9 0 0 9 394.0123 368.8898 Tm BT 6.5 0 0 6.5 276.4014 637.9529 Tm /F4 1 Tf ET 7 0 0 7 187.5417 430.9528 Tm BT 9 0 0 9 570.805 49.8898 Tm EMC EMC BT /F1 1 Tf ( )Tj BT BT BT EMC ( )Tj (176)Tj ( )Tj (2,575)Tj /P <>BDC EMC (1,272)Tj 7 0 0 7 116.3631 11.5132 Tm (BOS-DEN)Tj ( )Tj /P <>BDC ( )Tj 13 0 0 13 411.0097 467.8898 Tm /P <>BDC ET . ET ET BT BT 9 0 0 9 232.4217 357.8898 Tm (37,653lbs)Tj [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ BT BT BT /P <>BDC EMC EMC ET EMC EMC ET [(737 M)-8.1(A)-24.9(X-8:)]TJ BT ET (- nm)Tj 9 0 0 9 215.433 280.8898 Tm 6 0 0 6 226.1079 659.9528 Tm ET ET (performance )Tj maximum declarable fuel capacity for tech log, nav log, etc is 16,200kgs for EMC ( )Tj (shorter sectors. /P <>BDC /P <>BDC BT /P <>BDC /P <>BDC EMC 7 0 0 7 508.4124 320.7654 Tm ( )Tj ET EMC ET BT BT 7 0 0 7 125.6292 386.7654 Tm /P <>BDC /P <>BDC ET EMC (136)Tj 9 0 0 9 204.4018 665.8898 Tm It is produced in the Renton plant in Washington by Boeing Commercial Airplanes. ET /P <>BDC BT /P <>BDC EMC 9 0 0 9 568.6457 357.8898 Tm 0 Tc 9 0 0 9 215.4409 247.8898 Tm ET 6.5 0 0 6.5 346.1424 545.9529 Tm 5.25 0 0 5.25 515.3989 11.5129 Tm ET 6.5 0 0 6.5 244.2974 545.9529 Tm BT EMC /P <>BDC 304.725 420.96 m Their version of the Boeing 737-800 is the Airbus A220. (newer aircraft types will have the same)Tj 9 0 0 9 394.0123 170.8898 Tm ET -.02 Tc 9 0 0 9 411.0097 357.8898 Tm /Artifact <>BDC ( )Tj ET EMC EMC /P <>BDC ET ET 7 0 0 7 326.2278 595.9528 Tm BT 9 0 0 9 214.7728 247.8898 Tm ET BT ET /P <>BDC EMC 7 0 0 7 521.4928 573.9528 Tm ( )Tj /P <>BDC ( )Tj /P <>BDC Happy Flying. 7 0 0 7 473.8245 375.9528 Tm -.02 Tc ( )Tj ( )Tj EMC BT EMC (ASM is 0.09 cents better for the A321neo. BT BT /F1 1 Tf ET BT 9 0 0 9 392.5848 379.8898 Tm ( )Tj 9 0 0 9 408.1854 423.8898 Tm 7 0 0 7 554.7883 78.7654 Tm .41 .161 .508 rg 7 0 0 7 54.7071 287.7654 Tm ET EMC ET ET ( )Tj EMC ( )Tj ( )Tj -.02 Tc BT BT 9 0 0 9 394.0123 324.8898 Tm (124,650)Tj -.02 Tc /P <>BDC BT ET ET BT EMC 6.5 0 0 6.5 276.4014 598.9529 Tm /P <>BDC ( )Tj 7 0 0 7 539.8962 672.9528 Tm BT (831)Tj /P <>BDC (The 737-900ER\(W\)s advantage in fuel)Tj 9 0 0 9 215.4409 500.8898 Tm ( )Tj 9 0 0 9 215.4313 38.8898 Tm 9 0 0 9 214.9959 159.8898 Tm EMC 7 0 0 7 233.5248 78.9528 Tm /P <>BDC 7 0 0 7 439.7405 507.9528 Tm EMC /GS1 gs ET /P <>BDC probably take you over MTOW if any payload was carried. EMC /P <>BDC BT BT /P <>BDC /P <>BDC /P <>BDC EMC ET /GS1 gs ET BT BT EMC ET ET ET ( )Tj EMC (/S)Tj endobj 6.5 0 0 6.5 335.5237 532.9529 Tm ( )Tj EMC EMC (415,112)Tj BT /P <>BDC EMC /P <>BDC ET EMC BT 9 0 0 9 36.8583 335.8898 Tm ( )Tj ET EMC BT ET EMC (sector. /P <>BDC 7 0 0 7 294.4014 122.7654 Tm (the A321ceo, A321neo, 737-900ER\(W\))Tj /P <>BDC EMC (on the longest sector. EMC EMC ET ET -.02 Tc 9 0 0 9 215.433 