ET EMC ET (2,729)Tj 7 0 0 7 158.74 199.7654 Tm ET /P <>BDC EMC ( )Tj /P <>BDC ( )Tj 6 0 0 6 277.7064 715.9528 Tm BT /P <>BDC BT -.01 Tc BT ( )Tj EMC 8 0 0 8 531.9995 82.8898 Tm (over 400 MAXs, and Airbus a similar)Tj 9 0 0 9 215.433 379.8898 Tm ET ET ( )Tj BT /P <>BDC /P <>BDC ET Neither the 737-800 nor the 737-8)Tj ET EMC /OC /MC2281 BDC fuel burn. /P <>BDC /P <>BDC BT ( )Tj /P <>BDC EMC /P <>BDC BT .498 .4095 .5623 .1043 v (1,392)Tj ( )Tj /GS2 gs /P <>BDC ET /P <>BDC BT 0 Tc BT 7 0 0 7 439.2087 210.9528 Tm ( )Tj /OC /MC2269 BDC /P <>BDC ( )Tj ( )Tj BT ET ET ( )Tj BT 9 0 0 9 36.8504 445.8898 Tm 7 0 0 7 537.7804 67.9528 Tm BT /P <>BDC EMC BT ET ET ET (737-9)Tj EMC ET ( )Tj S 9 0 0 9 367.2442 379.8898 Tm EMC If a fuel gauge is u/s the quantity BT BT There are two AC powered fuel pumps in each tank; there are also EDPs at EMC 9 0 0 9 411.0181 159.8898 Tm ET /P <>BDC ( )Tj /P <>BDC 7 0 0 7 36.8504 11.5129 Tm BT EMC EMC ET ET BT ET 0 Tc 7 0 0 7 474.7064 331.9528 Tm ( )Tj ET ET 1 i EMC ET BT BT ET /P <>BDC BT /P <>BDC ET -.02 Tc BT 0 Tc /P <>BDC 0 Tc ( )Tj 9 0 0 9 53.8578 467.8898 Tm ET ( )Tj /P <>BDC BT ( )Tj 9 0 0 9 534.7515 599.8898 Tm ET BT BT EMC EMC ET ET ( )Tj ET 9 0 0 9 158.963 258.8898 Tm EMC ( )Tj EMC 9 0 0 9 53.8582 181.8898 Tm ET ( )Tj BT EMC Boeing 737 Assembly, the building of this popular City Jet. BT 8 0 0 8 225.1837 633.9528 Tm ( )Tj ET (the flight profile based on the cruise speed)Tj ET ( )Tj EMC ET (0.0122)Tj BT ET ET ( )Tj ET - Non Perele - News Online, Council Post: Aviation Is The Driving Force Of Hydrogen | QNewsHub, When will the Boeing 737 MAX fly again? 1 1 1 rg ET 56 0 obj 7 0 0 7 403.7368 705.7654 Tm 0 Tc 9 0 0 9 36.8504 357.8898 Tm EMC 7 0 0 7 403.478 694.7654 Tm (test programme is well underway for entry)Tj 0 Tc /P <>BDC /P <>BDC ( )Tj ( )Tj EMC BT (39,270)Tj ET EMC -.02 Tc /P <>BDC 0 Tc /P <>BDC ET BT ET /F1 1 Tf BT EMC /P <>BDC /P <>BDC 7 0 0 7 363.2711 221.9528 Tm /P <>BDC 8 0 0 8 365.7704 619.9528 Tm ET BT BT ET 6.5 0 0 6.5 324.4345 689.9529 Tm BT (0.0129)Tj (2,731)Tj 9 0 0 9 411.0181 390.8898 Tm ET EMC 7 0 0 7 534.621 100.7654 Tm 0 Tc ET 7 0 0 7 536.3849 463.7654 Tm EMC BT 0 Tc BT ET (0.0127)Tj ET 161.566 0 l BT ET ( )Tj BT EMC 7 0 0 7 537.7804 441.9528 Tm 6.5 0 0 6.5 477.8064 702.9529 Tm ET /P <>BDC ET ET BT ET EMC EMC EMC ET BT The wheel track, which is the distance between the main wheels is 5.25 metres. /P <>BDC EMC /P <>BDC EMC ( )Tj BT ( )Tj ( )Tj ( )Tj (1465,400)Tj ET BT EMC EMC EMC (10)Tj EMC /P <>BDC 0 Tc ET ET BT ( )Tj /P <>BDC ET /P <>BDC /P <>BDC .151 .147 .15 rg ( )Tj [(AIRL)8.1(INE & AIR)7.1(CRAF)-12.9(T)18.1( OPERA)56.9(T)-8.1(ION)-13.9(S)]TJ ET -.02 Tc EMC 7 0 0 7 99.8582 276.7654 Tm 7 0 0 7 316.0679 364.7654 Tm ET ET /F4 1 Tf ( )Tj BT (between 420nm and 2,429nm )Tj ET A series of ten tests were performed (five flight, EMC BT EMC ET BT BT 0 Tc BT W n [(CFM L)17.1(E)-8.1(AP-)]TJ EMC 0 Tc EMC /P <>BDC EMC BT 7 0 0 7 258.2805 496.7654 Tm 0 Tc /P <>BDC EMC ( )Tj EMC EMC ET ET (27,000lbs, a fan diameter of 69 inches and)Tj (603)Tj EMC 0 Tc BT /P <>BDC BT EMC BT (0.0153)Tj 9 0 0 9 191.0032 225.8898 Tm ( )Tj /P <>BDC -.02 Tc (34,650)Tj ( )Tj [(CFM L)17.1(E)-8.1(AP-1A32)]TJ EMC 7 0 0 7 321.6356 265.9528 Tm 7 0 0 7 444.737 265.7654 Tm 7 0 0 7 54.7071 661.7654 Tm EMC ( )Tj BT (make the range. (A fuel density of 6.55lbs per USG was)Tj /P <>BDC (248,200)Tj BT 7 0 0 7 365.035 639.9528 Tm (208)Tj 0 Tc 7 0 0 7 294.4014 331.7654 Tm 6 0 0 6 308.6461 743.9528 Tm 7 0 0 7 99.8582 122.7654 Tm BT (A321neo)Tj BT [(A3)24.9(21neo v)12.9(ersus 7)-33(3)8.1(7-9 )]TJ EMC /P <>BDC ET /P <>BDC 7 0 0 7 125.6292 430.7654 Tm BT ( )Tj -.01 Tc /P <>BDC BT ( A)Tj (payload reduction. 9 0 0 9 215.4409 269.8898 Tm EMC EMC BT -.02 Tc ( )Tj ( )Tj Since development and production Boeing has built 10,574 737-800s. EMC EMC BT 7 0 0 7 366.0641 727.9528 Tm ET -.02 Tc ( )Tj 9 0 0 9 232.4217 192.8898 Tm /P <>BDC ET EMC 0 Tc ET EMC 7 0 0 7 108.6215 639.9528 Tm ET 9 0 0 9 36.8504 390.8898 Tm ET BT .008 Tc /P <>BDC ( )Tj ET BT ( )Tj EMC (compares to a tracked distance of)Tj In-flight, the GW must be periodically 7 0 0 7 386.3929 683.9528 Tm ET ET Cabin EMC (31,416)Tj /P <>BDC BT ET way. BT ( )Tj BT /P <>BDC 7 0 0 7 70.1644 540.9528 Tm ET BT /P <>BDC ET BT ET BT /P <>BDC They move the 800 along at a max cruise speed of 473 knots. ( )Tj (up to 3,200nm when equipped with)Tj BT 7 0 0 7 187.0858 694.9528 Tm ( )Tj /P <>BDC ET )21(The )]TJ 7 0 0 7 457.0984 276.7654 Tm ET /P <>BDC -.02 Tc [(Aircr)10(aft types )]TJ BT /P <>BDC 6 0 0 6 214.8509 687.9528 Tm BT EMC BT /P <>BDC 0 Tc BT 0 Tc ET /P <>BDC endobj ET /P <>BDC ET 9 0 0 9 408.2047 566.8898 Tm /P <>BDC which in hot conditions will evaporate and create an explosive mixture with the BT BT 7 0 0 7 37.5838 551.9528 Tm capacitors in the tanks with fuel acting as the dielectric. 0 Tc ( )Tj ET EMC 0 Tw BT 7 0 0 7 247.7395 386.7654 Tm EMC (\(see table, page 21\))Tj (2,601)Tj BT (4.8:1. ( )Tj 7 0 0 7 297.632 738.9528 Tm BT 7 0 0 7 535.5029 89.7654 Tm EMC (The A320neo family and 737 MAX)Tj BT 9 0 0 9 194.7718 456.8898 Tm [(A3)24.9(20ceo v)12.9(ersus A3)24.9(20neo )]TJ 7 0 0 7 338.3085 188.9528 Tm EMC /P <>BDC /P <>BDC EMC ET /P <>BDC /P <>BDC EMC EMC ET /P <>BDC BT (136)Tj to standardise the total tank capacitance and allows for the replacement [(BOS-DF)-13.9(W)]TJ BT 5.25 0 0 5.25 64.5461 11.5129 Tm EMC EMC ( )Tj ET EMC /P <>BDC BT 7 0 0 7 230.7317 342.9528 Tm ( )Tj ( )Tj EMC BT 9 0 0 9 411.0234 731.8898 Tm EMC ( )Tj ( )Tj ( )Tj EMC ET (ONT/73)Tj /GS2 gs ( )Tj ET (generation aircraft continues to grow at a)Tj EMC EMC (737-800W)Tj BT /P <>BDC /P <>BDC -.01 Tc -.02 Tc automatically shut off when they detect a low output pressure and there have ET ( )Tj 9 0 0 9 394.0157 104.8898 Tm ET BT EMC ET EMC 7 0 0 7 554.7883 287.7654 Tm EMC /P <>BDC BT /P <>BDC BT BT ET 0 Tc BT /P <>BDC EMC Non-environmental Icing" or "Cold Soaked Fuel Frost" CSFF. /P <>BDC 0 Tc 0 Tc ( )Tj 7 0 0 7 535.5029 199.7654 Tm /P <>BDC 7 0 0 7 518.4953 210.9528 Tm EMC EMC Therefore,)Tj 9 0 0 9 565.9277 60.8898 Tm ET /P <>BDC 0 Tc [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ 9 0 0 9 408.2047 93.8898 Tm 9 0 0 9 53.8582 632.8898 Tm ET EMC BT 9 0 0 9 51.0236 401.8898 Tm /P <>BDC ET ( )Tj ( )Tj )Tj /F4 1 Tf ET EMC Although successful the A320 could not take on the Boeing 737s success. BT 9 0 0 9 68.3339 478.8898 Tm 7 0 0 7 125.6292 188.7654 Tm BT (also impact the actual flight time. /P <>BDC /F1 1 Tf ( )Tj /P <>BDC 7 0 0 7 446.5009 661.7654 Tm BT 7 0 0 7 116.3631 11.5132 Tm EMC 8 0 0 8 314.3535 675.9528 Tm -.01 Tc ( )Tj BT ( )Tj -.02 Tc ( )Tj (capacity with slimmer seats, and cabin)Tj EMC BT BT (westerly direction so that all operate)Tj 7 0 0 7 387.619 430.9528 Tm EMC 0 Tc q 1 0 0 1 36.85 797.54 cm 0 0 m (a 3.3% advantage for the A321neo on the)Tj This fuel would give a 7 0 0 7 535.5029 518.7654 Tm ET ( )Tj 9 0 0 9 196.725 654.8898 Tm /P <>BDC ( )Tj /P <>BDC The service ceiling is 41,000 feet. The charges are split by weight)Tj EMC 7 0 0 7 187.0858 705.9528 Tm ( )Tj BT /F1 1 Tf EMC ET ET /P <>BDC (420)Tj /P <>BDC All the aircraft would therefore)Tj ET BT 10 0 0 10 417.91 814.1973 Tm BT EMC /P <>BDC BT ET BT EMC EMC 8 0 0 8 182.2355 760.7654 Tm Over the nine)Tj 9 0 0 9 361.1316 214.8898 Tm ET ET /P <>BDC 7 0 0 7 430.039 705.9528 Tm EMC /P <>BDC EMC EMC 7 0 0 7 321.6356 276.9528 Tm -.02 Tc BT Hi All, ET EMC EMC /P <>BDC BT ET EMC BT BT /P <>BDC 7 0 0 7 294.4014 507.7654 Tm (A321ceo)Tj ET /P <>BDC ET ( The assumptions on flight track and)Tj -.02 Tc f /P <>BDC (A320ceo)Tj -4.2575 -4.8278 -4.5158 -4.0295 -4.515 -3.0604 c ET (105)Tj EMC /P <>BDC /P <>BDC (5.1% benefit in fuel burn with the heavier)Tj Everything you need to know about the Boeing 737 600/700/800/900 - NGs History & Development of . /P <>BDC EMC BT ET 9 0 0 9 229.6141 49.8898 Tm /P <>BDC /P <>BDC ( )Tj ( )Tj S ( )Tj /F1 1 Tf BT -.01 Tc BT BT BT ET BT 7 0 0 7 473.8245 221.9528 Tm EMC 7 0 0 7 204.0935 111.7654 Tm BT 9 0 0 9 188.0937 115.8898 Tm ( )Tj ET 340.964 0 0 625.44 232.441 31.168 cm ET 6.5 0 0 6.5 64.6596 545.9529 Tm BT 6 0 0 6 554.6981 760.7654 Tm BT /P <>BDC ET 9 0 0 9 379.3098 269.8898 Tm 9 0 0 9 211.8361 577.8898 Tm 0 Tc ( )Tj BT BT /P <>BDC 8 0 0 8 394.0237 49.8898 Tm ET -.02 Tc Note: Specifications are listed as standard and may vary slightly. ET /Artifact <>BDC (37,653)Tj -.02 Tc EMC ( )Tj BT EMC ET EMC 0 Tc ET 6.5 0 0 6.5 296.4841 689.9529 Tm EMC EMC EMC ( )Tj ET ( )Tj -.02 Tc EMC /P <>BDC ET (0.0119)Tj 0 Tc (310,080)Tj BT -.01 Tc ( )Tj /P <>BDC (109)Tj 9 0 0 9 364.8592 148.8898 Tm EMC BT 7 0 0 7 141.7322 705.9528 Tm EMC BT 7 0 0 7 82.8504 309.9528 Tm (industry is 210 US cents per USG for Jet A-)Tj (1,272)Tj 0 Tc 7 0 0 7 444.737 320.7654 Tm 0 Tc EMC ( )Tj (36,960)Tj (CFM LEAP-1B28B1 rated at 28,000lbs)Tj (impacted by external factors such as)Tj ( )Tj EMC 9 0 0 9 392.5848 346.8898 Tm /OC /MC2279 BDC (170)Tj BT EMC BT (payload in scenario 1. /P <>BDC EMC /P <>BDC /P <>BDC EMC ET ET 7 0 0 7 404.101 188.7654 Tm ET /P <>BDC ET /P <>BDC BT ET EMC 7 0 0 7 427.7291 331.9528 Tm ET 7 0 0 7 337.6855 595.9528 Tm (A320ceo)Tj (737-9)Tj (between the aircraft types even greater. /P <>BDC (4,329)Tj /P <>BDC ET /P <>BDC 0 Tc BT EMC EMC 7 0 0 7 131.6494 375.7654 Tm on 5 Nov 1990 have been destroyed on the ground due to explosions in the empty ET BT BT 9 0 0 9 535.2501 522.8898 Tm ET ET (2,732)Tj BT EMC 0 Tc /P <>BDC EMC 7 0 0 7 314.6398 518.7654 Tm /P <>BDC ( )Tj (capacity would further increase the)Tj EMC ET BT ( )Tj 0 Tc EMC ( )Tj /P <>BDC EMC ET ( )Tj BT ( )Tj ( )Tj 9 0 0 9 363.3015 775.8898 Tm EMC 7 0 0 7 554.7883 705.7654 Tm ET ET /P <>BDC ET BT BT [(CFM L)17.1(E)-8.1(AP-1B27)]TJ BT safer place! /P <>BDC BT 0 Tc 9 0 0 9 370.9169 379.8898 Tm (uses one of the 11 certified weight variants. ( )Tj ( )Tj EMC BT (1,824)Tj -.02 Tc EMC BT (356-369)Tj BT BT 7 0 0 7 445.619 518.7654 Tm EMC -.02 Tc ET BT EMC ET 0 Tc BT (20)Tj /P <>BDC ET ET ET ( )Tj -.01 Tc BT /P <>BDC EMC /P <>BDC /P <>BDC /P <>BDC BT EMC ( )Tj BT ( )Tj ET ET The 14 routes are listed)Tj 7 0 0 7 297.632 661.9528 Tm EMC 0 Tc EMC ET BT BT (376)Tj /P <>BDC 1.0437 2.7347 l EMC These incidents, and 15 more on other types since 1959, 9 0 0 9 522.5613 38.8898 Tm EMC ET /P <>BDC ( )Tj /P <>BDC 7 0 0 7 427.7291 166.9528 Tm /P <>BDC /P <>BDC 9 0 0 9 361.016 49.8898 Tm BT ET -.02 Tc (326-339)Tj 7 0 0 7 158.74 595.7654 Tm ( )Tj BT EMC BT /GS1 gs /P <>BDC EMC ( )Tj 9 0 0 9 197.3398 214.8898 Tm /P <>BDC 7 0 0 7 241.5317 540.9528 Tm 9 0 0 9 394.0237 302.8898 Tm 0 Tc (11.0:1)Tj 6.5 0 0 6.5 191.8316 585.9529 Tm EMC ( )Tj 7 0 0 7 404.101 331.7654 Tm BT ET EMC 0 Tc EMC 7 0 0 7 491.4046 111.9528 Tm ( )Tj 7 0 0 7 298.514 617.9528 Tm EMC ET 0 Tc ET ET -.02 Tc -.02 Tc (132,872)Tj BT ET BT EMC (City-pair)Tj BT /P <>BDC 7 0 0 7 326.2278 738.9528 Tm 6.5 0 0 6.5 397.1664 735.9529 Tm 8 0 0 8 153.6923 577.9528 Tm EMC 8 0 0 8 549.2646 49.8898 Tm /P <>BDC /P <>BDC BT 304.725 420.96 m EMC BT ET BT 9 0 0 9 195.3055 324.8898 Tm ( )Tj ET ET /P <>BDC 7 0 0 7 354.7351 683.7654 Tm BT /P <>BDC 7 0 0 7 326.2278 606.9528 Tm 0 Tc 9 0 0 9 68.0314 38.8898 Tm ( )Tj (34,650)Tj /P <>BDC EMC ( )Tj 7 0 0 7 204.0935 177.7654 Tm 7 0 0 7 141.7322 67.9528 Tm fuel and de-ice the fuel filter. BT ( )Tj ( )Tj ( )Tj BT -.02 Tc (LRC speed. 0 Tc EMC /P <>BDC ET BT 7 0 0 7 518.4953 309.9528 Tm ( )Tj -.01 Tc BT EMC 7 0 0 7 445.619 694.7654 Tm /P <>BDC /P <>BDC EMC 9 0 0 9 540.8301 489.8898 Tm (1,913)Tj Since no two)Tj ET ( )Tj ET ET ET -.02 Tc EMC ET 0 J 0 j 5 w 10 M [] 0 d 0 Tc ET 9 0 0 9 68.9175 247.8898 Tm EMC EMC -.02 Tc BT EMC ET (37,653lbs )Tj 9 0 0 9 36.8504 203.8898 Tm ( )Tj 9 0 0 9 375.3516 335.8898 Tm EMC 0 Tc ET /P <>BDC .559 .331 .619 rg 7 0 0 7 456.2165 111.7654 Tm /OC /MC835 BDC ( )Tj /P <>BDC ( )Tj /P <>BDC 9 0 0 9 36.8504 291.8898 Tm q 8 0 0 8 222.3212 771.9528 Tm -.02 Tc EMC ( )Tj /P <>BDC /P <>BDC ( )Tj BT BT 9 0 0 9 536.4734 313.8898 Tm 9 0 0 9 232.4217 511.8898 Tm EMC ET 9 0 0 9 213.8067 159.8898 Tm 7 0 0 7 158.74 177.7654 Tm [(D)12.9(A)-8.1(L/36)]TJ .023 .567 .626 RG higher. /P <>BDC /P <>BDC 17 0 0 17 550.9253 758.6944 Tm BT 9 0 0 9 53.8582 511.8898 Tm 7 0 0 7 230.7317 507.9528 Tm /P <>BDC /P <>BDC ( )Tj ET /P <>BDC ET EMC 9 0 0 9 552.5312 687.8898 Tm ET /P <>BDC /P <>BDC -.01 Tc ( )Tj ( )Tj 9 0 0 9 537.9817 445.8898 Tm ET ( )Tj /P <>BDC ET EMC <>stream (A321neo)Tj EMC BT BT EMC ET /P <>BDC 0 841.89 609.449 -841.89 re (830)Tj ( )Tj ( )Tj ET BT BT BT 9 0 0 9 232.4408 698.8898 Tm 0 Tc (The fuel burn improvement