BT /P <>BDC -.02 Tc BT BT 9 0 0 9 194.061 324.8898 Tm 7 0 0 7 299.0601 342.9528 Tm 6 0 0 6 240.5796 729.9528 Tm BT BT /F4 1 Tf EMC 0 Tc BT BT BT (31,416)Tj ( )Tj 9 0 0 9 411.0097 38.8898 Tm BT EMC /P <>BDC ET (LRC speed. (travelled for the aircraft on each route is)Tj BT /P <>BDC (34,650)Tj /P <>BDC ET Main tanks > 50%, -1 to 5 deg pitch, +/- 1 deg roll: +/- 2.5% ET 0 Tc 9 0 0 9 542.7234 489.8898 Tm /P <>BDC 6 0 0 6 132.3631 659.9528 Tm BT /P <>BDC ET 7 0 0 7 54.5916 540.7654 Tm (seat capacity, with no additional cargo. 0 Tc ET ET ET (36,960)Tj (to 3.3% less efficient than the A320neo)Tj 9 0 0 9 411.0234 698.8898 Tm 6.5 0 0 6.5 243.8814 689.9529 Tm 7 0 0 7 247.7395 562.7654 Tm Federal Aviation Administration and the Boeing Company to evaluate the EMC BT ET ET ET EMC /P <>BDC EMC ET 7 0 0 7 230.7317 419.9528 Tm EMC 7 0 0 7 430.039 639.9528 Tm -.01 Tc 7 0 0 7 82.2047 727.9528 Tm (2,518)Tj EMC ET 10 0 0 10 417.91 814.1973 Tm BT BT ( )Tj EMC /P <>BDC 7 0 0 7 107.1165 661.9528 Tm EMC BT 6 0 0 6 381.7993 757.9528 Tm ET EMC BT /P <>BDC /F1 1 Tf 7 0 0 7 380.2788 485.7654 Tm BT /OC /MC1956 BDC ( )Tj EMC EMC )Tj /P <>BDC /P <>BDC EMC BT ( )Tj 9 0 0 9 215.433 236.8898 Tm ET /P <>BDC EMC 9 0 0 9 528.248 643.8898 Tm /P <>BDC -.01 Tc /P <>BDC ET BT BT )Tj .008 Tc /P <>BDC EMC 9 0 0 9 196.4663 137.8898 Tm EMC 0 Tc 6.5 0 0 6.5 448.8744 558.9529 Tm either 907 or 453kg, NG fuel gauges can give messages such as BT EMC BT 8 0 0 8 447.8735 760.9529 Tm ( )Tj EMC 7 0 0 7 518.4953 188.9528 Tm ET /P <>BDC EMC ( )Tj -.02 Tc ( )Tj EMC 9 0 0 9 53.8578 82.8898 Tm 0 Tc -.02 Tc -.01 Tc EMC 6.5 0 0 6.5 397.9138 722.9529 Tm BT (163)Tj ET ET ET 7 0 0 7 247.7395 199.7654 Tm ET 9 0 0 9 425.1913 93.8898 Tm 9 0 0 9 198.2937 126.8898 Tm ( )Tj 7 0 0 7 380.2788 496.7654 Tm BT /P <>BDC 8 0 0 8 54.8194 771.9529 Tm ( )Tj ET /P <>BDC 9 0 0 9 232.438 346.8898 Tm 0 Tc 7 0 0 7 554.7883 188.7654 Tm 0 Tc BT EMC 9 0 0 9 232.438 291.8898 Tm /P <>BDC ET 9 0 0 9 546.3505 566.8898 Tm ET ET 10 0 0 10 408.1099 814.1973 Tm /OC /MC4771 BDC /P <>BDC 7 0 0 7 316.0679 298.7654 Tm -.02 Tc ET BT (I)Tj BT BT 7 0 0 7 315.1859 100.7654 Tm .151 .147 .15 rg 7 0 0 7 337.6855 221.9528 Tm BT ET /P <>BDC EMC ET (37,653)Tj ( )Tj ET BT ET 9 0 0 9 36.8504 