7 0 0 7 439.7405 617.9528 Tm ET 9 0 0 9 229.6064 49.8898 Tm BT /P <>BDC 10 0 0 10 36.2944 814.1973 Tm /P <>BDC 9 0 0 9 543.1465 511.8898 Tm [(Seat configur)10(ation)]TJ /P <>BDC 7 0 0 7 277.3936 276.9528 Tm 0 Tc 0 Tc ( )Tj /P <>BDC ET /P <>BDC (1,500)Tj 7 0 0 7 37.8848 452.9528 Tm /P <>BDC ET 36.85 824.882 572.599 17.008 re 13 0 0 13 215.4313 115.8898 Tm BT BT BT (The fuel tank capacity means the)Tj W n ( )Tj ET (flight levels. ET 9 0 0 9 211.035 709.8898 Tm (171,961)Tj ( )Tj 0 Tc BT EMC ( )Tj ET /P <>BDC 9 0 0 9 411.0097 49.8898 Tm BT /P <>BDC (In this comparison the passenger seat)Tj BT ( )Tj 7 0 0 7 379.3969 221.7654 Tm ET EMC ( )Tj 28.5749 0 TD ET BT 7 0 0 7 321.6356 166.9528 Tm BT ( )Tj /P <>BDC 7 0 0 7 491.7142 408.7654 Tm EMC BT ( )Tj 9 0 0 9 36.8583 478.8898 Tm BT (A320neo)Tj -.02 Tc ET EMC (31,416lbs)Tj ET 9 0 0 9 368.9649 423.8898 Tm 7 0 0 7 554.7883 122.7654 Tm ET ET The relative high)Tj BT -.02 Tc 7 0 0 7 404.101 276.7654 Tm ET 0 Tc EMC BT BT /P <>BDC ( )Tj EMC 7 0 0 7 99.8582 496.7654 Tm Aux fuel tank in aft hold of a BBJ2 (-800 fuselage). ET /P <>BDC 6.5 0 0 6.5 486.1525 722.9529 Tm ET ET ET ET (CFM56-5B3/P)Tj EMC /P <>BDC EMC .41 .161 .508 rg EMC 7 0 0 7 37.0536 716.9528 Tm 6 0 0 6 394.3996 687.9528 Tm /GS2 gs 9 0 0 9 53.8582 643.8898 Tm ET Until its launch on September 5, 1994 the 737-800 was known as the 737-400X Stretch. ( )Tj 10 0 0 10 54.8804 814.1973 Tm 5.25 0 0 5.25 549.1047 11.5132 Tm 9 0 0 9 53.8578 478.8898 Tm (377,550)Tj -.02 Tc 0 Tc /P <>BDC ET ( )Tj /P <>BDC -.02 Tc 7 0 0 7 403.478 727.7654 Tm BT ET 7 0 0 7 278.2756 672.9528 Tm 7 0 0 7 518.4953 122.9528 Tm 53.858 30.994 518.735 773.858 re BT BT EMC ( The taxi-in and taxi-out times and)Tj 9 0 0 9 394.0315 599.8898 Tm /P <>BDC 7 0 0 7 277.3936 144.9528 Tm /P <>BDC 9 0 0 9 376.2498 478.8898 Tm BT EMC BT /P <>BDC /P <>BDC ET EMC /OC /MC1956 BDC Hi Mark, S /P <>BDC ET Happy Flying. EMC ET -.02 Tc They are quite easy to find. ET BT -.02 Tc ET EMC EMC 7 0 0 7 294.4014 89.7654 Tm /F1 1 Tf 9 0 0 9 501.24 731.8898 Tm BT BT 9 0 0 9 36.8504 478.8898 Tm 9 0 0 9 394.0315 467.8898 Tm /P <>BDC BT EMC BT /P <>BDC 0 Tc ( )Tj EMC EMC /P <>BDC EMC ET ET 9 0 0 9 411.0097 38.8898 Tm EMC ET /P <>BDC ET EMC BT EMC ( )Tj 6.5 0 0 6.5 499.22 598.9529 Tm EMC BT ( )Tj /P <>BDC Classics could ET 9 0 0 9 383.3617 346.8898 Tm BT /P <>BDC /Artifact <>BDC /P <>BDC 9 0 0 9 261.8182 225.8898 Tm ET 9 0 0 9 394.0123 555.8898 Tm ( )Tj /GS2 gs BT 7 0 0 7 429.157 606.9528 Tm BT BT /P <>BDC /P <>BDC ET BT ( )Tj (direction, with an initial heading ranging)Tj [(E)-7.8(P)16.1(T)9(E)-13.9(MBE)-16.9(R)]TJ /P <>BDC EMC ET 9 0 0 9 126.1392 522.8898 Tm BT EMC 9 0 0 9 232.438 291.8898 Tm EMC EMC ET EMC EMC 0 Tc ET ( )Tj BT /P <>BDC ET (0.0135)Tj EMC 0 Tc 6.5 0 0 6.5 224.5532 598.9529 Tm BT ET BT ( )Tj BT ET ET ( )Tj ( )Tj 9 0 0 9 191.4329 786.8898 Tm The reductions in fuel burn also)Tj 6.5 0 0 6.5 433.3069 585.9529 Tm 7 0 0 7 539.8962 639.9528 Tm 0 Tw (The cost index used is heavily)Tj EMC The payload reduction is)Tj ET /P <>BDC (182,299)Tj ( )Tj EMC ET ( )Tj 6 0 0 6 61.517 645.9528 Tm 0 Tc (operating performance are analysed here,)Tj The service