on the)Tj 9 0 0 9 192.5225 489.8898 Tm EMC BT /P <>BDC /P <>BDC )Tj EMC 9 0 0 9 190.1186 247.8898 Tm ( )Tj 5.25 0 0 5.25 73.853 11.5132 Tm 9 0 0 9 215.4409 225.8898 Tm 9 0 0 9 538.7331 225.8898 Tm ( )Tj BT 7 0 0 7 82.2047 716.9528 Tm /P <>BDC EMC ET 9 0 0 9 232.4217 500.8898 Tm EMC /P <>BDC /P <>BDC 0 Tc BT Hi Peter, BT BT ( )Tj ( )Tj -.02 Tc ET ET ET /P <>BDC /P <>BDC BT -.02 Tc /P <>BDC ET EMC ET /P <>BDC 7 0 0 7 299.0601 276.9528 Tm BT EMC 0 Tc 7 0 0 7 404.101 111.7654 Tm (150)Tj 6 0 0 6 54.1367 771.9528 Tm EMC /P <>BDC ( )Tj 9 0 0 9 564.8379 269.8898 Tm -.02 Tc EMC ET BT ET (157,300)Tj 9 0 0 9 544.8128 412.8898 Tm BT BT )Tj 0 Tc 9 0 0 9 351.8271 203.8898 Tm EMC ET ( )Tj EMC -.02 Tc EMC BT EMC EMC 9 0 0 9 36.8504 368.8898 Tm /P <>BDC 7 0 0 7 403.478 573.7654 Tm -.02 Tc ET ET ( )Tj ( )Tj BT EMC /P <>BDC BT 6 0 0 6 425.0715 687.9528 Tm /P <>BDC /P <>BDC /P <>BDC 9 0 0 9 534.3536 577.8898 Tm ET EMC BT ET EMC ET (179)Tj endstream (2,515)Tj /P <>BDC /P <>BDC /P <>BDC ET 7 0 0 7 54.5916 738.7654 Tm 0 Tc (1,800 - )Tj /P <>BDC BT ET ET BT /P <>BDC EMC ( )Tj /P <>BDC 7 0 0 7 82.8504 210.9528 Tm BT ET /P <>BDC ET ET EMC ET (than 3% on the shorter sectors, but as the)Tj ET ( )Tj ET BT 0 Tc (fuel consumption and cost per seat or per)Tj 9 0 0 9 215.4409 104.8898 Tm The classics have 5 dripsticks in each wing tank and none in the centre ET 9 0 0 9 543.767 93.8898 Tm /P <>BDC /Im1 Do EMC ( )Tj /P <>BDC ET 7 0 0 7 379.3969 210.7654 Tm (CFM56-7B27B3 installed on the 737-)Tj 9 0 0 9 385.653 71.8898 Tm 7 0 0 7 99.8582 320.7654 Tm EMC ( )Tj 0 Tc ET ( )Tj 0 Tc /P <>BDC 7 0 0 7 387.0159 507.9528 Tm BT EMC EMC q [(E)-7.8(P)16.1(T)9(E)-13.9(MBE)-16.9(R)]TJ )Tj EMC ( )Tj 9 0 0 9 545.537 390.8898 Tm ET EMC BT 7 0 0 7 54.5916 441.7654 Tm EMC EMC ET EMC 0 Tc -.02 Tc 9 0 0 9 394.0315 269.8898 Tm -.02 Tc ET EMC BT ( )Tj ET 0 Tc (CFM56-5B4/P)Tj ET 7 0 0 7 404.101 166.7654 Tm EMC 9 0 0 9 215.4313 49.8898 Tm /P <>BDC /P <>BDC /P <>BDC ET ( )Tj /P <>BDC /P <>BDC ET BT 0 Tc 6.5 0 0 6.5 244.3754 565.9529 Tm ET ET BT The CFM56-7B26 engine on the heavier weight (evaluate the physical configuration of the)Tj ET ( )Tj 7 0 0 7 439.2087 243.9528 Tm ET Airbus A320 History a new player in the short-haul market. BT /P <>BDC ET ET -.005 Tc BT 0 Tc BT (I)Tj EMC BT BT ET -.02 Tc /GS2 gs ET /P <>BDC EMC 9 0 0 9 215.4409 258.8898 Tm ET (44,121)Tj ET EMC ET /P <>BDC 9 0 0 9 525.6696 192.8898 Tm BT BT 0 Tc 7 0 0 7 82.8504 430.9528 Tm /P <>BDC ( )Tj ( )Tj /P <>BDC ET /P <>BDC ET 0 Tc EMC 7 0 0 7 362.3891 199.9528 Tm 9 0 0 9 275.0764 401.8898 Tm BT /P <>BDC ET ET ( )Tj 9 0 0 9 229.6045 390.8898 Tm 0 Tc -.02 Tc EMC 7 0 0 7 158.74 463.7654 Tm BT 8 0 0 8 136.4919 661.9528 Tm /P <>BDC /P <>BDC ( )Tj BT BT EMC /P <>BDC 7 0 0 7 125.6292 243.7654 Tm -.02 Tc BT 9 0 0 9 527.5473 390.8898 Tm BT -.02 Tc 7 0 0 7 101.0963 210.9528 Tm ET EMC 7 0 0 7 210.1137 166.7654 Tm -.02 Tc 0 Tc EMC to illuminate the master caution to avoid spurious warnings at high AoAs or 6.5 0 0 6.5 426.4819 702.9529 Tm 9 0 0 9 194.9803 478.8898 Tm BT BT ( )Tj ( )Tj (150)Tj (5.7:1)Tj -.02 Tc 7 0 0 7 536.3849 265.7654 Tm BT ET 7 0 0 7 