BT BT [(BOS-S)8.1(TL)]TJ EMC ET EMC /P <>BDC (136)Tj ET (831)Tj BT ( )Tj 9 0 0 9 394.0315 533.8898 Tm ( )Tj (114)Tj ET EMC BT BT /P <>BDC 7 0 0 7 518.4953 89.9528 Tm EMC BT /P <>BDC BT EMC EMC ET ET BT (1,825)Tj BT /P <>BDC /P <>BDC On the Digital Sunburst fuel gauges, pressing the "Qty test" button will /P <>BDC -.01 Tc ET ET BT ET EMC 9 0 0 9 569.8068 511.8898 Tm ET (The aircraft is limited by its fuel tank)Tj ET ET /F1 1 Tf /P <>BDC Worlds Most Popular Passenger Airplane for $ 89.1 million. 5.25 0 0 5.25 73.853 11.5132 Tm /P <>BDC EMC 0 Tc /P <>BDC ( )Tj EMC BT /P <>BDC BT BT ET (150)Tj EMC ET (l)Tj BT /P <>BDC BT 7 0 0 7 241.5317 716.9528 Tm 0 Tc /P <>BDC BT .661 .752 .896 rg 9 0 0 9 527.3853 709.8898 Tm EMC BT (737-9)Tj 7 0 0 7 473.8245 287.9528 Tm ET ET -.02 Tc BT 232.441 656.608 340.813 -625.44 re ( )Tj 7 0 0 7 337.6855 529.9528 Tm /P <>BDC ( )Tj /GS1 gs ET EMC /F6 1 Tf /P <>BDC ET (0.0119)Tj (translate into increased range and)Tj BT BT 7 0 0 7 89.3229 342.7654 Tm 9 0 0 9 183.8303 324.8898 Tm 7 0 0 7 88.196 11.5129 Tm 9 0 0 9 36.8504 412.8898 Tm BT (A320neo)Tj 7 0 0 7 429.4931 122.9528 Tm EMC 6 0 0 6 403.0689 729.9528 Tm ET BT ( )Tj /P <>BDC ET BT ET ET BT BT (. -.02 Tc ET -.01 Tc EMC 7 0 0 7 355.3163 221.7654 Tm (which could reduce this difference. 7 0 0 7 355.3163 342.7654 Tm 5.25 0 0 5.25 123.5367 11.5132 Tm It provides code tables for aerodromes, air operators including the world's major airlines and for ICAO and IATA codes for aircraft. 7 0 0 7 187.0858 298.9528 Tm BT ( )Tj The fwd and aft tanks are switched off when the /GS2 gs BT FQIS accuracy with digital indicators: +/- 2.5 % 9 0 0 9 190.1653 456.8898 Tm /P <>BDC 7 0 0 7 473.8245 122.9528 Tm ( )Tj /P <>BDC 8 0 0 8 141.7322 771.9528 Tm 0 Tc BT 8 0 0 8 507.842 760.7654 Tm ET BT 6.5 0 0 6.5 244.2974 545.9529 Tm ET /P <>BDC EMC ( )Tj EMC BT 7 0 0 7 258.2805 419.7654 Tm -.02 Tc In payload scenario 1 the)Tj 0 Tc ( The time spent in potential holding)Tj (CFM56-7B26)Tj ET BT BT ( )Tj EMC auxiliary tank at the forward end of the aft hold; these were available in )Tj EMC ET ( )Tj 9 0 0 9 189.1673 137.8898 Tm ET BT /P <>BDC BT ET EMC /P <>BDC ET (170)Tj /P <>BDC /P <>BDC ( )Tj EMC /P <>BDC 0 Tc 9 0 0 9 36.8504 214.8898 Tm (166,090)Tj ET ( )Tj /P <>BDC ( )Tj /P <>BDC 0 Tc EMC EMC /P <>BDC BT ET (34,650)Tj .0081 Tc BT (CFM LEAP-1B28B1s thrust rating to)Tj EMC /P <>BDC 8 0 0 8 315.034 760.7654 Tm BT ET ( )Tj 9 0 0 9 549.0056 412.8898 Tm ET BT 9 0 0 9 411.0097 181.8898 Tm 7 0 0 7 337.9444 617.9528 Tm BT BT BT BT /P <>BDC EMC ET /P <>BDC EMC ET /P <>BDC ( )Tj BT Can we suggest copying and pasteing Aluminium alloy 7055 basis value into your search engine of choice? aux (AA) and fwd aux (FA) respectively. 7 0 0 7 490.8321 166.7654 Tm BT EMC /P <>BDC ( )Tj /P <>BDC /P <>BDC BT /P <>BDC 5 0 obj ( )Tj /P <>BDC EMC -.01 Tc 7 0 0 7 445.619 540.7654 Tm ET 6 0 0 6 246.6462 743.9528 Tm /P <>BDC /P <>BDC ET BT than the main wing tanks. 