endobj BT 9 0 0 9 215.433 214.8898 Tm 0 Tc [(CFM L)17.1(E)-8.1(AP-1A26)]TJ BT (. ET (4,000nm with maximum passenger)Tj ET /P <>BDC (5,394)Tj ET BT Over the nine)Tj ( )Tj ( )Tj BT ET ET ( )Tj /P <>BDC EMC /P <>BDC /P <>BDC BT /GS2 gs -.02 Tc (1,060)Tj BT EMC (The lowest fuel cost per ASM in the)Tj 9 0 0 9 394.0237 401.8898 Tm ( )Tj -.02 Tc /OC /MC828 BDC BT BT /P <>BDC 7 0 0 7 439.2087 111.9528 Tm (737-900ER\(W\) has an MTOW of)Tj 7 0 0 7 537.7804 210.9528 Tm ET ET 9 0 0 9 530.5634 280.8898 Tm EMC 6.5 0 0 6.5 173.5238 637.9529 Tm ET -.02 Tc /P <>BDC ET .023 .567 .626 rg BT The service ceiling is 41,000 feet. 6.5 0 0 6.5 332.6961 735.9529 Tm 9 0 0 9 232.438 170.8898 Tm BT /P <>BDC ET ( )Tj 7 0 0 7 444.737 232.7654 Tm ET ( )Tj Other)Tj -.02 Tc EMC 7 0 0 7 314.6398 507.7654 Tm BT 7 0 0 7 539.9176 11.5129 Tm (31,416)Tj (MTOW and OEW. /P <>BDC ( )Tj 6 0 0 6 195.6824 659.9528 Tm EMC ET /P <>BDC ET EMC /P <>BDC BT /P <>BDC /P <>BDC (is 2.54 cents per ASM for the same)Tj -.02 Tc W n 0 Tc ET ET )21(The r)10(elativ)12.9(e)]TJ ET -.02 Tc ET ( )Tj 7 0 0 7 473.8245 287.9528 Tm .014984 841.89 609.45 -841.89 re ET EMC EMC ( )Tj /P <>BDC /P <>BDC ( )Tj ET ET /P <>BDC ( )Tj /P <>BDC /P <>BDC ET (105,800lbs )Tj /P <>BDC 0 Tc Q ET ET (the 14 sectors with the 85% passenger)Tj 9 0 0 9 552.9554 357.8898 Tm -.02 Tc (in a more efficient engine. BT 6.5 0 0 6.5 54.877 722.9529 Tm EMC 7 0 0 7 337.6855 177.9528 Tm (737-9)Tj ( )Tj BT /Artifact <>BDC /P <>BDC ET BT (4,200)Tj ( )Tj ET BT 19.851 0 l ET ( )Tj BT ( )Tj BT ET EMC 6 0 0 6 277.7064 715.9528 Tm 9 0 0 9 408.1854 291.8898 Tm EMC /P <>BDC ET -.02 Tc /P <>BDC -.02 Tc BT (scenario, the difference in fuel burn)Tj EMC /P <>BDC BT EMC ET -.02 Tc 9 0 0 9 528.0825 368.8898 Tm BT /F4 1 Tf 6 0 0 6 277.7064 757.9528 Tm /P <>BDC 6 0 0 6 184.9362 743.9528 Tm ET 7 0 0 7 491.7142 331.7654 Tm 7 0 0 7 36.8504 155.9528 Tm EMC 7 0 0 7 387.0932 144.9528 Tm ET ET ET (0.0140)Tj .559 .331 .619 rg 8 0 0 8 43.6039 717.9528 Tm BT EMC /F2 1 Tf EMC BT ET ET (0.0137)Tj /P <>BDC EMC ( )Tj -.005 Tc EMC EMC ET EMC BT EMC /P <>BDC EMC ET ET 7 0 0 7 404.101 265.7654 Tm EMC 9 0 0 9 53.8338 49.8898 Tm BT ET 7 0 0 7 230.7317 111.9528 Tm The seat configuration)Tj BT /P <>BDC BT EMC 7 0 0 7 279.1575 606.9528 Tm BT (variant offers 26,000lbs of thrust, with a)Tj ET ET (150)Tj BT endstream ET 9 0 0 9 394.0157 588.8898 Tm EMC (0.0177)Tj /P <>BDC )Tj EMC ET ET 7 0 0 7 108.6215 727.9528 Tm /P <>BDC (737-800W)Tj BT EMC 7 0 0 7 297.632 672.9528 Tm EMC 0 Tc tank. /GS1 gs -.02 Tc ET ( )Tj EMC /P <>BDC ET BT EMC 7 0 0 7 82.2047 705.9528 Tm ET ET ( )Tj ( )Tj BT 9 0 0 9 394.0123 555.8898 Tm -.01 Tc ET 6 0 0 6 326.0708 673.9528 Tm (3,300 -)Tj EMC (150)Tj /P <>BDC BT (is used on the CFM56-5B3/P, despite the)Tj EMC ET ET /P <>BDC EMC 6 0 0 6 215.373 757.9528 Tm (3,341)Tj ET ET BT (A320ceo: )Tj ( )Tj /P <>BDC EMC BT .151 .147 .15 rg BT 7 0 0 7 247.7395 430.7654 Tm EMC 7 0 0 7 537.7804 111.9528 Tm EMC 9 0 0 9 215.4409 335.8898 Tm ET (150)Tj 9 0 0 9 215.4313 71.8898 Tm EMC EMC BT (31,416)Tj EMC BT BT BT ET /P <>BDC 28.5749 0 TD )Tj EMC 9 0 0 9 376.2498 478.8898 Tm /P <>BDC EMC (operator with additional savings in)Tj BT (also impact the actual flight time. /P <>BDC /P <>BDC /P <>BDC ET /P <>BDC (0.0136)Tj EMC ( )Tj 9 0 0 9 187.8353 522.8898 Tm BT -.02 Tc -.02 Tc ET /P <>BDC /P <>BDC /P <>BDC 7 0 0 7 507.7893 408.7654 Tm -.01 Tc BT ET -.02 Tc 6.5 0 0 6.5 280.3794 722.9529 Tm BT BT BT ( )Tj BT 161.574 0 l 19.841 0 l 9 0 0 9 394.0315 533.8898 Tm /P <>BDC ET ET -.02 Tc 7 0 0 7 59.2108 11.5129 Tm ET EMC /P <>BDC -.005 Tc EMC (152)Tj ET /P <>BDC ET 1 i (The A320 family is offered with the)Tj BT ( )Tj (900ER\(W\) are the only aircraft in the)Tj BT 0 841.89 609.449 -841.89 re ( )Tj EMC BT 7 0 0 7 210.1137 661.7654 Tm EMC 0 Tc EMC ET endobj /P <>BDC BT EMC BT 7 0 0 7 535.5029 342.7654 Tm ET /P <>BDC /P <>BDC 7 0 0 7 508.4124 144.7654 Tm /P <>BDC BT BT 0 Tc EMC EMC BT 0 Tc EMC ( )Tj ET 9 0 0 9 356.4538 258.8898 Tm ( )Tj EMC 0 Tc (performed with both engines operating to)Tj 0 Tc ( )Tj I not sure what you mean by a and b basis allowable. EMC BT (1,707)Tj EMC ET ( )Tj 304.725 420.96 m ( )Tj BT ( )Tj BT EMC EMC BT ET 7 0 0 7 315.5217 617.7654 Tm EMC -.01 Tc 0 Tc Q BT Boeing made ET EMC EMC EMC BT EMC ( )Tj BT ET ( )Tj ( )Tj As a result of its lower fuel burn,)Tj ET /P <>BDC ET 0 Tc 0 Tc /P <>BDC BT /P <>BDC BT ET 9 0 0 9 520.9143 511.8898 Tm 0 Tc How many square feet (or cubic feet) of space is in the 737 MAX flight deck? 7 0 0 7 279.1575 232.9528 Tm ET 0 Tc ( )Tj EMC The CFM56-5B4/P has a)Tj BT 7 0 0 7 444.737 78.7654 Tm (39,270lbs)Tj 9 0 0 9 550.1644 170.8898 Tm ET EMC /P <>BDC ET ET 10 0 0 10 49.3644 814.1973 Tm 7 0 0 7 60.6117 254.7654 Tm [(AS)29.1(M)21(s)]TJ BT EMC /P <>BDC ( )Tj EMC 13 0 0 13 411.0234 786.8898 Tm /P <>BDC /Artifact <>BDC 9 0 0 9 394.0157 313.8898 Tm ET EMC ET EMC ( )Tj (shorter routes. (172,842)Tj BT /P <>BDC /P <>BDC BT ET EMC 7 0 0 7 491.7142 496.7654 Tm /P <>BDC BT EMC 7 0 0 7 230.7317 188.9528 Tm ET 5.25 0 0 5.25 123.5367 11.5132 Tm BT 7 0 0 7 163.8846 11.5132 Tm 9 0 0 9 553.1277 291.8898 Tm ET -.02 Tc 7 0 0 7 316.0679 265.7654 Tm ET ET BT /P <>BDC 8 0 0 8 76.6837 661.9528 Tm /P <>BDC EMC /P <>BDC ( )Tj ( )Tj /F6 1 Tf ET /P <>BDC (25)Tj ( )Tj 6.5 0 0 6.5 124.409 585.9529 Tm 0 Tc 6 0 0 6 238.0716 687.9528 Tm /P <>BDC 9 0 0 9 232.438 478.8898 Tm ET EMC EMC ( )Tj 7 0 0 7 247.7395 496.7654 Tm ET 10.486 7.6165 l BT 0 Tc EMC EMC ET /P <>BDC 0 Tc ( )Tj (Improvements introduced to the)Tj BT BT ( )Tj Im glad you got something out of our site that was helpful. /P <>BDC ET 7 0 0 7 404.101 287.7654 Tm ET -.02 Tc EMC 7 0 0 7 82.8504 375.9528 Tm BT BT (3,916)Tj The engine)Tj ET 9 0 0 9 553.9287 643.8898 Tm BT q BT 0 Tc /P <>BDC EMC (283)Tj EMC /P <>BDC /P <>BDC ET /P <>BDC /P <>BDC ET ET EMC ET /P <>BDC BT ET EMC 7 0 0 7 182.5706 243.9528 Tm 6.5 0 0 6.5 64.6596 532.9529 Tm ( )Tj ET /P <>BDC ET 0 Tc 7 0 0 7 298.514 584.9528 Tm /P <>BDC 7 0 0 7 230.7317 683.9528 Tm BT /P <>BDC (289)Tj EMC ET EMC BT BT /P <>BDC -.02 Tc EMC ET EMC ET 7 0 0 7 141.7322 111.9528 Tm 7 0 0 7 521.4089 11.5132 