BT BT -.02 Tc ET ET EMC ( )Tj ET EMC EMC ET mandatory, but the FAA have repeatedly rejected it on cost grounds. (1A26)Tj BT 0 Tc 7 0 0 7 158.74 661.7654 Tm /P <>BDC BT EMC BT 7 0 0 7 354.6933 496.7654 Tm EMC (. BT 7 0 0 7 518.4953 232.9528 Tm ET ET EMC ET 7 0 0 7 182.5706 573.9528 Tm ET -.005 Tc 7 0 0 7 37.0536 496.9528 Tm /P <>BDC -.02 Tc /P <>BDC ( )Tj BT /P <>BDC BT BT 9 0 0 9 411.0181 137.8898 Tm ET /P <>BDC ET -.02 Tc 10 0 0 10 60.6037 794.2914 Tm next aircraft /P <>BDC 7 0 0 7 539.9176 11.5129 Tm EMC 6.5 0 0 6.5 317.7333 742.9529 Tm /P <>BDC 7 0 0 7 474.7064 100.9528 Tm /P <>BDC /P <>BDC ET /GS2 gs EMC ET 9 0 0 9 36.8504 38.8898 Tm updated to ensure the accuracy of VNAV speeds, buffet margin and max altitude. 6.5 0 0 6.5 192.6116 689.9529 Tm ET ( )Tj BT /P <>BDC 7 0 0 7 37.6993 188.9528 Tm ET /P <>BDC BT BT BT (manufacturers support these aircraft types)Tj /P <>BDC EMC ET BT EMC (487)Tj /Artifact <>BDC BT (195,200)Tj EMC ET ET /P <>BDC BT ET BT ET EMC -.01 Tc (similar rate, with Boeing having delivered)Tj /P <>BDC 6.5 0 0 6.5 274.6269 663.9529 Tm 9 0 0 9 51.0236 258.8898 Tm BT ( )Tj EMC /P <>BDC ET ( )Tj 9 0 0 9 112.3045 346.8898 Tm EMC 9 0 0 9 68.0071 412.8898 Tm EMC ( )Tj 7 0 0 7 554.7883 419.7654 Tm /P <>BDC ET The payload weights for)Tj ET ( )Tj EMC BT The Boeing 737-800 is one of the most popular choices for passenger transport on the market today priced in at 82 million dollars. BT [(BOS-D)17.1(T)-11(W)]TJ 6 0 0 6 466.0123 687.9528 Tm BT ET EMC 5.25 0 0 5.25 465.7151 11.5129 Tm EMC ET EMC BT ET /P <>BDC EMC 13 0 0 13 118.3688 390.8898 Tm /P <>BDC BT /P <>BDC (2,731)Tj ET ET /P <>BDC /P <>BDC 6 0 0 6 561.1918 687.9528 Tm Hi Mark, ET ET 8 0 0 8 397.6498 771.9529 Tm BT BT ( )Tj (380-396)Tj /P <>BDC ( )Tj -.02 Tc (737-8)Tj 9 0 0 9 194.9803 478.8898 Tm ET /P <>BDC 9 0 0 9 562.1829 236.8898 Tm EMC EMC -.02 Tc /P <>BDC /P <>BDC /P <>BDC EMC EMC (. /P <>BDC 6 0 0 6 146.7028 743.9528 Tm BT /P <>BDC ET /P <>BDC ET BT 0 Tc /P <>BDC EMC BT ( )Tj BT /P <>BDC ET (737-9)Tj (in engine cool-down times. EMC (1,272)Tj EMC ET BT 7 0 0 7 99.8582 320.7654 Tm 9 0 0 9 189.3204 324.8898 Tm ET ET ET ( )Tj /P <>BDC 9 0 0 9 197.3303 170.8898 Tm (9 has no payload limitation on any of the)Tj /P <>BDC /P <>BDC ET /P <>BDC -.02 Tc /P <>BDC /P <>BDC EMC (A321ceo)Tj EMC EMC /F7 1 Tf BT 7 0 0 7 427.7291 210.9528 Tm /P <>BDC BT /F7 1 Tf (20)Tj ET BT ET ( )Tj [(CFM L)17.1(E)-8.1(AP-1A26)]TJ .559 .331 .619 rg 0 Tc ( )Tj /P <>BDC /P <>BDC -.02 Tc BT /P <>BDC ET 9 0 0 9 36.8504 93.8898 Tm BT BT EMC BT ET 9 0 0 9 200.4718 38.8898 Tm EMC https://www.markuspilot.com/download/BOEING%20737%20MEASUREMENTS.pdf, Perhaps you will build a cockpit and use it with the new Flight Sim 2020. EMC 9 0 0 9 527.7692 511.8898 Tm BT /P <>BDC EMC 9 0 0 9 214.9959 