0 841.89 609.449 -841.89 re EMC EMC 7 0 0 7 54.7071 397.7654 Tm (distances, and alternate airports are shown)Tj ( )Tj BT (72,450)Tj BT ( )Tj EMC /P <>BDC /P <>BDC -.02 Tc /P <>BDC /P <>BDC ET EMC BT ( )Tj ET ET 6 0 0 6 195.6824 659.9528 Tm /P <>BDC (34,650)Tj ( )Tj BT /P <>BDC 7 0 0 7 354.6933 276.7654 Tm BT 13 0 0 13 127.1464 456.8898 Tm /P <>BDC ET ET 9 0 0 9 213.7241 467.8898 Tm ( )Tj 7 0 0 7 316.0679 309.7654 Tm /P <>BDC ( )Tj EMC EMC BT ET exacerbating the imbalance. 10 0 0 10 408.34 814.1973 Tm ET BT BT /P <>BDC /P <>BDC ET -.01 Tc ( )Tj ET 9 0 0 9 565.8376 577.8898 Tm ET BT ET (34,650)Tj 9 0 0 9 194.7833 236.8898 Tm (10)Tj -.01 Tc /P <>BDC 9 0 0 9 511.9579 335.8898 Tm EMC 0 Tc 8 0 0 8 43.6039 745.9528 Tm (573)Tj ET /P <>BDC ET 6 0 0 6 309.4742 687.9528 Tm EMC BT ( )Tj BT (737-800 is more efficient with up to a)Tj /P <>BDC BT ET EMC ( )Tj BT /P <>BDC /P <>BDC BT ET BT EMC ( )Tj 7 0 0 7 508.4124 694.7654 Tm BT BT ET EMC BT 6 0 0 6 258.3167 715.9528 Tm /P <>BDC ET The fuel flow indication is integrated over time to calculate the fuel used for each engine. EMC EMC ET /P <>BDC ET ET 7 0 0 7 429.157 727.9528 Tm ( )Tj (31,416)Tj 7 0 0 7 387.0932 210.9528 Tm BT EMC EMC (burn and cost per seat and per ASM than)Tj (737-9)Tj 0 Tc /GS1 gs -.02 Tc 10 0 0 10 422.8 814.1973 Tm 7 0 0 7 67.798 11.5132 Tm EMC ( )Tj ( )Tj BT 9 0 0 9 555.1066 434.8898 Tm ET /F6 1 Tf 7 0 0 7 403.478 617.7654 Tm BT /P <>BDC .41 .161 .508 rg /P <>BDC ( )Tj ET ( )Tj BT /GS1 gs ET (31,416)Tj 9 0 0 9 229.6141 390.8898 Tm EMC /P <>BDC (The improvement in fuel cost per ASM)Tj ET Hi Anna-Maria, /P <>BDC /P <>BDC BT ET ET EMC EMC 0 Tc BT 7 0 0 7 535.5029 705.7654 Tm ET /P <>BDC ET 0 Tc /P <>BDC ET 7 0 0 7 355.5753 584.7654 Tm 7 0 0 7 37.6993 100.9528 Tm ET EMC -.01 Tc EMC ( )Tj ET BT 7 0 0 7 429.157 507.9528 Tm EMC /P <>BDC -.02 Tc 1 i ET BT /P <>BDC EMC EMC ET ET 9 0 0 9 36.8504 434.8898 Tm ( )Tj EMC .151 .147 .15 rg Therefore, the Boeing 777-200 can carry 24,125 more gallons of fuel than the Boeing 737-800. ET -.02 Tc /P <>BDC /P <>BDC BT ET 9 0 0 9 195.6833 115.8898 Tm /P <>BDC (he 737 MAX returned to revenue)Tj ( )Tj ( )Tj ( )Tj 6 0 0 6 339.8239 701.9528 Tm /P <>BDC ET 7 0 0 7 535.5029 221.7654 Tm 0 Tc (737-8)Tj BT ET 9 0 0 9 384.8177 445.8898 Tm ET ( )Tj /P <>BDC ET ET (146,550)Tj ET 1 i It is recognised that most)Tj EMC ( )Tj BT EMC /P <>BDC 9 0 0 9 394.0315 368.8898 Tm ET /P <>BDC 7 0 0 7 258.5394 100.7654 Tm BT W n EMC ET EMC ET (404)Tj 9 0 0 9 36.8504 522.8898 Tm (- USG)Tj ( )Tj ( )Tj 7 0 0 7 474.7064 133.9528 Tm -.02 Tc /P <>BDC 7 0 0 7 114.6416 298.9528 Tm ET BT 9 0 0 9 232.4217 500.8898 Tm (CFM56-5B3/P)Tj BT ET 7 0 0 7 338.6433 309.7654 Tm 7 0 0 7 539.8962 716.9528 Tm ET EMC ( )Tj BT /P <>BDC 9 0 0 9 170.6722 104.8898 Tm ( )Tj ET 6.5 0 0 6.5 295.7432 545.9529 Tm 0 Tc ET EMC BT 0 Tc ( )Tj /P <>BDC EMC /P <>BDC EMC BT /P <>BDC EMC 7 0 0 7 427.7291 342.9528 Tm ( )Tj ET ET BT (0.0157)Tj BT /P <>BDC 7 0 0 7 473.8245 111.9528 Tm BT EMC EMC /P <>BDC ( )Tj 0 Tc EMC ( )Tj BT EMC EMC (carried - lbs)Tj /P <>BDC ET 7 0 0 7 474.3564 496.9528 Tm ( )Tj )Tj BT /P <>BDC ET BT /P <>BDC ET Leaving a fuel pump on with a low pressure light Irkut MC-21, Russias homegrown modern airliner. 