ceiling is 41,000 feet. 9 0 0 9 232.4217 170.8898 Tm 0 Tc ET 36.85 31.181 518.74 773.859 re EMC BT /P <>BDC EMC 9 0 0 9 532.8774 346.8898 Tm ( )Tj (SEA, SFO, YVR and LAX. 0 Tc 0 Tc (7,390)Tj 5.25 0 0 5.25 73.853 11.5132 Tm ( )Tj /P <>BDC /P <>BDC 0 Tw /P <>BDC ( )Tj 0 Tc EMC (39,270)Tj ET ET BT ET ET -.005 Tc ET 9 0 0 9 512.8093 434.8898 Tm EMC EMC 6 0 0 6 316.5908 771.9528 Tm BT BT BT 7 0 0 7 37.6993 78.9528 Tm 0 Tc BT 7 0 0 7 314.6398 540.7654 Tm /P <>BDC /P <>BDC /P <>BDC BT the climb. ET BT EMC ET BT ET ( )Tj (weight penalty in its OEW compared to its)Tj ET /P <>BDC EMC /F6 1 Tf /P <>BDC EMC ( )Tj /P <>BDC ET (174,606)Tj BT 6.5 0 0 6.5 379.1824 565.9529 Tm /P <>BDC -.01 Tc ( N)Tj BT ET /P <>BDC ( )Tj (0.0142)Tj ET As)Tj EMC ET EMC 10 0 0 10 47.8705 814.1973 Tm ET EMC ET 9 0 0 9 53.8582 709.8898 Tm BT ET ET )Tj EMC (737-800W)Tj 9 0 0 9 541.1665 599.8898 Tm BT ( )Tj 19.841 0 l EMC /P <>BDC /P <>BDC 7 0 0 7 344.1175 617.7654 Tm 0 Tc 5.25 0 0 5.25 40.8474 11.5129 Tm 7 0 0 7 247.7395 485.7654 Tm 7 0 0 7 491.7142 67.7654 Tm BT EMC /P <>BDC ET BT -.02 Tc ET /P <>BDC ET BT BT EMC 7 0 0 7 491.7142 133.7654 Tm ( )Tj 7 0 0 7 444.737 210.7654 Tm ( )Tj /P <>BDC /P <>BDC 9 0 0 9 195.4763 258.8898 Tm 7 0 0 7 279.1575 617.9528 Tm 7 0 0 7 355.3163 122.7654 Tm In reality, most models will operate in a combination of classes. ET ET /P <>BDC BT /P <>BDC 13 0 0 13 355.5757 115.8898 Tm /P <>BDC (39,270)Tj /P <>BDC BT EMC Required fields are marked *. ET 0 Tc The payload weights for)Tj EMC BT -.02 Tc (1,272)Tj /P <>BDC EMC ET /P <>BDC /P <>BDC EMC EMC EMC As stated, this makes a fair)Tj EMC 7 0 0 7 535.5029 496.7654 Tm /P <>BDC /P <>BDC 7 0 0 7 337.6855 485.9528 Tm ET ET ET 0 Tc ET (1,825)Tj /P <>BDC 6.5 0 0 6.5 191.7701 558.9529 Tm 7 0 0 7 230.7317 309.9528 Tm EMC -.02 Tc EMC /P <>BDC BT (16,170)Tj /P <>BDC (typically based on the aircrafts certified)Tj ET /P <>BDC EMC 7 0 0 7 554.7883 177.7654 Tm /P <>BDC EMC 0 Tc (277,248)Tj /P <>BDC endobj 0 Tc /P <>BDC /P <>BDC BT BT /P <>BDC 7 0 0 7 113.1366 221.9528 Tm EMC 9 0 0 9 53.8338 236.8898 Tm BT /P <>BDC EMC /P <>BDC ET (Using the evaluation payloads of 170)Tj /P <>BDC 7 0 0 7 230.7317 331.9528 Tm 6.5 0 0 6.5 228.7846 545.9529 Tm ( )Tj EMC ET /P <>BDC BT ET 9 0 0 9 182.8313 346.8898 Tm /P <>BDC ET ET ET ( )Tj BT 7 0 0 7 338.6433 177.7654 Tm 9 0 0 9 215.4313 456.8898 Tm /P <>BDC ( )Tj ( )Tj 9 0 0 9 394.0123 324.8898 Tm /P <>BDC 7 0 0 7 387.0932 265.9528 Tm q 1 0 0 1 36.85 84.878 cm 0 0 m /P <>BDC EMC BT /P <>BDC EMC /P <>BDC /P <>BDC /P <>BDC 7 0 0 7 445.619 639.7654 Tm 0 Tc /P <>BDC ET BT (capacity of 6,353USG, giving it a range of)Tj 0 Tc ET BT ET EMC ET 7 0 0 7 99.8582 430.7654 Tm 9 0 0 9 521.6329 137.8898 Tm f EMC BT 6 0 0 6 55.0668 701.9528 Tm 0 Tc ( )Tj /P <>BDC BT EMC ET .7 -.5345 .9114 -1.2305 y [(737-900E)-33(R)]TJ BT ( )Tj EMC 0 Tc EMC /P <>BDC (283)Tj 9 0 0 9 172.0312 357.8898 Tm -.02 Tc ( )Tj /P <>BDC BT ET BT BT /P <>BDC BT ET 7 0 0 7 95.225 11.5132 Tm 0 Tc ET BT /P <>BDC EMC ( )Tj 0 Tc BT ET ET /P <>BDC higher. EMC BT (170)Tj 7 0 0 7 210.1137 166.7654 Tm BT ET -.02 Tc (. ET ET /P <>BDC /P <>BDC -.02 Tc /GS1 gs /P <>BDC 7 0 0 7 258.2805 144.7654 Tm ET BT 8 0 0 8 456.5927 771.7654 Tm BT (performance than the 737-9. EMC EMC ET EMC /P <>BDC BT BT 0 Tc 9 0 0 9 369.0641 225.8898 Tm BT /P <>BDC ET ( )Tj ET /P <>BDC BT 0 Tc BT BT ( )Tj 7 0 0 7 54.7071 683.7654 Tm BT ET endobj -.02 Tc ( )Tj ( )Tj EMC 9 0 0 9 550.8315 247.8898 Tm BT (for seats. 