(0.0129)Tj ET 0 Tc 7 0 0 7 294.4014 320.7654 Tm BT BT ET ET EMC BT /P <>BDC BT 0 Tc /P <>BDC EMC EMC BT /GS1 gs ET ET EMC ET EMC ( )Tj 9 0 0 9 215.4409 280.8898 Tm ( )Tj ( )Tj 6.5 0 0 6.5 192.3255 742.9529 Tm /P <>BDC EMC BT ET ET EMC -.01 Tc 7 0 0 7 404.101 430.7654 Tm BT EMC BT ET BT ( )Tj BT -.01 Tc /P <>BDC ( )Tj 6 0 0 6 184.3662 673.9528 Tm ( )Tj 7 0 0 7 37.6993 111.9528 Tm EMC EMC ET ET BT 7 0 0 7 383.0719 727.7654 Tm 7 0 0 7 507.7893 166.7654 Tm 7 0 0 7 521.4928 727.9528 Tm 9 0 0 9 152.6787 566.8898 Tm -.02 Tc ET ET ( )Tj 0 Tc ( )Tj /P <>BDC EMC BT ( )Tj (177)Tj 10 0 0 10 230.6475 794.2914 Tm EMC (148,504)Tj 6jf/+6*Pe/[LeaVSjtLZ6*vXQ9b;(P+L(vV^V;,]2^JsGHqp]]&MDK1B39?ZVM,9P=2/ Zz>\\.. [(737-900E)-33(R)]TJ /P <>BDC ET The Boeing 737-800 is an example of an average sized airplane. /P <>BDC 9 0 0 9 232.4217 170.8898 Tm 0 Tc 7 0 0 7 386.4701 408.9528 Tm /P <>BDC -.02 Tc BT 5.25 0 0 5.25 73.853 11.5132 Tm -.02 Tc BT The fuel panels for the various series have not changed much over 9 0 0 9 394.0157 522.8898 Tm EMC EMC EMC /P <>BDC /P <>BDC ET /F4 1 Tf 9 0 0 9 534.7515 599.8898 Tm -.02 Tc EMC EMC /P <>BDC ET /P <>BDC BT (. ET EMC 17 0 0 17 560.3929 742.1944 Tm EMC 9 0 0 9 196.1514 390.8898 Tm Boeing 737 Assembly, the building of this popular City Jet. BT 6 0 0 6 302.9128 729.9528 Tm -.02 Tc 9 0 0 9 536.4271 60.8898 Tm ( )Tj /P <>BDC EMC -.02 Tc /P <>BDC 9 0 0 9 232.4217 566.8898 Tm 9 0 0 9 408.1854 610.8898 Tm 6.5 0 0 6.5 90.4525 676.9529 Tm ET /P <>BDC EMC -.02 Tc happened. -.02 Tc ET EMC /P <>BDC /P <>BDC BT 9 0 0 9 215.433 192.8898 Tm 9 0 0 9 205.6978 291.8898 Tm ET /P <>BDC BT ET (0.0137)Tj BT ET BT ET 9 0 0 9 246.595 423.8898 Tm EMC BT ET /P <>BDC ( )Tj ET 9 0 0 9 232.4408 720.8898 Tm ET EMC /P <>BDC BT BT endobj -.02 Tc BT BT ( )Tj /P <>BDC 8 0 0 8 136.5171 758.9528 Tm ET 0 Tc -.02 Tc 6.5 0 0 6.5 296.2827 598.9529 Tm ET ET EMC /P <>BDC EMC ET EMC EMC ( )Tj EMC ( )Tj ( )Tj ET EMC 8 0 0 8 394.0157 764.8898 Tm EMC BT EMC ET [(CFM L)17.1(E)-8.1(AP-1B27)]TJ ET EMC I am looking forward to your responses. BT ( )Tj 7 0 0 7 241.5317 210.9528 Tm EMC EMC ET /Im2 Do ET ( )Tj 0 Tc ( )Tj -.02 Tc -.02 Tc ( )Tj (1,960)Tj -.02 Tc 9 0 0 9 464.4377 621.8898 Tm BT [(P)11(ayload)]TJ ET 8 0 0 8 187.3427 675.9528 Tm ( )Tj /P <>BDC ET ET /P <>BDC ( )Tj /OC /MC4591 BDC /Artifact <>BDC EMC (1,130)Tj ET (0.0129)Tj ( )Tj )Tj (3,465)Tj -.02 Tc 7 0 0 7 316.0679 221.7654 Tm ( )Tj %
