-.02 Tc EMC BT ET 6 0 0 6 215.373 715.9528 Tm /P <>BDC ET 9 0 0 9 213.8067 159.8898 Tm ET 9 0 0 9 516.3894 247.8898 Tm BT For land the 800 needs 1372 meters or 4,501.26 feet. BT BT ET BT BT (0.0141)Tj /P <>BDC EMC /P <>BDC (used is 16/30/114, giving a seat count of)Tj -.01 Tc 9 0 0 9 411.0097 555.8898 Tm (A320neo will be evaluated with the same)Tj (152,800)Tj /P <>BDC ET f /OC /MC2278 BDC /P <>BDC BT ET EMC /P <>BDC BT In contrast, the 737-8s performance)Tj EMC 7 0 0 7 439.7405 507.9528 Tm EMC BT BT 0 Tw /P <>BDC EMC EMC BT BT BT 9 0 0 9 394.0315 522.8898 Tm EMC 53.858 30.994 518.735 773.858 re 7 0 0 7 95.225 11.5132 Tm BT ET q 0 Tc (737-8)Tj /P <>BDC ET BT EMC -.01 Tc ( )Tj ET 7 0 0 7 490.5101 562.9528 Tm (737-9)Tj -.01 Tc BT /P <>BDC BT 7 0 0 7 247.7395 320.7654 Tm /P <>BDC BT /P <>BDC 8 0 0 8 355.1264 760.7654 Tm ET ( )Tj -.02 Tc ET BT h /P <>BDC /P <>BDC BT /P <>BDC EMC EMC [(CFM L)17.1(E)-8.1(AP-1A26)]TJ EMC BT EMC 7 0 0 7 508.4124 496.7654 Tm EMC -.01 Tc EMC EMC (differences in the flight times. EMC -.02 Tc ET BT EMC /P <>BDC /P <>BDC 9 0 0 9 544.934 49.8898 Tm /P <>BDC BT ET 6.5 0 0 6.5 429.8944 598.9529 Tm ( )Tj /P <>BDC ET EMC EMC ET 0 Tc /P <>BDC (1,272)Tj ( )Tj /P <>BDC 0 Tc ET ( )Tj /OC /MC200 BDC /P <>BDC (A321ceo)Tj ( )Tj BT 0 Tc BT (the analysis is 20/29/143, so a total of 192)Tj /Artifact <>BDC BT ET ( )Tj BT endstream /P <>BDC ET /P <>BDC W n EMC /P <>BDC BT EMC EMC on 5 Nov 1990 have been destroyed on the ground due to explosions in the empty EMC 737-600/-700/-800/-900 without densitometer: BT 0 Tc (5,096)Tj BT BT BT BT 0 Tc EMC BT ET BT EMC BT ( )Tj ET BT ET BT (A320ceo)Tj BT (310,080)Tj EMC (The first-class layout uses four-abreast)Tj /P <>BDC 0 Tc -.02 Tc BT EMC -.005 Tc /P <>BDC /P <>BDC EMC /P <>BDC /P <>BDC BT ( )Tj 8 0 0 8 270.7815 771.9528 Tm /P <>BDC BT EMC ET ET /P <>BDC BT ( )Tj 7 0 0 7 258.2805 617.7654 Tm BT /P <>BDC BT 7 0 0 7 338.3085 342.9528 Tm BT ET ET /P <>BDC EMC 9 0 0 9 545.7273 731.8898 Tm ET 7 0 0 7 539.8962 496.9528 Tm 7 0 0 7 404.101 111.7654 Tm BT ( )Tj 7 0 0 7 521.4928 672.9528 Tm ( )Tj ( )Tj 0 Tc 7 0 0 7 491.4046 188.9528 Tm ET EMC 7 0 0 7 314.6398 529.7654 Tm ( )Tj EMC 2002-19-52 which requires the crew to maintain certain minimum fuel ( )Tj