(earlier counterpart. -.02 Tc ET ET BT BT EMC 7 0 0 7 258.2805 298.7654 Tm 6.5 0 0 6.5 447.8411 663.9529 Tm ( )Tj EMC ( )Tj EMC ( )Tj /P <>BDC 7 0 0 7 444.737 243.7654 Tm 7 0 0 7 326.2278 716.9528 Tm /P <>BDC 7 0 0 7 279.1575 386.9528 Tm BT (450,780)Tj EMC /P <>BDC 0 Tc EMC 7 0 0 7 108.6215 144.9528 Tm 6 0 0 6 184.072 659.9528 Tm ET ET EMC 6.5 0 0 6.5 346.3049 702.9529 Tm ET /P <>BDC 7 0 0 7 258.2805 683.7654 Tm BT BT Most of the differences comes from lighting in the overhead giving clear readings of digital gauges. BT /P <>BDC EMC -.02 Tc /P <>BDC 9 0 0 9 394.0315 291.8898 Tm EMC The charges are split by weight)Tj -.01 Tc EMC 7 0 0 7 366.0641 738.9528 Tm ET -.02 Tc ET ET 9 0 0 9 433.2572 104.8898 Tm (136)Tj ( )Tj /P <>BDC 7 0 0 7 258.2805 529.7654 Tm EMC BT ( )Tj 0 Tc BT /P <>BDC ET (136)Tj 9 0 0 9 359.0967 786.8898 Tm 9 0 0 9 530.624 269.8898 Tm ET EMC ( )Tj ( )Tj ET EMC BT 0 Tc 8 0 0 8 490.9813 771.9528 Tm EMC (ESAD)Tj ET ET BT BT 9 0 0 9 566.4993 698.8898 Tm ET BT BT (216)Tj EMC ET 9 0 0 9 36.8504 93.8898 Tm 7 0 0 7 536.3849 331.7654 Tm -.02 Tc 9 0 0 9 571.1344 742.8898 Tm /P <>BDC -.02 Tc (34,650)Tj ( )Tj EMC /P <>BDC 1 i EMC /P <>BDC For a 737-800 with 162 passengers on a 1000 NM trip, it's 96 mpg per passenger, or 0.593 mpg for the whole plane. 0 Tc /P <>BDC BT ET /P <>BDC /P <>BDC ET BT 0 Tc BT BT 7 0 0 7 158.74 78.7654 Tm BT ( )Tj ET EMC EMC 0 Tc /P <>BDC 9 0 0 9 202.1458 258.8898 Tm 0 Tc BT 9 0 0 9 53.8338 269.8898 Tm 9 0 0 9 411.0097 104.8898 Tm EMC 7 0 0 7 321.6356 243.9528 Tm /F6 1 Tf (fuel consumption and cost per seat or per)Tj ET EMC 9 0 0 9 394.0237 412.8898 Tm 7 0 0 7 520.6108 683.9528 Tm These incidents, and 15 more on other types since 1959, /P <>BDC ET EMC ET EMC BT BT 7 0 0 7 380.2788 485.7654 Tm EMC 0 Tc ET EMC BT ET The reserve policy)Tj ( )Tj 7 0 0 7 230.7317 287.9528 Tm 7 0 0 7 82.8504 188.9528 Tm BT BT 7 0 0 7 518.4953 232.9528 Tm /P <>BDC BT ET 17 0 0 17 36.8606 775.1944 Tm BT /P <>BDC ET ET 9 0 0 9 394.0157 269.8898 Tm 6 0 0 6 339.9977 687.9528 Tm /P <>BDC BT 13 0 0 13 355.5757 115.8898 Tm ET ET /P <>BDC BT (2,575)Tj ET 6 0 0 6 184.3662 673.9528 Tm ( )Tj ( )Tj BT /P <>BDC (297,475)Tj EMC ( )Tj /P <>BDC 0 J 0 j .5 w 10 M [] 0 d /P <>BDC ALERT light illuminates on the main panel. 7 0 0 7 491.7142 210.7654 Tm 7 0 0 7 247.7395 716.7654 Tm BT /P <>BDC 7 0 0 7 187.0858 364.9528 Tm /P <>BDC (31,416)Tj EMC /P <>BDC -.01 Tc BT EMC /P <>BDC 8 0 0 8 74.9636 717.9528 Tm 6 0 0 6 215.373 757.9528 Tm ET (CFM56-7B26)Tj EMC (737-8)Tj BT 7 0 0 7 445.619 584.7654 Tm ET 7 0 0 7 247.7395 485.7654 Tm ( )Tj /P <>BDC /P <>BDC (105)Tj EMC EMC 9 0 0 9 439.4008 324.8898 Tm (flight levels )Tj BT BT ( )Tj ( )Tj ( )Tj /P <>BDC 7 0 0 7 158.74 144.7654 Tm ET EMC ET 7 0 0 7 490.8321 166.7654 Tm /P <>BDC /P <>BDC EMC ET BT ET ET /P <>BDC /P <>BDC (operationally safe to do so, in the)Tj 9 0 0 9 215.4409 159.8898 Tm (A320ceo)Tj (148,504)Tj support combustion. BT EMC EMC -.02 Tc 7 0 0 7 469.2222 11.5129 Tm ET /P <>BDC BT ET ET EMC ET ET ET -.02 Tc EMC ET /Artifact <>BDC 9 0 0 9 394.0123 313.8898 Tm ET /P <>BDC BT 7 0 0 7 507.7893 584.7654 Tm ET /P <>BDC EMC ( )Tj 9 0 0 9 411.0181 38.8898 Tm ET /P <>BDC ( )Tj [(CFM L)17.1(E)-8.1(AP-)]TJ BT EMC EMC BT (150)Tj 9 0 0 9 548.3564 225.8898 Tm BT -.02 Tc ( )Tj EMC BT 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 ET (21)Tj /P <>BDC 0 Tc 9 0 0 9 371.7696 390.8898 Tm 7 0 0 7 440.3636 518.9528 Tm 7 0 0 7 54.7071 496.7654 Tm /P <>BDC BT Q either 907 or 453kg, NG fuel gauges can give messages such as ( )Tj 0 Tc ET ET /P <>BDC ET BT BT BT ( )Tj BT 9 0 0 9 53.8338 390.8898 Tm EMC EMC ET /P <>BDC 9 0 0 9 165.1533 258.8898 Tm ET EMC ET BT BT ET /P <>BDC EMC .7 -.5345 .9114 -1.2305 y ET EMC -.02 Tc ET /P <>BDC BT BT ( )Tj ET EMC /P <>BDC ET /P <>BDC 7 0 0 7 539.8962 727.9528 Tm 7 0 0 7 54.7071 397.7654 Tm BT )]TJ BT Also looking for the materials used for the front windscreen? ( )Tj 9 0 0 9 537.6801 258.8898 Tm ( )Tj .559 .331 .619 rg ( )Tj 7 0 0 7 387.0159 661.9528 Tm EMC /P <>BDC EMC ( )Tj /F4 1 Tf EMC ET /P <>BDC BT ET /P <>BDC ( )Tj ET EMC 9 0 0 9 274.8953 313.8898 Tm /P <>BDC /P <>BDC 6.5 0 0 6.5 90.4525 663.9529 Tm 7 0 0 7 476.1204 694.9528 Tm ET ( )Tj )Tj 9 0 0 9 53.8578 291.8898 Tm EMC BT ( )Tj BT 7 0 0 7 43.6039 243.9528 Tm 9 0 0 9 411.0097 93.8898 Tm BT BT BT /P <>BDC EMC 8 0 0 8 296.665 771.9529 Tm /GS2 gs -.02 Tc tank. BT BT ( )Tj /P <>BDC /P <>BDC EMC ET ET 7 0 0 7 429.157 562.9528 Tm /P <>BDC (410)Tj ET 0 Tc EMC ET differential pressure (and bleed air as a backup) is used to maintain a head of pressure in the EMC )Tj 9 0 0 9 212.2888 93.8898 Tm 10 0 0 10 37.304 794.2914 Tm EMC ( )Tj BT EMC ( )Tj /P <>BDC q 1 0 0 1 36.85 797.54 cm 0 0 m ET 0 Tc ( )Tj /P <>BDC ET 9 0 0 9 374.2479 71.8898 Tm /P <>BDC ( )Tj /P <>BDC EMC 7 0 0 7 59.2108 11.5129 Tm ET (operate with first, economy-plus and)Tj EMC 6 0 0 6 496.2633 673.9528 Tm ET /P <>BDC BT (A321neo:)Tj BT ( )Tj ET EMC /P <>BDC 7 0 0 7 247.7395 529.7654 Tm /P <>BDC /P <>BDC 7 0 0 7 294.4014 639.7654 Tm (0.0112)Tj EMC /P <>BDC ( )Tj ET /P <>BDC (551)Tj -.02 Tc /P <>BDC ET EMC ET -.02 Tc /P <>BDC BT 7 0 0 7 445.619 617.7654 Tm ET (0.0130)Tj ET BT 9 0 0 9 381.9109 456.8898 Tm /P <>BDC EMC -.02 Tc EMC EMC 0 Tc 9 0 0 9 551.4784 797.8898 Tm (Block time - mins)Tj (hugely successful. /P <>BDC /P <>BDC BT 7 0 0 7 429.157 540.9528 Tm EMC Have you got any exact places or web address please? BT ET ET BT BT BT EMC -.02 Tc BT /P <>BDC EMC [(OM)8.1(M)-12.9(E)-24.9(R)7.1(C)8.1(E)]TJ BT EMC ET ET 9 0 0 9 533.576 236.8898 Tm /F6 1 Tf EMC ET /F1 1 Tf ( )Tj EMC Regarding winglets, I think Simple Flying explains it well. -.02 Tc ( )Tj EMC ET 0 Tc /P <>BDC ET 431 0 obj (1,824)Tj (weights used are an MTOW of)Tj 9 0 0 9 53.8578 236.8898 Tm EMC ET /P <>BDC BT 9 0 0 9 232.438 489.8898 Tm EMC [(Aircr)10(aft)]TJ /P <>BDC 7 0 0 7 543.7693 11.5132 Tm EMC -.02 Tc 6 0 0 6 352.5857 659.9528 Tm 9 0 0 9 198.192 599.8898 Tm ( )Tj BT EMC ET ET EMC /P <>BDC 7 0 0 7 439.2087 199.9528 Tm EMC (improved engine efficiency and offer)Tj BT 6 0 0 6 495.9995 659.9528 Tm /P <>BDC (404)Tj ( N)Tj 7 0 0 7 82.8504 144.9528 Tm 9 0 0 9 51.0315 324.8898 Tm /P <>BDC 7 0 0 7 474.7064 100.9528 Tm ET -.02 Tc ET ET /P <>BDC ET EMC 0 Tc /P <>BDC ET ET 7 0 0 7 507.7893 210.7654 Tm -.01 Tc 9 0 0 9 290.9113 324.8898 Tm EMC EMC /P <>BDC 7 0 0 7 294.4014 430.7654 Tm BT 9 0 0 9 394.0157 93.8898 Tm -.02 Tc (371,552)Tj BT ( )Tj ET /P <>BDC /TT2 1 Tf 7 0 0 7 277.3936 265.9528 Tm 6 0 0 6 258.3167 757.9528 Tm (39,270lbs)Tj (408)Tj (29,432)Tj BT /P <>BDC /P <>BDC 7 0 0 7 82.8504 89.9528 Tm 6 0 0 6 490.4508 729.9528 Tm 0 Tc ( )Tj (34,650)Tj 9 0 0 9 189.1853 302.8898 Tm BT /P <>BDC /F1 1 Tf 6.5 0 0 6.5 