( )Tj /P <>BDC /P <>BDC BT /P <>BDC ( )Tj BT EMC 7 0 0 7 491.4046 331.9528 Tm 7 0 0 7 107.1165 661.9528 Tm BT /P <>BDC -.02 Tc 7 0 0 7 490.7815 265.9528 Tm BT EMC ET ( )Tj ( )Tj ( )Tj ( )Tj ( )Tj 7 0 0 7 36.8504 155.9528 Tm (\(neo\) families, and the 737NG family. ET 7 0 0 7 537.7804 111.9528 Tm ET 7 0 0 7 474.3564 628.9528 Tm BT BT EMC 6 0 0 6 184.4741 687.9528 Tm EMC 8 0 0 8 38.4438 633.9528 Tm EMC /P <>BDC (39,270lbs)Tj -.01 Tc EMC EMC EMC ( )Tj (50,800)Tj EMC /P <>BDC /P <>BDC EMC 7 0 0 7 491.7142 672.7654 Tm BT 7 0 0 7 429.4931 122.9528 Tm -.02 Tc (I)Tj 6.5 0 0 6.5 228.7846 545.9529 Tm /GS2 gs BT ET 6 0 0 6 184.072 659.9528 Tm BT BT EMC /F6 1 Tf 7 0 0 7 490.7815 67.9528 Tm ET 7 0 0 7 314.6398 507.7654 Tm EMC 6.5 0 0 6.5 64.6596 545.9529 Tm /P <>BDC Do you know how or where I would be able to get details on the dimensions or materials of the wingtip for this aircraft or other similar aircraft? ET ET -.01 Tc BT BT 7 0 0 7 37.5838 56.9528 Tm 0 Tc /P <>BDC ET /GS2 gs ( )Tj 9 0 0 9 215.433 357.8898 Tm BT ( )Tj /P <>BDC EMC EMC EMC (0.0123)Tj EMC /P <>BDC /P <>BDC 7 0 0 7 403.478 694.7654 Tm /P <>BDC ET -.01 Tc .41 .161 .508 rg 7 0 0 7 297.632 738.9528 Tm EMC /P <>BDC 9 0 0 9 193.2686 49.8898 Tm ET ET ( )Tj EMC 0 Tc BT /P <>BDC BT ET EMC 9 0 0 9 192.8213 60.8898 Tm 9 0 0 9 394.0123 236.8898 Tm ET 9 0 0 9 365.1208 346.8898 Tm ET EMC 7 0 0 7 387.0932 276.9528 Tm 7 0 0 7 382.0427 100.7654 Tm /P <>BDC BT ET 9 0 0 9 68.3339 555.8898 Tm ET EMC ET BT EMC (2,189)Tj 0 Tc EMC ET 7 0 0 7 490.5101 661.9528 Tm /P <>BDC /P <>BDC /P <>BDC /GS1 gs BT ( )Tj ( A)Tj BT ( )Tj BT ( )Tj EMC flugzeuginfo.net is a non-commercial webproject. 0 Tc ET /Im3 Do BT EMC /P <>BDC ET ET ( )Tj (37,653)Tj ET (fan diameter of 81 inches, and a bypass)Tj EMC /P <>BDC /Artifact <>BDC ( )Tj BT BT ET EMC (178)Tj EMC [(7)-33(3)8(7-800)]TJ ET /P <>BDC ET EMC ET (subsidiary airlines. 9 0 0 9 425.1913 181.8898 Tm (1,272)Tj /P <>BDC EMC 7 0 0 7 492.5963 430.7654 Tm BT ET /P <>BDC /P <>BDC (A320ceo)Tj ( )Tj 0 Tc /P <>BDC BT Of course, we know that there have been major hiccups in the introduction of the new 737 MAX with the tragic loss of life as a result. ET FQIS accuracy with analog indicators: +/- 3.0% /P <>BDC /P <>BDC EMC BT ET EMC 9 0 0 9 53.8582 280.8898 Tm BT 9 0 0 9 53.8578 335.8898 Tm /P <>BDC q 1 0 0 1 411.01 480.878 cm 0 0 m BT (operational factors that also have to be)Tj ET /F5 1 Tf EMC /P <>BDC EMC 7 0 0 7 95.225 11.5132 Tm 7 0 0 7 518.4953 419.9528 Tm ET 1 w BT BT EMC 9 0 0 9 542.4784 115.8898 Tm EMC 0 Tc /GS2 gs EMC EMC BT EMC ET -.01 Tc ( )Tj EMC ( )Tj /P <>BDC EMC ET BT EMC ET EMC EMC BT 7 0 0 7 182.5706 441.9528 Tm (575)Tj ET Engine