BT BT ( )Tj /P <>BDC 9 0 0 9 543.767 93.8898 Tm 0 Tc (The improvement in fuel cost per ASM)Tj ET (2,732)Tj 0 Tc 7 0 0 7 362.3891 309.9528 Tm (4,000nm with maximum passenger)Tj -.02 Tc 56 0 0 56 36.8606 622.1944 Tm BT 9 0 0 9 36.8504 269.8898 Tm 9 0 0 9 394.0157 346.8898 Tm BT /P <>BDC EMC /P <>BDC ET ET 7 0 0 7 387.0932 265.9528 Tm -.02 Tc EMC /P <>BDC 9 0 0 9 411.0181 203.8898 Tm EMC EMC (737-8)Tj EMC ET ( )Tj /P <>BDC BT EMC ET BT 0 Tc /P <>BDC /P <>BDC 0 Tc EMC /P <>BDC ( )Tj /P <>BDC ET 9 0 0 9 394.0123 555.8898 Tm ET EMC EMC -.02 Tc -.02 Tc 9 0 0 9 522.1112 247.8898 Tm BT BT (977)Tj BT BT ET 0 Tc ( )Tj ET ET .151 .147 .15 rg EMC ET EMC -.01 Tc 7 0 0 7 294.4014 441.7654 Tm /P <>BDC The reductions in fuel burn also)Tj /P <>BDC (0.0112)Tj 7 0 0 7 297.632 507.9528 Tm EMC /P <>BDC (2,516)Tj 7 0 0 7 297.632 606.9528 Tm 7 0 0 7 337.6855 408.9528 Tm ET EMC BT ET EMC EMC 9 0 0 9 68.0314 467.8898 Tm ( )Tj /P <>BDC ET EMC 6 0 0 6 55.0668 743.9528 Tm /P <>BDC 7 0 0 7 141.7322 683.9528 Tm EMC 9 0 0 9 181.0402 335.8898 Tm BT ET ET ET ET BT ET BT BT /P <>BDC (37,653)Tj 9 0 0 9 554.0057 566.8898 Tm ET /P <>BDC EMC ET BT /F4 1 Tf 6.5 0 0 6.5 295.7432 545.9529 Tm EMC /P <>BDC 7 0 0 7 554.7883 133.7654 Tm /P <>BDC /P <>BDC The maximum declarable fuel capacity for tech log, nav log, etc is 16,200kgs for 3-Tank Classics, 20,800kgs for NG/MAX's and up to 37,712kgs for BBJ's depending upon how many tanks the customer has specified (max 12). /P <>BDC /P <>BDC BT ET EMC 9 0 0 9 207.0841 203.8898 Tm 0 Tc [(www)60.7(.aircr)9.7(aft-commerce.com)]TJ /P <>BDC /P <>BDC BT -.02 Tc ( )Tj /P <>BDC 0 Tc ET S 7 0 0 7 37.6993 430.9528 Tm ( )Tj It is simply an 800 with certain modifications that might have been stipulated by the customer airliner. ET 9 0 0 9 532.8774 346.8898 Tm EMC ET ( )Tj ET (410)Tj -.02 Tc (category. EMC BT /GS2 gs [(737 M)-8.1(A)-24.9(X-8)]TJ EMC EMC ET EMC /P <>BDC (The A320neo has a 0.55-0.69 cents per)Tj BT ET EMC /P <>BDC 9 0 0 9 423.3885 401.8898 Tm 0 Tc 'http':'https';if(!d.getElementById(id)){js=d.createElement(s);js.id=id;js.src=p+'://platform.twitter.com/widgets.js';fjs.parentNode.insertBefore(js,fjs);}}(document, 'script', 'twitter-wjs'); The (A321ceo)Tj ET EMC [(E)-7.8(P)16.1(T)9(E)-13.9(MBE)-16.9(R)]TJ /P <>BDC EMC