ET (124,650)Tj 9 0 0 9 53.8578 247.8898 Tm i would like to know the dimension of both nose and main landing gear crates also the approximate weight of the shipment. BT 7 0 0 7 314.6398 705.7654 Tm (4,163)Tj EMC 9 0 0 9 53.8338 115.8898 Tm 9 0 0 9 394.0315 412.8898 Tm /P <>BDC ET 7 0 0 7 326.2278 683.9528 Tm ( )Tj 7 0 0 7 326.2278 540.9528 Tm BT /P <>BDC BT S 9 0 0 9 526.8813 445.8898 Tm ET ( )Tj .151 .147 .15 rg -.01 Tc 7 0 0 7 327.1097 617.9528 Tm /P <>BDC 0 Tc BT /P <>BDC ET EMC EMC -.01 Tc EMC EMC ET ( )Tj BT -.02 Tc 0 Tc EMC EMC EMC EMC -.02 Tc /P <>BDC EMC /P <>BDC 8 0 0 8 549.2646 49.8898 Tm /P <>BDC 8 0 0 8 38.4438 577.9528 Tm ET As a result of its lower fuel burn,)Tj ET -.01 Tc EMC EMC ( )Tj EMC EMC /P <>BDC 8 0 0 8 505.7415 771.9528 Tm BT /F4 1 Tf /P <>BDC ( )Tj 9 0 0 9 376.2498 478.8898 Tm BT EMC /P <>BDC ET /P <>BDC ET /P <>BDC The wheel track, which is the distance between the main wheels is 5.25 metres. /P <>BDC EMC -.02 Tc BT BT EMC ET 7 0 0 7 537.7804 386.9528 Tm /P <>BDC The reductions in fuel burn also)Tj /P <>BDC EMC 8 0 0 8 540.2806 60.8898 Tm ET ET 7 0 0 7 242.0225 430.9528 Tm EMC ( )Tj BT 7 0 0 7 338.6433 133.7654 Tm BT 9 0 0 9 562.1829 236.8898 Tm /P <>BDC (104)Tj 7 0 0 7 37.0536 507.9528 Tm EMC q 1 0 0 1 394.012 84.878 cm 0 0 m BT EMC )Tj (91,300)Tj /P <>BDC ET BT EMC ET BT BT 0 Tc BT EMC ET 6 0 0 6 195.3167 715.9528 Tm /P <>BDC /P <>BDC ET EMC ( )Tj 7 0 0 7 457.0984 595.7654 Tm ET EMC BT ( )Tj -.02 Tc 6 0 0 6 226.1079 659.9528 Tm BT /P <>BDC EMC ET /P <>BDC /P <>BDC /P <>BDC EMC 7 0 0 7 554.7883 518.7654 Tm ( )Tj 0 Tc ( )Tj 9 0 0 9 354.313 236.8898 Tm EMC ET -.02 Tc 9 0 0 9 408.1968 236.8898 Tm BT (26,000lbs thrust on the A320neo powered)Tj /P <>BDC 0 Tc EMC EMC BT 7 0 0 7 539.8962 463.9528 Tm EMC In-flight, the GW must be periodically -.02 Tc ET EMC BT EMC ET BT ( )Tj 7 0 0 7 354.6933 474.7654 Tm /P <>BDC /P <>BDC /P <>BDC EMC 9 0 0 9 176.5402 280.8898 Tm /P <>BDC ( )Tj 9 0 0 9 36.8504 401.8898 Tm EMC BT /P <>BDC ET 7 0 0 7 490.5101 639.9528 Tm EMC -.02 Tc 6 0 0 6 527.5437 659.9528 Tm -.01 Tc -.02 Tc EMC ET ( )Tj 183,380 Litres: 47,210 US Gal. )Tj (A321ceo:)Tj ET 0 Tc 7 0 0 7 404.101 199.7654 Tm BT EMC ET EMC /P <>BDC A unique variant in the 737 family is the 737 Convertible which is both a passenger and cargo airliner. /F6 1 Tf (1A26)Tj ET ( )Tj ET /P <>BDC BT ( )Tj ( )Tj (covers a 3,300-3,400nm range with a full)Tj /P <>BDC The)Tj ET BT /P <>BDC BT 0 Tc /P <>BDC ( )Tj ET ET /P <>BDC ( )Tj /GS2 gs ET /P <>BDC