/P <>BDC Main tanks > 50%, -1 to 5 deg pitch, +/- 1 deg roll: +/- 1.5% BT /P <>BDC 10 0 0 10 52.6304 814.1973 Tm /P <>BDC EMC BT Thank you. BT ET /P <>BDC (ESAD)Tj ET EMC -.02 Tc -.02 Tc BT EMC 8 0 0 8 365.7704 675.9528 Tm EMC EMC ()Tj 9 0 0 9 198.5183 445.8898 Tm -.02 Tc NG/MAX: The engine spar valves and APU are normally powered by the hot EMC EMC ET EMC -.01 Tc 7 0 0 7 294.4014 320.7654 Tm ET /P <>BDC 0 Tc BT 0 Tc 7 0 0 7 363.2711 397.9528 Tm (170)Tj 8 0 0 8 38.4438 675.9528 Tm ET BT (157)Tj BT ET ET .0161 Tc EMC -.02 Tc ET ( )Tj 7 0 0 7 337.6855 408.9528 Tm 0 Tc ET -.02 Tc EMC BT /P <>BDC 0 Tc EMC BT ( )Tj EMC ET EMC EMC EMC BT ET EMC BT (assume that the optimum flight level could)Tj BT (around the world. ET 9 0 0 9 36.8504 60.8898 Tm 7 0 0 7 508.4124 177.7654 Tm /GS2 gs EMC BT ET EMC ET /P <>BDC /P <>BDC BT EMC 0 Tc /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? /P <>BDC ET BT EMC 19.843 0 l EMC EMC ET BT ET EMC 8 0 0 8 315.7776 577.9528 Tm ET (0.0154)Tj 9 0 0 9 215.4409 489.8898 Tm /P <>BDC 9 0 0 9 53.8582 511.8898 Tm /P <>BDC ( )Tj ( )Tj BT ET EMC ET ET 7 0 0 7 338.6433 364.7654 Tm /P <>BDC ( )Tj ( )Tj BT 7 0 0 7 381.1608 595.7654 Tm [(AIRL)8.1(INE & AIR)7.1(CRAF)-12.9(T)18.1( OPERA)56.9(T)-8.1(ION)-13.9(S)]TJ 7 0 0 7 380.2788 496.7654 Tm 0 Tc BT (5,843)Tj /P <>BDC ( )Tj EMC BT -.02 Tc EMC /P <>BDC 304.725 420.96 m BT /P <>BDC EMC EMC BT ET ET 7 0 0 7 387.0932 133.9528 Tm EMC (It is recognised that on some of the)Tj Q They are quite easy to find. ( )Tj /P <>BDC BT BT each aircraft is sourced from different places. 9 0 0 9 551.0015 291.8898 Tm ET /P <>BDC EMC BT 0 Tc 7 0 0 7 99.8582 100.7654 Tm The 737 fuel quantity indication system has the following accuracy tolerances: 737-100/-200: /P <>BDC 9 0 0 9 542.1815 786.8898 Tm /P <>BDC EMC 7 0 0 7 99.5912 584.9528 Tm 7 0 0 7 508.4124 727.7654 Tm 0 Tc .023 .567 .626 rg 7 0 0 7 365.035 639.9528 Tm BT /P <>BDC ET [(CFM L)17.1(E)-8.1(AP-1B27)]TJ EMC ET EMC )Tj 10 0 0 10 425.05 814.1973 Tm 7 0 0 7 520.6108 529.9528 Tm /P <>BDC 6.5 0 0 6.5 244.2585 637.9529 Tm BT ET 9 0 0 9 567.1517 49.8898 Tm ET BT /P <>BDC BT BT ( )Tj /P <>BDC /P <>BDC /P <>BDC ET BT ( )Tj BT EMC (for seats. 