dtU7()euFVfvGWgw8HXhx9IYiy*:JZjz ? BT ( )Tj EMC EMC ( )Tj 7 0 0 7 125.6292 287.7654 Tm EMC 6.5 0 0 6.5 397.1339 663.9529 Tm 7 0 0 7 429.157 727.9528 Tm 7 0 0 7 99.8582 188.7654 Tm Boeing 737-800 Aircraft type: Commercial airplane Manufacturer: Boeing Maiden flight year: 1997 I have flown in this plane Reports (16) Reviews (2) Photos (333) Forum (8) List of aircraft operators Boeing 737-800 Specifications EMC BT /P <>BDC BT 8 0 0 8 314.3535 703.9528 Tm BT BT ( )Tj ET /P <>BDC .151 .147 .15 rg EMC /P <>BDC Hi there.. is anyone able to tell me the radius of the arc of the L1 and L2 doors as they are being opened? BT EMC -.02 Tc BT /P <>BDC -.01 Tc /GS1 gs 7 0 0 7 230.7317 474.9528 Tm /P <>BDC /P <>BDC 9 0 0 9 232.4217 489.8898 Tm BT BT ( )Tj ET EMC 7 0 0 7 299.0601 386.9528 Tm /P <>BDC -.02 Tc 7 0 0 7 182.5706 342.9528 Tm BT BT ( )Tj 9 0 0 9 53.8338 324.8898 Tm ET 7 0 0 7 404.101 342.7654 Tm (discussions in the industry to potentially)Tj ( )Tj EMC EMC Q BT BT ET ET ET (efficiency and so lower fuel burn. 9 0 0 9 394.0315 60.8898 Tm BT BT EMC (0.0140)Tj ET EMC /P <>BDC ( )Tj BT /P <>BDC ( )Tj EMC BT /P <>BDC BT (I)Tj EMC ET ( )Tj BT EMC ET /P <>BDC /P <>BDC 9 0 0 9 68.0314 126.8898 Tm ( )Tj ET EMC BT 9 0 0 9 207.5518 588.8898 Tm /P <>BDC /P <>BDC BT BT EMC ET BT ET ET 7 0 0 7 99.8582 419.7654 Tm 7 0 0 7 338.3085 199.9528 Tm EMC ET /P <>BDC 9 0 0 9 377.4586 676.8898 Tm ET BT ( )Tj /P <>BDC 0 Tc 9 0 0 9 534.3536 577.8898 Tm 6.5 0 0 6.5 499.1421 722.9529 Tm 7 0 0 7 354.6933 408.7654 Tm The same alternate airport was)Tj 0 Tc ET EMC ( )Tj EMC /P <>BDC /P <>BDC ( )Tj EMC ET ET /GS2 gs 7 0 0 7 539.8962 617.9528 Tm 394.516 71.673 160.63 -39.992 re (improvement of 13.1%. Can you please tell me where to look for the cabin height,width, seat height, width and door to door length. BT BT EMC the test, each gauge will display any error codes that they may have. EMC ( )Tj /P <>BDC BT ( )Tj EMC EMC /P <>BDC ET ET /P <>BDC ET EMC /P <>BDC /P <>BDC BT 9 0 0 9 215.4313 170.8898 Tm (31,416)Tj 7 0 0 7 116.3631 11.5132 Tm BT ( )Tj BT 9 0 0 9 538.8793 368.8898 Tm EMC EMC EMC ET (increases to 0.22 to 0.29 cents or 8.7%)Tj BT 9 0 0 9 411.0181 445.8898 Tm /P <>BDC ET ET EMC ET EMC ET 7 0 0 7 258.2805 463.7654 Tm /P <>BDC /P <>BDC /P <>BDC 7 0 0 7 536.3849 67.7654 Tm /P <>BDC /P <>BDC BT ( )Tj ( )Tj (PPS flight planning software is used to)Tj 9 0 0 9 36.8504 368.8898 Tm ( )Tj Neither the 737-800 nor the 737-8)Tj (this page\))Tj 9 0 0 9 375.0299 434.8898 Tm The NG has 6 dripsticks in each wing tank and 4 in the centre ( )Tj 9 0 0 9 394.0157 