159.8898 Tm 0 Tc ( )Tj EMC BT ET 9 0 0 9 344.8161 214.8898 Tm /P <>BDC ( )Tj /P <>BDC EMC 7 0 0 7 427.7291 111.9528 Tm -.02 Tc ( )Tj /P <>BDC EMC 9 0 0 9 370.9169 379.8898 Tm -.5815 -.9071 l ET BT 9 0 0 9 36.8504 126.8898 Tm 7 0 0 7 99.8582 694.7654 Tm ET Perhaps somebody has experience in shipment of landing gear. /P <>BDC -.02 Tc The cruise speed to the alternate was)Tj ET /P <>BDC (I)Tj ET 7 0 0 7 508.2252 11.5129 Tm /P <>BDC ET EMC EMC /P <>BDC ET ET ET 9 0 0 9 411.0097 357.8898 Tm 0 Tc 7 0 0 7 362.3891 320.9528 Tm -.02 Tc EMC 0 Tc 0 Tc ( )Tj /P <>BDC ( )Tj .661 .752 .896 rg ET 0 Tc ( )Tj 6.5 0 0 6.5 549.8557 598.9529 Tm 9 0 0 9 554.3696 269.8898 Tm 9 0 0 9 181.5424 71.8898 Tm 9 0 0 9 367.4248 280.8898 Tm BT ( )Tj 9 0 0 9 36.8504 192.8898 Tm -.02 Tc BT (. /P <>BDC -.01 Tc BT ET 9 0 0 9 394.0123 170.8898 Tm 9 0 0 9 394.0315 555.8898 Tm support combustion. EMC EMC BT Q BT BT 9 0 0 9 537.7245 676.8898 Tm BT ET 0 Tc BT ET ET /P <>BDC 9 0 0 9 530.7301 59.9073 Tm BT EMC (CFM56-7B27B3)Tj EMC ET BT EMC ET 0 Tc 8 0 0 8 74.9636 675.9528 Tm BT 9 0 0 9 394.0123 225.8898 Tm EMC /P <>BDC 9 0 0 9 394.0157 214.8898 Tm -.02 Tc EMC (0.0141)Tj 582 0 obj EMC ET -.01 Tc 7 0 0 7 474.7064 232.9528 Tm (l)Tj BT ( )Tj /P <>BDC /P <>BDC ET /P <>BDC ET EMC ( )Tj ET /P <>BDC ET 7 0 0 7 491.4046 331.9528 Tm 7 0 0 7 445.619 496.7654 Tm ET (136)Tj ( )Tj /P <>BDC BT EMC BT The Boeing 737-800 is an example of an average sized airplane. ( )Tj 7 0 0 7 131.6494 177.7654 Tm 9 0 0 9 215.4313 445.8898 Tm BT 0 Tc 0 Tc 0 Tc /P <>BDC 9 0 0 9 215.4313 313.8898 Tm BT EMC /P <>BDC ET BT ET EMC ET 9 0 0 9 571.0211 258.8898 Tm There are two AC powered fuel pumps in each tank; there are also EDPs at BT EMC At least with the Max 8, looking into the ACAP of Boeing (Rev E), I found it is 2500nm. EMC -.02 Tc EMC ( )Tj EMC EMC /P <>BDC /P <>BDC EMC /P <>BDC ( )Tj ET (A320ceo:)Tj ET /P <>BDC ET 0 Tc 7 0 0 7 386.3929 639.9528 Tm BT EMC EMC EMC BT BT BT ( )Tj ET ET /P <>BDC /P <>BDC [(BOS-A)56.9(TL)]TJ ( )Tj 9 0 0 9 194.7833 236.8898 Tm 9 0 0 9 215.4313 478.8898 Tm EMC ET ( )Tj /P <>BDC (310,080)Tj 0 Tc EMC /P <>BDC EMC ( )Tj /GS2 gs BT )Tj ET EMC aux (AA) and fwd aux (FA) respectively. BT EMC BT EMC /P <>BDC -.02 Tc BT (introduction of the newer aircraft types to)Tj EMC ET [(AIRL)8.1(INE & AIR)7.1(CRAF)-12.9(T)18.1( OPERA)56.9(T)-8.1(ION)-13.9(S)]TJ ET BT EMC 6 0 0 6 109.2916 743.9528 Tm EMC (4,163)Tj /P <>BDC 9 0 0 9 569.6968 346.8898 Tm BT EMC 9 0 0 9 384.8177 445.8898 Tm EMC EMC ET EMC 7 0 0 7 354.7351 694.7654 Tm It is)Tj BT (31,416)Tj 9 0 0 9 566.5209 379.8898 Tm BT EMC ET (5B3)Tj 261 0 obj ET ( )Tj 9 0 0 9 531.8156 280.8898 Tm ET This)Tj ( )Tj /P <>BDC BT /P <>BDC /P <>BDC /P <>BDC 7 0 0 7 43.6039 738.9528 Tm BT ET EMC ET (seats. ( )Tj BT ET /P <>BDC (comparing