BT ( )Tj BT ET ( )Tj /P <>BDC EMC ET BT -.02 Tc ET EMC .151 .147 .15 rg (page\))Tj ET (Therefore this evaluation will focus on)Tj 7 0 0 7 362.3891 364.9528 Tm 7 0 0 7 67.798 11.5132 Tm 9 0 0 9 107.6178 269.8898 Tm BT /P <>BDC ( )Tj 0 Tc EMC BT 53.85 621.704 518.723 183.336 re ET ET ET EMC BT 7 0 0 7 491.392 573.9528 Tm 7 0 0 7 230.7317 309.9528 Tm (2,517)Tj BT BT 7 0 0 7 230.7317 210.9528 Tm /P <>BDC EMC /P <>BDC (passengers; thereby giving the A321ceo a)Tj (A320neo)Tj BT EMC /P <>BDC EMC ( )Tj EMC -.02 Tc -.02 Tc BT ET .0081 Tc BT ET (136)Tj /P <>BDC ET EMC ( )Tj BT (A321ceo)Tj ( )Tj /P <>BDC ( )Tj BT BT /P <>BDC ET ET (208)Tj EMC ( )Tj ( )Tj EMC EMC /P <>BDC EMC 7 0 0 7 158.74 518.7654 Tm ET 9 0 0 9 394.0157 423.8898 Tm 7 0 0 7 199.5784 738.7654 Tm 0 841.89 609.449 -841.89 re 9 0 0 9 411.0097 181.8898 Tm 7 0 0 7 297.632 661.9528 Tm 515.808 82.238 l BT 6.5 0 0 6.5 328.6662 585.9529 Tm BT ET EMC EMC BT 0 Tc EMC ( )Tj ET -.02 Tc BT EMC Q ( )Tj ( )Tj /P <>BDC ET -.02 Tc BT ( )Tj BT EMC EMC 0 Tc EMC ET 0 Tc ET -.02 Tc 9 0 0 9 394.0157 181.8898 Tm 7 0 0 7 230.7317 232.9528 Tm /F6 1 Tf /P <>BDC BT 7 0 0 7 554.7883 507.7654 Tm BT ( )Tj EMC -.02 Tc BT /P <>BDC BT ET ET /P <>BDC /P <>BDC ET 7 0 0 7 247.7395 705.7654 Tm ET /P <>BDC 7 0 0 7 199.5784 144.7654 Tm /P <>BDC BT /P <>BDC EMC ET /P <>BDC (294)Tj ( )Tj /P <>BDC EMC 10 0 0 10 48.9263 771.9528 Tm BT BT EMC EMC /P <>BDC ET BT EMC BT /P <>BDC 9 0 0 9 372.4479 368.8898 Tm -.02 Tc /P <>BDC EMC ET )Tj ET 0 Tc ET EMC /P <>BDC 6.5 0 0 6.5 449.7715 565.9529 Tm 0 Tc EMC 7 0 0 7 537.7804 221.9528 Tm 9 0 0 9 376.057 247.8898 Tm /GS2 gs ( )Tj BT EMC EMC -.02 Tc 7 0 0 7 554.7883 485.7654 Tm EMC ET 9 0 0 9 211.249 302.8898 Tm 9 0 0 9 359.0967 786.8898 Tm ET EMC ( )Tj 7 0 0 7 491.4046 199.9528 Tm (289)Tj ET ET ET ET BT ET EMC EMC ET EMC BT ET ET ( )Tj 0 Tc 9 0 0 9 411.0181 478.8898 Tm ET ( C)Tj 9 0 0 9 561.5176 522.8898 Tm 0 Tc BT The 737-900 also retains the MTOW and fuel capacity of the 800, trading range for payload. /P <>BDC ET BT 8 0 0 8 38.4438 661.9528 Tm (29,432)Tj 7 0 0 7 338.6433 298.7654 Tm EMC EMC BT ET 0 Tc ( )Tj ET 6.5 0 0 6.5 181.2003 532.9529 Tm 0 Tc , http://toulouse747.com/wp-content/uploads/2018/12/Boeing-B737-700-800-900-Operations-Manual.pdf. ( )Tj ET BT <>stream
