ET BT BT ET EMC EMC BT (financing. ET (/S)Tj ( )Tj 7 0 0 7 379.3969 133.7654 Tm /P <>BDC /P <>BDC 9 0 0 9 215.4409 126.8898 Tm BT /P <>BDC (737-900ER\(W\) rather than the 737-900,)Tj BT /P <>BDC 7 0 0 7 141.7322 463.9528 Tm EMC 6 0 0 6 466.3124 757.9528 Tm EMC /P <>BDC /P <>BDC 7 0 0 7 554.7883 122.7654 Tm ET 8 0 0 8 38.4438 661.9528 Tm 7 0 0 7 141.7322 562.9528 Tm S [(CFM L)17.1(E)-8.1(AP-1A32)]TJ ET EMC ET EMC ET BT BT ( )Tj BT EMC /P <>BDC BT /P <>BDC /P <>BDC ( )Tj ET (3,031)Tj ET EMC 9 0 0 9 394.0157 247.8898 Tm 9 0 0 9 68.9175 247.8898 Tm 7 0 0 7 456.2165 320.7654 Tm 13 0 0 13 232.438 82.8898 Tm BT ET /P <>BDC 6 0 0 6 214.4975 659.9528 Tm f /P <>BDC ET /F6 1 Tf BT 0 Tc 0 Tc (34,650)Tj EMC ( )Tj EMC EMC ( )Tj BT ET /P <>BDC 5.25 0 0 5.25 64.5461 11.5129 Tm BT BT ( )Tj -.01 Tc /P <>BDC EMC EMC ( )Tj ET /P <>BDC ET BT ET /P <>BDC -.02 Tc EMC [(737-900E)-33(R)]TJ ET ET 7 0 0 7 439.2087 221.9528 Tm 9 0 0 9 526.8813 445.8898 Tm 0 Tc (which has the lowest fuel burn rate per)Tj EMC BT i.e..what is the maximum lateral distance the doors swing away from the aircraft, before they get to rest in the fully open position? ET (- USG)Tj /P <>BDC updated to ensure the accuracy of VNAV speeds, buffet margin and max altitude. EMC EMC BT )Tj (0.0140)Tj EMC ( )Tj ET EMC ET EMC 9 0 0 9 537.9817 445.8898 Tm 6 0 0 6 184.3662 673.9528 Tm ET In-flight, the GW must be periodically (404)Tj (0.0108)Tj EMC ET (74-82)Tj 7 0 0 7 53.8582 749.7654 Tm /P <>BDC BT 9 0 0 9 395.1859 258.8898 Tm (The A321neo is offered to airlines with)Tj ( )Tj ET -.01 Tc 7 0 0 7 554.7883 573.7654 Tm EMC /P <>BDC /P <>BDC ET (capacity of 6,353USG, giving it a range of)Tj ( )Tj BT ( )Tj BT ET -.02 Tc ( )Tj 7 0 0 7 430.039 628.9528 Tm EMC (The fuel burn improvement on the)Tj BT EMC BT /P <>BDC (34,650)Tj ( )Tj (. /P <>BDC 9 0 0 9 53.8338 225.8898 Tm BT 0 Tc (31,416)Tj EMC EMC BT ET /P <>BDC BT /F1 1 Tf 9 0 0 9 215.4313 313.8898 Tm EMC 8 0 0 8 43.6039 605.9528 Tm BT 7 0 0 7 343.2355 738.7654 Tm /P <>BDC (188,400)Tj 7 0 0 7 37.0536 584.9528 Tm (166,090)Tj ( )Tj ET 0 Tc EMC ( )Tj 7 0 0 7 37.6993 276.9528 Tm ( )Tj /P <>BDC ET (\(see)Tj EMC BT ET ( )Tj /P <>BDC BT 9 0 0 9 68.3339 467.8898 Tm EMC [(7)-33(3)8.1(7-800 v)12.9(ersus 7)-33(3)8.1(7-8 )]TJ BT (weights used are an MTOW of)Tj BT /P <>BDC EMC /P <>BDC BT ET /P <>BDC BT (195,200)Tj BT ET ET ( )Tj ET ET ( )Tj -.02 Tc BT /P <>BDC 0 Tc ET BT 0 Tc EMC BT EMC BT /P <>BDC EMC 6.5 0 0 6.5 437.571 532.9529 Tm -.01 Tc 7 0 0 7 37.5838 639.9528 Tm EMC BT -.02 Tc 7 0 0 7 294.4014 694.7654 Tm BT ( )Tj /P <>BDC BT EMC Perhaps somebody has experience in shipment of landing gear. /P <>BDC 7 0 0 7 338.3085 364.9528 Tm ( )Tj /P <>BDC EMC EMC ( )Tj /P <>BDC /P <>BDC EMC (types over a wide range of mission lengths)Tj BT 0 Tc 9 0 0 9 196.4663 137.8898 Tm 9 0 0 9 375.5153 291.8898 Tm BT (830)Tj EMC . ( )Tj -.005 Tc 6.5 0 0 6.5 191.8316 637.9529 Tm /P <>BDC /P <>BDC BT /P <>BDC BT EMC /P <>BDC EMC BT 7 0 0 7 343.2355 518.7654 Tm EMC ET EMC EMC EMC BT BT (0.0154)Tj /P <>BDC /P <>BDC 7 0 0 7 37.6993 122.9528 Tm BT 0 Tc /P <>BDC ( )Tj 17 0 0 17 36.8606 758.6944 Tm ( )Tj ET BT ET EMC BT -.02 Tc /P <>BDC ET ( )Tj ET ET That is because it is an 800. BT EMC 9 0 0 9 542.6167 159.8898 Tm -.01 Tc BT 9 0 0 9 411.0181 489.8898 Tm Vmo/Mmo Velocity/Mach Maximum Operating speed. ET BT 7 0 0 7 299.0601 276.9528 Tm 7 0 0 7 444.737 111.7654 Tm ET 7 0 0 7 247.7395 584.7654 Tm /P <>BDC 7 0 0 7 108.6215 67.9528 Tm /P <>BDC /P <>BDC ET -.02 Tc BT EMC /P <>BDC ( )Tj ET /P <>BDC ET The NG series are prone to "Upper Wing Surface ET 7 0 0 7 187.0858 100.9528 Tm ( )Tj /P <>BDC ( )Tj EMC 6 0 0 6 286.5632 771.9528 Tm BT ET BT ET EMC BT 9 0 0 9 377.4407 764.8898 Tm BT ET 1 i ( )Tj (339-353)Tj ET BT /P <>BDC (page\))Tj (31,416)Tj (1,498)Tj [(BOS-Y)-50(YZ)]TJ The three-class cabin)Tj BT BT ( )Tj W n EMC BT [(E)-24.9(SAD - nm )]TJ EMC 9 0 0 9 369.892 412.8898 Tm ET ( )Tj BT BT 0 Tc /P <>BDC (makes a flight-for-flight comparison)Tj ET ( )Tj BT ET 9 0 0 9 394.0123 555.8898 Tm /P <>BDC 9 0 0 9 36.8583 368.8898 Tm ET ET BT 304.725 420.96 m EMC 8 0 0 8 500.5689 771.9529 Tm 7 0 0 7 507.7893 463.7654 Tm -.02 Tc 6 0 0 6 54.1367 771.9528 Tm (The A321neo has a lower fuel burn)Tj 6.5 0 0 6.5 484.6315 545.9529 Tm ET ( )Tj /P <>BDC ( )Tj Is the Range with Max Payload NM(Km) wrong? EMC BT (manufacturers support these aircraft types)Tj /P <>BDC BT (375)Tj BT BT -.005 Tc BT (BOS-MIA)Tj ET /P <>BDC ( )Tj ( )Tj BT BT /P <>BDC (35,112)Tj /P <>BDC BT /P <>BDC BT