the 737-800 with the 737-8,)Tj EMC ET ( )Tj ( )Tj EMC ET 0 Tc /P <>BDC /P <>BDC ET ET EMC ET ET BT (All the mission lengths are within the)Tj BT ET /P <>BDC EMC EMC /P <>BDC (aircraft having to operate at the non-)Tj (assumed that no additional cargo is taken)Tj BT EMC EMC /P <>BDC 0 Tc ( )Tj 7 0 0 7 187.0858 496.9528 Tm /P <>BDC 9 0 0 9 229.6141 434.8898 Tm ET ( )Tj 9 0 0 9 469.5781 577.8898 Tm 7 0 0 7 554.7883 342.7654 Tm EMC 7 0 0 7 108.6215 67.9528 Tm EMC ET BT /P <>BDC 5.25 0 0 5.25 525.4061 11.5132 Tm /P <>BDC 9 0 0 9 36.8504 225.8898 Tm /P <>BDC ( )Tj ( )Tj ET ET ( )Tj BT BT 9 0 0 9 522.7491 280.8898 Tm EMC -.02 Tc BT ET 7 0 0 7 445.619 540.7654 Tm ET 0 Tc ET 9 0 0 9 68.3339 445.8898 Tm 9 0 0 9 215.4409 434.8898 Tm ET BT 9 0 0 9 185.4953 214.8898 Tm ET [(7)-33(3)8(7-900ER)]TJ [(CFM L)17.1(E)-8.1(AP-1B27)]TJ EMC (A321ceo)Tj /P <>BDC BT EMC ET 9 0 0 9 553.0217 93.8898 Tm ET ( )Tj /P <>BDC 0 Tc 9 0 0 9 348.0922 511.8898 Tm ET ET BT ET EMC /P <>BDC /P <>BDC ET BT ET 9 0 0 9 36.8504 214.8898 Tm ()Tj ET /P <>BDC ET /P <>BDC (reduces to an average 0.04 cents in favour)Tj 9 0 0 9 546.1516 445.8898 Tm EMC EMC EMC And I hope I will get some good stuff to post it to you. /P <>BDC (operator, so controlling this cost is a)Tj BT BT (37,653lbs)Tj BT ET BT /P <>BDC /P <>BDC EMC ET EMC EMC /P <>BDC ET EMC (than the A321ceo. BT ET /P <>BDC 9 0 0 9 36.8504 456.8898 Tm ET /Figure <>BDC EMC BT ET 0 Tc /P <>BDC (evaluate the relative performance of these)Tj (considered include fleet commonality,)Tj 9 0 0 9 411.0181 269.8898 Tm 7 0 0 7 314.6398 507.7654 Tm (150)Tj /P <>BDC 8 0 0 8 43.6039 661.9528 Tm -.01 Tc ET 7 0 0 7 299.0601 331.9528 Tm 7 0 0 7 316.0679 232.7654 Tm 0 Tc EMC EMC BT EMC ( )Tj EMC BT BT EMC EMC ET BT /P <>BDC ET ( )Tj 9 0 0 9 212.0769 71.8898 Tm .1334 -5.7288 l (the A320ceo, despite the neos 1,200lbs)Tj ET BT (to a larger increase when going from 5.7:1)Tj BT 0 Tc /P <>BDC 6 0 0 6 184.4022 729.9528 Tm 0 Tc ET EMC BT (5,376)Tj /P <>BDC EMC 0 Tc /P <>BDC 6 0 0 6 271.1569 743.9528 Tm 7 0 0 7 427.7291 100.9528 Tm BT BT 9 0 0 9 68.3339 511.8898 Tm EMC BT EMC EMC ( )Tj -.02 Tc 7 0 0 7 241.5317 89.9528 Tm EMC BT EMC ET must be determined by using the. -.02 Tc 6.5 0 0 6.5 448.257 637.9529 Tm BT ( )Tj (108 on BOS-SEA \(Seattle\); 123 on BOS-)Tj EMC ET 9 0 0 9 544.5056 302.8898 Tm -.02 Tc BT ( The wind component and)Tj EMC BT EMC /P <>BDC 8 0 0 8 491.3098 760.9528 Tm /P <>BDC BT 6 0 0 6 403.0689 729.9528 Tm (0.0108)Tj ( )Tj EMC BT EMC EMC ET .41 .161 .508 RG ( )Tj 7 0 0 7 158.74 485.7654 Tm 0 Tc ET /P <>BDC ET /P <>BDC ( )Tj ( )Tj /P <>BDC 0 Tc 0 Tc 0 Tw EMC 9 0 0 9 89.5187 104.8898 Tm ET endobj (fan diameter of 78 inches, and a bypass)Tj EMC BT [(E)-7.8(P)16.1(T)9(E)-13.9(MBE)-16.9(R)]TJ EMC [(A3)24.9(21ceo v)12.9(ersus 