187.0858 496.9528 Tm -.02 Tc BT ET EMC -.02 Tc BT EMC ET /P <>BDC 9 0 0 9 191.7774 423.8898 Tm /P <>BDC W n [(CFM L)17.1(E)-8.1(AP-1A32)]TJ ET BT /P <>BDC ET EMC ET It sports its powerful crew and passenger carrying abilities elegantly as it takes flight. EMC hello, i would like to know about the technology which applied on B737 NG flight cockpit lay out include its characteristics (advantages and disadvantages), especially on PFD and MFD, can you tell me or send me a link which discuss about that? BT 7 0 0 7 518.4953 287.9528 Tm EMC 9 0 0 9 539.8684 280.8898 Tm BT BT 0 Tc (150)Tj 6.5 0 0 6.5 397.1339 676.9529 Tm /P <>BDC 7 0 0 7 241.5317 441.9528 Tm /P <>BDC /P <>BDC 0 Tc ET 0 Tc /P <>BDC 7 0 0 7 141.7322 78.9528 Tm ET -2.4549 -3.9026 l ET 7 0 0 7 473.8245 199.9528 Tm ET BT ( )Tj /P <>BDC /P <>BDC 7 0 0 7 315.1859 100.7654 Tm EMC ( )Tj ET /P <>BDC BT EMC 9 0 0 9 543.3065 555.8898 Tm BT ( )Tj (The A321neo has a lower fuel burn)Tj [(P)11(ayload)]TJ /P <>BDC 9 0 0 9 211.3321 698.8898 Tm /P <>BDC /F4 1 Tf EMC EMC ET BT EMC -.01 Tc ET ET ET EMC 7 0 0 7 444.737 309.7654 Tm <> BT BT ET BT /P <>BDC BT ET BT ET /P <>BDC ( )Tj BT ET 9 0 0 9 36.8504 225.8898 Tm 7 0 0 7 337.6855 540.9528 Tm EMC ( )Tj BT BT ET BT BT 0 Tc S 9 0 0 9 557.1673 794.1039 Tm ET 6 0 0 6 255.8802 771.9528 Tm 6.5 0 0 6.5 448.3675 532.9529 Tm BT EMC 0 Tc EMC BT (34,650)Tj ET -.02 Tc 7 0 0 7 242.1547 672.9528 Tm ET BT probably take you over MTOW if any payload was carried. 9 0 0 9 505.9675 632.8898 Tm ET ET ( )Tj /P <>BDC BT /P <>BDC /P <>BDC ET 0 Tc BT ET 0 Tc BT /F1 1 Tf ( )Tj ET 0 841.89 609.449 -841.89 re ( )Tj EMC (3,691)Tj (The wind speed was based on an 85%)Tj /P <>BDC EMC /P <>BDC BT /P <>BDC 7 0 0 7 473.8245 78.9528 Tm EMC ET /P <>BDC 7 0 0 7 54.7071 716.7654 Tm /P <>BDC BT BT EMC EMC EMC -.02 Tc ET 6 0 0 6 357.8844 701.9528 Tm These improvements include the redesign of fuel pumps, FQIS, any /P <>BDC EMC BT /P <>BDC EMC 7 0 0 7 554.7883 111.7654 Tm (The performance improvement in the)Tj 0 Tc EMC /P <>BDC 183,380 Litres: 47,210 US Gal. BT [(B)-13.9(L)74(V/53)]TJ BT BT EMC (major airports, which could lead to the)Tj (193,344)Tj 9 0 0 9 207.5518 588.8898 Tm /P <>BDC /P <>BDC BT BT 9 0 0 9 229.6064 390.8898 Tm ET /P <>BDC /P <>BDC ( )Tj 7 0 0 7 491.4046 397.9528 Tm ( )Tj (373-388)Tj ( )Tj EMC /P <>BDC /GS1 gs -.02 Tc /P <>BDC /GS2 gs (O)Tj EMC ( )Tj /P <>BDC EMC ( )Tj /P <>BDC EMC BT BT BT BT BT EMC 7 0 0 7 37.5838 254.9528 Tm -.02 Tc )Tj EMC /P <>BDC Their version of the Boeing 737-800 is the Airbus A220. ( )Tj (166,090)Tj BT BT automatically moved back to OFF after one minute. (1,272)Tj BT ET 7 0 0 7 337.6855 573.9528 Tm /P <>BDC ET 0 Tc ET The 800 was developed to replace the 727 on short routes. /P <>BDC 518.697 0 l -.02 Tc /P <>BDC 6.5 0 0 6.5 549.8557 676.9529 Tm '''''''''' z" ET BT 9 0 0 9 394.0123 335.8898 Tm EMC -.02 Tc EMC ( )Tj 2001 - 2019, Karsten Palt, Leipzig / Germany - All rights reserved, Brussel/Bruxelles - Brussels Airport (EBBR / BRU). 