/P <>BDC (283)Tj ( )Tj BT 5.25 0 0 5.25 64.5461 11.5129 Tm ET 9 0 0 9 36.8504 181.8898 Tm /P <>BDC EMC BT 7 0 0 7 490.5101 474.9528 Tm ET ET 6.5 0 0 6.5 375.6529 689.9529 Tm BT /P <>BDC ET EMC ET ET 5 0 0 5 484.5872 11.5129 Tm BT 0 Tc /P <>BDC (Block time)Tj ( )Tj (2,601)Tj .0161 Tc wiring in tanks, proximity to hot air-conditioning or pneumatic systems, etc. /P <>BDC EMC /P <>BDC 9 0 0 9 53.8578 137.8898 Tm BT 6.5 0 0 6.5 398.2453 742.9529 Tm ET /P <>BDC 7 0 0 7 99.8582 661.7654 Tm /P <>BDC -.02 Tc BT must be switched OFF when both LP lights illuminate. 9 0 0 9 411.0181 104.8898 Tm (The alternate airports were selected based)Tj ET /GS2 gs EMC 0 Tc BT ( )Tj /P <>BDC EMC BT BT BT BT BT ( )Tj BT (the ACF cabin enhancements that offer)Tj /P <>BDC ( )Tj EMC /P <>BDC ET /P <>BDC 0 Tc BT BT 9 0 0 9 36.8504 247.8898 Tm /P <>BDC 7 0 0 7 316.0679 298.7654 Tm ( )Tj 7 0 0 7 294.4014 683.7654 Tm ( )Tj -.02 Tc EMC /F1 1 Tf ET (34,650)Tj BT ET 9 0 0 9 394.0237 170.8898 Tm EMC ( )Tj EMC /P <>BDC /P <>BDC ET EMC /P <>BDC (124,800)Tj ET ET BT 0 Tc 0 Tc BT EMC ()Tj -.02 Tc /P <>BDC EMC Fuel Capacity 6,875 U.S. gal (26,020 L) Seat Pitch: 40 inches Premier World 32 inches Economy Max. ET /P <>BDC /P <>BDC BT EMC EMC BT 0 Tc /P <>BDC EMC EMC BT /P <>BDC /P <>BDC 8 0 0 8 54.8194 771.9529 Tm ( )Tj BT ET -.02 Tc EMC ET ET EMC ( )Tj /P <>BDC EMC 9 0 0 9 394.0123 478.8898 Tm ( )Tj ( )Tj BT /P <>BDC (to 3.3% less efficient than the A320neo)Tj /P <>BDC FQIS accuracy with digital indicators: +/- 2.5 % 6.5 0 0 6.5 191.8316 637.9529 Tm (different available options, and gives the)Tj EMC /P <>BDC ( )Tj /P <>BDC BT EMC 7 0 0 7 241.5317 342.9528 Tm BT (The A320 family is offered with the)Tj ET EMC /GS2 gs ( )Tj 7 0 0 7 130.1443 221.7654 Tm ET 0 Tc /P <>BDC BT ( )Tj BT 9 0 0 9 394.0315 324.8898 Tm (than the 737-9. EMC 0 Tc ET 7 0 0 7 316.0679 441.7654 Tm 9 0 0 9 394.0315 71.8898 Tm /P <>BDC 6.5 0 0 6.5 279.814 585.9529 Tm BT BT 7 0 0 7 536.3849 595.7654 Tm 7 0 0 7 297.632 485.9528 Tm 0 Tc /P <>BDC 0 Tc BT /P <>BDC BT EMC BT EMC /P <>BDC 9 0 0 9 543.3065 555.8898 Tm BT (CFM LEAP-1B28B1 rated at 28,000lbs)Tj The relative high)Tj 9 0 0 9 352.4841 313.8898 Tm ( )Tj ET BT ET 10 0 0 10 49.3644 814.1973 Tm (The cost index used is heavily)Tj EMC ( )Tj ET /P <>BDC 6.5 0 0 6.5 549.8557 676.9529 Tm BT 9 0 0 9 215.4313 445.8898 Tm BT ( )Tj ET ( )Tj Fully . ET 9 0 0 9 199.0091 401.8898 Tm 0 Tc 6 0 0 6 477.5682 659.9528 Tm 6 0 0 6 333.9129 729.9528 Tm (A320ceo)Tj BT EMC 6 0 0 6 167.0441 757.9528 Tm /P <>BDC BT ( )Tj ( )Tj (financing. 