(9,451)Tj 6.5 0 0 6.5 170.1113 702.9529 Tm 7 0 0 7 316.0679 342.7654 Tm EMC /P <>BDC /P <>BDC BT BT (82,110)Tj EMC 7 0 0 7 230.7317 100.9528 Tm /P <>BDC ( )Tj ET EMC BT EMC /P <>BDC 9 0 0 9 568.024 148.8898 Tm /P <>BDC ( )Tj ET ( )Tj 9 0 0 9 195.4763 258.8898 Tm 9 0 0 9 394.0123 621.8898 Tm ET 9 0 0 9 394.0315 511.8898 Tm 6 0 0 6 246.6462 743.9528 Tm EMC 9 0 0 9 206.8842 522.8898 Tm ( )Tj EMC 7 0 0 7 321.4957 430.9528 Tm 0 Tc EMC /P <>BDC /P <>BDC 9 0 0 9 51.0236 302.8898 Tm BT 6.5 0 0 6.5 346.019 742.9529 Tm ET /P <>BDC 7 0 0 7 158.74 276.7654 Tm /P <>BDC 0 Tc 9 0 0 9 68.0071 566.8898 Tm /P <>BDC 9 0 0 9 394.0315 621.8898 Tm 9 0 0 9 557.1673 794.1039 Tm ( )Tj ET ET ET /P <>BDC ET ET .151 .147 .15 rg /P <>BDC /P <>BDC EMC /P <>BDC ET BT EMC BT /P <>BDC /P <>BDC ( )Tj /P <>BDC ET ET (39,270)Tj /P <>BDC EMC 9 0 0 9 53.8578 247.8898 Tm EMC 7 0 0 7 148.0554 11.5132 Tm BT EMC EMC BT next aircraft /P <>BDC /P <>BDC ( )Tj 7 0 0 7 338.6433 375.7654 Tm 9 0 0 9 552.2312 676.8898 Tm ( )Tj 7 0 0 7 429.157 738.9528 Tm 378 0 0 271.8 -.30716 30.902 cm ET BT (this analysis is 20/42/117, giving a total)Tj (increased the thrust ratings on the MAX)Tj EMC BT EMC (34,650)Tj BT BT BT ET /P <>BDC ( )Tj EMC 0 Tc BT BT ET /P <>BDC 8 0 0 8 122.6593 760.7654 Tm 0 Tc ET /P <>BDC ET 7 0 0 7 321.6356 287.9528 Tm EMC ET ET ET (major airports, which could lead to the)Tj EMC ET -.02 Tc /P <>BDC BT /P <>BDC ( )Tj 0 Tc 0 Tc 6.5 0 0 6.5 378.2463 598.9529 Tm /GS1 gs BT (0.0119)Tj 7 0 0 7 36.8504 155.9528 Tm EMC 7 0 0 7 259.1625 78.7654 Tm 7 0 0 7 294.4014 672.7654 Tm BT BT EMC -.02 Tc -.02 Tc (157)Tj -.02 Tc BT ET 9 0 0 9 53.8582 753.8898 Tm 9 0 0 9 215.4409 445.8898 Tm ET 7 0 0 7 70.8101 441.9528 Tm EMC ET /P <>BDC (A320ceo a range of 2,800-2,900nm with)Tj BT EMC EMC 9 0 0 9 53.8582 489.8898 Tm 7 0 0 7 492.5963 738.7654 Tm Its fuel burn and)Tj ET /P <>BDC 9 0 0 9 232.4408 698.8898 Tm BT ][F$, c;9M$ C[\SU~s#4B#g"DH V6S[_t099J'Nbqur((h\Yf'urV(nYYW6V*f]+ ET ( )Tj EMC (34,650)Tj 6 0 0 6 434.211 701.9528 Tm EMC ET /P <>BDC (166,090)Tj EMC /P <>BDC (US gallons \(USG\) )Tj BT EMC ET 7 0 0 7 363.2711 111.9528 Tm BT 9 0 0 9 195.231 423.8898 Tm (l)Tj /P <>BDC EMC ET (207,336)Tj BT BT ( )Tj EMC 7 0 0 7 404.3599 661.7654 Tm BT BT ET /P <>BDC BT BT ET ET