737 800 fuel capacity pounds
7 0 0 7 54.7071 78.7654 Tm 7 0 0 7 113.1366 122.9528 Tm BT ET (10)Tj (2,729)Tj ( )Tj 6.5 0 0 6.5 267.1065 742.9529 Tm /P <>BDC -.02 Tc 0 Tc /P <>BDC (5,243)Tj EMC EMC ( )Tj BT EMC EMC EMC BT BT /GS1 gs /P <>BDC /P <>BDC BT /P <>BDC In scenario 2, the 85% payload)Tj BT /P <>BDC BT BT ET (20)Tj ( )Tj BT /P <>BDC ( )Tj 7 0 0 7 141.7322 463.9528 Tm BT 9 0 0 9 408.1854 676.8898 Tm (or scenarios in this study. 7 0 0 7 343.2355 727.7654 Tm (1,272)Tj ( C)Tj (mainline US carriers like Alaska, American)Tj (the defined LRC speed, this has resulted in)Tj EMC /P <>BDC 7 0 0 7 404.101 298.7654 Tm BT ( N)Tj ET 7 0 0 7 490.5101 661.9528 Tm EMC (2,517)Tj EMC 7 0 0 7 380.2788 496.7654 Tm 9 0 0 9 374.0759 203.8898 Tm ET 0 Tc EMC 9 0 0 9 36.8504 269.8898 Tm ET /P <>BDC /OC /MC1974 BDC (operationally safe to do so, in the)Tj ET 7 0 0 7 490.8321 540.7654 Tm EMC /P <>BDC On the Digital Sunburst fuel gauges, pressing the "Qty test" button will ( )Tj ET ET /Artifact <>BDC ( )Tj /P <>BDC EMC /P <>BDC 0 Tc EMC /P <>BDC ET either 3,065 or 1,421 litre capacities. 5.25 0 0 5.25 100.8225 11.5132 Tm ET EMC 7 0 0 7 338.6433 408.7654 Tm 7 0 0 7 440.0906 133.9528 Tm 6.5 0 0 6.5 276.4014 637.9529 Tm -.02 Tc -.01 Tc (seating, while both the economy-plus and)Tj (passengers and the 737-900ER\(W\) 152)Tj BT BT 7 0 0 7 141.7322 397.9528 Tm ( )Tj EMC 7 0 0 7 299.0601 441.9528 Tm ET BT /P <>BDC BT BT could you point me in the right direction or tell me what the weight of the landing gear would be on a 737? BT Since no two)Tj EMC (or the CFM LEAP-1A32, rated at)Tj 6.5 0 0 6.5 486.1525 722.9529 Tm /P <>BDC (l)Tj 9 0 0 9 211.1071 764.8898 Tm ( )Tj 9 0 0 9 541.0135 159.8898 Tm /P <>BDC ET BT 9 0 0 9 36.8504 49.8898 Tm BT /P <>BDC ET ET 7 0 0 7 337.6855 210.9528 Tm /F5 1 Tf 7 0 0 7 507.5303 100.7654 Tm BT EMC EMC (369-383)Tj ET -.02 Tc (- nm)Tj BT /F4 1 Tf EMC BT BT (310,080)Tj EMC ET BT ET -.02 Tc EMC 7 0 0 7 204.0935 210.7654 Tm EMC /P <>BDC (\(see table, page 19\))Tj 7 0 0 7 539.9176 11.5129 Tm 0 Tc ET BT EMC EMC BT -.02 Tc 0 Tw ( )Tj EMC ET BT 8 0 0 8 43.6039 661.9528 Tm BT 0 Tc BT Boeing 737 MAX 9 reviews and traveller comments. EMC /P <>BDC ET ET /P <>BDC /P <>BDC (over 400 MAXs, and Airbus a similar)Tj -.02 Tc EMC BT tank. EMC ET ET -.02 Tc -.02 Tc BT /P <>BDC /P <>BDC /F2 1 Tf EMC 7 0 0 7 131.6494 177.7654 Tm ET ET ET ET ( )Tj EMC 7 0 0 7 404.3599 595.7654 Tm EMC 9 0 0 9 193.8472 236.8898 Tm ET EMC 8 0 0 8 338.514 745.9528 Tm 6 0 0 6 466.0123 687.9528 Tm The CFM56-5B4/P