ET 0 Tc 9 0 0 9 569.6968 346.8898 Tm /P <>BDC ET /P <>BDC - Modern Airliners, First International Sale of the COMAC ARJ21 Regional Jet. /P <>BDC ET EMC EMC EMC 7 0 0 7 491.392 672.9528 Tm Can you please tell me where to look for the cabin height,width, seat height, width and door to door length. EMC ( )Tj ( )Tj /OC /MC2 BDC 183,380 Litres: 47,210 US Gal. ET EMC BT ( )Tj EMC 9 0 0 9 544.6834 126.8898 Tm BT /P <>BDC BT ET 5.25 0 0 5.25 525.4061 11.5132 Tm 9 0 0 9 548.3644 533.8898 Tm EMC BT BT 7 0 0 7 338.6433 133.7654 Tm The use of composite materials in the 737 Next Gen or even the 737 Max is quite conservative. 9 0 0 9 276.2863 115.8898 Tm 7 0 0 7 258.2805 309.7654 Tm ( )Tj (an operating empty weight \(OEW\) of)Tj ( )Tj ET BT 9 0 0 9 36.8504 192.8898 Tm 9 0 0 9 524.3162 214.8898 Tm 7 0 0 7 241.5317 738.9528 Tm /P <>BDC ET ( )Tj BT -.02 Tc 7 0 0 7 366.0641 716.9528 Tm ( )Tj EMC 7 0 0 7 554.7883 276.7654 Tm BT 7 0 0 7 535.5029 375.7654 Tm -.02 Tc 0 Tc BT BT BT BT 9 0 0 9 534.7515 599.8898 Tm EMC q 1 0 0 1 215.433 480.878 cm 0 0 m /P <>BDC BT EMC 8 0 0 8 53.9373 760.7654 Tm BT BT (163)Tj 7 0 0 7 456.2165 419.7654 Tm BT /P <>BDC ET EMC The)Tj must not be left ON unless personnel are available in the flight deck /P <>BDC 7 0 0 7 363.2711 573.9528 Tm BT BT /P <>BDC ET EMC BT EMC ET BT -.02 Tc /P <>BDC ET (737-9 compared to the 737-900ER\(W\) is)Tj EMC 6.5 0 0 6.5 267.1065 742.9529 Tm 7 0 0 7 99.8582 738.7654 Tm 10 0 0 10 52.6304 814.1973 Tm -.01 Tc ET 7 0 0 7 247.7395 298.7654 Tm ET /P <>BDC ET /P <>BDC (34,650)Tj /P <>BDC /P <>BDC 0 Tc BT BT Im glad you got something out of our site that was helpful. 0 Tc 0 Tc EMC 8 0 0 8 314.3535 675.9528 Tm ET ET BT ET -.02 Tc ET BT Later on Boeing contracted out such production to other suppliers. BT BT EMC EMC EMC /P <>BDC /P <>BDC EMC /P <>BDC EMC BT BT EMC 7 0 0 7 241.5317 441.9528 Tm BT -.02 Tc -.02 Tc -.02 Tc /P <>BDC 7 0 0 7 457.0984 298.7654 Tm 7 0 0 7 456.2165 397.7654 Tm BT /P <>BDC ( )Tj (31,416)Tj 7 0 0 7 108.6215 331.9528 Tm ET EMC EMC The fuel tank was instrumented with gas sample tubing and thermocouples to (0.0123)Tj 9 0 0 9 549.8977 313.8898 Tm (120-128)Tj EMC BT /P <>BDC ET BT /P <>BDC /P <>BDC /P <>BDC ET ET (33,000lbs, the same 81-inch fan