EMC ET EMC ( )Tj EMC ET EMC /F4 1 Tf BT ET ET 7 0 0 7 520.6108 617.9528 Tm ET 7 0 0 7 297.632 606.9528 Tm ET /P <>BDC 8 0 0 8 136.4919 703.9528 Tm BT EMC /P <>BDC ET BT ET ET /P <>BDC BT 0 Tc BT ( )Tj BT [(r)10(atio)]TJ 7 0 0 7 99.8582 243.7654 Tm (310,080)Tj BT 9 0 0 9 394.0315 742.8898 Tm /P <>BDC BT BT /OC /MC1183 BDC ( )Tj 19.851 0 l 9 0 0 9 53.8578 390.8898 Tm BT ET [(F)11(uel capacity - U)-8.1(S)0(G)]TJ BT /P <>BDC 9 0 0 9 68.0071 577.8898 Tm 7 0 0 7 70.1644 540.9528 Tm EMC BT 9 0 0 9 394.0315 269.8898 Tm /P <>BDC (ESAD)Tj EMC [(737 M)-8.1(A)-24.9(X-8)]TJ After 7 0 0 7 456.2165 100.7654 Tm (830)Tj EMC ( )Tj BT ET EMC 9 0 0 9 214.575 115.8898 Tm ( )Tj ( )Tj BT (0.0155)Tj BT EMC 6 0 0 6 214.7428 673.9528 Tm 9 0 0 9 382.7137 93.8898 Tm /P <>BDC EMC 9 0 0 9 508.3771 698.8898 Tm ( )Tj ET EMC /GS1 gs (34,650)Tj 7 0 0 7 241.5317 584.9528 Tm 7 0 0 7 508.4124 716.7654 Tm ET The accuracy tolerance of the fuel flow transmitter is a function of the fuel flow. 7 0 0 7 444.737 78.7654 Tm EMC On the 1-500's, the centre tank pumps are located in a dry ET /P <>BDC (CFM56-5B4/P)Tj (27,000lbs, a fan diameter of 69 inches and)Tj ( )Tj 9 0 0 9 232.4408 753.8898 Tm EMC 9 0 0 9 535.511 379.8898 Tm /P <>BDC The advanced wing airfoil design provides an economical cruise speed of .789 Mach (530 mph) - compared to .745 Mach for earlier 737 models. EMC ET ET EMC EMC ( )Tj ET ( )Tj 9 0 0 9 394.0315 654.8898 Tm /P <>BDC BT 9 0 0 9 531.8156 280.8898 Tm The wheelbase which is the distance from the nosewheel to the line between the main wheels, which is 11.07 metres. BT /P <>BDC 7 0 0 7 118.104 210.7654 Tm EMC ET /P <>BDC 7 0 0 7 383.0719 716.7654 Tm EMC tanks into the centre tank where it is then fed to the engines in the normal ET 10 0 0 10 54.8804 814.1973 Tm (104)Tj BT -.02 Tc 7 0 0 7 439.4675 89.9528 Tm BT /P <>BDC EMC 6 0 0 6 561.1918 743.9528 Tm /P <>BDC ET ( )Tj EMC -.02 Tc cumulative errors it is recommended that the wings are filled once every few ET (182,200lbs, an MLW of 152,800lbs, and)Tj /P <>BDC ET 0 Tc ET /P <>BDC -.02 Tc BT 9 0 0 9 195.9803 247.8898 Tm 9 0 0 9 411.0097 390.8898 Tm 8 0 0 8 317.9854 771.9529 Tm /P <>BDC BT -.02 Tc 7 0 0 7 387.0159 661.9528 Tm -.01 Tc ( )Tj BT /P <>BDC /P <>BDC BT 7 0 0 7 116.3631 11.5132 Tm /P <>BDC ( )Tj ET 9 0 0 9 394.0315 214.8898 Tm ( )Tj /P <>BDC /P <>BDC /P <>BDC ET EMC (A320ceo)Tj /P <>BDC ( )Tj EMC (CFM56-5B3/P)Tj (0.0131)Tj ET ET BT /P <>BDC (maintenance costs. 