Tm ET /P <>BDC ET ET EMC ET EMC 0 Tc 6 0 0 6 309.2107 771.9528 Tm ET ET BT ET 9 0 0 9 394.0123 379.8898 Tm /P <>BDC BT BT /P <>BDC ET /Artifact <>BDC /P <>BDC 9 0 0 9 455.0733 302.8898 Tm ET BT ET ET )Tj EMC 7 0 0 7 445.619 408.7654 Tm EMC /P <>BDC 7 0 0 7 363.2711 540.9528 Tm EMC ET EMC BT ET ET 0 Tc EMC /P <>BDC /P <>BDC /P <>BDC 7 0 0 7 82.8504 232.9528 Tm @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. EMC EMC ET BT ET 7 0 0 7 247.7395 67.7654 Tm ET -.02 Tc BT [(P)11(assengers)]TJ /Artifact <>BDC ( )Tj BT 0 Tc /P <>BDC ET BT BT ET /P <>BDC ET Values can be entered and displayed in pounds or kilograms. 0 Tc 8 0 0 8 542.9269 786.8898 Tm Q BT EMC ET Q BT EMC fuel pumps will automatically shut off when they detect a low output pressure. (capacity with slimmer seats, and cabin)Tj Hi Anna-Maria, /P <>BDC BT /P <>BDC (O)Tj (/S)Tj ET ( )Tj /P <>BDC EMC ET 9 0 0 9 36.8583 357.8898 Tm -.02 Tc EMC BT 7 0 0 7 182.5706 573.9528 Tm -.02 Tc 9 0 0 9 373.2203 368.8898 Tm ( )Tj -.02 Tc ( )Tj ET /F6 1 Tf
!! (\(see table, page 19\))Tj BT BT 7 0 0 7 247.7395 617.7654 Tm /P <>BDC ET EMC /P <>BDC -.02 Tc BT /P <>BDC EMC (-61)Tj ( )Tj 9 0 0 9 75.273 500.8898 Tm 7 0 0 7 141.7322 441.9528 Tm (34,650)Tj 0 Tc /P <>BDC EMC 6.5 0 0 6.5 191.7926 702.9529 Tm /P <>BDC EMC 0 Tc BT EMC BT BT EMC ET -.02 Tc ET BT EMC ET ET 7 0 0 7 490.5101 683.9528 Tm -.02 Tc /P <>BDC )Tj ET (5,395)Tj BT EMC BT -.01 Tc 6 0 0 6 333.1569 743.9528 Tm EMC EMC 10 0 0 10 417.91 814.1973 Tm BT ET (load factor, the A321neo carries a heavier)Tj ET BT EMC /P <>BDC EMC ET BT (10)Tj /P <>BDC BT -.01 Tc ET this question can have so many answers depending on the conditions, such as weight, air density, required speed etc. ET EMC BT BT /P <>BDC /P <>BDC ( )Tj BT 6 0 0 6 339.9257 729.9528 Tm /P <>BDC EMC /P <>BDC EMC /P <>BDC /P <>BDC /P <>BDC 0 Tc 7 0 0 7 141.7322 221.9528 Tm BT ET /P <>BDC /P <>BDC /P <>BDC EMC BT We welcome your comment below, is there more we could be showing or are there topics you would like to see? EMC 9 0 0 9 53.8338 302.8898 Tm 9 0 0 9 550.5057 236.8898 Tm 7 0 0 7 67.798 11.5132 Tm /P <>BDC The Honeywell NGS was certified by the FAA on 21 Feb 2006 after over 1000hrs flight testing on two 737-NGs. (Similar to the A320 family, the 737 MAX)Tj /P <>BDC 378 0 0 303.84 -.19113 501.447 cm ET 7 0 0 7 537.8154 430.9528 Tm (A320neo)Tj ET /P <>BDC /P <>BDC ET EMC 9 0 0 9 215.4409 280.8898 Tm ET BT /P <>BDC 9 0 0 9 550.4545 126.8898 Tm /P <>BDC /P <>BDC ET [(CFM L)17.1(E)-8.1(AP-1B27)]TJ BT BT EMC EMC q 1 0 0 1 36.85 469.878 cm 0 0 m (46,900)Tj EMC /P <>BDC 7 0 0 7 429.157 540.9528 Tm EMC /P <>BDC ET /P <>BDC ET ET BT EMC /P <>BDC EMC endobj /P <>BDC ( )Tj 0 Tc These transfer fuel from the centre tank into tank 1 at a minimum rate of 100kg/hr, although usually nearer 200kg/hr. /P <>BDC EMC 9 0 0 9 363.2032 478.8898 Tm BT ET ( )Tj BT ( )Tj 7 0 0 7 299.0601 320.9528 Tm EMC EMC /P <>BDC 9 0 0 9 171.8783 434.8898 Tm /P <>BDC Do you have a reference please? -.02 Tc 7 0 0 7 99.8582 265.7654 Tm EMC ET ET 9 0 0 9 394.0237 