BT 7 0 0 7 163.8846 11.5132 Tm (148,504)Tj /P <>BDC BT ( )Tj /P <>BDC 9 0 0 9 270.3219 720.8898 Tm BT /P <>BDC BT (1,130)Tj EMC 0 Tc EMC ET ( )Tj ET 7 0 0 7 386.3929 716.9528 Tm [(Oper)10(ating Assumptions )]TJ /P <>BDC (737-8 has a 0.8-3.0% higher trip fuel burn than)Tj BT EMC EMC /P <>BDC 7 0 0 7 554.7883 485.7654 Tm /P <>BDC BT (westerly direction so that all operate)Tj /P <>BDC 0 Tc -.02 Tc (orders, while the 737-800 and 737-900ER)Tj /P <>BDC /P <>BDC ET -.02 Tc 9 0 0 9 543.767 93.8898 Tm EMC ET BT 9 0 0 9 53.8582 357.8898 Tm ET 0 Tc /P <>BDC 0 Tc ET ( )Tj 9 0 0 9 394.0157 203.8898 Tm BT /P <>BDC 0 Tc BT /P <>BDC ET ( )Tj /P <>BDC 9 0 0 9 522.5613 38.8898 Tm ET /P <>BDC BT 0 Tc ET EMC (some minor aerodynamic improvements)Tj /P <>BDC My simulation is focused on postcrash fires. EMC EMC 7 0 0 7 199.5784 738.7654 Tm /P <>BDC 9 0 0 9 53.8578 445.8898 Tm 9 0 0 9 374.887 346.8898 Tm (of aircraft types that are of equal size. BT 304.725 420.96 m 7 0 0 7 247.7395 309.7654 Tm EMC BT ( )Tj ET 0 Tc /P <>BDC BT ( )Tj 9 0 0 9 194.6573 456.8898 Tm ( )Tj (I)Tj BT ET /P <>BDC BT ET ET 6 0 0 6 191.3929 771.9528 Tm 9 0 0 9 68.0314 258.8898 Tm BT For instance, What is the Aluminium alloy 7055 basis values ? BT ( )Tj ( )Tj ( )Tj BT EMC The Boeing 737-800 is a twin-engined short-to-medium-range narrowbody airliner with a capacity of maximum 189 passengers produced by the American manufacturer Boeing Commercial Airplanes. ET BT BT 0 Tc /P <>BDC BT /P <>BDC 7 0 0 7 99.8582 617.7654 Tm EMC 0 Tc 9 0 0 9 51.0315 379.8898 Tm /P <>BDC 9 0 0 9 411.0097 335.8898 Tm ET BT EMC BT /P <>BDC ET BT BT 13 0 0 13 215.4409 445.8898 Tm ( )Tj to maintain C of G balance. -.02 Tc EMC BT BT ET ET EMC -.02 Tc ( )Tj BT BT ( )Tj 7 0 0 7 315.1859 89.7654 Tm I not sure what you mean by a and b basis allowable. ET .0081 Tc ET 7 0 0 7 247.7395 188.7654 Tm /P <>BDC ET 0 Tc /P <>BDC EMC BT EMC /P <>BDC EMC 9 0 0 9 394.0237 181.8898 Tm 7 0 0 7 321.6356 276.9528 Tm ET EMC 9 0 0 9 394.0237 390.8898 Tm 0 Tc 7 0 0 7 89.3229 342.7654 Tm /P <>BDC 789 0 obj ( )Tj (282)Tj ET 0 Tc /P <>BDC 9 0 0 9 361.5742 192.8898 Tm ( )Tj BT 9 0 0 9 232.4408 775.8898 Tm .023 .567 .626 rg ( )Tj EMC S EMC EMC ET EMC /P <>BDC 9 0 0 9 423.3885 401.8898 Tm 9 0 