737 800 fuel capacity pounds

8 0 0 8 319.1147 771.9528 Tm 9 0 0 9 552.9554 357.8898 Tm ( )Tj -.02 Tc ET BT ET 7 0 0 7 354.6933 199.7654 Tm ( )Tj /P <>BDC 6.5 0 0 6.5 433.3069 545.9529 Tm .008 Tc /P <>BDC 0 Tc EMC ( )Tj /P <>BDC ET EMC /P <>BDC ET (between the A320ceo and A320neo. EMC BT EMC BT /P <>BDC BT BT BT ET /P <>BDC ( )Tj BT /P <>BDC 6.5 0 0 6.5 178.4573 722.9529 Tm /P <>BDC 0 Tc EMC Why has Boeing maintained its designation to be B737, despite the latest B737 bears little resemblance to the original variant of the B737? ET ET EMC 10 0 0 10 137.0323 771.9528 Tm BT ( )Tj /P <>BDC /P <>BDC 0 Tc EMC /P <>BDC EMC 0 Tc BT EMC EMC /P <>BDC 7 0 0 7 230.7317 298.9528 Tm EMC 7 0 0 7 363.2711 386.9528 Tm 0 J 0 j 5 w 10 M [] 0 d 6.5 0 0 6.5 397.9138 722.9529 Tm BT ( )Tj 6.5 0 0 6.5 192.41 598.9529 Tm 7 0 0 7 535.5029 397.7654 Tm /P <>BDC /P <>BDC /P <>BDC EMC BT BT EMC /P <>BDC (369-383)Tj BT (2,899)Tj /P <>BDC /GS1 gs ET ET /P <>BDC BT EMC EMC ET 7 0 0 7 507.7893 166.7654 Tm BT (2,517)Tj /P <>BDC ET EMC 7 0 0 7 87.8179 144.7654 Tm /F1 1 Tf 8 0 0 8 365.7704 633.9528 Tm 0 Tc ET 9 0 0 9 53.8582 577.8898 Tm 0 Tc BT ( )Tj /P <>BDC /P <>BDC EMC 0 Tc W n /P <>BDC EMC BT EMC ET ET q ( )Tj 7 0 0 7 158.74 342.7654 Tm EMC /P <>BDC ET BT EMC /P <>BDC /P <>BDC EMC EMC /P <>BDC ET /P <>BDC -.02 Tc ( )Tj ET /GS2 gs ET 7 0 0 7 344.1175 595.7654 Tm /P <>BDC 6 0 0 6 178.2463 729.9528 Tm /P <>BDC BT BT 7 0 0 7 321.6356 100.9528 Tm (CFM56-5B3/P)Tj ET EMC 7 0 0 7 247.7395 331.7654 Tm (0.0133)Tj BT ET .014984 841.89 609.45 -841.89 re BT EMC ET EMC 7 0 0 7 82.8504 265.9528 Tm EMC EMC 6.5 0 0 6.5 534.5352 624.9529 Tm .023 .567 .626 rg EMC /P <>BDC ET ET 0 Tc BT [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ BT (average 0.06 cents per ASM advantage for)Tj 0 Tc automatically moved back to OFF after one minute. /P <>BDC BT (CFM56-5B4/P)Tj (l)Tj -.02 Tc EMC /P <>BDC ( )Tj BT 6 0 0 6 320.3167 757.9528 Tm [(SS)-9.1(U)8(E)]TJ EMC BT EMC BT 630,000 pounds (285,763 kg) Fuel capacity: 53,611 gallons (203,129 L) Range: 7,800 statute miles: Wing span: 195 feet, 8 inches (59.64 m) Length: 231 feet, 10 inches (70.66 m) Height: /P <>BDC /P <>BDC 9 0 0 9 369.892 93.8898 Tm 518.74 0 l 0 Tc /P <>BDC 7 0 0 7 380.2788 265.7654 Tm ( )Tj /P <>BDC 7 0 0 7 36.8504 749.9528 Tm ET EMC ET EMC EMC ET ET (136)Tj ( )Tj EMC EMC EMC ET /P <>BDC -.01 Tc (0.0115)Tj /GS2 gs /P <>BDC /P <>BDC ET BT /P <>BDC 9 0 0 9 394.0157 368.8898 