/P <>BDC 6 0 0 6 195.6824 659.9528 Tm (3,465)Tj EMC EMC 7 0 0 7 491.4046 133.9528 Tm ET EMC q 1 0 0 1 215.441 73.878 cm 0 0 m (minutes between aircraft types or 3.7% on)Tj BT EMC [(CFM L)17.1(E)-8.1(AP-1B27)]TJ EMC The aircraft in this)Tj 7 0 0 7 535.5029 441.7654 Tm 7 0 0 7 354.6933 474.7654 Tm 9 0 0 9 215.4409 38.8898 Tm BT BT ET 0 Tc 7 0 0 7 54.7071 606.7654 Tm 0 Tc /F1 1 Tf EMC BT ET All information is given in good faith and for information purposes only. ET 9 0 0 9 198.192 599.8898 Tm ET ET 9 0 0 9 215.4313 291.8898 Tm ( )Tj BT /F6 1 Tf 9 0 0 9 561.4773 753.8898 Tm 9 0 0 9 526.8993 643.8898 Tm ET ET EMC /P <>BDC ET ET -.02 Tc EMC (A)Tj EMC BT Aircraft have been NGS provisioned since l/n 1935 and it has been installed since l/n 2620 onwards. ET EMC BT 9 0 0 9 215.433 192.8898 Tm ET BT BT /P <>BDC (1,824)Tj /P <>BDC BT /P <>BDC ( )Tj ET EMC BT /P <>BDC EMC EMC ( )Tj /P <>BDC BT EMC Q ( )Tj ET 7 0 0 7 554.7883 529.7654 Tm ET 56 0 0 56 419.9569 622.1944 Tm 7 0 0 7 241.2727 276.9528 Tm EMC Fuel quantity is measured by using a series of ET ET /P <>BDC EMC (operationally safe to do so, in the)Tj ET ET 7 0 0 7 247.7395 210.7654 Tm ET BT EMC ET /P <>BDC 0 Tc 9 0 0 9 385.2246 148.8898 Tm 6 0 0 6 146.7028 743.9528 Tm /P <>BDC EMC EMC (on distance from the destination airport)Tj -.02 Tc -.02 Tc ET BT ( )Tj BT BT The design of the 737-800 lends itself to the sleek size and prowess of this aircraft. wiring in tanks, proximity to hot air-conditioning or pneumatic systems, etc. EMC BT /P <>BDC ET BT ( )Tj (A321ceo)Tj BT 7 0 0 7 87.8179 243.7654 Tm EMC /P <>BDC ET EMC BT (172,992)Tj EMC ET /P <>BDC 0 Tc ET /P <>BDC /P <>BDC /P <>BDC EMC For this reason, a)Tj ET BT ()Tj EMC 9 0 0 9 232.438 291.8898 Tm ET EMC BT EMC /P <>BDC BT 0 Tc 0 Tc EMC (CFM56-7B27B3)Tj EMC (150)Tj /P <>BDC ( )Tj (5.1% benefit in fuel burn with the heavier)Tj BT 7 0 0 7 337.4684 661.9528 Tm /P <>BDC /P <>BDC /P <>BDC ET Due to the additional structural)Tj /P <>BDC /P <>BDC /P <>BDC ET ET 0 Tc -.02 Tc BT EMC [(superior oper)10(ating performance. EMC (47,000)Tj /P <>BDC EMC 137 )Tj (150)Tj EMC EMC /P <>BDC /P <>BDC /Im2 Do ( )Tj BT 9 0 0 9 394.0157 566.8898 Tm EMC EMC 0 Tc BT /P <>BDC ET EMC (-47)Tj ( )Tj /P <>BDC 0 Tc 9 0 0 9 566.3776 192.8898 Tm Fuel temp is taken from main tank 1 because this will be the coldest as it has 10 0 0 10 52.6304 814.1973 Tm EMC (give the newer type a further advantage. 0 Tc -.02 Tc -.02 Tc BT EMC BT ET BT EMC /P <>BDC (the five)Tj BT BT ( )Tj BT ET ( )Tj 9 0 0 9 394.0123 390.8898 Tm EMC ET 6 0 0 6 466.0123 687.9528 Tm BT ( )Tj ( )Tj (2,429)Tj EMC (and their operational use by mainline)Tj ET BT ET ( )Tj ( )Tj BT BT BT 6.5 0 0 6.5 112.0328 637.9529 Tm 8 0 0 8 74.9636 577.9528 Tm /P <>BDC 0 Tc ( )Tj BT ET ( )Tj ET ET (273,600)Tj BT /P <>BDC /P <>BDC EMC 9 0 0 9 53.8578 335.8898 Tm BT ET EMC ET ET ( )Tj BT /F7 1 Tf EMC /P <>BDC (0.0194)Tj /P <>BDC ET 7 0 0 7 316.0679 309.7654 Tm BT /P <>BDC ET (282)Tj BT /P <>BDC ET ET /P <>BDC ET ET EMC ( )Tj ( )Tj BT (4,000nm with maximum passenger)Tj /P <>BDC /P <>BDC !! EMC 0 Tc (referred to as premium, main cabin extra)Tj EMC 9 0 0 9 43.6039 794.2914 Tm 10 0 0 10 49.3644 814.1973 Tm ( )Tj ( )Tj /P <>BDC /P <>BDC ( )Tj EMC (283)Tj EMC EMC /P <>BDC EMC ( )Tj BT /P <>BDC -.02 Tc EMC EMC EMC /P <>BDC EMC 7 0 0 7 338.6433 133.7654 Tm BT 5.25 0 0 5.25 515.3989 11.5129 Tm BT ( )Tj 9 0 0 9 522.5095 181.8898 Tm 7 0 0 7 294.4014 287.7654 Tm /P <>BDC BT BT ET 9 0 0 9 511.3603 412.8898 Tm 7 0 0 7 343.2355 705.7654 Tm EMC 9 0 0 9 53.8582 115.8898 Tm ( )Tj /P <>BDC -.02 Tc EMC /P <>BDC 0 Tc ET -.02 Tc BT ET 9 0 0 9 394.0123 522.8898 Tm EMC ( )Tj -.02 Tc BT /P <>BDC BT 7 0 0 7 70.1644 540.9528 Tm ET ( )Tj ( )Tj /P <>BDC [(R)13.9(OUT)10(E CHARA)16.1(CT)10(ERIS)8.1(T)-8.1(I)0(C)-17.1(S)0( F)8.1(OR ANAL)86.9(YSIS OF AIR)7.1(CRAF)-12.9(T)18.1( PERF)8.1(ORMANCE )]TJ ET EMC 9 0 0 9 36.8504 137.8898 Tm ET ET /P <>BDC BT 7 0 0 7 99.8582 419.7654 Tm EMC (increase the passenger weight assumptions)Tj EMC ET ET (\(see table, this page\))Tj Boeing 797, MNA-6x and MNA-7x. EMC 7 0 0 7 299.0601 309.9528 Tm ET [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ EMC EMC EMC EMC /P <>BDC EMC 7 0 0 7 258.2805 595.7654 Tm EMC /P <>BDC ET -.01 Tc BT 10 0 0 10 50.1204 814.1973 Tm /P <>BDC ET /P <>BDC EMC 7 0 0 7 141.7322 100.9528 Tm EMC 0 Tc BT /P <>BDC ET 8 0 0 8 136.4919 633.9528 Tm /P <>BDC EMC 9 0 0 9 232.4217 181.8898 Tm /P <>BDC Pisquali 19/05/2018 at 16:07 Reply. -.02 Tc )Tj ET 7 0 0 7 294.4014 639.7654 Tm BT BT EMC /P <>BDC 10 0 0 10 407.41 814.1973 Tm 7 0 0 7 37.0536 529.9528 Tm 7 0 0 7 158.74 265.7654 Tm EMC BT ET ET 7 0 0 7 535.5029 672.7654 Tm /P <>BDC (evaluate the physical configuration of the)Tj BT 7 0 0 7 230.7317 716.9528 Tm 8 0 0 8 355.1264 760.7654 Tm BT EMC ET 7 0 0 7 491.392 463.9528 Tm BT EMC BT BT EMC BT 9 0 0 9 165.0289 60.8898 Tm EMC 7 0 0 7 384.8358 694.7654 Tm BT <>stream ET /P <>BDC ( )Tj 0 Tc 7 0 0 7 298.514 584.9528 Tm /P <>BDC /P <>BDC BT -.015 Tc support combustion. 9 0 0 9 53.8582 104.8898 Tm 5 0 0 5 484.5872 11.5129 Tm EMC [(R)11(emaining car)13.9(go - lbs )]TJ /P <>BDC EMC ( )Tj BT /P <>BDC 9 0 0 9 53.8338 203.8898 Tm BT /P <>BDC EMC EMC 0 Tc 7 0 0 7 187.0858 496.9528 Tm EMC BT BT /P <>BDC BT EMC /P <>BDC 9 0 0 9 373.9458 159.8898 Tm (covers a 3,300-3,400nm range with a full)Tj (289)Tj BT (The A321neo has a lower fuel burn)Tj ET EMC 7 0 0 7 427.7291 364.9528 Tm EMC BT ET ( )Tj /P <>BDC BT EMC BT BT BT EMC 9 0 0 9 542.3175 522.8898 Tm 7 0 0 7 444.737 78.7654 Tm EMC (2,731)Tj EMC /P <>BDC BT /P <>BDC BT /P <>BDC <>stream EMC ET ( )Tj BT EMC EMC BT 5 0 0 5 92.725 11.5132 Tm EMC BT /P <>BDC EMC ( )Tj (CFM56-5B3/P)Tj EMC ( )Tj 8 0 0 8 53.9012 749.9529 Tm ET /P <>BDC )Tj ( )Tj 9 0 0 9 411.0181 478.8898 Tm ( )Tj .964 .834 .406 rg EMC 9 0 0 9 372.4479 368.8898 Tm BT ET /P <>BDC /P <>BDC 8 0 0 8 394.0237 38.8898 Tm ET ( )Tj /P <>BDC 8 0 0 8 38.4438 717.9528 Tm ( )Tj ET ET ET /P <>BDC ET BT BT ET ET EMC EMC 9 0 0 9 411.0097 71.8898 Tm EMC BT 304.725 420.96 m S 0 Tc )Tj 7 0 0 7 230.7317 375.9528 Tm (maximum landing weight \(MLW\) of)Tj (248,200)Tj EMC /P <>BDC 9 0 0 9 541.0405 621.8898 Tm 6.5 0 0 6.5 398.369 585.9529 Tm EMC 7 0 0 7 379.3969 111.7654 Tm 7 0 0 7 427.7291 243.9528 Tm ET ( )Tj /P <>BDC /GS1 gs ( )Tj BT BT BT BT EMC EMC BT BT /P <>BDC /P <>BDC /P <>BDC ET .023 .567 .626 rg /P <>BDC BT 6.5 0 0 6.5 324.4345 702.9529 Tm ET 7 0 0 7 241.5317 419.9528 Tm /P <>BDC 8 