ET /P <>BDC 9 0 0 9 394.0123 467.8898 Tm 7 0 0 7 456.2165 221.7654 Tm BT BT /P <>BDC (214)Tj ( )Tj /P <>BDC BT -.02 Tc ( )Tj 7 0 0 7 520.6108 540.9528 Tm 9 0 0 9 363.2032 478.8898 Tm 7 0 0 7 241.5317 221.9528 Tm ET exacerbating the imbalance. BT 6.5 0 0 6.5 486.1525 722.9529 Tm BT BT BT [(2,575nmn, the 737-8 has an av)12.9(er)10(age 13% lo)12(w)6.1(e)0(r)]TJ BT This compares)Tj EMC BT ( )Tj ET ET ( )Tj ( )Tj -.01 Tc And I hope I will get some good stuff to post it to you. (1,824)Tj BT /P <>BDC ( )Tj (216)Tj ET BT BT 9 0 0 9 548.3146 104.8898 Tm EMC 7 0 0 7 88.196 11.5129 Tm ( )Tj /P <>BDC /P <>BDC EMC -.02 Tc 7 0 0 7 507.7893 584.7654 Tm ET /P <>BDC /P <>BDC /P <>BDC EMC ( )Tj (evaluation that are payload-limited on the)Tj ET /P <>BDC ET EMC ET ET ( )Tj /P <>BDC EMC /P <>BDC ET EMC BT /P <>BDC /P <>BDC ET BT EMC BT BT /P <>BDC (A320ceo)Tj EMC /P <>BDC 9 0 0 9 229.6141 390.8898 Tm /P <>BDC EMC BT BT /P <>BDC ( )Tj 9 0 0 9 232.4408 764.8898 Tm - Non Perele - News Online, Council Post: Aviation Is The Driving Force Of Hydrogen | QNewsHub, When will the Boeing 737 MAX fly again? 7 0 0 7 338.6433 320.7654 Tm EMC ET 9 0 0 9 408.1854 511.8898 Tm /GS2 gs There are no pumps in the aux fuel system. (174,165)Tj 9 0 0 9 550.5057 236.8898 Tm ( )Tj EMC BT ( )Tj EMC ( )Tj /P <>BDC -.02 Tc BT EMC EMC 7 0 0 7 490.5101 628.9528 Tm (0.0115)Tj BT BT ( )Tj ET ET ET EMC BT ET ( )Tj EMC BT (34,650lbs)Tj ET 0 Tc 0 841.89 609.449 -841.89 re BT BT ET ET (182,200lbs, an MLW of 152,800lbs, and)Tj 7 0 0 7 326.2278 694.9528 Tm /P <>BDC ( )Tj 7 0 0 7 508.2252 11.5129 Tm BT BT 6 0 0 6 403.1408 687.9528 Tm ET (the 737-9 is nearly 7% higher than the)Tj ET /P <>BDC 1 i Centre tank pumps EMC EMC EMC BT 9 0 0 9 367.2442 379.8898 Tm ET EMC /P <>BDC ET Aerial Firefighting with Fire Fighting Airplanes. 9 0 0 9 212.7029 390.8898 Tm ET (CFM56-7B26 engine on the heavier weight)Tj endobj .151 .147 .15 rg EMC BT 9 0 0 9 194.7833 236.8898 Tm /P <>BDC /P <>BDC /P <>BDC EMC ET ET 7 0 0 7 258.2805 672.7654 Tm 7 0 0 7 316.0679 122.7654 Tm -.01 Tc EMC EMC BT 9 0 0 9 211.249 302.8898 Tm EMC /P <>BDC BT EMC 7 0 0 7 230.7317 111.9528 Tm /P <>BDC /P <>BDC 7 0 0 7 130.1443 617.7654 Tm BT /P <>BDC 9 0 0 9 370.2239 390.8898 Tm 6.5 0 0 6.5 176.9362 545.9529 Tm ( )Tj ET ET EMC 9 0 0 9 232.4217 236.8898 Tm ET /P <>BDC /P <>BDC 7 0 0 7 158.74 606.7654 Tm EMC BT ET BT ET /P <>BDC BT BT BT /P <>BDC /P <>BDC In comparison, the fuel cost per)Tj BT (\(see table, page 21\))Tj ET BFE; . BT 7 0 0 7 338.4211 430.9528 Tm .014984 841.89 609.45 -841.89 re (load factor, the A321neo carries a heavier)Tj EMC ( )Tj 7 0 0 7 554.7883 166.7654 Tm ( C)Tj 7 0 0 7 43.6039 144.9528 Tm 518.74 0 l ( )Tj The FAA developed an in-flight gas sampling system, integrated with EMC EMC /P <>BDC 7 0 0 7 439.8175 727.9528 Tm /P <>BDC 9 0 0 9 172.5802 467.8898 Tm ET 9 0 0 9 232.438 137.8898 Tm 9 0 0 9 566.5209 379.8898 Tm EMC EMC BT 0 Tc ET BT EMC ( )Tj EMC ET /P <>BDC ET -.02 Tc 7 0 0 7 141.7322 430.9528 Tm /P <>BDC A Boeing 737-800 NG with all seats removed can not carry more than 24 000 kg of payload and the maximum volume transported can not surpass 184 m3, no matter what you do, as long as, according to the article B737-800BDSF Passenger to Cargo Conversion, "the 737-800BDSF [a factory