Tm /TT2 1 Tf ET -.02 Tc ( )Tj 9 0 0 9 408.1889 324.8898 Tm EMC EMC /GS1 gs ( )Tj ET 7 0 0 7 387.0159 463.9528 Tm EMC -.02 Tc ET EMC ( )Tj ET ET 9 0 0 9 425.1967 775.8898 Tm 7 0 0 7 554.7883 111.7654 Tm ET 7 0 0 7 37.0536 518.9528 Tm (1,454)Tj ET /F1 1 Tf ( )Tj 9 0 0 9 68.3339 544.8898 Tm ET 9 0 0 9 215.4409 412.8898 Tm 9 0 0 9 394.0237 170.8898 Tm /P <>BDC /P <>BDC /P <>BDC EMC /P <>BDC ET [(BOS-SE)-13.9(A)]TJ (150)Tj ET EMC /F6 1 Tf EMC (A320neo)Tj ET ET 9 0 0 9 394.0157 126.8898 Tm /P <>BDC ( )Tj EMC /P <>BDC ET .498 .4095 .5623 .1043 v [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ BT ( )Tj BT EMC ET ET Seating in the 737 was a result of the design when moving the engines underneath the wings. EMC /P <>BDC ET BT /P <>BDC BT (214)Tj BT BT (2,516)Tj EMC /P <>BDC ET EMC (737-800W)Tj EMC BT EMC ET EMC ET EMC /P <>BDC 10 0 0 10 54.3039 794.2914 Tm [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ EMC BT BT BT EMC ET I am looking for some spec information in more detail for a project 7 0 0 7 277.3936 463.9528 Tm /P <>BDC 9 0 0 9 394.0157 170.8898 Tm (104)Tj (MTOW. ( )Tj 0 Tc ET /P <>BDC 5.25 0 0 5.25 64.5461 11.5129 Tm ET ( )Tj ET (34,650)Tj ET EMC ( )Tj (977)Tj -.02 Tc ( )Tj /P <>BDC EMC .023 .567 .626 rg (0.0115)Tj ( )Tj BT EMC BT BT (-59)Tj ET BT ET ( )Tj 9 0 0 9 394.0315 280.8898 Tm EMC BT ( )Tj q 1 0 0 1 394.016 747.971 cm 0 0 m EMC EMC (483)Tj -.02 Tc EMC EMC BT ET ( )Tj BT ( )Tj 10 0 0 10 425.05 814.1973 Tm /P <>BDC EMC EMC ( )Tj ( )Tj (20)Tj /P <>BDC BT 0 Tc 7 0 0 7 554.7883 133.7654 Tm /P <>BDC /P <>BDC /P <>BDC EMC EMC -.02 Tc /P <>BDC BT EMC 7 0 0 7 141.7322 320.9528 Tm 9 0 0 9 394.0157 500.8898 Tm (A320neos aircraft interior design and)Tj BT EMC /P <>BDC BT ( )Tj ET 0 Tc EMC 0 Tc 9 0 0 9 215.4313 225.8898 Tm ( )Tj ET ( )Tj ( )Tj fuel pumps were running in high ambient temperatures with empty or almost empty BT /P <>BDC ( )Tj W n EMC 7 0 0 7 380.2788 430.7654 Tm ET /P <>BDC /P <>BDC EMC 9 0 0 9 36.8583 423.8898 Tm /P <>BDC (which is BOS-LAX, whereas the 737-800)Tj EMC ET ET ET EMC /P <>BDC -.01 Tc aux tanks to push the aux fuel into the centre tank. EMC /P <>BDC .023 .567 .626 rg EMC ET 7 0 0 7 37.6993 89.9528 Tm 0 Tc /P <>BDC I think in the table you are talking about the range where payload is limited by MTOW. EMC BT BT Slats, flaps and Fuselage skin areas primarily loaded in tension Aluminium alloy 2024 (Aluminium and copper), Wing lower skin Aluminium alloy 