0 0 8 365.7704 703.9528 Tm BT 0 Tc ET W n BT 7 0 0 7 247.7395 265.7654 Tm ( )Tj ( )Tj 7 0 0 7 491.4046 177.9528 Tm (31,416)Tj 7 0 0 7 44.5789 463.9528 Tm the two components of the air are separated, the nitrogenenriched air (NEA) is BT BT ET /P <>BDC /P <>BDC Hi and thanks for your question. BT (A320neo)Tj BT The controls for main tanks 1 and 2 change to aft ET EMC BT /P <>BDC EMC BT (2,517)Tj /P <>BDC /P <>BDC ( )Tj /P <>BDC EMC EMC ( )Tj ( )Tj 7 0 0 7 387.0932 188.9528 Tm /P <>BDC ET /P <>BDC -.01 Tc EMC 9 0 0 9 411.0097 82.8898 Tm ET 7 0 0 7 491.7142 298.7654 Tm BT EMC 7 0 0 7 445.619 67.7654 Tm EMC ( )Tj [(BOS-L)-31(A)-24.9(X)]TJ 6.5 0 0 6.5 499.597 585.9529 Tm /P <>BDC /P <>BDC ET EMC 0 Tc ET BT /P <>BDC (39,270)Tj /P <>BDC -.01 Tc EMC EMC BT EMC EMC /P <>BDC 7 0 0 7 520.6108 518.9528 Tm (172,992)Tj EMC (same 85% passenger payload of 136. /P <>BDC q 1 0 0 1 53.858 150.878 cm 0 0 m BT ET BT BT ( )Tj EMC /P <>BDC EMC (network used in this study, due to fuel tank)Tj ET ( )Tj 0 J 0 j 5 w 10 M [] 0 d /P <>BDC [(CFM L)17.1(E)-8.1(AP-1B27)]TJ BT ( )Tj BT EMC EMC EMC ( )Tj ( )Tj ( )Tj /P <>BDC air separation module (ASM) to separate oxygen and nitrogen from the air. BT BT the rear of the fwd hold and the front of the aft hold, this reduces the C of G BT /P <>BDC BT (191,240)Tj ET EMC -.02 Tc ET /F6 1 Tf EMC /P <>BDC 7 0 0 7 299.0601 397.9528 Tm BT -2.4549 -3.9026 m (improvement of 13.1%. BT BT BT ET 0 Tc BT ET ( )Tj /P <>BDC ET (2,748)Tj EMC BT 7 0 0 7 182.3536 78.9528 Tm BT 6 0 0 6 238.0716 687.9528 Tm (On the sectors where the A321ceo and)Tj /P <>BDC /P <>BDC ( )Tj 6 0 0 6 107.8523 659.9528 Tm /P <>BDC 0 Tc EMC 7 0 0 7 427.7291 287.9528 Tm BT /P <>BDC /P <>BDC /P <>BDC (2.31 cents per ASM. BT ( )Tj The trend in engine thrust rating is)Tj 7 0 0 7 230.7317 243.9528 Tm ET BT ( )Tj ( )Tj EMC ET BT EMC BT BT ET BT (which has the lowest fuel burn rate per)Tj 10.486 7.6165 l 15 w EMC 9 0 0 9 332.7796 225.8898 Tm BT -.02 Tc (CFM56-5B4/P)Tj 9 0 0 9 232.4217 192.8898 Tm EMC BT 7 0 0 7 53.8582 11.5132 Tm 7 0 0 7 277.3936 463.9528 Tm EMC BT ET /P <>BDC /P <>BDC BT 9 0 0 9 192.4883 104.8898 Tm ET /P <>BDC 0 Tc /P <>BDC ET 9 0 0 9 36.8504 390.8898 Tm 7 0 0 7 279.1575 716.9528 Tm EMC /P <>BDC /P <>BDC /P <>BDC BT 36.85 824.882 572.599 17.008 re ET EMC 9 0 0 9 53.8338 49.8898 Tm ( )Tj thanks for stopping by. /P <>BDC 7 0 0 7 321.6356 166.9528 Tm ET /P <>BDC EMC (performing better on the shorter sectors. S /P <>BDC EMC EMC ET /GS1 gs ET ET /P <>BDC ( )Tj EMC -.02 Tc /P <>BDC (1,288)Tj (orders, while the 737-800 and 737-900ER)Tj /P <>BDC EMC -.02 Tc /P <>BDC 9 0 0 9 267.0826 500.8898 Tm 0 Tc ( )Tj ET /P <>BDC ( )Tj EMC /P <>BDC BT System Description. ET ( )Tj W n EMC EMC ( )Tj BT EMC ET 9 0 0 9 343.8357 423.8898 Tm EMC ET ET BT EMC /P <>BDC ET 9 0 0 9 411.0097 577.8898 Tm EMC /P <>BDC 7 0 0 7 204.0935 111.7654 Tm /P <>BDC Thank you so much. q 7 0 0 7 299.0601 210.9528 Tm EMC /P <>BDC /P <>BDC (shows an even greater fuel burn)Tj 7 0 0 7 490.8321 540.7654 Tm 7 0 0 7 118.104 463.7654 Tm BT 0 Tc (11.0:1)Tj BT (0.0141)Tj ET /P <>BDC ET ( )Tj 0 Tc /P <>BDC EMC ET ET ET ET BT ET ET The)Tj BT 9 0 0 9 182.2339 500.8898 Tm (98-107)Tj (1,392)Tj ( )Tj The initial concept