0 Tc /P <>BDC BT ( )Tj EMC /P <>BDC 9 0 0 9 518.5923 511.8898 Tm EMC 9 0 0 9 386.2848 170.8898 Tm (206,132)Tj ET ( )Tj ( )Tj (2,564)Tj EMC BT /P <>BDC EMC 8 0 0 8 38.4438 605.9528 Tm BT BT /GS2 gs /P <>BDC to test (177)Tj EMC ET /P <>BDC 0 Tc /P <>BDC ET ET 7 0 0 7 404.101 430.7654 Tm 7 0 0 7 554.7883 386.7654 Tm (CFM56-7B26)Tj ET EMC ET BT ET BT /P <>BDC EMC ET ( )Tj ET 9 0 0 9 376.0468 401.8898 Tm -.01 Tc 9 0 0 9 360.0909 115.8898 Tm BT 9 0 0 9 186.0353 291.8898 Tm EMC ( )Tj ( in absolute terms in USG,)Tj EMC ( )Tj /P <>BDC BT ( )Tj BT BT Note that the first 1,000 pounds of fuel are loaded into the center tank, then the wing tanks are . BT (the CFM56-5B4/P with a maximum take-)Tj (152)Tj ET BT EMC /P <>BDC ( )Tj /P <>BDC BT .41 .161 .508 RG EMC 7 0 0 7 187.0858 309.9528 Tm (performed with both engines operating to)Tj EMC EMC /P <>BDC (CFM56-7B26)Tj EMC ( )Tj -.02 Tc ( )Tj BT EMC BT (4,787)Tj ET ET EMC ET W n BT EMC -.02 Tc /P <>BDC 6.5 0 0 6.5 112.0328 637.9529 Tm 9 0 0 9 215.433 357.8898 Tm EMC EMC BT BT 9 0 0 9 493.9938 357.8898 Tm BT /P <>BDC 7 0 0 7 247.7395 617.7654 Tm ET (150)Tj 7 0 0 7 82.2047 540.9528 Tm EMC 9 0 0 9 348.3267 324.8898 Tm ( )Tj BT 0 Tw /P <>BDC (282-294)Tj (150)Tj ET EMC ( )Tj 7 0 0 7 537.7804 78.9528 Tm EMC /P <>BDC BT BT This)Tj BT 7 0 0 7 107.1165 375.9528 Tm BT BT EMC EMC -.02 Tc ( )Tj BT EMC ( )Tj BT /P <>BDC /P <>BDC ET ET 7 0 0 7 299.0601 298.9528 Tm /P <>BDC 0 Tc EMC ET (326-339)Tj /P <>BDC EMC Cruise Speed: 530 mph Propulsion: Two General Electric CFM56-7B24 High Bypass Ratio turbofan engines, rated at 24,200 pounds thrust each. /P <>BDC 7 0 0 7 321.6356 331.9528 Tm BT ET EMC ( )Tj BT [(P)11(assengers)]TJ ( )Tj ET 7 0 0 7 536.3849 265.7654 Tm EMC 7 0 0 7 299.0601 386.9528 Tm ET ( )Tj BT EMC ET EMC ET EMC /P <>BDC /P <>BDC ( )Tj ( )Tj ET (273,600)Tj ( )Tj ( )Tj EMC (Block time - mins)Tj ET 9 0 0 9 211.8218 533.8898 Tm EMC EMC 7 0 0 7 37.0536 595.9528 Tm EMC (82,110)Tj EMC BT BT ET (273,750)Tj 7 0 0 7 537.7804 419.9528 Tm /P <>BDC ( )Tj Hi. EMC (costs could almost double the per ASM)Tj /P <>BDC /P <>BDC BT BT ET /P <>BDC ( )Tj ET ET 7 0 0 7 491.4046 243.9528 Tm ( )Tj /P <>BDC BT ET /P <>BDC 9 0 0 9 232.438 280.8898 Tm 0 Tc BT /P <>BDC ET BT 9 0 0 9 204.06 742.8898 Tm ( )Tj 9 0 0 9 392.5848 346.8898 Tm /P <>BDC /P <>BDC 5.25 0 0 5.25 549.1047 11.5132 Tm 0 Tc ( )Tj (Boeing aircraft, the 737-800 has a 2.5%)Tj 7 0 0 7 241.2727 562.9528 Tm ET -.02 Tc 0 Tc 7 0 0 7 299.0601 166.9528 Tm ET /P <>BDC 9 0 0 9 199.4908 192.8898 Tm EMC BT ( )Tj Fuel remains one of the)Tj (3,882)Tj /P <>BDC BT BT -.02 Tc EMC EMC BT /P <>BDC BT ET ET /P <>BDC BT /P <>BDC /P <>BDC ET BT /P <>BDC 0 Tc /P <>BDC /P <>BDC BT /P <>BDC ET -.02 Tc ( )Tj (136)Tj ( )Tj 9 0 0 9 518.0203 170.8898 Tm ( )Tj /P <>BDC EMC /P <>BDC (are taxi fuel burn, flight fuel burn, the)Tj /P <>BDC /P <>BDC 6.5 0 0 6.5 221.9596 689.9529 Tm 0 Tc -.02 Tc /P <>BDC /P <>BDC BT -.01 Tc BT 9 0 0 9 36.8504 324.8898 Tm BT [(SS)-9.1(U)8(E)]TJ BT ( )Tj /P <>BDC ET ET BT BT 7 0 0 7 141.7322 386.9528 Tm EMC BT (the equivalent aircraft types, the lowest fuel)Tj BT /P <>BDC ET EMC BT BT ET 9 0 0 9 369.406 104.8898 Tm -.01 Tc EMC 9 0 0 9 53.8578 258.8898 Tm BT BT EMC ET ET ET ( )Tj ET 8 0 0 8 531.9995 82.8898 Tm /P <>BDC /P <>BDC ( )Tj 6.5 0 0 6.5 171.7493 689.9529 Tm (\(see table, this)Tj /OC /MC4794 BDC ( )Tj BT 9 0 0 9 356.7322 159.8898 Tm ET EMC /P <>BDC EMC (the A321ceo, A321neo, 737-900ER\(W\))Tj BT BT EMC ( )Tj W n The fwd and aft tanks are switched off when the 9 0 0 9 548.1057 610.8898 Tm /GS2 gs /P <>BDC /P <>BDC EMC ET ( )Tj 0 Tc -.01 Tc ET [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ BT ( )Tj ET ET BT (1,272)Tj /P <>BDC (2,154)Tj 9 0 0 9 213.1228 368.8898 Tm .151 .147 .15 rg 7 0 0 7 365.035 89.9528 Tm BT 0 Tc ET ET EMC Out of the 135 passengers on board there were 9 fatalities and 84 suffered injuries. BT ET EMC EMC EMC EMC 7 0 0 7 428.6112 419.9528 Tm ET ( )Tj 7 0 0 7 37.6993 375.9528 Tm ET /P <>BDC 9 0 0 9 53.8582 181.8898 Tm (considered include fleet commonality,)Tj ( )Tj 7 0 0 7 326.2278 529.9528 Tm /P <>BDC BT BT BT EMC EMC BT 9 0 0 9 557.1673 794.1039 Tm (allow a direct comparison of trip fuel burn)Tj ET ET ET 0 Tc EMC 7 0 0 7 439.2087 67.9528 Tm ( )Tj EMC BT EMC /P <>BDC -.02 Tc (patterns or delays )Tj 6.5 0 0 6.5 191.7926 702.9529 Tm ET BT The CFM56-5B4/P has a)Tj BT ET ET 7 0 0 7 343.2355 683.7654 Tm EMC ET 7 0 0 7 101.0963 287.9528 Tm 0 Tc ( )Tj EMC ( )Tj 7 0 0 7 457.0984 595.7654 Tm BT ET 7 0 0 7 554.7883 606.7654 Tm EMC 9 0 0 9 215.4409 500.8898 Tm 0 Tc ( )Tj /Artifact <>BDC ET BT EMC EMC EMC BT ( )Tj /P <>BDC BT ET /P <>BDC (in a more efficient engine. /P <>BDC /P <>BDC BT BT EMC ET 7 0 0 7 539.8962 529.9528 Tm tank. EMC BT /P <>BDC EMC 0 Tc BT (second payload scenario using the 85%)Tj ET EMC ET 7 0 0 7 294.4014 441.7654 Tm EMC Pisquali 19/05/2018 at 16:07 Reply. EMC ET EMC 9 0 0 9 202.684 357.8898 Tm EMC EMC BT /P <>BDC BT <>stream BT EMC /P <>BDC ET ET (subsidiary airlines. ( )Tj BT 7 0 0 7 473.8245 67.9528 Tm EMC BT ET /P <>BDC .023 .567 .626 rg BT BT 7 0 0 7 507.7893 628.7654 Tm BT 7 0 0 7 158.74 573.7654 Tm (I)Tj ET EMC BT /P <>BDC 7 0 0 7 387.0159 463.9528 Tm BT EMC 6 0 0 6 247.4022 729.9528 Tm ET (737-8)Tj ET EMC BT ET (0.0127)Tj 9 0 0 9 394.0315 38.8898 Tm ET EMC (seat count as the 737-900ER\(W\). /P <>BDC EMC ( )Tj 7 0 0 7 258.2805 364.7654 Tm ET [(C)17.1(OS/104)]TJ EMC 7 0 0 7 337.9444 89.9528 Tm ET ( )Tj ET EMC EMC 7 0 0 7 258.2805 122.7654 Tm /P <>BDC ( )Tj EMC ( )Tj EMC ( )Tj 7 0 0 7 474.3564 738.9528 Tm ET /P <>BDC 8 0 0 8 447.9182 771.9529 Tm BT BT /P <>BDC -.02 Tc ( )Tj 8 0 0 8 38.4744 758.9528 Tm BT The 737-900 also retains the MTOW and fuel capacity of the 800, trading range for payload. BT BT BT -.6563 -2.3409 l -2.4549 -3.9026 m EMC BT EMC ET BT 0 Tc ET 0 Tc /P <>BDC BT 9 0 0 9 531.3621 148.8898 Tm (1,162)Tj ET /F1 1 Tf 9 0 0 9 411.0234 687.8898 Tm allowed to run dry or be left running unsupervised. 