5 0 0 5 484.5872 11.5129 Tm EMC BT ( )Tj /P <>BDC BT BT 0 Tc /P <>BDC EMC 9 0 0 9 232.438 115.8898 Tm ( )Tj BT /P <>BDC (materials. BT ( )Tj ET ET ET 6 0 0 6 434.151 715.9528 Tm EMC 7 0 0 7 277.3936 177.9528 Tm EMC ( )Tj /P <>BDC 0 Tc ET ( )Tj BT 7 0 0 7 326.2278 738.9528 Tm /P <>BDC ( )Tj 7 0 0 7 363.2711 397.9528 Tm -.02 Tc EMC ( )Tj 6.5 0 0 6.5 398.3298 637.9529 Tm BT (CFM56-5B4/P)Tj 7 0 0 7 427.7291 111.9528 Tm ( )Tj ( )Tj BT ET 10 0 0 10 539.3945 794.2914 Tm BT /P <>BDC (results in the same payload being carried in)Tj /P <>BDC EMC /P <>BDC EMC EMC BT 7 0 0 7 299.0601 276.9528 Tm ( )Tj -.02 Tc 7 0 0 7 403.478 727.7654 Tm ET ET /P <>BDC EMC ET ET -.02 Tc ET ET ET ET /P <>BDC EMC EMC ET ET EMC (CFM56-7B27B3)Tj ( )Tj EMC EMC ( )Tj .151 .147 .15 rg ( )Tj ET ( )Tj ET /P <>BDC ET BT EMC BT /P <>BDC EMC ET /P <>BDC ( )Tj BT (0.0140)Tj /P <>BDC ET ET /P <>BDC BT 9 0 0 9 423.3885 401.8898 Tm -.005 Tc BT EMC ( )Tj (manufacturers support these aircraft types)Tj 7 0 0 7 440.0906 408.9528 Tm /P <>BDC BT BT 7 0 0 7 95.225 11.5132 Tm ET ET BT /P <>BDC ET EMC ET /P <>BDC 6.5 0 0 6.5 346.7208 624.9529 Tm /P <>BDC BT /GS1 gs 9 0 0 9 394.0157 489.8898 Tm BT BT (1,729)Tj /P <>BDC EMC ET EMC (The later generation aircraft are set to)Tj EMC BT ( )Tj /P <>BDC 9 0 0 9 411.0097 82.8898 Tm EMC EMC /P <>BDC EMC -.01 Tc 9 0 0 9 142.2128 335.8898 Tm BT EMC 0 Tc ET /P <>BDC 7 0 0 7 474.3564 584.9528 Tm (10)Tj 7 0 0 7 320.7537 78.9528 Tm /P <>BDC BT EMC [(F)11(uel capacity - U)-8.1(S)0(G)]TJ /P <>BDC ( )Tj ET ( )Tj /P <>BDC BT ( )Tj /P <>BDC 9 0 0 9 190.8846 379.8898 Tm 8 0 0 8 225.1837 633.9528 Tm There seem to be a lot of answers that come up, some of which might be what youre looking for. .0161 Tc ET BT ( )Tj ( )Tj ( )Tj ( )Tj ( )Tj EMC /P <>BDC BT 6 0 0 6 206.4048 687.9528 Tm 9 0 0 9 368.2199 247.8898 Tm EMC /P <>BDC BT EMC Airbus A320 Specs What is behind one of the most popular short-haul airliners? 