EMC -.02 Tc BT ET EMC EMC BT BT /P <>BDC ( )Tj (. ET BT ET (977)Tj 6 0 0 6 357.8844 701.9528 Tm /P <>BDC /P <>BDC (136)Tj /P <>BDC 7 0 0 7 338.3085 298.9528 Tm ( )Tj ET 10 0 0 10 408.1099 814.1973 Tm BT EMC /F6 1 Tf -.005 Tc Versions / Variants There are many variants of the 737. (178-187)Tj /P <>BDC EMC BT ( )Tj 8 0 0 8 266.591 745.9528 Tm (65,688)Tj (A US domestic reserve policy was)Tj 7 0 0 7 130.1443 221.7654 Tm /P <>BDC (136)Tj 7 0 0 7 362.3891 199.9528 Tm BT /P <>BDC BT ET ET /P <>BDC EMC /P <>BDC EMC [(MR)32(TX - lbs)]TJ The system tolerance is then +/- 200 KG at any fuel level within the tank. BT BT It sounds like you have a bit of a project on your hands. BT EMC ET /F1 1 Tf ET EMC 9 0 0 9 170.6722 104.8898 Tm ET ET /P <>BDC 7 0 0 7 299.0601 441.9528 Tm ET -.015 Tc ET -.02 Tc ET All the aircraft would therefore)Tj 9 0 0 9 36.8504 478.8898 Tm BT 7 0 0 7 444.737 144.7654 Tm /P <>BDC 6.5 0 0 6.5 346.5844 735.9529 Tm BT 9 0 0 9 552.6437 434.8898 Tm 13 0 0 13 186.9936 588.8898 Tm 7 0 0 7 241.2727 144.9528 Tm (range for both the A320ceo and A320neo. ( )Tj BT BT EMC Because of (170)Tj -.02 Tc This is the same)Tj ET BT EMC /P <>BDC /P <>BDC (47,000)Tj ET /P <>BDC The BBJ is based on the 737-700 airliner and the BBJ2 on the 737-800. The 1/200's had heater switches; these used bleed air to heat the BT 5.25 0 0 5.25 515.3989 11.5129 Tm -.02 Tc .151 .147 .15 rg BT /P <>BDC EMC /P <>BDC /P <>BDC EMC BT BT BT 9 0 0 9 394.0315 368.8898 Tm 0 Tc BT ET 7 0 0 7 520.6108 628.9528 Tm 6.5 0 0 6.5 128.6016 558.9529 Tm -.02 Tc ( )Tj 0 Tc EMC BT ET BT -.02 Tc ET (136)Tj BT ( )Tj 9 0 0 9 215.4409 379.8898 Tm EMC BT /P <>BDC 9 0 0 9 371.6638 247.8898 Tm /P <>BDC EMC 0 Tc ET /P <>BDC ET /P <>BDC /Artifact <>BDC 7 0 0 7 279.1575 529.9528 Tm ET 7 0 0 7 247.7395 639.7654 Tm EMC EMC EMC ( )Tj /P <>BDC BT EMC ET 7 0 0 7 259.1625 199.7654 Tm 9 0 0 9 375.9258 49.8898 Tm BT [(7)-33(3)8.1(7-900ER\(W)-19(\) v)12.9(ersus 7)-33(3)8.1(7-9 )]TJ 9 0 0 9 394.0123 654.8898 Tm /P <>BDC 7 0 0 7 490.8321 309.7654 Tm ET EMC ET /P <>BDC ET EMC ( )Tj This would make)Tj BT EMC BT /P <>BDC ET (120-128)Tj /P <>BDC 9 0 0 9 68.3339 511.8898 Tm /P <>BDC BT ( )Tj 6 0 0 6 215.4988 701.9528 Tm (makes a flight-for-flight comparison)Tj ( )Tj ( )Tj .023 .567 .626 RG EMC 7 0 0 7 439.9995 694.9528 Tm 7 0 0 7 199.3614 100.7654 Tm /P <>BDC 9 0 0 9 215.4409 104.8898 Tm ET /P <>BDC ET 7 0 0 7 124.1242 100.7654 Tm -.02 Tc BT Boeing made BT -.02 Tc /P <>BDC The total capacity is 526 seats broken down to 162 first class seats, 175 