0 Tc )Tj 7 0 0 7 82.8504 100.9528 Tm /P <>BDC EMC 6.5 0 0 6.5 90.4525 663.9529 Tm EMC /P <>BDC /P <>BDC ET ET ET BT ( )Tj BT ET 9 0 0 9 75.273 478.8898 Tm (174,200)Tj BT 7 0 0 7 362.3891 199.9528 Tm BT 9 0 0 9 211.8218 533.8898 Tm /P <>BDC BT EMC ET 7 0 0 7 456.4753 716.7654 Tm 0 Tc EMC /P <>BDC BT 7 0 0 7 87.8179 144.7654 Tm BT ET ( )Tj 7 0 0 7 362.3891 243.9528 Tm remain illuminated for more than 19 seconds then this is probably what has BT (136)Tj (. (aim was remove this variability from the)Tj (2,500)Tj 0 Tc BT )Tj /P <>BDC BT ( )Tj /F4 1 Tf 7 0 0 7 518.4953 122.9528 Tm EMC /P <>BDC ( )Tj /P <>BDC On older aircraft the trimmers were accessible from the 7 0 0 7 362.3891 320.9528 Tm BT /P <>BDC /P <>BDC BT /P <>BDC EMC ET ET /P <>BDC BT EMC 9 0 0 9 53.8582 797.8898 Tm /P <>BDC 9 0 0 9 552.9554 357.8898 Tm 0 Tc (series of aircraft compared to the)Tj 7 0 0 7 109.3921 430.9528 Tm 9 0 0 9 179.5372 313.8898 Tm /P <>BDC ET ET 0 Tc EMC /Im1 Do ET /P <>BDC /GS2 gs ET BT BT EMC (150)Tj /P <>BDC ET /P <>BDC /P <>BDC BT EMC -.02 Tc ( )Tj BT EMC BT EMC 7 0 0 7 53.8582 650.7654 Tm ET ET 9 0 0 9 232.4217 126.8898 Tm 6.5 0 0 6.5 531.9417 637.9529 Tm ( )Tj q 1 0 0 1 36.85 469.878 cm 0 0 m 13 0 0 13 36.8504 456.8898 Tm 6.5 0 0 6.5 549.8557 545.9529 Tm /P <>BDC ET ( )Tj EMC -.02 Tc to the centre tank through a manual valve by cabin pressure. ET 0 Tc ET ( )Tj EMC BT /P <>BDC 9 0 0 9 552.5356 445.8898 Tm ( )Tj BT /P <>BDC 9 0 0 9 232.438 192.8898 Tm -.005 Tc 6.5 0 0 6.5 280.6329 545.9529 Tm EMC /P <>BDC (1,351)Tj The 737-800 has a maximum fuel capacity of 6,875 gallons, which it carries in fuel tanks in its wings, as seen here, and in a fuel tank located underneath the passenger cabin's midsection. ET EMC 7 0 0 7 118.104 606.7654 Tm The seat configuration)Tj ET ET /P <>BDC /P <>BDC /P <>BDC /P <>BDC 6.5 0 0 6.5 191.8316 637.9529 Tm (977)Tj [(P)11(ayload scenario one)]TJ /P <>BDC EMC EMC ET /P <>BDC /P <>BDC -.01 Tc In one insistence a 737-800 on a route from Istanbul crashing in a field near the Polderbaan. (39,270)Tj 9 0 0 9 374.4497 214.8898 Tm EMC ( )Tj 0 Tc BT BT (737-800W)Tj 1 i /P <>BDC ET 6 0 0 6 215.373 757.9528 Tm /Figure <>BDC EMC EMC -.02 Tc /P <>BDC /P <>BDC 7 0 0 7 519.3773 364.9528 Tm 9 0 0 9 215.4409 170.8898 Tm (impact on the