size 7 0 0 7 535.5029 705.7654 Tm 6.5 0 0 6.5 243.7903 611.9529 Tm ( )Tj EMC BT ET ET BT (A321ceo:)Tj 9 0 0 9 215.4313 170.8898 Tm EMC (similar-sized and directly competing)Tj 0 Tc /P <>BDC /P <>BDC EMC Reads payload (passenger and baggage) weights via FSUIPC. EMC /P <>BDC BT BT -.01 Tc ET EMC EMC ET ET 0 Tc ( )Tj EMC BT -.02 Tc /P <>BDC (37,653)Tj ET /P <>BDC EMC BT (load factor, the A321neo carries a heavier)Tj 9 0 0 9 455.0733 302.8898 Tm ET /P <>BDC ET BT EMC /GS2 gs ET 9 0 0 9 544.8903 698.8898 Tm ET ( )Tj BT https://www.researchgate.net/publication/302903333_On_Boeing_737_-_300_Wing_Aerodynamics_Calculations_Based_on_VLM_Theory. /P <>BDC BT ET ET /P <>BDC /P <>BDC EMC BT EMC BT BT BT ( )Tj [(YH)-23.9(M/58)]TJ ( )Tj ( )Tj EMC BT /Artifact <>BDC EMC 6 0 0 6 434.151 715.9528 Tm In payload scenario 1 the)Tj (65,688)Tj /P <>BDC EMC ET /P <>BDC 6.5 0 0 6.5 296.4841 650.9529 Tm /P <>BDC 7 0 0 7 230.7317 529.9528 Tm BT /P <>BDC -.02 Tc 7 0 0 7 158.74 562.7654 Tm /P <>BDC -.02 Tc EMC BT BT 6.5 0 0 6.5 346.019 742.9529 Tm 9 0 0 9 411.0097 60.8898 Tm ET BT /P <>BDC BT EMC 7 0 0 7 380.2788 518.7654 Tm %
9 0 0 9 215.4409 368.8898 Tm BT /P <>BDC 5.25 0 0 5.25 123.5367 11.5132 Tm EMC /P <>BDC EMC 7 0 0 7 187.0858 265.9528 Tm EMC /P <>BDC /P <>BDC BT 6.5 0 0 6.5 192.0331 663.9529 Tm EMC -.02 Tc BT -.02 Tc EMC 0 Tc EMC EMC ET /P <>BDC (The A321ceo has a maximum fuel)Tj BT (2,013)Tj (bypass ratio of 9.0:1. 0 Tc /P <>BDC ( )Tj EMC ( )Tj BT ET -.02 Tc (passenger payload - nm)Tj /P <>BDC BT BT ( )Tj EMC BT EMC ET 9 0 0 9 232.4408 720.8898 Tm 7 0 0 7 148.0554 11.5132 Tm 7 0 0 7 362.3891 309.9528 Tm [(Aircr)10(aft type)]TJ 9 0 0 9 200.4718 38.8898 Tm 9 0 0 9 36.8504 159.8898 Tm 0 Tc -.02 Tc EMC ( )Tj 0 Tc EMC BT -.02 Tc 9 0 0 9 36.8504 291.8898 Tm BT ( )Tj 0 Tc BT ET BT 9 0 0 9 77.618 82.8898 Tm 7 0 0 7 456.2165 474.7654 Tm /P <>BDC EMC (financing. -.02 Tc BT 7 0 0 7 354.6933 364.7654 Tm ET /P <>BDC /P <>BDC /P <>BDC EMC 7 0 0 7 354.7351 683.7654 Tm ET ( )Tj 8 0 0 8 136.5171 758.9528 Tm EMC ( )Tj -.5815 -.9071 l 0 Tc BT (737-9)Tj BT /P <>BDC BT .151 .147 .15 rg (and in fuel burn per ASM. (737-9)Tj (737-800W)Tj /P <>BDC EMC BT ET EMC BT /P <>BDC /P <>BDC /P <>BDC /P <>BDC /P <>BDC ET 9 0 0 9 411.0234 764.8898 Tm EMC -.02 Tc BT BT BT BT ( )Tj /P <>BDC ET (Recent improvements in cabin design)Tj 6 0 0 6 450.9814 701.9528 Tm 7 0 0 7 490.8321 375.7654 Tm /P <>BDC 0 Tc EMC EMC BT EMC BT EMC EMC 9 0 0 9 53.8338 181.8898 Tm /P <>BDC (constraints, the 737 MAX has a smaller)Tj BT ET BT 7 0 0 7 36.8504 11.5129 Tm (2,517)Tj BT /P <>BDC /P <>BDC 36.85 824.882 572.599 17.008 re /Im4 Do EMC EMC q 1 0 0 1 36.858 403.878 cm 0 0 m 6.5 0 