modified 737-800 NG] is the second B737 New Generation converted EMC 7 0 0 7 54.7071 419.7654 Tm ( )Tj 6 0 0 6 465.9579 659.9528 Tm )Tj (170)Tj ( )Tj EMC -.02 Tc EMC (prices, and can vary by the aircraft type)Tj 7 0 0 7 490.5101 474.9528 Tm /P <>BDC ET /P <>BDC ( )Tj (0.0160)Tj ET ET ET ( )Tj (of fuel against time-related costs. BT EMC ( )Tj 518.735 0 l ET BT /P <>BDC )Tj ET BT /P <>BDC /OC /MC27 BDC The NG/MAX's have separate ENG VALVE CLOSED & SPAR VALVE CLOSED lights in ET ET (1,392)Tj 7 0 0 7 379.3969 78.7654 Tm BT ET /P <>BDC ET The)Tj 7 0 0 7 380.2788 485.7654 Tm 0 Tc (The wider intake fan diameters leading)Tj /P <>BDC EMC 0 Tc .41 .161 .508 rg ( )Tj EMC -.015 Tc EMC ( )Tj (31,416)Tj ET 0 Tc BT [(On a gr)10(oup of r)10(outes betw)6.1(een 484nm and)]TJ Boeing airplanes would have to be modified to prevent loss of inerting at EMC ( )Tj EMC )Tj BT EMC EMC -.02 Tc BT EMC BT ET EMC EMC 7 0 0 7 326.2278 463.9528 Tm BT /P <>BDC Modern Airliners and Civil Aviation Aircraft. 9 0 0 9 36.8583 467.8898 Tm BT /P <>BDC ET (160)Tj /P <>BDC 6 0 0 6 154.1438 757.9528 Tm EMC EMC (483)Tj 13 0 0 13 53.8338 588.8898 Tm ET ( )Tj EMC /P <>BDC (BOS-DEN)Tj 7 0 0 7 53.8582 11.5132 Tm 9 0 0 9 232.438 302.8898 Tm ET 9 0 0 9 202.0349 753.8898 Tm Q BT 7 0 0 7 519.3773 276.9528 Tm ( )Tj (737-800W)Tj /P <>BDC 7 0 0 7 141.7322 309.9528 Tm BT BT BT BT BT /P <>BDC BT ( )Tj (737-8)Tj EMC EMC ( )Tj -.02 Tc ET (141,270)Tj EMC EMC EMC ET BT /F6 1 Tf ET EMC ( N)Tj BT 6.5 0 0 6.5 54.877 722.9529 Tm ET ( )Tj EMC /P <>BDC 9 0 0 9 68.0071 357.8898 Tm 6 0 0 6 153.0397 715.9528 Tm (405)Tj ( )Tj ( )Tj 1 i BT (170)Tj ( )Tj 9 0 0 9 173.7412 203.8898 Tm (141,757)Tj -.02 Tc [(UG)-17.1(U)-8(S)8.1(T)]TJ ET 7 0 0 7 456.2165 78.7654 Tm BT BT BT ET Q 7 0 0 7 445.7203 11.5129 Tm (setting. )Tj (As with the rest of the Airbus aircraft,)Tj ( )Tj -.02 Tc BT ( )Tj /P <>BDC 7 0 0 7 326.2278 518.9528 Tm EMC 7 0 0 7 554.7883 188.7654 Tm ( )Tj ET BT /P <>BDC 7 0 0 7 187.0858 133.9528 Tm BT ET 9 0 0 9 372.9598 170.8898 Tm BT (9.0:1)Tj (0.0154)Tj EMC ( )Tj 9 0 0 9 53.8582 280.8898 Tm EMC ET ET 9 0 0 9 189.8423 467.8898 Tm ET 9 0 0 9 425.183 456.8898 Tm BT ET BT ( )Tj ( )Tj (This is chosen to represent a typical airline)Tj /P <>BDC ( )Tj endstream ET EMC ET ( )Tj 8 0 0 8 259.5105 675.9528 Tm ET EMC Its sales cant be matched. ET ET ET ET ET 0 Tc (170-178)Tj BT 7 0 0 7 204.0935 133.7654 Tm ET ( )Tj 7 0 0 7 520.6108 694.9528 Tm EMC BT (The 737-9 has an 11.2% to 12.7%)Tj BT EMC ET /P <>BDC ET ET EMC (1,074)Tj /P <>BDC .151 .147 .15 rg BT /P <>BDC -.02 Tc 7 0 0 7 365.035 89.9528 Tm BT (74-82)Tj ET BT 9 0 0 9 232.4217 412.8898 Tm BT /P <>BDC BT BT EMC .014984 841.89 609.45 -841.89 re (passenger load factor based on each types)Tj EMC EMC BT EMC EMC BT ( )Tj /P <>BDC /P <>BDC ET /P <>BDC BT 9 0 0 9 232.4217 192.8898 Tm (34,650)Tj /P <>BDC EMC BT -.02 Tc EMC /P <>BDC ( )Tj Q ET BT -.02 Tc ( )Tj ET 7 0 0 7 473.8245 386.9528 Tm ET EMC ET EMC )Tj BT ( )Tj 9 0 0 9 566.9979 423.8898 Tm BT 9 0 0 9 394.0315 632.8898 Tm BT 788 0 obj ET (The first is payload scenario 1, which)Tj (2,115)Tj /P <>BDC 0 Tc ET 7 0 0 7 36.8504 11.5129 Tm 6.5 0 0 6.5 448.3675 532.9529 Tm EMC The flight)Tj /P <>BDC 7 0 0 7 496.3063 727.7654 Tm BT For ground ET 6.5 0 0 6.5 224.5532 598.9529 Tm BT 1 