fuel cost per ASM. 10 0 0 10 422.8 814.1973 Tm 9 0 0 9 543.5425 522.8898 Tm /P <>BDC /P <>BDC BT /P <>BDC ET 9 0 0 9 358.9372 346.8898 Tm /P <>BDC (All the aircraft were evaluated using)Tj [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ EMC ET EMC BT /P <>BDC ( )Tj EMC -.02 Tc EMC /P <>BDC ET EMC 9 0 0 9 371.6638 247.8898 Tm -.02 Tc ( )Tj /P <>BDC /P <>BDC -.01 Tc On the longer sectors, however, the)Tj EMC EMC EMC EMC ET ( )Tj ET (with an ESAD of 2,576nm in payload)Tj ET 9 0 0 9 541.1665 599.8898 Tm EMC ( 2021)Tj ( )Tj /P <>BDC EMC EMC 7 0 0 7 491.7142 485.7654 Tm EMC 8 0 0 8 370.117 771.9529 Tm 7 0 0 7 230.7317 243.9528 Tm 7 0 0 7 204.0935 529.7654 Tm EMC 7 0 0 7 444.737 133.7654 Tm ( )Tj -.02 Tc ET /P <>BDC BT BT /P <>BDC ET ET ET 0 Tc (\(see table, this page\))Tj ET BT -.02 Tc EMC ET /P <>BDC (152,800)Tj EMC 7 0 0 7 187.0858 606.9528 Tm ET ( )Tj BT 0 Tc EMC /P <>BDC (1B engine as the 737-8. BT ( )Tj 8 0 0 8 302.5117 577.9528 Tm 7 0 0 7 440.0906 232.9528 Tm 7 0 0 7 294.4014 573.7654 Tm ET BT EMC ( )Tj 0 Tc ( )Tj /OC /MC21 BDC 7 0 0 7 537.267 232.7654 Tm 7 0 0 7 354.4763 672.7654 Tm 0 Tc 9 0 0 9 394.0123 335.8898 Tm BT -.02 Tc EMC ET EMC (113)Tj BT ET )Tj ( )Tj /P <>BDC /P <>BDC BT 6 0 0 6 255.8802 771.9528 Tm /P <>BDC ET EMC 6.5 0 0 6.5 54.877 637.9529 Tm EMC -.01 Tc /P <>BDC ( )Tj BT ET EMC (170)Tj 7 0 0 7 537.7804 320.9528 Tm 0 Tc ET 7 0 0 7 537.7804 122.9528 Tm EMC ( N)Tj ( )Tj /P <>BDC ET BT EMC EMC ET BT ET /P <>BDC ET /P <>BDC ET EMC ET ( )Tj /P <>BDC BT EMC /P <>BDC /P <>BDC 7 0 0 7 387.0932 177.9528 Tm EMC 9 0 0 9 529.6118 302.8898 Tm EMC /P <>BDC BT BT 7 0 0 7 247.7395 606.7654 Tm /P <>BDC 9 0 0 9 553.9287 643.8898 Tm EMC 7 0 0 7 82.2047 705.9528 Tm ET EMC 0 Tc /P <>BDC For the purposes of)Tj EMC EMC 7 0 0 7 199.5784 595.7654 Tm ET ET -.02 Tc (CFM56-5B4/P)Tj support combustion. BT EMC -.02 Tc 0 Tc 9 0 0 9 541.1655 478.8898 Tm 0 Tc BT BT /P <>BDC 7 0 0 7 82.2047 463.9528 Tm (l)Tj ( )Tj BT ET -.02 Tc ( )Tj ET (483)Tj 9 0 0 9 246.6113 401.8898 Tm EMC /P <>BDC EMC ET EMC /P <>BDC (The improvement in fuel cost per ASM)Tj ET ( )Tj /F6 1 Tf ET /P <>BDC BT /P <>BDC (113,016)Tj EMC The VNE or never exceed speed for the Boeing 737-800 is 340 KIAS(Knots indicated airspeed) or Mach 0.82. 