business class and 189 economy seats. ET ET -.02 Tc BT /P <>BDC BT ( )Tj ET /P <>BDC BT BT 851 0 obj 0 Tc ET ET ET BT /P <>BDC ET ET ET BT EMC /P <>BDC /P <>BDC [(C)17.1(OS/104)]TJ 7 0 0 7 316.0679 287.7654 Tm ( )Tj 7 0 0 7 404.101 331.7654 Tm 10 0 0 10 47.1144 814.1973 Tm /P <>BDC EMC ( The wind component and)Tj /P <>BDC 6 0 0 6 268.0069 701.9528 Tm 6.5 0 0 6.5 276.4014 637.9529 Tm BT 9 0 0 9 357.6917 192.8898 Tm /P <>BDC /P <>BDC ( )Tj 6.5 0 0 6.5 191.63 624.9529 Tm -.01 Tc -.02 Tc ET /P <>BDC EMC /P <>BDC (150)Tj EMC EMC 28.5749 0 TD /P <>BDC -.02 Tc 9 0 0 9 553.6047 423.8898 Tm ( )Tj EMC ET 0 Tc BT BT ET BT 9 0 0 9 192.0203 313.8898 Tm /P <>BDC EMC EMC EMC 7 0 0 7 204.0935 584.7654 Tm ( )Tj 9 0 0 9 129.4781 489.8898 Tm ET ( )Tj ( )Tj BT EMC 7 0 0 7 241.5317 617.9528 Tm 7 0 0 7 364.1531 166.9528 Tm BT 9 0 0 9 36.8504 324.8898 Tm BT EMC BT /P <>BDC 9 0 0 9 53.8582 786.8898 Tm [(F)-21(LL/47)]TJ EMC (16,268)Tj 9 0 0 9 394.0123 500.8898 Tm 9 0 0 9 215.4409 357.8898 Tm ET -.01 Tc BT /P <>BDC /P <>BDC 7 0 0 7 380.2788 540.7654 Tm (CFM56-7B27B3)Tj ET /OC /MC27 BDC EMC ET EMC In reality, most models will operate in a combination of classes. BT (types )Tj BT BT /P <>BDC )]TJ EMC EMC EMC 6 0 0 6 352.5857 659.9528 Tm 9 0 0 9 161.2491 126.8898 Tm ET BT BT 6 0 0 6 130.4965 771.9528 Tm ET 515.808 82.238 l 7 0 0 7 337.9444 100.9528 Tm BT BT EMC ( )Tj EMC 9 0 0 9 166.1068 313.8898 Tm EMC ( )Tj ( )Tj (176)Tj /GS2 gs ( )Tj ( )Tj BT 7 0 0 7 187.0858 606.9528 Tm 0 Tc ET 0 Tc ET EMC EMC ( )Tj /P <>BDC 7 0 0 7 554.7883 507.7654 Tm ET 9 0 0 9 182.8403 93.8898 Tm EMC 9 0 0 9 68.031 170.8898 Tm BT 7 0 0 7 113.1366 122.9528 Tm ET ET (34,650)Tj 7 0 0 7 387.0159 661.9528 Tm /P <>BDC 7 0 0 7 363.2711 507.9528 Tm /P <>BDC ET 8 0 0 8 43.6039 619.9528 Tm EMC Boeing 797, MNA-6x and MNA-7x. /P <>BDC EMC 9 0 0 9 53.8582 269.8898 Tm 5.25 0 0 5.25 515.3989 11.5129 Tm ( )Tj /P <>BDC BT -.02 Tc /P <>BDC BT ET BT ET BT 7 0 0 7 491.4046 298.9528 Tm -.02 Tc 0 Tc ET ET EMC ET 0 Tc BT ( )Tj ET /GS2 gs BT EMC (310,080)Tj ( )Tj ET EMC 7 0 0 7 535.5029 243.7654 Tm -.02 Tc /P <>BDC 0 Tc (ranges from 0.47 to 0.33 cents, and is)Tj EMC 7 0 0 7 247.7395 463.7654 Tm ET /P <>BDC /P <>BDC EMC EMC ET 6 0 0 6 412.4713 715.9528 Tm EMC EMC EMC 7 0 0 7 279.1575 738.9528 Tm During cruise, the tolerance is less than 1.5%. BT EMC 9 0 0 9 181.6136 456.8898 Tm 7 0 0 7 539.8962 639.9528 Tm BT ET ET ET EMC aircraft BT EMC ET /P <>BDC EMC ( )Tj BT BT (BOS-PHX)Tj (1,058)Tj EMC 9 0 0 9 215.4313 346.8898 Tm ET EMC 9 0 0 9 232.438 423.8898 Tm