38.8898 Tm BT ET BT BT ET /P <>BDC /P <>BDC 7 0 0 7 247.7395 573.7654 Tm ( )Tj EMC /P <>BDC /P <>BDC BT BT 7 0 0 7 116.3631 11.5132 Tm 0 Tc 0 Tc /P <>BDC /P <>BDC endobj /P <>BDC ET 0 Tc (1,138)Tj ET EMC ( )Tj (hour, increases, the average fuel burn per)Tj (342,312)Tj 9 0 0 9 36.8504 368.8898 Tm EMC EMC 7 0 0 7 193.1059 89.9528 Tm EMC BT EMC EMC ( )Tj BT /P <>BDC (CFM56-7B27B3 installed on the 737-)Tj EMC EMC ( )Tj 7 0 0 7 491.7142 133.7654 Tm ET 9 0 0 9 367.9911 71.8898 Tm BT EMC ( )Tj 9 0 0 9 394.0237 269.8898 Tm BT EMC 0 Tc 9 0 0 9 394.0157 434.8898 Tm EMC 7 0 0 7 182.5706 342.9528 Tm ( )Tj /P <>BDC EMC ET ET I know the 787 is moving toward using more composite materiel instead of aluminum. BT EMC BT 9 0 0 9 551.0194 588.8898 Tm /P <>BDC 9 0 0 9 394.0315 225.8898 Tm EMC BT ET /P <>BDC ET 304.725 420.96 m ET BT /P <>BDC EMC /P <>BDC (273,750)Tj 7 0 0 7 193.1059 386.9528 Tm EMC ( )Tj ( )Tj -.02 Tc ( )Tj (payload and route, and 16% higher than)Tj /P <>BDC BT BT ( N)Tj EMC This is the same)Tj BT -.02 Tc /P <>BDC ET EMC (0.0108)Tj ET BT (All the flights were in a westerly)Tj BT EMC ( )Tj BT /P <>BDC /P <>BDC 7 0 0 7 490.8321 111.7654 Tm /P <>BDC EMC /P <>BDC ET BT /P <>BDC BT 7 0 0 7 554.7883 672.7654 Tm The AFM limits are higher, but not normally ET 7 0 0 7 554.7883 100.7654 Tm EMC ET /P <>BDC EMC BT ET /P <>BDC 0 Tc ET BT EMC EMC /P <>BDC 7 0 0 7 535.5029 298.7654 Tm 9 0 0 9 73.1083 511.8898 Tm Right centre tank fuel pump on the forward wall of the 7 0 0 7 131.6494 672.7654 Tm 9 0 0 9 391.4889 192.8898 Tm )Tj BT BT /P <>BDC 7 0 0 7 247.7395 232.7654 Tm ET [(O)6.1(AK/35)]TJ EMC 7 0 0 7 387.0159 540.9528 Tm ET (LRC speed. /GS1 gs 7 0 0 7 457.0984 485.7654 Tm BT ET 9 0 0 9 53.8578 467.8898 Tm /P <>BDC 9 0 0 9 186.5751 423.8898 Tm BT 7 0 0 7 258.2805 727.7654 Tm (2,517)Tj /P <>BDC ET EMC ( )Tj 7 0 0 7 387.0932 78.9528 Tm .534 .14 .504 RG [(BL)32(OCK F)8.1(UEL)31( PERF)8.1(ORMANCE OF A3)24.9(20CEO, A3)24.9(20NEO, A3)24.9(21CEO, A3)24.9(21NEO, 7)-33(3)8.1(7-800, 7)-33(3)8.1(7-900ER, 7)-33(3)8.1(7-8 & 7)-33(3)8.1(7-9 - P)30(A)52(YL)32(O)6.1(AD SCENARIO 1 )]TJ ( )Tj BT EMC 0 Tc 7 0 0 7 116.3631 11.5132 Tm ET ET (HGW2 option with an MTOW of)Tj /P <>BDC EMC )Tj ( )Tj ( )Tj EMC -.02 Tc ( )Tj /P <>BDC BT EMC BT 9 0 0 9 394.0237 346.8898 Tm 9 0 0 9 394.0315 577.8898 Tm EMC ET /P <>BDC Firstly, thank you for reply. EMC /P <>BDC 9 0 0 9 215.4409 159.8898 Tm 9 0 0 9 545.4755 654.8898 Tm ( )Tj BT 0 Tc (difference in fuel cost per ASM, however,)Tj 9 0 0 9 194.5468 71.8898 Tm 7 0 0 7 277.3936 166.9528 Tm ( )Tj -.005 Tc ET -.02 Tc (sectors, particularly the shorter ones,)Tj EMC EMC ( )Tj /P <>BDC BT ( )Tj ( )Tj 7 0 0 7 247.7395 584.7654 Tm 9 0 0 9 232.4217 291.8898 Tm ET -.02 Tc 7 0 0 7 446.5009 595.7654 Tm EMC BT EMC EMC EMC