i 9 0 0 9 53.8578 368.8898 Tm -.02 Tc /P <>BDC ET ET /P <>BDC EMC BT 6 0 0 6 527.6392 715.9528 Tm ( )Tj BT ET EMC /P <>BDC BT /P <>BDC 0 Tw EMC ( )Tj 0 Tc /P <>BDC /P <>BDC ET Airbus has come to dethrone the 737 as the leader of the industry. /P <>BDC 9 0 0 9 411.0097 170.8898 Tm /F6 1 Tf 9 0 0 9 379.0889 291.8898 Tm Hi there.. is anyone able to tell me the radius of the arc of the L1 and L2 doors as they are being opened? BT ET EMC EMC BT EMC Boeing 737-800 Aircraft type: Commercial airplane Manufacturer: Boeing Maiden flight year: 1997 I have flown in this plane Reports (16) Reviews (2) Photos (333) Forum (8) List of aircraft operators Boeing 737-800 Specifications ( )Tj 9 0 0 9 369.4947 357.8898 Tm BT ( )Tj EMC /P <>BDC -.02 Tc BT ( )Tj -.0003 Tc ( )Tj ET EMC -.02 Tc (passenger numbers are 136 for the)Tj 8 0 0 8 336.1225 771.7654 Tm ( )Tj ET ET ET BT BT EMC ( )Tj /F1 1 Tf EMC ET (737 MAX 8 & 9 fuel)Tj EMC (56,869)Tj BT (1,824)Tj 7 0 0 7 99.8582 177.7654 Tm /P <>BDC 7 0 0 7 99.8582 540.7654 Tm ( )Tj EMC ET BT /P <>BDC /P <>BDC ET -.02 Tc 53.85 621.704 518.723 183.336 re ET BT -.02 Tc ET 9 0 0 9 215.4313 379.8898 Tm 9 0 0 9 232.438 445.8898 Tm EMC ET /P <>BDC ( )Tj 8 0 0 8 447.9182 771.9529 Tm ET ET 7 0 0 7 163.8846 11.5132 Tm /P <>BDC 7 0 0 7 247.7395 474.7654 Tm BT EMC EMC BT -.02 Tc 789 0 obj EMC 6 0 0 6 339.8239 701.9528 Tm ET ET EMC EMC /P <>BDC 6.5 0 0 6.5 397.1339 702.9529 Tm (evaluate the physical configuration of the)Tj EMC /P <>BDC EMC ( )Tj EMC be fitted with an auxiliary fourth tank which was controlled from the main panel /Artifact <>BDC /P <>BDC ET (136)Tj EMC EMC 6 0 0 6 134.6187 715.9528 Tm EMC BT ET EMC BT EMC (is 2.54 cents per ASM for the same)Tj ET 9 0 0 9 541.6875 489.8898 Tm Because of ( )Tj (1,498)Tj BT /P <>BDC /P <>BDC /P <>BDC EMC ET EMC /P <>BDC /P <>BDC /P <>BDC BT ET /P <>BDC BT EMC /P <>BDC 8 0 0 8 38.4438 647.9528 Tm 9 0 0 9 232.4217 599.8898 Tm 7 0 0 7 82.8504 210.9528 Tm ( )Tj ( )Tj ET ( )Tj -.02 Tc BT EMC ( )Tj ET EMC 8 0 0 8 43.6039 619.9528 Tm EMC /P <>BDC /F4 1 Tf (127 passengers on the longest sector,)Tj 0 Tc EMC ( )Tj EMC ( )Tj BT EMC 9 0 0 9 421.0664 401.8898 Tm ET EMC /P <>BDC BT /P <>BDC 13 0 0 13 53.8578 181.8898 Tm BT 6.5 0 0 6.5 296.4841 689.9529 Tm 5.25 0 0 5.25 100.8225 11.5132 Tm Q 6 0 0 6 154.2695 743.9528 Tm 9 0 0 9 374.2479 71.8898 Tm EMC [(BOS-SE)-13.9(A)]TJ 8 0 0 8 74.9636 591.9528 Tm -.015 Tc ( )Tj ET ( )Tj BT -.01 Tc 0 Tc /P <>BDC 17 0 0 17 526.2604 775.1944 Tm 6.5 0 0 6.5 480.4 650.9529 Tm My simulation is focused on postcrash fires. /P <>BDC ( )Tj ET 9 0 0 9 204.9907 467.8898 Tm /P <>BDC ( )Tj It is produced in the Renton plant in Washington by Boeing Commercial Airplanes. EMC Download the Final ET ET (. /P <>BDC 7 0 0 7 299.0601 298.9528 Tm ET BT (483)Tj ET ET /P <>BDC EMC ET /F4 1 Tf ET /P <>BDC ET -.02 Tc ET /F6 1 Tf ET ET 56 0 0 56 447.1169 682.1944 Tm All the)Tj BT -.02 Tc ET BT ET EMC ET EMC 9 0 0 9 36.8504 214.8898 Tm EMC /GS2 gs (which is BOS-LAX, whereas the 737-800)Tj 6.5 0 0 6.5 347.0849 722.9529 Tm Regarding winglets, I think Simple Flying explains it well. BT EMC 7 0 0 7 337.6855 210.9528 Tm ()Tj ( )Tj 9 0 0 9 385.6838 346.8898 Tm ( )Tj EMC 9 0 0 9 411.0181 225.8898 Tm 0 Tc BT (34,650)Tj EMC BT ET ( )Tj BT BT -.02 Tc 9 0 0 9 