has a)Tj EMC unit, Open or short in [(CFM L)17.1(E)-8.1(AP-)]TJ ET /P <>BDC /P <>BDC EMC EMC EMC ( )Tj ( )Tj BT 10 0 0 10 420.16 814.1973 Tm 10 0 0 10 422.8 814.1973 Tm (1,272)Tj BT EMC ET ET ET BT 9 0 0 9 394.0237 478.8898 Tm 7 0 0 7 230.7317 397.9528 Tm ET 7 0 0 7 536.3849 595.7654 Tm EMC 7 0 0 7 338.6433 199.7654 Tm 6.5 0 0 6.5 296.3606 735.9529 Tm EMC /P <>BDC 7 0 0 7 337.6855 518.9528 Tm ( )Tj ET BT BT EMC 9 0 0 9 544.5056 302.8898 Tm It is)Tj ET EMC /P <>BDC 9 0 0 9 363.1048 522.8898 Tm ET EMC ET EMC 6 0 0 6 167.0441 757.9528 Tm /P <>BDC Aux fuel control panel (Aft overhead panel). ET /P <>BDC ( )Tj BT /P <>BDC EMC 304.725 420.96 m EMC /P <>BDC 0 Tc BT EMC /P <>BDC BT 0 Tc 7 0 0 7 490.7815 67.9528 Tm /P <>BDC 10 0 0 10 417.91 814.1973 Tm ET BT EMC 0 Tc /P <>BDC BT /P <>BDC ( )Tj ( )Tj 9 0 0 9 393.5047 181.8898 Tm ET ET EMC ( )Tj ( )Tj ( )Tj 7 0 0 7 387.0932 331.9528 Tm /P <>BDC /P <>BDC /P <>BDC BT ( )Tj BT BT ET Whatever the reason, we hope that both Boeing and the F.A.A. EMC 0 Tc 9 0 0 9 492.5143 500.8898 Tm Do you know how or where I would be able to get details on the dimensions or materials of the wingtip for this aircraft or other similar aircraft? /P <>BDC 9 0 0 9 411.0097 533.8898 Tm 9 0 0 9 394.0237 225.8898 Tm EMC As a result of its lower fuel burn,)Tj /Artifact <>BDC (materials. ( )Tj /F1 1 Tf .151 .147 .15 rg /P <>BDC 9 0 0 9 215.4313 379.8898 Tm 9 0 0 9 394.0157 104.8898 Tm EMC EMC ET ( )Tj BT ET -.02 Tc BT 9 0 0 9 361.9529 159.8898 Tm /P <>BDC /P <>BDC 0 Tc [(P)11(ayload)]TJ ( )Tj -.01 Tc /P <>BDC [(R)30(elativ)12.9(e fuel burn )]TJ thanks for stopping by. /P <>BDC 6 0 0 6 165.5504 659.9528 Tm 9 0 0 9 408.1968 324.8898 Tm /P <>BDC -.02 Tc The total tolerance for the FQIS system is based on a full tank. /P <>BDC 7 0 0 7 343.2355 474.7654 Tm EMC EMC 9 0 0 9 408.1854 423.8898 Tm While the MAX 10 is still yet to be certified, the legacy of the -900ER lives on, and the type will likely continue to fly for many more years before retirement. ET 7 0 0 7 230.7317 540.9528 Tm EMC 7 0 0 7 343.2355 694.7654 Tm ( )Tj ( )Tj (1B engine as the 737-8. BT 7 0 0 7 508.4124 727.7654 Tm EMC 6 0 0 6 433.8509 687.9528 Tm /P <>BDC (136-145)Tj ET /P <>BDC /P <>BDC ET BT 0 841.89 609.449 -841.89 re -.02 Tc EMC 9 0 0 9 516.4593 412.8898 Tm 6 0 0 6 351.3743 757.9528 Tm ET 0 Tw ET /P <>BDC EMC (137,789)Tj BT /P <>BDC BT 9 0 0 9 562.2737 379.8898 Tm 9 0 0 9 550.8315 247.8898 Tm 7 0 0 7 518.4953 122.9528 Tm /P <>BDC BT BT /P <>BDC [(BOS-L)-31(A)-24.9(X)]TJ ET EMC ( )Tj ET 7 0 0 7 158.74 716.7654 Tm EMC /P <>BDC BT ET ( )Tj 7 0 0 7 491.392 463.9528 Tm (344-358)Tj 6.5 0 0 6.5 499.597 624.9529 Tm /P <>BDC ET EMC EMC (sharklets. 