737 800 fuel capacity poundssouthwest flights from denver to slc today
BT 9 0 0 9 394.0123 258.8898 Tm ET /P <>BDC /P <>BDC /P <>BDC 0 Tc ET /P <>BDC ET /P <>BDC /P <>BDC (104)Tj Take-off Weight 154,500 lb (70,080 kg) Entertainment System: Full cabin Overhead screens 8 Stereo Music Channels Maximum Range: 3,365 nautical miles (6,225 km) Cargo: 966 cu ft (27.3 cu m) Typical Cruise Speed @ 35,000ft altitude 0.785 Mach . 7 0 0 7 491.392 573.9528 Tm -.02 Tc ET 0 Tc EMC BT 7 0 0 7 520.6108 628.9528 Tm ET 9 0 0 9 370.8228 302.8898 Tm (passengers and 163 passengers on the)Tj /P <>BDC .151 .147 .15 rg (342,312)Tj BT /P <>BDC 7 0 0 7 241.5317 232.9528 Tm (A321ceo)Tj (costs could almost double the per ASM)Tj ET EMC 304.725 420.96 m EMC (1,938)Tj ET BT 9 0 0 9 189.0772 115.8898 Tm /P <>BDC (20/29/143, giving a maximum capacity of)Tj BT /P <>BDC [(Aircr)10(aft types )]TJ ET BT ET ( )Tj /P <>BDC (the flight profile based on the cruise speed)Tj BT ( )Tj The 737-900ER's successor is set to be the MAX 10, which will have a maximum capacity of 230 passengers and can fly 3,300 nautical miles (narrowly beating its predecessor). ET ( )Tj ET /P <>BDC ( )Tj /P <>BDC ET ET /P <>BDC ( )Tj /P <>BDC EMC Each version in the 737 family fills a differ role. EMC ET 7 0 0 7 277.3936 166.9528 Tm 6 0 0 6 333.1569 743.9528 Tm 7 0 0 7 37.5838 144.9528 Tm S /P <>BDC 9 0 0 9 376.0986 324.8898 Tm 7 0 0 7 125.6292 584.7654 Tm EMC 9 0 0 9 232.4217 357.8898 Tm LO-Z wiring, Open or short circuit in a LO-Z to a tank unit, Calibration unit does not operate correctly. 6 0 0 6 475.3427 715.9528 Tm 9 0 0 9 532.082 247.8898 Tm 6 0 0 6 55.0668 687.9528 Tm ( )Tj ( )Tj ET EMC 7 0 0 7 387.0159 661.9528 Tm (37,653)Tj BT 0 Tc 0 Tc EMC ET EMC /P <>BDC EMC BT /P <>BDC ET 7 0 0 7 53.8582 452.7654 Tm /P <>BDC (1,272)Tj 9 0 0 9 258.18 60.8898 Tm Fuel burn in cruise for B737-800 is 5,511lbs/hr Fuel burn at idle of a CFM56 engine = 661lbs/hr, so for the half hour descent two engines burn through 661 Total fuel for a 2 hour flight is 16,753lbs 6 More answers below Teodor Negru Passioned about flight and the art of flying Author has 425 answers and 1.8M answer views 4 y BT -.02 Tc ET EMC (737-800W)Tj ( 2021)Tj ET ET ( )Tj EMC /P <>BDC /P <>BDC BT /P <>BDC 6.5 0 0 6.5 295.5027 565.9529 Tm /P <>BDC /P <>BDC 7 0 0 7 99.8582 672.7654 Tm ET ET EMC /P <>BDC BT ( )Tj ET ET EMC 7 0 0 7 338.6433 397.7654 Tm /P <>BDC 7 0 0 7 82.8504 166.9528 Tm /F4 1 Tf (load factor to provide a better evaluation)Tj ET EMC EMC 9 0 0 