9 0 0 9 215.4313 379.8898 Tm EMC ET EMC Follow this link to see the "Quick Change" Aux fuel system offered by Long Range, expected 2015. (the fuel consumption for each type over)Tj EMC More Economical Dash Speed Capacity; Lower Landing . /TT2 1 Tf EMC BT BT 7 0 0 7 343.2355 463.7654 Tm -.02 Tc (the longest sector BOS-SFO. EMC ( )Tj 6 0 0 6 309.3004 673.9528 Tm ET BT ET ( )Tj EMC /P <>BDC /P <>BDC EMC EMC /P <>BDC BT (190-199)Tj /P <>BDC Do you have the estimated production material used for the 737 Next Gen? ET BT (112)Tj ( )Tj -.02 Tc EMC (170)Tj Boeing 737-800 commercial aircraft. /P <>BDC 7 0 0 7 439.7405 606.9528 Tm ET EMC EMC BT EMC (1,130)Tj ET 7 0 0 7 343.2355 496.7654 Tm (seats. ( )Tj ET EMC BT EMC ET ET ( )Tj ET 7 0 0 7 491.392 672.9528 Tm /P <>BDC ET (1,074)Tj EMC 7 0 0 7 445.619 628.7654 Tm 6.5 0 0 6.5 295.373 742.9529 Tm (popular variants of this aircraft family. /P <>BDC /P <>BDC 6.5 0 0 6.5 176.1172 558.9529 Tm ET BT EMC BT ET ( )Tj 7 0 0 7 241.5317 133.9528 Tm EMC ET ET 0 Tc /P <>BDC ( )Tj ET EMC /P <>BDC BT 56 0 0 56 419.9569 622.1944 Tm BT 7 0 0 7 387.0932 276.9528 Tm .498 .4095 .5623 .1043 v ( )Tj W n 9 0 0 9 183.8303 324.8898 Tm ET [(R)30(elativ)12.9(e fuel burn )]TJ 0 Tc EMC [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ (737-9)Tj For the wheels, I will give you two measurements. BT ET q 9 0 0 9 538.8445 588.8898 Tm BT EMC /F6 1 Tf ( )Tj ET EMC 7 0 0 7 387.0159 540.9528 Tm /GS2 gs ET ET -.005 Tc 6 0 0 6 286.5632 771.9528 Tm ET 6 0 0 6 403.5248 659.9528 Tm (178)Tj (39,270)Tj ( )Tj EMC /P <>BDC EMC (The overflight and airport charges are)Tj (A320neo)Tj ET 9 0 0 9 36.8504 434.8898 Tm ( )Tj ability of GBI to reduce fuel tank flammability. EMC BT ET /P <>BDC (be achieved. EMC ( )Tj ET endobj EMC EMC ET ET 7 0 0 7 297.632 507.9528 Tm 7 0 0 7 37.6993 375.9528 Tm EMC ET 7 0 0 7 299.0601 331.9528 Tm BT 9 0 0 9 188.8887 60.8898 Tm 7 0 0 7 82.2047 716.9528 Tm 0 Tc ( )Tj ET ET 378 0 0 303.84 -.19113 501.447 cm ( )Tj ET 7 0 0 7 70.8101 243.9528 Tm 7 0 0 7 315.5217 617.7654 Tm ( )Tj /P <>BDC /P <>BDC /P <>BDC 