This)Tj 7 0 0 7 158.74 617.7654 Tm 6 0 0 6 466.3723 701.9528 Tm /P <>BDC ( )Tj 9 0 0 9 232.4217 390.8898 Tm EMC EMC BT EMC BT EMC 7 0 0 7 496.3063 727.7654 Tm ET EMC EMC EMC <>/ExtGState<>/Properties<>>> 9 0 0 9 53.8582 313.8898 Tm EMC 6.5 0 0 6.5 375.6529 676.9529 Tm EMC ET <>/XObject<>/ExtGState<>/Properties<>>> /P <>BDC /P <>BDC /P <>BDC /P <>BDC BT /P <>BDC EMC Note: The gauges are still considered to be operating normally with /P <>BDC 9 0 0 9 394.0157 115.8898 Tm /P <>BDC (0.0141)Tj EMC [(AS)29(M)21(s)]TJ (78,729)Tj BT /P <>BDC 9 0 0 9 408.1854 566.8898 Tm ET (In this comparison, the A321neo)Tj 7 0 0 7 491.4046 188.9528 Tm . 9 0 0 9 215.4313 280.8898 Tm 7 0 0 7 554.7883 463.7654 Tm 6 0 0 6 61.517 771.9528 Tm This is equivalent to)Tj ( )Tj /P <>BDC BT ET /P <>BDC ( )Tj BT BT 0 Tc EMC /P <>BDC ( )Tj 7 0 0 7 473.8245 144.9528 Tm 9 0 0 9 194.9081 346.8898 Tm /P <>BDC EMC /P <>BDC EMC ET 7 0 0 7 141.7322 727.9528 Tm BT /P <>BDC EMC 9 0 0 9 341.4411 247.8898 Tm 17 0 0 17 36.8606 742.1944 Tm ET ET ET BT ( )Tj EMC BT ET 7 0 0 7 491.4046 100.9528 Tm /P <>BDC 5 0 0 5 92.725 11.5132 Tm BT /P <>BDC 9 0 0 9 53.8578 104.8898 Tm /OC /MC1323 BDC )Tj 7 0 0 7 321.6356 210.9528 Tm 8 0 0 8 124.845 633.9528 Tm (136)Tj ET ET 0 Tc EMC EMC ET EMC BT 7 0 0 7 314.6398 474.7654 Tm 9 0 0 9 363.2032 478.8898 Tm /P <>BDC ET BT /P <>BDC /P <>BDC /P <>BDC /P <>BDC /P <>BDC BT EMC EMC 13 0 0 13 215.4409 60.8898 Tm /P <>BDC BT 9 0 0 9 53.8578 368.8898 Tm ET 6 0 0 6 403.5009 701.9528 Tm 9 0 0 9 43.6039 794.2914 Tm BT /P <>BDC ET ET ( )Tj /P <>BDC 0 Tc endobj 6 0 0 6 527.2669 729.9528 Tm ET 9 0 0 9 53.8582 654.8898 Tm /P <>BDC EMC EMC Additionally, below 10,000 feet it should not exceed 250 knots. 6 0 0 6 295.8268 673.9528 Tm ET EMC 9 0 0 9 36.8504 192.8898 Tm BT BT (0.0122)Tj BT /P <>BDC ET 786 0 obj BT 9 0 0 9 36.8504 269.8898 Tm ET ET EMC -.005 Tc BT BT (140-148)Tj <>/ExtGState<>/Properties<>>> W n BT EMC EMC EMC /F1 1 Tf (310,080)Tj ( )Tj ( )Tj BT ET EMC /P <>BDC ET /OC /MC171 BDC 9 0 0 9 36.8504 115.8898 Tm /P <>BDC 7 0 0 7 491.4046 320.9528 Tm ET (382,280)Tj ( )Tj EMC ( )Tj EMC BT EMC 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. BT /P <>BDC BT /P <>BDC /P <>BDC ET If you like us, please share with your followers. ET EMC 9 0 0 9 53.8578 159.8898 Tm BT ( )Tj BT EMC BT ( )Tj re-primed. BT /P <>BDC (31,416lbs)Tj BT 9 0 0 9 411.0097 357.8898 Tm ET BT (I)Tj 7 0 0 7 508.4124 122.7654 Tm ET EMC BT /GS1 gs /P <>BDC -.02 Tc /P <>BDC ( )Tj BT /P <>BDC 7 0 0 7 241.5317 287.9528 Tm 7 0 0 7 520.6108 