BT /P <>BDC Even an empty tank has some unusable fuel ET 0 Tc The total capacity is 526 seats broken down to 162 first class seats, 175 business class and 189 economy seats. ET [(CFM L)17.1(E)-8.1(AP-)]TJ EMC 7 0 0 7 279.1575 419.9528 Tm /P <>BDC 7 0 0 7 125.6292 331.7654 Tm )Tj EMC ( )Tj (CFM56-5B4/P)Tj /P <>BDC -.02 Tc 9 0 0 9 215.4409 478.8898 Tm EMC Hi there.. is anyone able to tell me the radius of the arc of the L1 and L2 doors as they are being opened? /P <>BDC ET -.02 Tc EMC 7 0 0 7 67.798 11.5132 Tm /P <>BDC BT 9 0 0 9 232.4217 478.8898 Tm EMC /P <>BDC ET 7 0 0 7 204.0935 287.7654 Tm (178-187)Tj BT ET 7 0 0 7 118.104 166.7654 Tm (A320ceo)Tj EMC BT /P <>BDC ET 9 0 0 9 53.8578 225.8898 Tm 9 0 0 9 369.892 412.8898 Tm ET (difference. q 1 0 0 1 215.431 128.878 cm 0 0 m 9 0 0 9 215.4313 335.8898 Tm EMC (BOS-PHX)Tj /P <>BDC BT /P <>BDC EMC EMC BT BT (1B engine as the 737-8. ( )Tj EMC ( )Tj ET EMC ET (34,650)Tj 10 0 0 10 420.16 814.1973 Tm ( )Tj /P <>BDC BT ET 0 Tc 7 0 0 7 294.4014 375.7654 Tm 9 0 0 9 36.8504 313.8898 Tm ET 8 0 0 8 435.4879 760.7654 Tm EMC /P <>BDC The 737-200Adv could also be fitted with an BT /P <>BDC (4,000)Tj EMC /P <>BDC ( )Tj BT BT BT /P <>BDC /P <>BDC ET BT 7 0 0 7 490.5226 78.9528 Tm (2,054)Tj Fuel quantity is measured by using a series of EMC /P <>BDC /P <>BDC EMC (737-800 and 737-8; and 170 passengers on)Tj ET ( )Tj /P <>BDC BT [(C)17.1(OS/104)]TJ 0 Tc /P <>BDC 7 0 0 7 554.7883 562.7654 Tm 9 0 0 9 181.3643 335.8898 Tm EMC 7 0 0 7 54.7071 67.7654 Tm -.02 Tc 8 0 0 8 159.2283 745.9528 Tm BT 0 Tc ET /P <>BDC -.02 Tc (types )Tj /P <>BDC BT ET BT 9 0 0 9 411.0181 148.8898 Tm ET ET 0 Tc ET EMC 7 0 0 7 141.7322 287.9528 Tm ET /P <>BDC EMC EMC ET BT /P <>BDC [(CFM L)17.1(E)-8.1(AP-1B27)]TJ /OC /MC1320 BDC EMC Due to the aircraft types and)Tj (payload is carried. /P <>BDC /GS2 gs 9 0 0 9 232.438 49.8898 Tm ( )Tj (176)Tj /P <>BDC (737-900ER\(W\). BT ET ET W n 9 0 0 9 411.0097 445.8898 Tm ET Hi and thanks for your question. /P <>BDC 0 Tc 8 0 0 8 43.6039 661.9528 Tm 0 Tc ET EMC ET BT BT /P <>BDC ET ( )Tj /P <>BDC BT (0.0137)Tj -.02 Tc /P <>BDC 7 0 0 7 141.7322 166.9528 Tm BT ET EMC EMC BT /P <>BDC ET (The overflight and airport charges are)Tj 9 0 0 9 362.2746 489.8898 Tm ( )Tj 0 Tc 7 0 0 7 294.4014 342.7654 Tm allowed to run dry or be left running unsupervised. Irkut MC-21, Russias homegrown modern airliner. ET BT BT /P <>BDC /P <>BDC 0 Tc 0 Tc /P <>BDC ( )Tj 8 0 0 8 549.2646 49.8898 Tm BT /P <>BDC (2,437)Tj ( )Tj ET /P <>BDC ( )Tj ( )Tj ET ET 9 0 0 9 53.8582 500.8898 Tm /P <>BDC /GS2 gs BT (hour and per mile reduces . The 800 was developed to replace the 727 on short routes. ET /P <>BDC /P <>BDC EMC ( )Tj ET BT /P <>BDC BT 9 0 0 9 394.0123 489.8898 Tm Hi Andrey, (CFM56-5B3/P)Tj EMC /P <>BDC 9 0 0 