412.8898 Tm BT ET (Comparing the older Airbus and)Tj .023 .567 .626 RG /P <>BDC /P <>BDC ET /P <>BDC -.02 Tc /P <>BDC BT -.02 Tc -.02 Tc EMC 201.803 814.197 m /P <>BDC BT ET Because of ET ( )Tj BT 0 Tc /P <>BDC 7 0 0 7 54.7071 562.7654 Tm )Tj BT 7 0 0 7 338.6433 232.7654 Tm -.01 Tc [(SS)-9(U)8.1(E)]TJ BT 7 0 0 7 554.7883 727.7654 Tm (44,352)Tj ET 8 0 0 8 319.1147 771.9528 Tm /P <>BDC ET /P <>BDC 7 0 0 7 444.737 144.7654 Tm 0 Tc EMC 7 0 0 7 363.2711 507.9528 Tm BT ET Download the Final ET 7 0 0 7 363.2711 111.9528 Tm BT /P <>BDC /P <>BDC -.02 Tc 9 0 0 9 544.5056 302.8898 Tm 17 0 0 17 560.3929 742.1944 Tm /F7 1 Tf EMC /P <>BDC 9 0 0 9 261.8182 225.8898 Tm 9 0 0 9 215.4313 49.8898 Tm /P <>BDC ET 9 0 0 9 534.5925 753.8898 Tm ET /P <>BDC EMC 8 0 0 8 439.9149 760.9528 Tm /P <>BDC ( )Tj 9 0 0 9 382.6039 434.8898 Tm (162,701)Tj ( )Tj /P <>BDC /P <>BDC /P <>BDC ET (page\))Tj BT /P <>BDC )Tj 9 0 0 9 544.0105 258.8898 Tm ET ET 9 0 0 9 547.562 126.8898 Tm ( )Tj /P <>BDC ( )Tj EMC ( )Tj 8 0 0 8 43.6039 591.9528 Tm The CFM56-5B4/P has a)Tj EMC BT (City-pair)Tj ET ET (CFM LEAP-1B28B1s thrust rating to)Tj /P <>BDC /P <>BDC /P <>BDC /P <>BDC /P <>BDC 7 0 0 7 444.737 309.7654 Tm ( )Tj /P <>BDC /P <>BDC 7 0 0 7 247.7395 617.7654 Tm 0 Tc ( )Tj -.01 Tc ET 7 0 0 7 326.2278 716.9528 Tm (831)Tj /P <>BDC /Artifact <>BDC ET BT EMC ET BT 0 Tc 8 0 0 8 314.3535 675.9528 Tm ET 7 0 0 7 82.2047 518.9528 Tm ( )Tj EMC 36.85 824.882 572.599 17.008 re 9 0 0 9 515.4913 555.8898 Tm BT 7 0 0 7 343.2355 606.7654 Tm ET EMC /P <>BDC 7 0 0 7 204.0935 111.7654 Tm ET 7 0 0 7 294.4014 188.7654 Tm (. 7 0 0 7 258.2805 122.7654 Tm (150)Tj -.02 Tc BT Engine size EMC ET ET BT EMC BT (-61)Tj /P <>BDC -.02 Tc ET 6.5 0 0 6.5 379.1824 565.9529 Tm /P <>BDC /P <>BDC /P <>BDC BT 6.5 0 0 6.5 437.571 532.9529 Tm ( )Tj ( )Tj 0 Tc /P <>BDC ( )Tj /P <>BDC (182,299)Tj -.01 Tc ET 7 0 0 7 343.2355 518.7654 Tm Hi Peter, BT ET (The cost index used is heavily)Tj (20)Tj ET BT BT ET ET -.02 Tc EMC /GS2 gs EMC /P <>BDC /P <>BDC ET ( )Tj 9 0 0 9 215.433 38.8898 Tm EMC BT ET EMC 9 0 0 9 53.8578 148.8898 Tm BT (0.0122)Tj 7 0 0 7 316.0679 386.7654 Tm 7 0 0 7 297.632 716.9528 Tm 7 0 0 7 230.7317 397.9528 Tm 9 0 0 9 173.2978 247.8898 Tm EMC ET ET [(E)-7.8(P)16.1(T)9(E)-13.9(MBE)-16.9(R)]TJ 0 841.89 609.449 -841.89 re BT ET BT ET BT (989)Tj EMC BT [(CFM L)17.1(E)-8.1(AP-)]TJ )Tj BT /P <>BDC /P <>BDC ET 7 0 0 7 101.0963 386.9528 Tm /P <>BDC /P <>BDC BT 7 0 0 7 507.7893 67.7654 Tm 7 0 0 7 536.3849 265.7654 Tm 9 0 0 9 381.3998 126.8898 Tm /P <>BDC Main tanks < 50%, -1 to 5 deg pitch, +/- 1 deg roll: +/- 1.0% 7 0 0 7 536.3849 529.7654 Tm BT (compared to 16,200kg on classics). BT 7 0 0 7 321.6356 133.9528 Tm /P <>BDC EMC 9 0 0 9 394.0315 148.8898 Tm EMC 7 0 0 7 241.2727 166.9528 Tm 9 0 0 9 383.0289 544.8898 Tm EMC -1.2026 -5.3154 -.8984 -5.2108 -.5848 -4.9925 c 0 Tc ( )Tj ( )Tj /P <>BDC EMC BT EMC 0 Tc /P <>BDC ( )Tj 7 0 0 7 99.8582 628.7654 Tm ( )Tj ()Tj ET (369-383)Tj q 1 0 0 1 36.85 797.54 cm 0 0 m 7 0 0 7 141.7322 309.9528 Tm (A321ceo)Tj EMC ET -.02 Tc /P <>BDC EMC EMC 6.5 0 0 6.5 499.1812 689.9529 Tm ET (737-900ER\(W\). BT /P <>BDC BT ET 0 Tc EMC 9 0 0 9 53.8582 731.8898 Tm ET APU fuel pump in the No 1 tank which operates automatically during the start ET ( )Tj EMC EMC q 1 0 0 1 53.901 797.54 cm 0 0 m 7 0 0 7 537.7804 408.9528 Tm endobj (151)Tj 0 Tc BT ET ( )Tj ET EMC EMC EMC (trip-?? 0 Tc ET EMC 9 0 0 9 36.8504 269.8898 Tm ET ET ET EMC /P <>BDC -.02 Tc EMC ET /P <>BDC 7 0 0 7 196.5683 716.7654 Tm EMC -.01 Tc ( )Tj (T)Tj /P <>BDC ET (I)Tj ET ( )Tj /P <>BDC BT /P <>BDC BT ET 19.843 0 l BT /P <>BDC BT /P <>BDC (5,338)Tj ( )Tj EMC 7 0 0 7 537.7804 287.9528 Tm /P <>BDC ( )Tj BT /P <>BDC 7 0 0 7 247.7395 430.7654 Tm BT 0 Tc EMC ( )Tj ET 0 Tc BT /P <>BDC 1 g /P <>BDC BT 13 0 0 13 205.5668 412.8898 Tm (32,000lbs, down from the 33,000lbs that)Tj 9 0 0 9 191.3244 324.8898 Tm -.01 Tc /P <>BDC ( )Tj EMC ET EMC EMC /F4 1 Tf BT /P <>BDC ET ET /P <>BDC EMC EMC 7 0 0 7 187.0858 595.9528 Tm ( )Tj 6 0 0 6 520.876 743.9528 Tm f BT [(CFM L)17.1(E)-8.1(AP-1A26)]TJ 6.5 0 0 6.5 486.1525 722.9529 Tm BT /P <>BDC ( )Tj BT ET ( )Tj ET Boeing has its 737 in almost every single developed nation. 