included podded engines and a T-tail as seen on the 727. EMC ET BT EMC ET (32,000lbs, down from the 33,000lbs that)Tj (better for the A321neo due to its increased)Tj EMC EMC /P <>BDC -.02 Tc 7 0 0 7 230.7317 628.9528 Tm ET 6.5 0 0 6.5 534.5352 585.9529 Tm )Tj BT -.02 Tc Modern Airliners and Civil Aviation Aircraft. BT BT EMC EMC EMC /P <>BDC /P <>BDC BT 9 0 0 9 192.6957 346.8898 Tm 9 0 0 9 215.4409 324.8898 Tm /P <>BDC 7 0 0 7 536.3849 408.7654 Tm EMC EMC EMC (0.0141)Tj EMC ( )Tj /P <>BDC /P <>BDC /P <>BDC (choice of engine variant. EMC As mentioned this allowed the fuselage to be expanded and have six-abreast seating. /P <>BDC /P <>BDC ET -.02 Tc available a Boeing 737 for modification and testing. /P <>BDC EMC /P <>BDC ET EMC BT 9 0 0 9 526.8813 445.8898 Tm /P <>BDC /P <>BDC /P <>BDC -.02 Tc EMC BT (this page\))Tj 7 0 0 7 77.36 11.5132 Tm (and 4.3% better performance on the 737-)Tj EMC EMC 6 0 0 6 538.428 771.9528 Tm EMC BT It rolled out of the productionhangar on June 30th, 1997 and made her maiden flight on the 31st of July. EMC 7 0 0 7 491.4046 309.9528 Tm ( )Tj /P <>BDC 7 0 0 7 241.5317 221.9528 Tm 7 0 0 7 343.2355 727.7654 Tm /P <>BDC EMC 6 0 0 6 489.6948 743.9528 Tm /P <>BDC 9 0 0 9 53.8338 93.8898 Tm ( )Tj ( )Tj EMC 0 Tc 5.25 0 0 5.25 64.5461 11.5129 Tm 7 0 0 7 258.2805 265.7654 Tm BT BT .151 .147 .15 rg ET ET (passengers and 163 passengers on the)Tj EMC Boeings 737-800 isnt called the most popular airliner for no reason. /P <>BDC (737-9)Tj 7 0 0 7 404.101 188.7654 Tm /P <>BDC ET ET 6 0 0 6 418.9814 701.9528 Tm ET BT BT /P <>BDC ET EMC (class cabin configuration used in this study)Tj 9 0 0 9 541.5243 720.8898 Tm ( )Tj ( )Tj 9 0 0 9 341.4411 247.8898 Tm BT (The fourth generation 737-8 is)Tj /P <>BDC BT ET ET (O)Tj BT The Boeing 737-800 to date has around 5000 units produced and 2019 saw 138 of the 800 roll of the production line. 9 0 0 9 425.1967 720.8898 Tm /P <>BDC (that in real airline operations the taxi-out)Tj /P <>BDC (The lowest fuel cost per ASM in the)Tj EMC ET 8 0 0 8 38.4438 731.9528 Tm 9 0 0 9 394.0123 280.8898 Tm BT BT 7 0 0 7 116.3631 11.5132 Tm BT ( )Tj ( )Tj 7 0 0 7 247.7395 562.7654 Tm ( )Tj 7 0 0 7 537.7804 375.9528 Tm BT 0 Tc 0 Tc 3 i EMC BT EMC BT BT 0 Tc BT /P <>BDC 7 0 0 7 474.3564 595.9528 Tm /P <>BDC BT EMC ET /P <>BDC -.02 Tc ( )Tj 9 0 0 9 411.0097 49.8898 Tm EMC /P <>BDC (989)Tj EMC /P <>BDC (0.0115)Tj BT ( )Tj BT BT BT BT -.02 Tc ET BT 0 Tc ET 7 0 0 7 247.7395 705.7654 Tm ET ET /P <>BDC EMC EMC (737-8)Tj /F1 1 Tf EMC 0 Tc BT BT /P <>BDC /P <>BDC ( )Tj /P <>BDC (192)Tj ET ( )Tj BT BT 7 0 0 7 337.6855 232.9528 Tm 8 0 0 8 225.1837 703.9528 Tm ( )Tj /P <>BDC ET 9 0 0 9 411.0234 764.8898 Tm BT /P <>BDC EMC ( )Tj 7 0 0 7 158.74 639.7654 Tm 7 0 0 7 82.2047 727.9528 Tm ET ET -.02 Tc /P <>BDC EMC EMC EMC /P <>BDC ( )Tj EMC -.02 Tc ( )Tj EMC 9 0 0 9 68.0071 357.8898 Tm 7 0 0 7 179.5605 419.9528 Tm ( )Tj ( )Tj /P <>BDC Airbus A320 Specs What is behind one of the most popular short-haul airliners? 