BT BT /P <>BDC 6 0 0 6 481.8528 701.9528 Tm /P <>BDC BT EMC BT ( )Tj BT ET ET (\(see table,)Tj 378 0 0 271.8 -.30716 30.902 cm /P <>BDC EMC ( )Tj BT ( )Tj EMC 5.25 0 0 5.25 515.3989 11.5129 Tm BT /F6 1 Tf /P <>BDC BT (The A320neo family and 737 MAX)Tj 8 0 0 8 302.5117 703.9528 Tm BT ET 0 Tc /P <>BDC -.02 Tc ET BT endstream (\(see table, this page\))Tj BT BT /P <>BDC ET ET 9 0 0 9 215.4409 500.8898 Tm A unique variant in the 737 family is the 737 Convertible which is both a passenger and cargo airliner. /OC /MC828 BDC -.02 Tc EMC ET EMC ET ET 7 0 0 7 403.478 221.7654 Tm 7 0 0 7 258.2805 441.7654 Tm BT EMC EMC Q (34,650)Tj Fokker 100, the Netherlands regional jet. /P <>BDC EMC ET BT /P <>BDC /P <>BDC (1.111)Tj 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. /P <>BDC EMC BT BT BT EMC ( )Tj /P <>BDC EMC 7 0 0 7 403.478 683.7654 Tm ET (and the 737 MAX family with the CFM)Tj BT (hour and per mile reduces . /P <>BDC BT BT 7 0 0 7 445.7203 11.5129 Tm 6.5 0 0 6.5 228.7846 545.9529 Tm BT BT 0 Tc EMC Engine size EMC -.02 Tc /P <>BDC ( )Tj /P <>BDC ET /P <>BDC ( )Tj (The aircraft are examined on the basis)Tj /P <>BDC /OC /MC200 BDC [(737-900E)-33(R)]TJ ET EMC BT /P <>BDC ( )Tj 6 0 0 6 214.7788 729.9528 Tm 9 0 0 9 229.6064 126.8898 Tm /OC /MC186 BDC /P <>BDC 7 0 0 7 316.0679 331.7654 Tm 9 0 0 9 232.4217 401.8898 Tm BT ET EMC EMC /P <>BDC ET /P <>BDC /P <>BDC 0 Tc ( )Tj BT ET EMC /P <>BDC /P <>BDC BT ET ( )Tj EMC EMC ET EMC -.02 Tc /P <>BDC .559 .331 .619 rg /P <>BDC BT 0 Tc [(P)11(assenger payload - lbs )]TJ /P <>BDC BT EMC 7 0 0 7 82.8504 67.9528 Tm BT 304.725 420.96 m ET /P <>BDC ET BT BT EMC ET 0 Tc BT BT /Im3 Do EMC ET ET 7 0 0 7 54.7071 661.7654 Tm 8 0 0 8 136.4919 591.9528 Tm ( )Tj ET ( )Tj 6 0 0 6 425.0715 687.9528 Tm 10 0 0 10 37.304 794.2914 Tm BT /P <>BDC BT EMC ( )Tj 6 0 0 6 277.9402 687.9528 Tm EMC /P <>BDC /P <>BDC ( )Tj BT EMC EMC /P <>BDC ET (371,552)Tj ( )Tj EMC ET endobj BT I not sure what you mean by a and b basis allowable. /P <>BDC BT 0 Tc The same alternate airport was)Tj (some minor aerodynamic improvements)Tj EMC ET 7 0 0 7 379.3969 309.7654 Tm 7 0 0 7 54.7071 133.7654 Tm /P <>BDC ( )Tj BT ET ( )Tj BT /P <>BDC BT 7 0 0 7 429.157 529.9528 Tm For Example: .0081 Tc BT 9 0 0 9 360.5848 104.8898 Tm /P <>BDC /P <>BDC -.02 Tc 7 0 0 7 539.9176 11.5129 Tm BT BT EFVU(eufv7GWgw8HXhx)9IYiy*:JZjz m !1AQa"q2#BRbr3$4CS%cs5DT ET The)Tj 0 Tc BT ET /P <>BDC ( )Tj EMC EMC EMC BT (150)Tj BT BT ET 9 0 0 9 36.8504 269.8898 Tm /P <>BDC BT -.02 Tc (Block fuel)Tj (and bypass ratio of 12.5:1 as the A320neo;)Tj EMC /P <>BDC EMC /P <>BDC ( )Tj ET ( )Tj ET /P <>BDC (introduction of the newer aircraft types to)Tj EMC /P <>BDC BT BT 7 0 0 7 108.6215 364.9528 Tm 7 0 0 7 445.619 540.7654 Tm [(CFM L)17.1(E)-8.1(AP-1B27)]TJ BT BT (an OEW of 98,500lbs )Tj q 1 0 0 1 36.85 84.878 cm 0 0 m BT EMC ET BT BT EMC BT EMC ET (1,824)Tj (These results will allow a better)Tj ( )Tj .151 .147 .15 rg /P <>BDC /P <>BDC EMC ET BT 7 0 0 7 554.7883 375.7654 Tm /P <>BDC EMC ( )Tj ( )Tj /P <>BDC EMC BT ET (2,220)Tj /P <>BDC BT BT EMC (The comparison will be for eight)Tj ET (0.0141)Tj EMC EMC ET ET BT /P <>BDC 9 0 0 9 411.0097 412.8898 Tm EMC 0 Tc 7 0 0 7 158.74 716.7654 Tm 0 Tc ET (170)Tj EMC (The A321neo is offered to airlines with)Tj BT /P <>BDC 9 0 0 9 372.2987 181.8898 Tm ( )Tj /P <>BDC 8 0 0 8 258.7094 760.9528 Tm - Modern Airliners, A New Opportunity For Hydrogen is Aviation Aeronautics, A New Opportunity For Hydrogen is Aviation - Revolution-Green, Southwest CEO Says It's Safe to Fly Again. EMC BT EMC BT BT EMC EMC -.01 Tc (economy seats are at six-abreast. 7 0 0 7 427.7291 177.9528 Tm BT ( )Tj 0 Tc /P <>BDC -.02 Tc EMC ET ( )Tj (297,475)Tj -.01 Tc ET /P <>BDC /P <>BDC EMC 7 0 0 7 492.5963 584.7654 Tm These transfer fuel from the centre tank into tank 1 at a minimum rate of 100kg/hr, although usually nearer 200kg/hr. EMC 9 0 0 9 215.4409 412.8898 Tm ET /F1 1 Tf BT ET ET battery bus but have a dedicated battery to ensure that there is always BT BT BT BT 7 0 0 7 387.0159 727.9528 Tm ET BT -.02 Tc 7 0 0 7 82.2047 518.9528 Tm /P <>BDC ET 9 0 0 9 411.0181 82.8898 Tm ET BT 7 0 0 7 326.2278 727.9528 Tm 7 0 0 7 386.4701 89.9528 Tm 0 Tc ET 0 Tw ET ( )Tj ET /P <>BDC ET /F4 1 Tf /P <>BDC ET (34,650)Tj (374)Tj (the destination airports. ( )Tj ET EMC BT 8 0 0 8 354.3239 771.7654 Tm /P <>BDC /P <>BDC BT BT 7 0 0 7 337.6855 496.9528 Tm ET ET EMC (31,416lbs)Tj BT ET ( )Tj ( )Tj ( )Tj BT BT /P <>BDC (mainline US carriers like Alaska, American)Tj 9 0 0 9 207.2279 511.8898 Tm 9 