6 0 0 6 289.3167 757.9528 Tm BT 9 0 0 9 332.7796 225.8898 Tm /P <>BDC ( )Tj BT EMC EMC EMC EMC 9 0 0 9 394.0315 225.8898 Tm /P <>BDC /P <>BDC (464,270)Tj ( )Tj )Tj 9 0 0 9 215.4313 500.8898 Tm 9 0 0 9 229.6141 49.8898 Tm 9 0 0 9 232.4217 434.8898 Tm /GS1 gs /F1 1 Tf BT EMC /P <>BDC 6.5 0 0 6.5 233.8677 611.9529 Tm The cabin layout used for)Tj EMC BT (The A320 and the 737 families will)Tj EMC (2,732)Tj /P <>BDC (418)Tj EMC BT 9 0 0 9 565.1177 280.8898 Tm ET BT /P <>BDC /P <>BDC ET EMC ET EMC /P <>BDC ET ( )Tj -.02 Tc BT 7 0 0 7 247.7395 386.7654 Tm (831)Tj 7 0 0 7 158.74 463.7654 Tm /P <>BDC BT Whilst bigger than the Embraer E-Jets, Boeing feels this is an optimum size range for a small city jet which can also be used for medium-haul international services. ET ET BT 7 0 0 7 158.74 342.7654 Tm EMC [(E)-7.8(P)16.1(T)9(E)-13.9(MBE)-16.9(R)]TJ ET -.02 Tc 8 0 0 8 334.994 717.9528 Tm EMC /P <>BDC (planned for each aircraft type. /P <>BDC ET /P <>BDC BT ET BT Note that the first 1,000 pounds of fuel are loaded into the center tank, then the wing tanks are . ET EMC /P <>BDC BT /P <>BDC BT (which is BOS-LAX, whereas the 737-800)Tj EMC BT 7 0 0 7 247.7395 199.7654 Tm /P <>BDC ET EMC (403)Tj EMC (737-800W)Tj 8 0 0 8 136.5171 758.9528 Tm /F1 1 Tf (288)Tj EMC EMC BT ( )Tj ET EMC 6 0 0 6 226.9834 715.9528 Tm /P <>BDC /P <>BDC (483)Tj ET ET EMC 0 Tc 7 0 0 7 490.8321 309.7654 Tm 7 0 0 7 473.8245 221.9528 Tm 9 0 0 9 394.0123 533.8898 Tm ( )Tj BT ET /P <>BDC .0081 Tc BT BT EMC EMC (-55)Tj /P <>BDC EMC ( )Tj 9 0 0 9 246.6113 247.8898 Tm 9 0 0 9 197.3123 379.8898 Tm /P <>BDC BT ET BT (0.0108)Tj (CFM56-7B27B3)Tj EMC /P <>BDC /P <>BDC ( )Tj 6.5 0 0 6.5 397.9138 722.9529 Tm ET EMC EMC 0 Tc BT 9 0 0 9 185.3513 159.8898 Tm (0.0134)Tj EMC /P <>BDC 9 0 0 9 501.24 731.8898 Tm -.01 Tc BT ( )Tj ET 9 0 0 9 541.0405 621.8898 Tm I am looking for a wheelbase in one main shin and the pressure in the wheel ( Boeing 737-500). /P <>BDC -.02 Tc EMC (\(see table,)Tj BT 6.5 0 0 6.5 528.5291 676.9529 Tm -.02 Tc /P <>BDC ( )Tj ( A)Tj /P <>BDC -.02 Tc EMC EMC ET EMC 7 0 0 7 536.3849 628.7654 Tm /P <>BDC EMC EMC 6 0 0 6 164.6501 715.9528 Tm /P <>BDC EMC BT Q 6 0 0 6 389.0654 673.9528 Tm ET [(Aircr)10(aft type)]TJ 9 0 0 9 53.8338 170.8898 Tm ( )Tj (39,270)Tj EMC (CFM56-)Tj ET 0 841.89 609.449 -841.89 re EMC /P <>BDC BT ET /P <>BDC /P <>BDC /P <>BDC BT EMC 7 0 0 7 314.6398 507.7654 Tm /P <>BDC 0 Tc /P <>BDC ET /P <>BDC ( )Tj ( )Tj ( )Tj /P <>BDC EMC EMC ET /P <>BDC EMC /P <>BDC BT EMC ET 0 Tc EMC EMC (34,650)Tj EMC /P <>BDC /P <>BDC BT EMC /P <>BDC EMC BT EMC BT q 1 0 0 1 394.024 91.644 