500.8898 Tm ( )Tj 19.841 0 l ET 7 0 0 7 82.2047 727.9528 Tm EMC /P <>BDC BT EMC /P <>BDC 7 0 0 7 187.5417 430.9528 Tm /P <>BDC EMC EMC EMC BT BT /P <>BDC BT ET 8 0 0 8 394.0157 797.8898 Tm ( )Tj BT BT EMC EMC (273,917)Tj ET /P <>BDC ( )Tj BT (fuel consumption and cost per seat or per)Tj ET EMC (403)Tj 7 0 0 7 492.5963 738.7654 Tm (maximum passenger payload of 160. EMC (to a larger increase when going from 5.7:1)Tj (A320neo will be evaluated with the same)Tj /P <>BDC BT ET BT ET BT EMC The NGS requires no flight or ground crew action for normal system operation and is not dispatch critical. /P <>BDC BT EMC 6.5 0 0 6.5 295.373 742.9529 Tm You were right, there were some discrepancies around the range. ET ET ET ( )Tj ET /P <>BDC 9 0 0 9 206.8842 522.8898 Tm /P <>BDC EMC EMC EMC BT 9 0 0 9 550.8315 247.8898 Tm ET Wed love you to share what you build when youre done. waiting with pax ET 7 0 0 7 233.5248 78.9528 Tm EMC (1,202)Tj BT ( )Tj EMC ( )Tj EMC EMC BT ET ET (31,416lbs)Tj ET ET BT BT EMC ( )Tj /P <>BDC /P <>BDC BT (105,000lbs. EMC 9 0 0 9 215.4313 203.8898 Tm EMC ET BT /P <>BDC EMC /P <>BDC BT (As with the rest of the Airbus aircraft,)Tj BT EMC (lighter aircraft. ET /P <>BDC /P <>BDC EMC /P <>BDC (burn and operating)Tj ET /F1 1 Tf BT BT BT ET EMC ET ET -.01 Tc /P <>BDC -.02 Tc /F6 1 Tf /P <>BDC -.01 Tc /P <>BDC Hi All, 7 0 0 7 338.3085 298.9528 Tm ( )Tj BT BT ET EMC /P <>BDC BT (163)Tj 7 0 0 7 355.3163 67.7654 Tm [(R)21(oute )]TJ /P <>BDC 7 0 0 7 187.0858 496.9528 Tm /P <>BDC ET .023 .567 .626 rg (\(see table, this)Tj (737-9)Tj /GS1 gs EMC .41 .161 .508 RG [(T)53.9(r)10(acked distance - nm)]TJ BT Q ( )Tj /P <>BDC 9 0 0 9 411.0181 368.8898 Tm 7 0 0 7 387.0932 188.9528 Tm ET BT 10 0 0 10 36.8504 814.1973 Tm ( )Tj The B737-800SF Cargo Conversion consists of the installation of a 86x137 cargo door on the left side of the fuselage, and modification of the main deck to a Class E cargo compartment. /P <>BDC (A320ceo and A320neo in this study. ET 7 0 0 7 536.3849 628.7654 Tm 0 Tc ET The)Tj /P <>BDC /P <>BDC 199,158 Litres: . ET (7B27B3)Tj ( )Tj ET EMC ET /GS2 gs /P <>BDC ET /P <>BDC BT /P <>BDC EMC ( )Tj /P <>BDC (A321neo)Tj BT EMC BT ET 7 0 0 7 537.7804 397.9528 Tm BT 7 0 0 7 403.478 529.7654 Tm (5,394)Tj BT ( )Tj EMC -.02 Tc ( )Tj 9 0 0 9 36.8504 368.8898 Tm BT EMC BT EMC BT ( )Tj ET BT EMC EMC -.01 Tc BT EMC /P <>BDC [(UG)-17.1(U)-8(S)8.1(T)]TJ 7 0 0 7 554.7883 342.7654 Tm 9 0 0 9 537.7245 676.8898 Tm ( )Tj 9 0 0 9 172.5802 467.8898 Tm ET 7 0 0 7 343.2355 694.7654 Tm
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