(2,732)Tj EMC 9 0 0 9 53.8582 753.8898 Tm ET ( )Tj /P <>BDC /P <>BDC 7 0 0 7 386.4701 397.9528 Tm BT BT 7 0 0 7 294.4014 496.7654 Tm BT ET /F4 1 Tf BT /P <>BDC -.01 Tc BT BT /P <>BDC ET ET BT EMC ( )Tj /P <>BDC /P <>BDC 7 0 0 7 539.8962 485.9528 Tm /P <>BDC (150 passengers on the A320ceo, A320neo,)Tj ET EMC EMC /P <>BDC (34,650)Tj ET /P <>BDC /P <>BDC -.02 Tc (The A321neo has a lower fuel burn)Tj /P <>BDC 9 0 0 9 521.6329 137.8898 Tm Pisquali 19/05/2018 at 16:07 Reply. BT ET 7 0 0 7 258.2805 243.7654 Tm EMC ET /P <>BDC /P <>BDC ET /P <>BDC EMC ET /P <>BDC EMC ET -.01 Tc .023 .567 .626 rg 0 Tc ET ET EMC 7 0 0 7 429.157 595.9528 Tm ET ET EMC 10 0 0 10 408.34 814.1973 Tm /P <>BDC EMC /F4 1 Tf 7 0 0 7 278.2756 672.9528 Tm -.02 Tc /P <>BDC 9 0 0 9 36.8504 467.8898 Tm BT 7 0 0 7 508.4124 496.7654 Tm What was the Super Sonic Transport (SST) Concorde plane?? BT 19.85 0 l ( )Tj BT 0 Tc /P <>BDC (thereby giving it a seat capacity of 160)Tj ET /P <>BDC EMC EMC /F4 1 Tf BT ET 7 0 0 7 250.5326 100.7654 Tm (A320ceo)Tj ET /P <>BDC BT ( )Tj /P <>BDC BT ET EMC ( )Tj 6.5 0 0 6.5 324.4345 689.9529 Tm (A)Tj EMC 6 0 0 6 495.9995 659.9528 Tm (150)Tj ET 9 0 0 9 563.4796 324.8898 Tm EMC EMC ET ET ET ET ET (difference. 6.5 0 0 6.5 332.6961 735.9529 Tm ( )Tj /P <>BDC 9 0 0 9 53.8338 225.8898 Tm 7 0 0 7 294.4014 628.7654 Tm /F6 1 Tf ( )Tj ET 9 0 0 9 215.433 181.8898 Tm ET ET EMC EMC (150)Tj /P <>BDC ( )Tj EMC BT ( )Tj ( )Tj ET BT BT (2,347)Tj ( )Tj 7 0 0 7 294.4014 639.7654 Tm ET ( )Tj [(E)-7.8(P)16.1(T)9(E)-13.9(MBE)-16.9(R)]TJ q )Tj 7 0 0 7 230.7317 199.9528 Tm EMC /P <>BDC 9 0 0 9 411.0097 269.8898 Tm /P <>BDC EMC EMC -.02 Tc /P <>BDC EMC 9 0 0 9 212.5589 148.8898 Tm 5.25 0 0 5.25 465.7151 11.5129 Tm BT /P <>BDC BT ( )Tj ET (can carry the 150-passenger payload. ET /P <>BDC (141,757)Tj (31,416)Tj BT -.02 Tc BT (class cabin configuration used in this study)Tj BT ET (2,498)Tj EMC BT 7 0 0 7 539.8962 738.9528 Tm ET /P <>BDC ET ( )Tj 7 0 0 7 403.478 584.7654 Tm 0 Tc EMC EMC Heres the list of Boeing Customer Codes: https://en.m.wikipedia.org/wiki/List_of_Boeing_customer_codes. ET ( )Tj ( )Tj ET BT ET ( )Tj (CFM56-5B3/P)Tj BT EMC ET EMC /P <>BDC BT EMC BT /P <>BDC 9 0 0 9 36.8504 346.8898 Tm /P <>BDC 9 0 0 9 393.4057 379.8898 Tm ( )Tj BT EMC BT EMC /P <>BDC [(737-900E)-33(R)]TJ 0 Tc /P <>BDC BT ( )Tj ET BT 9 0 0 9 183.0922 148.8898 Tm (483)Tj EMC BT ( )Tj 9 0 0 9 68.0071 357.8898 Tm 9 0 0 9 166.7302 126.8898 Tm EMC EMC ( )Tj (108 on BOS-SEA \(Seattle\); 123 on