9 0 0 9 68.0314 401.8898 Tm 0 Tc BT (39,270)Tj ET ET 19.843 0 l ET ( )Tj ( )Tj EMC BT BT /P <>BDC (39,270)Tj (second payload scenario using the 85%)Tj BT BT 7 0 0 7 518.4953 320.9528 Tm ET [(M)-13.9(KE/84)]TJ /P <>BDC ET /P <>BDC 9 0 0 9 68.3339 544.8898 Tm BT /P <>BDC 7 0 0 7 363.0612 430.9528 Tm BT 0 Tc /P <>BDC EMC EMC ET 7 0 0 7 54.7071 100.7654 Tm EMC EMC EMC 9 0 0 9 379.0889 291.8898 Tm /P <>BDC ET /P <>BDC BT /P <>BDC /P <>BDC BT /P <>BDC 7 0 0 7 355.3163 331.7654 Tm ET 0 Tc (37,416)Tj BT ( )Tj BT BT ET /P <>BDC EMC [(SS)-9.1(U)8(E)]TJ ET BT 9 0 0 9 195.3413 181.8898 Tm /P <>BDC 0 841.89 609.449 -841.89 re 7 0 0 7 299.0601 342.9528 Tm BT /P <>BDC ET 9 0 0 9 394.0157 522.8898 Tm ET ( )Tj ( )Tj 9 0 0 9 36.8504 390.8898 Tm 0 Tc BT -.02 Tc EMC BT /P <>BDC ( )Tj (and bypass ratio of 12.5:1 as the A320neo;)Tj EMC 8 0 0 8 334.994 633.9528 Tm /P <>BDC EMC ( )Tj EMC EMC /P <>BDC BT EMC 0 Tc [(v)21(ariant)]TJ 9 0 0 9 215.4313 467.8898 Tm 7 0 0 7 537.267 133.7654 Tm EMC 9 0 0 9 207.8168 445.8898 Tm (The 737-8 has a block fuel burn)Tj EMC ET ET EMC Q /P <>BDC ET BT /P <>BDC EMC EMC ( )Tj /P <>BDC endobj q 1 0 0 1 232.438 95.878 cm 0 0 m (A320ceo)Tj /P <>BDC /F4 1 Tf ET 6.5 0 0 6.5 449.7715 565.9529 Tm (737-8)Tj /P <>BDC EMC ET 7 0 0 7 163.8846 11.5132 Tm 7 0 0 7 141.7322 661.9528 Tm EMC /P <>BDC EMC 9 0 0 9 53.8578 225.8898 Tm ET ET BT ET 7 0 0 7 337.6855 419.9528 Tm (category. EMC /P <>BDC /P <>BDC /P <>BDC BT )Tj /F4 1 Tf /P <>BDC ( )Tj EMC /P <>BDC ET 9 0 0 9 193.0013 302.8898 Tm (831)Tj ( )Tj /P <>BDC (50,800)Tj EMC 7 0 0 7 158.74 727.7654 Tm BT ( )Tj /P <>BDC (The comparison of the A320ceo)Tj /P <>BDC -.01 Tc BT /P <>BDC /F1 1 Tf ( )Tj -.02 Tc )Tj EMC /P <>BDC ET 7 0 0 7 445.619 639.7654 Tm 9 0 0 9 532.082 247.8898 Tm /P <>BDC /P <>BDC ET (The flight tracks and cruise altitudes)Tj ET BT 7 0 0 7 54.7071 364.7654 Tm /P <>BDC EMC BT EMC (will take into account the additional)Tj EMC ( )Tj Additional Aircraft accessibility information is available online for customers with disabilities.. Aircraft specifications. EMC ( )Tj BT /P <>BDC /P <>BDC EMC 8 0 0 8 241.2609 771.9528 Tm ET ( )Tj EMC ( )Tj /P <>BDC ( )Tj EMC ET EMC EMC (485)Tj BT ( )Tj /P <>BDC /P <>BDC EMC ET ( )Tj ( )Tj EMC EMC ET BT ( )Tj /P <>BDC 7 0 0 7 439.2087 265.9528 Tm ET BT ET EMC BT EMC 9 0 0 9 196.4663 137.8898 Tm /P <>BDC EMC /P <>BDC ET (170)Tj ET EMC 0 Tc ET BT 6 0 0 6 561.1918 687.9528 Tm /P <>BDC /P <>BDC ET EMC 6 0 0 6 309.5222 701.9528 Tm /P <>BDC -.02 Tc /P <>BDC ( )Tj ET ET -.02 Tc /P <>BDC 6.5 0 0 6.5 243.4784 624.9529 Tm EMC /P <>BDC BT 9 0 0 9 546.1516 445.8898 Tm BT 6 0 0 6 55.0668 659.9528 Tm EMC ( )Tj ET /P <>BDC BT Jump to Specification Table Boeing 737 Original and Boeing 737 Classic. ( )Tj EMC ( )Tj /P <>BDC (0.0131)Tj BT EMC /P <>BDC ET What was the Super Sonic Transport (SST) Concorde plane?? ET 9 0 0 9 394.0123 489.8898 Tm BT 9 0 0 9 215.433 324.8898 Tm 7 0 0 7 37.0536 617.9528 Tm ET 7 0 0 7 125.6292 683.7654 Tm BT /P <>BDC /P <>BDC /P <>BDC /P <>BDC ET ( )Tj (4,631)Tj BT )Tj /P <>BDC BT 7 0 0 7 518.4953 386.9528 Tm BT 7 0 0 7 233.5248 78.9528 Tm ET /P <>BDC 7 0 0 7 387.0932 232.9528 Tm 0 Tc ET /F4 1 Tf 7 0 0 7 141.7322 166.9528 Tm /F4 1 Tf EMC 8 0 0 8 276.7109 633.9528 Tm ET /P <>BDC /P <>BDC BT /P <>BDC 7 0 0 7 130.1443 122.7654 Tm battery bus but have a dedicated battery to ensure that there is always BT ET /F2 1 Tf ET BT (408)Tj EMC 6 0 0 6 519.1239 687.9528 Tm BT 7 0 0 7 131.6494 375.7654 Tm BT 7 0 0 7 294.4014 188.7654 Tm EMC ET 9 0 0 9 229.6141 478.8898 Tm /P <>BDC BT EMC BT EMC ET 9 0 0 9 232.4217 71.8898 Tm 7 0 0 7 247.7395 232.7654 Tm (208)Tj ET BT 8 0 0 8 531.7294 771.9529 Tm (5.7:1)Tj ET (1,938)Tj ET ( )Tj ( )Tj 7 0 0 7 535.5029 496.7654 Tm (charges combined with the time-related)Tj 10 0 0 10 36.8504 814.1973 Tm ET (\(see table, page 19\))Tj BT /P <>BDC EMC -.02 Tc /P <>BDC /P <>BDC ( )Tj 7 0 0 7 365.035 606.9528 Tm (ratio of 5.1:1. EMC ET /P <>BDC EMC /P <>BDC 0 Tc ET BT ( )Tj /P <>BDC 13 0 0 13 202.8899 533.8898 Tm )Tj (A320ceo)Tj /P <>BDC /P <>BDC ET /P <>BDC ET ( )Tj ( )Tj ET BT EMC ET ET /P <>BDC 7 0 0 7 539.8962 738.9528 Tm EMC /P <>BDC ET EMC (off weight \(MTOW\) of 171,961lbs, a)Tj BT 9 0 0 9 541.8752 775.8898 Tm /P <>BDC EMC (1,089)Tj EMC ( )Tj EMC EMC ET (72,450)Tj ET ET ET ET /P <>BDC ET /P <>BDC 7 0 0 7 299.0601 287.9528 Tm 7 0 0 7 338.3085 320.9528 Tm 9 0 0 9 215.4313 49.8898 Tm ( )Tj /P <>BDC /P <>BDC /P <>BDC BT BT BT EMC /P <>BDC ET BT BT ( )Tj /P <>BDC EMC (\(Toronto Pearson\) sector, to 2,730nm for)Tj [(AIRL)8.1(INE & AIR)7.1(CRAF)-12.9(T)18.1( OPERA)56.9(T)-8.1(ION)-13.9(S)]TJ BT 8 0 0 8 38.4438 619.9528 Tm 7 0 0 7 379.3969 133.7654 Tm (271,728)Tj BT /P <>BDC 9 0 0 9 68.0314 522.8898 Tm ET ET EMC ET BT BT ET 7 0 0 7 554.7883 243.7654 Tm /F6 1 Tf /P <>BDC BT 6 0 0 6 215.3128 743.9528 Tm (payload on any sector in this evaluation. /P <>BDC 0 Tc 7 0 0 7 366.0641 716.9528 Tm ( )Tj ET BT ( )Tj W* n (City-pair)Tj /P <>BDC EMC (1,272)Tj /P <>BDC ET 0 Tc /P <>BDC EMC (900ER and 737-9, A320ceo and A320neo,)Tj (Federal Aviation Administration) have cleaned up their act and made the MAX as safe an airliner as its predecessors. /F6 1 Tf EMC /P <>BDC 6.5 0 0 6.5 549.8557 650.9529 Tm /P <>BDC ET ET /P <>BDC /P <>BDC (\(see table, this)Tj (significant enough that operating the)Tj 7 0 0 7 535.5029 540.7654 Tm 6.5 0 0 6.5 430.0114 565.9529 Tm EMC BT (25,307)Tj ET BT .41 .161 .508 rg /P <>BDC BT /P <>BDC EMC EMC BT EMC BT BT 6.5 0 0 6.5 480.5169 565.9529 Tm EMC ET EMC BT BT the years. (A320neo:)Tj EMC BT -.02 Tc ( )Tj BT /P <>BDC /P <>BDC 5.25 0 0 5.25 64.5461 11.5129 Tm BT EMC 7 0 0 7 54.7071 485.7654 Tm BT /P <>BDC BT ET EMC BT (289)Tj EMC BT BT ET EMC 9 0 0 9 183.72 