0 6.5 477.8064 689.9529 Tm BT /P <>BDC EMC EMC /P <>BDC /P <>BDC 9 0 0 9 411.0181 159.8898 Tm ET [(BOS-D)17.1(T)-11(W)]TJ BT EMC /P <>BDC 9 0 0 9 36.8504 137.8898 Tm 9 0 0 9 408.1889 137.8898 Tm ( )Tj 7 0 0 7 535.5029 177.7654 Tm EMC ( )Tj BT BT BT /P <>BDC ET (1,824)Tj /P <>BDC BT S 0 Tc /P <>BDC (This is chosen to represent a typical airline)Tj 9 0 0 9 232.438 324.8898 Tm BT EFVU(eufv7GWgw8HXhx)9IYiy*:JZjz m !1AQa"q2#BRbr3$4CS%cs5DT <>stream
ET (35,112)Tj W* n EMC (aircraft variants on 14 sectors departing)Tj BT /OC /MC5086 BDC BT /P <>BDC EMC EMC 7 0 0 7 508.4124 287.7654 Tm EMC /P <>BDC BT EMC EMC Fully loaded, the jet can fly up to 3,159 miles without refueling. EMC 9 0 0 9 544.0105 258.8898 Tm /P <>BDC BT BT 737-600/-700/-800/-900 without densitometer: [(CFM L)17.1(E)-8.1(AP-1A26)]TJ 0 Tc ( )Tj (379)Tj BT 9 0 0 9 394.0123 335.8898 Tm 9 0 0 9 215.433 225.8898 Tm /F1 1 Tf 9 0 0 9 376.0986 324.8898 Tm (1,920)Tj 7 0 0 7 539.8962 595.9528 Tm /P <>BDC -.02 Tc 9 0 0 9 370.891 302.8898 Tm BT BT /P <>BDC ET BT /P <>BDC ET ( )Tj BT 7 0 0 7 355.3163 210.7654 Tm /P <>BDC 0 Tc EMC ET ( )Tj (7B27B3)Tj EMC (737-800 results in a fuel cost per ASM that)Tj EMC ( )Tj BT 10 0 0 10 50.1204 814.1973 Tm BT ( )Tj 7 0 0 7 294.4014 89.7654 Tm 9 0 0 9 373.708 181.8898 Tm Hi. /F6 1 Tf ET BT /P <>BDC ( )Tj ( )Tj BT EMC BT 9 0 0 9 36.8583 335.8898 Tm (56,869)Tj EMC 0 Tc BT EMC 7 0 0 7 187.0858 133.9528 Tm 6.5 0 0 6.5 328.6662 585.9529 Tm EMC -.02 Tc BT ( )Tj EMC ET 6.5 0 0 6.5 332.6961 735.9529 Tm ET /P <>BDC [(AIRL)8.1(INE & AIR)7.1(CRAF)-12.9(T)18.1( OPERA)56.9(T)-8.1(ION)-13.9(S)]TJ BT BT ET (BOS-DEN)Tj (141,270)Tj /P <>BDC (total cost for fuel burn, time-related costs,)Tj ET ( )Tj thank you for stopping by. EMC 7 0 0 7 193.1059 188.9528 Tm -.07 Tc 7 0 0 7 386.3929 573.9528 Tm (A320ceo)Tj ET EMC BT 9 0 0 9 36.8504 192.8898 Tm ET (24)Tj ( )Tj EMC EMC 169 0 obj /P <>BDC EMC ( )Tj /P <>BDC ET ET ET BT BT 7 0 0 7 554.7883 243.7654 Tm 7 0 0 7 518.3203 430.9528 Tm (39,270)Tj /P <>BDC ET BT /P <>BDC EMC /P <>BDC EMC BT BT BT BT 9 0 0 9 246.6113 247.8898 Tm 10 0 0 10 422.8 814.1973 Tm EMC (31,416)Tj /P <>BDC EMC /P <>BDC ( )Tj BT ( )Tj -.02 Tc /P <>BDC /P <>BDC 9 0 0 9 182.7142 247.8898 Tm 7 0 0 7 230.7317 573.9528 Tm BT EMC /P <>BDC /F7 1 Tf 19.843 0 l ( )Tj /P <>BDC EMC /P <>BDC EMC ( )Tj ET /P <>BDC 7 0 0 7 535.5029 320.7654 Tm ET /P <>BDC 7 0 0 7 539.8962 496.9528 Tm EMC EMC EMC ET EMC (44,121)Tj (on the A320ceo to 11.0:1 on the A320neo. ET ( )Tj ( )Tj ET EMC ET BT EMC ( )Tj (2,517)Tj /F4 1 Tf ET 8 0 0 8 334.994 619.9528 Tm EMC BT EMC ( )Tj BT /P <>BDC ET ( )Tj EMC EMC This maybe? 