BOS-)Tj BT ET EMC /P <>BDC ( )Tj BT /P <>BDC BT EMC EMC BT /P <>BDC /P <>BDC q ET ET 6 0 0 6 481.8528 701.9528 Tm How an instrument landing system(ILS) can autoland aircraft. ET ET (CFM56-5B3/P)Tj 9 0 0 9 389.8867 269.8898 Tm /P <>BDC EMC ET /P <>BDC EMC ET EMC /P <>BDC ( )Tj /P <>BDC EMC BT /GS1 gs (of being configured like those of the)Tj ET ET ( )Tj /P <>BDC -.02 Tc /P <>BDC In which manual could you find the cross-sectional dimensions of the wing spars and stabilizer (737-300) BT ET /P <>BDC ET EMC (The comparison of the two aircraft)Tj EMC /P <>BDC ET 7 0 0 7 362.3891 331.9528 Tm ET ET BT 0 Tc ( )Tj /F7 1 Tf /P <>BDC 7 0 0 7 429.157 529.9528 Tm BT ET -.02 Tc ET BT BT BT ( )Tj EMC 7 0 0 7 337.6855 386.9528 Tm /P <>BDC EMC -.02 Tc 7 0 0 7 535.5029 705.7654 Tm ET -.02 Tc 7 0 0 7 554.7883 529.7654 Tm -.02 Tc (27,000lbs of thrust compared to the)Tj -.02 Tc /P <>BDC 9 0 0 9 126.1392 522.8898 Tm 7 0 0 7 387.0159 507.9528 Tm 7 0 0 7 490.8321 474.7654 Tm ET /P <>BDC EMC BT EMC -.02 Tc 9 0 0 9 215.433 225.8898 Tm ( )Tj 7 0 0 7 491.7142 188.7654 Tm /P <>BDC /P <>BDC 8 0 0 8 124.845 661.9528 Tm /P <>BDC ET EMC BT /P <>BDC 8 0 0 8 141.7322 760.9528 Tm 7 0 0 7 490.8321 419.7654 Tm /P <>BDC EMC EMC ET 9 0 0 9 215.4313 170.8898 Tm -.02 Tc (. ET 9 0 0 9 361.7 456.8898 Tm BT /P <>BDC 9 0 0 9 197.7229 522.8898 Tm EMC ( )Tj ( )Tj /P <>BDC ET 9 0 0 9 354.463 49.8898 Tm -.02 Tc ET BT EMC ET 9 0 0 9 394.0237 357.8898 Tm EMC /P <>BDC 7 0 0 7 383.0719 727.7654 Tm 5.25 0 0 5.25 55.7484 11.5132 Tm ( )Tj BT /P <>BDC BT 6 0 0 6 115.1719 701.9528 Tm BT how can i know the material of 737NGs nose landing gear lower drag strut?thank you. 0 Tc BT /P <>BDC 9 0 0 9 189.1853 302.8898 Tm /P <>BDC 7 0 0 7 364.1531 133.9528 Tm ET [(737-900E)-33(R)]TJ BT ET ET 7 0 0 7 554.7883 606.7654 Tm BT 9 0 0 9 192.1006 456.8898 Tm 6 0 0 6 268.0069 673.9528 Tm -.02 Tc EMC BT ET BT These incidents, and 15 more on other types since 1959, ET BT 10 0 0 10 37.304 794.2914 Tm 7 0 0 7 520.6108 584.9528 Tm 9 0 0 9 547.9955 401.8898 Tm 7 0 0 7 199.5784 199.7654 Tm ( )Tj BT ET ET ( )Tj ( )Tj I am looking for some spec information in more detail for a project 7 0 0 7 386.3929 628.9528 Tm -.02 Tc ET /P <>BDC BT -.02 Tc 7 0 0 7 199.5784 639.7654 Tm EMC ET /P <>BDC 7 0 0 7 457.0984 485.7654 Tm ET /P <>BDC 9 0 0 9 36.8504 357.8898 Tm EMC BT EMC (404)Tj BT 6 0 0 6 214.8509 687.9528 Tm (464,440)Tj /P <>BDC 7 0 0 7 363.2711 276.9528 Tm EMC 9 0 0 9 541.1655 478.8898 Tm EMC (170)Tj 7 0 0 7 314.6398 