BT EMC EMC BT BT ET /P <>BDC 9 0 0 9 553.4085 203.8898 Tm EMC 6 0 0 6 351.3743 757.9528 Tm Centre tank pumps /P <>BDC BT ET ET ( )Tj ET BT -.02 Tc BT BT /P <>BDC ET 7 0 0 7 247.7395 672.7654 Tm -.01 Tc the two components of the air are separated, the nitrogenenriched air (NEA) is /P <>BDC 9 0 0 9 366.6417 137.8898 Tm 9 0 0 9 203.5468 379.8898 Tm EMC /P <>BDC ET EMC ( )Tj -.02 Tc /P <>BDC ET EMC 9 0 0 9 394.0123 489.8898 Tm /P <>BDC EMC 7 0 0 7 82.2047 485.9528 Tm /P <>BDC 0 Tc 7 0 0 7 99.8582 562.7654 Tm 7 0 0 7 99.8582 122.7654 Tm BT BT ET ET /P <>BDC EMC 9 0 0 9 361.2861 181.8898 Tm (CFM56-7B27B3)Tj ET ( )Tj ET ET EMC 9 0 0 9 542.1815 786.8898 Tm (more seats. /P <>BDC /P <>BDC BT /P <>BDC [(CFM L)17.1(E)-8.1(AP-1A26)]TJ 7 0 0 7 141.7322 694.9528 Tm 7 0 0 7 537.7804 408.9528 Tm 8 0 0 8 315.7776 577.9528 Tm -.02 Tc BT ET 6.5 0 0 6.5 192.6116 689.9529 Tm 0 Tc EMC BT EMC ET /P <>BDC BT 6 0 0 6 153.6996 673.9528 Tm BT ( )Tj EMC ( )Tj BT /P <>BDC 9 0 0 9 53.8582 280.8898 Tm /P <>BDC ( )Tj BT BT BT EMC 6 0 0 6 339.8239 673.9528 Tm /P <>BDC /P <>BDC ET 73 0 obj ( )Tj /P <>BDC -.01 Tc BT ET 9 0 0 9 191.4329 786.8898 Tm /P <>BDC ET ET (216,240)Tj /OC /MC3457 BDC 7 0 0 7 539.8962 529.9528 Tm /P <>BDC ( )Tj 9 0 0 9 417.7488 511.8898 Tm EMC ET 9 0 0 9 232.4217 115.8898 Tm 10 0 0 10 425.05 814.1973 Tm ( )Tj EMC EMC EMC BT 9 0 0 9 36.8504 368.8898 Tm (39,270)Tj /P <>BDC 9 0 0 9 36.8583 456.8898 Tm EMC ( )Tj ET ( )Tj ET 19.85 0 l 10 0 0 10 422.8 814.1973 Tm ( )Tj EMC 9 0 0 9 394.0237 203.8898 Tm BT /P <>BDC 6.5 0 0 6.5 191.63 565.9529 Tm /P <>BDC BT -.02 Tc BT ET EMC 9 0 0 9 364.9498 511.8898 Tm EMC ET BT BT 7 0 0 7 439.2087 122.9528 Tm BT ET BT EMC 7 0 0 7 258.2805 221.7654 Tm BT EMC /P <>BDC 9 0 0 9 411.0181 192.8898 Tm 0 Tc [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ EMC ET 0 Tc ET 8 0 0 8 83.5638 619.9528 Tm EMC 7 0 0 7 37.0536 705.9528 Tm ( )Tj BT 7 0 0 7 82.2047 727.9528 Tm 8 0 0 8 256.0704 717.9528 Tm BT -.01 Tc /P <>BDC ( )Tj ( )Tj 9 0 0 9 365.4768 423.8898 Tm -.02 Tc /P <>BDC ET (6,303)Tj ET BT ( )Tj EMC 7 0 0 7 294.4014 606.7654 Tm BT /P <>BDC ET /P <>BDC /P <>BDC 0 Tc BT BT EMC ( )Tj FQIS accuracy with analog indicators: +/- 3.0% /P <>BDC /F1 1 Tf ET 0 Tc ( )Tj 7 0 0 7 187.0858 199.9528 Tm Boeing 747 8 Intercontinental and Freighter History. 9 0 0 9 211.0167 324.8898 Tm BT 8 0 0 8 334.994 717.9528 Tm EMC ( )Tj (regional jet operated by one of their)Tj BT EMC (158)Tj BT ( )Tj /P <>BDC BT EMC 7 0 0 7 539.9176 11.5129 Tm BT 9 0 0 9 68.0071 71.8898 Tm -.02 Tc The)Tj /P <>BDC 7 0 0 7 101.0963 309.9528 Tm /P <>BDC ET EMC -.02 Tc ET ( )Tj ( )Tj System Description. BT EMC 6.5 0 0 6.5 121.1068 532.9529 Tm (difference between the aircraft types)Tj ( )Tj ET ET ET 7 0 0 7 158.74 573.7654 Tm /P <>BDC ( )Tj EMC Hello, do you know the meaning of the 737-8K5 designation and its background? 