0 Tc /P <>BDC ET endobj (BOS, and take 10 minutes to taxi in at all)Tj /P <>BDC 9 0 0 9 368.2199 247.8898 Tm EMC EMC /P <>BDC EMC BT ET 377.677 0 0 271.254 -.32779 534.078 cm /P <>BDC (170)Tj ET ( )Tj /P <>BDC EMC BT /P <>BDC /P <>BDC EMC BT BT ET 0 Tc 9 0 0 9 374.887 346.8898 Tm /P <>BDC /P <>BDC EMC /P <>BDC ET 6.5 0 0 6.5 426.4819 702.9529 Tm ET ET /P <>BDC 7 0 0 7 444.737 243.7654 Tm /P <>BDC ET (CFM56-5B3/P)Tj BT 8 0 0 8 256.0704 717.9528 Tm 7 0 0 7 37.6993 364.9528 Tm ( )Tj /P <>BDC /P <>BDC ( )Tj ET /P <>BDC 0 Tc EMC BT 0 Tc ET (and Boeing aircraft benefit from the)Tj 9 0 0 9 215.4313 434.8898 Tm (generated per route. BT EMC EMC ET BT (0.0132)Tj ET 9 0 0 9 229.6045 390.8898 Tm 7 0 0 7 241.2727 265.9528 Tm /P <>BDC 7 0 0 7 241.5317 606.9528 Tm 6 0 0 6 555.6477 729.9528 Tm ET /P <>BDC BT EMC /P <>BDC /P <>BDC BT Q BT ( )Tj ( )Tj EMC BT 7 0 0 7 508.4124 617.7654 Tm ET /P <>BDC 7 0 0 7 535.5029 188.7654 Tm 9 0 0 9 232.4217 434.8898 Tm 0 Tc EMC EMC 13 0 0 13 530.7245 434.8898 Tm EMC 7 0 0 7 430.039 639.9528 Tm ET ET -.02 Tc ET In November 2005, Boeing unveiled the BBJ3, based on the 737-900ER. [(CFM L)17.1(E)-8.1(AP-1B27)]TJ /P <>BDC ET /F4 1 Tf ( )Tj EMC 7 0 0 7 337.9444 617.9528 Tm EMC EMC EMC 7 0 0 7 440.3636 540.9528 Tm EMC ET 9 0 0 9 369.7648 346.8898 Tm EMC Calculates enroute fuel burn based on cruise altitude and trip distance. BT BT ( )Tj BT BT EMC 7 0 0 7 518.4953 397.9528 Tm 0 J 0 j .5 w 10 M [] 0 d EMC ( )Tj BT 0 Tc ( )Tj EMC ( )Tj ( )Tj (404)Tj (A320neos 7,000lbs higher MTOW. BT /P <>BDC 7 0 0 7 365.035 617.9528 Tm -.02 Tc ET (/S)Tj EMC BT BT EMC /P <>BDC BT BT /P <>BDC 9 0 0 9 53.8338 390.8898 Tm ET /P <>BDC BT (112)Tj 7 0 0 7 158.74 408.7654 Tm BT .023 .567 .626 RG aircraft ( )Tj /F4 1 Tf BT The Boeing 737-700 is together with the 737-600, 737-800 and 737-900 member of the 737-Next Generation-Family. BT /P <>BDC (136)Tj (170)Tj EMC 7 0 0 7 53.8582 650.7654 Tm (to allow a clearer performance and fuel)Tj ( )Tj 7 0 0 7 366.0641 661.9528 Tm (379)Tj (31,416)Tj ET The 737-200 had BT 9 0 0 9 540.3981 588.8898 Tm /P <>BDC BT ET ET /P <>BDC EMC 7 0 0 7 554.7883 474.7654 Tm 9 0 0 9 53.8338 401.8898 Tm /P <>BDC ET EMC /P <>BDC The website has also a photo gallery and gives you an overview of all aviation museums worldwide. Limitations: Max fuel temp +49C, Min ET (A320ceo:)Tj -.02 Tc BT BT 7 0 0 7 403.478 364.7654 Tm 0 Tc 6.5 0 0 6.5 532.7606 598.9529 Tm (0.0141)Tj /P <>BDC 9 0 0 9 389.6888 203.8898 Tm EMC -.02 Tc ET -.02 Tc EMC 7 0 0 7 537.7804 199.9528 Tm ET 9 0 0 9 394.0157 247.8898 Tm /P <>BDC EMC BT 7 0 0 7 535.5029 122.7654 Tm 9 0 0 9 53.8578 236.8898 Tm BT /P <>BDC 7 0 0 7 337.4684 694.9528 Tm /P <>BDC /P <>BDC EMC EMC ET EMC 7 0 0 7 456.2165 