0 9 183.3893 456.8898 Tm EMC /P <>BDC BT 9 0 0 9 36.8504 93.8898 Tm BT BT 7 0 0 7 364.1531 78.9528 Tm ( )Tj 0 Tc 7 0 0 7 99.8582 584.7654 Tm ET ( )Tj BT 7 0 0 7 241.2727 166.9528 Tm ET BT (136)Tj 8 0 0 8 365.7704 619.9528 Tm (to in-flight service levels will increase seat)Tj /P <>BDC ( )Tj /P <>BDC BT /P <>BDC (7,379)Tj /OC /MC5095 BDC /P <>BDC EMC 7 0 0 7 343.2355 496.7654 Tm EMC BT ET 7 0 0 7 554.7883 562.7654 Tm ( )Tj .0081 Tc BT 9 0 0 9 53.8578 357.8898 Tm EMC ET support combustion. 0 841.89 609.449 -841.89 re EMC /P <>BDC 5.25 0 0 5.25 73.853 11.5132 Tm 8 0 0 8 38.4438 605.9528 Tm 9 0 0 9 375.0299 434.8898 Tm higher. /P <>BDC (A321ceo)Tj ET BT ( )Tj /P <>BDC (services. /P <>BDC BT /P <>BDC BT /P <>BDC (150)Tj 7 0 0 7 54.5916 738.7654 Tm EMC EMC /P <>BDC BT BT 7 0 0 7 539.9176 11.5129 Tm EMC BT /P <>BDC 7 0 0 7 343.2355 507.7654 Tm /F1 1 Tf ( )Tj -.02 Tc /P <>BDC EMC /P <>BDC ( )Tj BT A series of ten tests were performed (five flight, BT EMC ( )Tj ET /P <>BDC /P <>BDC (977)Tj EMC /P <>BDC EMC EMC ET /P <>BDC ET 9 0 0 9 186.0514 60.8898 Tm 7 0 0 7 54.5916 540.7654 Tm ET 0 Tc 6.5 0 0 6.5 397.0428 532.9529 Tm ( )Tj (1,272)Tj ET /P <>BDC ET EMC )Tj ET (0.0129)Tj EMC ( )Tj EMC -.02 Tc EMC 7 0 0 7 474.3564 606.9528 Tm ET 9 0 0 9 232.4217 214.8898 Tm /P <>BDC /P <>BDC /F1 1 Tf /P <>BDC (737-900ER\(W\). 9 0 0 9 553.4085 203.8898 Tm 9 0 0 9 394.0123 599.8898 Tm ET (maximum fuel capacity, the A320neo)Tj EMC BT ET BT ( )Tj BT ( )Tj -.02 Tc EMC EMC BT EMC 7 0 0 7 230.7317 100.9528 Tm ( )Tj ET (178)Tj /P <>BDC EMC /P <>BDC ET ( )Tj EMC BT EMC /P <>BDC /P <>BDC BT /P <>BDC /P <>BDC /P <>BDC /P <>BDC BT BT ET ( )Tj BT BT BT ( )Tj 0 Tc ( )Tj ET . 7 0 0 7 298.514 584.9528 Tm ( )Tj /P <>BDC ( )Tj ET BT EMC 9 0 0 9 246.595 49.8898 Tm ( )Tj 0 Tc ET /P <>BDC BT EMC 9 0 0 9 394.0315 148.8898 Tm ET EMC BT EMC 6.5 0 0 6.5 488.8955 532.9529 Tm /P <>BDC BT BT ET 8 0 0 8 187.3427 675.9528 Tm 9 0 0 9 526.2638 401.8898 Tm BT 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: ET 7 0 0 7 321.6356 221.9528 Tm (900ER\(W\) are the only aircraft in the)Tj BT /P <>BDC ( )Tj 6.5 0 0 6.5 227.9655 624.9529 Tm /P <>BDC ET allowed for deposit of the ground-based NEA into the center wing tank (CWT). 