6 0 0 6 427.5796 729.9528 Tm (scenario 2, which uses an 85% passenger)Tj ET 8 0 0 8 53.9373 760.7654 Tm ET BT /P <>BDC ET f BT 6.5 0 0 6.5 331.0061 722.9529 Tm EMC BT -.02 Tc BT EMC 7 0 0 7 554.7883 144.7654 Tm EMC ET ET EMC /P <>BDC ( )Tj BT 7 0 0 7 242.1547 78.9528 Tm /P <>BDC 0 Tc /P <>BDC BT BT /P <>BDC 6.5 0 0 6.5 324.4345 676.9529 Tm BT [(7)-33(3)8.1(7-800 & 7)-33(3)8.1(7-8 )]TJ /F1 1 Tf (1,498)Tj They were solenoid held and /P <>BDC EMC ET /OC /MC171 BDC /P <>BDC 7 0 0 7 429.157 595.9528 Tm (HGW2 option with an MTOW of)Tj 0 Tc BT /P <>BDC 9 0 0 9 535.0095 423.8898 Tm 8 0 0 8 314.3535 633.9528 Tm 6.5 0 0 6.5 375.6529 676.9529 Tm BT ET (1,705)Tj 0 Tc /P <>BDC ET /P <>BDC -.02 Tc BT /P <>BDC /P <>BDC EMC EMC 7 0 0 7 82.8504 111.9528 Tm ET 7 0 0 7 355.3163 144.7654 Tm 7 0 0 7 554.7883 441.7654 Tm /P <>BDC -.01 Tc ( )Tj 9 0 0 9 570.6951 291.8898 Tm BT /P <>BDC 9 0 0 9 394.0157 544.8898 Tm EMC EMC /F6 1 Tf ET /F6 1 Tf ET ET /P <>BDC ET BT 7 0 0 7 445.619 122.7654 Tm ET ET ET EMC EMC -.02 Tc /P <>BDC BT BT 0 Tc Cheers Peter. ET y9ou may find what you are looking for by clicking here. ( )Tj EMC ET BT 6.5 0 0 6.5 426.4819 676.9529 Tm /P <>BDC BT ET ET (\(see table,)Tj ET ( )Tj ET 7 0 0 7 508.2252 11.5129 Tm /P <>BDC ET ET ( )Tj /P <>BDC /P <>BDC BT centre fuel tanks. BT ET 9 0 0 9 117.7519 170.8898 Tm (. BT ET /P <>BDC BT ( )Tj 7 0 0 7 258.2805 529.7654 Tm (159,251)Tj ET ET ( )Tj 0 Tc /P <>BDC BT EMC ( )Tj BT 0 Tc ET EMC 7 0 0 7 99.8582 78.7654 Tm 7 0 0 7 315.1859 111.7654 Tm /P <>BDC /P <>BDC ET ET EMC ET /P <>BDC (0.0119)Tj BT 8 0 0 8 366.8367 771.9528 Tm ET /P <>BDC EMC ET EMC ET 9 0 0 9 191.9099 93.8898 Tm 9 0 0 9 232.4217 115.8898 Tm /P <>BDC 9 0 0 9 215.4313 38.8898 Tm ET ET /P <>BDC EMC EMC ( )Tj ( )Tj ET -.02 Tc ET Thanks now. ( )Tj ( )Tj ( )Tj 9 0 0 9 187.5717 126.8898 Tm ET /P <>BDC 7 0 0 7 297.632 540.9528 Tm /P <>BDC 6.5 0 0 6.5 346.9224 650.9529 Tm /P <>BDC /OC /MC2278 BDC /P <>BDC EMC ET 0 Tc ( )Tj ET EMC 6 0 0 6 77.6053 771.9528 Tm BT /P <>BDC EMC BT 7 0 0 7 77.36 11.5132 Tm 0 Tc BT [(A3)24.9(21neo)]TJ BT ET 6.5 0 0 6.5 399.2659 565.9529 Tm /P <>BDC ET 7 0 0 7 179.5605 419.9528 Tm 0 Tc BT EMC -.01 Tc BT 7 0 0 7 404.101 144.7654 Tm /P <>BDC ET This study uses a)Tj BT EMC The relative high)Tj ET -.02 Tc (category. /P <>BDC ( )Tj 7 0 0 7 337.6855 540.9528 Tm ( )Tj 6.5 0 0 6.5 398.369 585.9529 Tm /P <>BDC BT 6.5 0 0 6.5 549.8557 598.9529 Tm BT EMC /P <>BDC ET 0 Tc EMC ET /P <>BDC /P <>BDC EMC ET Any)Tj could you point me in the