9 190.9763 38.8898 Tm /GS2 gs -.02 Tc EMC 7 0 0 7 241.5317 518.9528 Tm /P <>BDC ET ET Other)Tj BT ET BT BT BT -.02 Tc BT 1 i ET BT (34,650)Tj ( )Tj 7 0 0 7 230.7317 144.9528 Tm ET 304.725 420.96 m ( )Tj fuel and de-ice the fuel filter. BT 7 0 0 7 258.2805 67.7654 Tm 8 0 0 8 332.978 591.9528 Tm (151)Tj /P <>BDC BT (900ER\(W\) compared to the A321ceo in)Tj ( )Tj /P <>BDC Cheers Peter, Thanks, peter! 9 0 0 9 371.548 291.8898 Tm EMC /P <>BDC 7 0 0 7 430.039 628.9528 Tm ET 0 Tc 9 0 0 9 189.3204 324.8898 Tm BT -.02 Tc -.02 Tc /P <>BDC ET EMC BT 6.5 0 0 6.5 499.22 598.9529 Tm (Block time)Tj EMC ( 2021)Tj EMC EMC /P <>BDC 6.5 0 0 6.5 448.7448 742.9529 Tm EMC BT ( )Tj 7 0 0 7 457.0984 210.7654 Tm EMC /P <>BDC 36.85 824.882 572.599 17.008 re 9 0 0 9 363.1048 522.8898 Tm BT Fully loaded, the jet can fly up to 3,159 miles without refueling. ET ( )Tj BT 7 0 0 7 99.8582 331.7654 Tm 6.5 0 0 6.5 449.7715 565.9529 Tm EMC ET EMC ( )Tj 168 0 obj ET EMC (flight relate to fuel burn, overflight and)Tj EMC /P <>BDC BT BT EMC (capacity with slimmer seats, and cabin)Tj (longest sectors from BOS to PHX,)Tj /P <>BDC /P <>BDC /P <>BDC 7 0 0 7 118.104 67.7654 Tm EMC EMC endobj 9 0 0 9 394.0315 82.8898 Tm EMC EMC ( )Tj /P <>BDC EMC 7 0 0 7 247.7395 683.7654 Tm EMC )21(The r)10(elativ)12.9(e)]TJ ET 7 0 0 7 141.7322 100.9528 Tm EMC ( )Tj 6.5 0 0 6.5 191.63 565.9529 Tm /P <>BDC (170)Tj BT ( )Tj ( )Tj 9 0 0 9 165.5977 478.8898 Tm ( )Tj /TT2 1 Tf ( )Tj ET EMC ET 9 0 0 9 382.9368 148.8898 Tm 8 0 0 8 490.9813 771.9528 Tm BT ET -.01 Tc [(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 9 394.0157 181.8898 Tm ( )Tj EMC BT 7 0 0 7 474.3564 617.9528 Tm EMC ET ET (35,112)Tj (831)Tj 6 0 0 6 427.5796 729.9528 Tm (\(Miami\) sector, to 299 degrees on the)Tj BT EMC 7 0 0 7 258.2805 419.7654 Tm EMC BT EMC /P <>BDC BT /P <>BDC /F4 1 Tf BT ET ET -.02 Tc BT (1,272)Tj 7 0 0 7 259.1625 199.7654 Tm EMC 7 0 0 7 241.5317 540.9528 Tm EMC /P <>BDC ET 7 0 0 7 473.8245 320.9528 Tm /P <>BDC 56 0 0 56 36.8606 622.1944 Tm ET /P <>BDC 0 Tc /P <>BDC ET EMC (195,200)Tj ET ET ET ET [(CFM L)17.1(E)-8.1(AP-1B27)]TJ /P <>BDC EMC (136-145)Tj EMC ET /F6 1 Tf 0 Tc 5.25 0 0 5.25 515.3989 11.5129 Tm /P <>BDC -.01 Tc /P <>BDC ET ( )Tj /P <>BDC 7 0 0 7 337.4684 694.9528 Tm -.02 Tc ET ( )Tj ET BT BT 9 0 0 9 394.0157 159.8898 Tm ET ( )Tj EMC ET Q /P <>BDC BT ( )Tj /GS1 gs ET BT ET ( )Tj 9 0 0 9 53.8582 588.8898 Tm 6 0 0 6 396.9076 729.9528 Tm /P <>BDC ET ET /P <>BDC ET 7 0 0 7 543.7693 11.5132 Tm 9 0 0 9 203.1969 