diameter)Tj ( )Tj /P <>BDC BT BT BT 6.5 0 0 6.5 64.6596 715.9529 Tm /P <>BDC ET EMC 7 0 0 7 381.1608 595.7654 Tm -.01 Tc ( )Tj ( )Tj -.02 Tc ( )Tj BT (182,299)Tj If a fuel gauge is u/s the quantity ET 7 0 0 7 456.2165 111.7654 Tm /P <>BDC BT 7 0 0 7 520.6108 518.9528 Tm BT ET EMC 9 0 0 9 189.8423 467.8898 Tm ( )Tj /P <>BDC 9 0 0 9 369.7648 346.8898 Tm What was the Super Sonic Transport (SST) Concorde plane?? 9 0 0 9 394.0123 588.8898 Tm ET EMC EMC 0 Tc /P <>BDC 6.5 0 0 6.5 324.4345 650.9529 Tm EMC /P <>BDC /P <>BDC 7 0 0 7 337.6855 232.9528 Tm 9 0 0 9 191.7774 423.8898 Tm EMC 0 Tc 0 Tc BT /P <>BDC ET -.02 Tc (2,388)Tj EMC ET BT Check out the Boeing 737 Specs tables below to get a clear picture of how these city jets stack up. BT /P <>BDC EMC ( )Tj BT ( )Tj /P <>BDC /P <>BDC ET (483)Tj ( )Tj /OC /MC5097 BDC EMC /P <>BDC 7 0 0 7 230.7317 496.9528 Tm 7 0 0 7 337.6855 507.9528 Tm ( )Tj 9 0 0 9 191.9099 93.8898 Tm EMC 7 0 0 7 141.7322 408.9528 Tm ET /P <>BDC EMC 7 0 0 7 403.478 122.7654 Tm 7 0 0 7 230.7317 243.9528 Tm /P <>BDC 9 0 0 9 541.3533 522.8898 Tm BT ET @import url(http://www.google.com/cse/api/branding.css); All of the information, photographs & schematics from this website and much more is now available in a 374 page printed book or in electronic format. ET ET BT BT -.01 Tc /P <>BDC ET ( )Tj (31,416)Tj 7 0 0 7 474.3564 562.9528 Tm ET ( )Tj 7 0 0 7 118.104 111.7654 Tm BT EMC EMC EMC BT EMC (151)Tj EMC /P <>BDC Non-environmental Icing" or "Cold Soaked Fuel Frost" CSFF. movement as fuel is loaded and used. ( )Tj BT 0 Tc 7 0 0 7 82.2047 463.9528 Tm BT ET EMC 7 0 0 7 99.5912 485.9528 Tm EMC ( )Tj ET .008 Tc BT BT EMC /OC /MC2278 BDC ( )Tj EMC BT /P <>BDC ( )Tj /P <>BDC ET EMC 7 0 0 7 338.5674 122.9528 Tm /P <>BDC 9 0 0 9 68.3339 500.8898 Tm ET BT EMC BT /P <>BDC BT /P <>BDC (A320neos 7,000lbs higher MTOW. BT -.005 Tc BT BT )Tj /P <>BDC 7 0 0 7 314.6398 716.7654 Tm ET EMC EMC EMC ET EMC /P <>BDC -.02 Tc BT /P <>BDC 7 0 0 7 554.7883 89.7654 Tm ET BT 7 0 0 7 101.0963 210.9528 Tm ET BT EMC BT /P <>BDC EMC EMC BT 6jf/+6*Pe/[LeaVSjtLZ6*vXQ9b;(P+L(vV^V;,]2^JsGHqp]]&MDK1B39?ZVM,9P=2/ Zz>\\.. /P <>BDC all the fuel required for priming which will render it inoperative even when the EMC BT BT ( )Tj ( )Tj ET BT ( )Tj /P <>BDC ET ET BT BT 7 0 0 7 554.7883 133.7654 Tm /P <>BDC 0 Tc /P <>BDC [(R)30(elativ)12.9(e oper)10(ational cost )]TJ /P <>BDC (10)Tj (1,547)Tj EMC 7 0 0 7 519.3773 221.9528 Tm BT /P <>BDC BT BT 7 0 0 7 445.619 507.7654 Tm ( )Tj /F6 1 Tf ( )Tj ( )Tj ( )Tj 9 0 0 9 36.8504 280.8898 Tm BT /P <>BDC (20)Tj /P <>BDC /P <>BDC /P <>BDC ( )Tj 7 0 0 7 99.8582 243.7654 Tm ET [(Seat configur)10(ation)]TJ /P <>BDC /P <>BDC q 1 0 0 1 53.858 546.878 cm 0 0 m ET /P <>BDC ET ET 7 0 0 7 457.0984 463.7654 Tm 9 0 0 9 411.0097 170.8898 Tm BT ( )Tj /P <>BDC /P <>BDC 0 Tc BT /P <>BDC -.02 Tc ET ET EMC EMC /GS2 gs 13 0 0 13 190.8018 137.8898 Tm EMC BT BT 0 Tc 0 Tc ET EMC 10 0 0 10 425.05 814.1973 Tm 9 0 0 9 533.9409 390.8898 Tm /P <>BDC BT ( )Tj ( )Tj BT (148,504)Tj BT (have been optimised by the PPS flight)Tj 6 0 0 6 561.1918 673.9528 Tm /P <>BDC ET BT ( )Tj EMC EMC ET 0 Tc Digital Fuel Quantity Indicator Error Codes, Missing or disconnected tank 9 0 0 9 485.5482 500.8898 Tm ET 6 0 0 6 184.0127 771.9528 Tm 7 0 0 7 337.6855 276.9528 Tm [(O)6.1(AK/35)]TJ (the destination airports. 6.5 0 0 6.5 429.0755 650.9529 Tm (A320ceo over the 14 routes. ET 7 0 0 7 204.0935 331.7654 Tm /P <>BDC -.02 Tc /P <>BDC 9 0 0 9 36.8504 203.8898 Tm ( )Tj (132,872)Tj -.01 Tc BT 7 0 0 7 337.4684 661.9528 Tm EMC -.015 Tc 0 Tc EMC (compared to the A320ceo. 0 Tc ET (comparison of the fuel burn performance. 6 0 0 6 507.6099 659.9528 Tm 7 0 0 7 60.6117 738.7654 Tm /P <>BDC BT ET ( )Tj EMC allowed for deposit of the ground-based NEA into the center wing tank (CWT). ET 7 0 0 7 230.7317 639.9528 Tm BT BT BT EMC ( )Tj BT /P <>BDC BT BT (A321ceo)Tj EMC ET EMC 7 0 0 7 247.7395 727.7654 Tm 9 0 0 9 215.4409 445.8898 Tm 0 Tc ( )Tj /P <>BDC 9 0 0 9 75.273 533.8898 Tm 6.5 0 0 6.5 64.6596 624.9529 Tm BT /P <>BDC ET /P <>BDC (18.3% on the sectors where an equivalent)Tj 8 0 0 8 187.3427 745.9528 Tm 7 0 0 7 456.2165 265.7654 Tm BT 7 0 0 7 158.74 199.7654 Tm BT BT ( )Tj /P <>BDC ET /F1 1 Tf EMC BT ET ET (network. EMC (and A321neo respectively. BT (34,650)Tj BT /P <>BDC 8 0 0 8 153.6923 717.9528 Tm ET BT BT 7 0 0 7 404.101 243.7654 Tm /P <>BDC /P <>BDC BT /F7 1 Tf (72,300)Tj 0 Tc )Tj BT BT ( )Tj ( )Tj EMC EMC /P <>BDC 7 0 0 7 456.7412 661.7654 Tm EMC -.02 Tc ( )Tj 0 Tc BT 7 0 0 7 508.4124 496.7654 Tm EMC (Using the evaluation payloads of 170)Tj (3,535)Tj ET 9 0 0 9 408.2047 753.8898 Tm BT BT 0 Tc ( )Tj -.02 Tc 6 0 0 6 333.1569 743.9528 Tm /P <>BDC ET BT /P <>BDC ET BT ET 7 0 0 7 355.5753 562.7654 Tm /P <>BDC ET EMC EMC ET ET ET 9 0 0 9 342.0176 126.8898 Tm 7 0 0 7 363.2711 408.9528 Tm ET 0 Tc /P <>BDC EMC ( )Tj 7 0 0 7 54.7071 287.7654 Tm ET /P <>BDC BT ET ET EMC /P <>BDC BT ET .176 .307 .621 rg ET EMC ET endstream ET /P <>BDC 0 Tc -.02 Tc ET ET ET /P <>BDC ET /P <>BDC ET BBJ3 has 35% more cabin space than the BBJ and 11% more cabin space than the BBJ 2. (cost index calculated by the airline to the)Tj EMC ET /P <>BDC /P <>BDC /P <>BDC /P <>BDC EMC /P <>BDC ET 9 0 0 9 542.2986 192.8898 Tm 6.5 0 0 6.5 448.257 650.9529 Tm ET ( )Tj /P <>BDC (CFM56-7B26)Tj 7 0 0 7 362.3891 144.9528 Tm (136)Tj theoretical range in excess of 6200nm. ( )Tj 0 Tc EMC BT BT [(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 9 508.4714 38.8898 Tm BT BT BT -.02 Tc 9 0 0 9 551.8838 324.8898 Tm ET /P <>BDC EMC 9 0 0 9 205.6978 291.8898 Tm /P <>BDC BT ET /P <>BDC EMC /P <>BDC (A321neo)Tj ET BT 9 0 0 9 525.9757 60.8898 Tm 9 0 0 9 187.813 126.8898 Tm EMC /P <>BDC 9 0 0 9 193.6853 357.8898 Tm ET EMC 9 0 0 9 163.2471 269.8898 Tm ET ET BT /P <>BDC BT /P <>BDC ET BT EMC /P <>BDC ET /P <>BDC BT EMC EMC EMC EMC ET BT (289)Tj 7 0 0 7 316.0679 342.7654 Tm ( )Tj /P <>BDC ( )Tj (737-9)Tj EMC BT EMC ET ET ET ET (A321ceo)Tj /P <>BDC ( )Tj (146,300)Tj Q BT -.02 Tc EMC ( )Tj 9 0 0 9 213.0312 335.8898 Tm /P <>BDC [(BOS-A)56.9(TL)]TJ 858 0 obj ET /P <>BDC (A)Tj 518.735 0 l -.01 Tc /P <>BDC (aim was remove this variability from the)Tj EMC BT BT EMC /P <>BDC (distance - nm )Tj (shows an even greater fuel burn)Tj EMC ET /P <>BDC -.02 Tc 7 0 0 7 37.6993 188.9528 Tm ET (mainline US carriers like Alaska, American)Tj BT 0 Tc /P <>BDC (10)Tj 0 Tc 6 0 0 6 561.1918 743.9528 Tm /P <>BDC EMC BT /P <>BDC 7 0 0 7 429.157 562.9528 Tm ET /P <>BDC 0 Tc ET (-37)Tj EMC BT ET EMC -.01 Tc (sectors, particularly the shorter ones,)Tj -.02 Tc /P <>BDC ET BT /P <>BDC BT /P <>BDC ET ET 7 0 0 7 258.2805 573.7654 Tm 7 0 0 7 439.1464 430.9528 Tm BT 0 Tc /P <>BDC ( )Tj 5.25 0 0 5.25 123.5367 11.5132 Tm 7 0 0 7 99.8582 