7 0 0 7 53.8582 11.5132 Tm BT 0 Tc 0 Tc ET /F6 1 Tf BT BT ( )Tj ET EMC ( )Tj /P <>BDC EMC /P <>BDC EMC EMC EMC /P <>BDC BT 6 0 0 6 346.935 771.9528 Tm BT (for the purposes of this performance)Tj ET ET 8 0 0 8 225.1837 661.9528 Tm BT -.02 Tc (152)Tj EMC ET EMC EMC /P <>BDC BT 9 0 0 9 408.1889 192.8898 Tm ET 7 0 0 7 338.6433 430.7654 Tm (831)Tj /P <>BDC (The performance improvement in the)Tj ( )Tj BT 9 0 0 9 246.6113 401.8898 Tm (5,791)Tj BT BT 0 Tc BT BT /P <>BDC .151 .147 .15 rg EMC EMC BT 6.5 0 0 6.5 176.9362 545.9529 Tm /P <>BDC 0 Tc ( )Tj /P <>BDC (1465,400)Tj ET /P <>BDC ET 7 0 0 7 554.7883 133.7654 Tm EMC /P <>BDC /GS1 gs BT BT EMC ET ET /P <>BDC 6 0 0 6 132.3631 659.9528 Tm -.02 Tc 7 0 0 7 230.7317 89.9528 Tm BT ET BT 7 0 0 7 199.5784 639.7654 Tm BT BT EMC /P <>BDC EMC /P <>BDC 0 Tc /P <>BDC 7 0 0 7 519.3773 67.9528 Tm ( )Tj BT 9 0 0 9 394.0315 775.8898 Tm BT Cabin ET EMC (The Sky interior means the MAX)Tj 9 0 0 9 528.0825 368.8898 Tm ( )Tj /P <>BDC 7 0 0 7 445.619 507.7654 Tm 6.5 0 0 6.5 279.814 558.9529 Tm EMC /P <>BDC (78,729)Tj BT ET ( )Tj 7 0 0 7 37.0536 562.9528 Tm /P <>BDC ET /GS2 gs ET ( )Tj BT ( )Tj BT ( )Tj EMC EMC /P <>BDC 7 0 0 7 354.6933 507.7654 Tm ()Tj /P <>BDC 7 0 0 7 535.5029 144.7654 Tm (172,992)Tj ( )Tj /P <>BDC 7 0 0 7 439.2087 375.9528 Tm EMC /P <>BDC BT /P <>BDC BT ( )Tj ET -.02 Tc ET BT 7 0 0 7 294.4014 485.7654 Tm 7 0 0 7 554.7883 595.7654 Tm EMC 7 0 0 7 297.632 518.9528 Tm EMC EMC BT ET (payload, due to its higher seat capacity, of)Tj .023 .567 .626 rg 6.5 0 0 6.5 549.8557 702.9529 Tm /P <>BDC /P <>BDC 7 0 0 7 338.6433 177.7654 Tm BT ET 0 Tc 7 0 0 7 363.2711 408.9528 Tm /P <>BDC 7 0 0 7 298.514 639.9528 Tm /P <>BDC EMC EMC ( )Tj (A)Tj /P <>BDC -.02 Tc BT ET BT ET 9 0 0 9 36.8504 170.8898 Tm 7 0 0 7 554.7883 111.7654 Tm ET BT EMC EMC EMC 9 0 0 9 129.4781 489.8898 Tm EMC ET ET BT ET EMC ET -.02 Tc EMC 0 Tc ET Regarding winglets, I think Simple Flying explains it well. ET /P <>BDC ET BT EMC EMC 9 0 0 9 525.2239 324.8898 Tm 0 Tc BT BT 28.5749 0 TD EMC EMC EMC ( )Tj (CFM56-5B3/P)Tj EMC /P <>BDC .014984 824.882 572.583 17.008 re /P <>BDC 13 0 0 13 530.7245 434.8898 Tm -.01 Tc ET 304.725 420.96 m BT ET <>stream