7055 (Aluminium, zinc, magnesium and copper), Wing ribs, Frames, stringers, keel and floor beams Aluminium alloy 7075 (Aluminium and zinc), Spars, beams and Wing upper skin Aluminium alloy 7178 (Aluminium, zinc, magnesium and copper), Landing gear beam Aluminium alloy 7175 (Aluminium, zinc, magnesium and copper), Hi. BT BT EMC EMC ET )Tj EMC /P <>BDC 7 0 0 7 554.7883 661.7654 Tm EMC 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 7 0 0 7 490.8321 265.7654 Tm ET ( )Tj -.01 Tc EMC EMC /P <>BDC /TT2 1 Tf 7 0 0 7 70.8101 441.9528 Tm (1A26-powered aircraft that is used in this)Tj BT EMC 9 0 0 9 53.8582 412.8898 Tm EMC (2,900)Tj Q 7 0 0 7 387.0932 166.9528 Tm 7 0 0 7 380.2788 298.7654 Tm 7 0 0 7 439.2087 419.9528 Tm ( )Tj ( )Tj Q ET 9 0 0 9 518.0203 170.8898 Tm BT EMC (-61)Tj ( )Tj -.02 Tc ET BT -.02 Tc 7 0 0 7 473.8245 78.9528 Tm BT EMC 6.5 0 0 6.5 192.0331 676.9529 Tm ET BT BT 7 0 0 7 37.6993 210.9528 Tm ET BT EMC ET ET BT /P <>BDC EMC ( )Tj /P <>BDC /P <>BDC /P <>BDC BT ET BT EMC BT EMC /P <>BDC 9 0 0 9 232.438 137.8898 Tm ET BT /P <>BDC 7 0 0 7 490.7815 265.9528 Tm /P <>BDC /P <>BDC (aircraft again in the future. /P <>BDC ET EMC BT /F4 1 Tf (34,650)Tj BT EMC /P <>BDC EMC EMC BT (146,300)Tj /P <>BDC BT EMC /P <>BDC ET ( )Tj EMC BT EMC Maximum zero fuel weight (kg) 70 990: Standard fuel capacity (litres) 25 800: Performance; Range with max payload (km) 6 500: Cruise speed (km/h) 840: Maximum operating altitude (m) 12 000: Engines: CFMI LEAP-1B, 2 x 26790-29310 lb: /P <>BDC ( )Tj /P <>BDC /P <>BDC ( )Tj 10 0 0 10 55.0104 814.1973 Tm endobj /P <>BDC ET 9 0 0 9 53.8582 60.8898 Tm ET ET /P <>BDC BT BT BT 7 0 0 7 363.2711 111.9528 Tm BT EMC /P <>BDC ET EMC BT 9 0 0 9 53.8582 247.8898 Tm /P <>BDC 7 0 0 7 141.7322 430.9528 Tm ET /P <>BDC BT 9 0 0 9 487.056 434.8898 Tm (11,593)Tj 0 Tc 7 0 0 7 124.1242 595.7654 Tm BT 6.5 0 0 6.5 534.5352 585.9529 Tm 9 0 0 9 53.8338 192.8898 Tm EMC /P <>BDC 0 Tc The New Midsized Airplane. ET .151 .147 .15 rg ( )Tj ET EMC EMC EMC BT BT ET BT /P <>BDC /P <>BDC 199,158 Litres: . ET 0 Tc 28.5749 0 TD ET /P <>BDC ET BT -.02 Tc ET /P <>BDC (a cost index, which is a more cost-efficient)Tj ET (increase in engine efficiency to offer)Tj ET /P <>BDC BT /P <>BDC EMC 6.5 0 0 6.5 397.1339 676.9529 Tm 7 0 0 7 193.1059 485.9528 Tm 0 Tc .014984 841.89 609.45 -841.89 re BT /P <>BDC BT ( )Tj ET EMC -.02 Tc /P <>BDC 9 0 0 9 394.0315 742.8898 Tm /P <>BDC EMC To date, two 