9 0 0 9 432.7111 49.1073 Tm BT 7 0 0 7 59.2108 11.5129 Tm EMC BT EMC BT (to in-flight service levels will increase seat)Tj 9 0 0 9 215.4409 511.8898 Tm ( A)Tj 7 0 0 7 491.4046 188.9528 Tm 7 0 0 7 355.3163 210.7654 Tm ET 9 0 0 9 215.4313 500.8898 Tm ( )Tj /P <>BDC BT BT ( )Tj 6 0 0 6 214.8509 687.9528 Tm /P <>BDC EMC (31,416lbs)Tj (136)Tj ( )Tj BT /P <>BDC /P <>BDC -.02 Tc /P <>BDC 5.25 0 0 5.25 515.3989 11.5129 Tm BT (1,683)Tj BT /P <>BDC ET /P <>BDC EMC /P <>BDC EMC ( )Tj 9 0 0 9 103.7478 390.8898 Tm (burn difference is 2.2%, and results in an)Tj BT EMC ( )Tj -.02 Tc /P <>BDC [(SS)-9.1(U)8(E)]TJ BT (207,630)Tj BT ( )Tj 7 0 0 7 492.5963 430.7654 Tm ET ( )Tj (2,900)Tj /P <>BDC (41,289)Tj EMC EMC EMC BT 9 0 0 9 382.6146 368.8898 Tm EMC EMC Note: for aircraft delivered after May 2004, centre tank ET BT BT EMC flammability exposure of the center wing tank to a level equivalent to or less /P <>BDC 7 0 0 7 445.619 122.7654 Tm -.02 Tc ET BT ( )Tj BT (aircraft variants on 14 sectors departing)Tj 6.5 0 0 6.5 176.1172 624.9529 Tm (39,270lbs)Tj EMC /P <>BDC 9 0 0 9 51.0236 159.8898 Tm 7 0 0 7 403.478 408.7654 Tm /P <>BDC the aircraft data bus. /P <>BDC S 10.479 -.009 l ET /P <>BDC /P <>BDC (comparison more challenging. EMC EMC BT .0161 Tc /P <>BDC /Artifact <>BDC (78,729)Tj EMC EMC ET 6.5 0 0 6.5 426.4819 663.9529 Tm EMC EMC EMC ET -.01 Tc 7 0 0 7 343.2355 716.7654 Tm ( )Tj BT /P <>BDC 0 Tc ET (0.0126)Tj BT EMC 9 0 0 9 368.9994 225.8898 Tm 0 Tc /P <>BDC 9 0 0 9 202.845 357.8898 Tm ( )Tj /P <>BDC -.02 Tc BT 0 Tc -.02 Tc 9 0 0 9 411.0181 269.8898 Tm EMC ET EMC ( )Tj 6 0 0 6 409.8614 771.9528 Tm EMC ( )Tj EMC /P <>BDC ET 13 0 0 13 53.8582 533.8898 Tm (generation aircraft continues to grow at a)Tj ET (PPS flight planning software is used to)Tj ET 10 0 0 10 417.91 814.1973 Tm BT /P <>BDC <>/ExtGState<>/Properties<>>> /GS2 gs EMC -.02 Tc BT EMC ET /P <>BDC /P <>BDC ET (2,220)Tj 7 0 0 7 439.2087 265.9528 Tm BT ( )Tj ( )Tj /P <>BDC EMC EMC ET In this scenario, the calculated)Tj 7 0 0 7 337.6855 221.9528 Tm ( )Tj 7 0 0 7 474.3564 716.9528 Tm /P <>BDC /P <>BDC /F6 1 Tf ET EMC BT BT /P <>BDC (the IAE V2533-A5 engine, rated at)Tj BT ET ( )Tj EMC 0 Tc 7 0 0 7 187.5417 430.9528 Tm 0 Tc 7 0 0 7 473.4744 518.9528 Tm 7 0 0 7 298.1781 