7 0 0 7 233.5248 78.9528 Tm ET BT BT ( )Tj /P <>BDC EMC Hi Andrey, BT EMC BT /P <>BDC EMC BT 10 0 0 10 425.05 814.1973 Tm EMC (A)Tj EMC ET EMC EMC EMC 9 0 0 9 394.0315 709.8898 Tm ET .151 .147 .15 rg ET /P <>BDC ( )Tj BT /P <>BDC /P <>BDC ET EMC BT EMC /P <>BDC BT 7 0 0 7 507.7893 595.7654 Tm ( )Tj EMC EMC EMC EMC ET BT EMC ET ( )Tj ET (the results show that the lighter payload on)Tj BT BT BT 9 0 0 9 546.1516 203.8898 Tm /P <>BDC 8 0 0 8 447.8735 760.9529 Tm (418)Tj /P <>BDC 6 0 0 6 363.2184 687.9528 Tm /P <>BDC -2.5306 -6.3496 -3.213 -6.0519 -3.7399 -5.4283 c (The fuel cost per ASM improves with)Tj BT Seating in the 737 was a result of the design when moving the engines underneath the wings. 0 Tc (maximum fuel capacity, the A320neo)Tj BT 0 Tc 0 Tc ( )Tj [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ /P <>BDC (evaluation that are payload-limited on the)Tj 9 0 0 9 215.433 71.8898 Tm BT /P <>BDC BT EMC ( )Tj EMC 7 0 0 7 344.1175 584.7654 Tm (21)Tj EMC BT ET BT /P <>BDC ( )Tj /P <>BDC ( )Tj ET (297,475)Tj -.02 Tc A lower)Tj BT /P <>BDC BT 6.5 0 0 6.5 244.0438 722.9529 Tm ET EMC EMC /P <>BDC BT BT 9 0 0 9 53.8582 665.8898 Tm EMC EMC BT /P <>BDC Q ( )Tj ET ( )Tj ( )Tj ( )Tj BT EMC BT -.02 Tc 6.5 0 0 6.5 346.1424 545.9529 Tm BT /P <>BDC BT BT 9 0 0 9 420.5961 38.3073 Tm 7 0 0 7 187.5417 430.9528 Tm (sectors where a 170-passenger payload is)Tj ET 0 Tc /P <>BDC 10 0 0 10 539.3945 794.2914 Tm /P <>BDC /P <>BDC 9 0 0 9 455.0733 302.8898 Tm (170)Tj EMC ( )Tj ET /P <>BDC How Many Flight Attendants Are on a Plane. I already checked in the AMM, SRM. /P <>BDC /P <>BDC q 1 0 0 1 515.394 88.945 cm 0 0 m /P <>BDC 7 0 0 7 326.2278 474.9528 Tm BT BT 9 0 0 9 535.2501 522.8898 Tm BT ET ET -.02 Tc 13 0 0 13 274.8818 137.8898 Tm EMC EMC BT 6.5 0 0 6.5 276.5184 565.9529 Tm ET ET 0 Tc Airbus A330 Specs What can this popular long haul twin jet do? ( )Tj ET EMC /P <>BDC ET ET On the Digital Sunburst fuel gauges, pressing the "Qty test" button will EMC 7 0 0 7 403.478 419.7654 Tm 7 0 0 7 457.0984 606.7654 Tm (464,270)Tj ET ( )Tj /P <>BDC ( )Tj Alaska Airlines launched the 737-900 in 1997, the 737-900 made its first . EMC 9 0 0 9 205.6978 291.8898 Tm 7 0 0 7 363.2711 276.9528 Tm BT ET BT ET /P <>BDC 9 0 0 9 385.5399 115.8898 Tm ET 8 0 0 8 488.4333 760.7654 Tm ET 9 0 0 9 553.5856 467.8898 Tm BT -.02 Tc ( )Tj 7 0 0 7 131.6494 375.7654 Tm BT EMC /P <>BDC /F6 1 Tf 0 Tc 0 Tc (A320ceo)Tj /P <>BDC BT (seat capacity of 179. 7 0 0 7 315.5217 584.7654 Tm ( )Tj 9 0 0 9 394.0237 335.8898 Tm BT 9 0 0 9 191.9099 93.8898 Tm (. EMC BT ( )Tj 9 0 0 9 206.3999 445.8898 Tm ( )Tj EMC /P <>BDC ( )Tj EMC EMC BT EMC /P <>BDC ET ET ET -.02 Tc ET 9 0 0 9 545.0095 357.8898 Tm BT ( )Tj EMC 0 Tc ET EMC ET 9 0 0 9 36.8504 148.8898 Tm EMC -.02 Tc 7 0 0 7 537.7804 89.9528 Tm /P <>BDC ( )Tj 0 Tc ET EMC ET BT /GS2 gs 9 0 0 9 36.8504 137.8898 Tm EMC ET ET ET ET )Tj EMC (464,440)Tj EMC /P <>BDC /P <>BDC 6.5 0 0 6.5 296.3931 532.9529 Tm EMC 0 Tc BT BT /P <>BDC /P <>BDC -.02 Tc -.02 Tc /P <>BDC BT (CFM56-5B3/P)Tj EMC .151 .147 .15 rg /P <>BDC ET BT /P <>BDC EMC 0 Tc EMC (737-9)Tj BT /P <>BDC ET ET 7 0 0 7 457.0984 408.7654 Tm /P <>BDC BT 7 0 0 7 537.267 232.7654 