191.7926 702.9529 Tm /P <>BDC BT /P <>BDC ( )Tj ( )Tj BT BT 7 0 0 7 537.7804 331.9528 Tm /GS2 gs ET 7 0 0 7 344.1175 595.7654 Tm EMC 9 0 0 9 68.3339 544.8898 Tm EMC BT ET .661 .752 .896 rg 7 0 0 7 158.74 122.7654 Tm When this runs dry the scavenge EMC BT (page\))Tj ET BT ( )Tj /F7 1 Tf /F7 1 Tf -.02 Tc thanks for stopping by. ET BT /P <>BDC ( )Tj ET (3,850)Tj BT EMC ET 0 Tc 6.5 0 0 6.5 171.7493 689.9529 Tm BT BT 9 0 0 9 552.5493 357.8898 Tm ET BT 9 0 0 9 232.4217 412.8898 Tm -.02 Tc ET BT q 1 0 0 1 36.85 513.878 cm 0 0 m 9 0 0 9 215.4409 93.8898 Tm 6.5 0 0 6.5 174.4663 735.9529 Tm BT ET ( )Tj 10 0 0 10 36.8504 814.1973 Tm /P <>BDC 0 Tc /P <>BDC 9 0 0 9 394.0123 280.8898 Tm BT 9 0 0 9 246.595 302.8898 Tm 7 0 0 7 241.5317 210.9528 Tm ( )Tj /P <>BDC ET BT ( )Tj BT ET 394.516 71.673 160.63 -39.992 re ET ET 9 0 0 9 544.9208 280.8898 Tm EMC BT EMC ( )Tj 9 0 0 9 36.8583 456.8898 Tm BT EMC BT 0 Tc 7 0 0 7 241.5317 221.9528 Tm /P <>BDC EMC 6.5 0 0 6.5 399.2659 565.9529 Tm 9 0 0 9 424.4247 764.8898 Tm 7 0 0 7 99.8582 441.7654 Tm ET 304.725 420.96 m BT ( )Tj EMC EMC ( N)Tj BT ( )Tj EMC ( )Tj ET BT EMC EMC ET EMC BT ET 7 0 0 7 107.1165 474.9528 Tm 9 0 0 9 545.0725 434.8898 Tm ET /P <>BDC /P <>BDC ET EMC EMC 9 0 0 9 182.7142 247.8898 Tm 9 0 0 9 551.4604 269.8898 Tm BT BT BT /P <>BDC ET ET -.01 Tc (cabin interior enhancements and changes)Tj -.02 Tc ( )Tj /P <>BDC ET ET /P <>BDC /P <>BDC EMC EMC EMC /P <>BDC /P <>BDC (difference. BT BT -.02 Tc BT EMC /P <>BDC ET 7 0 0 7 82.8504 364.9528 Tm ET EMC BT 9 0 0 9 232.438 236.8898 Tm q ET ( )Tj EMC /P <>BDC 7 0 0 7 53.8582 11.5132 Tm 6.5 0 0 6.5 243.8814 663.9529 Tm BT ET ET BT ET -.02 Tc /P <>BDC EMC /P <>BDC 9 0 0 9 394.0123 104.8898 Tm 0 Tc /GS2 gs BT 7 0 0 7 316.0679 243.7654 Tm ET EMC 7 0 0 7 82.8504 100.9528 Tm /P <>BDC /P <>BDC ( )Tj EMC ET ET ET BT 7 0 0 7 99.8582 386.7654 Tm 7 0 0 7 295.2833 199.7654 Tm ET ET ET /P <>BDC -.01 Tc EMC (3,443)Tj BT /P <>BDC ET EMC /P <>BDC BT ET BT BT EMC 8 0 0 8 124.845 661.9528 Tm ( )Tj ET BT /P <>BDC BT ET 9 0 0 9 394.0123 401.8898 Tm 6 0 0 6 496.3652 743.9528 Tm EMC ET 9 0 0 9 549.8977 313.8898 Tm ET BT 9 0 0 9 550.3917 456.8898 Tm 9 0 0 9 411.0181 170.8898 Tm ET ET EMC ET ET .008 Tc each engine. BT (0.0129)Tj EMC 0 Tc EMC /P <>BDC 7 0 0 7 258.2805 441.7654 Tm /P <>BDC 6 0 0 6 459.5796 729.9528 Tm 7 0 0 7 459.6601 11.5129 Tm ET EMC /P <>BDC BT BT 9 0 0 9 192.1373 401.8898 Tm ET /P <>BDC /P <>BDC BT EMC BT ( )Tj /P <>BDC ( )Tj /P <>BDC ET BT ET BT 9 0 0 9 362.0968 324.8898 Tm ( )Tj ET EMC 9 0 0 9 53.8582 236.8898 Tm BT ET BT ( )Tj ( )Tj BT 0 Tc BT (0.0158)Tj /P <>BDC ( )Tj 9 0 0 9 382.7137 93.8898 Tm ( )Tj /P <>BDC /P <>BDC ( )Tj 7 0 0 7 54.7071 628.7654 Tm BT 7 0 0 7 355.5753 584.7654 Tm ( )Tj (737-800W)Tj .014984 841.89 609.45 -841.89 re BT 6.5 0 0 6.5 499.4674 742.9529 Tm ET EMC ET ( )Tj ET ( )Tj /P <>BDC BT -.02 Tc -.02 Tc EMC 0 Tc ET soaked fuel causing frost to form on the wings during the turnarounds - even in EMC BT ( )Tj 9 0 0 9 566.3417 423.8898 Tm 9 0 0 9 191.0032 225.8898 Tm /P <>BDC /P <>BDC BT EMC /P <>BDC EMC EMC 6 0 0 6 61.517 743.9528 Tm /P <>BDC 56.25 0 0 56.25 36.8583 489.8898 Tm 0 Tc /P <>BDC /P <>BDC 6.5 0 0 6.5 387.561 532.9529 Tm /P <>BDC ET (the A320ceo. 9 0 0 9 377.4586 676.8898 Tm ( )Tj (39,270)Tj BT 7 0 0 7 241.2727 177.9528 Tm /P <>BDC 0 Tc -.02 Tc 6 0 0 6 106.1775 