7 0 0 7 99.8582 694.7654 Tm /P <>BDC 7 0 0 7 535.5029 320.7654 Tm EMC ET 9 0 0 9 186.3413 291.8898 Tm 9 0 0 9 198.192 599.8898 Tm BT 9 0 0 9 194.5468 71.8898 Tm EMC BT 0 Tc /P <>BDC ET EMC ET /P <>BDC -.02 Tc (different available options, and gives the)Tj /P <>BDC -.02 Tc .0063 7.6255 l .41 .161 .508 RG 6 0 0 6 103.6577 715.9528 Tm 5.25 0 0 5.25 100.8225 11.5132 Tm These transfer fuel from the centre tank into tank 1 at a minimum rate of 100kg/hr, although usually nearer 200kg/hr. EMC /P <>BDC ET /P <>BDC )Tj BT ET (10)Tj EMC BT BT BT BT 9 0 0 9 246.6113 247.8898 Tm BT ET BT EMC /P <>BDC 9 0 0 9 394.0157 280.8898 Tm EMC BT /P <>BDC ET EMC /P <>BDC EMC ET 9 0 0 9 195.4763 258.8898 Tm /GS2 gs 7 0 0 7 537.7804 276.9528 Tm /P <>BDC ET /P <>BDC /P <>BDC 6.5 0 0 6.5 488.8955 532.9529 Tm EMC ET /OC /MC2287 BDC /P <>BDC 9 0 0 9 195.3055 324.8898 Tm [(Y)-7.1(XX/104)]TJ BT -.02 Tc EMC 9 0 0 9 394.0123 412.8898 Tm 9 0 0 9 36.8504 126.8898 Tm 10 0 0 10 539.3945 794.2914 Tm [(b)6.1(ypass r)10(atio engines pr)10(o)16.1(vide it with the most)]TJ /P <>BDC EMC /P <>BDC /P <>BDC 10 0 0 10 49.3644 814.1973 Tm /P <>BDC 9 0 0 9 394.0123 104.8898 Tm 0 Tc ( )Tj (1,202)Tj /P <>BDC /P <>BDC EMC 7 0 0 7 439.2087 144.9528 Tm 9 0 0 9 53.8578 247.8898 Tm ET 9 0 0 9 385.6838 346.8898 Tm 9 0 0 9 550.4974 599.8898 Tm BT 0 Tc /P <>BDC /P <>BDC ET BT EMC ( )Tj EMC EMC 0 Tc 8 0 0 8 158.74 771.7654 Tm [(AIRL)8.1(INE & AIR)7.1(CRAF)-12.9(T)18.1( OPERA)56.9(T)-8.1(ION)-13.9(S)]TJ EMC 9 0 0 9 411.0097 214.8898 Tm /P <>BDC 9 0 0 9 394.0123 390.8898 Tm 7 0 0 7 82.8504 78.9528 Tm (comparison to allow a better review of the)Tj BT ET (0.0123)Tj [(BOS-C)-8.1(V)18.1(G)]TJ ( )Tj EMC BT ET 9 0 0 9 394.0237 456.8898 Tm EMC 9 0 0 9 53.8338 324.8898 Tm ET ET 0 Tc BT /P <>BDC ( )Tj ET 7 0 0 7 82.2047 496.9528 Tm BT EMC ( )Tj /P <>BDC BT ( )Tj /P <>BDC BT ET EMC (3,200)Tj EMC BT 9 0 0 9 433.049 544.8898 Tm ( )Tj EMC 6 0 0 6 184.4022 729.9528 Tm (2,517)Tj EMC EMC BT EMC BT 7 0 0 7 242.1547 672.9528 Tm 9 0 0 9 75.3887 489.8898 Tm 7 0 0 7 445.619 694.7654 Tm 8 0 0 8 298.0262 760.9528 Tm ( )Tj BT (484nm for the shortest BOS-YYZ)Tj 7 0 0 7 439.2087 265.9528 Tm 8 0 0 8 43.6039 605.9528 Tm /P <>BDC ( )Tj ET EMC BT EMC (170)Tj BT /P <>BDC EMC ET 6 0 0 6 320.3167 757.9528 Tm ( )Tj /P <>BDC 7 0 0 7 314.6398 606.7654 Tm (163)Tj BT EMC /P <>BDC BT ( )Tj 9 0 0 9 232.4217 