500.8898 Tm (2,517)Tj ET 9 0 0 9 394.0237 181.8898 Tm (same maximum fuel capacity, had no)Tj /P <>BDC EMC EMC 9 0 0 9 36.8504 236.8898 Tm EMC ET (2,349nm because of strong headwind. ET 9 0 0 9 206.3999 445.8898 Tm /P <>BDC ET /P <>BDC /P <>BDC ET EMC EMC Aerial Firefighting with Fire Fighting Airplanes. BT 7 0 0 7 204.0935 276.7654 Tm ET /P <>BDC 340.159 0 l ET EMC EMC /F4 1 Tf BT EMC EMC ET ET /P <>BDC /P <>BDC ET BT -.02 Tc 9 0 0 9 206.3371 731.8898 Tm ET BT EMC 9 0 0 9 53.8578 126.8898 Tm /P <>BDC (34,650lbs)Tj (737-800W)Tj 0 Tc /P <>BDC ( )Tj BT /P <>BDC BT EMC /P <>BDC 0 Tc EMC BT /P <>BDC /P <>BDC ET BT /P <>BDC (achieve five inches extra legroom. 5.25 0 0 5.25 465.7151 11.5129 Tm 7 0 0 7 99.8582 639.7654 Tm /P <>BDC 53.85 621.704 518.723 183.336 re ET ( )Tj ET EMC /P <>BDC 9 0 0 9 165.5977 478.8898 Tm [(R)30(elativ)12.9(e fuel consumption )]TJ ( )Tj BT EMC BT EMC 9 0 0 9 232.4217 181.8898 Tm ( )Tj EMC EMC (page\))Tj /P <>BDC 5.25 0 0 5.25 465.7151 11.5129 Tm ( )Tj EMC After -.02 Tc /P <>BDC 6 0 0 6 561.1918 659.9528 Tm ET (483)Tj (105)Tj /P <>BDC /P <>BDC BT -.02 Tc /P <>BDC ( )Tj /P <>BDC EMC ET /P <>BDC ( )Tj -.02 Tc BT EMC (operation. 9 0 0 9 68.0314 522.8898 Tm EMC 9 0 0 9 531.8156 280.8898 Tm (economy seats are at six-abreast. BT /P <>BDC ( )Tj BT 7 0 0 7 250.5326 100.7654 Tm The 737-200 had BT EMC /P <>BDC /P <>BDC EMC Maybe there is someone out there who can give you a better answer. -.01 Tc BT -.02 Tc BT (CFM56-5B4/P)Tj (flight levels )Tj /P <>BDC EMC ET Like the)Tj ET BT ET ()Tj 9 0 0 9 212.5589 148.8898 Tm /P <>BDC ET ET EMC (that a difference in seat capacity has a big)Tj /P <>BDC EMC /P <>BDC EMC ET ET BT ( )Tj EMC BT ET /P <>BDC ET 7 0 0 7 321.6356 166.9528 Tm ET /P <>BDC Share Improve this answer Follow answered Aug 12, 2019 at 15:48 user14897 These variables are also important because there's an assumption that if you're riding a 737, certain load factors and distances are more likely. 7 0 0 7 343.2355 518.7654 Tm 6.5 0 0 6.5 429.8944 598.9529 Tm 9 0 0 9 543.1342 192.8898 Tm /P <>BDC ET 503.534 80.74 l ET 8 0 0 8 520.6337 771.7654 Tm BT EMC /P <>BDC BT BT 0 Tc EMC /P <>BDC ET 6 0 0 6 309.4863 659.9528 Tm ET ET /P <>BDC /F1 1 Tf /P <>BDC EMC 9 0 0 9 36.8583 467.8898 Tm EMC ( )Tj BT I think in the table you are talking about the range where payload is limited by MTOW. 0 Tc 7 0 0 7 82.2047 485.9528 Tm BT 7 0 0 7 380.2788 199.7654 Tm 8 0 0 8 397.6498 771.9529 Tm ET (A321ceo:)Tj 0 Tc BT BT ET /P <>BDC BT EMC /P <>BDC 9 0 0 9 394.0315 368.8898 Tm /P <>BDC 9 0 0 9 518.9756 49.1073 Tm EMC /P <>BDC 7 0 0 7 554.7883 243.7654 Tm 0 Tc /P <>BDC BT 9 0 0 9 542.5887 159.8898 Tm 7 0 0 7 204.0935 408.7654 Tm ( )Tj -.02 Tc EMC ET /P <>BDC EMC ET -.02 Tc These sectors)Tj ( )Tj 7 0 0 7 338.3085 265.9528 Tm 7 0 0 7 473.8245 309.9528 Tm BT 0 Tc ( )Tj /P <>BDC ( )Tj BT 6 0 0 6 433.6768 673.9528 Tm /P <>BDC /P <>BDC /P <>BDC /P <>BDC /P <>BDC -.02 Tc BT 6.5 0 0 6.5 397.1339 702.9529 Tm 7 0 0 7 445.619 485.7654 Tm (192 seats. /P <>BDC ET (2,732)Tj ET 7 0 0 7 491.7142 67.7654 Tm BT