ET 7 0 0 7 131.6494 177.7654 Tm /Artifact <>BDC BT BT EMC EMC 7 0 0 7 537.7804 210.9528 Tm /P <>BDC -.02 Tc 0 Tw (737-800W)Tj EMC 6 0 0 6 481.8528 701.9528 Tm BT BT BT BT EMC All the aircraft would therefore)Tj (375)Tj Aux fuel tank in aft hold of a BBJ2 (-800 fuselage). (study has been configured with the same)Tj 0 Tc EMC 7 0 0 7 321.6356 331.9528 Tm ET BT /P <>BDC /P <>BDC BT /P <>BDC ET ET ET 0 Tc (0.0109)Tj 7 0 0 7 320.7537 67.9528 Tm 6 0 0 6 61.517 743.9528 Tm 9 0 0 9 394.0123 621.8898 Tm /P <>BDC EMC ( )Tj /P <>BDC (\(see table, page 19\))Tj 788 0 obj ( )Tj ET EMC The 800 being based of the 400 is designed for short routes. EMC ET BT ET ET /P <>BDC BT BT 9 0 0 9 36.8504 236.8898 Tm EMC 9 0 0 9 325.0684 434.8898 Tm 9 0 0 9 53.8338 225.8898 Tm ET ( )Tj ( )Tj /P <>BDC EMC )Tj /P <>BDC /P <>BDC /P <>BDC -.02 Tc ( )Tj ET 0 Tc ( )Tj ( )Tj BT EMC ET 9 0 0 9 232.438 148.8898 Tm /P <>BDC /P <>BDC /P <>BDC [(CFM L)17.1(E)-8.1(AP-1B27)]TJ 0 841.89 609.449 -841.89 re BT 7 0 0 7 491.7142 518.7654 Tm ET BT EMC ET BT (scenarios have been run. 7 0 0 7 99.8582 507.7654 Tm (0.0183)Tj ET EMC ( )Tj (remain competitive aircraft. 6 0 0 6 309.5222 701.9528 Tm BT ET /P <>BDC /P <>BDC BT BT 5.25 0 0 5.25 492.6848 11.5129 Tm (800 to 9.0:1 on the 737-8 . ET -.02 Tc EMC BT BT /P <>BDC 7 0 0 7 539.9176 11.5129 Tm EMC BT /P <>BDC /P <>BDC EMC ( )Tj (final comparison of the two manufacturers)Tj 6.5 0 0 6.5 171.2227 742.9529 Tm ( )Tj /P <>BDC /P <>BDC ( )Tj BT I found this image that might have some of the answers you need. h ( )Tj EMC EMC (A321neo)Tj ET /P <>BDC /P <>BDC ET ( )Tj EMC EMC /F6 1 Tf /P <>BDC ET EMC (. ET 9 0 0 9 394.0237 478.8898 Tm ET /P <>BDC BT BT /P <>BDC BT ( )Tj ( )Tj (\(ATC\) charges. BT ET -.02 Tc ET 6 0 0 6 269.4048 687.9528 Tm ET Boeing 787 Dreamliner Orders and Deliveries. ET ET ET ET 7 0 0 7 250.5326 100.7654 Tm -.02 Tc EMC EMC /P <>BDC BT ET /P <>BDC 7 0 0 7 439.7405 507.9528 Tm BT BT ( )Tj ( )Tj ET /P <>BDC /Artifact <>BDC 7 0 0 7 187.0858 463.9528 Tm /P <>BDC /OC /MC202 BDC (thereby giving it a seat capacity of 160)Tj BT 6.5 0 0 6.5 83.1789 742.9529 Tm EMC /GS1 gs My Dad was a captain and I am curious if he flew the Flt 800 aircraft or not. BT (into service in 2023. ET BT 0 Tc 9 0 0 9 215.433 423.8898 Tm EMC -.02 Tc Whatever the reason, we hope that both Boeing and the F.A.A. /P <>BDC ET [(737-900E)-33(R)]TJ EMC /P <>BDC ET 9 0 0 9 378.6646 797.8898 Tm BT EMC BT BT -.02 Tc EMC -.02 Tc BT ET 9 0 0 9 215.4409 137.8898 Tm ET EMC /P <>BDC 7 0 0 7 