566.8898 Tm /P <>BDC /P <>BDC BT ET /P <>BDC /P <>BDC ET ET 9 0 0 9 394.0315 511.8898 Tm ( )Tj EMC BT ET EMC -.02 Tc /P <>BDC BT 7 0 0 7 554.7883 595.7654 Tm 5 0 0 5 92.725 11.5132 Tm BT BT 6.5 0 0 6.5 499.597 624.9529 Tm -.02 Tc 7 0 0 7 429.157 474.9528 Tm ET EMC ET EMC 9 0 0 9 379.7168 225.8898 Tm 7 0 0 7 554.7883 144.7654 Tm BT /P <>BDC 7 0 0 7 241.5317 727.9528 Tm each aircraft is sourced from different places. EMC 9 0 0 9 530.4152 423.8898 Tm ( )Tj /P <>BDC EMC ET EMC ( )Tj 9 0 0 9 359.1448 181.8898 Tm 7 0 0 7 491.4046 144.9528 Tm 9 0 0 9 36.8504 203.8898 Tm 7 0 0 7 445.7203 11.5129 Tm (In both cases, the A320neo has a lower)Tj ( )Tj -.02 Tc ET BT EMC 7 0 0 7 158.74 694.7654 Tm ET ET EMC [(A3)24.9(20ceo v)12.9(ersus A3)24.9(20neo )]TJ ET /P <>BDC /P <>BDC ET /P <>BDC (better for the A321neo due to its increased)Tj Just not sure how to access these. /P <>BDC /F1 1 Tf ET 7 0 0 7 387.0159 617.9528 Tm ET ET (stage lengths or tracked distances of)Tj ET ET 7 0 0 7 158.74 496.7654 Tm BT /P <>BDC /P <>BDC BT /P <>BDC 7 0 0 7 54.7071 408.7654 Tm BT 28.5749 0 TD ( )Tj ( )Tj EMC 518.735 0 l /P <>BDC ET EMC ( )Tj ET (39,270)Tj /P <>BDC BT /P <>BDC /P <>BDC ET EMC /P <>BDC BT 137 )Tj BT [(OM)8.1(M)-12.9(E)-24.9(R)7.1(C)8.1(E)]TJ EMC EMC EMC /P <>BDC I will be very happy to share with you once I get decent results. BT BT /P <>BDC BT /F7 1 Tf /P <>BDC EMC 9 0 0 9 326.8538 60.8898 Tm BT (A320neo)Tj -.02 Tc ( )Tj 0 Tc BT [(Summar)-33(y )]TJ ET EMC 7 0 0 7 535.5029 276.7654 Tm BT ET ( )Tj EMC EMC EMC ET BT ET EMC /GS1 gs endobj ET EMC (The second comparison is payload)Tj ET The 737-800 is the most popular variant of the four NG models, with nearly 5,000 aircraft delivered and making up 72% of the NG fleet in service. ( )Tj /P <>BDC ( )Tj ET ( )Tj BT ET BT /P <>BDC 9 0 0 9 53.8578 115.8898 Tm EMC BT ET 7 0 0 7 125.6292 342.7654 Tm 6.5 0 0 6.5 324.4345 676.9529 Tm BT 7 0 0 7 537.7804 342.9528 Tm -.02 Tc ET /P <>BDC 9 0 0 9 411.0181 38.8898 Tm EMC In payload scenario 1 the)Tj EMC EMC 7 0 0 7 440.0906 100.9528 Tm ( )Tj 7 0 0 7 314.6398 705.7654 Tm 0 Tc EMC /F6 1 Tf ET ET ET /P <>BDC BT /P <>BDC /P <>BDC /P <>BDC EMC BT /P <>BDC ET 0 Tc ET ET ET 0 Tc 6 0 0 6 178.2463 729.9528 Tm ET 9 0 0 9 232.4217 137.8898 Tm BT EMC ( )Tj EMC /F7 1 Tf (72,450)Tj /P <>BDC EMC 6 0 0 6 403.5248 659.9528 Tm 0 Tc /P <>BDC /P <>BDC 7 0 0 7 141.7322 210.9528 Tm -.02 Tc ET EMC BT S (150)Tj EMC EMC BT EMC 9 0 0 9 566.9717 236.8898 Tm ET /P <>BDC This is because it)Tj (\(see table, page 19\))Tj (over 400 MAXs, and Airbus a similar)Tj 7 0 0 7 230.7317 683.9528 Tm EMC 6.5 0 0 6.5 499.4541 735.9529 Tm .151 .147 .15 rg EMC 7 0 0 7 314.6398 507.7654 Tm BT ET ( )Tj 7 0 0 7 241.2727 573.9528 Tm /P <>BDC 7 0 0 7 380.2788 386.7654 Tm EMC (1B27)Tj ET BT 7 0 0 7 474.7064 331.9528 Tm /P <>BDC (1A32)Tj 6.5 0 0 6.5 480.5169 565.9529 Tm EMC 0 Tc BT 7 0 0 7 491.4046 342.9528 Tm ( )Tj The advanced wing airfoil design provides an economical cruise speed of .789 Mach (530 mph) - compared to .745 Mach for earlier 737 models. ( )Tj BT 5 0 0 5 484.5872 11.5129 Tm BT 7 0 0 7 380.2788 529.7654 Tm BT /P <>BDC EMC /P <>BDC ET EMC EMC BT ET ET Click here. Modern Airliners and Civil Aviation Aircraft. BT BT EMC 9 0 0 9 394.0315 786.8898 Tm -.02 Tc /P <>BDC (5,350)Tj EMC (989)Tj ( )Tj [(BOS-SE)-13.9(A)]TJ EMC BT ET ( )Tj BT /P <>BDC ET ET /P <>BDC ET 7 0 0 7 445.619 507.7654 Tm 7 0 0 7 387.0932 100.9528 Tm )Tj BT ( )Tj BT /P <>BDC BT BT /P <>BDC 9 0 0 9 352.4841 313.8898 Tm ET 7 0 0 7 446.5009 672.7654 Tm EMC (977)Tj BT /P <>BDC -.02 Tc ET BT ET -.02 Tc ET /P <>BDC EMC 6 0 0 6 507.6099 659.9528 Tm /P <>BDC 0 Tc EMC 9 0 0 9 394.0123 500.8898 Tm BT ( )Tj /P <>BDC 7 0 0 7 521.4089 11.5132 Tm 6.5 0 0 6.5 398.369 545.9529 Tm 7 0 0 7 199.5784 441.7654 Tm /P <>BDC ET 9 0 0 9 533.576 236.8898 Tm BT EMC ET ET /Artifact <>BDC 13 0 0 13 512.5669 467.8898 Tm /P <>BDC 7 0 0 7 158.74 364.7654 Tm (737-800W)Tj BT /P <>BDC ET BT ET (analysis has an MTOW of 194,700lbs, an)Tj (customers better performance and lower)Tj 7 0 0 7 487.0872 11.5129 Tm 9 0 0 9 369.4048 467.8898 Tm /P <>BDC BT EMC ( )Tj 9 0 0 9 376.7938 500.8898 Tm ET 7 0 0 7 338.6433 67.7654 Tm ET /P <>BDC 7 0 0 7 366.0641 738.9528 Tm -.01 Tc EMC /P <>BDC /P <>BDC ET -.02 Tc ET 6 0 0 6 434.211 701.9528 Tm 9 0 0 9 215.4313 412.8898 Tm /P <>BDC 7 0 0 7 404.3599 672.7654 Tm 0 Tc /P <>BDC EMC 9 0 0 9 394.0123 588.8898 Tm EMC EMC 0 Tc 0 Tc ( )Tj BT -.02 Tc 9 0 0 9 533.9409 390.8898 Tm ET /P <>BDC /P <>BDC ( )Tj ( )Tj ET /P <>BDC ET 0 Tc (scenarios have been run. 137 )Tj /P <>BDC EMC The wings on the above models are able to hold 30% more fuel then previous generations. /P <>BDC (the A321ceo, A321neo, 737-900ER\(W\))Tj ET ET 7 0 0 7 457.0984 408.7654 Tm levels in the center fuel tanks. /P <>BDC flightdeck (below the F/O's FMC) but they have since been removed to a BT BT /P <>BDC ET /P <>BDC ET ET EMC 0 Tc BT ( )Tj ET ( )Tj (124,650)Tj BT ET /P <>BDC ( )Tj 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. /P <>BDC ET EMC ( )Tj 0 Tc ( )Tj (37,653)Tj 0 Tc EMC (passengers and the 737-900ER\(W\) 152)Tj /P <>BDC /P <>BDC ET Fokker 100, the Netherlands regional jet. BT EMC /P <>BDC EMC 7 0 0 7 338.3085 331.9528 Tm ET /P <>BDC EMC (bypass ratio of 9.0:1. BT EMC 0 Tc q 1 0 0 1 215.441 73.878 cm 0 0 m 7 0 0 7 82.2047 584.9528 Tm /P <>BDC 7 0 0 7 446.5009 661.7654 Tm ET /P <>BDC ET EMC 0 Tc /P <>BDC ET (engine bypass ratio in the case of the 737)Tj BT BT BT ET 9 0 0 9 53.8582 478.8898 Tm EMC EMC BT aircraft /P <>BDC BT EMC ET /P <>BDC ( )Tj BT /P <>BDC BT ET BT 7 0 0 7 439.2087 221.9528 Tm 7 0 0 7 445.619 485.7654 Tm EMC /P <>BDC BT (172,992)Tj /P <>BDC EMC 9 0 0 9 53.8582 379.8898 Tm EMC ET 7 0 0 7 354.6933 441.7654 Tm ET EMC EMC BT 7 0 0 7 258.2805 474.7654 Tm EMC 0 Tc 7 0 0 7 187.0858 727.9528 Tm BT ( )Tj BT ( )Tj /GS1 gs /P <>BDC /P <>BDC /P <>BDC ET -.02 Tc (would be no additional holding required,)Tj ET BT ET EMC /P <>BDC 10 0 0 10 37.304 794.2914 Tm EMC 7 0 0 7 337.6855 67.9528 Tm BT 9 0 0 9 192.1373 401.8898 Tm /P <>BDC EMC EMC ( )Tj -.02 Tc 7 0 0 7 337.6855 276.9528 Tm (376)Tj 0 Tc EMC ET BT BT (170)Tj 8 0 0 8 124.845 675.9528 Tm -.02 Tc ET EMC ET /P <>BDC /P <>BDC BT /P <>BDC ET ET -.02 Tc EMC /P <>BDC BT (3,021)Tj EMC ET )Tj -.02 Tc BT ET EMC 7 0 0 7 457.0984 562.7654 Tm ET ET /P <>BDC 8 0 0 8 270.7815 771.9528 Tm /P <>BDC ( )Tj BT /P <>BDC 8 0 0 8 334.994 661.9528 Tm -.01 Tc 0 Tc ET BT 6.5 0 0 6.5 379.0655 650.9529 Tm 7 0 0 7 141.7322 67.9528 Tm ET 0 Tc (408)Tj BT .001 Tc BT ( )Tj ET BT EMC BT /P <>BDC /P <>BDC ( )Tj /GS1 gs ( )Tj 9 0 0 9 53.8338 269.8898 Tm EMC Q ET /P <>BDC (831)Tj (187,700lbs, an MLW of 157,300lbs and a)Tj BT BT /P <>BDC -.342 -1.2294 l EMC /P <>BDC EMC EMC 9 0 0 9 194.061 324.8898 Tm (5,279)Tj /P <>BDC ET BT BT 9 0 0 9 381.2556 500.8898 Tm BT /P <>BDC EMC 9 0 0 9 53.8582 60.8898 Tm ET 8 0 0 8 38.4438 675.9528 Tm 0 Tw EMC ET /P <>BDC 9 0 0 9 544.8128 412.8898 Tm EMC BT ET BT EMC ET ( )Tj 9 0 0 9 195.3055 324.8898 Tm ET ET (0.0142)Tj 7 0 0 7 37.0536 606.9528 Tm EMC 9 0 0 9 367.2172 269.8898 Tm EMC 7 0 0 7 507.7893 595.7654 Tm EMC ET 7 0 0 7 539.8962 474.9528 Tm EMC BT [(F)43(uel burn/)]TJ ET .41 .161 .508 rg ET 6.5 0 0 6.5 536.8751 722.9529 Tm 7 0 0 7 539.8962 606.9528 Tm of 12% is sufficient to prevent ignition, this is achievable with one module on BT BT ( )Tj ( )Tj /P <>BDC 9 0 0 9 232.4217 291.8898 Tm 9 0 0 9 197.3303 170.8898 Tm 6.5 0 0 6.5 399.2659 565.9529 Tm /P <>BDC 8 0 0 8 365.7704 661.9528 Tm ET ( )Tj /P <>BDC 6.5 0 0 6.5 448.4585 