111.9528 Tm 7 0 0 7 299.0601 199.9528 Tm 7 0 0 7 507.7893 331.7654 Tm BT EMC 0 Tc BT ET BT /P <>BDC /P <>BDC ( )Tj (A)Tj (\(ATC\) charges. -.02 Tc ( )Tj EMC EMC EMC ( )Tj 7 0 0 7 141.7322 309.9528 Tm ( )Tj EMC (on the same sector is almost the same as)Tj BT /P <>BDC BT ( )Tj /P <>BDC 9 0 0 9 183.0113 214.8898 Tm BT 0 Tc BT (equipped with the more fuel-efficient CFM)Tj 6.5 0 0 6.5 244.3754 565.9529 Tm /P <>BDC ( )Tj 9 0 0 9 197.3752 357.8898 Tm EMC )Tj EMC BT EMC EMC BT EMC BT ET (These are the 737-800 and 737-8, 737-)Tj EMC /P <>BDC BT /F7 1 Tf BT /P <>BDC BT EMC /P <>BDC BT (O)Tj ( )Tj 8 0 0 8 457.2753 771.9528 Tm EMC /P <>BDC /P <>BDC ET ET 0 Tc BT 7 0 0 7 491.7142 243.7654 Tm .41 .161 .508 rg /P <>BDC ET EMC (2,518)Tj ( )Tj BT /P <>BDC EMC ( )Tj ET ET [(CFM L)17.1(E)-8.1(AP-1A32)]TJ (performance deterioration factor added to)Tj 7 0 0 7 387.0159 518.9528 Tm ET Pictures, specifications, reviews. EMC [(The A321neo)43()74(s)0( lar)13.9(ge seat capacity and high)]TJ ET 7 0 0 7 37.0536 529.9528 Tm (0.0113)Tj [(looks at the performance of eight Airbus and Boeing narr)10(o)12(wbody types)]TJ ( )Tj [(M)21(T)39.1(O)7.1(W)0( - lbs)]TJ ( )Tj ET ET ET /P <>BDC EMC /P <>BDC ET 7 0 0 7 507.7893 628.7654 Tm ET (24)Tj 7 0 0 7 354.4763 672.7654 Tm EMC ( )Tj BT ET -.02 Tc 6.5 0 0 6.5 433.3069 585.9529 Tm (difference to an average of 2.1% over the)Tj BT 7 0 0 7 179.5605 518.9528 Tm ET EMC (the 737-9 is nearly 7% higher than the)Tj EMC EMC EMC 7 0 0 7 124.1242 100.7654 Tm BT BT EMC the years. EMC (342,312)Tj 7 0 0 7 440.0906 331.9528 Tm /P <>BDC /P <>BDC BT EMC (0.0108)Tj BT ET -.02 Tc BT (35,112)Tj /P <>BDC BT ( )Tj (0.0142)Tj [(CFM L)17.1(E)-8.1(AP-1A26)]TJ EMC 6 0 0 6 277.7064 715.9528 Tm BT ET BT /P <>BDC EMC EMC (152)Tj ET [(Airlines acr)10(oss the world ar)10(e r)10(eturning their eets to ser)-25.9(vice. 7 0 0 7 439.7405 628.9528 Tm /P <>BDC /P <>BDC .0161 Tc /P <>BDC 7 0 0 7 43.6039 738.9528 Tm EMC (39,270)Tj ET EMC 0 Tc -.02 Tc /P <>BDC ( )Tj BT /P <>BDC ET 9 0 0 9 555.1594 379.8898 Tm BT ( )Tj BT BT EMC BT 7 0 0 7 314.6398 529.7654 Tm EMC -.02 Tc /P <>BDC BT /P <>BDC (977)Tj /P <>BDC BT 10 0 0 10 36.8504 814.1973 Tm -.02 Tc 0 Tc EMC (152)Tj /P <>BDC ET [(OM)8(M)-13(E)-25(R)7(C)8(E)]TJ (3,300 -)Tj ET soaked fuel