0 0 9 36.8504 126.8898 Tm ( )Tj BT 7 0 0 7 241.2727 474.9528 Tm ET EMC 8 0 0 8 302.5117 577.9528 Tm -.02 Tc EMC EMC BT ET ET 7 0 0 7 108.6215 331.9528 Tm /P <>BDC ET (136)Tj BT EMC ( )Tj /P <>BDC EMC 10 0 0 10 52.0044 814.1973 Tm 9 0 0 9 545.1909 346.8898 Tm EMC ( )Tj /P <>BDC 0 Tc /P <>BDC /GS2 gs ET ( )Tj ( )Tj (2,042)Tj 7 0 0 7 539.9176 11.5129 Tm BT /P <>BDC BT (aircraft an economic advantage in terms of)Tj EMC BT ET 0 Tc (113,016)Tj (bypass ratio than the A320/321neo. (1A32)Tj EMC ET /P <>BDC /P <>BDC /P <>BDC EMC ET BT ( )Tj EMC ET BT ET ET 9 0 0 9 204.9907 467.8898 Tm /P <>BDC ( )Tj (A321ceo)Tj ET (136)Tj 7 0 0 7 554.7883 386.7654 Tm EMC BT /P <>BDC BT BT 7 0 0 7 258.2805 133.7654 Tm (39,270lbs)Tj 0 Tw ET -.02 Tc (35,112)Tj EMC -.02 Tc /P <>BDC ET -.02 Tc EMC BT BT ( )Tj /P <>BDC /P <>BDC ET ( )Tj (bypass ratio of 9.0:1. on the Simmonds gauges or error codes 1,3 and 6 on the Smiths gauges. /P <>BDC 7 0 0 7 99.8582 276.7654 Tm 9 0 0 9 394.0315 555.8898 Tm ET ET /P <>BDC ET EMC ET EMC /P <>BDC ET 6.5 0 0 6.5 471.1051 742.9529 Tm ET 7 0 0 7 82.2047 507.9528 Tm BT 7 0 0 7 439.2087 298.9528 Tm BT 7 0 0 7 535.5029 122.7654 Tm The aux tanks are located at [(P)11(ayload)]TJ EMC /P <>BDC ( )Tj -.02 Tc 9 0 0 9 546.4149 456.8898 Tm BT ( )Tj ET /P <>BDC /P <>BDC (35,112)Tj ET ET 5.25 0 0 5.25 55.7484 11.5132 Tm ET ET /P <>BDC ( )Tj ( The cruise speed and flight profile )Tj ET 7 0 0 7 338.3085 375.9528 Tm ( )Tj EMC 9 0 0 9 232.438 115.8898 Tm /P <>BDC 0 Tc (160-169)Tj BT ET EMC /P <>BDC /P <>BDC ET (planning software was allowed to optimise)Tj EMC EMC BT /P <>BDC ET 7 0 0 7 99.5912 683.9528 Tm ET 0 Tc /P <>BDC EMC 6.5 0 0 6.5 430.0114 565.9529 Tm BT /P <>BDC [(P)11(ayload scenario two)]TJ EMC 0 Tc ( )Tj /P <>BDC BT 9 0 0 9 196.8174 390.8898 Tm EMC Boeing made BT ET ET BT 7 0 0 7 537.7804 298.9528 Tm /P <>BDC /P <>BDC BT /P <>BDC 7 0 0 7 366.0641 672.9528 Tm ET /P <>BDC EMC /P <>BDC 7 0 0 7 294.4014 397.7654 Tm ET ( )Tj BT BT /P <>BDC ( )Tj ET EMC 7 0 0 7 403.478 496.7654 Tm /P <>BDC BT EMC BT 9 0 0 9 394.0157 566.8898 Tm /P <>BDC BT ET ET /P <>BDC EMC 63 0 obj ( )Tj 7 0 0 7 354.6933 617.7654 Tm ( )Tj EMC 7 0 0 7 99.8582 298.7654 Tm /P <>BDC BT 9 0 0 9 372.0688 324.8898 Tm /P <>BDC ET (To enable a comparison of the different)Tj ( )Tj BT /P <>BDC EMC BT five ground) under different ground and flight conditions to demonstrate the BT ET The FAA developed an in-flight gas sampling system, integrated with )Tj ( )Tj ( )Tj ( )Tj /GS2 gs /P <>BDC 0 Tc ( )Tj BT /P <>BDC q 1 0 0 1 505.328 82.247 cm 0 0 m ( )Tj -.02 Tc BT (propulsive efficiency. 