Tm ET BT (the longest BOS-LAX sector. /P <>BDC 5.25 0 0 5.25 515.3989 11.5129 Tm /P <>BDC 7 0 0 7 337.6855 419.9528 Tm BT (35,112lbs)Tj ET EMC BT ET BT ET )Tj 9 0 0 9 229.6045 390.8898 Tm 7 0 0 7 279.1575 716.9528 Tm BT BT -.02 Tc ET ( )Tj ( )Tj EMC BT /P <>BDC EMC 56 0 0 56 36.8606 562.1944 Tm BT 0 Tc BT /P <>BDC ET -.02 Tc ET BT 9 0 0 9 366.4417 533.8898 Tm ET /P <>BDC 9 0 0 9 229.6045 236.8898 Tm ( )Tj ( 2021)Tj ( )Tj ( )Tj /P <>BDC BT 9 0 0 9 68.0314 775.8898 Tm ET BT EMC /P <>BDC (The aircraft weights used in this)Tj BT ET The 737-800 project began in 1994, with Hapag-Lloyd Airlines ofGermany placing the first order for this aircraft. ET BT ET /P <>BDC ET [(737 M)-8.1(A)-24.9(X-9:)]TJ 7 0 0 7 141.7322 78.9528 Tm EMC ET /P <>BDC /P <>BDC 13 0 0 13 53.8578 181.8898 Tm )Tj BT -.02 Tc /P <>BDC /P <>BDC ET ET (assumes that an equal number of)Tj .1334 -5.7288 l 6.5 0 0 6.5 296.4841 663.9529 Tm 7 0 0 7 521.4089 11.5132 Tm BT ( )Tj -.02 Tc 9 0 0 9 173.6527 500.8898 Tm BT 6.5 0 0 6.5 448.2959 585.9529 Tm ET ET EMC (1,272)Tj /P <>BDC ET ET ( )Tj /P <>BDC ET ( )Tj It sounds like you have a bit of a project on your hands. ET EMC (976)Tj (comparison. -.02 Tc 0 Tc /P <>BDC ET 6.5 0 0 6.5 346.1035 637.9529 Tm ( )Tj /P <>BDC 6 0 0 6 153.0397 715.9528 Tm EMC BT ET BT ( )Tj ET /P <>BDC 7 0 0 7 439.2087 210.9528 Tm (assume that the optimum flight level could)Tj ( )Tj EMC BT ET -.02 Tc BT ( )Tj /P <>BDC EMC EMC ET 9 0 0 9 232.4408 764.8898 Tm /P <>BDC 0 Tc 7 0 0 7 539.9176 11.5129 Tm 7 0 0 7 99.8582 188.7654 Tm 7 0 0 7 362.3891 364.9528 Tm BT 9 0 0 9 382.4508 159.8898 Tm ET EMC BT /P <>BDC /P <>BDC EMC /GS1 gs 6 0 0 6 184.4022 729.9528 Tm [(UG)-17.1(U)-8(S)8.1(T)]TJ ( )Tj BT ET BT /GS1 gs 0 Tc /P <>BDC 0 Tc EMC EMC ET BT BT BT -.02 Tc EMC EMC /P <>BDC (410)Tj 0 Tc ET ET ET ET 7 0 0 7 316.0679 232.7654 Tm 7 0 0 7 508.4124 78.7654 Tm BT ( )Tj .151 .147 .15 rg BT 9 0 0 9 252.5189 181.8898 Tm /P <>BDC BT -.02 Tc /P <>BDC ( )Tj ( )Tj BT EMC ( )Tj ET ( )Tj BT /P <>BDC movement as fuel is loaded and used. ET /P <>BDC 6 0 0 6 434.151 715.9528 Tm 7 0 0 7 338.6433 199.7654 Tm /P <>BDC ET (and taxi-in times would vary by flight. BT 7 0 0 7 204.0935 485.7654 Tm /P <>BDC The 800 shares a lineage with the 300, 400, and 500. ET BT /P <>BDC ( )Tj 7 0 0 7 539.8962 518.9528 Tm /P <>BDC ( )Tj 6 0 0 6 214.8454 771.9528 Tm 7 0 0 7 278.2756 78.9528 Tm ( )Tj 9 0 0 9 538.8445 588.8898 Tm 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. EMC EMC (98-107)Tj EMC /P <>BDC (150)Tj ( )Tj EMC /P <>BDC ( )Tj ET 7 0 0 7 199.5784 144.7654 Tm ET 7 0 0 7 230.7317 122.9528 Tm 6 0 0 6 278.7028 659.9528 Tm BT /P <>BDC 0 Tc -.02 Tc (between 420nm and 2,429nm )Tj ET EMC BT BT EMC BT ET EMC 137 )Tj EMC EMC EMC ET /P <>BDC ( )Tj /P <>BDC EMC 8 0 0 8 270.7815 771.9528 Tm (2,220)Tj 7 0 0 7 99.8582 738.7654 Tm 7 0 0 7 187.0858 210.9528 Tm <> BT /P <>BDC BT /P <>BDC compensator /P <>BDC BT /P <>BDC BT 9 0 0 9 550.3666 247.8898 Tm EMC 7 0 0 7 508.2252 11.5129 Tm BT /P <>BDC ( )Tj /P <>BDC 7 0 0 7 204.0935 232.7654 Tm EMC ET BT EMC EMC (performance deterioration factor added to)Tj EMC /P <>BDC 7 0 0 7 125.6292 144.7654 Tm ET