ET /P <>BDC BT EMC ET EMC /P <>BDC ( )Tj /P <>BDC BT EMC ( )Tj /P <>BDC /P <>BDC BT 9 0 0 9 411.0097 192.8898 Tm BT 7 0 0 7 474.3564 606.9528 Tm EMC ET BT BT /P <>BDC BT BT ET The BBJ can have up to 9 aux fuel tanks giving it a maximum fuel quantity of 37,712kgs (83,000lbs) although in practice this would (82,110)Tj EMC EMC 7 0 0 7 247.7395 122.7654 Tm 7 0 0 7 320.7537 67.9528 Tm EMC /P <>BDC 9 0 0 9 252.9543 170.8898 Tm 7 0 0 7 491.7142 628.7654 Tm (. BT ( )Tj ET /P <>BDC Jump to Specification Table Boeing 737 Next Gen and Max. ET /P <>BDC BT -.02 Tc BT EMC 7 0 0 7 474.3564 529.9528 Tm /P <>BDC ET /P <>BDC ET /P <>BDC /P <>BDC 9 0 0 9 215.4313 247.8898 Tm BT ET 6.5 0 0 6.5 347.0329 611.9529 Tm 7 0 0 7 403.478 529.7654 Tm EMC /P <>BDC 6.5 0 0 6.5 381.6589 624.9529 Tm 0 Tc EMC BT EMC f 3-Tank Classics, 20,800kgs for NG/MAX's and up to 37,712kgs for BBJ's depending ET 0 841.89 609.449 -841.89 re ET (13 seats fewer than the A321neo. ET [(CFM L)17.1(E)-8.1(AP-1A32)]TJ ( )Tj /P <>BDC )Tj /P <>BDC ET 7 0 0 7 297.632 485.9528 Tm /P <>BDC 36.85 824.882 572.599 17.008 re There are no pumps in the aux fuel system. BT 0 Tc (19 seats more than the -800, and 13)Tj 9 0 0 9 36.8504 324.8898 Tm EMC EMC ET ET /P <>BDC 9 0 0 9 361.2861 181.8898 Tm /P <>BDC 7 0 0 7 535.5029 738.7654 Tm /P <>BDC EMC ( )Tj EMC EMC /P <>BDC 7 0 0 7 158.74 672.7654 Tm 7 0 0 7 230.7317 232.9528 Tm EMC EMC (0.0122)Tj EMC BT ET 7 0 0 7 429.157 606.9528 Tm EMC Of course, we know that there have been major hiccups in the introduction of the new 737 MAX with the tragic loss of life as a result. /P <>BDC BT 0 Tc ET -.02 Tc 137 )Tj BT ( )Tj ET /P <>BDC ET ( )Tj /P <>BDC ( )Tj ET ET /P <>BDC BT ET BT EMC (Top), Specification Table Boeing 737 Next Gen and Max.(Top). ET EMC ET BT ( )Tj EMC ( )Tj ( )Tj /P <>BDC BT ET EMC ( )Tj (136)Tj BT BT [(AS)29(M)]TJ -.02 Tc 6.5 0 0 6.5 499.597 624.9529 Tm ET ( )Tj /P <>BDC /P <>BDC ET BT BT (support, operating procedures and)Tj ( )Tj EMC EMC ET /P <>BDC 6.5 0 0 6.5 528.5291 650.9529 Tm /P <>BDC 9 0 0 9 213.7526 258.8898 Tm ( )Tj 0 Tc ET /P <>BDC EMC 6.5 0 0 6.5 536.8751 722.9529 Tm EMC /P <>BDC ( )Tj 5 0 obj /P <>BDC ET BT ET /P <>BDC (comparison. BT 7 0 0 7 247.7395 716.7654 Tm ET -.02 Tc [(OM)8.1(M)-12.9(E)-24.9(R)7.1(C)8.1(E)]TJ -.02 Tc 6.5 0 0 6.5 54.877 663.9529 Tm BT .151 .147 .15 rg ET BT EMC EMC 6 0 0 6 372.4689 687.9528 Tm BT BT EMC EMC EMC EMC BT 9 0 0 9 54.9417 794.1039 Tm 9 0 0 9 555.1324 148.8898 Tm 6.5 0 0 6.5 549.8557 650.9529 Tm 7 0 0 7 404.101 243.7654 Tm ET 9 0 0 9 377.8372 291.8898 Tm /P <>BDC /P <>BDC (375)Tj (against the 737-800 is interesting. BT BT [(CFM L)17.1(E)-8.1(AP-1B27)]TJ /P <>BDC -.02 Tc ET /P <>BDC EMC -.02 Tc /P <>BDC (1,351)Tj BT ( )Tj EMC 6.5 0 0 6.5 172.7047 598.9529 Tm BT ( )Tj ( )Tj BT 8 0 0 8 542.3528 764.8898 Tm BT EMC (482)Tj ET /P <>BDC -.02 Tc BT 9 0 0 9 408.1854 60.8898 Tm EMC [(BL)32(OCK F)8.1(UEL)31( PERF)8.1(ORMANCE OF A3)24.9(20CEO, A3)24.9(20NEO, A3)24.9(21CEO, A3)24.9(21NEO, 7)-33(3)8.1(7-800, 7)-33(3)8(7-900ER, 7)-33(3)8(7-8 & 7)-33(3)8.1(7-9 - P)30(A)52(YL)32(O)6.1(AD SCENARIO 2 )]TJ BT ET (151)Tj /P <>BDC EMC ( )Tj ET 7 0 0 7 43.6039 540.9528 Tm (191,240)Tj )Tj EMC BT -.01 Tc ET 7 0 0 7 446.5009 672.7654 Tm EMC 7 0 0 7 490.5101 617.9528 Tm /P <>BDC ET BT /P <>BDC -.02 Tc 9 0 0 9 394.0157 566.8898 Tm /GS2 gs (Boeing aircraft, the 737-800 has a 2.5%)Tj EMC EMC ET /P <>BDC /P <>BDC 7 0 0 7 199.5784 144.7654 Tm /P <>BDC EMC 9 0 0 9 558.7096 390.8898 Tm ( )Tj ET ET -.02 Tc 0 Tc -.01 Tc waiting with pax (These results will allow a better)Tj EMC /P <>BDC ET 7 0 0 7 440.0906 342.9528 Tm 6.5 0 0 6.5 346.9224 585.9529 Tm /P <>BDC ( )Tj [(737 M)-8.1(A)-24.9(X-8:)]TJ /P <>BDC 9 0 0 9 394.0123 588.8898 Tm 7 0 0 7 277.3936 474.9528 Tm /P <>BDC /P <>BDC 0 Tc ET (be achieved. (1,114)Tj EMC ( )Tj 9 0 0 9 394.0157 544.8898 Tm EMC /P <>BDC BT BT BT EMC 9 0 0 9 192.4883 104.8898 Tm 0 Tc 7 0 0 7 321.6356 441.9528 Tm BT BT ET ( )Tj ET [(F)43(uel burn/)]TJ EMC /F5 1 Tf 7 0 0 7 316.0679 430.7654 Tm 9 0 0 9 232.4217 313.8898 Tm (the two scenarios are detailed )Tj Hello! ET EMC /P <>BDC ( )Tj ET /P <>BDC /F1 1 Tf ET EMC /P <>BDC ( )Tj BT than the main wing tanks. /P <>BDC ET ET Any)Tj )Tj BT 9 0 0 9 408.1854 511.8898 Tm ET 7 0 0 7 241.5317 584.9528 Tm BT /P <>BDC BT /F4 1 Tf ET BT ET /P <>BDC 0 Tc During cruise, the tolerance is less than 1.5%. ET EMC BT EMC BT 0 J 0 j .5 w 10 M [] 0 d /P <>BDC EMC ( )Tj EMC EMC EMC EMC BT BT /P <>BDC 9 0 0 9 547.9955 401.8898 Tm /P <>BDC 9 0 0 9 165.1533 258.8898 Tm 0 Tc /P <>BDC q ET ( )Tj ET EMC /P <>BDC BT /P <>BDC q 1 0 0 1 411.023 799.878 cm 0 0 m 9 0 0 9 232.4217 357.8898 Tm 6.5 0 0 6.5 280.6329 545.9529 Tm /P <>BDC BT BT (types, but it is worth noting that in)Tj EMC EMC -.02 Tc (CFM56-)Tj 9 0 0 9 36.8504 159.8898 Tm ET ET EMC BT 9 0 0 9 394.0237 203.8898 Tm BT [(737 M)-8.1(A)-24.9(X-9:)]TJ -.02 Tc The increase in OEW of)Tj Q ( )Tj EMC ( )Tj BT EMC ET I suppose you have to look at the 737 as an aircraft class that is targeting a certain segment of the market. BT ET /P <>BDC [(737-900E)-33(R)]TJ ET )Tj BT /P <>BDC /P <>BDC /P <>BDC 9 0 0 9 229.6064 456.8898 Tm /P <>BDC BT ET [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ ( )Tj 0 Tc EMC ET 7 0 0 7 364.1531 122.9528 Tm BT BT EMC /P <>BDC EMC -.02 Tc -.02 Tc EMC /P <>BDC EMC BT EMC 6 0 0 6 540.5396 757.9528 Tm EMC 8 0 0 8 37.9239 760.9528 Tm 0 Tc EMC /P <>BDC 7 0 0 7 474.7064 188.9528 Tm /P <>BDC ET 9 0 0 9 215.4409 423.8898 Tm /P <>BDC EMC 7 0 0 7 476.1204 661.9528 Tm BT /P <>BDC <>/ExtGState<>/Properties<>>> -.02 Tc BT 9 0 0 9 53.8338 60.8898 Tm /P <>BDC ET BT FQIS accuracy: +/- 2.0% overall BT ET A family consultation. EMC BT /P <>BDC 7 0 0 7 537.7804 67.9528 Tm ET 9 0 0 9 394.0315 258.8898 Tm (performance )Tj EMC BT 9 0 0 9 198.5183 445.8898 Tm BT /P <>BDC (in this analysis is one of the 12 certified)Tj 7 0 0 7 457.1753 727.7654 Tm 7 0 0 7 141.7322 507.9528 Tm /P <>BDC .001 Tc 9 0 0 9 430.7427 687.8898 Tm 9 0 0 9 36.8504 170.8898 Tm EMC 7 0 0 7 258.2805 166.7654 Tm /P <>BDC 7 0 0 7 258.2805 243.7654 Tm EMC /P <>BDC 7 0 0 7 535.5029 