7 0 0 7 230.7317 188.9528 Tm BT 6 0 0 6 184.072 659.9528 Tm ET ET ET ( )Tj 7 0 0 7 427.7291 221.9528 Tm (calculate the fuel burns and times. EMC .534 .14 .504 RG BT ET endobj EMC BT EMC ET /P <>BDC EMC ET been many other improvements to wiring and FQIS. -.02 Tc /P <>BDC 7 0 0 7 37.6993 177.9528 Tm ET ( )Tj EMC /P <>BDC .0081 Tc q 1 0 0 1 53.858 797.352 cm 0 0 m ET /P <>BDC BT ET During cruise, the tolerance is less than 0.5%. 7 0 0 7 363.2711 386.9528 Tm BT BT /P <>BDC ET (216,240)Tj BT /P <>BDC 7 0 0 7 37.6993 309.9528 Tm BT ET /P <>BDC 0 Tc EMC -.02 Tc 7 0 0 7 490.5226 78.9528 Tm -.02 Tc ET 7 0 0 7 250.5326 100.7654 Tm /P <>BDC These sectors)Tj EMC ( )Tj -.02 Tc BT /P <>BDC ( )Tj ( )Tj ET -.01 Tc BT (157)Tj Q EMC BT EMC ET BT /P <>BDC 7 0 0 7 474.3564 705.9528 Tm ET ( )Tj ( )Tj EMC BT ET 9 0 0 9 186.8966 357.8898 Tm ( )Tj EMC 9 0 0 9 206.7178 181.8898 Tm BT 7 0 0 7 380.2788 199.7654 Tm ET EMC endobj ET EMC BT /P <>BDC EMC ( )Tj ET /P <>BDC 9 0 0 9 394.0123 379.8898 Tm /GS1 gs 0 Tc ET )Tj ( )Tj BT ET BT -.02 Tc ET /P <>BDC 7 0 0 7 82.2047 617.9528 Tm BT (152)Tj (170)Tj 9 0 0 9 356.7322 159.8898 Tm EMC 7 0 0 7 118.104 661.7654 Tm EMC ET EMC 9 0 0 9 332.7796 225.8898 Tm EMC BT ET 7 0 0 7 429.157 507.9528 Tm EMC Thanks, Hi Henna, -.02 Tc [(UG)-17.1(U)-8(S)8.1(T)]TJ ET /P <>BDC ( )Tj ET ET ET BT BT /P <>BDC 0 Tc 7 0 0 7 383.0719 716.7654 Tm ( )Tj ET 0 Tc EMC EMC EMC BT BT (than the A321ceo. ET ( )Tj following conditions: Takeoff with CSFF on the upper wing surfaces is ( )Tj (900ER and 737-9, A320ceo and A320neo,)Tj ( )Tj (The flight tracks and cruise altitudes)Tj 7 0 0 7 387.0932 320.9528 Tm [(BOS-SF)8(O)]TJ EMC 7 0 0 7 241.5317 617.9528 Tm ET /P <>BDC /P <>BDC (170)Tj ET ET BT decrease the oxygen content to a level where the air volume (ullage) will not BT BT /P <>BDC EMC EMC 9 0 0 9 53.8338 181.8898 Tm BT 9 0 0 9 411.0097 511.8898 Tm 7 0 0 7 321.6356 221.9528 Tm (A)Tj ( )Tj 9 0 0 9 53.8582 720.8898 Tm /P <>BDC ET 9 0 0 9 553.8705 93.8898 Tm BT BT BT EMC EMC 300.229 562.194 m 7 0 0 7 439.2087 111.9528 Tm (airlines across the world. .151 .147 .15 rg 6 0 0 6 153.0397 715.9528 Tm BT BT BT EMC 8 0 0 8 394.0237 38.8898 Tm /P <>BDC .151 .147 .15 rg /P <>BDC /P <>BDC 8 0 0 8 365.7704 745.9528 Tm ( )Tj ET EMC /P <>BDC EMC ( )Tj 7 0 0 7 199.5784 738.7654 Tm EMC (388)Tj EMC /P <>BDC ET ET EMC /P <>BDC /P <>BDC ET /F1 1 Tf /P <>BDC EMC ET /P <>BDC 9 0 0 9 495.0108 170.8898 Tm ET BT /P <>BDC ET ET EMC ( )Tj (O)Tj -.02 Tc BT /P <>BDC 13 0 0 13 177.4468 500.8898 Tm 0 Tc ET EMC /P <>BDC EMC ( )Tj Any help would be greatly appreciated and thank you for all your work its extremely helpful! BT ( )Tj 7 0 0 7 492.5963 738.7654 Tm 7 0 0 7 457.0984 210.7654 Tm ET BT /P <>BDC EMC EMC [(A3)24.9(21ceo v)12.9(ersus 7)-33(3)8.1(7-900ER\(W)-19(\) )]TJ BT 0 Tc ( )Tj ET ET 9 0 0 9 394.0123 368.8898 Tm ( )Tj BT Can we suggest copying and pasteing Aluminium alloy 7055 basis value into your search engine of choice? 848 0 obj ( )Tj EMC /P <>BDC 7 0 0 7 338.6433 67.7654 Tm 9 0 0 9 185.6303 225.8898 Tm 9 0 0 9 53.8338 49.8898 Tm ( )Tj 9 0 0 9 197.9514 148.8898 Tm BT next aircraft ET (. /P <>BDC /GS1 gs ET The website is currently in the process of optimizing and will have further functions added in order to improve the usability. 