7)-33(3)8.1(7-900ER\(W)-19(\) )]TJ ET -.02 Tc ( )Tj 9 0 0 9 394.0237 423.8898 Tm /P <>BDC /P <>BDC 6 0 0 6 55.0668 645.9528 Tm EMC 7 0 0 7 314.6398 474.7654 Tm [(M)-9(L)51(W - lbs)]TJ 0 Tc (operationally safe to do so, in the)Tj ET /P <>BDC (2,518)Tj ET ET -.02 Tc ET (6,303)Tj 9 0 0 9 376.2498 478.8898 Tm BT ET /P <>BDC EMC /P <>BDC (. ET BT /P <>BDC (A)Tj ET ( )Tj -.02 Tc -.01 Tc EMC EMC EMC BT ET EMC ET ET ET /P <>BDC 8 0 0 8 456.5927 771.7654 Tm EMC 0 Tc /P <>BDC /P <>BDC ET /P <>BDC ET /P <>BDC /P <>BDC Their version of the Boeing 737-800 is the Airbus A220. 0 Tc BT /P <>BDC BT (10)Tj ET ET ET EMC /P <>BDC /F1 1 Tf 7 0 0 7 82.8504 166.9528 Tm EMC BT EMC ET 9 0 0 9 36.8504 368.8898 Tm BT ET EMC EMC 7 0 0 7 355.5753 584.7654 Tm ( )Tj ET /P <>BDC BT 0 Tc ET -.02 Tc .008 Tc BT 0 J 0 j 15 w 10 M [] 0 d EMC /P <>BDC /P <>BDC ET /F6 1 Tf /P <>BDC BT BT EMC EMC 7 0 0 7 386.4701 408.9528 Tm /P <>BDC EMC -.01 Tc Wed love you to share what you build when youre done. /P <>BDC ET EMC ET /P <>BDC /P <>BDC ET /P <>BDC )Tj 9 0 0 9 394.0315 434.8898 Tm (32,000lbs, down from the 33,000lbs that)Tj EMC ET /F6 1 Tf (CFM56-7B27B3)Tj ET /P <>BDC /P <>BDC EMC 9 0 0 9 232.4217 280.8898 Tm /P <>BDC EMC /P <>BDC BT 5 0 0 5 484.5872 11.5129 Tm EMC /P <>BDC /P <>BDC /P <>BDC BT -.02 Tc /P <>BDC During cruise, the tolerance is less than 0.5%. -.02 Tc 9 0 0 9 206.8842 522.8898 Tm /P <>BDC /Artifact <>BDC ET ET 9 0 0 9 215.4409 313.8898 Tm BT (weights plus the interior cabin)Tj ( )Tj -.02 Tc ET /P <>BDC ET )Tj ET 0 Tc 0 Tc /P <>BDC ET /P <>BDC ET ( )Tj (170)Tj 9 0 0 9 363.4443 390.8898 Tm ( )Tj Although successful the A320 could not take on the Boeing 737s success. ( )Tj BT BT -.02 Tc ET BT ET 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 -.02 Tc /P <>BDC EMC ( )Tj 0 Tc ET BT /P <>BDC (number of seats and ASMs will give an)Tj /P <>BDC BT BT 9 0 0 9 532.3544 214.8898 Tm BT ( )Tj /P <>BDC 0 Tc 7 0 0 7 118.104 408.7654 Tm 7 0 0 7 230.7317 738.9528 Tm BT Main tanks < 50%, -1 to 5 deg pitch, +/- 1 deg roll: +/- 1.0% EMC 10.486 7.6165 l ET levels in the center fuel tanks. EMC 0 Tc BT EMC EMC ET /P <>BDC 7 0 0 7 258.2805 474.7654 Tm EMC -.02 Tc ET ET EMC BT -.02 Tc 0 Tc ET EMC BT ET EMC 9 0 0 9 53.8578 313.8898 Tm ET /P <>BDC been many other improvements to wiring and FQIS. (1,824)Tj ( )Tj BT BT BT BT (170)Tj BT Q EMC 7 0 0 7 141.7322 452.9528 Tm BT EMC ( )Tj EMC ET ( )Tj BT BT EMC BT (the results show that the lighter payload on)Tj BT BT ET /P <>BDC ET BT /P <>BDC EMC EMC BT BT EMC ET BT (I)Tj /P <>BDC 7 0 0 7 187.0858 67.9528 Tm 6.5 0 0 6.5 539.6182 532.9529 Tm EMC /F1 1 Tf BT ( )Tj /P <>BDC EMC ( )Tj BT 9 0 0 9 382.4508 159.8898 Tm /P <>BDC ( )Tj (900ER\(W\) due to the heavier payload. (2,042)Tj BT ET ET ( )Tj BT ( )Tj 7 0 0 7 490.8321 441.7654 