676.9529 Tm 7 0 0 7 321.6356 287.9528 Tm /P <>BDC EMC provision for a ferry kit. (150)Tj /P <>BDC BT EMC 0 Tc /P <>BDC BT ( )Tj BT ET EMC EMC /P <>BDC (136)Tj /P <>BDC /P <>BDC EMC /P <>BDC -.5815 -.9071 l BT /P <>BDC 0 Tc .151 .147 .15 rg 9 0 0 9 565.8376 577.8898 Tm /P <>BDC BT BT EMC ( )Tj BT /GS2 gs 9 0 0 9 541.0135 159.8898 Tm ET ( )Tj EMC ET EMC 6.5 0 0 6.5 375.6529 689.9529 Tm ( )Tj (2,207)Tj (16,170)Tj ET ( )Tj ET EMC ET /P <>BDC ET 6.5 0 0 6.5 330.4406 624.9529 Tm 7 0 0 7 473.8245 144.9528 Tm /P <>BDC [(UG)-17.1(U)-8(S)8.1(T)]TJ ET The service ceiling is 41,000 feet. BT 6.5 0 0 6.5 280.6329 545.9529 Tm Required fields are marked *. /P <>BDC /P <>BDC 7 0 0 7 82.2047 562.9528 Tm EMC 7 0 0 7 230.7317 276.9528 Tm BT BT Thanks now. q ET ET BT -.02 Tc BT ET 7 0 0 7 241.5317 441.9528 Tm 7 0 0 7 326.2278 540.9528 Tm 7 0 0 7 539.8962 463.9528 Tm 7 0 0 7 535.5029 727.7654 Tm 9 0 0 9 53.8338 49.8898 Tm EMC EMC 7 0 0 7 37.0536 683.9528 Tm ( )Tj /P <>BDC EMC 13 0 0 13 358.8579 60.8898 Tm ( )Tj EMC -.02 Tc (. ( )Tj BT 9 0 0 9 215.433 434.8898 Tm /Artifact <>BDC BT 9 0 0 9 552.5493 357.8898 Tm ( )Tj ET ET BT f ( )Tj EMC 9 0 0 9 394.0123 654.8898 Tm 9 0 0 9 568.024 148.8898 Tm EMC /P <>BDC BT EMC (900ER\(W\) are the only aircraft in the)Tj /P <>BDC BT /P <>BDC EMC (which could reduce this difference. EMC /P <>BDC /P <>BDC /P <>BDC 9 0 0 9 411.0181 357.8898 Tm EMC /P <>BDC ( )Tj EMC 0 Tc EMC EMC ( )Tj BT 0 Tc ET 7 0 0 7 444.737 111.7654 Tm BT BT ( )Tj /P <>BDC 0 Tc BT 5 0 0 5 92.725 11.5132 Tm ( )Tj BT (0.0140)Tj (The 737-800 is the most popular)Tj Tweet !function(d,s,id){var js,fjs=d.getElementsByTagName(s)[0],p=/^http:/.test(d.location)? EMC 8 0 0 8 187.3427 703.9528 Tm /P <>BDC EMC ET ET EMC EMC /P <>BDC (O)Tj 9 0 0 9 394.0315 742.8898 Tm 9 0 0 9 394.0157 214.8898 Tm BT ET 7 0 0 7 554.7883 540.7654 Tm ET /P <>BDC .964 .834 .406 rg EMC ( )Tj ET EMC EMC -.02 Tc /P <>BDC BT ET ( )Tj /Artifact <>BDC 0 Tc /P <>BDC BT 9 0 0 9 53.8578 148.8898 Tm ( )Tj 7 0 0 7 37.6993 100.9528 Tm ET /P <>BDC EMC /GS1 gs (34,650lbs)Tj BT /P <>BDC BT ( )Tj /P <>BDC BT ET BT ET /P <>BDC ET 7 0 0 7 320.7537 111.9528 Tm BT EMC ET /P <>BDC 7 0 0 7 279.1575 221.9528 Tm (47,000)Tj /P <>BDC 9 0 0 9 541.0405 621.8898 Tm 7 0 0 7 444.737 89.7654 Tm 7 0 0 7 439.7405 595.9528 Tm BT 7 0 0 7 337.4684 738.9528 Tm These are: Below is a table of the main features and specifications for the Boeing 737 family of aircraft. -.02 Tc ( )Tj ( )Tj
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