9 0 0 9 189.8338 49.8898 Tm /P <>BDC (. ( )Tj /P <>BDC 9 0 0 9 177.6653 445.8898 Tm /P <>BDC ( )Tj ( )Tj (0.0158)Tj It requires a 2316 meter or 7,598.33 feet of take off distance. EMC BT ET /P <>BDC /P <>BDC ET ET EMC BT I am looking for the radius of the fuselage specifically the cargo door. 0 Tc BT EMC BT (182,200lbs, an MLW of 152,800lbs, and)Tj 7 0 0 7 125.6292 441.7654 Tm /P <>BDC 9 0 0 9 232.438 225.8898 Tm /P <>BDC ( )Tj ET ( )Tj 9 0 0 9 411.0097 280.8898 Tm BT (136)Tj ET /P <>BDC 7 0 0 7 130.1443 419.7654 Tm BT ( )Tj /P <>BDC 7 0 0 7 445.619 518.7654 Tm /P <>BDC EMC 9 0 0 9 336.3455 313.8898 Tm 9 0 0 9 394.0123 654.8898 Tm -.01 Tc This will)Tj ( )Tj )Tj 9 0 0 9 378.9498 368.8898 Tm ET 0 Tc )Tj /P <>BDC /P <>BDC BT 7 0 0 7 82.2047 639.9528 Tm In reality, most models will operate in a combination of classes. 9 0 0 9 215.433 434.8898 Tm ET 5.25 0 0 5.25 100.8225 11.5132 Tm 7 0 0 7 355.3163 232.7654 Tm /P <>BDC -.02 Tc 6.5 0 0 6.5 282.0695 735.9529 Tm BT still drawing fuel from the centre tank. ET EMC (163)Tj ET 8 0 0 8 187.3427 577.9528 Tm BT 7 0 0 7 535.5029 683.7654 Tm 7 0 0 7 338.6433 210.7654 Tm (190-199)Tj ( )Tj BT ET EMC BT BT 0 Tc EMC BT ET (A)Tj ( )Tj ( )Tj 9 0 0 9 36.8583 368.8898 Tm EMC EMC 0 Tc /P <>BDC ET BT /P <>BDC BT EMC ( )Tj 9 0 0 9 229.6045 104.8898 Tm 7 0 0 7 444.737 287.7654 Tm ( )Tj /P <>BDC BT ET ET BT ( )Tj BT (The A320neo family and 737 MAX)Tj BT /P <>BDC EMC ET BT (31,416)Tj ET 9 0 0 9 550.3618 324.8898 Tm 7 0 0 7 456.4753 639.7654 Tm ET BT /P <>BDC EMC 9 0 0 9 394.0157 280.8898 Tm 0 Tc /Artifact <>BDC BT BT BT The wings on the above models are able to hold 30% more fuel then previous generations. (evaluation that are payload-limited on the)Tj /P <>BDC 7 0 0 7 537.7804 177.9528 Tm 9 0 0 9 215.4409 401.8898 Tm ( )Tj BT ET 0 Tc ET (propulsive efficiency. ET (method of operation that balances the cost)Tj ET (977)Tj ( )Tj -.02 Tc /P <>BDC ET ET For example, the)Tj 7 0 0 7 439.7405 716.9528 Tm ET ET BT ( )Tj ( )Tj /P <>BDC (72,450)Tj 6.5 0 0 6.5 324.4345 663.9529 Tm EMC ET BT /P <>BDC (14 the sectors in this study. EMC ET ( )Tj /P <>BDC ET EMC (150)Tj ( )Tj EMC ( )Tj EMC EMC /P <>BDC /P <>BDC BT ET ET The fuel flow indication is integrated over time to calculate the fuel used for each engine. The FILTER BYPASS 8 0 0 8 505.7415 771.9528 Tm EMC ET EMC ( )Tj ( )Tj /P <>BDC /GS2 gs BT BT ET 0 Tc BT (uses one of the 11 certified weight variants. ET BT BT 0 Tc EMC /P <>BDC ET -.02 Tc ( )Tj /GS2 gs EMC 9 0 0 9 411.0097 500.8898 Tm -.02 Tc /P <>BDC BT ET 9 0 0 9 552.2312 676.8898 Tm 0 Tc ET 9 0 0 9 368.2867 357.8898 Tm It sounds like you have a bit of a project on your hands. EMC EMC EMC 6 0 0 6 339.5547 771.9528 Tm EMC (weight variants for this aircraft. BT 6 0 0 6 482.6087 673.9528 Tm BT EMC W* n /P <>BDC EMC ET 9 0 0 9 408.1854 511.8898 Tm /P <>BDC EMC ET /P <>BDC ET ( )Tj -.02 Tc EMC ET ET (1,272)Tj EMC 9 0 0 9 138.3634 544.8898 Tm BT (1,454)Tj 7 0 0 7 491.4046 386.9528 Tm (A)Tj 7 0 0 7 141.7322 232.9528 Tm 9 0 0 9 199.3527 390.8898 Tm BT <> 7 0 0 7 403.478 639.7654 Tm /F4 1 Tf ( )Tj EMC /P <>BDC ( )Tj EMC 9 0 0 9 202.845 357.8898 Tm BT -.01 Tc ( )Tj ET ET EMC 9 0 0 9 215.4313 82.8898 Tm <>stream EMC .559 .331 .619 rg 7 0 0 7 67.798 11.5132 Tm ET 0 Tc /P <>BDC Cheers Peter. /Artifact <>BDC /P <>BDC ( )Tj /P <>BDC (2,517)Tj ET BT )Tj ET BT 9 0 0 9 208.354 291.8898 Tm ET BT ET 9 0 0 9 53.8578 390.8898 Tm ET ET ( )Tj ( )Tj 7 0 0 7 179.5605 716.9528 Tm /P <>BDC 9 0 0 9 387.3578 258.8898 Tm /P <>BDC /P <>BDC [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ 6 0 0 6 61.517 743.9528 Tm ( )Tj ( )Tj BT BT ( 2021)Tj ( )Tj /P <>BDC ( )Tj [(BOS-C)-8.1(V)18.1(G)]TJ ET BT BT /F6 1 Tf 7 0 0 7 258.2805 661.7654 Tm BT BT ET EMC 0 Tc 7 0 0 7 37.5838 738.9528 Tm BT /P <>BDC The global climate of rising fuel costs, as well as increased competition in the form of the Airbus A320, have ensured that Boeing continues to bring out more improved versions of the type. /P <>BDC (more than 3% is more than offset by the)Tj 7 0 0 7 321.6356 100.9528 Tm BT q ET (0.0112)Tj 7 0 0 7 508.4124 727.7654 Tm ( )Tj ET BT 9 0 0 9 215.4409 192.8898 Tm ET BT EMC BT BT ET EMC /P <>BDC /P <>BDC The FAA developed an in-flight gas sampling system, integrated with 9 0 0 9 394.0237 302.8898 Tm ET 7 0 0 7 343.2355 463.7654 Tm /P <>BDC EMC (2,437)Tj ET (seats. EMC EMC f (14 sectors. ET EMC /GS2 gs ET 0 Tc ET BT (be charged the same in operation for this)Tj (45,276)Tj 7 0 0 7 508.4124 441.7654 Tm 8 0 0 8 394.0237 82.8898 Tm [(SS)-9.1(U)8(E)]TJ 7 0 0 7 379.3969 122.7654 Tm ET -.02 Tc 0 Tc ET /P <>BDC ET ET 9 0 0 9 363.3015 775.8898 Tm BT (35,112)Tj ET /P <>BDC ET ET (weights used are an MTOW of)Tj f /P <>BDC 9 0 0 9 36.8504 148.8898 Tm EMC EMC /P <>BDC EMC 9 0 0 9 196.7724 412.8898 Tm ( )Tj /P <>BDC endobj EMC /P <>BDC /P <>BDC BT ET /P <>BDC BT ET ET BT 7 0 0 7 258.2805 716.7654 Tm 9 0 0 9 215.4313 280.8898 Tm ET BT EMC ET 0 Tc 9 0 0 9 392.5128 236.8898 Tm ( )Tj ( )Tj ET ET BT /F4 1 Tf ET 7 0 0 7 445.619 683.7654 Tm BT /P <>BDC EMC 7 0 0 7 519.3773 364.9528 Tm 0 Tc 7 0 0 7 247.7395 386.7654 Tm ( )Tj BT /P <>BDC (35,112)Tj ( )Tj 8 0 0 8 322.6267 760.9528 Tm It is recognised that most)Tj 7 0 0 7 36.8504 11.5129 Tm 0 Tc /P <>BDC EMC 7 0 0 7 158.74 111.7654 Tm BT ET -.01 Tc BT (5.1:1)Tj 8 0 0 8 394.0157 786.8898 Tm EMC BT EMC 6 0 0 6 61.517 771.9528 Tm ( )Tj ET ET -.02 Tc /GS1 gs /F4 1 Tf EMC ( )Tj EMC effectiveness of ground-based inerting (GBI) as a means of reducing the 7 0 0 7 187.0858 705.9528 Tm ( )Tj /P <>BDC BT ( )Tj (CFM56-7B26)Tj /P <>BDC /P <>BDC (271,728)Tj BT BT ( )Tj -.02 Tc EMC ( )Tj 6 0 0 6 561.1918 701.9528 Tm 9 0 0 9 232.438 467.8898 Tm -.02 Tc BT (CFM56-5B4/P)Tj ET 0 Tc (evaluation both taxi-out and taxi-in were)Tj /P <>BDC /P <>BDC 13 0 0 13 53.8578 181.8898 Tm ET 7 0 0 7 554.7883 276.7654 Tm EMC EMC ( )Tj EMC BT ET BT ET ET )Tj EMC EMC /P <>BDC ( )Tj 7 0 0 7 187.0858 694.9528 Tm BT /P <>BDC (82,110)Tj 0 Tc 7 0 0 7 326.2278 485.9528 Tm /P <>BDC ( )Tj 9 0 0 9 528.0345 511.8898 Tm 7 0 0 7 82.8504 408.9528 Tm BT -.02 Tc /P <>BDC BT /P <>BDC EMC ET ET /P <>BDC BT 0 Tc ET 7 0 0 7 354.4763 672.7654 Tm /P <>BDC (0.0109)Tj 7 0 0 7 230.7317 386.9528 Tm 7 0 0 7 279.1575 309.9528 Tm BT BT 7 0 0 7 241.5317 507.9528 Tm BT /P <>BDC BT EMC BT /P <>BDC BT EMC FQIS accuracy with analog indicators: +/- 3.0% /P <>BDC ( )Tj -.02 Tc .023 .567 .626 rg ET (applied to all flights. 