737's, 737-400 HS-TDC of updated to ensure the accuracy of VNAV speeds, buffet margin and max altitude. /P <>BDC ( )Tj 6.5 0 0 6.5 549.8557 663.9529 Tm BT BT ( )Tj 6 0 0 6 442.408 771.9528 Tm 7 0 0 7 536.3849 628.7654 Tm BT 7 0 0 7 491.392 672.9528 Tm /P <>BDC BT 7 0 0 7 37.0536 661.9528 Tm BT EMC EMC )Tj ET (Therefore this evaluation will focus on)Tj This is universally considered to be the .661 .752 .896 rg /P <>BDC -.01 Tc 0 Tc ET EMC ET ET /P <>BDC ET ET BT -.02 Tc -.01 Tc -.02 Tc [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ ET /P <>BDC -.02 Tc EMC BT BT EMC Aircraft have been NGS provisioned since l/n 1935 and it has been installed since l/n 2620 onwards. /P <>BDC 7 0 0 7 536.3849 210.7654 Tm EMC 9 0 0 9 53.8578 38.8898 Tm EMC /P <>BDC (The three main operational costs for)Tj 9 0 0 9 394.0157 357.8898 Tm EMC ET 7 0 0 7 258.2805 727.7654 Tm ET 7 0 0 7 474.3564 716.9528 Tm ET I started of using with this image. EMC EMC BT EMC EMC EMC EMC 7 0 0 7 141.7322 375.9528 Tm EMC ET BT 7 0 0 7 124.1242 298.7654 Tm BT /P <>BDC /P <>BDC ET EMC EMC /P <>BDC .014984 841.89 609.45 -841.89 re ET 6.5 0 0 6.5 176.1172 558.9529 Tm EMC BT ( )Tj ( )Tj BT BT ( )Tj 9 0 0 9 181.6136 456.8898 Tm 7 0 0 7 439.7405 584.9528 Tm EMC /P <>BDC 7 0 0 7 403.478 496.7654 Tm ET (variant. EMC EMC EMC (0.0123)Tj ET 7 0 0 7 554.7883 738.7654 Tm /P <>BDC 7 0 0 7 539.8962 705.9528 Tm 7 0 0 7 230.7317 188.9528 Tm ET EMC 9 0 0 9 533.576 236.8898 Tm .014984 841.89 609.45 -841.89 re 7 0 0 7 118.104 661.7654 Tm /P <>BDC /P <>BDC BT ET EMC S BT 7 0 0 7 337.6855 540.9528 Tm (CFM56-7B26)Tj EMC EMC 7 0 0 7 387.0932 265.9528 Tm ( )Tj /P <>BDC This compares)Tj EMC Im not sure I understand the question. EMC /P <>BDC (0.0137)Tj 7 0 0 7 380.2788 364.7654 Tm /P <>BDC higher. /P <>BDC 9 0 0 9 257.2834 214.8898 Tm 9 0 0 9 53.8338 49.8898 Tm /P <>BDC -.02 Tc /P <>BDC 9 0 0 9 36.8504 269.8898 Tm ET EMC -.02 Tc ET /P <>BDC ET (would be no additional holding required,)Tj EMC ET 7 0 0 7 490.5101 485.9528 Tm BT ( )Tj ET ET ET ET EMC 0 Tc /P <>BDC (2,347)Tj /P <>BDC 0 Tc EMC EMC EMC ET BT BT ET EMC ET BT ET ET BT ET EMC BT /P <>BDC BT (-61)Tj BT BT 7 0 0 7 337.6855 386.9528 Tm ET ( )Tj BT ET BT 0 Tc ET (Recent improvements in cabin design)Tj ET ET ET 7 0 0 7 539.8962 639.9528 Tm ET EMC 7 0 0 7 403.478 562.7654 Tm S EMC /P <>BDC BT /P <>BDC EMC EMC BT /P <>BDC ET EMC /P <>BDC /F4 1 Tf /P <>BDC /P <>BDC ( )Tj 8 0 0 8 124.845 591.9528 Tm