9 0 0 9 232.438 489.8898 Tm BT ET /P <>BDC (These results will allow a better)Tj ET 0 Tc EMC BT /P <>BDC /P <>BDC (shorter routes. /P <>BDC ET EMC 6.5 0 0 6.5 324.4345 702.9529 Tm 8 0 0 8 243.3422 771.9529 Tm /P <>BDC /P <>BDC [(CFM L)17.1(E)-8.1(AP-1B27)]TJ /P <>BDC (273,917)Tj ET BT 9 0 0 9 36.8504 115.8898 Tm BT EMC .151 .147 .15 rg 9 0 0 9 350.8533 104.8898 Tm ET 13 0 0 13 118.3688 390.8898 Tm /P <>BDC BT /GS2 gs ET BT 7 0 0 7 380.2788 441.7654 Tm -.02 Tc ET (rules relating to the cruise altitudes and)Tj 7 0 0 7 439.2087 419.9528 Tm (0.0135)Tj EMC (of the Boeing aircraft, with the A321ceo)Tj ( )Tj /P <>BDC EMC 6.5 0 0 6.5 448.7448 742.9529 Tm ( )Tj /F6 1 Tf ET 9 0 0 9 179.7604 159.8898 Tm /P <>BDC ET EMC ET ET ET ( )Tj EMC ET ( )Tj /P <>BDC ET 7 0 0 7 507.7893 210.7654 Tm 0 Tc /P <>BDC /P <>BDC 0 Tc /P <>BDC /P <>BDC 6.5 0 0 6.5 64.6596 650.9529 Tm /P <>BDC Specification Table Boeing 737 Original and Boeing 737 Classic (Top). 7 0 0 7 535.5029 78.7654 Tm EMC 7 0 0 7 82.2047 639.9528 Tm EMC BT ET BT illuminated is not only an explosion risk (see Thai and Philippine write offs) /P <>BDC ( )Tj 8 0 0 8 365.7704 717.9528 Tm /P <>BDC BT /P <>BDC 6 0 0 6 371.479 757.9528 Tm BT BT BT BT ( )Tj ( )Tj ET /F6 1 Tf BT /P <>BDC BT BT (between: the Pratt & Whitney PW1127G,)Tj 9 0 0 9 394.0157 126.8898 Tm 9 0 0 9 408.1889 533.8898 Tm ( )Tj 6.5 0 0 6.5 279.814 624.9529 Tm 7 0 0 7 101.0963 89.9528 Tm EMC /F7 1 Tf -.01 Tc ( )Tj ( )Tj BT 9 0 0 9 394.0157 291.8898 Tm 9 0 0 9 546.3754 159.8898 Tm BT (largest operating costs for any aircraft)Tj -.02 Tc (A US domestic reserve policy was)Tj ( )Tj /P <>BDC 7 0 0 7 54.5916 243.7654 Tm 7 0 0 7 536.3849 166.7654 Tm EMC 9 0 0 9 270.2513 93.8898 Tm (covers a 3,300-3,400nm range with a full)Tj /P <>BDC ( )Tj ( )Tj W n EMC 7 0 0 7 82.2047 584.9528 Tm ( )Tj 7 0 0 7 316.0679 375.7654 Tm BT 7 0 0 7 535.5029 672.7654 Tm EMC ET ET /P <>BDC 6.5 0 0 6.5 54.877 637.9529 Tm /P <>BDC ET ET ( )Tj BT 7 0 0 7 469.2222 11.5129 Tm /P <>BDC EMC /P <>BDC BT 9 0 0 9 215.433 324.8898 Tm (9.0:1)Tj EMC ET BT ET ET -.02 Tc /P <>BDC EMC ( )Tj (39,270)Tj BT 9 0 0 9 36.8504 456.8898 Tm BT (the IAE V2533-A5 engine, rated at)Tj ET EMC (and 4.3% better performance on the 737-)Tj ET Alaska Airlines launched the 737-900 in 1997, the 737-900 made its first . 7 0 0 7 247.7395 463.7654 Tm BT ET EMC ET ET 9 0 0 9 386.3946 137.8898 Tm EMC ( )Tj (82,110)Tj 6.5 0 0 6.5 90.4525 663.9529 Tm ( )Tj 0 Tc /P <>BDC -.02 Tc -.02 Tc 7 0 0 7 494.3672 661.7654 Tm ET (2,900)Tj q 1 0 0 1 36.85 84.878 cm 0 0 m /P <>BDC BT (2,731)Tj 7 0 0 7 554.7883 309.7654 Tm (5,025)Tj BT ( )Tj EMC BT BT 9 0 0 9 276.2863 115.8898 Tm /P <>BDC /P <>BDC ( )Tj ( )Tj (aircraft types, however, it was decided to)Tj BT EMC BT 8 0 0 8 76.6837 661.9528 Tm 9 0 0 9 53.8338 302.8898 Tm 7 0 0 7 241.5317 309.9528 Tm 7 0 0 7 82.8504 320.9528 Tm /P <>BDC EMC BT BT /P <>BDC BT ET ( )Tj ( )Tj 9 0 0 9 536.5664 269.8898 Tm 9 0 0 9 389.1758 522.8898 Tm 8 0 0 8 258.7094 760.9528 Tm EMC (0.0113)Tj -.02 Tc ET ET ET EMC /P <>BDC /P <>BDC ET EMC /P <>BDC

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