204.06 742.8898 Tm [(BOS-D)17.1(T)-11(W)]TJ ( )Tj EMC /P <>BDC ( )Tj /P <>BDC /P <>BDC (900ER and 737-9, A320ceo and A320neo,)Tj 9 0 0 9 408.1854 610.8898 Tm 9 0 0 9 212.3652 775.8898 Tm BT (makes a flight-for-flight comparison)Tj EMC /P <>BDC BT BT (0.0142)Tj ET BT BT .151 .147 .15 rg /P <>BDC BT (same number of passengers is carried on)Tj ( )Tj BT /P <>BDC EMC 7 0 0 7 37.0536 661.9528 Tm BT ET 5.25 0 0 5.25 40.8474 11.5129 Tm EMC 7 0 0 7 508.4124 540.7654 Tm BT (5,277)Tj EMC (Engine)Tj /P <>BDC BT 6.5 0 0 6.5 397.8619 611.9529 Tm (more than 3% is more than offset by the)Tj ET EMC /P <>BDC The VNE or never exceed speed for the Boeing 737-800 is 340 KIAS(Knots indicated airspeed) or Mach 0.82. BT ET 9 0 0 9 546.3754 159.8898 Tm 0 Tc /P <>BDC /P <>BDC ET q 1 0 0 1 215.441 73.878 cm 0 0 m ET /P <>BDC EMC 7 0 0 7 86.3128 540.7654 Tm 9 0 0 9 215.4313 478.8898 Tm S 9 0 0 9 36.8504 60.8898 Tm ET EMC ET ET /P <>BDC BT EMC ET ( )Tj ET ET 9 0 0 9 53.8582 489.8898 Tm /P <>BDC ET /P <>BDC (273,917)Tj BT 0 Tc ET (achieve five inches extra legroom. (The sectors are chosen to ensure a)Tj /P <>BDC EMC BT /P <>BDC 9 0 0 9 202.684 357.8898 Tm 8 0 0 8 520.6337 771.7654 Tm 7 0 0 7 141.7322 518.9528 Tm /P <>BDC 0 Tc /P <>BDC BT (150)Tj ET /P <>BDC ET /P <>BDC ( )Tj 9 0 0 9 394.0123 632.8898 Tm /P <>BDC 0 Tc /P <>BDC ET (36,960)Tj /P <>BDC BT ( )Tj BT EMC ( )Tj - Non Perele - News Online, Hi, EMC ( )Tj ET EMC /P <>BDC 7 0 0 7 363.2711 419.9528 Tm /P <>BDC EMC -.02 Tc BT /P <>BDC ( )Tj ( )Tj 0 Tc ET ( )Tj ET 0 Tc ET BT 0 Tc /P <>BDC 7 0 0 7 113.1366 419.9528 Tm /P <>BDC EMC BT /P <>BDC EMC ( )Tj EMC ET ( )Tj BT EMC -.02 Tc BT EMC /P <>BDC EMC /P <>BDC ( )Tj (revenue benefit of 11 passengers. BT ( )Tj 9 0 0 9 411.0097 412.8898 Tm ET [(C)17.1(OS/104)]TJ (The A320neo family and 737 MAX)Tj 7 0 0 7 43.6039 254.9528 Tm ( )Tj EMC /P <>BDC 0 Tc EMC ET ( )Tj ET BT ( )Tj EMC ET )Tj (payload is carried. EMC ( )Tj Wed love you to share what you build when youre done. .023 .567 .626 RG ET 7 0 0 7 54.7071 507.7654 Tm EMC /P <>BDC (136)Tj BT /P <>BDC ET -.02 Tc /P <>BDC 7 0 0 7 294.4014 89.7654 Tm EMC 0 Tc ET -.02 Tc BT ( )Tj 0 Tc ET 7 0 0 7 539.8962 507.9528 Tm EMC 0 Tc ( )Tj (39,732)Tj (403)Tj 9 0 0 9 394.0123 357.8898 Tm (BOS-LAX due to the strong headwind)Tj 7 0 0 7 82.2047 474.9528 Tm 9 0 0 9 36.8504 379.8898 Tm BT -.02 Tc EMC ET ET /P <>BDC BT ET The relative high)Tj BT EMC BT (163)Tj ET BT 0 Tc EMC ET BT EMC BT BT 0 Tc EMC BT EMC EMC ET EMC /P <>BDC ( )Tj ET 7 0 0 7 141.7322 441.9528 Tm EMC BT 6.5 0 0 6.5 64.6596 637.9529 Tm ET /P <>BDC ET BT ET 7 0 0 7 182.5706 639.9528 Tm /P <>BDC BT BT ET A series of ten tests were performed (five flight, EMC ET BT ET EMC EMC BT EMC EMC /P <>BDC /P <>BDC 7 0 0 7 404.3599 661.7654 Tm ET ET 6.5 0 0 6.5 346.9224 585.9529 Tm /P <>BDC BT ET /P <>BDC /P <>BDC 9 0 0 9 548.2598 489.8898 Tm EMC ET (11,593)Tj 7 0 0 7 37.0536 672.9528 Tm 7 0 0 7 554.7883 562.7654 Tm BT 7 0 0 7 37.6993 78.9528 Tm /P <>BDC ET ( )Tj /P <>BDC 9 0 0 9 276.2863 115.8898 Tm BT EMC /P <>BDC ET 9 0 0 9 411.0097 148.8898 Tm ET ET 7 0 0 7 343.2355 683.7654 Tm BT ET /P <>BDC Q ET 1 i -.005 Tc BT -.02 Tc EMC ET BT )Tj ET /P <>BDC /P <>BDC -.02 Tc 0 Tc 737-600/-700/-800/-900 with densitometer: BT ( )Tj ( )Tj EMC ET -.02 Tc ET 7 