729.9528 Tm EMC 0 Tc EMC 8 0 0 8 136.4919 661.9528 Tm EMC EMC 7 0 0 7 158.74 595.7654 Tm /OC /MC1957 BDC ( )Tj ET EMC ET ET /P <>BDC 9 0 0 9 394.0315 775.8898 Tm /P <>BDC ET (CFM56-7B27B3)Tj 0 Tc EMC /P <>BDC 7 0 0 7 364.1531 122.9528 Tm EMC ET ( )Tj ET ( )Tj 7 0 0 7 363.2711 518.9528 Tm ET BT ( )Tj 7 0 0 7 82.2047 507.9528 Tm 9 0 0 9 534.7124 401.8898 Tm /P <>BDC BT /P <>BDC 7 0 0 7 344.1175 573.7654 Tm ( )Tj EMC (977)Tj /P <>BDC /P <>BDC 6.5 0 0 6.5 54.877 689.9529 Tm (34,650)Tj [(CFM L)17.1(E)-8.1(AP-1B27)]TJ EMC ( )Tj ET ET /P <>BDC EMC /P <>BDC 7 0 0 7 258.2805 111.7654 Tm 9 0 0 9 36.8504 280.8898 Tm ET EMC ET EMC BT EMC EMC BT ( )Tj (737-8)Tj BT ET BT BT EMC ET 6 0 0 6 215.4988 701.9528 Tm EMC BT EMC ET BT ET /P <>BDC EMC /P <>BDC /P <>BDC EMC /P <>BDC ET /P <>BDC ET BT /P <>BDC 56 0 0 56 447.1169 682.1944 Tm EMC ( )Tj ET ET EMC 6 0 0 6 495.9463 771.9528 Tm (0.0177)Tj (39,270lbs)Tj ET BT EMC ET 9 0 0 9 68.0314 258.8898 Tm 9 0 0 9 215.4409 511.8898 Tm BT ET EMC ( )Tj ET EMC EMC ET /P <>BDC [(UG)-17.1(U)-8(S)8.1(T)]TJ BT The wheel track, which is the distance between the main wheels is 5.25 metres. EMC ET ET BT BT ET ET 0 Tc ET 7 0 0 7 131.6494 672.7654 Tm /P <>BDC ET 7 0 0 7 297.632 705.9528 Tm /OC /MC2 BDC /P <>BDC ( )Tj 7 0 0 7 315.1859 89.7654 Tm (170)Tj ET BT (1,272)Tj ET /P <>BDC ET ET BT BT achievable with standard SG's. EMC (176)Tj 9 0 0 9 196.8174 390.8898 Tm EMC /P <>BDC EMC (greater improvement in fuel burn on the)Tj /P <>BDC ( )Tj /P <>BDC BT BT /P <>BDC ET BT /P <>BDC 0 Tc ( )Tj ( )Tj /P <>BDC 9 0 0 9 187.2574 302.8898 Tm BT (All the flights were in a westerly)Tj 9 0 0 9 542.1815 786.8898 Tm 7 0 0 7 204.0935 331.7654 Tm BT /P <>BDC EMC 7 0 0 7 141.7322 661.9528 Tm -.02 Tc ET ET 7 0 0 7 99.8582 199.7654 Tm ET /P <>BDC 13 0 0 13 215.4409 60.8898 Tm (34,650)Tj /P <>BDC /P <>BDC EMC The cause of the accident was determined to be a malfunctioning left radar altimeter. 7 0 0 7 298.514 617.9528 Tm 7 0 0 7 387.0932 221.9528 Tm EMC 0 Tc ET 9 0 0 9 53.8338 148.8898 Tm EMC BT EMC ET BT 7 0 0 7 520.6108 639.9528 Tm ET ET /P <>BDC /P <>BDC EMC 9 0 0 9 394.0315 214.8898 Tm EMC 7 0 0 7 387.0159 617.9528 Tm ET 0 Tw ET BT (20)Tj (35,112)Tj /P <>BDC (39,270)Tj BT /P <>BDC ( )Tj /P <>BDC BT EMC BT 7 0 0 7 537.7804 166.9528 Tm EMC 0 Tc EMC ( )Tj (evaluation it has been assumed that the)Tj ET ET 9 0 0 9 177.6653 445.8898 Tm ET EMC ( )Tj 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 ET (CFM56-5B3/P)Tj BT ( )Tj S ( )Tj EMC BT 9 0 0 9 36.8504 269.8898 Tm (170)Tj /P <>BDC EMC EMC 0 Tc (payload reduction. /P <>BDC 9 0 0 9 36.8504 346.8898 Tm /P <>BDC /P <>BDC 7 0 0 7 439.7405 485.9528 Tm EMC ET ET [(CFM L)17.1(E)-8.1(AP-1A26)]TJ BT /P <>BDC ET EMC BT BT Thank you so much. /P <>BDC BT 7 0 0 7 59.2108 11.5129 Tm ET 7 0 0 7 539.8962 518.9528 Tm /P <>BDC ET BT 9 0 0 9 360.5848 104.8898 Tm 9 0 0 9 411.0181 159.8898 Tm EMC BT /P <>BDC ET EMC (737-900ER\(W\) has an MTOW of)Tj BT ET /P <>BDC ET BT BT EMC This)Tj 10 0 0 10 47.7404 814.1973 Tm 7 0 0 7 82.2047 540.9528 Tm (0.0123)Tj ( )Tj 7 0 0 7 337.7614 100.7654 Tm /P <>BDC (35,112)Tj ET (travelled for the aircraft on each route is)Tj BT 9 0 0 9 527.3853 709.8898 Tm EMC /P <>BDC BT wing surface (rain, drizzle, snow, fog). EMC (in a more efficient engine. /P <>BDC EMC 0 Tc -.02 Tc -.02 Tc Q /P <>BDC EMC (thrust. BT 9 0 0 