7 0 0 7 36.8504 749.9528 Tm (5,466)Tj /P <>BDC BT EMC EMC (34,650lbs)Tj ET ET -.02 Tc ET /P <>BDC /P <>BDC 0 Tc EMC EMC (150)Tj (this evaluation are all in the same weight)Tj ET ( )Tj ET 9 0 0 9 388.8047 390.8898 Tm EMC EMC 7 0 0 7 365.035 639.9528 Tm EMC 7 0 0 7 82.2047 694.9528 Tm /P <>BDC ET /P <>BDC EMC 7 0 0 7 539.9176 11.5129 Tm /P <>BDC BT ( )Tj /OC /MC4771 BDC BT /F6 1 Tf ET /OC /MC4800 BDC ( )Tj /P <>BDC 9 0 0 9 394.0315 104.8898 Tm ( )Tj 6 0 0 6 403.4411 715.9528 Tm EMC BT ET ET 7 0 0 7 490.5101 606.9528 Tm EMC ET BT EMC 7 0 0 7 315.1859 89.7654 Tm ET 7 0 0 7 326.2278 672.9528 Tm EMC 7 0 0 7 125.6292 287.7654 Tm BT 0 Tc EMC /P <>BDC 0 Tc BT ( )Tj ET 9 0 0 9 394.0157 181.8898 Tm BT -.01 Tc ET EMC -.005 Tc /P <>BDC ET /P <>BDC ET ET BT BT -.015 Tc the 737 but will require up to six on the 747. ET BT BT /P <>BDC /P <>BDC (34,650)Tj -.02 Tc ET BT /P <>BDC 0 Tc -.02 Tc BT /P <>BDC /P <>BDC tank. EMC Boeing 737 History, the story behind this hugely successful City Jet. /P <>BDC /P <>BDC 6.5 0 0 6.5 64.6596 637.9529 Tm 6 0 0 6 254.6866 659.9528 Tm BT /P <>BDC ET BT ET BT ET BT BT 9 0 0 9 36.8504 368.8898 Tm BBJ3 was officially launched in October 2006, with orders from two undisclosed customers. BT EMC ( )Tj ( )Tj ET EMC EMC ( )Tj ( )Tj /P <>BDC ET (hugely successful. [(CFM L)17.1(E)-8.1(AP-1A26)]TJ 7 0 0 7 258.2805 496.7654 Tm /P <>BDC (A320ceo: )Tj -.02 Tc ET 9 0 0 9 555.4203 346.8898 Tm /P <>BDC /P <>BDC EMC /P <>BDC 6.5 0 0 6.5 433.3069 585.9529 Tm -.01 Tc 0 Tc [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ BT /P <>BDC (31,416)Tj 7 0 0 7 491.4046 232.9528 Tm 9 0 0 9 346.6898 280.8898 Tm -.02 Tc ET 6.5 0 0 6.5 549.8557 650.9529 Tm 7 0 0 7 108.6215 441.9528 Tm BT 0 Tc 7 0 0 7 316.0679 265.7654 Tm 7 0 0 7 520.6108 595.9528 Tm ET /P <>BDC ET 7 0 0 7 473.8245 419.9528 Tm (0.0142)Tj /GS2 gs /P <>BDC 7 0 0 7 445.619 496.7654 Tm ET 7 0 0 7 299.0601 243.9528 Tm /OC /MC5086 BDC ( )Tj /P <>BDC ( )Tj 6.5 0 0 6.5 327.0283 637.9529 Tm 5.25 0 0 5.25 515.3989 11.5129 Tm ( )Tj ET -.02 Tc 6 0 0 6 153.7355 729.9528 Tm EMC ( )Tj EMC 9 0 0 9 232.4217 170.8898 Tm ET /P <>BDC BT (was planned with fuel to reach a defined)Tj EMC ET ET 9 0 0 9 370.891 302.8898 Tm ( )Tj ET ET -.02 Tc BT EMC /P <>BDC 7 0 0 7 99.8582 232.7654 Tm EMC BT /P <>BDC BT 7 0 0 7 130.1443 221.7654 Tm ( )Tj /P <>BDC EMC 9 0 0 9 570.6951 291.8898 Tm EMC ET [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ BT 7 0 0 7 82.2047 518.9528 Tm 0 Tc /P <>BDC /P <>BDC /P <>BDC q 1 0 0 1 53.858 194.878 cm 0 0 m BT Cheers Peter, Pingback:Is Covid-19 isolation an opportunity to learn to fly? ET ET /P <>BDC /P <>BDC ET EMC ET (same number of passengers is carried on)Tj 7 0 0 7 473.8245 309.9528 Tm (A321neo)Tj /P <>BDC /P <>BDC ET -.02 Tc ( )Tj (737-8 has a 0.8-3.0% higher trip fuel burn than)Tj BT EMC EMC EMC EMC /P <>BDC (and taxi-in times would vary by flight. Airbus A330 Specs What can this popular long haul twin jet do? -.02 Tc ( )Tj /P <>BDC BT ET /P <>BDC ( )Tj ( )Tj BT (82,110)Tj 6 0 0 6 351.3743 715.9528 Tm EMC EMC BT ET ET 7 0 0 7 187.0858 408.9528 Tm EMC EMC ( )Tj EMC /P <>BDC -.01 Tc 9 0 0 9 68.0314 522.8898 Tm ( )Tj (economy seating by 12 seats when)Tj BT BT ( )Tj BT EMC EMC BT (this analysis is 20/42/117, giving a total)Tj (results in the same payload being carried in)Tj /P <>BDC BT ET -.02 Tc /P <>BDC 9 0 0 9 53.8578 258.8898 Tm BT BT /P <>BDC (The spot fuel price for the US aviation)Tj 9 0 0 9 548.3115 412.8898 Tm [(BOS-A)56.9(TL)]TJ BT 7 0 