797.8898 Tm EMC /P <>BDC 7 0 0 7 491.7142 188.7654 Tm /P <>BDC 9 0 0 9 36.8504 148.8898 Tm 7 0 0 7 508.6712 430.7654 Tm -.01 Tc (payload reduction. EMC EMC EMC 7 0 0 7 536.3849 67.7654 Tm EMC BT EMC ][F$, c;9M$ C[\SU~s#4B#g"DH V6S[_t099J'Nbqur((h\Yf'urV(nYYW6V*f]+ 0 Tc EMC 7 0 0 7 456.2165 100.7654 Tm ET ET (282)Tj EMC ET EMC (136)Tj /P <>BDC /P <>BDC EMC ( )Tj BT (which has the lowest fuel burn rate per)Tj 7 0 0 7 70.1644 540.9528 Tm ET 7 0 0 7 337.9444 606.9528 Tm /P <>BDC The NTSB ET /P <>BDC EMC ( )Tj ET 7 0 0 7 355.3163 188.7654 Tm 9 0 0 9 551.0015 291.8898 Tm /GS2 gs ( )Tj /P <>BDC Right centre tank fuel pump on the forward wall of the on the Simmonds gauges or error codes 1,3 and 6 on the Smiths gauges. ET /P <>BDC /GS1 gs EMC BT EMC .151 .147 .15 rg ( )Tj I am looking for the radius of the fuselage specifically the cargo door. EMC EMC This leaves about 20,000 kg (45,000 lbs) for passengers, cargo, and crew. ( )Tj ET BT (aircraft types; and with no additional cargo)Tj EMC (A321neo carry the same passenger)Tj 6 0 0 6 327.5828 701.9528 Tm 7 0 0 7 241.5317 485.9528 Tm -.02 Tc BT EMC /P <>BDC 0 Tc 7 0 0 7 456.2165 78.7654 Tm These transfer fuel from the centre tank into tank 1 at a minimum rate of 100kg/hr, although usually nearer 200kg/hr. 9 0 0 9 394.0123 181.8898 Tm ET EMC BT BT Boeing made ET BT (give the A321neo a range of up to)Tj (A321neo)Tj 9 0 0 9 103.7478 390.8898 Tm BT 7 0 0 7 338.3085 309.9528 Tm ( )Tj ET BT BT BT /P <>BDC -.01 Tc (214,730)Tj ( )Tj 9 0 0 9 561.5176 522.8898 Tm BT BT (A320neo)Tj BT /Artifact <>BDC /P <>BDC ET EMC BT EMC 0 Tw ET (0.0123)Tj /P <>BDC BT ET ( )Tj )Tj ET ( )Tj -.005 Tc /P <>BDC /P <>BDC EMC 0 Tc -.02 Tc 9 0 0 9 53.8582 698.8898 Tm EMC (earlier counterpart. BT /P <>BDC BT wiring in tanks, proximity to hot air-conditioning or pneumatic systems, etc. 9 0 0 9 36.8504 115.8898 Tm 13 0 0 13 338.1052 82.8898 Tm ET EMC /P <>BDC BT /P <>BDC /P <>BDC BT 53.858 30.994 518.735 773.858 re 9 0 0 9 394.0315 71.8898 Tm BT /P <>BDC ET ET EMC BT (. /P <>BDC EMC EMC 7 0 0 7 187.0858 100.9528 Tm 7 0 0 7 386.4701 89.9528 Tm (CFM56-7B26)Tj EMC (0.0140)Tj 7 0 0 7 354.7351 694.7654 Tm EMC ( )Tj /P <>BDC BT /P <>BDC ( )Tj EMC ET (landing\) fuel burns for seven of the 14)Tj (for the purposes of this performance)Tj EMC /P <>BDC BT /P <>BDC BT BT 7 0 0 7 116.3631 11.5132 Tm (cost compared to fuel. ET /P <>BDC Boeing 737 Interior. BT BT 7 0 0 7 116.3631 11.5132 Tm EMC /F6 1 Tf BT BT )Tj 0 Tc ET EMC 9 0 0 9 89.5187 104.8898 Tm -.02 Tc 9 0 0 9 377.4586 676.8898 Tm BT 7 0 0 7 141.7322 342.9528 Tm (977)Tj (37,653)Tj BT ET ( )Tj ET EMC How Many Flight Attendants Are on a Plane. /P <>BDC EMC ET BT EMC EMC 0 Tc ET /P <>BDC EMC EMC /GS1 gs 9 0 0 9 535.2501 522.8898 Tm EMC ET BT /P <>BDC EMC EMC BT (not been used for the A321ceo against the)Tj ( )Tj 7 0 0 7 362.3891 287.9528 Tm BT 9 0 0 9 183.0113 214.8898 Tm ET ( )Tj /OC /MC854 BDC 7 0 0 7 187.0858 496.9528 Tm ( )Tj -.01 Tc 0 Tc BT 9 0 0 9 425.1913 