9 163.2471 269.8898 Tm BT 0 Tc 9 0 0 9 182.8403 93.8898 Tm /P <>BDC /P <>BDC ET ET )Tj 9 0 0 9 215.433 368.8898 Tm (150)Tj /P <>BDC ( A)Tj /F6 1 Tf ET 7 0 0 7 439.7405 617.9528 Tm /P <>BDC BT BT 6 0 0 6 466.3124 757.9528 Tm (the engine option chosen for this study is)Tj ET EMC 0 Tc ( )Tj (1,019)Tj 7 0 0 7 54.7071 331.7654 Tm BT ET /P <>BDC ET EMC EMC EMC EMC ET BT -.01 Tc EMC EMC BT ( )Tj ET (9.0:1)Tj BT -.02 Tc [(737-900E)-33(R\(W)-19(\):)]TJ /P <>BDC Hello, do you know the meaning of the 737-8K5 designation and its background? EMC )Tj EMC Thank you. ET S BT EMC ( )Tj (171,520)Tj ( )Tj 7 0 0 7 404.101 188.7654 Tm ET BT /GS2 gs ( )Tj BT BT /P <>BDC BT /P <>BDC ET BT ( )Tj ET ( )Tj EMC EMC ET /P <>BDC ET BT ET ET ET -.01 Tc EMC EMC 7 0 0 7 487.0872 11.5129 Tm ET 9 0 0 9 344.8161 214.8898 Tm BT -.01 Tc /P <>BDC 9 0 0 9 36.8504 390.8898 Tm [(E)-7.8(P)16.1(T)9(E)-13.9(MBE)-16.9(R)]TJ ET ET /P <>BDC .151 .147 .15 rg /P <>BDC ET (will take into account the additional)Tj ET ET /P <>BDC /P <>BDC (31,416)Tj 7 0 0 7 158.74 276.7654 Tm ( )Tj BT BT 6 0 0 6 309.5222 701.9528 Tm BT EMC EMC 9 0 0 9 36.8583 478.8898 Tm ET (1,824)Tj 8 0 0 8 334.994 619.9528 Tm BT EMC ET EMC 0 Tc /P <>BDC 6 0 0 6 403.4411 757.9528 Tm BT EMC -.02 Tc /P <>BDC (burn and operating)Tj 0 Tc (0.0134)Tj BT /P <>BDC ( )Tj ET (A320neo)Tj BT [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ ET ET BT Q EMC EMC The Boeing 737-800 is one of the most popular choices for passenger transport on the market today priced in at 82 million dollars. 7 0 0 7 37.5838 551.9528 Tm (737-8)Tj /P <>BDC /P <>BDC /P <>BDC ( )Tj (fan diameter of 78 inches, and a bypass)Tj 7 0 0 7 338.3085 375.9528 Tm /P <>BDC /P <>BDC 0 Tc 7 0 0 7 320.7537 144.9528 Tm /P <>BDC EMC /P <>BDC 0 Tc ET EMC ( )Tj ET ET BT ( )Tj /P <>BDC (342,312)Tj 0 Tc /P <>BDC BT /P <>BDC EMC /P <>BDC BT (A321ceo)Tj BT [(Airlines acr)10(oss the world ar)10(e r)10(eturning their eets to ser)-25.9(vice. 0 Tc ET BT 9 0 0 9 232.4217 280.8898 Tm ET EMC ET 0 Tc ET /P <>BDC /P <>BDC BT EMC EMC BT BT ET EMC ET ET 7 0 0 7 316.0679 320.7654 Tm 7 0 0 7 521.4089 11.5132 Tm BT /P <>BDC /P <>BDC /OC /MC5080 BDC ( )Tj ( )Tj 9 0 0 9 372.4012 412.8898 Tm ( )Tj /P <>BDC EMC /P <>BDC BT /P <>BDC /P <>BDC EMC BT ( )Tj 6 0 0 6 403.0689 729.9528 Tm -.02 Tc ET /P <>BDC BT 7 0 0 7 338.6433 386.7654 Tm EMC BT ( )Tj EMC (at 27,000lbs thrust compared to the)Tj ET -.02 Tc /P <>BDC ET 7 0 0 7 148.0554 11.5132 Tm .151 .147 .15 rg BT (A320ceo. /P <>BDC ET (-60)Tj It is simply an 800 with certain modifications that might have been stipulated by the customer airliner. /P <>BDC ET 9 0 0 9 411.0097 192.8898 Tm BT ET EMC (makes a flight-for-flight comparison)Tj EMC EMC /P <>BDC EMC /P <>BDC BT 10 0 0 10 36.8504 814.1973 Tm BT EMC EMC 9 0 0 9 531.3621 148.8898 Tm ET (2,601)Tj /P <>BDC ET ET BT 7 0 0 7 99.8582 144.7654 Tm 9 0 0 9 194.9081 346.8898 Tm 7 0 0 7 539.8962 672.9528 Tm EMC /GS2 gs BT /P <>BDC /P <>BDC ( )Tj BT <> ET EMC (OEW being 6,500lbs higher. (that in real airline operations the taxi-out)Tj BT (39,270lbs)Tj BT EMC /P <>BDC ( )Tj -.02 Tc /P <>BDC 10 0 0 10 420.16 814.1973 Tm to test 7 0 0 7 179.5605 122.9528 Tm 7 0 0 7 518.4953 342.9528 Tm -.02 Tc EMC ET EMC the permissible CSFF area, the outside air temperature is above freezing(0 C, 32 ( )Tj /P <>BDC BT EMC 7 0 0 7 518.4953 122.9528 