595.9528 Tm /P <>BDC EMC /F4 1 Tf 7 0 0 7 536.3849 628.7654 Tm ET BT EMC EMC 7 0 0 7 508.6712 430.7654 Tm BT BT /P <>BDC ( )Tj 7 0 0 7 387.0159 584.9528 Tm ET -.02 Tc /P <>BDC BT ET -.02 Tc 9 0 0 9 363.052 357.8898 Tm /P <>BDC [(CFM L)17.1(E)-8.1(AP-1A26)]TJ /P <>BDC ( )Tj .964 .834 .406 rg EMC EMC /OC /MC5093 BDC EMC BT BT ( )Tj BT BT ET /P <>BDC EMC EMC EMC EMC ( )Tj BT 6.5 0 0 6.5 230.3055 722.9529 Tm ET /P <>BDC ET (1,622)Tj BT 7 0 0 7 490.8321 386.7654 Tm ET /P <>BDC (1,619)Tj EMC ET ET 7 0 0 7 60.6117 243.7654 Tm ET ET ET BT ET BT ET EMC ( A)Tj 7 0 0 7 473.8245 78.9528 Tm -.02 Tc /P <>BDC (2,731)Tj ET BT /P <>BDC EMC (5,277)Tj (performing better on the shorter sectors. (150)Tj ( )Tj ET /P <>BDC 7 0 0 7 519.3773 67.9528 Tm BT 6 0 0 6 371.479 715.9528 Tm ET 0 Tc EMC 7 0 0 7 299.0601 397.9528 Tm EMC 0 Tc EMC 9 0 0 9 232.4217 544.8898 Tm /P <>BDC EMC BT 9 0 0 9 535.511 379.8898 Tm BT 6.5 0 0 6.5 295.5027 624.9529 Tm /P <>BDC 0 Tc 0 Tc ET ( )Tj -.02 Tc /P <>BDC -.02 Tc 8 0 0 8 38.4438 745.9528 Tm BT -.02 Tc /GS2 gs /P <>BDC /P <>BDC ( )Tj EMC EMC (37,653lbs)Tj 9 0 0 9 394.0123 313.8898 Tm (152)Tj BT BT /P <>BDC 0 Tc EMC ET 0 Tc /P <>BDC /P <>BDC -.015 Tc (the A320neo in the 85% payload scenario. endstream -.02 Tc BT /P <>BDC BT 9 0 0 9 354.463 49.8898 Tm ( )Tj 6.5 0 0 6.5 489.7146 611.9529 Tm BT BT EMC /P <>BDC .151 .147 .15 rg /P <>BDC EMC 9 0 0 9 339.3695 192.8898 Tm 10 0 0 10 422.8 814.1973 Tm EMC EMC the two components of the air are separated, the nitrogenenriched air (NEA) is (6,353)Tj /P <>BDC EMC EMC 9 0 0 9 411.0234 742.8898 Tm ET (cents, with a network average)Tj /P <>BDC 7 0 0 7 114.6416 397.9528 Tm ET /P <>BDC 7 0 0 7 258.2805 573.7654 Tm ET 9 0 0 9 411.0234 698.8898 Tm EMC 7 0 0 7 456.2165 474.7654 Tm EMC EMC ( )Tj EMC 7 0 0 7 554.7883 210.7654 Tm EMC ET ET EMC /P <>BDC EMC ET ( )Tj It sports its powerful crew and passenger carrying abilities elegantly as it takes flight. 9 0 0 9 158.963 258.8898 Tm /Artifact <>BDC EMC -.02 Tc BT EMC EMC 8 0 0 8 181.9279 771.7654 Tm BT /P <>BDC 7 0 0 7 403.478 628.7654 Tm EMC Fuel burn in cruise for B737-800 is 5,511lbs/hr Fuel burn at idle of a CFM56 engine = 661lbs/hr, so for the half hour descent two engines burn through 661 Total fuel for a 2 hour flight is 16,753lbs 6 More answers below Teodor Negru Passioned about flight and the art of flying Author has 425 answers and 1.8M answer views 4 y 0 Tc /P <>BDC ET ET 1 i ( )Tj ET 0 Tc 9 0 0 9 550.4545 126.8898 Tm [(CFM L)17.1(E)-8.1(AP-1A32)]TJ /OC /MC186 BDC BT /F6 1 Tf ( )Tj 