cm 0 0 m EMC /P <>BDC BT ET /P <>BDC BT 9 0 0 9 355.7787 379.8898 Tm -.02 Tc EMC (34,650)Tj BT ( )Tj /P <>BDC ET BT 7 0 0 7 230.7317 419.9528 Tm 6.5 0 0 6.5 480.4 637.9529 Tm 9 0 0 9 375.8752 258.8898 Tm BT -.01 Tc /P <>BDC EMC ET ET BT EMC /P <>BDC /P <>BDC EMC 7 0 0 7 294.4014 177.7654 Tm BT EMC ( )Tj ET ET (1,824)Tj /P <>BDC 7 0 0 7 520.6108 507.9528 Tm 9 0 0 9 207.5339 280.8898 Tm EMC BT ET ET 6 0 0 6 289.3167 715.9528 Tm BT ET /P <>BDC ET ( )Tj 737 Updates. BT BT /P <>BDC ET BT 7 0 0 7 554.7883 562.7654 Tm BT 7 0 0 7 107.1165 177.9528 Tm BT BT EMC EMC ( )Tj ET EMC ET 0 Tc 7 0 0 7 321.6356 287.9528 Tm BT EMC -.02 Tc 8 0 0 8 38.4438 605.9528 Tm 7 0 0 7 294.4014 463.7654 Tm 9 0 0 9 532.5876 137.8898 Tm ( )Tj /P <>BDC 7 0 0 7 338.3085 199.9528 Tm BT 0 Tc 8 0 0 8 334.994 703.9528 Tm BT ET EMC EMC 7 0 0 7 241.5317 100.9528 Tm 0 Tc /P <>BDC /P <>BDC ( )Tj (7,379)Tj /P <>BDC /P <>BDC ET (City-pair)Tj 0 Tc ( )Tj 7 0 0 7 54.7071 309.7654 Tm (4,514)Tj Their version of the Boeing 737-800 is the Airbus A220. ET 9 0 0 9 195.0251 434.8898 Tm (operating the 737 has increased its)Tj ET EMC BT 9 0 0 9 299.3893 478.8898 Tm 10 0 0 10 50.1204 814.1973 Tm ET /P <>BDC (39,732)Tj (737-9)Tj /P <>BDC 9 0 0 9 394.0123 214.8898 Tm /P <>BDC ET ET /P <>BDC /P <>BDC EMC ( )Tj 7 0 0 7 520.6108 705.9528 Tm (The 737-800 is the most popular)Tj ET ( )Tj /P <>BDC ET BT ( )Tj BT EMC BT ET /P <>BDC ( )Tj EMC f /P <>BDC /P <>BDC EMC BT /P <>BDC EMC -.02 Tc /P <>BDC BT 8 0 0 8 187.3427 745.9528 Tm ( )Tj BT BT ( )Tj BT BT BT [(M)21(T)39.1(O)7.1(W)0( - lbs)]TJ BT ET ET ( )Tj /P <>BDC 0 Tc EMC ET EMC 9 0 0 9 394.0315 357.8898 Tm (170)Tj ET BT ET 9 0 0 9 548.3564 225.8898 Tm BT ET /P <>BDC 262 0 obj ( )Tj 9 0 0 9 53.8582 214.8898 Tm /P <>BDC -.02 Tc /P <>BDC 7 0 0 7 37.0536 496.9528 Tm 9 0 0 9 232.4217 115.8898 Tm [(A3)24.9(21neo v)12.9(ersus 7)-33(3)8.1(7-9 )]TJ BT ET 6.5 0 0 6.5 64.6596 663.9529 Tm EMC ET (the results show that the lighter payload on)Tj ET BT EMC BT EMC There was no additional)Tj ET ET /P <>BDC EMC 7 0 0 7 316.0679 133.7654 Tm ( )Tj ( )Tj EMC ET BT 9 0 0 9 53.8582 313.8898 Tm ET BT ET 7 0 0 7 204.0935 287.7654 Tm /P <>BDC BT 7 0 0 7 247.7395 331.7654 Tm /P <>BDC BT BT [(7)-33(3)8(7-8)]TJ EMC 9 0 0 9 362.4471 82.8898 Tm /P <>BDC EMC 7 0 0 7 314.6398 683.7654 Tm q /P <>BDC 304.725 420.96 m ET (1,144)Tj BT EMC BT /P <>BDC