0 0 7 108.6215 133.9528 Tm 9 0 0 9 36.8504 236.8898 Tm (hour and per mile reduces . EMC /P <>BDC /P <>BDC EMC EMC 7 0 0 7 430.039 705.9528 Tm [(737 M)-8.1(A)-24.9(X-8:)]TJ /P <>BDC ET 7 0 0 7 247.7395 408.7654 Tm ET BT 17 0 0 17 550.9253 758.6944 Tm /P <>BDC EMC -.02 Tc ET EMC BT /P <>BDC EMC 9 0 0 9 524.3162 214.8898 Tm BT BT 6 0 0 6 176.4941 687.9528 Tm BT ET BT 9 0 0 9 215.4313 357.8898 Tm (City-pair)Tj ( )Tj 0 Tc (0.0286)Tj 0 Tc ( )Tj EMC ET )Tj /P <>BDC EMC 9 0 0 9 53.8582 665.8898 Tm 9 0 0 9 372.2129 192.8898 Tm Refuelling of the aux tanks is done by moving the guarded switch in the ( )Tj 9 0 0 9 527.0365 456.8898 Tm ET 0 Tc (10)Tj ET EMC BT BT 8 0 0 8 302.5117 675.9528 Tm 0 Tc /F1 1 Tf /P <>BDC ET ET 9 0 0 9 53.8338 225.8898 Tm EMC 7 0 0 7 294.4014 441.7654 Tm ET BT -.02 Tc /P <>BDC BT /TT2 1 Tf /P <>BDC Reads payload (passenger and baggage) weights via FSUIPC. 7 0 0 7 187.0858 232.9528 Tm EMC . ET ( )Tj /P <>BDC /P <>BDC /P <>BDC ( )Tj BT BT 6.5 0 0 6.5 447.8411 663.9529 Tm ( )Tj 7 0 0 7 37.6993 221.9528 Tm /P <>BDC ET /F1 1 Tf EMC ( )Tj (used in flight planning, the scenarios use a)Tj ET ET 7 0 0 7 54.7071 89.7654 Tm /P <>BDC BT BT EMC -.02 Tc BT /P <>BDC (airlines across the world. BT 0 Tc 7 0 0 7 158.74 67.7654 Tm 7 0 0 7 536.3849 628.7654 Tm ET ( )Tj (36,960)Tj BT BT EMC ET EMC ET ET EMC 7 0 0 7 379.3969 144.7654 Tm EMC ( )Tj /P <>BDC 6.5 0 0 6.5 448.4585 702.9529 Tm ET (136)Tj -.02 Tc EMC EMC ( )Tj BT BT BT 9 0 0 9 505.9653 115.8898 Tm ( )Tj EMC EMC /P <>BDC /P <>BDC /P <>BDC BT /GS2 gs /P <>BDC BT 0 Tc EMC BT 7 0 0 7 316.0679 133.7654 Tm (33,000lbs of thrust with a fan diameter of)Tj EMC ( )Tj 7 0 0 7 258.2805 606.7654 Tm 7 0 0 7 338.3085 331.9528 Tm EMC /P <>BDC BT 9 0 0 9 210.9209 104.8898 Tm ( )Tj /OC /MC1320 BDC BT BT 8 0 0 8 334.994 619.9528 Tm 7 0 0 7 204.0935 584.7654 Tm BT EMC (The later generation aircraft are set to)Tj (City-pair)Tj BT EMC /P <>BDC /P <>BDC BT ( )Tj 0 Tc ( )Tj 6 0 0 6 215.4988 701.9528 Tm EMC EMC ET /P <>BDC EMC Max T/O Weight: 174200 Lb Max Landing Weight: 146300 Lb Operating Weight: 102100 Lb Fuel Capacity: 69982 lbs Lb Payload W/Full Fuel: 2618 Lb Max Payload: 36200 Lb Range Normal Range: 5644 nm Max Range: 5673 nm Service Ceiling: 41000 ft Distances Balanced Field Length: 7210 ft Landing Distance: 4117 ft Performance Rate of Climb: 3100 fpm ET 9 0 0 9 369.892 412.8898 Tm (BOS-DEN)Tj 7 0 0 7 141.7322 67.9528 Tm BT EMC BT ET -.01 Tc EMC /P <>BDC ET 7 0 0 7 125.6292 342.7654 Tm /P <>BDC ( )Tj EMC ET /P <>BDC EMC ( )Tj ET /P <>BDC ( )Tj .41 .161 .508 RG ET 7 0 0 7 294.4014 518.7654 Tm ET /P <>BDC BT ET 9 0 0 9 376.0986 324.8898 Tm /P <>BDC BT EMC EMC ET /P <>BDC /P <>BDC EMC -.02 Tc (10)Tj /P <>BDC EMC ET ET 7 0 0 7 230.7317 309.9528 Tm /P <>BDC /P <>BDC ET EMC 9 0 0 9 215.4313 346.8898 Tm ( )Tj ( )Tj /Artifact <>BDC /P <>BDC 9 0 0 9 373.9277 478.8898 Tm ( )Tj ET ET BT /P <>BDC 8 0 0 8 164.9203 771.9528 Tm /P <>BDC /P <>BDC BT EMC ET 9 0 0 9 36.8504 49.8898 Tm 7 0 0 7 355.3163 188.7654 Tm ET ET /P <>BDC (fuel capacity of 6,303USG )Tj The New Midsized Airplane. (LEAP-1B. BT /P <>BDC 9 0 0 9 550.3618 324.8898 Tm EMC EMC EMC /P <>BDC ET EMC EMC flightdeck (below the F/O's FMC) but they have since been removed to a ET /P <>BDC ( )Tj 0 Tc BT 7 0 0 7 404.101 