9 0 0 9 394.0123 269.8898 Tm -.02 Tc 9 0 0 9 515.4913 555.8898 Tm ET ( )Tj ( )Tj ET -.02 Tc 9 0 0 9 408.1968 236.8898 Tm EMC EMC ET 9 0 0 9 68.0071 423.8898 Tm EMC ET ( )Tj (0.0111)Tj BT -.02 Tc BT 0 Tc 6.5 0 0 6.5 76.9446 715.9529 Tm EMC BT (maximise their service offering. ( )Tj ( )Tj ET ( )Tj BT 7 0 0 7 141.7322 463.9528 Tm 7 0 0 7 554.7883 298.7654 Tm BT EMC ET EMC BT EMC 7 0 0 7 247.7395 199.7654 Tm BT BT /P <>BDC /P <>BDC EMC -.02 Tc EMC /P <>BDC ET EMC BT BT EMC EMC 9 0 0 9 411.0181 170.8898 Tm ET 7 0 0 7 364.1531 584.9528 Tm BT EMC ( )Tj BT /P <>BDC /P <>BDC -.02 Tc ET )Tj BT /P <>BDC .41 .161 .508 rg ET ET BT q EMC /P <>BDC BT BT (37,653)Tj /P <>BDC ET (0.0142)Tj ET [(737-900E)-33(R)]TJ /P <>BDC BT 7 0 0 7 294.4014 463.7654 Tm /P <>BDC 1 i EMC BT (2,431)Tj 7 0 0 7 321.6356 166.9528 Tm EMC (O)Tj BT 9 0 0 9 232.4217 203.8898 Tm EMC ET BT EMC /P <>BDC EMC BT 6 0 0 6 106.1775 729.9528 Tm BT /F1 1 Tf /P <>BDC EMC 7 0 0 7 37.0536 584.9528 Tm (160)Tj EMC ET BT EMC 7 0 0 7 537.7804 441.9528 Tm /P <>BDC ET (96,500)Tj 9 0 0 9 194.5132 38.8898 Tm (450,780)Tj will be centre fuel tank inerting. ( )Tj BT BT ET -.02 Tc BT (payload and route, and 16% higher than)Tj /P <>BDC BT ET EMC BT 7 0 0 7 387.0159 496.9528 Tm 7 0 0 7 82.8504 265.9528 Tm 6.5 0 0 6.5 430.0114 565.9529 Tm BT BT 0 Tc ET 7 0 0 7 439.2087 199.9528 Tm [(looks at the performance of eight Airbus and Boeing narr)10(o)12(wbody types)]TJ /P <>BDC ET The 800 shares a lineage with the 300, 400, and 500. (MTOW and OEW. (this evaluation. BT 6 0 0 6 278.4021 729.9528 Tm [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ /Artifact <>BDC /P <>BDC EMC BT 9 0 0 9 53.8578 137.8898 Tm EMC (typically based on the aircrafts certified)Tj BT EMC (737-9)Tj ( )Tj (1,995)Tj ET BT ( )Tj /P <>BDC /P <>BDC BT /P <>BDC ET (39,270)Tj EMC /P <>BDC /P <>BDC (comprehensive comparison of the aircraft)Tj EMC ET BT BT ET /P <>BDC ( )Tj EMC /P <>BDC EMC /P <>BDC EMC 9 0 0 9 372.2467 170.8898 Tm BT /P <>BDC 7 0 0 7 99.8582 584.7654 Tm EMC /P <>BDC Boeing 737 800 Hainan Airlines Alan Wilson. ET (163)Tj EMC 9 0 0 9 53.8582 236.8898 Tm EMC 8 0 0 8 474.6331 771.7654 Tm 6 0 0 6 481.8528 701.9528 Tm 0 Tc ( )Tj EMC ET ( )Tj ET 7 0 0 7 247.7395 133.7654 Tm EMC 7 0 0 7 158.74 276.7654 Tm EMC BT /P <>BDC ( )Tj ( )Tj /P <>BDC ET (A321ceo)Tj (0.0112)Tj EMC ( )Tj ET -.01 Tc /P <>BDC 9 0 0 9 215.4313 302.8898 Tm 7 0 0 7 386.3929 639.9528 Tm 9 0 0 9 194.7718 456.8898 Tm /P <>BDC ( )Tj /P <>BDC Just not sure how to access these. 