7 0 0 7 315.5217 595.7654 Tm 9 0 0 9 229.6064 335.8898 Tm .41 .161 .508 RG /F1 1 Tf 0 Tc ( )Tj (. EMC -.02 Tc EMC ( )Tj ( )Tj EMC BT /P <>BDC /P <>BDC 9 0 0 9 68.0314 38.8898 Tm 10 0 0 10 230.6475 794.2914 Tm 848 0 obj BT BT (737-800W)Tj ( )Tj ET BT 5.25 0 0 5.25 549.1047 11.5132 Tm ( )Tj (follow in their footsteps, having already)Tj BT BT BT 9 0 0 9 535.511 379.8898 Tm ET ET EMC 8 0 0 8 394.0237 82.8898 Tm 0 Tc /GS2 gs EMC BT EMC 9 0 0 9 408.2047 489.8898 Tm /P <>BDC /P <>BDC EMC EMC BT 7 0 0 7 387.0159 661.9528 Tm 9 0 0 9 376.057 247.8898 Tm ET ET /P <>BDC /P <>BDC /P <>BDC -.02 Tc 6 0 0 6 258.3167 715.9528 Tm 7 0 0 7 82.8504 188.9528 Tm The charges are split by weight)Tj BT EMC In comparison, the fuel cost per)Tj ( )Tj ET /P <>BDC EMC /P <>BDC BT ET /P <>BDC EMC /P <>BDC 7 0 0 7 294.4014 419.7654 Tm 9 0 0 9 536.0613 49.8898 Tm EMC /P <>BDC 9 0 0 9 362.8235 401.8898 Tm (I)Tj 6.5 0 0 6.5 192.41 598.9529 Tm /P <>BDC 9 0 0 9 232.4217 489.8898 Tm (150)Tj ( )Tj /P <>BDC EMC EMC (150)Tj ( )Tj /P <>BDC BT BT (273,750)Tj EMC BT /F4 1 Tf EMC EMC -.02 Tc ET 9 0 0 9 536.024 533.8898 Tm ET EMC ET /P <>BDC 9 0 0 9 190.8846 379.8898 Tm 7 0 0 7 380.2788 364.7654 Tm 9 0 0 9 51.0236 302.8898 Tm (0.0115)Tj ET (170)Tj /P <>BDC BT /P <>BDC /P <>BDC /P <>BDC /P <>BDC ET 0 Tc EMC ET (136)Tj -.02 Tc ET /P <>BDC EMC (208-217)Tj ET /P <>BDC 9 0 0 9 53.8582 346.8898 Tm ET BT BT In-flight, the GW must be periodically -.01 Tc 9 0 0 9 538.0952 500.8898 Tm /P <>BDC EMC 8 0 0 8 136.5171 758.9528 Tm BT EMC 7 0 0 7 59.2108 11.5129 Tm (170)Tj It also boasts a 3,060 Nautical Mile or 5,667 Kilometers travel range. (800 is not as large as the difference)Tj ET EMC BT [(Summar)-33(y )]TJ /P <>BDC BT ET BT 8 0 0 8 136.4919 703.9528 Tm ET 0 Tc -.02 Tc /P <>BDC /P <>BDC BT /P <>BDC /P <>BDC /P <>BDC ET 0 Tc /F4 1 Tf -.02 Tc 9 0 0 9 394.0123 390.8898 Tm EMC 9 0 0 9 212.0769 71.8898 Tm EMC 7 0 0 7 491.4046 100.9528 Tm 7 0 0 7 475.2383 639.9528 Tm