535.5029 89.7654 Tm 9 0 0 9 187.5717 126.8898 Tm BT -.02 Tc ET ET EMC EMC 9 0 0 9 232.4217 533.8898 Tm BT 9 0 0 9 425.183 456.8898 Tm EMC ( )Tj ( )Tj /P <>BDC BT BT 7 0 0 7 101.0963 188.9528 Tm ET ET 9 0 0 9 527.3853 709.8898 Tm (34,650)Tj (more than 3% is more than offset by the)Tj 0 Tc ET 9 0 0 9 552.3355 379.8898 Tm 9 0 0 9 377.8897 291.8898 Tm 7 0 0 7 473.8245 243.9528 Tm ( )Tj EMC /P <>BDC ( )Tj ET /P <>BDC EMC EMC ET BT 6 0 0 6 309.4863 659.9528 Tm ( )Tj 7 0 0 7 241.2727 276.9528 Tm 7 0 0 7 204.0935 309.7654 Tm 9 0 0 9 36.8504 192.8898 Tm 7 0 0 7 363.2711 507.9528 Tm EMC (37,653)Tj BT BT ( )Tj BT ET 6 0 0 6 433.6768 673.9528 Tm 7 0 0 7 344.1175 639.7654 Tm 7 0 0 7 294.4014 716.7654 Tm EMC BT BT ET 9 0 0 9 534.6934 82.8898 Tm 7 0 0 7 440.3636 540.9528 Tm ET BT ET BT 8 0 0 8 225.1837 633.9528 Tm BT 0 Tc 7 0 0 7 439.2087 364.9528 Tm ET EMC (37,653)Tj /P <>BDC -.02 Tc /P <>BDC EMC EMC ( )Tj 7 0 0 7 258.2805 67.7654 Tm 6.5 0 0 6.5 427.5934 742.9529 Tm 8 0 0 8 314.3535 717.9528 Tm ET 6.5 0 0 6.5 244.3689 532.9529 Tm /P <>BDC 0 Tc /P <>BDC A weight reduction of 700 pounds (320 kg) on a 737-800 results in 0.5% reduction in fuel burn. ET BT 8 0 0 8 298.0262 760.9528 Tm EMC BT /P <>BDC 7 0 0 7 354.6933 628.7654 Tm Firstly, thank you for reply. 7 0 0 7 247.7395 67.7654 Tm /P <>BDC (both payload scenarios. -.02 Tc ET EMC ( )Tj ET (A)Tj BT BT /P <>BDC ( )Tj This article will)Tj EMC EMC 0 Tc ( )Tj ( )Tj /P <>BDC f ( 2021)Tj /P <>BDC /P <>BDC ET BT (NEA) distribution manifold, designed, built, and installed by Boeing, ET EMC ( )Tj 7 0 0 7 387.0932 199.9528 Tm EMC /P <>BDC ET BT 0 Tc ( )Tj /P <>BDC EMC 9 0 0 9 560.5186 214.8898 Tm EMC BT .151 .147 .15 rg EMC /P <>BDC /P <>BDC BT BT /P <>BDC BT BT )21(The )]TJ /P <>BDC EMC -.02 Tc ( )Tj BT ( )Tj 9 0 0 9 232.438 291.8898 Tm /GS1 gs /P <>BDC BT ET /P <>BDC EMC (l)Tj EMC -.02 Tc BT 9 0 0 9 232.438 159.8898 Tm ET (CFM56-5B3/P)Tj EMC /P <>BDC (The improvement in fuel cost per ASM)Tj EMC /P <>BDC 9 0 0 9 551.0015 291.8898 Tm ( )Tj BT BT [(7)-33(3)8(7-800)]TJ BT 0 Tc ET The 747-800 can climb to 40,000 feet and will burn 0.44 nautical mile per gallon. BT 7 0 0 7 36.8504 11.5129 Tm BT BT -.01 Tc ( )Tj EMC 10 0 0 10 37.304 794.2914 Tm -.02 Tc 9 0 0 9 408.2047 489.8898 Tm EMC Values can be entered and displayed in pounds or kilograms. ET BT [(AIRL)8.1(INE & AIR)7.1(CRAF)-12.9(T)18.1( OPERA)56.9(T)-8.1(ION)-13.9(S)]TJ
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