7 0 0 7 507.7893 419.7654 Tm 6.5 0 0 6.5 54.877 650.9529 Tm BT ( C)Tj /P <>BDC EMC 7 0 0 7 294.4014 672.7654 Tm EMC BT EMC EMC 6 0 0 6 365.7265 729.9528 Tm ET /P <>BDC 0 Tc EMC [(BOS-Y)-50.1(YZ)]TJ BT BT ( )Tj EMC ET BT /P <>BDC ET /P <>BDC ( )Tj EMC -.02 Tc BT -.02 Tc tank. EMC EMC (157)Tj 10 0 0 10 312.5146 771.9528 Tm 9 0 0 9 117.7519 170.8898 Tm BT (burns. 7 0 0 7 354.6933 518.7654 Tm /P <>BDC /P <>BDC -.02 Tc ( )Tj ET /P <>BDC /P <>BDC /P <>BDC BT BT /P <>BDC ( )Tj /P <>BDC 9 0 0 9 411.0181 313.8898 Tm BT ET 7 0 0 7 277.3936 144.9528 Tm 7 0 0 7 403.478 419.7654 Tm (136)Tj 7 0 0 7 131.6494 309.7654 Tm 9 0 0 9 68.0314 335.8898 Tm BT /P <>BDC /P <>BDC EMC /P <>BDC BT EMC 6 0 0 6 309.3004 673.9528 Tm ( )Tj BT /P <>BDC BT BT EMC /P <>BDC EMC ( )Tj /P <>BDC ET EMC BT 0 Tc 7 0 0 7 314.6398 540.7654 Tm /P <>BDC BT ET EMC EMC ET /Artifact <>BDC ET BT ( )Tj EMC /P <>BDC ET /P <>BDC /P <>BDC /P <>BDC 9 0 0 9 188.8887 60.8898 Tm Aircraft have been NGS provisioned since l/n 1935 and it has been installed since l/n 2620 onwards. BT EMC /P <>BDC /P <>BDC (is 16/30/114, giving a maximum passenger)Tj EMC /P <>BDC ET BT EMC BT ( )Tj 9 0 0 9 362.6813 357.8898 Tm ET EMC ( )Tj (1,945)Tj 9 0 0 9 206.8496 346.8898 Tm ( )Tj ( )Tj BT ( )Tj W n ( )Tj (170)Tj 9 0 0 9 394.0315 544.8898 Tm (0.0133)Tj ET EMC EMC 7 0 0 7 338.6433 320.7654 Tm -.02 Tc EMC /P <>BDC ( )Tj ET EMC ET 6.5 0 0 6.5 330.4406 565.9529 Tm For ground /P <>BDC ET BT EMC /P <>BDC /P <>BDC ( )Tj 7 0 0 7 444.737 265.7654 Tm BT ET ET ( )Tj ( )Tj 7 0 0 7 204.0935 309.7654 Tm 9 0 0 9 36.8504 302.8898 Tm 7 0 0 7 355.3163 144.7654 Tm EMC ET BT EMC (CFM56-7B27B3)Tj /P <>BDC ( )Tj BT 7 0 0 7 247.7395 584.7654 Tm -.02 Tc ET 6.5 0 0 6.5 499.22 598.9529 Tm ( )Tj 0 Tc -.02 Tc EMC ET ET 7 0 0 7 54.7071 606.7654 Tm 8 0 0 8 542.9269 786.8898 Tm BT ET 9 0 0 9 187.8892 159.8898 Tm ET /P <>BDC ET 9 0 0 9 391.278 313.8898 Tm battery bus but have a dedicated battery to ensure that there is always ET 5.25 0 0 5.25 447.6106 11.5129 Tm 9 0 0 9 232.4217 368.8898 Tm BT 0 Tc BT ET 7 0 0 7 294.4014 705.7654 Tm ( )Tj ET /P <>BDC /P <>BDC ET EMC ( )Tj concentration at eight different locations. BT ET ( )Tj to the centre tank through a manual valve by cabin pressure. EMC ET (\(see table, this)Tj ET EMC (39,270lbs)Tj EMC ET ET (1,876)Tj /P <>BDC BT /P <>BDC /P <>BDC -.02 Tc 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 thanks for stopping by. (network. 