7 0 0 7 337.4684 705.9528 Tm ET BT BT EMC EMC BT (evaluated for both types, the 737-)Tj ( )Tj BT /P <>BDC EMC BT ( )Tj BT 9 0 0 9 117.7519 170.8898 Tm BT 0 Tc (maximum passenger payload of 160. /P <>BDC /P <>BDC /P <>BDC Due to the additional structural)Tj 9 0 0 9 204.483 104.8898 Tm EMC ET (BOS-DEN)Tj BT EMC -.02 Tc 9 0 0 9 215.4313 170.8898 Tm (page\))Tj BT q Thanks for stopping by. 7 0 0 7 321.6356 89.9528 Tm EMC 304.725 420.96 m 9 0 0 9 543.0273 192.8898 Tm ET (The lowest fuel cost per ASM in the)Tj ( )Tj /P <>BDC /P <>BDC ET BT -.01 Tc BT /P <>BDC ET ET EMC BT (483)Tj 9 0 0 9 551.0557 467.8898 Tm /P <>BDC EMC /P <>BDC Hello! /P <>BDC EMC ( )Tj 7 0 0 7 37.6993 221.9528 Tm ET EMC 7 0 0 7 535.5029 188.7654 Tm ET ( )Tj -.02 Tc BT -.02 Tc (be achieved. ET EMC ET BT 8 0 0 8 275.1912 745.9528 Tm The NG series are prone to "Upper Wing Surface BT EMC BT BT /P <>BDC 9 0 0 9 512.8093 434.8898 Tm BT /P <>BDC ( )Tj 7 0 0 7 338.6433 133.7654 Tm ( )Tj EMC /P <>BDC ET /P <>BDC /P <>BDC ET (375)Tj 7 0 0 7 337.6855 221.9528 Tm /P <>BDC 0 Tc 0 Tc 0 Tc 6 0 0 6 147.4588 729.9528 Tm ET ( )Tj EMC EMC 7 0 0 7 298.514 639.9528 Tm (configuration to increase passenger seat)Tj The aircraft in this)Tj -.02 Tc ET 9 0 0 9 232.4408 742.8898 Tm /P <>BDC /P <>BDC 9 0 0 9 547.3786 71.8898 Tm EMC 7 0 0 7 554.7883 199.7654 Tm 6 0 0 6 403.1408 687.9528 Tm (CFM56-7B26)Tj 6 0 0 6 61.517 729.9528 Tm EMC ET /P <>BDC FQIS accuracy: +/- 2.0% overall ( )Tj 7 0 0 7 457.0984 463.7654 Tm 7 0 0 7 354.6933 474.7654 Tm 9 0 0 9 394.0157 412.8898 Tm BT 9 0 0 9 36.8504 93.8898 Tm ( )Tj /P <>BDC 6.5 0 0 6.5 279.814 585.9529 Tm ET BT /P <>BDC 9 0 0 9 370.891 302.8898 Tm 7 0 0 7 279.1575 386.9528 Tm ( )Tj ET 5.25 0 0 5.25 465.7151 11.5129 Tm 9 0 0 9 36.8583 467.8898 Tm each engine. /P <>BDC /P <>BDC ET BT .151 .147 .15 rg EMC EMC -.01 Tc 7 0 0 7 456.2165 320.7654 Tm EMC ET ( )Tj BT EMC EMC 9 0 0 9 345.8168 445.8898 Tm ( )Tj 8 0 0 8 480.7187 771.9529 Tm BT (2,731)Tj BT BT /P <>BDC ET BT EMC BT (37,653)Tj ET ET BT [(CFM L)17.1(E)-8.1(AP-1A32)]TJ 9 0 0 9 196.8605 115.8898 Tm 0 Tc Q EMC EMC 9 0 0 9 182.8313 346.8898 Tm /P <>BDC ET 13 0 0 13 530.7245 434.8898 Tm )Tj -.02 Tc BT 9 0 0 9 232.438 368.8898 Tm /P <>BDC /P <>BDC ( )Tj /P <>BDC BT 9 0 0 9 554.3696 269.8898 Tm ET EMC EMC /P <>BDC 9 0 0 9 394.0315 720.8898 Tm ( The taxi-in and taxi-out times and)Tj /P <>BDC ET ET /P <>BDC BT 0 Tc ET BT EMC [(SS)-9(U)8.1(E)]TJ 9 0 0 9 215.4409 500.8898 Tm EMC BT ET fuel and de-ice the fuel filter. EMC EMC /P <>BDC ET EMC 8 0 0 8 43.6039 771.9528 Tm BT /P <>BDC ET EMC 8 0 0 8 225.1837 633.9528 Tm 0 Tc ET BT BT /P <>BDC /P <>BDC )Tj /P <>BDC ET ET 7 0 0 7 54.5916 441.7654 Tm 0 Tc Q 0 Tc 9 0 0 9 53.8578 214.8898 Tm BT EMC 0 Tc /P <>BDC ( )Tj EMC ET W n ET BT (/S)Tj 6 0 0 6 214.4975 659.9528 Tm 8 0 0 8 187.3427 619.9528 Tm (2,060)Tj EMC BT 9 0 0 9 527.3954 313.8898 Tm 6.5 0 0 6.5 54.877 624.9529 Tm (. /P <>BDC 7 0 0 7 439.7405 705.9528 Tm EMC ( )Tj /P <>BDC 0 Tc BT /P <>BDC (0.0129)Tj /P <>BDC /P <>BDC EMC ET BT /P <>BDC ET /P <>BDC BT BT ( C)Tj ET ET 6.5 0 0 6.5 54.877 702.9529 Tm 6 0 0 6 540.5396 715.9528 Tm 0 Tc /P <>BDC BT (optimum cruise altitude. 786 0 obj ( )Tj 0 Tc .151 .147 .15 rg BT 6.5 0 0 6.5 191.7701 558.9529 Tm ET 7 0 0 7 490.8321 78.7654 Tm /P <>BDC ( )Tj /P <>BDC ET BT EMC (ASM. EMC /P <>BDC EMC BT 9 0 0 9 566.9979 423.8898 Tm ET /OC /MC3451 BDC EMC ET EMC 0 Tc BT BT 7 0 0 7 241.2727 463.9528 Tm ET -.02 Tc .559 .331 .619 rg /GS2 gs BT ET ET ( )Tj ET BT (10)Tj BT /P <>BDC /P <>BDC (487)Tj 10 0 0 10 408.1099 814.1973 Tm BT ET /P <>BDC ET ET ( )Tj EMC EMC /P <>BDC 9 0 0 9 394.0157 588.8898 Tm BT ET 7 0 0 7 279.1575 496.9528 Tm EMC q ET ET (A321ceo)Tj BT ET ET 6 0 0 6 55.0668 673.9528 Tm 6.5 0 0 6.5 172.8217 565.9529 Tm /P <>BDC 0 Tc 5 0 0 5 484.5872 11.5129 Tm ( )Tj 7 0 0 7 539.8962 738.9528 Tm ( )Tj ET /P <>BDC 0 Tc .41 .161 .508 rg EMC -.02 Tc BT EMC 7 0 0 7 107.1165 661.9528 Tm ( )Tj ET As you can appreciate, the cockpit of any aircraft is always a non-standard shape. -.01 Tc ET BT /P <>BDC 9 0 0 9 53.8338 225.8898 Tm 7 0 0 7 314.6398 727.7654 Tm ET -.02 Tc 0 Tc ET EMC ET ET Limitations: Max fuel temp +49C, Min ET ( )Tj EMC (2,042)Tj EMC (170)Tj ET /P <>BDC /P <>BDC ET ( )Tj 394.516 71.673 160.63 -39.992 re EMC /P <>BDC 9 0 0 9 36.8583 445.8898 Tm EMC EMC EMC BT BT /P <>BDC (The wider intake fan diameters leading)Tj ET -.02 Tc ET ET ET EMC /P <>BDC ( )Tj /P <>BDC /P <>BDC 9 0 0 9 165.0289 