291.8898 Tm ( )Tj EMC /P <>BDC /P <>BDC EMC ET /P <>BDC EMC 7 0 0 7 387.0159 661.9528 Tm /P <>BDC 9 0 0 9 68.031 170.8898 Tm EMC BT S -.02 Tc (Improvements introduced to the)Tj /P <>BDC ET BT /P <>BDC EMC (A320neos aircraft interior design and)Tj -.02 Tc EMC BT -.02 Tc BT EMC BT EMC ( )Tj /P <>BDC 7 0 0 7 387.0159 672.9528 Tm 7 0 0 7 141.7322 177.9528 Tm /P <>BDC 9 0 0 9 209.6398 489.8898 Tm ET EMC BT ( )Tj ET ( )Tj ET EMC (improvement of 0.58 cents per ASM over)Tj (136)Tj ET 7 0 0 7 279.1575 232.9528 Tm ET 0 Tc /OC /MC2281 BDC (192)Tj BT /P <>BDC BT 7 0 0 7 294.4014 518.7654 Tm BT EMC 0 Tc EMC BT EMC 9 0 0 9 377.8897 291.8898 Tm 0 Tc ET /P <>BDC BT /P <>BDC 7 0 0 7 279.1575 309.9528 Tm BT EMC 0 Tc /P <>BDC And the 800 has shown to be one of the most popular models for filling this role. ET /P <>BDC EMC ( )Tj 6 0 0 6 465.3942 771.9528 Tm ( A)Tj 232.441 656.608 340.813 -625.44 re ET ( )Tj BT 9 0 0 9 206.6251 236.8898 Tm EMC EMC /P <>BDC /P <>BDC 8 0 0 8 554.6981 771.7654 Tm BT 7 0 0 7 82.2047 507.9528 Tm EMC EMC /P <>BDC ET /P <>BDC 8 0 0 8 43.6039 647.9528 Tm ET BT ET EMC /P <>BDC -.02 Tc BT /P <>BDC EMC EMC BT 9 0 0 9 36.8504 236.8898 Tm ET BT EMC EMC /OC /MC2267 BDC [(UG)-17.1(U)-8(S)8.1(T)]TJ EMC EMC EMC BT (from Boston \(BOS\) Logan International)Tj BT ET ET (342,448)Tj EMC (additional benefit in this comparison. BT BT ET BT EMC /P <>BDC ET EMC ET /P <>BDC BT /P <>BDC /P <>BDC ET /P <>BDC 7 0 0 7 294.4014 584.7654 Tm ( )Tj ( )Tj BT /P <>BDC 6 0 0 6 115.1719 701.9528 Tm ( )Tj /P <>BDC BT BT .008 Tc 7 0 0 7 491.7142 298.7654 Tm ET /P <>BDC 9 0 0 9 68.3339 478.8898 Tm BT BT /P <>BDC BT ET 7 0 0 7 299.0601 243.9528 Tm EMC ET (35,112)Tj ( )Tj 6.5 0 0 6.5 397.1664 735.9529 Tm ET Maybe there is someone out there who can give you a better answer. /P <>BDC BT /P <>BDC EMC 0 Tc ET BT (35,112)Tj /P <>BDC BT ET EMC /GS2 gs BT BT BT /P <>BDC ET 9 0 0 9 187.5717 126.8898 Tm /P <>BDC ET 7 0 0 7 362.3891 309.9528 Tm /P <>BDC (31,416)Tj ET /P <>BDC 7 0 0 7 508.4124 683.7654 Tm /P <>BDC BT ET 0 Tc BT ET 7 0 0 7 101.0963 210.9528 Tm ET EMC ET ET 9 0 0 9 246.6141 786.8898 Tm /P <>BDC EMC EMC 9 0 0 9 501.24 731.8898 Tm 9 0 0 9 53.8582 665.8898 Tm EMC -.02 Tc /F6 1 Tf -1.1093 -3.9038 l /P <>BDC ET ET /P <>BDC 7 0 0 7 116.3631 11.5132 Tm BT BT /P <>BDC EMC BT 9 0 0 9 261.8182 225.8898 Tm EMC Boeings 737-800 isnt called the most popular airliner for no reason. -.02 Tc )Tj ET /P <>BDC (977)Tj EMC BT 0 Tc [(family competitors, the 737 M)-8.1(A)-24.9(X also has)]TJ BT /P <>BDC ( )Tj ( )Tj