7 0 0 7 196.5683 320.7654 Tm /P <>BDC ( )Tj (impact on the fuel cost per ASM. EMC ET ( A)Tj EMC ET /P <>BDC /P <>BDC ( )Tj BT BT [(BOS-C)-8.1(V)18.1(G)]TJ -.01 Tc ET 6 0 0 6 277.9402 687.9528 Tm 7 0 0 7 518.4953 408.9528 Tm 9 0 0 9 232.4217 511.8898 Tm 6 0 0 6 61.517 729.9528 Tm (1,825)Tj BT /P <>BDC EMC ( )Tj (cost compared to fuel. 0 Tc 0 Tc /P <>BDC /P <>BDC ( )Tj /P <>BDC -.07 Tc q 1 0 0 1 36.858 403.878 cm 0 0 m ET EMC /OC /MC3431 BDC EMC ( )Tj ET BT /P <>BDC ET EMC 9 0 0 9 530.5354 665.8898 Tm ET EMC BT (0.0115)Tj 7 0 0 7 537.7804 441.9528 Tm 7 0 0 7 343.2355 694.7654 Tm 8 0 0 8 187.3427 577.9528 Tm /P <>BDC (A321neo)Tj /P <>BDC (A)Tj 0 Tc EMC 7 0 0 7 430.039 716.9528 Tm BT 56 0 0 56 36.8606 622.1944 Tm EMC EMC -.02 Tc BT ET ET 137 )Tj 9 0 0 9 165.1533 258.8898 Tm ET -.02 Tc [(S)8(eats)]TJ <> ( )Tj 9 0 0 9 548.5375 225.8898 Tm EMC ( )Tj ET ET /P <>BDC 7 0 0 7 247.7395 210.7654 Tm EMC ET /P <>BDC ET /P <>BDC 9 0 0 9 36.8504 214.8898 Tm 7 0 0 7 508.4124 320.7654 Tm BT EMC ET (1,161)Tj ET BT EMC BT BT 9 0 0 9 181.5424 71.8898 Tm ( )Tj EMC 7 0 0 7 54.7071 694.7654 Tm BT /P <>BDC BT ET BT BT (282-294)Tj ET EMC 7 0 0 7 326.2278 606.9528 Tm 7 0 0 7 199.5784 298.7654 Tm ET ET EMC 9 0 0 9 215.4409 357.8898 Tm ET /P <>BDC (City-pair)Tj /P <>BDC ( )Tj BT (39,270)Tj 9 0 0 9 201.2426 445.8898 Tm (average for the month of June, and the)Tj ET 0 Tc ET 7 0 0 7 54.7071 232.7654 Tm ET 7 0 0 7 179.5605 518.9528 Tm BT BT 9 0 0 9 534.395 599.8898 Tm /P <>BDC ET .151 .147 .15 rg /P <>BDC BT -.02 Tc EMC /P <>BDC BT ET BT /P <>BDC /P <>BDC ET (37,653)Tj ET endobj /P <>BDC .151 .147 .15 rg ET /P <>BDC EMC ( )Tj BT 7 0 0 7 363.2711 507.9528 Tm ET (operating the 737 has increased its)Tj 0 Tc ( )Tj BT /P <>BDC BT EMC 19.841 0 l BT BT 7 0 0 7 193.1059 485.9528 Tm EMC /P <>BDC ET 9 0 0 9 394.0237 302.8898 Tm 7 0 0 7 491.7142 331.7654 Tm ( N)Tj EMC EMC ET ET BT 7 0 0 7 258.2805 397.7654 Tm EMC (214,730)Tj 7 0 0 7 491.4046 232.9528 Tm /P <>BDC /P <>BDC .151 .147 .15 rg BT BT EMC /P <>BDC ET /P <>BDC ET BT 7 0 0 7 158.74 441.7654 Tm ET EMC EMC ET W n /P <>BDC (The second comparison is payload)Tj BT ET /P <>BDC BT EMC -.02 Tc ET /P <>BDC EMC ET For example, if the fuel tank maximum capacity is 10,000 KG, then the tolerance of the