0 Tc 9 0 0 9 53.8578 280.8898 Tm BT BT -.02 Tc EMC -.02 Tc /P <>BDC ET (against the 737-800 is interesting. BT point +3C, whichever is EMC BT ET EMC ET ET ET 0 Tc BT ET ( )Tj 7 0 0 7 384.8358 683.7654 Tm /P <>BDC BT [(BOS-A)56.9(TL)]TJ BT (and the A321ceo and A321neo. .151 .147 .15 rg EMC 9 0 0 9 232.4217 566.8898 Tm /P <>BDC 9 0 0 9 394.0157 104.8898 Tm (737-900ER\(W\) rather than the 737-900,)Tj EMC /P <>BDC EMC EMC (OEW being 6,500lbs higher. (A320ceo)Tj /P <>BDC BT EMC ET ET EMC /P <>BDC 9 0 0 9 197.8317 379.8898 Tm 0 Tc /P <>BDC 0 Tc /P <>BDC ( )Tj BT ET 9 0 0 9 536.1277 247.8898 Tm 9 0 0 9 68.0071 159.8898 Tm ( )Tj /P <>BDC EMC EMC EMC (192 seats versus 179 on the 737-9. (more seats. ET However, it was also shown that the dual venting configuration of some BT [(A3)24.9(21neo v)12.9(ersus 7)-33(3)8.1(7-9 )]TJ 9 0 0 9 540.3981 588.8898 Tm EMC 0 Tc ET BT ( )Tj -.02 Tc BT 0 Tc /P <>BDC 7 0 0 7 299.0601 276.9528 Tm How Many Flight Attendants Are on a Plane. 0 Tc EMC ET EMC (1,824)Tj /P <>BDC BT ET /P <>BDC 7 0 0 7 277.3936 67.9528 Tm -.02 Tc ( )Tj EMC ET -.02 Tc -.01 Tc EMC /P <>BDC /P <>BDC 7 0 0 7 99.8582 298.7654 Tm ET ET 7 0 0 7 294.4014 210.7654 Tm /P <>BDC The A320neo in this study)Tj ( )Tj BT refuelling panel to AUX TANKS. EMC BT ET EMC 9 0 0 9 341.1717 478.8898 Tm /Artifact <>BDC 7 0 0 7 247.7395 518.7654 Tm /GS1 gs ( )Tj BT /P <>BDC 9 0 0 9 394.0315 214.8898 Tm /P <>BDC ET BT 0 Tc ET 0 Tw ET (248,064)Tj /P <>BDC ET 6.5 0 0 6.5 328.6662 585.9529 Tm ET ( )Tj 9 0 0 9 36.8504 423.8898 Tm /P <>BDC ET ET ET EMC ET BT (payload is carried. 9 0 0 9 359.1448 181.8898 Tm ET ( )Tj EMC ET EMC 0 Tc BT /OC /MC5080 BDC ET 0 Tc BT ( )Tj BT -.07 Tc Centre tank LP lights are armed only when their pumps are ON. 7 0 0 7 230.7317 342.9528 Tm The 737-800 is the most popular variant of the four NG models, with nearly 5,000 aircraft delivered and making up 72% of the NG fleet in service. /P <>BDC ET EMC ( )Tj ET /P <>BDC /P <>BDC W n /OC /MC3449 BDC ( )Tj /P <>BDC EMC 9 0 0 9 394.0315 401.8898 Tm EMC ET ( )Tj 9 0 0 9 215.4313 467.8898 Tm 7 0 0 7 429.157 540.9528 Tm /P <>BDC ET 0 Tc BT ET 0 Tc EMC ET ET )Tj ( )Tj ET EMC 6 0 0 6 333.1569 743.9528 Tm ET ET ET /P <>BDC ( )Tj /P <>BDC BT ET EMC ( )Tj BT 7 0 0 7 518.4953 89.9528 Tm /P <>BDC EMC 6.5 0 0 6.5 397.8619 611.9529 Tm ET EMC (ONT/73)Tj EMC 7 0 0 7 491.4046 342.9528 Tm BT 9 0 0 9 518.9756 49.1073 Tm EMC BT ET EMC EMC BT BT 9 0 0 9 182.0482 379.8898 Tm -.02 Tc /P <>BDC /P <>BDC EMC ET 7 0 0 7 379.3969 177.7654 Tm ET 9 0 0 9 197.0674 258.8898 Tm -.02 Tc BT ET 9 0 0 9 51.0236 159.8898 Tm EMC EMC /P <>BDC ET BBJ Aux fuel panel located on Capt's & F/O's main /P <>BDC EMC -.02 Tc ET /P <>BDC ET /P <>BDC -.02 Tc (CFM56-7B27B3 installed on the 737-)Tj EMC /P <>BDC EMC /P <>BDC EMC EMC (passenger payload. 