ET ET ET /P <>BDC /P <>BDC /P <>BDC BT (33,000lbs, the same 81-inch fan diameter)Tj /P <>BDC /F4 1 Tf ET )Tj EMC 7 0 0 7 141.7322 716.9528 Tm -.02 Tc (288)Tj ( )Tj /F1 1 Tf EMC (economy cabin, but some airlines can)Tj ET EMC ET BT /P <>BDC EMC /P <>BDC BT EMC ET 6 0 0 6 538.428 771.9528 Tm ( )Tj 7 0 0 7 298.514 573.9528 Tm /P <>BDC /P <>BDC /P <>BDC ( )Tj EMC 7 0 0 7 537.7804 166.9528 Tm BT EMC 7 0 0 7 387.0159 463.9528 Tm ET BT ( )Tj q 1 0 0 1 53.858 797.352 cm 0 0 m 0 Tw BT (standard passenger weight of 231lbs that)Tj EMC ET The)Tj BT BT BT EMC ET ( )Tj 9 0 0 9 36.8504 522.8898 Tm 6.5 0 0 6.5 397.0428 532.9529 Tm BT /P <>BDC 0 Tc /P <>BDC EMC /P <>BDC (-58)Tj EMC 7 0 0 7 338.6433 133.7654 Tm EMC /P <>BDC 0 Tc EMC BT [(AS)29(M)]TJ BT 6 0 0 6 540.5396 715.9528 Tm ET /P <>BDC On the longer sectors, however, the)Tj 6 0 0 6 527.3577 771.9528 Tm -.01 Tc BT -.02 Tc 9 0 0 9 374.887 346.8898 Tm 9 0 0 9 394.0157 390.8898 Tm /P <>BDC 0 Tc ( )Tj /P <>BDC EMC -.2034 -.7911 -.1202 -.4766 0 0 c BT BT ET ET ( )Tj ( )Tj /P <>BDC BT (2,349)Tj ET /P <>BDC BT 5.25 0 0 5.25 64.5461 11.5129 Tm /P <>BDC ET (170)Tj ET -.02 Tc ET 7 0 0 7 315.5217 639.7654 Tm /P <>BDC (4,182)Tj BT ( )Tj EMC 7 0 0 7 554.7883 111.7654 Tm ET BT ET /P <>BDC BT (0.0129)Tj /P <>BDC ET BT /P <>BDC -.02 Tc /P <>BDC /P <>BDC 9 0 0 9 68.0314 522.8898 Tm -.02 Tc /P <>BDC ET /P <>BDC 7 0 0 7 67.798 11.5132 Tm .0161 Tc ET /P <>BDC /P <>BDC 9 0 0 9 36.8504 115.8898 Tm BT BT ( )Tj ( )Tj BT ET /P <>BDC - Simmonds, Digital Fuel Quantity Indicator Error Codes 7 0 0 7 490.8321 166.7654 Tm 9 0 0 9 173.7412 203.8898 Tm /P <>BDC (297,475)Tj 73 0 obj /P <>BDC EMC ET /P <>BDC /P <>BDC (381)Tj EMC BT 7 0 0 7 354.6933 496.7654 Tm BT BT 7 0 0 7 204.0935 276.7654 Tm BT 0 Tc BT ET EMC /P <>BDC 9 0 0 9 211.8218 533.8898 Tm ET (the analysis is 20/29/143, so a total of 192)Tj ET ET /P <>BDC /P <>BDC EMC (0.0121)Tj EMC BT /F1 1 Tf -.02 Tc EMC ( )Tj -4.2575 -4.8278 -4.5158 -4.0295 -4.515 -3.0604 c EMC 9 0 0 9 469.5781 577.8898 Tm BT /P <>BDC ( )Tj (the BOS-LAX \(Los Angeles\) route. 0 Tc EMC BT 7 0 0 7 543.7693 11.5132 Tm 9 0 0 9 537.6801 258.8898 Tm BT ( )Tj ET ET ET ET 7 0 0 7 427.7291 133.9528 Tm Im glad you got something out of our site that was helpful. ( )Tj ET ET EMC 6.5 0 0 6.5 280.6329 545.9529 Tm ET EMC It provides code tables for aerodromes, air operators including the world's major airlines and for ICAO and IATA codes for aircraft. /P <>BDC EMC 7 0 0 7 294.4014 430.7654 Tm ET 6.5 0 0 6.5 192.41 598.9529 Tm (170)Tj ()Tj ( )Tj EMC /P <>BDC EMC 7 0 0 7 118.104 166.7654 Tm EMC ET EMC ET EMC /P <>BDC EMC EMC EMC BT ET /P <>BDC /P <>BDC ET BT /P <>BDC (series has a weight penalty because of its)Tj ET ET ET ET BT ET 0 Tc 9 0 0 9 370.9169 379.8898 Tm EMC ET ET /P <>BDC /P <>BDC BT EMC EMC BT /P <>BDC f -.01 Tc ( )Tj (282)Tj (4,552)Tj BT BT .014984 841.89 609.45 -841.89 re EMC ( )Tj BT ET BT ET 0 Tc ( )Tj 7 0 0 7 404.101 199.7654 Tm 9 0 0 9 394.0123 269.8898 Tm BT /P <>BDC BT ( )Tj EMC ET ET EMC /P <>BDC 8 0 0 8 99.8582 760.7654 Tm ET /P <>BDC /P <>BDC EMC -.02 Tc /P <>BDC BT ET -.02 Tc ( )Tj BT EMC -.02 Tc BT 9 0 0 9 527.7692 511.8898 Tm 9 0 0 9 53.8578 38.8898 Tm The controls for main tanks 1 and 2 change to aft BT BT BT BT /P <>BDC BT EMC ( )Tj 6.5 0 0 6.5 178.4573 722.9529 Tm EMC 9 0 0 9 53.8338 60.8898 Tm 6 0 0 6 507.2798 715.9528 Tm 7 0 0 7 54.7071 408.7654 Tm ET /P <>BDC must be determined by using the. /P <>BDC (performance deterioration factor added to)Tj EMC BT /P <>BDC 6.5 0 0 6.5 54.877 624.9529 Tm 9 0 0 9 373.4379 324.8898 Tm /P <>BDC (70)Tj (The A321ceo is equipped with either:)Tj EMC ( )Tj 8 0 0 8 90.0179 771.7654 Tm EMC BT EMC /P <>BDC ( )Tj /P <>BDC BT 9 0 0 9 343.5117 489.8898 Tm -.01 Tc /P <>BDC -.02 Tc BT EMC 9 0 0 9 527.0365 456.8898 Tm ET ET EMC BT 9 0 0 9 568.1771 115.8898 Tm 7 0 0 7 258.2805 265.7654 Tm BT 9 0 0 9 362.3666 269.8898 Tm ET BT EMC ( )Tj 7 0 0 7 125.6292 738.7654 Tm 9 0 0 9 521.2213 170.8898 Tm ET The Boeing 737-800 variant has as mentioned 27300 pound-force delivered by two turbo fans. BT EMC EMC q 1 0 0 1 53.85 797.54 cm 0 0 m (2,900)Tj BT 7 0 0 7 355.3163 89.7654 Tm ET Delta Air Lines received the first Next-Gen 737 model with this brake package, a . ( )Tj ET BT 0 Tc 9 0 0 9 394.0237 412.8898 Tm BT BT EMC EMC /P <>BDC 7 0 0 7 338.3085 265.9528 Tm ET BT /P <>BDC 0 Tc ( )Tj EMC f 0 Tc 0 Tc EMC ET 7 0 0 7 490.8321 144.7654 Tm /P <>BDC EMC EMC 7 0 0 7 539.8962 573.9528 Tm ET /P <>BDC EMC ET BT EMC ( )Tj ( )Tj 9 0 0 9 369.3136 698.8898 Tm BT EMC 7 0 0 7 99.8582 617.7654 Tm ET /P <>BDC (have been optimised by the PPS flight)Tj ET ET /P <>BDC ET /P <>BDC 9 0 0 9 544.9208 280.8898 Tm /P <>BDC 0 Tc 0 Tc EMC 9 0 0 9 524.2249 478.8898 Tm ET 0 Tc EMC ET BT 8 0 0 8 474.6331 771.7654 Tm EMC BT 7 0 0 7 247.7395 221.7654 Tm EMC BT (be achieved. 