265.7654 Tm BT /P <>BDC EMC 7 0 0 7 277.3936 375.9528 Tm BT 7 0 0 7 108.6215 738.9528 Tm BT EMC BT 7 0 0 7 204.0935 408.7654 Tm ET EMC ( )Tj /P <>BDC (170)Tj BT (sector. /P <>BDC /P <>BDC ( )Tj 7 0 0 7 537.7804 166.9528 Tm 8 0 0 8 95.6042 633.9528 Tm /P <>BDC EMC BT /P <>BDC /P <>BDC BT ET 5.25 0 0 5.25 100.8225 11.5132 Tm ET 6 0 0 6 371.6897 659.9528 Tm ET 0 Tc BT EMC /P <>BDC 9 0 0 9 394.0123 401.8898 Tm ET EMC EMC EMC ( )Tj 7 0 0 7 439.2087 386.9528 Tm /P <>BDC (operate with first, economy-plus and)Tj /P <>BDC BT -.02 Tc BT BT ET ET /P <>BDC /P <>BDC 9 0 0 9 551.0194 588.8898 Tm [(737-900E)-33(R)]TJ ( )Tj EMC EMC /P <>BDC EMC /P <>BDC 7 0 0 7 478.9484 727.9528 Tm 7 0 0 7 404.101 287.7654 Tm /OC /MC4777 BDC BT 0 Tw Bombardier CRJ 700/CRJ 900/CRJ 1000 Series. (scenario 2, where all types carry an 85%)Tj 9 0 0 9 394.0315 269.8898 Tm ET EMC 0 Tc BT BT /P <>BDC BT EMC 9 0 0 9 537.6801 258.8898 Tm ET 9 0 0 9 229.6064 126.8898 Tm ( )Tj ET BT /P <>BDC /P <>BDC /P <>BDC EMC 7 0 0 7 473.8245 364.9528 Tm ( )Tj 7 0 0 7 294.4014 386.7654 Tm ET (34,650)Tj 7 0 0 7 491.4046 111.9528 Tm EMC EMC ET /P <>BDC the two components of the air are separated, the nitrogenenriched air (NEA) is EMC 7 0 0 7 404.101 100.7654 Tm )Tj /P <>BDC -.02 Tc ET BT S EMC 7 0 0 7 554.7883 474.7654 Tm 7 0 0 7 82.8504 177.9528 Tm endobj /P <>BDC BT 7 0 0 7 99.8582 100.7654 Tm 8 0 0 8 394.0237 49.8898 Tm ET ET .014984 841.89 609.45 -841.89 re (shows an even greater fuel burn)Tj 7 0 0 7 158.74 298.7654 Tm ET 9 0 0 9 543.5425 522.8898 Tm EMC EMC ET (materials. ET EMC )Tj 7 0 0 7 337.6855 573.9528 Tm 9 0 0 9 361.1316 214.8898 Tm -.02 Tc BT BT /P <>BDC EMC /P <>BDC .151 .147 .15 rg /P <>BDC EMC The NG has 6 dripsticks in each wing tank and 4 in the centre BT 9 0 0 9 170.752 368.8898 Tm (maintenance. BT /P <>BDC ET BT EMC /P <>BDC EMC (126,312)Tj ET -.01 Tc ( )Tj 6 0 0 6 459.5796 729.9528 Tm 7 0 0 7 491.7142 694.7654 Tm /P <>BDC -.02 Tc ( )Tj /P <>BDC BT ( )Tj BT EMC /P <>BDC BT ( )Tj /P <>BDC 9 0 0 9 411.0097 137.8898 Tm /P <>BDC /P <>BDC 8 0 0 8 243.3422 771.9529 Tm ( )Tj BT /P <>BDC BT EMC /P <>BDC -.548 -4.9642 -.5018 -4.9261 -.4557 -4.8883 c /P <>BDC /P <>BDC The average fuel)Tj 0 Tc EMC [(Aircr)10(aft type)]TJ /P <>BDC 0 Tc [(equal-siz)6.1(ed 737NG counterpar)-23(ts and A320ceo)]TJ 7 0 0 7 297.632 727.9528 Tm ET (A320ceo a range of 2,800-2,900nm with)Tj BT ET (some minor aerodynamic improvements)Tj Q In the)Tj BT BT 9 0 0 9 53.8578 335.8898 Tm EMC In contrast, Boeing has)Tj /P <>BDC EMC 9 0 0 9 215.4409 324.8898 Tm ET BT EMC 7 0 0 7 315.5217 573.7654 Tm BT ET ET ( )Tj /P <>BDC /P <>BDC BT ET (29,432)Tj BT EMC ( )Tj /P <>BDC EMC /P <>BDC 9 0 0 9 394.0157 423.8898 Tm (LRC; the same as the primary sector. BT /P <>BDC q 1 0 0 1 411.01 480.878 cm 0 0 m /P <>BDC 7 0 0 7 490.8321 122.7654 Tm BT 7 0 0 7 99.8582 342.7654 Tm /P <>BDC ( )Tj EMC 7 0 0 7 404.101 298.7654 Tm 7 0 0 7 387.0932 298.9528 Tm 7 0 0 7 37.0536 573.9528 Tm BT /P <>BDC BT (. /P <>BDC /P <>BDC ( )Tj ET EMC EMC /P <>BDC BT [(A3)24.9(20ceo v)12.9(ersus 7)-33(3)8.1(7-800 )]TJ ET EMC ET 7 0 0 7 518.4953 397.9528 Tm (between different aircraft types impossible)Tj BT EMC -.02 Tc /P <>BDC BT /P <>BDC /P <>BDC 9 0 0 9 411.0181 335.8898 Tm /P <>BDC 0 Tc EMC BT 0 Tc -.02 Tc /P <>BDC 7 0 0 