0 7 204.0935 584.7654 Tm ET 9 0 0 9 232.438 489.8898 Tm EMC BT /P <>BDC /P <>BDC EMC BT ( )Tj (170)Tj EMC 7 0 0 7 387.0932 144.9528 Tm 7 0 0 7 491.4046 199.9528 Tm EMC ET 9 0 0 9 373.1937 357.8898 Tm ET (The thrust ratings on the engines show)Tj EMC /P <>BDC /P <>BDC EMC 7 0 0 7 427.7291 342.9528 Tm EMC ET EMC /P <>BDC BT ET 9 0 0 9 36.8504 38.8898 Tm BT /P <>BDC BT BT not sure where to find that kind of detail. EMC ET 7 0 0 7 338.6433 408.7654 Tm ET /P <>BDC ET 9 0 0 9 68.3339 533.8898 Tm BT BT ET BT ( )Tj EMC 7 0 0 7 199.5784 441.7654 Tm /P <>BDC -.02 Tc (performance on this sector is 2.19 cents per)Tj ET ET /P <>BDC 8 0 0 8 38.4438 703.9528 Tm BT 7 0 0 7 294.4014 243.7654 Tm BT /P <>BDC 9 0 0 9 394.0315 170.8898 Tm BT /P <>BDC 9 0 0 9 215.433 401.8898 Tm BT EMC ET ET -.02 Tc 7 0 0 7 457.1753 727.7654 Tm ( )Tj /P <>BDC 7 0 0 7 187.0858 463.9528 Tm (lighter aircraft. EMC BT 0 Tc 7 0 0 7 439.7405 496.9528 Tm ET ( )Tj 7 0 0 7 491.7142 188.7654 Tm /P <>BDC /P <>BDC EMC ET ( )Tj W n /P <>BDC BT (0.0134)Tj EMC ET ET -.02 Tc EMC EMC 7 0 0 7 535.5029 298.7654 Tm (31,416)Tj ET (2,730)Tj /P <>BDC (performance, it was also assumed there)Tj EMC 7 0 0 7 445.619 540.7654 Tm EMC /P <>BDC (The block- and flight- \(take-off to)Tj EMC EMC BT ( )Tj BT BT BT EMC (evaluated for both types, the 737-)Tj 9 0 0 9 51.0236 489.8898 Tm BT ET BT /P <>BDC (5,121)Tj /P <>BDC /P <>BDC 6.5 0 0 6.5 397.7514 598.9529 Tm ET 0 Tc BT -.02 Tc ET 7 0 0 7 298.1781 67.9528 Tm /P <>BDC BT 9 0 0 9 566.5209 379.8898 Tm ET ( )Tj power to shut off the fuel in an emergency. (. 0 Tc /P <>BDC ET ( )Tj /P <>BDC 9 0 0 9 190.2832 49.8898 Tm ET BT /P <>BDC 19.84 0 l /P <>BDC 7 0 0 7 125.6292 540.7654 Tm 9 0 0 9 518.9185 401.8898 Tm BT BT EMC 0 Tc 7 0 0 7 490.6002 430.9528 Tm been many other improvements to wiring and FQIS. ET BT ET ( )Tj ET EMC 7 0 0 7 158.74 529.7654 Tm ( )Tj /P <>BDC ET /P <>BDC 9 0 0 9 121.2888 38.8898 Tm ET BT -.02 Tc EMC EMC ( )Tj ET 7 0 0 7 403.478 375.7654 Tm EMC 9 0 0 9 215.433 71.8898 Tm /P <>BDC ET Hi, How can I learn aerospace materails about a and b basis allowables for Boeing-737 ? BT EMC ET /P <>BDC BT BT EMC (\(see table, page 21\))Tj /P <>BDC EMC ( )Tj )]TJ EMC ET ET /P <>BDC )Tj 7 0 0 7 54.7071 705.7654 Tm EMC /P <>BDC BT /P <>BDC /P <>BDC ET EMC ET 0 Tc 56.25 0 0 56.25 36.8583 489.8898 Tm ( )Tj (the 737-9 reduces the block fuel burn)Tj (1,162)Tj 9 0 0 9 194.6103 401.8898 Tm How much fuel does a A350 burn? ET /P <>BDC ET BT EMC EMC 9 0 0 9 411.0181 280.8898 Tm BT ( )Tj ( )Tj 7 0 0 7 456.2165 100.7654 Tm (68.3 inches and a bypass ratio of up to)Tj 518.74 0 l (A321neo)Tj ( )Tj 0 Tc /P <>BDC ( )Tj BT ET (379)Tj 9 0 0 9 36.8504 60.8898 Tm BT 0 Tc BT ET EMC 6.5 0 0 6.5 347.0393 565.9529 Tm /P <>BDC ET 6.5 0 0 6.5 500.4875 532.9529 Tm BT (0.0155)Tj EMC BT 7 0 0 7 326.2278 518.9528 Tm 0 Tc /P <>BDC BT BT EMC BT .001 Tc /P <>BDC ET /P <>BDC /P <>BDC BT ET ET BT ET /P <>BDC (150)Tj 6 0 0 6 326.0708 673.9528 Tm EMC 7 0 0 7 141.7322 507.9528 Tm ET My Dad was a captain and I am curious if he flew the Flt 800 aircraft or not. 7 0 0 7 387.0932 265.9528 Tm /P <>BDC /P <>BDC EMC (34,650)Tj 0 Tc /P <>BDC BT (0.0135)Tj BT Q ET
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