518.7654 Tm -.02 Tc 0 Tc /GS1 gs /P <>BDC ET ( )Tj 7 0 0 7 37.5838 254.9528 Tm EMC BT ET /P <>BDC ET EMC /P <>BDC BT 7 0 0 7 539.8962 463.9528 Tm (2,207)Tj BT ET ET ET ET BT ( )Tj /P <>BDC (108)Tj ( )Tj ET 7 0 0 7 554.7883 496.7654 Tm ( )Tj ( )Tj BT /P <>BDC EMC (576)Tj /P <>BDC 7 0 0 7 387.0932 298.9528 Tm EMC 6.5 0 0 6.5 232.6392 735.9529 Tm BT 6.5 0 0 6.5 284.897 532.9529 Tm (In this comparison the passenger seat)Tj /P <>BDC /P <>BDC 9 0 0 9 53.8338 115.8898 Tm /P <>BDC /P <>BDC /P <>BDC 7 0 0 7 314.6398 716.7654 Tm (BOS-PHX)Tj BT BT ( )Tj EMC /P <>BDC 9 0 0 9 215.4313 357.8898 Tm (than the A321ceo. (170-178)Tj (209)Tj ( )Tj EMC EMC 5.25 0 0 5.25 123.5367 11.5132 Tm 7 0 0 7 507.7893 584.7654 Tm (. -.02 Tc (maximum landing weight \(MLW\) of)Tj .151 .147 .15 rg )Tj EMC EMC /P <>BDC ET 7 0 0 7 258.2805 408.7654 Tm EMC (282)Tj ET EMC -.02 Tc EMC ET BT EMC (35,112)Tj EMC (2,349nm because of strong headwind. 7 0 0 7 294.4014 419.7654 Tm More Economical Dash Speed Capacity; Lower Landing . EMC /P <>BDC (The data in the second table is payload)Tj EMC BT ET BT ET 7 0 0 7 457.0984 606.7654 Tm 7 0 0 7 364.1531 463.9528 Tm ET EMC support combustion. EMC /P <>BDC What are the ATR 42 and ATR 72 aircraft made by Arospatiale and Leonardo? (makes a flight-for-flight comparison)Tj -.01 Tc (150)Tj (A321ceo, in contrast to the A320neo over)Tj ET In the)Tj /P <>BDC /P <>BDC 6.5 0 0 6.5 90.4525 663.9529 Tm /P <>BDC .023 .567 .626 RG /P <>BDC ET -.02 Tc 9 0 0 9 36.8504 302.8898 Tm EMC ( )Tj 7 0 0 7 247.7395 683.7654 Tm BT BT BT BT EMC ET 5.25 0 0 5.25 549.1047 11.5132 Tm BT 9 0 0 9 394.0157 313.8898 Tm 0 Tc 0 Tc ET 583 0 obj 0 Tc (136)Tj 9 0 0 9 376.0468 401.8898 Tm /P <>BDC /P <>BDC -.02 Tc (carriers. ET ET BT BT 6.5 0 0 6.5 54.877 585.9529 Tm /F1 1 Tf (0.0140)Tj ( )Tj BT ( )Tj EMC BT ET BT /GS1 gs ( )Tj EMC EMC 9 0 0 9 411.0097 357.8898 Tm EMC ET EMC BT BT /P <>BDC -.02 Tc ( )Tj ( )Tj 7 0 0 7 37.6993 276.9528 Tm BT EMC 10 0 0 10 54.8804 814.1973 Tm /P <>BDC /P <>BDC 6.5 0 0 6.5 549.8557 702.9529 Tm 7 0 0 7 258.2805 529.7654 Tm For Example: /P <>BDC BT 9 0 0 9 206.3371 731.8898 Tm ( )Tj ( )Tj /P <>BDC 0 Tc EMC /P <>BDC EMC /P <>BDC -.02 Tc thanks for stopping by. Q (I)Tj -.02 Tc EMC ET /P <>BDC 9 0 0 9 361.007 126.8898 Tm (I)Tj 9 0 0 9 371.6638 247.8898 Tm /P <>BDC ET (\(see table, page 19\))Tj /P <>BDC (485)Tj In contrast, Boeing has)Tj /P <>BDC 9 0 0 9 411.0097 423.8898 Tm /P <>BDC BT /P <>BDC (5B3)Tj For example, if the fuel tank maximum capacity