gauging is 0.03 (airplane with analog indicators) * 10000 = 300 KG. EMC /P <>BDC ET ET BT /P <>BDC /P <>BDC EMC 0 Tc /P <>BDC ( )Tj remain illuminated for more than 19 seconds then this is probably what has /P <>BDC ET BT BT 9 0 0 9 53.8578 302.8898 Tm /P <>BDC EMC ET ET ET EMC ( )Tj ET ET 9 0 0 9 232.4217 104.8898 Tm /P <>BDC EMC 7 0 0 7 380.2788 408.7654 Tm 9 0 0 9 394.0123 588.8898 Tm ( )Tj EMC -.02 Tc 9 0 0 9 53.8338 38.8898 Tm how can i know the material of 737NGs nose landing gear lower drag strut?thank you. ET 9 0 0 9 215.4409 93.8898 Tm ET BT [(A3)24.9(21neo v)12.9(ersus 7)-33(3)8.1(7-9 )]TJ ( )Tj 9 0 0 9 162.5427 412.8898 Tm (104)Tj -.01 Tc ET BT BT 0 Tc /P <>BDC ET /P <>BDC -.02 Tc 0 Tc 0 Tc /P <>BDC /P <>BDC 9 0 0 9 546.3754 159.8898 Tm 7 0 0 7 554.7883 705.7654 Tm BT -.02 Tc BT EMC -.02 Tc EMC (163)Tj ( )Tj EMC 8 0 0 8 225.1837 633.9528 Tm -.02 Tc 7 0 0 7 508.4124 661.7654 Tm ET -.02 Tc 0 Tc ( )Tj )Tj ET At engine idle, the system tolerance can be 12%. 9 0 0 9 215.4409 236.8898 Tm ET 0 Tc BT 7 0 0 7 403.478 738.7654 Tm /GS2 gs 7 0 0 7 279.1575 188.9528 Tm EMC 10 0 0 10 52.7604 814.1973 Tm (not been used for the A321ceo against the)Tj 7 0 0 7 247.7395 375.7654 Tm (0.0124)Tj /P <>BDC (stage lengths or tracked distances of)Tj ET ET ( )Tj EMC BT BT EMC EMC 9 0 0 9 68.0071 159.8898 Tm EMC EMC 9 0 0 9 214.4188 478.8898 Tm 6.5 0 0 6.5 295.5027 565.9529 Tm EMC 7 0 0 7 537.7804 419.9528 Tm ( )Tj ( )Tj ( )Tj 7 0 0 7 383.0719 716.7654 Tm BT ( )Tj EMC BT ( )Tj ET must be switched OFF when both LP lights illuminate. /P <>BDC EMC 9 0 0 9 394.0157 401.8898 Tm BT /P <>BDC ( )Tj BT ET BT /F6 1 Tf EMC 7 0 0 7 82.8504 342.9528 Tm /P <>BDC BT /P <>BDC EMC /P <>BDC EMC for water. ( )Tj EMC EMC ET BT ( )Tj This would make)Tj BT /P <>BDC -.02 Tc Centre tank pumps ET /P <>BDC EMC ET BT BT ET ( )Tj /Artifact <>BDC BT ( )Tj 7 0 0 7 241.5317 529.9528 Tm Q /P <>BDC ET ( )Tj (The main operating parameters are: )Tj ( )Tj ET ET /P <>BDC BT EMC W n ( )Tj EMC ET BT )Tj EMC 8 0 0 8 314.3535 717.9528 Tm BT 0 Tc 9 0 0 9 566.3417 423.8898 Tm ( )Tj 9 0 0 9 550.6401 401.8898 Tm ET 7 0 0 7 158.74 518.7654 Tm BT (the two scenarios are detailed )Tj /P <>BDC EMC EMC EMC ET ( )Tj EMC BT ( )Tj 9 0 0 9 558.7096 390.8898 