ET BT /P <>BDC 6 0 0 6 184.9964 715.9528 Tm 9 0 0 9 36.8504 71.8898 Tm -.02 Tc 7 0 0 7 321.6356 188.9528 Tm 7 0 0 7 404.101 100.7654 Tm 7 0 0 7 299.0601 287.9528 Tm /P <>BDC ET 7 0 0 7 279.1575 320.9528 Tm 7 0 0 7 37.6993 276.9528 Tm BT (34,650)Tj (190,800)Tj 6 0 0 6 561.1918 715.9528 Tm (2,732)Tj EMC BT EMC BT ET 7 0 0 7 141.7322 694.9528 Tm 0 Tc 7 0 0 7 247.7395 298.7654 Tm BT /P <>BDC ET 0 Tc BT 9 0 0 9 215.4409 379.8898 Tm EMC /OC /MC854 BDC BT 9 0 0 9 367.2442 379.8898 Tm BT 0 Tc EMC BT BT 0 Tc /F4 1 Tf BT ( )Tj ET 6 0 0 6 472.7745 771.9528 Tm BT 7 0 0 7 60.6117 254.7654 Tm EMC BT (72% of the NG fleet in service. There are many variants of the 737. 9 0 0 9 215.4313 346.8898 Tm /P <>BDC (294)Tj BT EMC /P <>BDC EMC ET 0 Tc ( )Tj 9 0 0 9 394.0237 500.8898 Tm 0 Tc 0 Tc (31,416)Tj EMC BT (The three main operational costs for)Tj EMC BT EMC BT ( )Tj EMC ET -.01 Tc EMC ET /P <>BDC BT BT /P <>BDC /P <>BDC ET EMC ET ET ET 6.5 0 0 6.5 192.4489 545.9529 Tm BT BT This makes it more challenging to)Tj 9 0 0 9 215.433 445.8898 Tm ( )Tj 7 0 0 7 473.8245 298.9528 Tm BT ( )Tj 9 0 0 9 51.0236 258.8898 Tm 7 0 0 7 43.6039 254.9528 Tm (fan diameter of 81 inches, and a bypass)Tj 7 0 0 7 539.9176 11.5129 Tm ET /P <>BDC /P <>BDC 9 0 0 9 215.433 346.8898 Tm EMC 7 0 0 7 54.7071 111.7654 Tm EMC 9 0 0 9 36.8504 203.8898 Tm EMC 7 0 0 7 343.2355 661.7654 Tm ( )Tj /P <>BDC 5.25 0 0 5.25 123.5367 11.5132 Tm (0.0123)Tj ET /P <>BDC EMC 0 841.89 609.449 -841.89 re 13 0 0 13 319.14 445.8898 Tm (3,300 -)Tj 7 0 0 7 326.2278 463.9528 Tm ET ( )Tj (136)Tj EMC ET ET EMC EMC 6 0 0 6 403.0689 729.9528 Tm /P <>BDC BT /P <>BDC 9 0 0 9 232.438 148.8898 Tm /P <>BDC ET BT ( )Tj 9 0 0 9 232.4217 324.8898 Tm ET EMC EMC [(BOS-SE)-13.9(A)]TJ 0 Tc ET will be centre fuel tank inerting. BT 9 0 0 9 197.9514 148.8898 Tm /P <>BDC 9 0 0 9 369.2608 38.8898 Tm 6.5 0 0 6.5 223.0711 742.9529 Tm ET /P <>BDC ( )Tj -.02 Tc /P <>BDC EMC (2,517)Tj /P <>BDC /P <>BDC 0 Tc /P <>BDC ET 9 0 0 9 373.2203 368.8898 Tm /P <>BDC BT BT BT 13 0 0 13 532.9001 786.8898 Tm EMC 7 0 0 7 187.0858 331.9528 Tm ET BT BT (136)Tj 7 0 0 7 387.0159 727.9528 Tm EMC /P <>BDC 7 0 0 7 508.4124 243.7654 Tm 0 Tc BT 6 0 0 6 246.1841 687.9528 Tm ( )Tj (is 0.01 to 0.15 cents better than the)Tj 7 0 0 7 297.632 518.9528 Tm ET /P <>BDC EMC /P <>BDC EMC BT BT BT BT ET /P <>BDC These sectors)Tj ET NEA