is 10,000 KG, then the tolerance of the gauging is 0.03 (airplane with analog indicators) * 10000 = 300 KG. 7 0 0 7 444.737 397.7654 Tm ET EMC /P <>BDC EMC BT ET 304.725 420.96 m -.02 Tc /P <>BDC 0 Tc ET EMC /P <>BDC 9 0 0 9 187.8892 159.8898 Tm /P <>BDC BT BT /P <>BDC 7 0 0 7 387.0932 100.9528 Tm (The first-class layout uses four-abreast)Tj BT 7 0 0 7 379.3969 331.7654 Tm /P <>BDC 7 0 0 7 427.7291 144.9528 Tm 7 0 0 7 439.7405 496.9528 Tm /P <>BDC ET (737 MAX 10s \(737-10\) ight)Tj 9 0 0 9 232.4217 236.8898 Tm ET (I)Tj EMC ( )Tj 0 Tc (10)Tj 9 0 0 9 425.1913 181.8898 Tm BT BT (977)Tj BT EMC BT EMC /P <>BDC ET 7 0 0 7 230.7317 177.9528 Tm S BT 7 0 0 7 37.6993 364.9528 Tm BT ET -.02 Tc 9 0 0 9 36.8583 478.8898 Tm BT ET ET BT ( )Tj 9 0 0 9 394.0237 170.8898 Tm ET (from 208 degrees on the BOS-MIA)Tj ( )Tj (payload 1 and payload 2 scenarios, the)Tj ET However, it was also shown that the dual venting configuration of some /P <>BDC BT /P <>BDC EMC BT EMC EMC EMC BT Of course, we know that there have been major hiccups in the introduction of the new 737 MAX with the tragic loss of life as a result. BT EMC /P <>BDC 9 0 0 9 186.5751 423.8898 Tm BT ET EMC BT Limitations: Max fuel temp +49C, Min ( )Tj BT EMC ET BT /P <>BDC ( )Tj (289)Tj /F4 1 Tf EMC /P <>BDC EMC ( )Tj /P <>BDC -.02 Tc /P <>BDC ET 7 0 0 7 427.7291 320.9528 Tm EMC ET 9 0 0 9 551.8838 324.8898 Tm EMC BT 7 0 0 7 299.0601 177.9528 Tm EMC ET ( )Tj BT )Tj ET ( )Tj 9 0 0 9 215.4409 401.8898 Tm 0 Tc /P <>BDC BT 0 Tc ( )Tj 6.5 0 0 6.5 480.4 637.9529 Tm 9 0 0 9 204.483 104.8898 Tm /P <>BDC ET ET ( )Tj 0 Tc (0.0112)Tj -.02 Tc -.02 Tc BT /P <>BDC 7 0 0 7 82.2047 463.9528 Tm ET /P <>BDC (. ET BT BT ET EMC Can you please tell me where to look for the cabin height,width, seat height, width and door to door length. /P <>BDC EMC EMC ET 7 0 0 7 534.621 100.7654 Tm ET ( )Tj /P <>BDC EMC EMC ET EMC ET 7 0 0 7 535.5029 144.7654 Tm W n /P <>BDC BT /P <>BDC 9 0 0 9 232.438 467.8898 Tm EMC -.02 Tc /F6 1 Tf EMC 7 0 0 7 67.798 11.5132 Tm ET EMC W n /P <>BDC EMC ( )Tj EMC ( )Tj EMC /P <>BDC /P <>BDC EMC /P <>BDC ET /P <>BDC 9 0 0 9 276.2863 115.8898 Tm 6 0 0 6 153.1846 771.9528 Tm 8 0 0 8 524.1105 760.9528 Tm EMC 7 0 0 7 354.4763 672.7654 Tm EMC ET The trigger for the scavenge pump is different for the series as follows: NB On the classics, when departing with less than 1,000kg of fuel in the centre tank, an imbalance may occur during ET EMC ET EMC /P <>BDC /P <>BDC 7 0 0 7 53.8582 749.7654 Tm 7 0 0 