375.7654 Tm 9 0 0 9 163.2471 269.8898 Tm ET 7 0 0 7 387.0932 188.9528 Tm /P <>BDC BT 6 0 0 6 226.1079 659.9528 Tm BT /P <>BDC Boeing 737 Max, a new generation of this highly successful City Jet. BT 9 0 0 9 53.8582 511.8898 Tm 5.25 0 0 5.25 515.3989 11.5129 Tm 5.25 0 0 5.25 525.4061 11.5132 Tm 7 0 0 7 199.5784 496.7654 Tm EMC ET 9 0 0 9 36.8583 434.8898 Tm BT 9 0 0 9 51.0236 60.8898 Tm ET ( )Tj 0 Tc ( C)Tj 6 0 0 6 319.5607 715.9528 Tm EMC (148,504)Tj 6 0 0 6 459.5796 729.9528 Tm Hi I was just wondering where you got this data from. ET BT 9 0 0 9 394.0237 456.8898 Tm 8 0 0 8 76.6837 661.9528 Tm ( N)Tj ET EMC ET ET EMC EMC BT ET 7 0 0 7 99.5912 507.9528 Tm -.02 Tc /P <>BDC BT BT /P <>BDC ET 7 0 0 7 457.0984 243.7654 Tm /F6 1 Tf (alternates used and their distance from the)Tj ( )Tj EMC (1,060)Tj ET ( )Tj 9 0 0 9 215.433 280.8898 Tm BT BT Boeings main competitor is with Airbus. BT EMC ( The reserve fuel policy )Tj EMC Vmo/Mmo Velocity/Mach Maximum Operating speed. BT BT ET EMC EMC /P <>BDC BT (fuel consumption and cost per seat or per)Tj EMC ( )Tj ET ET For the purposes of)Tj BT BT ( )Tj ( )Tj ET EMC /P <>BDC BT ET ( )Tj ET EMC /P <>BDC ( )Tj /P <>BDC /P <>BDC ( )Tj EMC 6.5 0 0 6.5 243.8814 689.9529 Tm 0 Tc )Tj ET S ET /P <>BDC EMC 7 0 0 7 37.6993 111.9528 Tm Because of ET 7 0 0 7 337.6855 397.9528 Tm BT -.02 Tc (optimum cruise altitude. I cannot find any more information anywhere, but if I stumble across it, I will be sure to post it! ( )Tj EMC BT /P <>BDC ET (A)Tj ( )Tj BT EMC 9 0 0 9 252.5189 181.8898 Tm 0 Tc /P <>BDC -.02 Tc ( )Tj ET EMC /F6 1 Tf BT BT /P <>BDC BT ET ET ET EMC ( )Tj BT (170)Tj BT EMC /P <>BDC 9 0 0 9 53.8582 456.8898 Tm EMC 7 0 0 7 99.8582 210.7654 Tm /P <>BDC EMC (209)Tj BT 7 0 0 7 439.7405 705.9528 Tm On the)Tj EMC ( )Tj EMC /P <>BDC BT EMC BT /OC /MC171 BDC /P <>BDC BT 0 Tc BT /P <>BDC ( )Tj 0 Tc ( )Tj 9 0 0 9 180.5261 423.8898 Tm (weights used are an MTOW of)Tj ET 9 0 0 9 188.3303 181.8898 Tm EMC 0 Tc /P <>BDC /P <>BDC EMC /P <>BDC /P <>BDC EMC /P <>BDC /P <>BDC ( )Tj EMC /P <>BDC EMC /P <>BDC (. ][F$, c;9M$
C[\SU~s#4B#g"DH V6S[_t099J'Nbqur((h\Yf'urV(nYYW6V*f]+ 7 0 0 7 82.8504 243.9528 Tm 9 0 0 9 394.0237 434.8898 Tm 7 0 0 7 337.7614 111.7654 Tm /P <>BDC BT The Boeing 737-800 has a maximum fuel capacity of 6,875 gallons or 26,020 liters. ( )Tj /P <>BDC 0 Tc BT ( )Tj ET ( )Tj 0 Tc BT BT 7 0 0 7 387.0159 727.9528 Tm BT 9 0 0 9 270.2513 93.8898 Tm ( )Tj (To enable a comparison of the different)Tj 6 0 0 6 371.6897 659.9528 Tm BT ET BT BT ET 9 0 0 9 569.7076 148.8898 Tm BT EMC /P <>BDC EMC (150)Tj 6 0 0 6 466.3124 715.9528 Tm ET 9 0 0 9 179.7604 159.8898 Tm ET 7 0 0 7 277.3936 177.9528 