Tm ET /P <>BDC EMC 0 841.89 609.449 -841.89 re ( )Tj -.9858 .528 -.35 .3166 0 0 c EMC ( )Tj EMC /OC /MC225 BDC ( )Tj EMC /P <>BDC /P <>BDC (the relative fuel costs between the aircraft)Tj 6 0 0 6 319.5607 715.9528 Tm ET EMC BT ET /P <>BDC 9 0 0 9 385.6838 346.8898 Tm /P <>BDC 0 Tc /P <>BDC BT /P <>BDC EMC /P <>BDC EMC EMC (CFM56-5B4/P)Tj ET 7 0 0 7 327.1097 628.9528 Tm 0 Tc EMC BT EMC 6 0 0 6 247.27 771.9528 Tm /P <>BDC (150)Tj /P <>BDC Other data such as fuel load, -.02 Tc BT EMC <>/XObject<>/ExtGState<>/Properties<>>> EMC BT ( )Tj )Tj ET /P <>BDC BT ET ET .176 .307 .621 rg /P <>BDC EMC ET 9 0 0 9 383.6209 423.8898 Tm ET 583 0 obj 7 0 0 7 535.5029 188.7654 Tm /P <>BDC 0 Tc EMC EMC ( )Tj BT 9 0 0 9 534.6123 302.8898 Tm -.02 Tc ET EMC ET 9 0 0 9 229.6141 302.8898 Tm ( )Tj ( )Tj 7 0 0 7 491.4046 320.9528 Tm BT -.015 Tc Q EMC /P <>BDC ( )Tj -.02 Tc .41 .161 .508 rg 7 0 0 7 490.8321 540.7654 Tm ET BT ET EMC 6.5 0 0 6.5 324.4345 650.9529 Tm ET ET /P <>BDC [(OM)8(M)-13(E)-25(R)7(C)8(E)]TJ 0 Tc BT BT (. ET /P <>BDC EMC ( )Tj /P <>BDC BT 9 0 0 9 408.1854 676.8898 Tm 9 0 0 9 53.8578 214.8898 Tm /P <>BDC EMC 9 0 0 9 394.0315 698.8898 Tm /P <>BDC BT 6 0 0 6 371.479 757.9528 Tm For example, the)Tj ET 7 0 0 7 535.5029 221.7654 Tm ET /P <>BDC BT BT BT 9 0 0 9 215.4409 203.8898 Tm ET 7 0 0 7 258.2805 617.7654 Tm ET [(r)10(atio)]TJ 7 0 0 7 241.2727 573.9528 Tm EMC /P <>BDC ( )Tj ( )Tj 9 0 0 9 394.0315 654.8898 Tm EMC 0 Tc EMC ET ( )Tj ET ET BT 7 0 0 7 43.6039 540.9528 Tm -.02 Tc ET BT 7 0 0 7 299.0601 232.9528 Tm EMC /P <>BDC [(C)17.1(OS/104)]TJ BT 9 0 0 9 115.2588 214.8898 Tm /P <>BDC ( )Tj EMC [(737-900E)-33(R)]TJ ET BT EMC (136)Tj (1,938)Tj ( )Tj EMC 73 0 obj ET ET ET ET -.02 Tc /P <>BDC ET EMC /P <>BDC EMC EMC /P <>BDC /P <>BDC (163)Tj BT BT ( )Tj ET ET /P <>BDC ET 6.5 0 0 6.5 499.597 585.9529 Tm BT ET EMC BT ET BT EMC /F4 1 Tf ET ET /P <>BDC ET 9 0 0 9 548.4937 71.8898 Tm EMC ET 0 Tc 9 0 0 9 546.1516 445.8898 Tm 7 0 0 7 428.6112 386.9528 Tm 9 0 0 9 548.6884 137.8898 Tm BT The seat configuration used in)Tj 6 0 0 6 309.4863 659.9528 Tm ET ( )Tj EMC 0 Tc (138,300)Tj (0.0141)Tj BT ET ET 9 0 0 9 53.8578 489.8898 Tm BT /P <>BDC BT BT EMC ET ET /P <>BDC EMC 9 0 0 9 411.0234 698.8898 Tm EMC ET (31,416)Tj <>stream BT BT ET EMC ( )Tj /P <>BDC 0 Tc -.02 Tc 7 0 0 7 379.3969 210.7654 Tm EMC /P <>BDC ( )Tj BT ( )Tj 9 0 0 9 299.3893 478.8898 Tm 7 0 0 7 439.2087 386.9528 Tm /P <>BDC (The improvements in engine design)Tj EMC /P <>BDC ET EMC ET [(A3)24.9(20neo)]TJ -.02 Tc EMC ET BT /P <>BDC BT BT ( )Tj BT 53.858 511.715 518.74 293.325 re BT hi! BT ( )Tj EMC 5.25 0 0 5.25 492.6848 11.5129 Tm (capacity of 160 \(the same as the 737-800\))Tj ( )Tj (157)Tj ( )Tj BT BT BT BT 0 Tc 7 0 0 7 491.392 573.9528 Tm ET ( )Tj ( )Tj (34,650)Tj BT /P <>BDC BT EMC EMC BT 0 Tc ( )Tj EMC ET ( )Tj ET BBJ Aux fuel panel located on Capt's & F/O's main EMC BT 9 0 0 9 455.2971 478.8898 Tm /OC /MC5093 BDC It also boasts a 3,060 Nautical Mile or 5,667 Kilometers travel range. EMC EMC ( )Tj ET must be switched OFF when both LP lights illuminate. EMC BT EMC BT (136)Tj EMC .559 .331 .619 rg EMC /P <>BDC (3,465)Tj ET EMC 7 0 0 7 491.7142 463.7654 Tm ET (period in 2020. BT ET EMC safest way forward, but is very expensive and possibly impractical. (136)Tj 10 0 0 10 38.6761 771.9528 Tm ( )Tj 7 0 0 7 457.0984 595.7654 Tm BT