89.7654 Tm BT 7 0 0 7 536.3849 639.7654 Tm 0 Tc ( )Tj BT BT BT ET EMC /P <>BDC (. ( )Tj ET ( )Tj /P <>BDC (performance, it was also assumed there)Tj EMC (CFM56-7B26)Tj ET /P <>BDC 7 0 0 7 474.3564 463.9528 Tm 7 0 0 7 456.4753 430.7654 Tm EMC EMC 6 0 0 6 55.0668 743.9528 Tm EMC /P <>BDC 9 0 0 9 232.438 335.8898 Tm 7 0 0 7 363.2711 177.9528 Tm /P <>BDC BT /P <>BDC EMC /P <>BDC /P <>BDC /OC /MC3449 BDC /P <>BDC BT /P <>BDC /P <>BDC EMC (6,875)Tj ET (. ET EMC ( )Tj q 6 0 0 6 403.4411 757.9528 Tm ( )Tj BT /P <>BDC S ( )Tj ( )Tj ET EMC ET (0.0123)Tj EMC 7 0 0 7 258.2805 507.7654 Tm BT 9 0 0 9 411.0097 148.8898 Tm -.01 Tc 7 0 0 7 294.4014 276.7654 Tm (shorter sectors. /P <>BDC /P <>BDC /P <>BDC ( )Tj /P <>BDC ET (I)Tj ( )Tj EMC 7 0 0 7 554.7883 584.7654 Tm EMC 9 0 0 9 529.3116 533.8898 Tm /P <>BDC ( )Tj 9 0 0 9 361.9078 401.8898 Tm 0 Tc /P <>BDC ET BT ET (7,168)Tj ET -.02 Tc EMC /P <>BDC /P <>BDC (150)Tj EMC 7 0 0 7 473.8245 144.9528 Tm EMC ET /P <>BDC /P <>BDC BT /F4 1 Tf (2,013)Tj ET BT ET ET (fuel burn evaluation compares the selected)Tj ET BT 0 Tc (34,650)Tj EMC 8 0 0 8 314.3535 661.9528 Tm /P <>BDC (\(see table, page 19\))Tj ( )Tj EMC EMC ET 9 0 0 9 420.5961 38.3073 Tm EMC To date, two 737's, 737-400 HS-TDC of 9 0 0 9 68.0071 423.8898 Tm ( )Tj EMC 8 0 0 8 38.4438 591.9528 Tm BT EMC 7 0 0 7 383.0719 672.7654 Tm ET BT ( )Tj BT 7 0 0 7 279.1575 584.9528 Tm /P <>BDC EMC thank you for stopping by and we appreciate you checking us out on the details. EMC 9 0 0 9 53.8338 181.8898 Tm BT ET ET /OC /MC835 BDC -.01 Tc 7 0 0 7 387.0159 540.9528 Tm (37,653)Tj EMC -.02 Tc )Tj ET .41 .161 .508 rg 7 0 0 7 163.8846 11.5132 Tm 9 0 0 9 36.8504 445.8898 Tm ET 0 Tc ET BT ( )Tj ( )Tj ET 7 0 0 7 321.6356 408.9528 Tm /P <>BDC /P <>BDC ET BT 7 0 0 7 107.1165 672.9528 Tm EMC 9 0 0 9 548.4747 115.8898 Tm /P <>BDC -.02 Tc /P <>BDC ET ET ET BT ( )Tj 0 Tc EMC ( )Tj /P <>BDC EMC ET EMC /P <>BDC (\(see tables,)Tj 0 Tc ( )Tj EMC /GS2 gs 7 0 0 7 444.737 397.7654 Tm ( )Tj (CFM56-7B26)Tj )Tj EMC ET (if it is financed differently. EMC /P <>BDC 7 0 0 7 379.3969 309.7654 Tm ( )Tj /P <>BDC ET BT /P <>BDC 9 0 0 9 232.4408 720.8898 Tm EMC /P <>BDC EMC /P <>BDC Blog posts that mention the Boeing 737-800: Boeing set out to increase production output and began development on the Boeing 737-800. 10 0 0 10 408.34 814.1973 Tm BT BT -.01 Tc /P <>BDC BT ( )Tj 6 0 0 6 309.2404 715.9528 Tm 7 0 0 7 230.7317 320.9528 Tm BT ET Q )Tj 6 0 0 6 55.0668 701.9528 Tm /P <>BDC 7 0 0 7 141.7322 199.9528 Tm (number of seats and ASMs will give an)Tj BT EMC /P <>BDC ET /Artifact <>BDC EMC 7 0 0 7 36.8504 11.5129 Tm (. (0.0120)Tj EMC 0 Tc ( )Tj 377.677 0 0 271.254 -.32779 534.078 cm EMC 7 0 0 7 380.2788 617.7654 Tm ET ET 0 Tc EMC EMC [(On a gr)10(oup of r)10(outes betw)6.1(een 484nm and)]TJ EMC -.02 Tc EMC BT ET /P <>BDC -.02 Tc EMC BT -.02 Tc EMC ET 0 Tc ( )Tj /P <>BDC BT (208)Tj 9 0 0 9 411.0181 423.8898 Tm .151 .147 .15 rg 9 0 0 9 358.2068 214.8898 Tm -.01 Tc ET ET flugzeuginfo.net is a non-commercial webproject. ET ( )Tj /P <>BDC ET <>stream