7 37.0536 617.9528 Tm /P <>BDC EMC 9 0 0 9 192.8213 60.8898 Tm <>stream BT (destination airport are listed )Tj 9 0 0 9 246.6141 709.8898 Tm EMC EMC (make the range. ET ET EMC (2,729)Tj ET 7 0 0 7 99.5912 606.9528 Tm .023 .567 .626 rg ET ET /P <>BDC ET 9 0 0 9 229.6064 49.8898 Tm BT EMC ET /P <>BDC EMC - Modern Airliners. ET BT (170)Tj /P <>BDC BT 7 0 0 7 298.514 639.9528 Tm 9 0 0 9 394.0237 247.8898 Tm /GS1 gs /P <>BDC /P <>BDC /P <>BDC 6.5 0 0 6.5 279.814 624.9529 Tm EMC ET ET ( )Tj ET /P <>BDC EMC 0 Tc EMC 0 Tc BT (fuselage length. BT EMC (and bypass ratio of 12.5:1 as the A320neo;)Tj ET /P <>BDC ET EMC ET /P <>BDC ( )Tj /P <>BDC EMC ( )Tj BT 0 Tc )Tj -.02 Tc /P <>BDC ET ( )Tj (the CFM LEAP-1A32 variant. EMC 0 Tc 7 0 0 7 404.101 276.7654 Tm /P <>BDC -.02 Tc 0 Tc ( )Tj ( )Tj EMC EMC 9 0 0 9 299.3893 478.8898 Tm 0 Tc -.01 Tc (Using the evaluation payloads of 170)Tj BT ET EMC /F6 1 Tf 0 Tc ET 9 0 0 9 229.6045 104.8898 Tm (The 737-9 uses the same CFM LEAP-)Tj BT /P <>BDC /P <>BDC BT 7 0 0 7 554.7883 320.7654 Tm ( )Tj /P <>BDC BT 0 Tc BT BT /P <>BDC /P <>BDC BT ( )Tj EMC ( )Tj 5.25 0 0 5.25 73.853 11.5132 Tm BT EMC (0.0111)Tj ET BT ET 7 0 0 7 520.6108 705.9528 Tm Pisquali 19/05/2018 at 16:07 Reply. 7 0 0 7 445.619 606.7654 Tm ET EMC ( )Tj ( )Tj ET BT EMC BT /P <>BDC 0 Tc ( )Tj EMC /P <>BDC /P <>BDC ( )Tj /P <>BDC /P <>BDC 6 0 0 6 497.1212 729.9528 Tm EMC EMC 6.5 0 0 6.5 382.9199 735.9529 Tm ( )Tj ET /P <>BDC BT BT /P <>BDC ( )Tj BT 7 0 0 7 247.7395 298.7654 Tm BT 7 0 0 7 297.632 683.9528 Tm /P <>BDC )Tj 0 Tc 9 0 0 9 53.8582 115.8898 Tm EMC -.02 Tc BT /P <>BDC EMC BT -.02 Tc EMC The aircraft in this)Tj /P <>BDC EMC /P <>BDC BT BT ET /P <>BDC ( )Tj BT ET BT EMC EMC (economy-plus seats typically offer two to)Tj BT BT 0 Tc 8 0 0 8 43.6039 689.9528 Tm /P <>BDC /P <>BDC ET BT ET ( )Tj BT EMC ET ( )Tj ( )Tj EMC BT EMC EMC 5.25 0 0 5.25 447.6106 11.5129 Tm 9 0 0 9 215.4409 434.8898 Tm EMC /P <>BDC /P <>BDC EMC 9 0 0 9 99.3355 170.8898 Tm EMC 7 0 0 7 53.8582 11.5132 Tm 9 0 0 9 394.0123 390.8898 Tm 7 0 0 7 241.5317 320.9528 Tm ET BT ET 9 0 0 9 200.7278 170.8898 Tm /GS1 gs (\(see)Tj ET ET ET BT EMC /P <>BDC EMC BT EMC EMC /P <>BDC BT ( )Tj BT /P <>BDC /P <>BDC ET BT q 1 0 0 1 232.438 95.878 cm 0 0 m /P <>BDC EMC /P <>BDC 0 Tc 7 0 0 7 518.4953 243.9528 Tm BT /P <>BDC 9 0 0 9 177.7731 181.8898 Tm ET /P <>BDC 7 0 0 7 430.039 573.9528 Tm BT S -.02 Tc ( )Tj (20)Tj S /P <>BDC ET /P <>BDC 0 Tc ET ET ET EMC /GS1 gs BT 7 0 0 7 279.1575 441.9528 Tm BT 9 0 0 9 232.438 357.8898 Tm EMC /P <>BDC 7 0 0 7 387.0159 507.9528 Tm EMC BT ET 7 0 0 7 37.6993 309.9528 Tm /P <>BDC BT 0 Tc EMC EMC ET 9 0 0 9 534.7515 599.8898 Tm ( )Tj 0 Tc /P <>BDC EMC 9 0 0 9 411.0181 159.8898 Tm 6 0 0 6 365.7265 729.9528 Tm /P <>BDC EMC /P <>BDC BT BT ( )Tj -.02 Tc /P <>BDC EMC 7 0 0 7 473.4744 518.9528 Tm EMC /P <>BDC 7 0 0 7 101.0963 408.9528 Tm BT /P <>BDC (19)Tj EMC ET EMC /P <>BDC ET 0 Tc (148,504)Tj ET ET EMC (comparison more challenging. 