7 491.4046 309.9528 Tm ET ET A nitrogen-enriched air BT ET /P <>BDC (operating performance are analysed here,)Tj /P <>BDC (A320ceo)Tj 7 0 0 7 473.8245 364.9528 Tm -.02 Tc ET /P <>BDC ET 9 0 0 9 374.6152 269.8898 Tm ( )Tj /P <>BDC ET EMC /P <>BDC BT /P <>BDC /P <>BDC -.02 Tc 9 0 0 9 391.5788 478.8898 Tm 6.5 0 0 6.5 181.2003 532.9529 Tm /P <>BDC EMC BT ( )Tj ET BT BT 7 0 0 7 279.1575 507.9528 Tm /P <>BDC ET BT /P <>BDC BT ET [(E)-7.8(P)16.1(T)9(E)-13.9(MBE)-16.9(R)]TJ /P <>BDC /F1 1 Tf /P <>BDC EMC 9 0 0 9 359.0967 786.8898 Tm BT EMC (158)Tj BT 0 Tc ET EMC EMC /GS2 gs /P <>BDC -.02 Tc BT 7 0 0 7 355.3163 320.7654 Tm -.02 Tc EMC ET EMC 0 Tc 9 0 0 9 294.2183 346.8898 Tm ( )Tj BT ET (an improvement in fuel cost per ASM of)Tj BT BT BT BT 6 0 0 6 115.2799 687.9528 Tm /P <>BDC Pingback:Council Post: Aviation Is The Driving Force Of Hydrogen | QNewsHub, Pingback:When will the Boeing 737 MAX fly again? BT endobj 6.5 0 0 6.5 267.1065 742.9529 Tm ET 7 0 0 7 95.225 11.5132 Tm BT ( )Tj EMC -.02 Tc BT /P <>BDC EMC EMC BT /P <>BDC 9 0 0 9 341.4411 247.8898 Tm (payload is carried. ET ( )Tj ET ET 7 0 0 7 490.8321 100.7654 Tm ET EMC BT BT -.02 Tc ET ET /P <>BDC /P <>BDC 7 0 0 7 427.7291 342.9528 Tm -.015 Tc ET BT /P <>BDC BT EMC ( )Tj /P <>BDC BT (39,270)Tj EMC EMC /P <>BDC 0 Tc 7 0 0 7 37.0536 474.9528 Tm BT ET EMC BT /P <>BDC EMC could you point me in the right direction or tell me what the weight of the landing gear would be on a 737? EMC 9 0 0 9 394.0157 610.8898 Tm /P <>BDC 0 Tc (380-396)Tj 7 0 0 7 196.5683 320.7654 Tm 9 0 0 9 252.5351 214.8898 Tm 7 0 0 7 299.0601 408.9528 Tm -.01 Tc ( )Tj /P <>BDC BT 7 0 0 7 279.1575 100.9528 Tm /P <>BDC BT 6.5 0 0 6.5 549.8557 611.9529 Tm /P <>BDC ( )Tj BT ET ET /P <>BDC 9 0 0 9 232.438 302.8898 Tm /P <>BDC ( )Tj BT BT ( )Tj EMC EMC /P <>BDC EMC 6 0 0 6 214.4975 659.9528 Tm 7 0 0 7 403.478 67.7654 Tm /P <>BDC 0 Tc /P <>BDC EMC /P <>BDC (been carried on the similar-sized aircraft. /P <>BDC ET ET 9 0 0 9 348.0922 511.8898 Tm BT The service ceiling is 41,000 feet. -.01 Tc BT (analysis are: an MTOW of 213,848lbs; an)Tj BT BT -.02 Tc 9 0 0 9 213.0312 335.8898 Tm /P <>BDC ( )Tj EMC ET ( )Tj ET BT (and considered against the A320 current)Tj (2,731)Tj 9 0 0 9 36.8504 247.8898 Tm 7 0 0 7 258.2805 386.7654 Tm BT EMC ET 7 0 0 7 247.7395 232.7654 Tm BT ( )Tj EMC /GS1 gs (Engine)Tj ET BT 6 0 0 6 339.8239 701.9528 Tm (603)Tj BT /P <>BDC (0.0119)Tj ET ET EMC /P <>BDC 8 0 0 8 539.8061 771.9528 Tm EMC 7 0 0 7 82.8504 122.9528 