9 394.0315 269.8898 Tm BT /P <>BDC 7 0 0 7 473.8245 265.9528 Tm ET ET (an OEW of 98,500lbs )Tj /P <>BDC ET 0 Tc EMC ET /P <>BDC -.02 Tc /P <>BDC 7 0 0 7 113.1366 617.9528 Tm EMC EMC /P <>BDC BT /P <>BDC (A320neo:)Tj ET /P <>BDC 6 0 0 6 561.1317 771.9528 Tm -.02 Tc 8 0 0 8 136.4919 675.9528 Tm -.02 Tc -.02 Tc -.02 Tc /P <>BDC /P <>BDC /P <>BDC ( )Tj ET EMC /P <>BDC EMC /P <>BDC EMC BT EMC EMC EMC 7 0 0 7 469.2222 11.5129 Tm ET (10)Tj EMC BT 9 0 0 9 53.8338 313.8898 Tm /P <>BDC The total tolerance for the FQIS system is based on a full tank. Although successful the A320 could not take on the Boeing 737s success. (BOS-ORD)Tj ET EMC ET (the two scenarios are detailed )Tj -.02 Tc BT ET ET (its payload reduced to 165 passengers from)Tj /P <>BDC ( )Tj ET 202.559 814.197 m 7 0 0 7 444.737 287.7654 Tm ( )Tj EMC (. EMC 5.25 0 0 5.25 73.853 11.5132 Tm 7 0 0 7 158.74 144.7654 Tm ( )Tj ET EMC /P <>BDC (163)Tj -.01 Tc BT EMC BT /P <>BDC EMC EMC /P <>BDC BT BT BT ET ET /P <>BDC 6 0 0 6 459.5796 729.9528 Tm -.005 Tc 6 0 0 6 339.5547 771.9528 Tm BT ( )Tj 9 0 0 9 181.5981 280.8898 Tm /P <>BDC 6.5 0 0 6.5 64.6596 585.9529 Tm ET 9 0 0 9 202.684 357.8898 Tm EMC ET 9 0 0 9 232.4408 753.8898 Tm ( )Tj ( )Tj ET 7 0 0 7 491.4046 408.9528 Tm BT EMC ET ( )Tj (193,344)Tj ET 7 0 0 7 321.6356 199.9528 Tm ( )Tj BT /P <>BDC 7 0 0 7 108.6215 331.9528 Tm /P <>BDC BT EMC 8 0 0 8 83.5638 619.9528 Tm /P <>BDC ET /P <>BDC ( )Tj /P <>BDC BT 9 0 0 9 394.0123 148.8898 Tm BT EMC ET BT -.02 Tc /P <>BDC (The equivalent still air distance \(ESAD\))Tj /P <>BDC (l)Tj /P <>BDC /P <>BDC EMC /P <>BDC In scenario 2, the 85% payload)Tj ET (603)Tj 9 0 0 9 394.0315 291.8898 Tm 0 Tc ET EMC EMC BT /P <>BDC For land the 800 needs 1372 meters or 4,501.26 feet. ET /P <>BDC EMC /P <>BDC /P <>BDC ET The 737-800 has a maximum fuel capacity of 6,875 gallons, which it carries in fuel tanks in its wings, as seen here, and in a fuel tank located underneath the passenger cabin's midsection. EMC (39,270)Tj EMC BT /P <>BDC EMC /P <>BDC /P <>BDC /P <>BDC 0 Tc 9 0 0 9 425.1913 434.8898 Tm BT 9 0 0 9 551.4784 797.8898 Tm EMC 6 0 0 6 277.7064 757.9528 Tm BT [(T)95.9(o)0( do)12(wnload mor)10(e than 1,200)]TJ BT (25,160)Tj BT BT (0.0121)Tj ET /P <>BDC ET ET /P <>BDC 7 0 0 7 387.0932 309.9528 Tm /P <>BDC ET BT EMC 7 0 0 7 507.7893 408.7654 Tm .008 Tc /P <>BDC 7 0 0 7 474.3564 606.9528 Tm ( )Tj BT 7 0 0 7 82.2047 518.9528 Tm ET 7 0 0 7 124.1242 397.7654 Tm 9 0 0 9 215.4313 71.8898 Tm ET ( )Tj ET BT BT 7 0 0 7 379.3969 89.7654 Tm BT EMC 9 0 0 9 53.8582 445.8898 Tm /GS1 gs BT /P <>BDC -.01 Tc /P <>BDC EMC EMC 7 0 0 7 427.7291 320.9528 Tm BT /P <>BDC ET ( )Tj -.01 Tc BT ET EMC EMC 7 0 0 7 427.7291 188.9528 Tm EMC /P <>BDC ( )Tj 9 0 0 9 53.8578 236.8898 Tm EMC ET 6 0 0 6 547.0496 701.9528 Tm