ET BT (It was assumed that all flights would)Tj 8 0 0 8 99.8582 771.7654 Tm 7 0 0 7 444.737 386.7654 Tm 9 0 0 9 411.0097 599.8898 Tm 0 Tc (2,800 -)Tj BT 7 0 0 7 204.0935 188.7654 Tm EMC ( )Tj BT ET ET 6.5 0 0 6.5 486.1525 722.9529 Tm ET /P <>BDC 6.5 0 0 6.5 244.0438 722.9529 Tm 0 Tc 6 0 0 6 371.479 757.9528 Tm BT -.02 Tc BT (10)Tj 0 Tc BT ET ET ( )Tj ( )Tj Can you please tell me where to look for the cabin height,width, seat height, width and door to door length. 9 0 0 9 178.1318 71.8898 Tm ( )Tj -.02 Tc (1,824)Tj BT ET EMC ET ET (CFM56-7B27B3)Tj EMC EMC EMC 7 0 0 7 89.3229 639.7654 Tm BT ( )Tj 7 0 0 7 508.4124 243.7654 Tm 7 0 0 7 196.5683 122.7654 Tm /P <>BDC ET ET BT 7 0 0 7 439.2087 122.9528 Tm ET /P <>BDC /P <>BDC 5.25 0 0 5.25 525.4061 11.5132 Tm /P <>BDC EMC BT BT BT /P <>BDC /P <>BDC EMC ( )Tj ( )Tj (146,300)Tj EMC [(737-900E)-33(R)]TJ EMC EMC (CFM56-7B26 engine on the heavier weight)Tj BT EMC ( )Tj ET BT EMC EMC 7 0 0 7 439.2087 67.9528 Tm 6 0 0 6 496.2633 673.9528 Tm EMC ET EMC )Tj EMC /P <>BDC 10 0 0 10 49.2604 814.1973 Tm [(A3)24.9(21ceo & A3)24.9(21neo )]TJ EMC /P <>BDC The 737-800 is used in airlines such as Aircal, Delta Air Lines, New York Air and United Airlines just to name a few. ET 9 0 0 9 232.4217 379.8898 Tm /P <>BDC (126,312)Tj /F1 1 Tf ET 9 0 0 9 68.0071 412.8898 Tm BT ( )Tj BT /P <>BDC EMC /P <>BDC /P <>BDC /P <>BDC 6 0 0 6 184.4741 687.9528 Tm ET ET ET ET -.02 Tc /P <>BDC BT 9 0 0 9 181.5424 71.8898 Tm -.02 Tc ET BT 9 0 0 9 194.4504 203.8898 Tm ( )Tj (passengers are carried on each of the four)Tj BT BT 9 0 0 9 53.8582 786.8898 Tm 0 Tc EMC /P <>BDC (3,443)Tj ET EMC EMC 9 0 0 9 534.395 599.8898 Tm 7 0 0 7 279.1575 133.9528 Tm <> EMC BT /P <>BDC ET /P <>BDC BT EMC 9 0 0 9 270.2513 93.8898 Tm ET ET EMC ET /P <>BDC BT ( )Tj ( )Tj EMC BT 6 0 0 6 513.0339 701.9528 Tm 7 0 0 7 60.6117 639.7654 Tm ( )Tj EMC EMC 28.5749 0 TD BT 6 0 0 6 519.1239 687.9528 Tm 7 0 0 7 242.0225 430.9528 Tm EMC /P <>BDC BT 7 0 0 7 537.7804 309.9528 Tm EMC /P <>BDC ( )Tj -.01 Tc 7 0 0 7 158.74 265.7654 Tm ET BT 0 Tc 7 0 0 7 259.1625 78.7654 Tm ( A)Tj ET BT EMC 7 0 0 7 440.0906 188.9528 Tm 7 0 0 7 364.1531 166.9528 Tm /P <>BDC EMC ET BT ET 6 0 0 6 466.3124 757.9528 Tm 9 0 0 9 377.4586 676.8898 Tm ET /P <>BDC (- USG)Tj ET ( )Tj