291.8898 Tm ET ET 9 0 0 9 394.0237 489.8898 Tm The data for our pages are sourced from various locations, ranging from airliner manufacturer websites, technical airliner manuals etc. ET ET EMC BT ( )Tj /P <>BDC /P <>BDC ET ( )Tj 9 0 0 9 252.9543 170.8898 Tm /P <>BDC -.02 Tc BT EMC EMC EMC 9 0 0 9 551.8838 324.8898 Tm BT ( )Tj EMC ET /P <>BDC ET /P <>BDC (burns. ( )Tj BT /P <>BDC 9 0 0 9 544.6834 126.8898 Tm -1.2026 -5.3154 -.8984 -5.2108 -.5848 -4.9925 c 9 0 0 9 343.6557 148.8898 Tm 0 Tc BT 6.5 0 0 6.5 499.8375 545.9529 Tm EMC BT 0 Tc ET 0 Tc BT EMC ( )Tj BT EMC 7 0 0 7 241.2727 474.9528 Tm EMC BT /P <>BDC ( )Tj ET (based on the cost index set is different, it)Tj ET BT ( )Tj EMC ET EMC W n 0 Tc ( )Tj /P <>BDC ET 0 Tc ET BT BT 737-600/-700/-800/-900 with densitometer: ET ( )Tj (. ( )Tj 9 0 0 9 566.9717 236.8898 Tm ( )Tj /P <>BDC I am looking to build a prototype of Boeing 737 for numerical simulation purpose. BT 7 0 0 7 508.4124 342.7654 Tm /P <>BDC 5.25 0 0 5.25 492.6848 11.5129 Tm 0 Tc /F7 1 Tf BT BT (industry is 210 US cents per USG for Jet A-)Tj 9 0 0 9 347.6589 478.8898 Tm ET )Tj 9 0 0 9 53.8578 445.8898 Tm ( )Tj EMC 9 0 0 9 79.8339 489.8898 Tm BT EMC EMC S ET ET -.02 Tc 8 0 0 8 520.6337 771.7654 Tm 8 0 0 8 302.5117 675.9528 Tm BT /P <>BDC /P <>BDC ET (compared to the CFM56-7B-powered 737-)Tj EMC EMC EMC BT BT ET 8 0 0 8 124.845 577.9528 Tm (number of available seat-miles \(ASM\))Tj EMC ( )Tj EMC /P <>BDC BT ET EMC 7 0 0 7 108.6215 738.9528 Tm BT ET BT [(OEW/DO)7.1(W - lbs)]TJ EMC ET [(CFM L)17.1(E)-8.1(AP-1A26)]TJ /Artifact <>BDC /P <>BDC EMC ET /P <>BDC (ASM of 0.55 to 0.88 cents per ASM)Tj ET EMC 7 0 0 7 456.2165 397.7654 Tm BT BT ( )Tj EMC ET /P <>BDC 0 Tc EMC <> ( )Tj In-flight, the GW must be periodically /P <>BDC /P <>BDC )Tj EMC /F7 1 Tf ET BT EMC EMC BT EMC /P <>BDC 7 0 0 7 101.0963 287.9528 Tm ET ET BT 7 0 0 7 363.2711 276.9528 Tm (0.0177)Tj /P <>BDC [(7)-33(3)8(7-8)]TJ 9 0 0 9 169.3109 643.8898 Tm /P <>BDC /P <>BDC .7 -.5345 .9114 -1.2305 y 7 0 0 7 445.619 474.7654 Tm (A321ceo)Tj /P <>BDC ET /P <>BDC 9 0 0 9 529.8783 621.8898 Tm EMC BT /P <>BDC ( )Tj ( )Tj 6.5 0 0 6.5 330.4406 565.9529 Tm BT 9 0 0 9 566.5558 544.8898 Tm /P <>BDC ET (impact on the fuel cost per ASM. (used is 16/30/114, giving a seat count of)Tj (68.3 inches and a bypass ratio of up to)Tj BT BT 9 0 0 9 54.9417 794.1039 Tm [(OM)8.1(M)-12.9(E)-24.9(R)7.1(C)8.1(E)]TJ BT EMC ET ET For more detailed information on the Boeing 737 Specs, you can click on this Boeing 737 PDF. (Improvements introduced to the)Tj ET BT ( )Tj EMC BT ET /P <>BDC ET 7 0 0 7 294.4014 716.7654 Tm ( )Tj ET 0 Tc BT /P <>BDC EMC 9 0 0 9 252.5351 214.8898 Tm ET [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ ET ET EMC ET /P <>BDC 7 0 0 7 362.3891 364.9528 Tm /P <>BDC I think in the table you are talking about the range where payload is limited by MTOW. 7 0 0 7 314.6398 485.7654 Tm BT /P <>BDC /P <>BDC /P <>BDC 9 0 0 9 536.0613 49.8898 Tm EMC