Specification Table Boeing 737 Original and Boeing 737 Classic (Top). BT 0 Tc (73,872)Tj EMC 0 Tc /P <>BDC BT ET (significant enough that operating the)Tj EMC /P <>BDC /P <>BDC ( )Tj ET (BOS-MIA)Tj Take-off Weight 154,500 lb (70,080 kg) Entertainment System: Full cabin Overhead screens 8 Stereo Music Channels Maximum Range: 3,365 nautical miles (6,225 km) Cargo: 966 cu ft (27.3 cu m) Typical Cruise Speed @ 35,000ft altitude 0.785 Mach . BT 7 0 0 7 439.7405 584.9528 Tm BT BT ET 7 0 0 7 321.6356 100.9528 Tm 7 0 0 7 535.5029 474.7654 Tm /P <>BDC W n EMC BT ET /P <>BDC /P <>BDC ET ET 7 0 0 7 403.478 628.7654 Tm /P <>BDC EMC ( )Tj /P <>BDC 7 0 0 7 315.1859 100.7654 Tm EMC 7 0 0 7 337.6855 540.9528 Tm 7 0 0 7 210.1137 661.7654 Tm BT BT ET EMC BT /P <>BDC 6.5 0 0 6.5 448.8744 558.9529 Tm ( )Tj EMC )Tj Well, the fuel capacity of this airplane varies depending on the specific model and generation. 0 Tc BT /P <>BDC [(SS)-9.1(U)8(E)]TJ (A321neo:)Tj /P <>BDC /OC /MC3432 BDC /P <>BDC -.02 Tc 7 0 0 7 316.0679 287.7654 Tm EMC [(CFM L)17.1(E)-8.1(AP-1A32)]TJ 7 0 0 7 327.1097 628.9528 Tm I am looking to build a prototype of Boeing 737 for numerical simulation purpose. 7 0 0 7 294.4014 298.7654 Tm 7 0 0 7 520.6108 683.9528 Tm EMC EMC 8 0 0 8 124.845 717.9528 Tm ET EMC EMC ET EMC 0 Tc 7 0 0 7 427.7291 177.9528 Tm ET ( )Tj 7 0 0 7 474.7064 408.9528 Tm BT (34,650)Tj ET (37,653lbs)Tj 6 0 0 6 381.7993 715.9528 Tm /P <>BDC BT ( )Tj 6 0 0 6 184.3662 701.9528 Tm ( N)Tj /P <>BDC 7 0 0 7 298.514 617.9528 Tm ET (. -.02 Tc EMC 7 0 0 7 535.5029 441.7654 Tm /P <>BDC 9 0 0 9 533.0564 181.8898 Tm BT /P <>BDC (carried - lbs)Tj EMC 6.5 0 0 6.5 500.4941 565.9529 Tm EMC /P <>BDC BBJ Aux fuel panel located on Capt's & F/O's main 7 0 0 7 507.7893 111.7654 Tm ET /P <>BDC EMC /P <>BDC BT EMC EMC /P <>BDC (payload carried. (Although it is most fuel-efficient to)Tj )Tj /P <>BDC BT 7 0 0 7 363.2711 397.9528 Tm 7 0 0 7 338.6433 397.7654 Tm /F6 1 Tf /P <>BDC BT ( )Tj BT 9 0 0 9 342.6025 368.8898 Tm 0 Tc ET [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ (35,112)Tj EMC EMC i.e..what is the maximum lateral distance the doors swing away from the aircraft, before they get to rest in the fully open position? ( )Tj BT ET (2,731)Tj ET /P <>BDC (34,650lbs)Tj 7 0 0 7 108.6215 265.9528 Tm /P <>BDC ( )Tj ET EMC /P <>BDC BT EMC 6 0 0 6 496.2034 757.9528 Tm 9 0 0 9 213.0312 335.8898 Tm BT ( )Tj ( )Tj ET 0 Tc 8 0 0 8 266.591 745.9528 Tm ( )Tj ET BT (It is recognised that on some of the)Tj EMC /P <>BDC 7 0 0 7 230.7317 111.9528 Tm ET BT 9 0 0 9 411.0181 324.8898 Tm /P <>BDC EMC 9 0 0 9 215.4409 192.8898 Tm -.02 Tc BT /P <>BDC ET ( )Tj (0.0126)Tj (24)Tj BT /P <>BDC ET 17 0 0 17 526.2604 775.1944 Tm -.02 Tc EMC ET ET EMC .0161 Tc (170)Tj /F6 1 Tf EMC ( )Tj EMC BT -.01 Tc (163)Tj automatically shut off when they detect a low output pressure and there have /P <>BDC ( )Tj /P <>BDC /P <>BDC BT ( )Tj EMC /P <>BDC ET 7 0 0 7 439.2087 177.9528 Tm ET 0 J 0 j .5 w 10 M [] 0 d /P <>BDC (192 seats. BT ET BT (34,650)Tj ( The wind component and)Tj EMC BT 9 0 0 9 186.1613 49.8898 Tm ET 