is produced in sufficient quantities, during most conditions, to ET 7 0 0 7 457.0984 133.7654 Tm ET 9 0 0 9 252.5189 181.8898 Tm ( )Tj ET ( )Tj EMC EMC ( )Tj Cheers Peter. EMC 9 0 0 9 372.4479 368.8898 Tm 6 0 0 6 215.3128 743.9528 Tm -.01 Tc 9 0 0 9 165.1533 258.8898 Tm 0 Tc BT BT (9,451)Tj -.02 Tc ( )Tj ET ET 0 Tc ( )Tj 0 Tc BT /P <>BDC ( )Tj EMC ( )Tj ET BT (reduces to an average 0.04 cents in favour)Tj (136)Tj EMC /P <>BDC /P <>BDC ET ET EMC ET 7 0 0 7 37.0536 716.9528 Tm [(SS)-9.1(U)8(E)]TJ 7 0 0 7 279.1575 221.9528 Tm BT -.02 Tc /P <>BDC /P <>BDC ET BT [(On a gr)10(oup of r)10(outes betw)6.1(een 484nm and)]TJ ET /P <>BDC (213)Tj 7 0 0 7 543.7693 11.5132 Tm 8 0 0 8 302.5117 591.9528 Tm BT ET 9 0 0 9 36.8504 148.8898 Tm /P <>BDC (379)Tj /P <>BDC (13 seats fewer than the A321neo. ( )Tj /P <>BDC BT ET ET /P <>BDC BT ET 6.5 0 0 6.5 244.4599 702.9529 Tm ( )Tj EMC /P <>BDC EMC 7 0 0 7 459.6601 11.5129 Tm EMC BT /P <>BDC 1.6741 -3.9062 l ( )Tj -.01 Tc /P <>BDC EMC 7 0 0 7 54.7071 606.7654 Tm BT BT EMC EMC BT /P <>BDC /P <>BDC /P <>BDC BT ( )Tj ET /P <>BDC /P <>BDC (32,000lbs, down from the 33,000lbs that)Tj -.01 Tc 9 0 0 9 51.0315 324.8898 Tm (Max payload - lbs)Tj -.02 Tc (CFM56-5B4/P)Tj /P <>BDC )Tj EMC ( )Tj ET EMC ET ET ( )Tj /P <>BDC ET ET EMC 8 0 0 8 163.4218 771.9529 Tm -.02 Tc BT ET 9 0 0 9 350.8533 104.8898 Tm EMC (if it is financed differently. EMC EMC EMC EMC BT ( )Tj h -.02 Tc ( )Tj EMC ET /P <>BDC /P <>BDC ( )Tj (277,248)Tj ( )Tj 7 0 0 7 210.1137 463.7654 Tm 9 0 0 9 187.8443 346.8898 Tm EMC ET BT (family of aircraft, despite increases in)Tj EMC /P <>BDC BT EMC (capacity on the later aircraft models and)Tj EMC EMC EMC ( )Tj ( )Tj )Tj EMC BT 0 Tc /P <>BDC 9 0 0 9 548.0225 368.8898 Tm ( )Tj (analysis is for the A320neo on BOS-SFO,)Tj EMC /P <>BDC EMC /P <>BDC BT ET BT (112)Tj ( )Tj 9 0 0 9 36.8504 412.8898 Tm 7 0 0 7 518.4953 298.9528 Tm EMC BT (31,416)Tj ET 0 Tc /P <>BDC /P <>BDC /P <>BDC -.02 Tc 7 0 0 7 108.6215 727.9528 Tm 7 0 0 7 158.74 683.7654 Tm -.02 Tc BT BT /P <>BDC ET BT ( )Tj With the tapering of the aircraft nose, it is hard to give any one clear answer. -.02 Tc EMC /P <>BDC /P <>BDC 6.5 0 0 6.5 54.877 722.9529 Tm -.02 Tc BT ET EMC ( )Tj /P <>BDC ET 7 0 0 7 508.4124 89.7654 Tm ( )Tj /P <>BDC BT (39,270)Tj 7 0 0 7 158.74 639.7654 Tm ( )Tj BT 7 0 0 7 327.1097 639.9528 Tm ET EMC 9 0 0 9 