thanks for stopping by. ET /P <>BDC /P <>BDC BT EMC EMC BT ET 9 0 0 9 53.8578 390.8898 Tm BT EMC EMC BT 7 0 0 7 387.0932 243.9528 Tm BT ET EMC ET EMC -.02 Tc 9 0 0 9 544.8903 698.8898 Tm BT /P <>BDC [(A3)24.9(20ceo v)12.9(ersus 7)-33(3)8.1(7-800 )]TJ 7 0 0 7 59.2108 11.5129 Tm ( )Tj /P <>BDC ET On older aircraft the trimmers were accessible from the BT BT /P <>BDC ( )Tj EMC BT EMC EMC 0 Tc ( )Tj ET -.02 Tc EMC ( )Tj EMC /P <>BDC EMC %PDF-1.4 8 0 0 8 136.8677 745.9528 Tm wheel well - NG's only. ET BT 7 0 0 7 294.4014 463.7654 Tm BT EMC ET [(E)-24.9(SAD - nm )]TJ 7 0 0 7 492.5963 617.7654 Tm 9 0 0 9 68.0314 302.8898 Tm BT /P <>BDC 9 0 0 9 190.1186 247.8898 Tm -.02 Tc 0 Tc BT ET (LRC; the same as the primary sector. 9 0 0 9 370.2844 489.8898 Tm ET EMC The Boeing 737 is designed to fill the smaller jet airliners space over a given range of seats. ( )Tj ET ( )Tj .014984 841.89 609.45 -841.89 re 7 0 0 7 158.74 419.7654 Tm ET (192)Tj /P <>BDC /P <>BDC EMC ET /P <>BDC EMC BT EMC (737 MAX 10s \(737-10\) ight)Tj BT BT 9 0 0 9 347.4891 203.8898 Tm (network. -.02 Tc BT h EMC ET /P <>BDC BT ET 7 0 0 7 294.4014 331.7654 Tm (1,272)Tj ( )Tj ET (0.0137)Tj EMC ( )Tj ET -.02 Tc 9 0 0 9 526.2638 401.8898 Tm 9 0 0 9 53.8582 49.8898 Tm EMC ET (This is chosen to represent a typical airline)Tj ET 0 Tc EMC 7 0 0 7 258.2805 562.7654 Tm ET EMC ( )Tj BT ET EMC EMC ET BT /P <>BDC /P <>BDC 9 0 0 9 411.0181 368.8898 Tm EMC /P <>BDC /P <>BDC (1,581)Tj EMC /P <>BDC ET BT .41 .161 .508 RG 6 0 0 6 346.935 771.9528 Tm /P <>BDC /P <>BDC endstream (the two scenarios are detailed )Tj 9 0 0 9 411.0097 49.8898 Tm (would be no additional holding required,)Tj BT 9 0 0 9 215.4313 346.8898 Tm EMC BT 9 0 0 9 53.8338 368.8898 Tm (163)Tj ET -.02 Tc BT /P <>BDC 9 0 0 9 394.0237 258.8898 Tm /P <>BDC EMC ET ET /P <>BDC EMC (146,550)Tj Wingspan: 112 feet, 7 inches ( )Tj BT 9 0 0 9 384.7818 137.8898 Tm BT 9 0 0 9 53.8582 742.8898 Tm (CFM56-5B4/P)Tj 0 Tc ET ET /P <>BDC BT ET EMC ET EMC /F6 1 Tf 7 0 0 7 344.1175 584.7654 Tm ET /P <>BDC BT EMC (409,650)Tj 7 0 0 7 204.0935 133.7654 Tm 7 0 0 7 99.8582 199.7654 Tm BT 7 0 0 7 491.4046 122.9528 Tm /P <>BDC EMC .964 .834 .406 rg BT ET /P <>BDC BT 7 0 0 7 297.632 606.9528 Tm BT 7 0 0 7 43.6039 540.9528 Tm BT BT ( )Tj /P <>BDC 7 0 0 7 141.7322 243.9528 Tm /P <>BDC [(looks at the performance of eight Airbus and Boeing narr)10(o)12(wbody types)]TJ /P <>BDC ( )Tj /P <>BDC 9 0 0 9 374.5629 82.8898 Tm (A320neo)Tj ( )Tj ET EMC 0 Tc ET 9 0 0 9 372.8879 412.8898 Tm ET ( )Tj EMC BT ET EMC BT ET ET (170)Tj ET EMC Thai Airways on 3 Mar 2001 and 737-300 EI-BZG operated by Philippine Airlines ET /P <>BDC EMC ET /P <>BDC EMC BT 7 0 0 7 354.6933 529.7654 Tm /P <>BDC BT ET 0 Tc /P <>BDC ET 7 0 0 7 294.4014 705.7654 Tm .023 .567 .626 rg /P <>BDC EMC ET /P <>BDC BT EMC EMC 6.5 0 0 6.5 192.0331 676.9529 Tm EMC [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ EMC /P <>BDC EMC (CFM56-5B4/P)Tj /P <>BDC /P <>BDC ET BT BT 6.5 0 