Tm ( )Tj ET ET /P <>BDC EMC 7 0 0 7 457.0984 188.7654 Tm /OC /MC2261 BDC EMC ( )Tj ET 7 0 0 7 473.4744 518.9528 Tm ( )Tj ( )Tj EMC 7 0 0 7 99.8582 683.7654 Tm BT BT The NG series are prone to "Upper Wing Surface /P <>BDC /P <>BDC ET ( )Tj BT 7 0 0 7 491.4046 100.9528 Tm ( )Tj (CFM56-7B27B3)Tj 0 Tc 6 0 0 6 184.072 659.9528 Tm ( )Tj /P <>BDC BT 6.5 0 0 6.5 375.6529 689.9529 Tm EMC ET EMC (makes a flight-for-flight comparison)Tj /P <>BDC BT ( )Tj EMC ( )Tj BT -.02 Tc /P <>BDC 0 Tc EMC ET EMC /P <>BDC EMC ( )Tj ET EMC EMC BT 7 0 0 7 379.3969 78.7654 Tm BT ( )Tj 7 0 0 7 54.7071 133.7654 Tm 0 Tc BT ET ( )Tj ET 6 0 0 6 442.408 771.9528 Tm (alternate and 45 minutes continued cruise. BT -.02 Tc BT /P <>BDC BT 0 Tc 6.5 0 0 6.5 64.6596 742.9529 Tm ET ET /P <>BDC BT -.02 Tc EMC BT 7 0 0 7 99.8582 595.7654 Tm ET /P <>BDC (403)Tj 6.5 0 0 6.5 54.877 572.9529 Tm BT (28,000lbs compared to 27,000lbs for the)Tj EMC ET ET /P <>BDC ( )Tj -.02 Tc /P <>BDC -.02 Tc EMC 9 0 0 9 178.8353 478.8898 Tm ( )Tj 0 Tc BT ET /P <>BDC ( )Tj BT ET /P <>BDC [(737-900E)-33(R)]TJ ET BT /P <>BDC -.01 Tc (capacity of 6,353USG, giving it a range of)Tj ET /P <>BDC ET 0 Tc /P <>BDC ET ( )Tj EMC ( )Tj ET ET EMC ( )Tj 6 0 0 6 143.5527 673.9528 Tm .008 Tc BT 0 Tc BT ET /F4 1 Tf BT /P <>BDC ET /P <>BDC ET EMC ET EMC The Boeing 737-800 is an example of an average sized airplane. EMC ET EMC BT /P <>BDC ( )Tj /P <>BDC /P <>BDC EMC BT EMC 9 0 0 9 209.6398 489.8898 Tm 7 0 0 7 379.3969 144.7654 Tm 7 0 0 7 338.6433 419.7654 Tm The 800 being based of the 400 is designed for short routes. ET ET EMC ( )Tj -.01 Tc ET 7 0 0 7 298.3957 430.9528 Tm /P <>BDC 9 0 0 9 75.3887 489.8898 Tm ET /P <>BDC EMC BT /P <>BDC 9 0 0 9 195.0251 434.8898 Tm ( )Tj EMC BT BT EMC 7 0 0 7 158.74 507.7654 Tm 7 0 0 7 469.2222 11.5129 Tm (tracked distance, ESAD, and the difference)Tj 0 Tc ET movement as fuel is loaded and used. EMC 7 0 0 7 456.2165 375.7654 Tm The AFM limits are higher, but not normally achievable with standard SG's. /P <>BDC -.02 Tc -.02 Tc 9 0 0 9 538.8793 368.8898 Tm EMC 0 Tc 0 Tc (CFM56-7B26)Tj BT 7 0 0 7 82.8504 78.9528 Tm

Education System Rankings By State, Submit Wedding To Brides Magazine, Cars For Sale In Stockton, Ca Under $1,000, Articles OTHER