BT ET /P <>BDC ET ET EMC BT 0 Tc 9 0 0 9 368.9994 225.8898 Tm /P <>BDC ET 9 0 0 9 351.8271 203.8898 Tm ET 6.5 0 0 6.5 398.3298 650.9529 Tm BT BT ( )Tj ( )Tj BT ET EMC ET /P <>BDC /P <>BDC BT EMC BT 8 0 0 8 124.845 717.9528 Tm 8 0 0 8 543.5282 797.8898 Tm 6 0 0 6 418.9814 673.9528 Tm 7 0 0 7 387.0159 474.9528 Tm ( )Tj ( )Tj (1,800 - )Tj 9 0 0 9 382.4508 159.8898 Tm /P <>BDC (significant enough that operating the)Tj ET ( )Tj ET (98-107)Tj (7B26)Tj ( )Tj BT EMC ET 9 0 0 9 377.4407 764.8898 Tm /P <>BDC -.02 Tc BT EMC ET /P <>BDC EMC BT EMC ( )Tj All the aircraft would therefore)Tj /P <>BDC 0 Tc The engine)Tj (-58)Tj BT (151)Tj ( )Tj /P <>BDC EMC ET BT 7 0 0 7 279.1575 617.9528 Tm EMC ET -.02 Tc /P <>BDC EMC 0 Tc ( )Tj (4,329)Tj BT -.005 Tc BT ET EMC 7 0 0 7 383.0719 705.7654 Tm ( )Tj ( )Tj 7 0 0 7 99.5912 705.9528 Tm /P <>BDC ET /P <>BDC ET /P <>BDC /P <>BDC 7 0 0 7 491.4046 122.9528 Tm BT ET EMC BT EMC BT 0 Tc 7 0 0 7 338.6433 408.7654 Tm /P <>BDC EMC ET /P <>BDC (this page\))Tj /P <>BDC /F6 1 Tf BT BT ET EMC /P <>BDC ET 0 Tc ET ET 6 0 0 6 286.5632 771.9528 Tm (136)Tj ET /P <>BDC 9 0 0 9 394.0315 467.8898 Tm 7 0 0 7 456.4753 738.7654 Tm /P <>BDC BT BT ( )Tj ( )Tj 9 0 0 9 394.0315 126.8898 Tm ( )Tj (104)Tj ( )Tj BT EMC /P <>BDC EMC 9 0 0 9 552.5356 445.8898 Tm 6 0 0 6 538.428 771.9528 Tm EMC EMC /P <>BDC 8 0 0 8 276.7109 633.9528 Tm ( )Tj ET ET /P <>BDC ET 9 0 0 9 529.6118 302.8898 Tm BT (170)Tj (than 3% on the shorter sectors, but as the)Tj ET -.02 Tc 0 841.89 609.449 -841.89 re /P <>BDC 0 Tc EMC BT ET ET /P <>BDC ET ( )Tj BT ( )Tj BT 0 Tc BT ET EMC (104)Tj (scheduled times planned by the carrier may)Tj BT EMC (0.0282)Tj BT ET ET BT -.01 Tc /P <>BDC 6 0 0 6 278.7028 659.9528 Tm ET /P <>BDC 9 0 0 9 430.7427 687.8898 Tm ET ( )Tj endobj 7 0 0 7 118.104 705.7654 Tm ET /P <>BDC ET BT ET /P <>BDC ( )Tj ET 9 0 0 9 186.5212 225.8898 Tm /P <>BDC the rear of the fwd hold and the front of the aft hold, this reduces the C of G ET -.02 Tc 0 Tc /P <>BDC Greetings. These are: Below is a table of the main features and specifications for the Boeing 737 family of aircraft. EMC 6.5 0 0 6.5 192.41 598.9529 Tm 0 Tc ( )Tj ( )Tj (977)Tj /P <>BDC EMC BT 7 0 0 7 338.6433 221.7654 Tm BT EMC 13 0 0 13 215.4409 445.8898 Tm ( )Tj /P <>BDC ( )Tj 10 0 0 10 52.6304 814.1973 Tm [(BOS-C)-8.1(V)18.1(G)]TJ 7 0 0 7 404.101 89.7654 Tm (same passenger payload. EMC ET ( )Tj 6 0 0 6 132.3631 659.9528 Tm The PPS flight)Tj /P <>BDC -.02 Tc /P <>BDC ( )Tj Digital Fuel Quantity Indicator Error Codes, Missing or disconnected tank EMC /P <>BDC -.02 Tc /P <>BDC /P <>BDC -.01 Tc (evaluation that are payload-limited on the)Tj ET ( )Tj 0 Tc ( )Tj BT ET EMC BT EMC (flight relate to fuel burn, overflight and)Tj ( )Tj EMC EMC EMC ET 6 0 0 6 61.517 701.9528 Tm (O)Tj 7 0 0 7 107.1165 661.9528 Tm /F6 1 Tf 0 Tc (900ER\(W\) has a 4.3% lower fuel burn)Tj /P <>BDC -.02 Tc EMC /P <>BDC (20)Tj BT 9 0 0 9 199.5582 38.8898 Tm BT BT 9 0 0 9 425.183 544.8898 Tm ( )Tj 9 0 0 9 363.4443 390.8898 Tm 7 0 0 7 297.632 661.9528 Tm (190,800)Tj ET /P <>BDC /P <>BDC BT ( )Tj EMC ET /P <>BDC /P <>BDC EMC EMC (\(see table, this)Tj ET 9 0 0 9 394.0315 390.8898 Tm Centre tank pumps ET /P <>BDC EMC /P <>BDC -.02 Tc BT EMC [(CFM L)17.1(E)-8.1(AP-1B27)]TJ /P <>BDC BT ET ET /P <>BDC 7 0 0 7 386.3929 694.9528 Tm 7 0 0 7 241.2727 474.9528 Tm BT ( )Tj /Im3 Do ET /F7 1 Tf BT 9 0 0 9 394.0157 544.8898 Tm /P <>BDC ET 9 0 0 9 201.162 500.8898 Tm /P <>BDC ( )Tj BT BT (39,270lbs)Tj EMC ( )Tj EMC ET EMC the aircraft data bus. EMC 0 Tc (performance on this sector is 2.19 cents per)Tj ET ET 8 0 0 8 394.0237 71.8898 Tm 9 0 0 9 394.0157 489.8898 Tm ET ET EMC /P <>BDC 9 0 0 9 545.8646 522.8898 Tm ET 8 0 0 8 43.6039 661.9528 Tm EMC EMC /P <>BDC ET ET BT /GS2 gs EMC EMC /P <>BDC ET ET 9 0 0 9 381.2556 500.8898 Tm ( )Tj 6 0 0 6 295.8268 673.9528 Tm BT EMC f 9 0 0 9 215.4313 269.8898 Tm -.02 Tc ET /P <>BDC 7 0 0 7 427.7291 111.9528 Tm EMC ( )Tj 7 0 0 7 354.6933 474.7654 Tm EMC )Tj /P <>BDC EMC (0.0153)Tj (217)Tj EMC 0 Tc BT ET 7 0 0 7 141.7322 496.9528 Tm 9 0 0 9 167.7561 192.8898 Tm EMC BT -.02 Tc BT BT ET 6.5 0 0 6.5 232.6392 735.9529 Tm /P <>BDC /P <>BDC /P <>BDC -.02 Tc ET BT ( )Tj ( )Tj ET EMC /P <>BDC 7 0 0 7 82.2047 584.9528 Tm 0 Tc EMC BT BT /P <>BDC BT /P <>BDC 7 0 0 7 343.2355 716.7654 Tm BT 9 0 0 9 36.8504 379.8898 Tm ( )Tj EMC ET ( )Tj ( )Tj -.02 Tc /P <>BDC BT ( )Tj EMC 0 Tc (19 seats more than the -800, and 13)Tj EMC ET .008 Tc ET EMC ET EMC EMC 6 0 0 6 246.9464 659.9528 Tm BT [(equal-siz)6.1(ed 737NG counterpar)-23(ts and A320ceo)]TJ ET 9 0 0 9 112.3045 346.8898 Tm 8 0 0 8 456.5927 771.7654 Tm /Artifact <>BDC EMC ET The A320neos ASM)Tj ET BT 9 0 0 9 411.0097 38.8898 Tm 5 0 0 5 92.725 11.5132 Tm EMC BT .014984 841.89 609.45 -841.89 re ( )Tj EMC BT 1 i /P <>BDC BT EMC 13 0 0 13 411.0234 786.8898 Tm /F1 1 Tf EMC 9 0 0 9 246.6113 401.8898 Tm (number of available seat-miles \(ASM\))Tj ET (737-800W)Tj BT EMC (MTOW and OEW. /P <>BDC BT /P <>BDC BT Our Math Says It Isn't. (4,158)Tj (A320ceo)Tj ET /P <>BDC EMC BT 7 0 0 7 508.2252 11.5129 Tm -.01 Tc /P <>BDC (31,416)Tj BT EMC ET 9 0 0 9 246.595 159.8898 Tm ET BT ( )Tj EMC 7 0 0 7 99.8582 529.7654 Tm ET ET ET /P <>BDC BT BT -.01 Tc /P <>BDC 8 0 0 8 339.6345 760.7654 Tm (\(ATC\) charges. EMC BT 9 0 0 9 411.0234 742.8898 Tm BT (187,700)Tj EMC ET /P <>BDC (CFM56-7B27B3)Tj ( )Tj EMC The)Tj ( )Tj BT ET /P <>BDC ET ET 7 0 0 7 354.4763 716.7654 Tm ( )Tj EMC (with 2,000 feet separation. BT BT 7 0 0 7 193.1059 287.9528 Tm /P <>BDC /P <>BDC 6.5 0 0 6.5 54.877 598.9529 Tm 6 0 0 6 339.7639 757.9528 Tm ET ET EMC /P <>BDC ET 137 )Tj ET ET (O)Tj EMC ET ET -.02 Tc /P <>BDC BT 8 0 0 8 241.2609 771.9528 Tm ( )Tj EMC BT 0 Tc EMC /P <>BDC ( )Tj BT 8 0 0 8 500.5689 771.9529 Tm 9 0 0 9 532.082 247.8898 Tm /P <>BDC ET ET BT 7 0 0 7 539.9176 11.5129 Tm (generated per route. 0 Tc /P <>BDC ET ET BT /P <>BDC [(SS)-9.1(U)8(E)]TJ /P <>BDC ET (737-8)Tj ( )Tj EMC 7 0 0 7 387.0159 727.9528 Tm What was the Super Sonic Transport (SST) Concorde plane?? ( )Tj 7 0 0 7 158.74 67.7654 Tm BT EMC (ratio of 11.0:1. ET BT EMC /P <>BDC ET 7 0 0 7 403.478 221.7654 Tm /P <>BDC ET BT ( )Tj ET /P <>BDC 0 Tc Q /P <>BDC EMC 7 0 0 7 199.5784 441.7654 Tm /P <>BDC 7 0 0 7 108.6215 364.9528 Tm -.005 Tc 7 0 0 7 326.2278 463.9528 Tm 7 0 0 7 199.5784 199.7654 Tm 7 0 0 7 241.5317 89.9528 Tm 9 0 0 9 68.3339 500.8898 Tm EMC -.02 Tc ET 8 0 0 8 412.41 771.9529 Tm ( )Tj BT (91,300)Tj ( )Tj ET BT EMC /P <>BDC 0 Tc /P <>BDC /P <>BDC 9 0 0 9 379.7078 588.8898 Tm 7 0 0 7 440.0906 276.9528 Tm 7 0 0 7 508.4124 276.7654 Tm EMC BT (A321neo)Tj /P <>BDC been many other improvements to wiring and FQIS. -.02 Tc ( )Tj 9 0 0 9 376.057 247.8898 Tm