Tm 9 0 0 9 568.555 82.8898 Tm ( )Tj -.02 Tc ( )Tj /P <>BDC (1,824)Tj /P <>BDC 7 0 0 7 456.4753 584.7654 Tm .0161 Tc BT BT 0 Tc )Tj 7 0 0 7 490.7815 276.9528 Tm 0 Tc EMC 7 0 0 7 380.2788 485.7654 Tm 10 0 0 10 420.16 814.1973 Tm BT /P <>BDC ET EMC EMC EMC ( )Tj /P <>BDC ET Airbus A320 Specs What is behind one of the most popular short-haul airliners? /P <>BDC EMC 7 0 0 7 199.5784 595.7654 Tm 7 0 0 7 277.3936 67.9528 Tm ET (483)Tj 9 0 0 9 411.0181 324.8898 Tm ( )Tj BT EMC 9 0 0 9 468.446 335.8898 Tm EMC 7 0 0 7 279.1575 210.9528 Tm BT EMC 7 0 0 7 141.7322 67.9528 Tm ( )Tj BT 9 0 0 9 232.4217 456.8898 Tm BT 0 Tw ( )Tj BT )Tj /P <>BDC )Tj /P <>BDC ( )Tj ( )Tj 9 0 0 9 445.6725 302.8898 Tm (considers these routes to give a more)Tj /P <>BDC /P <>BDC EMC BT BT /P <>BDC -.02 Tc BT 7 0 0 7 404.101 276.7654 Tm /P <>BDC ( )Tj 304.725 420.96 m 0 Tw ET 6 0 0 6 403.4411 757.9528 Tm 9 0 0 9 371.4208 522.8898 Tm EMC EMC (737-800:)Tj EMC BT BT 9 0 0 9 377.8897 291.8898 Tm ET ( )Tj (Since all eight aircraft types are in)Tj EMC 6 0 0 6 309.2107 771.9528 Tm EMC BT BT ET EMC EMC BT -.005 Tc ET EMC 9 0 0 9 215.4409 511.8898 Tm BT (airport charges, while the time-dependent)Tj 7 0 0 7 204.0935 672.7654 Tm BT 10 0 0 10 49.3644 814.1973 Tm 9 0 0 9 394.0315 379.8898 Tm 9 0 0 9 36.8504 247.8898 Tm 9 0 0 9 531.902 467.8898 Tm 9 0 0 9 188.1863 170.8898 Tm ET ET 9 0 0 9 53.8582 478.8898 Tm /P <>BDC ET BT ET /P <>BDC (6,875)Tj ET ET ET EMC )Tj 7 0 0 7 141.7322 452.9528 Tm ET 9 0 0 9 53.8338 346.8898 Tm EMC ( )Tj BT BT ET ET BT -.02 Tc BT ET 0 Tc ET EMC /P <>BDC (156)Tj 7 0 0 7 247.7395 705.7654 Tm /P <>BDC /P <>BDC BT /P <>BDC 8 0 0 8 276.7109 633.9528 Tm BT BT ET EMC /P <>BDC (170)Tj /P <>BDC 9 0 0 9 36.8504 159.8898 Tm ( )Tj EMC 0 Tc ET ET 7 0 0 7 403.478 419.7654 Tm BT BT EMC 9 0 0 9 377.4586 676.8898 Tm /P <>BDC /P <>BDC (2,800 -)Tj 7 0 0 7 71.6694 738.9528 Tm 7 0 0 7 519.3773 221.9528 Tm ET 7 0 0 7 54.7071 628.7654 Tm /P <>BDC ET ( )Tj ( )Tj ET BT /P <>BDC 0 Tc ET ET /P <>BDC ET /P <>BDC 9 0 0 9 367.4248 280.8898 Tm EMC 0 841.89 609.449 -841.89 re BT 0 Tc EMC 9 0 0 9 553.9287 643.8898 Tm /P <>BDC EMC ( )Tj BT /GS2 gs ( )Tj ( )Tj BT ET EMC /P <>BDC 9 0 0 9 360.9261 280.8898 Tm EMC (network used in this study, due to fuel tank)Tj 9 0 0 9 215.4313 401.8898 Tm BT ET 9 0 0 9 411.0097 379.8898 Tm /P <>BDC /P <>BDC 0 Tc 7 0 0 7 403.478 727.7654 Tm ET /F4 1 Tf /P <>BDC /P <>BDC Well, what do you know?! 7 0 0 7 457.0984 672.7654 Tm BT 9 0 0 9 394.0237 247.8898 Tm 0 J 