'http':'https';if(!d.getElementById(id)){js=d.createElement(s);js.id=id;js.src=p+'://platform.twitter.com/widgets.js';fjs.parentNode.insertBefore(js,fjs);}}(document, 'script', 'twitter-wjs'); The /P <>BDC ET 7 0 0 7 379.3969 166.7654 Tm EMC 0 Tc ET 0 841.89 609.449 -841.89 re 360 0 obj BT ET ( )Tj EMC EMC EMC /P <>BDC ET ( )Tj ET EMC mandatory, but the FAA have repeatedly rejected it on cost grounds. /P <>BDC (1,824)Tj (operator, so controlling this cost is a)Tj /OC /MC3449 BDC /P <>BDC EMC (737-9)Tj ET -.02 Tc (heavier than the A320ceo. ET ET /P <>BDC -.02 Tc 9 0 0 9 370.9169 379.8898 Tm BT EMC BT ET ET /P <>BDC EMC EMC ET ( )Tj ET BT ET BT EMC /P <>BDC /F1 1 Tf /P <>BDC EMC (47,000)Tj 7 0 0 7 108.6215 232.9528 Tm EMC ET ( )Tj BT 0 Tc ( )Tj 7 0 0 7 99.8582 276.7654 Tm BT BT 9 0 0 9 563.4796 324.8898 Tm ET /P <>BDC /P <>BDC (burns. 9 0 0 9 68.3339 533.8898 Tm ET 9 0 0 9 518.9185 401.8898 Tm BT /P <>BDC 10 0 0 10 54.1504 814.1973 Tm 6.5 0 0 6.5 274.6269 689.9529 Tm BT (to allow a clearer performance and fuel)Tj BT 9 0 0 9 189.1673 137.8898 Tm BT 0 Tc EMC BT 6 0 0 6 371.7608 701.9528 Tm ( )Tj ET (350-365)Tj 9 0 0 9 534.7515 599.8898 Tm /P <>BDC 9 0 0 9 394.0157 203.8898 Tm BT ( )Tj ( )Tj /P <>BDC 0 Tc /P <>BDC I will be very happy to share with you once I get decent results. /P <>BDC BT EMC ET (34,650lbs)Tj /P <>BDC /GS1 gs ET allowed for deposit of the ground-based NEA into the center wing tank (CWT). 7 0 0 7 403.478 694.7654 Tm /P <>BDC ( )Tj ( )Tj ET 5.25 0 0 5.25 515.3989 11.5129 Tm ET /P <>BDC 0 Tc ET ET 7 0 0 7 54.7071 210.7654 Tm -.02 Tc BT EMC EMC 7 0 0 7 230.7317 320.9528 Tm 9 0 0 9 186.0514 60.8898 Tm (The A321ceo is equipped with either:)Tj ET 737-800 & 737-8 The 737NG family has a single engine offering: the 737NG with the CFM56-7B; and the 737 MAX family with the CFM LEAP-1B. 0 Tc ( )Tj /P <>BDC EMC 9 0 0 9 374.2211 379.8898 Tm ET 9 0 0 9 53.8578 346.8898 Tm EMC /P <>BDC (A321ceo)Tj 0 Tc /P <>BDC 9 0 0 9 68.0314 522.8898 Tm ET BT EMC 7 0 0 7 554.7883 199.7654 Tm ET ( )Tj (1,913)Tj /P <>BDC BT /P <>BDC pump will also transfer any remaining centre tank fuel into main tank 1, thereby 6 0 0 6 403.5009 701.9528 Tm /P <>BDC ET /P <>BDC BT 9 0 0 9 216.03 687.8898 Tm (0.0112)Tj ET Whatever the reason, we hope that both Boeing and the F.A.A. ET (variant. (and A321neo respectively. EMC /P <>BDC 9 0 0 9 394.0123 115.8898 Tm /P <>BDC 9 0 0 9 551.1635 181.8898 Tm /P <>BDC ( )Tj BT ( )Tj EMC (1,825)Tj EMC BT ( )Tj EMC ET BT f 0 Tc 9 0 0 9 551.4784 797.8898 Tm BT 9 0 0 9 36.8504 104.8898 Tm 7 0 0 7 326.2278 463.9528 Tm ET /GS1 gs BT EMC EMC EMC ET ET BT BT /P <>BDC EMC /P <>BDC /P <>BDC EMC 7 0 0 7 474.7064 342.9528 Tm BT 9 0 0 9 411.0097 445.8898 Tm ET /P <>BDC /P <>BDC EMC 9 0 0 9 170.6722 104.8898 Tm ET Thank you, an example of one that was used is in the link below. EMC EMC EMC 6.5 0 0 6.5 243.3486 742.9529 Tm /P <>BDC <>/XObject<>/ExtGState<>/Properties<>>> -.02 Tc ET /P <>BDC 9 0 0 9 366.7762 390.8898 Tm Good luck. (2,437)Tj 7 0 0 7 54.7071 606.7654 Tm ET /P <>BDC /P <>BDC ET BT ET /P <>BDC For example, the)Tj ET /P <>BDC EMC BT ET /P <>BDC /P <>BDC EMC 7 0 0 7 535.5029 705.7654 Tm
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