525.9757 60.8898 Tm This is why only the NG's are affected by AD ( )Tj BT (A321ceo, in contrast to the A320neo over)Tj 8 0 0 8 332.978 577.9528 Tm BT /P <>BDC /P <>BDC BT 9 0 0 9 354.463 49.8898 Tm 5.25 0 0 5.25 55.7484 11.5132 Tm 737-800 & 737-8 The 737NG family has a single engine offering: the 737NG with the CFM56-7B; and the 737 MAX family with the CFM LEAP-1B. 7 0 0 7 99.8582 639.7654 Tm BT /P <>BDC /P <>BDC BT EMC /P <>BDC EMC EMC EMC EMC ET 7 0 0 7 363.2711 67.9528 Tm /P <>BDC ET BT (A320ceo)Tj ( )Tj (47,000)Tj BT EMC ( )Tj BT ET EMC 9 0 0 9 51.0236 335.8898 Tm ET 0 Tc EMC [(M)-13.9(KE/84)]TJ BT ( )Tj /P <>BDC ET /F7 1 Tf 7 0 0 7 199.5784 298.7654 Tm 7 0 0 7 469.2222 11.5129 Tm EMC BT BT EMC BT BT 7 0 0 7 554.7883 507.7654 Tm ET In contrast, Boeing has)Tj /P <>BDC 7 0 0 7 457.0984 331.7654 Tm EMC 7 0 0 7 258.2805 595.7654 Tm ET EMC EMC EMC [(CFM L)17.1(E)-8.1(AP-1A26)]TJ EMC EMC /P <>BDC 7 0 0 7 82.2047 474.9528 Tm 7 0 0 7 474.5665 430.9528 Tm ET -.02 Tc ET ( )Tj /P <>BDC EMC ET 7 0 0 7 54.7071 67.7654 Tm ET /P <>BDC ET /P <>BDC /P <>BDC ( )Tj /P <>BDC ( )Tj ET 7 0 0 7 554.7883 364.7654 Tm (. 7 0 0 7 427.7291 331.9528 Tm BT BT 0 Tc 7 0 0 7 148.0554 11.5132 Tm BT ET ET BT BT ET ET ( )Tj (0.0109)Tj 9 0 0 9 361.7 456.8898 Tm /P <>BDC ET 7 0 0 7 37.0536 705.9528 Tm BT ET EMC 7 0 0 7 456.2165 100.7654 Tm 9 0 0 9 408.1889 467.8898 Tm [(CFM L)17.1(E)-8.1(AP-1B27)]TJ (150-158)Tj ET ( 2021)Tj aircraft EMC BT BT ET ET 7 0 0 7 299.0601 100.9528 Tm ET 0 Tc EMC ET ET /P <>BDC 9 0 0 9 536.6833 500.8898 Tm EMC 9 0 0 9 53.8338 236.8898 Tm ET BT /P <>BDC -.02 Tc EMC EMC 9 0 0 9 187.5717 126.8898 Tm /P <>BDC /P <>BDC EMC ET 7 0 0 7 520.6108 628.9528 Tm BT 9 0 0 9 394.0157 434.8898 Tm EMC EMC BT EMC ET BT BT ET 7 0 0 7 537.267 430.7654 Tm /P <>BDC 9 0 0 9 215.4409 379.8898 Tm /P <>BDC 7 0 0 7 241.5317 221.9528 Tm 304.725 420.96 m (0.0177)Tj EMC You were right, there were some discrepancies around the range. (planned 170 passengers as follows: 145 on)Tj 6 0 0 6 540.5396 715.9528 Tm )Tj /P <>BDC /GS2 gs (737-8)Tj BT ET -.02 Tc endobj ET 7 0 0 7 54.7071 188.7654 Tm accelerations. /F1 1 Tf [(Aircr)10(aft type)]TJ BT /P <>BDC BT EMC EMC 9 0 0 9 36.8504 258.8898 Tm EMC 6.5 0 0 6.5 221.9596 650.9529 Tm 0 Tc /P <>BDC /P <>BDC ( )Tj EMC EMC (A321ceo)Tj EMC (The first-class layout uses four-abreast)Tj BT ET 0 Tc EMC EMC ET /F1 1 Tf (832)Tj /P <>BDC EMC ET /P <>BDC ( )Tj ET BT /P <>BDC ET /P <>BDC EMC /F6 1 Tf EMC 9 0 0 9 515.4913 555.8898 Tm BT /P <>BDC EMC 6 0 0 6 214.7428 673.9528 Tm /P <>BDC 7 0 0 7 444.737 89.7654 Tm (weather, traffic and ATC constraints, all of)Tj BT ET BT /P <>BDC (capacity would further increase the)Tj /P <>BDC 7 0 0 7 53.8582 11.5132 Tm BT 9 0 0 9 194.4504 203.8898 Tm /P <>BDC ET /P <>BDC 7 0 0 7 316.0679 364.7654 Tm /P <>BDC 7 0 0 7 337.7614 144.7654 Tm BT 1 g ( )Tj ET 7 0 0 7 321.6356 89.9528 Tm /P <>BDC /P <>BDC /P <>BDC 0 Tc (additional benefit in this comparison. /GS1 gs ET /P <>BDC /P <>BDC BT /P <>BDC /OC /MC3451 BDC ET ( )Tj /P <>BDC -.02 Tc EMC EMC ET ET EMC BT 56 0 obj 9 0 0 9 68.3339 555.8898 Tm (hugely successful. ( )Tj BT /P <>BDC ET /P <>BDC BT /P <>BDC 7 0 0 7 338.3085 298.9528 Tm Boeing 737 Max, a new generation of this highly successful City Jet. BT ET /P <>BDC 0 Tc Are there any useful sources where I might find the exact materials used in other aircraft? ( )Tj -.02 Tc BT -.02 Tc /P <>BDC 7 0 0 7 114.6416 595.9528 Tm ET EMC )Tj 53.85 621.704 518.723 183.336 re 9 0 0 9 54.9417 794.1039 Tm EMC BT /P <>BDC 6 0 0 6 153.9401 659.9528 Tm /P <>BDC EMC BT /P <>BDC (comparison more challenging. /P <>BDC /P <>BDC [(BOS-SE)-13.9(A)]TJ EMC EMC ET ET -.02 Tc /P <>BDC /P <>BDC BT -.02 Tc 9 0 0 9 552.4684 71.8898 Tm /P <>BDC )Tj 7 0 0 7 294.4014 67.7654 Tm 7 0 0 7 70.8101 144.9528 Tm (150)Tj EMC EMC ( )Tj ET EMC BT 7 0 0 7 158.74 672.7654 Tm ( )Tj BT [(737-900E)-33(R)]TJ 7 0 0 7 490.5101 716.9528 Tm (payload resulting in an average)Tj 7 0 0 7 337.6855 507.9528 Tm ET /P <>BDC ( )Tj [(Aircr)10(aft )]TJ 7 0 0 7 444.737 78.7654 Tm 7 0 0 7 439.9995 661.9528 Tm /P <>BDC /P <>BDC /P <>BDC 9 0 0 9 373.1937 357.8898 Tm /P <>BDC BT EMC 7 0 0 7 490.5101 518.9528 Tm /P <>BDC BT BT ET ET
!! (2,517)Tj ET /P <>BDC 9 0 0 9 187.813 126.8898 Tm ET BT BT BT EMC 7 0 0 7 459.6601 11.5129 Tm EMC (earlier counterpart. /P <>BDC 7 0 0 7 520.6108 617.9528 Tm /P <>BDC [(E)-7.8(P)16.1(T)9(E)-13.9(MBE)-16.9(R)]TJ /P <>BDC /P <>BDC EMC EMC EMC ( )Tj 7 0 0 7 535.5029 188.7654 Tm 0 Tc BT 7 0 0 7 520.6108 716.9528 Tm BT For more detailed information on the Boeing 737 Specs, you can click on this Boeing 737 PDF. 9 0 0 9 408.2047 489.8898 Tm 36.85 824.882 572.599 17.008 re
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