right direction or tell me what the weight of the landing gear would be on a 737? ET ET 0 Tc ET ET (payload, due to its higher seat capacity, of)Tj (248,064)Tj (2,732)Tj 7 0 0 7 355.3163 243.7654 Tm ( )Tj /P <>BDC BT (CFM56-5B4/P)Tj (CFM56-5B4/P)Tj 0 Tc /P <>BDC -.02 Tc BT (the A321ceo, A321neo, 737-900ER\(W\))Tj EMC 9 0 0 9 553.9287 643.8898 Tm BT EMC 9 0 0 9 53.8338 104.8898 Tm BT /P <>BDC 7 0 0 7 539.8962 672.9528 Tm /P <>BDC ( )Tj (170)Tj (tracked distance, ESAD, and the difference)Tj ET BT ET BT ET ET still drawing fuel from the centre tank. 9 0 0 9 53.8582 324.8898 Tm EMC .151 .147 .15 rg EMC EMC .151 .147 .15 rg 7 0 0 7 95.225 11.5132 Tm 9 0 0 9 36.8504 423.8898 Tm 9 0 0 9 394.0157 643.8898 Tm BT /P <>BDC ET EMC /P <>BDC -.02 Tc /P <>BDC ET ( The reserve fuel policy )Tj -.02 Tc 7 0 0 7 247.7395 364.7654 Tm 0 Tc ET (maintenance. 0 Tc /P <>BDC .41 .161 .508 rg ET .534 .14 .504 RG ET BT ET BT ET (economy seats are at six-abreast. 6 0 0 6 466.3124 715.9528 Tm BT BT /P <>BDC 9 0 0 9 548.0225 368.8898 Tm ET 7 0 0 7 108.6215 441.9528 Tm /F7 1 Tf EMC BT /P <>BDC Q /P <>BDC BT ET /P <>BDC ET ( )Tj ( )Tj EMC ( )Tj ( )Tj BT 8 0 0 8 38.4744 758.9528 Tm 9 0 0 9 212.0769 71.8898 Tm BT ( )Tj ET BT ( )Tj BT 8 0 0 8 302.5117 703.9528 Tm ( )Tj EMC /P <>BDC ET 0 Tc 0 Tc EMC ET BT BT ( )Tj ET ( )Tj (273,600)Tj This from the FAA Systems ET /P <>BDC /P <>BDC BT (generated per route. ET BT 7 0 0 7 490.8321 122.7654 Tm EMC EMC (A320ceo)Tj (1,825)Tj ( )Tj but also if a pump is left running dry for over approx 10 minutes it will lose BT /P <>BDC 7 0 0 7 230.7317 694.9528 Tm -.01 Tc ET ET -.01 Tc EMC from cockpit door to the kitchen alley . ET /P <>BDC 0 Tc 7 0 0 7 182.3536 78.9528 Tm (A)Tj BT EMC ET ET /P <>BDC ( )Tj 6.5 0 0 6.5 191.942 532.9529 Tm 7 0 0 7 554.7883 100.7654 Tm EMC (900ER and 737-9, A320ceo and A320neo,)Tj 9 0 0 9 190.4723 71.8898 Tm /P <>BDC 6 0 0 6 389.0654 673.9528 Tm (182,700)Tj BT /P <>BDC (1,272)Tj /P <>BDC 9 0 0 9 36.8504 115.8898 Tm /P <>BDC /P <>BDC BT ET However engineers designing the 737 opted to lighten the structure with the engines underneath he wings and allow for the fuselage to be widened for six-abreast seating.
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