Tm BT 9 0 0 9 53.8582 368.8898 Tm ET /P <>BDC /P <>BDC EMC /P <>BDC ( )Tj /P <>BDC ET 6.5 0 0 6.5 64.6596 702.9529 Tm [(AIRL)8.1(INE & AIR)7.1(CRAF)-12.9(T)18.1( OPERA)56.9(T)-8.1(ION)-13.9(S)]TJ 9 0 0 9 36.8504 357.8898 Tm /P <>BDC EMC ET /P <>BDC BT 7 0 0 7 241.2727 166.9528 Tm /P <>BDC BT /P <>BDC BT BT ( )Tj BT (based on the cost index set is different, it)Tj ET /F1 1 Tf /P <>BDC ET (seat capacity as the 737-800 due to the exit)Tj (575)Tj EMC EMC /P <>BDC 7 0 0 7 131.6494 78.7654 Tm /P <>BDC /P <>BDC /P <>BDC 8 0 0 8 60.6117 771.7654 Tm aux tanks to push the aux fuel into the centre tank. /P <>BDC 7 0 0 7 404.101 243.7654 Tm 9 0 0 9 215.433 291.8898 Tm (difference between the aircraft types)Tj /P <>BDC EMC 0 Tc BT BT BT BT EMC EMC five ground) under different ground and flight conditions to demonstrate the 9 0 0 9 394.0157 423.8898 Tm EMC BT [(7)-33(3)8.1(7-800 & 7)-33(3)8.1(7-8 )]TJ ( )Tj EMC 9 0 0 9 536.1277 247.8898 Tm (the fuel burn and operating performance of)Tj ( )Tj The fuel panels for the various series have not changed much over 9 0 0 9 36.8504 192.8898 Tm BT ( )Tj /P <>BDC /P <>BDC ( )Tj EMC 9 0 0 9 394.0157 115.8898 Tm 7 0 0 7 344.1175 562.7654 Tm EMC )Tj 9 0 0 9 394.0315 247.8898 Tm /P <>BDC ET 0 Tc 7 0 0 7 124.1242 595.7654 Tm ET /P <>BDC ET /P <>BDC /P <>BDC BT /P <>BDC (. BT (20)Tj 7 0 0 7 473.8245 419.9528 Tm ET /P <>BDC /GS2 gs 6 0 0 6 527.3389 687.9528 Tm /P <>BDC /P <>BDC BT BT 0 Tc 7 0 0 7 82.8504 177.9528 Tm /OC /MC188 BDC EMC 9 0 0 9 215.433 93.8898 Tm EMC EMC EMC /P <>BDC EMC BT ET /P <>BDC /P <>BDC ET EMC (136-145)Tj BT EMC -.01 Tc EMC ET /P <>BDC ET )Tj (translate into increased range and)Tj ET EMC 9 0 0 9 394.0237 291.8898 Tm EMC BT ( )Tj /P <>BDC ET ( )Tj BT BT EMC 9 0 0 9 552.9554 357.8898 Tm EMC 9 0 0 9 394.0123 533.8898 Tm /P <>BDC (services. 7 0 0 7 537.7804 67.9528 Tm 9 0 0 9 53.8338 269.8898 Tm EMC ( )Tj A family consultation. BT BT ET BT BT (113,016)Tj ( )Tj [(SS)-9(U)8.1(E)]TJ BT EMC ET q 1 0 0 1 394.016 747.971 cm 0 0 m EMC (subsidiary airlines. EMC 7 0 0 7 473.8245 265.9528 Tm 6 0 0 6 412.5551 659.9528 Tm 7 0 0 7 277.3936 177.9528 Tm /P <>BDC 0 Tc BT EMC ET BT ET /P <>BDC EMC BT BT /P <>BDC ( )Tj ( )Tj ( )Tj 7 0 0 7 54.5916 639.7654 Tm /P <>BDC /P <>BDC 7 0 0 7 95.225 11.5132 Tm ET ( )Tj ET 10 0 0 10 225.1837 771.9528 Tm /P <>BDC EMC [(Aircr)10(aft type)]TJ 8 0 0 8 182.2355 760.7654 Tm ET /P <>BDC /P <>BDC ( )Tj /P <>BDC ET next aircraft 7 0 0 7 440.0906 232.9528 Tm /P <>BDC ET EMC EMC BT ( )Tj BT (-62)Tj ET 7 0 0 7 490.8321 419.7654 Tm ( )Tj ET /P <>BDC ET ET ET EMC 7 0 0 7 490.5101 683.9528 Tm ( )Tj ET /P <>BDC BT -.02 Tc BT EMC EMC In contrast, the 737-8s performance)Tj /P <>BDC 7 0 0 7 82.8504 309.9528 Tm EMC BT 7 0 0 7 321.6356 133.9528 Tm ( )Tj ( )Tj ( )Tj /P <>BDC -.01 Tc ET EMC ( )Tj /P <>BDC BT 9 0 0 9 53.8582 478.8898 Tm 7 0 0 7 99.8582 683.7654 Tm /P <>BDC EMC (977)Tj BT EMC ET /P <>BDC 6 0 0 6 184.0127 771.9528 Tm BT (146,550)Tj BT 9 0 0 9 356.7322 159.8898 Tm -.02 Tc ET (A)Tj -.01 Tc EMC BT )Tj BT ET .0161 Tc (3,031)Tj ET EMC EMC /P <>BDC /P <>BDC 8 0 0 8 187.3427 661.9528 Tm ET EMC 0 Tc 9 0 0 9 533.9409 390.8898 Tm 0 Tc 9 0 0 9 36.8504 456.8898 Tm /P <>BDC BT ET 9 0 0 9 455.2971 478.8898 Tm ( )Tj /P <>BDC -.02 Tc EMC /P <>BDC ET BT ET ET /P <>BDC ( )Tj BT ( )Tj BT .0161 Tc EMC ( )Tj EMC ET 9 0 0 9 53.8582 60.8898 Tm <>/XObject<>/ExtGState<>/Properties<>>> EMC BT 7 0 0 7 457.0984 331.7654 Tm 9 0 0 9 51.0236 335.8898 Tm /P <>BDC ET ( )Tj q 1 0 0 1 53.858 150.878 cm 0 0 m 6 0 0 6 554.8917 743.9528 Tm BT EMC BT ET 9 0 0 9 361.2861 181.8898 Tm 0 Tc ET ET (The in-service fleet of the newer)Tj (37,653)Tj 9 0 0 9 394.0315 137.8898 Tm )Tj ET ET /GS2 gs 7 0 0 7 158.74 386.7654 Tm BT BT EMC 6 0 0 6 54.1367 771.9528 Tm 10 0 0 10 36.8504 814.1973 Tm BT -.02 Tc /P <>BDC ( )Tj 0 Tc ( )Tj EMC The 737-800 incorporates an advanced-technology wing design that helps increase fuel capacity and efficiency, both of which increase range. ET /P <>BDC 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. EMC ( )Tj /P <>BDC ET EMC 7 0 0 7 445.619 518.7654 Tm /P <>BDC 73 0 obj ET /P <>BDC [(Seat configur)10(ation)]TJ (distances, and alternate airports are shown)Tj [(CFM L)17.1(E)-8.1(AP-1B27)]TJ EMC EMC ( )Tj ET 6 0 0 6 326.0708 673.9528 Tm (10)Tj ( )Tj /P <>BDC -.02 Tc (0.0111)Tj ( )Tj EMC /P <>BDC BT (39,270)Tj BT /P <>BDC /P <>BDC ET ( )Tj 0 841.89 609.449 -841.89 re EMC ET 7 0 0 7 363.2711 386.9528 Tm BT /Artifact <>BDC 7 0 0 7 99.8582 441.7654 Tm 7 0 0 7 37.6993 375.9528 Tm 0 Tc (342,312)Tj ET ET ET /P <>BDC /P <>BDC ET ET ET BT /P <>BDC ET BT 9 0 0 9 36.8504 346.8898 Tm (load factor, the A321neo carries a heavier)Tj 0 Tc -.02 Tc /P <>BDC 5.25 0 0 5.25 73.853 11.5132 Tm 7 0 0 7 343.2355 474.7654 Tm 9 0 0 9 411.0097 379.8898 Tm ET /P <>BDC BT 9 0 0 9 53.8338 192.8898 Tm BT BT EMC ET BT 9 0 0 9 411.0234 698.8898 Tm BT ( )Tj )Tj -.02 Tc EMC EMC EMC ET 9 0 0 9 386.3946 137.8898 Tm (have been optimised by the PPS flight)Tj /P <>BDC . EMC EMC 7 0 0 7 355.3163 133.7654 Tm .151 .147 .15 rg /P <>BDC BT 0 Tc EMC ET 6 0 0 6 246.6462 743.9528 Tm ET /P <>BDC /P <>BDC BT ET It requires a 2316 meter or 7,598.33 feet of take off distance. 7 0 0 7 247.7395 430.7654 Tm ET EMC 7 0 0 7 363.2711 485.9528 Tm /P <>BDC /P <>BDC /P <>BDC (214,730)Tj (comparison is the CFM56-5B3/P. 0 Tc ( )Tj /P <>BDC /P <>BDC ET ET ET EMC /P <>BDC 9 0 0 9 408.2047 313.8898 Tm EMC EMC EMC ( )Tj BT (method of operation that balances the cost)Tj ET /P <>BDC 0 Tc (1,581)Tj BT -.02 Tc 9 0 0 9 455.0733 60.8898 Tm (418)Tj ( )Tj 9 0 0 9 538.8445 588.8898 Tm 7 0 0 7 508.4124 397.7654 Tm 7 0 0 7 536.3849 507.7654 Tm ET 7 0 0 7 37.0536 584.9528 Tm ( )Tj 9 0 0 9 73.1083 500.8898 Tm /P <>BDC ET BT ALERT light illuminates on the main panel. BT /P <>BDC ET ( )Tj 7 0 0 7 490.5101 694.9528 Tm -.02 Tc ( )Tj Well, the fuel capacity of this airplane varies depending on the specific model and generation. 