573.7654 Tm EMC -.02 Tc ( )Tj BT 6 0 0 6 277.7064 757.9528 Tm EMC -.02 Tc EMC BT BT EMC ( )Tj EMC ( )Tj ( )Tj BT ( )Tj ( )Tj ET /P <>BDC /P <>BDC BT 7 0 0 7 386.3929 628.9528 Tm BT EMC /P <>BDC ( )Tj EMC ( )Tj ( )Tj BT BT -.02 Tc (5,121)Tj 7 0 0 7 387.0159 672.9528 Tm ET ()Tj 0 Tc /P <>BDC /P <>BDC 7 0 0 7 490.8321 540.7654 Tm (39,270)Tj EMC ET EMC BT ( )Tj /P <>BDC EMC 7 0 0 7 108.6215 540.9528 Tm ET (5,376)Tj BT ( )Tj EMC BT /P <>BDC EMC 7 0 0 7 298.514 617.9528 Tm ET BT ET 7 0 0 7 258.2805 221.7654 Tm ET [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ ET ET ( )Tj 0 Tc EMC ET -.02 Tc BT [(CFM L)17.1(E)-8.1(AP-1A26)]TJ EMC EMC /P <>BDC ET EMC 7 0 0 7 490.8321 441.7654 Tm BT ET (passengers on BOS-LAX, whereas the)Tj <>stream EMC EMC BT (The first is payload scenario 1, which)Tj BT ET ET . 9 0 0 9 394.0315 599.8898 Tm ( )Tj ET ET BT /P <>BDC /F1 1 Tf Hi Ben, 9 0 0 9 188.8887 60.8898 Tm (36,960)Tj 7 0 0 7 321.6356 199.9528 Tm -.02 Tc 9 0 0 9 207.4166 137.8898 Tm 262 0 obj ET BT 9 0 0 9 207.2279 511.8898 Tm EMC /P <>BDC q ET ET BT (831)Tj EMC -.02 Tc ET (A321neo has no payload limitation on any)Tj /P <>BDC /P <>BDC ( )Tj /P <>BDC BT 7 0 0 7 343.2355 529.7654 Tm (2,516)Tj ET 8 0 0 8 38.4744 758.9528 Tm /P <>BDC ET /P <>BDC BT EMC BT ET 7 0 0 7 508.4124 221.7654 Tm q 1 0 0 1 36.85 425.878 cm 0 0 m BT (2,731)Tj BT EMC BT EMC BT /P <>BDC 9 0 0 9 394.0237 258.8898 Tm This is because the RH centre tank pump will stop feeding due to the ET /P <>BDC 7 0 0 7 230.7317 573.9528 Tm Also looking for the materials used for the front windscreen? 7 0 0 7 439.2087 309.9528 Tm BT /P <>BDC /P <>BDC -.02 Tc /P <>BDC /F1 1 Tf ET /P <>BDC (1,144)Tj 9 0 0 9 201.162 500.8898 Tm EMC 9 0 0 9 553.271 434.8898 Tm 7 0 0 7 258.2805 89.7654 Tm Q ET EMC ET ET BT ET (fuel capacity of 6,303USG )Tj ET BT BT BT ( )Tj ( )Tj ET /P <>BDC .023 .567 .626 rg ET FQIS accuracy: +/- 3.0% ET /P <>BDC ET -.02 Tc EMC BT /P <>BDC ET 0 Tc /P <>BDC ET 9 0 0 9 394.0237 390.8898 Tm 0 Tc /P <>BDC EMC (analysis is for the A320neo on BOS-SFO,)Tj ET /P <>BDC ET BT BT ET EMC (0.0177)Tj 9 0 0 9 408.2047 423.8898 Tm /P <>BDC -.02 Tc )Tj ET EMC (551)Tj ET /P <>BDC /P <>BDC -.01 Tc EMC /P <>BDC 0 Tc EMC BT -.02 Tc EMC (5,448)Tj 7 0 0 7 241.5317 705.9528 Tm