0 j .5 w 10 M [] 0 d ET BT -.01 Tc ET /P <>BDC /P <>BDC EMC BT ET (0.0117)Tj EMC ET EMC ( )Tj 19.841 0 l 9 0 0 9 212.1598 302.8898 Tm BT 7 0 0 7 258.2805 606.7654 Tm /P <>BDC 7 0 0 7 316.0679 309.7654 Tm 9 0 0 9 570.805 49.8898 Tm ET 0 Tc -.01 Tc ET ET [(CFM L)17.1(E)-8.1(AP-1B27)]TJ ET ( )Tj 9 0 0 9 351.6906 456.8898 Tm BT ( )Tj ET ( )Tj BT EMC ( )Tj BT ET BT )Tj /P <>BDC ET /P <>BDC ( )Tj EMC BT 9 0 0 9 554.9974 456.8898 Tm 9 0 0 9 68.3339 544.8898 Tm warmer air or accelerate to increase the kinetic heating. ET 9 0 0 9 411.0181 104.8898 Tm -.02 Tc /P <>BDC /P <>BDC ET ET 7 0 0 7 54.5916 243.7654 Tm BT ET ( )Tj /F1 1 Tf ET 6 0 0 6 381.7993 715.9528 Tm ET (977)Tj Q ET 9 0 0 9 215.4313 192.8898 Tm BT (- mins)Tj BT EMC BT /P <>BDC ET BT ET ( )Tj 7 0 0 7 355.3163 166.7654 Tm ( )Tj -.02 Tc (dependent on the operators internal)Tj /P <>BDC BT ET /P <>BDC (2,517)Tj BT BT BT 10 0 0 10 359.2822 794.2914 Tm to test BT EMC 0 Tc EMC 7 0 0 7 473.8245 111.9528 Tm 304.725 420.96 m /P <>BDC (some minor aerodynamic improvements)Tj 7 0 0 7 492.5963 738.7654 Tm /P <>BDC ET -.02 Tc EMC EMC /P <>BDC /P <>BDC /P <>BDC 0 Tc ET EMC EMC BT 7 0 0 7 124.1242 496.7654 Tm EMC EMC 9 0 0 9 411.0097 291.8898 Tm -.02 Tc ( )Tj -.02 Tc (A321ceo)Tj EMC movement as fuel is loaded and used. ET ( )Tj /P <>BDC /P <>BDC ( )Tj ET (additional benefit in this comparison. ET EMC BT 9 0 0 9 246.595 49.8898 Tm EMC ( The reserve fuel policy )Tj BT (between: the Pratt & Whitney PW1127G,)Tj BT BT BT BT /P <>BDC BT EMC /P <>BDC ET EMC /P <>BDC (comparison. BT BT EMC (also impact the actual flight time. (2,220)Tj (382,280)Tj 6.5 0 0 6.5 244.4599 676.9529 Tm endobj 9 0 0 9 232.4217 588.8898 Tm -.02 Tc BT BT ET 8 0 0 8 82.2047 760.9528 Tm /P <>BDC 6 0 0 6 55.0668 645.9528 Tm BT /P <>BDC 6.5 0 0 6.5 549.8557 676.9529 Tm 0 Tc 0 Tc /P <>BDC 7 0 0 7 539.8962 507.9528 Tm 7 0 0 7 379.3969 243.7654 Tm EMC S BT 9 0 0 9 550.6401 401.8898 Tm (136)Tj EMC [(737-900E)-33(R)]TJ ET ( )Tj ( )Tj BT 7 0 0 7 403.478 606.7654 Tm EMC ET 9 0 0 9 368.2199 247.8898 Tm -.02 Tc /P <>BDC ET /P <>BDC /P <>BDC 9 0 0 9 349.1631 60.8898 Tm /P <>BDC /P <>BDC ( )Tj BT ( )Tj 6 0 0 6 61.517 743.9528 Tm BT 0 Tc Wed love you to share what you build when youre done. BT 9 0 0 9 53.8338 280.8898 Tm 6.5 0 0 6.5 432.488 558.9529 Tm BT ET EMC EMC ( )Tj ( )Tj EMC (136)Tj EMC ( )Tj BT BT 7 0 0 7 179.5605 221.9528 Tm (prices, and can vary by the aircraft type)Tj /P <>BDC 0 Tc /P <>BDC 7 0 0 7 457.0984 507.7654 Tm EMC BT /P <>BDC