7 0 0 7 337.4684 672.9528 Tm BT Additionally, below 10,000 feet it should not exceed 250 knots. BT ET ET 7 0 0 7 247.7395 111.7654 Tm (0.0153)Tj /P <>BDC EMC BT EMC /P <>BDC Bombardier CRJ 700/CRJ 900/CRJ 1000 Series. /P <>BDC /P <>BDC 0 Tc BT - Modern Airliners. EMC ET ET 7 0 0 7 36.8504 11.5129 Tm 9 0 0 9 394.0315 115.8898 Tm BT Thank you. 9 0 0 9 411.0097 214.8898 Tm EMC BT /P <>BDC -.02 Tc 6.5 0 0 6.5 244.2585 598.9529 Tm 7 0 0 7 445.619 463.7654 Tm BT EMC BT (1,960)Tj BT EMC endobj ET ET 7 0 0 7 204.0935 628.7654 Tm 7 0 0 7 354.6933 287.7654 Tm ET EMC (\(ATC\) charges. /P <>BDC /P <>BDC /P <>BDC It works by transferring fuel from the aux /P <>BDC BT 0 Tc 8 0 0 8 91.2605 771.9529 Tm BT ( )Tj ET /P <>BDC EMC ET /P <>BDC BT ( )Tj /P <>BDC ET (CFM56-5B3/P)Tj 9 0 0 9 36.8504 489.8898 Tm ET /P <>BDC ET /P <>BDC ( )Tj -.02 Tc [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ BT /P <>BDC BT EMC (1,761)Tj 7 0 0 7 321.6356 309.9528 Tm /P <>BDC ET /P <>BDC /P <>BDC (US airspace can be congested near the)Tj BT 6.5 0 0 6.5 93.2476 702.9529 Tm (uses one of the 11 certified weight variants. /P <>BDC 6.5 0 0 6.5 295.373 742.9529 Tm 0 Tc Values can be entered and displayed in pounds or kilograms. Its fuel burn and)Tj 0 Tc /P <>BDC 0 Tc EMC (35,112)Tj 0 Tc BT ET (2,731)Tj EMC EMC 517.244 80.729 l ET /P <>BDC 7 0 0 7 554.7883 628.7654 Tm /Artifact <>BDC 10 0 0 10 422.8 814.1973 Tm [(b)6.1(ypass r)10(atio engines pr)10(o)16.1(vide it with the most)]TJ EMC (I)Tj (136)Tj (passenger payload. ( )Tj BT BT ET 0 Tc (0.0158)Tj EMC /Artifact <>BDC /P <>BDC ET /P <>BDC 0 Tc ( )Tj /P <>BDC 7 0 0 7 247.7395 716.7654 Tm /P <>BDC /P <>BDC Seating in the 737 was a result of the design when moving the engines underneath the wings. ET BT 9 0 0 9 411.0181 258.8898 Tm ET 7 0 0 7 131.6494 474.7654 Tm BT /P <>BDC BT ET EMC /P <>BDC 0 Tc EMC EMC ET /P <>BDC /P <>BDC /P <>BDC EMC /P <>BDC BT ET 8 0 0 8 38.4438 577.9528 Tm q 1 0 0 1 36.85 84.878 cm 0 0 m 0 Tc BT 9 0 0 9 232.4217 93.8898 Tm BT )Tj /OC /MC1321 BDC BT ()Tj ( )Tj 7 0 0 7 297.632 727.9528 Tm 7 0 0 7 99.8582 265.7654 Tm /P <>BDC /P <>BDC /GS2 gs /P <>BDC /P <>BDC ( )Tj ET ET 7 0 0 7 141.7322 122.9528 Tm (assumes that an equal number of)Tj BT /P <>BDC /P <>BDC BT EMC 7 0 0 7 158.74 298.7654 Tm EMC -.02 Tc 7 0 0 7 387.0932 287.9528 Tm 9 0 0 9 547.562 126.8898 Tm ( )Tj ( )Tj EMC /P <>BDC /P <>BDC 8 0 0 8 543.5282 797.8898 Tm BT EMC EMC ET ET /P <>BDC [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ ET BT /P <>BDC /P <>BDC EMC BT /P <>BDC /P <>BDC EMC ( )Tj ( )Tj Boeing 737 Interior. 