60.8898 Tm /P <>BDC BT 6 0 0 6 153.1846 771.9528 Tm /P <>BDC ( )Tj BT -.02 Tc EMC ET -.01 Tc /P <>BDC BT The system tolerance is then +/- 300 KG at any fuel level within the tank. ET ET 9 0 0 9 372.4479 368.8898 Tm BT EMC 0 Tc /P <>BDC (CFM56-7B27B3)Tj EMC EMC 6 0 0 6 61.517 715.9528 Tm ( )Tj EMC EMC /P <>BDC /P <>BDC 9 0 0 9 232.4217 401.8898 Tm ( )Tj /P <>BDC ET BT /P <>BDC BT /P <>BDC /P <>BDC 7 0 0 7 445.619 375.7654 Tm (170)Tj -.02 Tc ET 9 0 0 9 75.3887 489.8898 Tm ( )Tj EMC ET EMC BT ET ( )Tj ( )Tj ET ET BT EMC ET BT /P <>BDC (burn and cost per seat and per ASM than)Tj /P <>BDC BT 7 0 0 7 380.2788 617.7654 Tm 7 0 0 7 314.6398 705.7654 Tm BT .41 .161 .508 RG 7 0 0 7 315.5217 562.7654 Tm Federal Aviation Administration and the Boeing Company to evaluate the ET BT ET /P <>BDC 6.5 0 0 6.5 295.5027 565.9529 Tm ET ET 7 0 0 7 535.5029 78.7654 Tm BT 8 0 0 8 225.1837 717.9528 Tm (10)Tj /P <>BDC /P <>BDC EMC /P <>BDC (170)Tj ( )Tj /P <>BDC /P <>BDC /P <>BDC BT ET BT ET 518.735 0 l 9 0 0 9 206.8496 346.8898 Tm BT BT (150)Tj 8 0 0 8 95.6042 633.9528 Tm ET (104)Tj /P <>BDC (0.39 to 0.48 cents per ASM with an)Tj EMC /P <>BDC /P <>BDC /P <>BDC /F4 1 Tf EMC 9 0 0 9 411.0097 599.8898 Tm /P <>BDC ET 0 Tc EMC 0 841.89 609.449 -841.89 re BT 7 0 0 7 539.8962 496.9528 Tm BT 304.725 420.96 m 7 0 0 7 491.392 463.9528 Tm ET ET ( )Tj ET ET BT EMC -.02 Tc -4.2575 -4.8278 -4.5158 -4.0295 -4.515 -3.0604 c EMC /P <>BDC ET (to 165 passengers on BOS-LAX. Q ( )Tj /GS1 gs EMC EMC (types will only be made where unrestricted)Tj /P <>BDC /P <>BDC EMC EMC /P <>BDC [(v)21(ariant)]TJ ET -.01 Tc EMC EMC ET ( )Tj BT 7 0 0 7 491.7142 683.7654 Tm ET The aux tanks are located at ET /P <>BDC ( )Tj EMC -.02 Tc EMC 0 Tc BT /P <>BDC /P <>BDC BT ( )Tj ET q 1 0 0 1 394.016 747.971 cm 0 0 m [(A3)24.9(20neo)]TJ /P <>BDC .023 .567 .626 rg /P <>BDC ET (70)Tj BT ET 0 Tc BT ET /P <>BDC BT 8 0 0 8 539.8061 771.9528 Tm ET ET 9 0 0 9 53.8582 203.8898 Tm 6 0 0 6 254.6866 659.9528 Tm BT EMC EMC /P <>BDC EMC EMC EMC ET 28.5749 0 TD /P <>BDC 6.5 0 0 6.5 499.4541 735.9529 Tm ET EMC 7 0 0 7 278.9827 430.9528 Tm The common factor in both accidents was that the centre tank /P <>BDC BT 6 0 0 6 208.1569 743.9528 Tm (2,899)Tj EMC (31,416lbs)Tj