EMC /P <>BDC EMC [(R)30(elativ)12.9(e fuel burn )]TJ EMC (payload, the A321neo has an 18.9%)Tj ( )Tj 9 0 0 9 554.8713 709.8898 Tm ( )Tj /P <>BDC ( )Tj 7 0 0 7 337.6855 221.9528 Tm ( )Tj EMC -.02 Tc 9 0 0 9 394.0315 368.8898 Tm 8 0 0 8 256.0704 717.9528 Tm BT (weight penalty in its OEW compared to its)Tj /P <>BDC 13 0 0 13 53.8338 588.8898 Tm BT 7 0 0 7 536.3849 419.7654 Tm /P <>BDC 7 0 0 7 404.101 100.7654 Tm /P <>BDC EMC 9 0 0 9 538.8445 588.8898 Tm EMC BT BT 6.5 0 0 6.5 107.0213 650.9529 Tm BT EMC 9 0 0 9 547.2866 390.8898 Tm endstream (The 737-9 has an 11.2% to 12.7%)Tj ( )Tj ( )Tj ET (39,270)Tj /P <>BDC /P <>BDC /P <>BDC EMC /P <>BDC 9 0 0 9 394.0123 258.8898 Tm 7 0 0 7 490.5101 507.9528 Tm ( )Tj ( )Tj /P <>BDC EMC /P <>BDC -.02 Tc ET 0 Tc BT /P <>BDC 9 0 0 9 411.0097 566.8898 Tm 0 Tc ET 0 Tc BT BT 0 Tc 7 0 0 7 459.6601 11.5129 Tm EMC )Tj EMC /P <>BDC EMC /OC /MC1974 BDC 7 0 0 7 60.6117 441.7654 Tm 7 0 0 7 158.74 265.7654 Tm 9 0 0 9 550.4545 126.8898 Tm 9 0 0 9 215.4313 148.8898 Tm ( )Tj ( )Tj /P <>BDC ( )Tj A lower)Tj ( )Tj 9 0 0 9 75.273 533.8898 Tm In the 90s Boeing produced 80% of components in house including the wings, fuselage and tall assemblies. 7 0 0 7 204.0935 188.7654 Tm BT ( )Tj /P <>BDC /P <>BDC BT /GS1 gs EMC BT EMC /P <>BDC -.02 Tc BT 7 0 0 7 99.8582 144.7654 Tm EMC ( )Tj 9 0 0 9 53.8338 236.8898 Tm EMC BT EMC ( )Tj EMC EMC 9 0 0 9 369.0641 225.8898 Tm ( )Tj /P <>BDC /P <>BDC EMC ET ET /P <>BDC ( )Tj 9 0 0 9 379.7078 588.8898 Tm /P <>BDC 9 0 0 9 212.5107 313.8898 Tm EMC EMC -.02 Tc (150)Tj 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. /P <>BDC ET 137 )Tj ( )Tj ET /P <>BDC /P <>BDC ET (CFM56-5B4/P)Tj /P <>BDC [(7)-33(3)8(7-800)]TJ /P <>BDC ET EMC ( )Tj 7 0 0 7 537.7804 177.9528 Tm EMC ET (420)Tj BT EMC 7 0 0 7 295.2833 78.7654 Tm ET ( )Tj /P <>BDC EMC 9 0 0 9 571.0211 258.8898 Tm ET /P <>BDC /P <>BDC This from the FAA Systems 7 0 0 7 554.7883 276.7654 Tm BT BT /P <>BDC BT /F6 1 Tf EMC BT 6.5 0 0 6.5 448.257 650.9529 Tm ET BT ET EMC (10)Tj /P <>BDC /OC /MC27 BDC 7 0 0 7 297.632 727.9528 Tm EMC /P <>BDC ET ET /P <>BDC -.02 Tc /P <>BDC BT EMC /P <>BDC 0 Tc BT 7 0 0 7 315.1859 111.7654 Tm The 737-900 also retains the MTOW and fuel capacity of the 800, trading range for payload. EMC 9 0 0 9 411.0234 742.8898 Tm EMC (0.0122)Tj EMC W n (The engine choice on the A320neo is)Tj /P <>BDC ( )Tj /P <>BDC BT ET [(737-900E)-33(R)]TJ BT BT 3-Tank Classics, 20,800kgs for NG/MAX's and up to 37,712kgs for BBJ's depending