7 0 0 7 518.4953 309.9528 Tm 0 Tc ET -.02 Tc /P <>BDC /P <>BDC /P <>BDC EMC /P <>BDC EMC ET /P <>BDC 7 0 0 7 403.478 562.7654 Tm BT (\(Miami\) sector, to 299 degrees on the)Tj EMC EMC ET 7 0 0 7 508.6712 232.7654 Tm EMC (3,850)Tj ET 6.5 0 0 6.5 225.3721 585.9529 Tm -.01 Tc 10 0 0 10 51.9004 814.1973 Tm EMC BT (163)Tj -.02 Tc /P <>BDC BT ET /P <>BDC 6.5 0 0 6.5 397.0428 532.9529 Tm /P <>BDC EMC BT EMC each aircraft is sourced from different places. ET .964 .834 .406 rg (39,270)Tj /P <>BDC EMC /P <>BDC ET 7 0 0 7 445.619 408.7654 Tm /Artifact <>BDC ( )Tj EMC EMC ET (The overflight and airport charges are)Tj 0 Tc 9 0 0 9 408.2047 93.8898 Tm ( )Tj BT BT BT (4,218)Tj 9 0 0 9 206.8407 412.8898 Tm 7 0 0 7 518.4953 441.9528 Tm BT /P <>BDC ET EMC EMC 9 0 0 9 36.8583 445.8898 Tm ( )Tj /GS1 gs EMC 7 0 0 7 439.2087 364.9528 Tm S /P <>BDC BT BT 9 0 0 9 206.6251 236.8898 Tm /P <>BDC BT BT /P <>BDC EMC EMC BT ( )Tj EMC ( )Tj 9 0 0 9 357.6917 192.8898 Tm ET 7 0 0 7 187.0858 496.9528 Tm ET 9 0 0 9 232.4217 390.8898 Tm 9 0 0 9 522.1225 555.8898 Tm BT (0.0124)Tj (The engine choice on the A320neo is)Tj ( )Tj [(UG)-17.1(U)-8(S)8.1(T)]TJ /P <>BDC -.02 Tc 19.843 0 l ET BT 0 Tc 7 0 0 7 387.0159 474.9528 Tm ( )Tj ET EMC ( )Tj (124,650)Tj Everything you need to know about the Boeing 737 600/700/800/900 - NGs History & Development of . 0 Tc ET Flight crew can select fwd or aft tanks but normal practice is to use both ( )Tj BT 9 0 0 9 192.1373 401.8898 Tm /P <>BDC ET (737-800:)Tj (34,650)Tj BT EMC 7 0 0 7 297.632 474.9528 Tm BT -.02 Tc ET BT ET EMC ET ( )Tj BT /P <>BDC EMC /P <>BDC ET 0 Tc h 9 0 0 9 211.0081 82.8898 Tm (6,875)Tj ET ( )Tj 9 0 0 9 495.0108 170.8898 Tm ET -.01 Tc 6.5 0 0 6.5 276.4014 637.9529 Tm 0 Tc 7 0 0 7 187.0858 408.9528 Tm (operation the overflight and airport)Tj /P <>BDC BT (45,276)Tj 9 0 0 9 548.1865 522.8898 Tm ( )Tj 0 Tc ET EMC ( )Tj BT 9 0 0 9 53.8338 115.8898 Tm ( )Tj EMC /P <>BDC EMC .176 .307 .621 rg ET 6 0 0 6 206.4048 687.9528 Tm ET ( )Tj 7 0 0 7 99.8582 309.7654 Tm ET ET 9 0 0 9 373.708 181.8898 Tm 9 0 0 9 411.0097 115.8898 Tm /P <>BDC BT 9 0 0 9 195.6833 115.8898 Tm ( )Tj 7 0 0 7 204.0935 232.7654 Tm 9 0 0 9 386.0797 71.8898 Tm BT BT ET (variant used in this study is the CFM)Tj /P <>BDC /P <>BDC (35,112)Tj /P <>BDC [(AIRL)8.1(INE & AIR)7.1(CRAF)-12.9(T)18.1( OPERA)56.9(T)-8.1(ION)-13.9(S)]TJ 7 0 0 7 338.6433 177.7654 Tm ET ET ( )Tj (translate into increased range and)Tj /F6 1 Tf (737-8)Tj 7 0 0 7 278.2756 78.9528 Tm EMC BT BT ET -.02 Tc 7 0 0 7 179.5605 221.9528 Tm BT EMC (2,601)Tj EMC BT BT EMC -.01 Tc 7 0 0 7 258.2805 408.7654 Tm EMC EMC (31,416lbs)Tj EMC 0 Tc EMC EMC 7 0 0 7 199.5784 694.7654 Tm EMC 9 0 0 9 394.0157 82.8898 Tm EMC ET 9 0 0 9 564.8296 82.8898 Tm 7 0 0 7 490.5101 694.9528 Tm EMC ET ET /GS1 gs (economy seats are at six-abreast. EMC EMC ( )Tj -.02 Tc EMC The A321ceo is restricted on four)Tj BT /P <>BDC ET BT EMC /P <>BDC EMC EMC BT EMC BT /P <>BDC /P <>BDC ET ET EMC EMC 7 0 0 7 82.8504 386.9528 Tm /P <>BDC (166,090)Tj EMC (800 to 9.0:1 on the 737-8 . EMC /P <>BDC BT /P <>BDC EMC ET EMC /P <>BDC /P <>BDC EMC 7 0 0 7 508.4124 320.7654 Tm /P <>BDC (0.0110)Tj /P <>BDC BT /P <>BDC ET 9 0 0 9 207.2279 511.8898 Tm (A321ceo versus the 737-900ER\(W\), in the)Tj 7 0 0 7 403.478 474.7654 Tm EMC BT -.01 Tc /Artifact <>BDC /P <>BDC BT [(T)95.9(o)0( do)12(wnload mor)10(e than 1,200)]TJ /P <>BDC 7 0 0 7 387.0932 221.9528 Tm 7 0 0 7 518.4953 232.9528 Tm 8 0 0 8 53.9012 749.9529 Tm /P <>BDC 7 0 0 7 554.7883 111.7654 Tm ( )Tj (248,064)Tj /P <>BDC EMC ( )Tj ( )Tj EMC ET 8 0 0 8 97.5245 745.9528 Tm