causing frost to form on the wings during the turnarounds - even in BT /P <>BDC ET /P <>BDC EMC 9 0 0 9 267.0826 500.8898 Tm 0 Tc That is because it is an 800. ( )Tj ET EMC EMC ( )Tj /P <>BDC -.02 Tc BT BT EMC BT BT /P <>BDC EMC ET BT EMC (2,732)Tj EMC BT ET 9 0 0 9 365.7772 467.8898 Tm ( )Tj ( )Tj (1,089)Tj /P <>BDC 7 0 0 7 294.4014 386.7654 Tm 7 0 0 7 490.8321 166.7654 Tm EMC ( )Tj ( )Tj EMC 9 0 0 9 36.8504 247.8898 Tm 9 0 0 9 354.313 236.8898 Tm /P <>BDC EMC /P <>BDC EMC -.02 Tc ET /P <>BDC ( )Tj BT q 1 0 0 1 232.438 95.878 cm 0 0 m BT ( )Tj BT EMC ET BT ET 6 0 0 6 339.7639 715.9528 Tm ( )Tj 7 0 0 7 125.6292 430.7654 Tm /GS1 gs ET 7 0 0 7 141.7322 166.9528 Tm EMC BT /P <>BDC ( )Tj ( )Tj /P <>BDC 7 0 0 7 54.5916 342.7654 Tm ET ET BT BT 6 0 0 6 444.4713 715.9528 Tm -.02 Tc ET Q 7 0 0 7 187.0858 408.9528 Tm EMC ET BT EMC 7 0 0 7 427.7291 309.9528 Tm EMC EMC )]TJ 9 0 0 9 261.8182 225.8898 Tm EMC ET ET ( )Tj ET ET BT ET BT ET ( )Tj BT (aim was remove this variability from the)Tj 7 0 0 7 130.1443 320.7654 Tm ET /P <>BDC ET /P <>BDC ET ET f (3,693)Tj /P <>BDC BT ET EMC (2,731)Tj -.02 Tc 0 Tc ( )Tj BT 7 0 0 7 520.6108 540.9528 Tm BT EMC /P <>BDC ET (410)Tj (payload resulting in an average)Tj 7 0 0 7 158.74 529.7654 Tm /P <>BDC EMC ( )Tj [(family competitors, the 737 M)-8.1(A)-24.9(X also has)]TJ 9 0 0 9 537.5864 291.8898 Tm /P <>BDC [(B)-13.9(L)74(V/53)]TJ 0 Tc ET 0 Tc ( )Tj EMC BT BT BT 0 J 0 j 5 w 10 M [] 0 d ET ET /P <>BDC EMC 7 0 0 7 82.8504 111.9528 Tm EMC ET EMC /P <>BDC 9 0 0 9 572.0386 115.8898 Tm ( )Tj EMC 7 0 0 7 279.1575 122.9528 Tm /P <>BDC EMC (0.0126)Tj EMC (average 0.06 cents per ASM advantage for)Tj (CFM56-5B3/P)Tj BT 9 0 0 9 232.438 203.8898 Tm (The A320 family is offered with the)Tj The Boeing 737 is designed to fill the smaller jet airliners space over a given range of seats. /F4 1 Tf (I)Tj ET 9 0 0 9 373.2203 368.8898 Tm EMC /P <>BDC 6.5 0 0 6.5 449.7715 565.9529 Tm (45,276)Tj 0 Tc EMC /P <>BDC (737-9)Tj ( )Tj 9 0 0 9 372.0688 324.8898 Tm 0 Tc 1 i 7 0 0 7 37.5838 551.9528 Tm 13 0 0 13 205.5668 412.8898 Tm /P <>BDC ET EMC -.02 Tc ( )Tj ET EMC 7 0 0 7 439.2087 298.9528 Tm 9 0 0 9 36.8504 258.8898 Tm /P <>BDC EMC ET /P <>BDC the test, each gauge will display any error codes that they may have. EMC