7 0 0 7 314.6398 683.7654 Tm 7 0 0 7 247.7395 485.7654 Tm EMC 7 0 0 7 182.5706 738.9528 Tm EMC 9 0 0 9 53.8582 643.8898 Tm /F1 1 Tf EMC ET 0 Tc BT /P <>BDC ET EMC BT EMC ( )Tj [(737 M)-8.1(A)-24.9(X-8:)]TJ 0 Tc illuminated is not only an explosion risk (see Thai and Philippine write offs) BT BT EMC /P <>BDC ET 7 0 0 7 88.196 11.5129 Tm 9 0 0 9 411.0181 390.8898 Tm /P <>BDC /P <>BDC BT BT BT /P <>BDC ET BT /P <>BDC EMC EMC 7 0 0 7 537.7804 188.9528 Tm ET This is due to cold EMC 7 0 0 7 314.6398 672.7654 Tm 6 0 0 6 268.0069 673.9528 Tm /P <>BDC 7 0 0 7 326.2278 518.9528 Tm (capacity of 160 \(the same as the 737-800\))Tj (3,031)Tj /P <>BDC 9 0 0 9 566.9979 423.8898 Tm ET ET /P <>BDC ( )Tj 9 0 0 9 51.0236 203.8898 Tm -.02 Tc Fuel remains one of the)Tj 7 0 0 7 440.0906 441.9528 Tm 9 0 0 9 368.3979 38.8898 Tm -.02 Tc 0 Tc BT 7 0 0 7 427.7291 287.9528 Tm EMC BT /P <>BDC /P <>BDC ( )Tj -.02 Tc /P <>BDC (1,272)Tj BT ET 5.25 0 0 5.25 492.6848 11.5129 Tm ( )Tj /P <>BDC -.02 Tc 9 0 0 9 215.4313 247.8898 Tm /P <>BDC BT BT 9 0 0 9 372.3347 412.8898 Tm ( )Tj /P <>BDC ( )Tj ET ( )Tj EMC 9 0 0 9 36.8583 467.8898 Tm 9 0 0 9 229.6141 302.8898 Tm ( )Tj ( )Tj 9 0 0 9 215.4313 38.8898 Tm /P <>BDC -.02 Tc EMC /F6 1 Tf ET /P <>BDC 9 0 0 9 411.0181 82.8898 Tm EMC 0 Tc ( )Tj 7 0 0 7 444.737 287.7654 Tm .41 .161 .508 RG 9 0 0 9 193.7007 236.8898 Tm BT ET EMC 0 Tc 7 0 0 7 294.4014 67.7654 Tm BT /P <>BDC ET BT EMC (ASM. BT /P <>BDC 7 0 0 7 363.0612 430.9528 Tm (in engine cool-down times. /P <>BDC EMC .151 .147 .15 rg (3,850)Tj ET (doors configuration. EMC (150)Tj /P <>BDC BT 0 Tc EMC ET ET EMC ( )Tj EMC ( )Tj ET ET BT ( )Tj /GS2 gs 9 0 0 9 548.3564 225.8898 Tm ET 9 0 0 9 394.0237 203.8898 Tm EMC 8 0 0 8 315.7776 577.9528 Tm /P <>BDC -.02 Tc /P <>BDC [(OM)8.1(M)-12.9(E)-24.9(R)7.1(C)8.1(E)]TJ EMC EMC ET 9 0 0 9 566.9709 126.8898 Tm EMC BT -.02 Tc /P <>BDC 9 0 0 9 552.5493 357.8898 Tm ET (37,653)Tj ( )Tj ET 7 0 0 7 53.8582 11.5132 Tm EMC (. BT /P <>BDC (163)Tj ET 0 Tc -.02 Tc 7 0 0 7 457.0984 287.7654 Tm ( )Tj EMC BT ET (136)Tj q 1 0 0 1 53.901 797.54 cm 0 0 m 6.5 0 0 6.5 170.1113 702.9529 Tm EMC /GS2 gs 0 Tc ET ET 7 0 0 7 131.6494 265.7654 Tm (172,842)Tj 7 0 0 7 440.0906 342.9528 Tm It is recognised that most)Tj (MTOW. [(differ)10(ences in fuel burn betw)6.1(een the types ar)10(e examined by Ian Britchfor)7.1(d. )]TJ
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