EMC EMC BT EMC BT EMC ET ET ET BT EMC ET BT BT BT BT EMC -.02 Tc The fuel was fed /P <>BDC (5.1:1)Tj 9 0 0 9 411.0097 423.8898 Tm ET BT EMC ET 0 Tc BT ET BT ( )Tj BT 9 0 0 9 79.8339 434.8898 Tm 7 0 0 7 279.1575 386.9528 Tm ET ET BT 0 Tc ET EMC (350-365)Tj BT ET /P <>BDC EMC ET /P <>BDC ET BT (A320neo)Tj 7 0 0 7 380.2788 606.7654 Tm ET ET /P <>BDC 0 Tc ET BT ( )Tj ( )Tj -.02 Tc BT 17 0 0 17 550.9253 758.6944 Tm ET 7 0 0 7 182.5706 342.9528 Tm /P <>BDC ( )Tj ET EMC /P <>BDC ( )Tj EMC .0161 Tc 9 0 0 9 394.0157 522.8898 Tm 0 Tc BT -.02 Tc 9 0 0 9 388.4178 49.8898 Tm ET (172,842)Tj /P <>BDC /P <>BDC /P <>BDC ( )Tj EMC - Non Perele - News Online, Hi, EMC (the A320ceo. 7 0 0 7 354.6933 507.7654 Tm EMC (20)Tj EMC ET 56.25 0 0 56.25 36.8583 489.8898 Tm /P <>BDC ( 2021)Tj ( )Tj ( )Tj 7 0 0 7 439.2087 210.9528 Tm ET BT 0 Tc EMC EMC 9 0 0 9 53.8338 137.8898 Tm BT (737-800W)Tj EMC /P <>BDC /P <>BDC ET /P <>BDC /P <>BDC blue VALVE OPEN lights similar to that on the crossfeed valve. 7 0 0 7 473.8245 386.9528 Tm ET ET /P <>BDC BT /P <>BDC /P <>BDC EMC /P <>BDC BT Wingspan: 112 feet, 7 inches BT 7 0 0 7 258.2805 496.7654 Tm /P <>BDC /P <>BDC EMC BT 0 Tc -.01 Tc 13 0 0 13 202.8899 533.8898 Tm ET ( )Tj ( )Tj ET BT h ET (operation the overflight and airport)Tj ET ET EMC BT BT BT (0.0142)Tj BT EMC ( )Tj ET ET /P <>BDC ET 9 0 0 9 36.8504 313.8898 Tm ( )Tj ET ET -.02 Tc 9 0 0 9 389.1758 522.8898 Tm ( )Tj 7 0 0 7 299.0601 375.9528 Tm BT BT EMC EMC EMC 8 0 0 8 164.9203 771.9528 Tm 7 0 0 7 379.3969 243.7654 Tm 0 Tc ET ET ET -1.2026 -5.3154 -.8984 -5.2108 -.5848 -4.9925 c ET /P <>BDC ET ET /P <>BDC 7 0 0 7 387.0932 199.9528 Tm ET BT (737-8)Tj W n 9 0 0 9 411.0181 49.8898 Tm BT EMC EMC 9 0 0 9 561.4773 753.8898 Tm BT -.01 Tc (A321ceo)Tj /P <>BDC EMC 7 0 0 7 338.6433 397.7654 Tm (21)Tj /P <>BDC ( )Tj BT /P <>BDC BT 7 0 0 7 427.7291 67.9528 Tm 7 0 0 7 354.7351 694.7654 Tm ET EMC )Tj 7 0 0 7 440.0906 441.9528 Tm 7 0 0 7 279.1575 705.9528 Tm -.02 Tc EMC BT EMC /P <>BDC /P <>BDC q ET ET 0 Tc This is equivalent to)Tj [(737 M)-8.1(A)-24.9(X-8:)]TJ ( )Tj BT -.02 Tc -.02 Tc BT ( )Tj 7 0 0 7 199.5784 298.7654 Tm BT /P <>BDC EMC 9 0 0 9 215.4313 313.8898 Tm /P <>BDC BT BT (A320ceo)Tj ( )Tj BT EMC 9 0 0 9 215.4409 500.8898 Tm (0.0160)Tj 518.735 0 l ET EMC 9 0 0 9 68.0314 467.8898 Tm EMC EMC /P <>BDC /P <>BDC BT 7 0 0 7 315.5217 573.7654 Tm It is)Tj ( )Tj /GS1 gs EMC 7 0 0 7 387.0159 507.9528 Tm ET BT ET /P <>BDC EMC EMC ( )Tj /P <>BDC 6.5 0 0 6.5 54.2794 735.9529 Tm 10.486 7.6165 l ET ( )Tj 8 0 0 8 488.4333 760.7654 Tm 9 0 0 9 194.7833 236.8898 Tm ET ( )Tj BT EMC BT 0 Tc BT BT (31,416)Tj ( )Tj ET (170)Tj BT 6.5 0 0 6.5 116.0238 624.9529 Tm /P <>BDC ( )Tj ET ( )Tj 9 0 0 9 196.8605 115.8898 Tm Production has run from 1998 to present day. EMC EMC ET 7 0 0 7 387.0932 78.9528 Tm /P <>BDC EMC EMC EMC BT .0161 Tc ET -.02 Tc [(T)53.9(r)10(acked distance - nm)]TJ 0 Tc /P <>BDC 8 0 0 8 99.8582 771.7654 Tm 9 0 0 9 545.537 390.8898 Tm /P <>BDC EMC -.02 Tc -.02 Tc ET EMC BT 9 0 0 9 53.8338 170.8898 Tm ET EMC 9 0 0 9 215.4409 401.8898 Tm EMC BT -.02 Tc BT /P <>BDC ( )Tj BT EMC ET /P <>BDC S ( )Tj /P <>BDC EMC -.02 Tc 9 0 0 9 394.0315 621.8898 Tm -.02 Tc BT /P <>BDC /P <>BDC The A320neo in this study)Tj EMC /P <>BDC (influence the payloads carried and the)Tj EMC 9 0 0 9 204.483 104.8898 Tm 7 0 0 7 337.9444 89.9528 Tm 9 0 0 9 394.0157 236.8898 Tm [(Aircr)10(aft)]TJ /P <>BDC BT EMC BT EMC 6.5 0 0 6.5 480.4 650.9529 Tm EMC [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ 7 0 0 7 37.5838 639.9528 Tm ( )Tj /P <>BDC ( )Tj ET ET 1 i -.02 Tc ( )Tj ET BT /P <>BDC /P <>BDC ( )Tj ( )Tj /P <>BDC 9 0 0 9 411.0097 335.8898 Tm ET /P <>BDC BT EMC (174,165lbs, an MLW of 148,592lbs, and a)Tj ET )Tj EMC EMC ( )Tj Irkut MC-21, Russias homegrown modern airliner. /P <>BDC EMC ET 7 0 0 7 439.2087 309.9528 Tm /P <>BDC EMC ET /P <>BDC /P <>BDC BT 7 0 0 7 37.6993 309.9528 Tm /P <>BDC 9 0 0 9 199.3527 390.8898 Tm BT The classics have 5 dripsticks in each wing tank and none in the centre ( )Tj ET /P <>BDC (4,773)Tj EMC 9 0 0 9 195.3413 181.8898 Tm ET BT (planned for each aircraft type. EMC 13 0 0 13 36.8504 412.8898 Tm (economics of the aircraft types with more)Tj )Tj ET 9 0 0 9 418.1167 335.8898 Tm /P <>BDC [(AS)29(M)21(s)]TJ BT 9 0 0 9 383.6398 709.8898 Tm 7 0 0 7 199.5784 199.7654 Tm BT EMC ET 7 0 0 7 321.6356 276.9528 Tm ( )Tj EMC 9 0 0 9 536.6833 500.8898 Tm ET 7 0 0 7 491.4046 199.9528 Tm -.02 Tc 7 0 0 7 363.2711 441.9528 Tm EMC 7 0 0 7 445.7203 11.5129 Tm 0 Tc EMC ( )Tj 7 0 0 7 230.7317 386.9528 Tm ET 7 0 0 7 158.74 364.7654 Tm EMC 7 0 0 7 321.6356 232.9528 Tm 0 Tc BT ( )Tj ET Boeing supplied 10,574 since initial development as of 2020. EMC 7 0 0 7 337.7614 144.7654 Tm ET ET EMC ET EMC /P <>BDC (follow in their footsteps, having already)Tj 8 0 0 8 334.994 619.9528 Tm EMC

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