Tm BT 8 0 0 8 187.3427 745.9528 Tm EMC -.02 Tc 9 0 0 9 214.7728 247.8898 Tm BT ( )Tj 1 1 1 rg BT -.02 Tc 7 0 0 7 343.2355 529.7654 Tm BT EMC /P <>BDC /P <>BDC BT ET ET ET /P <>BDC /P <>BDC BT (900ER\(W\) are the only aircraft in the)Tj ( )Tj 0 Tc [(CFM L)17.1(E)-8.1(AP-1A26)]TJ /GS1 gs /GS1 gs (217)Tj EMC 7 0 0 7 297.632 540.9528 Tm ET -.02 Tc 0 Tc BT /P <>BDC EMC [(CFM L)17.1(E)-8.1(AP-1A32)]TJ /P <>BDC /P <>BDC ET ET EMC BT BT .151 .147 .15 rg ( )Tj ( )Tj ET -.02 Tc (136)Tj ( )Tj ( )Tj ET BT ( )Tj -.02 Tc /P <>BDC ( )Tj 9 0 0 9 539.9583 236.8898 Tm BT BT ET Hello, do you know the meaning of the 737-8K5 designation and its background? (I)Tj 0 Tc ET ET (2,732)Tj -.02 Tc ET ( )Tj EMC ET BT BT (0.0123)Tj /F6 1 Tf /P <>BDC 7 0 0 7 141.7322 309.9528 Tm BT BT /P <>BDC EMC ( )Tj /P <>BDC BT ( )Tj 7 0 0 7 539.8962 529.9528 Tm ET (the CFM LEAP-1A32 variant. 7 0 0 7 279.1575 199.9528 Tm 5.25 0 0 5.25 492.6848 11.5129 Tm BT 9 0 0 9 550.1644 170.8898 Tm /P <>BDC (31,416)Tj .151 .147 .15 RG ET /P <>BDC (Like the A321neo, the 737-9 has a)Tj 0 Tc -.02 Tc /P <>BDC (150)Tj ( )Tj cumulative errors it is recommended that the wings are filled once every few ET ( )Tj 9 0 0 9 394.0123 126.8898 Tm /P <>BDC ET BT ET ET ET EMC BT ET BT /P <>BDC 6 0 0 6 409.8614 771.9528 Tm wheel well - NG's only. BT ET 7 0 0 7 86.3128 540.7654 Tm EMC ( )Tj [(A3)24.9(20ceo & A3)24.9(20neo )]TJ 9 0 0 9 553.5856 467.8898 Tm (5.1:1)Tj illuminated is not only an explosion risk (see Thai and Philippine write offs) The AFM limits are higher, but not normally achievable with standard SG's. BT EMC [(ar)-22.9(ticles like this, visit: )]TJ /P <>BDC EMC 6 0 0 6 465.8383 673.9528 Tm EMC /F6 1 Tf BT 0 Tc EMC 9 0 0 9 377.8897 291.8898 Tm /P <>BDC 9 0 0 9 232.4217 588.8898 Tm /P <>BDC EMC 0 Tc /P <>BDC ( )Tj BT [(UG)-17.1(U)-8(S)8.1(T)]TJ /P <>BDC ( )Tj /P <>BDC ET 6.5 0 0 6.5 531.9417 637.9529 Tm EMC ET EMC ET BT EMC /P <>BDC ( )Tj EMC /P <>BDC 9 0 0 9 530.7301 59.9073 Tm 6.5 0 0 6.5 76.9446 715.9529 Tm ET ET EMC ( )Tj ET /GS2 gs BT /P <>BDC BT 7 0 0 7 294.4014 287.7654 Tm ET BT /P <>BDC (A)Tj The classics have 5 dripsticks in each wing tank and none in the centre /P <>BDC /P <>BDC 9 0 0 9 73.1083 489.8898 Tm 9 0 0 9 187.813 126.8898 Tm /P <>BDC ( )Tj 7 0 0 7 404.101 386.7654 Tm BT /P <>BDC EMC BT EMC BT BT /P <>BDC ( )Tj 7 0 0 7 507.7893 485.7654 Tm 7 0 0 7 445.619 485.7654 Tm ET 0 Tc /P <>BDC The BBJ is based on the 737-700 airliner and the BBJ2 on the 737-800. EMC ET 6.5 0 0 6.5 433.3069 585.9529 Tm BT BT EMC ET BT /GS2 gs EMC /P <>BDC ET ET ET ET (I)Tj /OC /MC2 BDC BT (ASM. EMC ET BT BT /P <>BDC (capacity and potentially improved)Tj ET EMC /P <>BDC BT -.02 Tc /P <>BDC ( )Tj 7 0 0 7 258.2805 441.7654 Tm 9 0 0 9 394.0315 720.8898 Tm (1A32)Tj 7 0 0 7 296.1653 100.7654 Tm BT 7 0 0 7 130.1443 221.7654 Tm [(OM)8(M)-13(E)-25(R)7(C)8(E)]TJ 9 0 0 9 53.8578 82.8898 Tm BT EMC 7 0 0 7 54.7071 320.7654 Tm ET FQIS accuracy: +/- 3.0% ET BT -.02 Tc BT ET /P <>BDC 7 0 0 7 520.6108 496.9528 Tm BT [(W)7.1(ind component - kts)]TJ ET /P <>BDC 0 Tc EMC 9 0 0 9 232.4217 225.8898 Tm EMC (208-217)Tj /P <>BDC EMC 9 0 0 9 562.507 203.8898 Tm -.01 Tc 7 0 0 7 337.6855 210.9528 Tm EMC EMC /P <>BDC to the centre tank through a manual valve by cabin pressure. BT EMC /P <>BDC /P <>BDC ET ET EMC The 737-8 offers)Tj BT BT /P <>BDC BT 9 0 0 9 394.0237 258.8898 Tm 0 Tw 9 0 0 9 394.0157 346.8898 Tm The 737 fuel quantity indication system has the following accuracy tolerances: 737-100/-200: 7 0 0 7 337.9444 606.9528 Tm 9 0 0 9 543.4875 456.8898 Tm /F4 1 Tf After /P <>BDC 9 0 0 9 53.8582 665.8898 Tm 9 0 0 9 232.438 346.8898 Tm -.02 Tc /P <>BDC BT (136)Tj EMC 7 0 0 7 387.0932 67.9528 Tm 9 0 0 9 551.0194 588.8898 Tm /P <>BDC ET 8 0 0 8 516.0245 775.8898 Tm BT BT ET EMC EMC BT ET ET 9 0 0 9 185.3513 159.8898 Tm EMC ( )Tj 7 0 0 7 474.7064 166.9528 Tm /P <>BDC BT BT /P <>BDC ET EMC )Tj ET 7 0 0 7 158.74 529.7654 Tm -.02 Tc /P <>BDC ( )Tj ET ET -.02 Tc EMC EMC ET ( )Tj /P <>BDC ET EMC BT EMC BT /F6 1 Tf 6 0 0 6 290.3132 659.9528 Tm 9 0 0 9 390.2557 511.8898 Tm EMC EMC 7 0 0 7 230.7317 397.9528 Tm EMC EMC 7 0 0 7 403.478 496.7654 Tm /P <>BDC EMC EMC 7 0 0 7 230.7317 122.9528 Tm 7 0 0 7 37.6993 276.9528 Tm (/S)Tj .151 .147 .15 rg BT ET [(CFM L)17.1(E)-8.1(AP-1A32)]TJ /P <>BDC /P <>BDC ( )Tj EMC /P <>BDC BT 0 Tc EMC ET ET /P <>BDC BT /P <>BDC -.01 Tc EMC /P <>BDC BT /P <>BDC 7 0 0 7 82.8504 199.9528 Tm After BT EMC 9 0 0 9 529.8783 621.8898 Tm ET (A321neo)Tj ET 0 Tc ET 7 0 0 7 326.2278 705.9528 Tm /P <>BDC /P <>BDC /P <>BDC ET 7 0 0 7 487.0872 11.5129 Tm BT ET BT /P <>BDC /P <>BDC 28.5749 0 TD /P <>BDC 7 0 0 7 187.0858 309.9528 Tm ( )Tj /P <>BDC BT EMC EMC (The A320neo offers a significant)Tj /P <>BDC /P <>BDC EMC EMC ET BT BT 0 Tc ET /P <>BDC 7 0 0 7 37.6993 133.9528 Tm (doors configuration. ET 7 0 0 7 456.2165 265.7654 Tm Q EMC -.01 Tc ET BT ET 9 0 0 9 79.8339 522.8898 Tm (International Aero Engines V2527-A5)Tj EMC ET EMC EMC ET 7 0 0 7 508.6712 133.7654 Tm 7 0 0 7 82.8504 430.9528 Tm EMC (82,110)Tj EMC BT ( )Tj /P <>BDC 7 0 0 7 554.7883 727.7654 Tm BT /P <>BDC 6.5 0 0 6.5 477.8064 676.9529 Tm EMC EMC /P <>BDC /P <>BDC EMC /P <>BDC /P <>BDC supplied to the center wing tank and the oxygenenriched air (OEA) is vented 7 0 0 7 124.1242 496.7654 Tm ET EMC /Artifact <>BDC ET 9 0 0 9 392.5128 236.8898 Tm /P <>BDC 9 0 0 9 373.9458 159.8898 Tm EMC 9 0 0 9 229.6064 126.8898 Tm /P <>BDC 9 0 0 9 232.4217 511.8898 Tm EMC 0 Tc BT ET ET ET /P <>BDC BT -.02 Tc 7 0 0 7 187.0858 661.9528 Tm 7 0 0 7 362.3891 265.9528 Tm /P <>BDC ET ET /P <>BDC /P <>BDC BT EMC (976)Tj ET EMC EMC BT The Boeing 737-800 is an example of an average sized airplane. BT 7 0 0 7 386.4701 408.9528 Tm /TT2 1 Tf (136)Tj 6 0 0 6 561.1918 715.9528 Tm BT EMC /P <>BDC /P <>BDC /P <>BDC /P <>BDC EMC 0 Tc EMC (load factor to provide a better evaluation)Tj )]TJ 8 0 0 8 355.1264 760.7654 Tm ET ET EMC ET EMC /P <>BDC automatically shut off when they detect a low output pressure and there have EMC 7 0 0 7 258.2805 122.7654 Tm /F4 1 Tf 7 0 0 7 88.196 11.5129 Tm /P <>BDC /P <>BDC BT (variant used in this study is the CFM)Tj 6.5 0 0 6.5 227.9655 565.9529 Tm /P <>BDC ( )Tj Z{V ud1i9gq/+ /P <>BDC This from the FAA Systems ET /P <>BDC ET /P <>BDC ( )Tj 7 0 0 7 539.8962 573.9528 Tm /P <>BDC BT EMC (0.0113)Tj -.01 Tc Hi All, BT ET 7 0 0 7 247.7395 518.7654 Tm EMC BT /P <>BDC 0 Tc 0 Tc BT ET /P <>BDC /P <>BDC BT EMC /Artifact <>BDC /P <>BDC /P <>BDC [(AIRL)8.1(INE & AIR)7.1(CRAF)-12.9(T)18.1( OPERA)56.9(T)-8.1(ION)-13.9(S)]TJ /Artifact <>BDC BT (operation the overflight and airport)Tj /P <>BDC EMC ET ET ET 9 0 0 9 53.8338 49.8898 Tm (35,112lbs)Tj /P <>BDC EMC /P <>BDC BT EMC -2.4549 -3.9026 m 7 0 0 7 365.035 100.9528 Tm The Boeing 737-800 is a twin-engined short-to-medium-range narrowbody airliner with a capacity of maximum 189 passengers produced by the American manufacturer Boeing Commercial Airplanes. ( )Tj 6 0 0 6 226.9834 715.9528 Tm /P <>BDC ET BT ET ( )Tj BT ET ( )Tj /P <>BDC /P <>BDC ET 9 0 0 9 388.7779 38.8898 Tm (356-369)Tj /P <>BDC 7 0 0 7 294.4014 144.7654 Tm 9 0 0 9 388.6428 357.8898 Tm /P <>BDC (0.0183)Tj ET ET 7 0 0 7 247.7395 144.7654 Tm ET (Block time)Tj 0 Tc -.02 Tc 0 Tc EMC 8 0 0 8 136.8677 745.9528 Tm 7 0 0 7 247.7395 441.7654 Tm ET 7 0 0 7 258.2805 89.7654 Tm /P <>BDC EMC 9 0 0 9 342.6025 368.8898 Tm ET /F1 1 Tf ( )Tj BT EMC ET EMC 10 0 0 10 408.34 814.1973 Tm endobj /P <>BDC /P <>BDC 6.5 0 0 6.5 499.597 624.9529 Tm BT ( )Tj EMC EMC (CFM56-7B26)Tj -.02 Tc -.02 Tc BT BT BT /P <>BDC /P <>BDC /P <>BDC 7 0 0 7 439.9995 694.9528 Tm 9 0 0 9 389.1758 522.8898 Tm 7 0 0 7 379.3969 188.7654 Tm ET ET EMC /P <>BDC (32,000lbs of thrust, a fan diameter of 78)Tj ET 9 0 0 9 560.5186 214.8898 Tm ET ET EMC BT EMC BT (150)Tj EMC /P <>BDC 7 0 0 7 131.6494 265.7654 Tm EMC ET BT ET 9 0 0 9 394.0157 126.8898 Tm (CFM56-)Tj EMC BT EMC 7 0 0 7 537.7804 221.9528 Tm -.02 Tc /P <>BDC The reductions in fuel burn also)Tj
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