6 0 0 6 527.3389 687.9528 Tm /P <>BDC EMC /P <>BDC BT /P <>BDC EMC BT /P <>BDC BT EMC (-53)Tj 7 0 0 7 247.7395 518.7654 Tm 7 0 0 7 536.3849 562.7654 Tm /P <>BDC ( )Tj BT EMC /TT2 1 Tf /P <>BDC /P <>BDC -.02 Tc (I)Tj 7 0 0 7 404.101 166.7654 Tm EMC -.02 Tc -.02 Tc EMC BT ( )Tj (alternates used and their distance from the)Tj The fuel panels for the various series have not changed much over EMC 232.441 655.706 340.157 -624.522 re EMC ( )Tj EMC EMC ET ET /P <>BDC BT EMC /P <>BDC 7 0 0 7 456.4753 639.7654 Tm 7 0 0 7 456.2165 320.7654 Tm BT ( )Tj BT EMC ( )Tj ( )Tj ( )Tj /P <>BDC (\(neo\) families, and the 737NG family. BT ( )Tj BT ET -.02 Tc -.02 Tc BT BT /P <>BDC EMC (977)Tj (831)Tj 7 0 0 7 354.6933 628.7654 Tm ET /P <>BDC /P <>BDC EMC (163)Tj BT 19.851 0 l EMC 0 Tc BT ( )Tj (0.0130)Tj EMC Aluminium alloys are still the mainstay of the construction materials used with various blends used according to the strength required for the particular component. 9 0 0 9 36.8504 280.8898 Tm 7 0 0 7 59.2108 11.5129 Tm (A320ceo: )Tj )Tj BT 0 Tc 6 0 0 6 176.4941 687.9528 Tm 7 0 0 7 404.101 276.7654 Tm EMC /P <>BDC BT BT EMC EMC /P <>BDC /P <>BDC /P <>BDC 9 0 0 9 112.6132 302.8898 Tm /P <>BDC EMC EMC ET (108 on BOS-SEA \(Seattle\); 123 on BOS-)Tj BT ET /P <>BDC 9 0 0 9 388.8047 390.8898 Tm EMC Pisquali 19/05/2018 at 16:07 Reply. BT (737-9)Tj EMC (planned for each aircraft type. ET /P <>BDC EMC ( )Tj EMC /P <>BDC EMC ET (heavier than the A320ceo. ( )Tj (5,121)Tj ( )Tj (3,882)Tj BT BT /F6 1 Tf ET BT /P <>BDC BT (5,183)Tj ( )Tj -.02 Tc (. /P <>BDC 7 0 0 7 387.0932 364.9528 Tm BT ET EMC (2,800 -)Tj /P <>BDC EMC /P <>BDC BT (follow in their footsteps, having already)Tj ET (136)Tj 0 Tc EMC 9 0 0 9 192.1006 456.8898 Tm BT -.02 Tc (CFM56-5B4/P)Tj 9 0 0 9 411.0097 170.8898 Tm EMC BT /P <>BDC 9 0 0 9 75.273 533.8898 Tm EMC EMC EMC sectors to ensure an even fuel balance. W n 7 0 0 7 230.7317 331.9528 Tm /P <>BDC 7 0 0 7 457.0984 518.7654 Tm BT (comparison of the fuel burn performance. EMC EMC EMC /P <>BDC 7 0 0 7 118.104 67.7654 Tm /P <>BDC /P <>BDC BT ET 0 Tc -.02 Tc ( )Tj ( )Tj BT ET ET EMC /P <>BDC BT (route structure so these charges would not)Tj 7 0 0 7 491.4046 210.9528 Tm ET BT (scenarios have been run. The website is currently in the process of optimizing and will have further functions added in order to improve the usability. EMC /P <>BDC /P <>BDC BT The typical range for this)Tj EMC -.02 Tc (variant used in this study is the CFM)Tj BT EMC ( )Tj ET /P <>BDC Boeing 737Specs Tablefor Original and Classic. ET /P <>BDC ET /P <>BDC /P <>BDC (CFM LEAP-1B28B1s thrust rating to)Tj /P <>BDC 7 0 0 7 379.3969 67.7654 Tm Boeing 737 Assembly, the building of this popular City Jet. BT ( )Tj ( )Tj /P <>BDC /P <>BDC