0 6.5 64.6596 722.9529 Tm EMC 7 0 0 7 241.5317 639.9528 Tm BT ET /P <>BDC 7 0 0 7 37.5838 650.9528 Tm /P <>BDC EMC -.005 Tc BT EMC EMC /P <>BDC /P <>BDC /P <>BDC BT EMC BT ET EMC EMC BT ET BT EMC 0 Tw 8 0 0 8 38.4438 731.9528 Tm 5.25 0 0 5.25 549.1047 11.5132 Tm EMC (369-383)Tj ET BT /P <>BDC -.02 Tc ET 9 0 0 9 394.0157 335.8898 Tm ( )Tj BT (34,650)Tj BT ( )Tj EMC ET BT ET (space, thereby freeing up more floor area)Tj /F6 1 Tf ( )Tj 0 Tc 9 0 0 9 425.1967 775.8898 Tm ET BT BT 7 0 0 7 490.5101 562.9528 Tm BT ( )Tj 7 0 0 7 53.8582 11.5132 Tm 7 0 0 7 107.1165 573.9528 Tm [(v)21(ariant)]TJ Blended Winglets provide a simple and elegant solution to measurably improving aircraft fuel burn, managing operating costs and extending the economic life of an aircraft. (35,112)Tj /P <>BDC ET 7 0 0 7 387.0932 133.9528 Tm /P <>BDC BT BT EMC /P <>BDC /P <>BDC BT BT BT ET EMC 7 0 0 7 404.3599 672.7654 Tm /P <>BDC The use of composite materials in the 737 Next Gen or even the 737 Max is quite conservative. EMC /P <>BDC 9 0 0 9 36.8504 71.8898 Tm BT .014984 824.882 572.583 17.008 re EMC (to higher bypass ratios provide better)Tj ( )Tj ET BT BT ET 7 0 0 7 404.3599 661.7654 Tm /P <>BDC BT BT (T)Tj BT BT ( )Tj EMC 5 0 0 5 92.725 11.5132 Tm fuel pumps were running in high ambient temperatures with empty or almost empty (configurations for these aircraft types. 19.848 0 l (passengers; thereby giving the A321ceo a)Tj BT 8 0 0 8 53.9012 749.9529 Tm 7 0 0 7 445.619 738.7654 Tm ET -.02 Tc the aircraft data bus. /P <>BDC 0 Tc EMC (A320ceo:)Tj BT ( )Tj 6 0 0 6 61.517 701.9528 Tm 0 Tc 6 0 0 6 451.7374 673.9528 Tm ( )Tj (A320ceo and A320neo in this study. ET ET q BT /P <>BDC /F7 1 Tf ( )Tj ET EMC ET /P <>BDC BT EMC BT Q /P <>BDC EMC ET /P <>BDC BT 9 0 0 9 202.684 357.8898 Tm ( )Tj ( )Tj 7 0 0 7 337.6855 67.9528 Tm ( )Tj 9 0 0 9 246.595 302.8898 Tm EMC 8 0 0 8 225.1837 675.9528 Tm /P <>BDC BT 8 0 0 8 122.6593 760.7654 Tm EMC ( )Tj (. -.02 Tc 7 0 0 7 241.5317 298.9528 Tm EMC /P <>BDC (150)Tj BT ET (136)Tj 6.5 0 0 6.5 296.4841 663.9529 Tm BT ET /P <>BDC BT BT each aircraft is sourced from different places. /GS2 gs ET /P <>BDC (37,653lbs )Tj EMC 9 0 0 9 202.845 357.8898 Tm BT 0 Tc ( )Tj 6.5 0 0 6.5 328.6662 585.9529 Tm (192 seats. ET ET )Tj (makes a flight-for-flight comparison)Tj EMC ET /F4 1 Tf /P <>BDC 0 Tc 7 0 0 7 297.632 507.9528 Tm /P <>BDC /P <>BDC ( )Tj -.01 Tc ( )Tj /P <>BDC ET ET BT 0 Tc (CFM56-5B3/P)Tj EMC this question can have so many answers depending on the conditions, such as weight, air density, required speed etc. BT EMC Q ET ET EMC ( )Tj /P <>BDC 7 0 0 7 427.7291 199.9528 Tm /P <>BDC EMC BT ET 7 0 0 7 314.6398 507.7654 Tm ET EMC ET -.02 Tc /P <>BDC 6.5 0 0 6.5 426.4819 702.9529 Tm <>stream ET EMC ET EMC BT ET EMC ( )Tj /P <>BDC 0 Tc BT ET 7 0 0 7 444.737 144.7654 Tm EMC ET ET 0 Tc 6.5 0 0 6.5 499.4541 735.9529 Tm ET ET /P <>BDC ET EMC 7 0 0 7 536.3849 111.7654 Tm /P <>BDC BT 0 Tc 9 0 0 9 53.8582 236.8898 Tm EMC ( )Tj