9 0 0 9 394.0157 379.8898 Tm -.01 Tc BT EMC ET EMC ET EMC 7 0 0 7 445.619 122.7654 Tm 9 0 0 9 215.433 225.8898 Tm 6.5 0 0 6.5 448.4585 689.9529 Tm 9 0 0 9 546.3135 258.8898 Tm 9 0 0 9 394.0157 291.8898 Tm 8 0 0 8 332.978 591.9528 Tm ET ET /P <>BDC EMC /P <>BDC BT (737-800W)Tj ( )Tj BT (the 14 sectors with the 85% passenger)Tj 0 Tc /P <>BDC EMC ET 0 Tc (category. ( )Tj ( )Tj BT BT (31,416)Tj EMC BT 7 0 0 7 158.74 496.7654 Tm BT /P <>BDC (2,732)Tj (The specifications and weights of all)Tj 7 0 0 7 439.2087 320.9528 Tm 7 0 0 7 536.3849 584.7654 Tm /P <>BDC BT 9 0 0 9 411.0097 434.8898 Tm 7 0 0 7 95.225 11.5132 Tm EMC ( )Tj ET ( )Tj 6.5 0 0 6.5 64.6596 532.9529 Tm EMC EMC ET /P <>BDC ET 9 0 0 9 361.016 49.8898 Tm 7 0 0 7 294.4014 298.7654 Tm BT EMC ET BT BT EMC EMC 6.5 0 0 6.5 484.6315 545.9529 Tm /P <>BDC (831)Tj BT ET 7 0 0 7 118.104 364.7654 Tm (. EMC ( )Tj EMC 9 0 0 9 394.0157 104.8898 Tm /P <>BDC 9 0 0 9 75.273 478.8898 Tm ( )Tj BT -.02 Tc 7 0 0 7 241.5317 232.9528 Tm EMC 9 0 0 9 394.0157 522.8898 Tm ( )Tj ( )Tj EMC 9 0 0 9 215.4313 258.8898 Tm .559 .331 .619 rg 9 0 0 9 270.2513 313.8898 Tm endobj 19.84 0 l 9 0 0 9 232.4217 148.8898 Tm (A321ceo)Tj (158)Tj /P <>BDC ( )Tj BT )Tj BT ET ( )Tj EMC /P <>BDC /P <>BDC 7 0 0 7 141.7322 67.9528 Tm EMC ET BT (111)Tj 9 0 0 9 375.5153 291.8898 Tm /P <>BDC EMC BT (339-353)Tj EMC EMC BT /P <>BDC /P <>BDC ET /P <>BDC -.02 Tc 9 0 0 9 522.1112 247.8898 Tm EMC BT 0 Tc ET Thank you. ET BT BT (192)Tj On the 1-500's, the centre tank pumps are located in a dry /P <>BDC /P <>BDC BT ET EMC 6.5 0 0 6.5 528.5291 689.9529 Tm EMC 0 Tc /P <>BDC /P <>BDC EMC EMC /P <>BDC /OC /MC834 BDC ( )Tj 0 Tc 9 0 0 9 53.8582 214.8898 Tm EMC EMC EMC 9 0 0 9 362.6813 357.8898 Tm 7 0 0 7 427.7291 375.9528 Tm ET ( )Tj EMC BT /P <>BDC ( )Tj ET !! /P <>BDC /P <>BDC BT BT /P <>BDC 0 Tc .151 .147 .15 rg ET ( )Tj 0 Tc ( )Tj BT ET BT 9 0 0 9 215.4409 324.8898 Tm 9 0 0 9 373.4379 324.8898 Tm 9 0 0 9 146.3 346.8898 Tm 9 0 0 9 53.8338 38.8898 Tm ET /P <>BDC EMC 7 0 0 7 158.74 364.7654 Tm /P <>BDC 7 0 0 7 37.0536 529.9528 Tm ET 7 0 0 7 491.4046 144.9528 Tm 0 Tc ( )Tj EMC 9 0 0 9 382.9368 148.8898 Tm /P <>BDC /P <>BDC (5,350)Tj 9 0 0 9 229.6064 335.8898 Tm EMC ( )Tj ET f 9 0 0 9 536.024 533.8898 Tm 7 0 0 7 439.8175 727.9528 Tm ET -.02 Tc BT BT 9 0 0 9 199.3017 401.8898 Tm 9 0 0 9 163.2471 269.8898 Tm /P <>BDC 9 0 0 9 521.2213 170.8898 Tm (operation the overflight and airport)Tj 7 0 0 7 380.2788 496.7654 Tm 13 0 0 13 162.9571 181.8898 Tm EMC /P <>BDC BT ( C)Tj ( )Tj 7 0 0 7 456.2165 144.7654 Tm 9 0 0 9 180.5261 423.8898 Tm

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