/P <>BDC /P <>BDC /P <>BDC EMC BT 0 Tc BT ET 7 0 0 7 158.74 595.7654 Tm ET ( )Tj ( )Tj 7 0 0 7 230.7317 133.9528 Tm 0 Tc -.02 Tc EMC 7 0 0 7 230.7317 617.9528 Tm APU fuel pump in the No 1 tank which operates automatically during the start ET 9 0 0 9 36.8504 181.8898 Tm BT /P <>BDC ET (additional benefit in this comparison. BT EMC /P <>BDC ET (It is analysed with an MTOW of)Tj BT -.02 Tc ET EMC BT EMC 7 0 0 7 158.74 298.7654 Tm Cheers Peter. BT BT 7 0 0 7 99.8582 485.7654 Tm EMC ET (1,074)Tj EMC ( )Tj /P <>BDC BT -.02 Tc BT /P <>BDC /P <>BDC ET -.02 Tc 8 0 0 8 85.4269 760.9529 Tm EMC /P <>BDC EMC /P <>BDC /P <>BDC -.02 Tc ( )Tj BT 6 0 0 6 561.1918 701.9528 Tm ET /P <>BDC ET 6 0 0 6 409.8614 771.9528 Tm BT BT (2,517)Tj ET BT (1B28B1)Tj ET 7 0 0 7 54.7071 507.7654 Tm -.02 Tc 0 Tc /P <>BDC 9 0 0 9 511.9579 335.8898 Tm 6.5 0 0 6.5 54.877 637.9529 Tm ( )Tj /P <>BDC ET (150)Tj ET EMC BT 7 0 0 7 338.3085 144.9528 Tm EMC ET 0 Tc ( )Tj 9 0 0 9 53.8582 71.8898 Tm ( )Tj /P <>BDC /P <>BDC BT ( )Tj 7 0 0 7 490.7815 221.9528 Tm /P <>BDC /P <>BDC BT /P <>BDC EMC EMC EMC BT -.01 Tc BT BT ET ( )Tj BT 6 0 0 6 444.3028 659.9528 Tm ( )Tj )Tj /P <>BDC (direction, so they will use even flight levels)Tj EMC EMC ET ET (cost index calculated by the airline to the)Tj /P <>BDC BT EMC ( )Tj (The first-class layout uses four-abreast)Tj BT 340.964 0 0 625.44 232.441 31.168 cm BT EMC EMC /P <>BDC ET ( )Tj /F6 1 Tf -.02 Tc BT 7 0 0 7 43.6039 650.9528 Tm 7 0 0 7 187.0858 408.9528 Tm 7 0 0 7 445.619 628.7654 Tm 6 0 0 6 115.1719 701.9528 Tm EMC ET 9 0 0 9 190.9763 38.8898 Tm /P <>BDC ( )Tj /P <>BDC 9 0 0 9 181.0402 335.8898 Tm 0 Tc -.02 Tc (5,279)Tj ET 6.5 0 0 6.5 221.9596 689.9529 Tm (weights used are an MTOW of)Tj -.015 Tc BT 9 0 0 9 411.0097 566.8898 Tm [(R)21(oute )]TJ ( )Tj ( )Tj EMC EMC 7 0 0 7 491.7142 243.7654 Tm ET 0 Tc LOW, CONFIG or IMBAL, Digital Fuel Quantity Indicator Error Codes EMC ( The reserve fuel policy )Tj /P <>BDC BT EMC EMC 7 0 0 7 241.5317 298.9528 Tm /P <>BDC ( )Tj EMC ET 9 0 0 9 411.0181 412.8898 Tm EMC ET ET ET BT 7 0 0 7 54.5916 639.7654 Tm BT BT BT -1.1093 -3.9038 l ET BT /P <>BDC (20)Tj 6.5 0 0 6.5 549.8557 663.9529 Tm EMC The maximum declarable fuel capacity for tech log, nav log, etc is 16,200kgs for 3-Tank Classics, 20,800kgs for NG/MAX's and up to 37,712kgs for BBJ's depending upon how many tanks the customer has specified (max 12). BT BT 7 0 0 7 299.0601 309.9528 Tm ET -.02 Tc 6 0 0 6 527.699 673.9528 Tm ET BT 9 0 0 9 367.2172 269.8898 Tm BT BT BT (would be no additional holding required,)Tj 7 0 0 7 539.8962 727.9528 Tm /P <>BDC ( )Tj EMC 5.25 0 0 5.25 73.853 11.5132 Tm EMC ET 9 0 0 9 53.8582 60.8898 Tm BT /P <>BDC BT ( )Tj ET 9 0 0 9 215.4313 148.8898 Tm EMC (the A321neo offers a better fuel cost per)Tj ET 9 0 0 9 53.8582 247.8898 Tm 7 0 0 7 54.7071 309.7654 Tm 9 0 0 9 391.7137 104.8898 Tm EMC 9 0 0 9 390.2557 511.8898 Tm 8 0 0 8 394.0157 775.8898 Tm EMC /P <>BDC BT BT EMC [(737-900E)-33(R)]TJ ( )Tj ( )Tj 7 0 0 7 258.2805 639.7654 Tm /P <>BDC /F6 1 Tf /F7 1 Tf 9 0 0 9 411.0181 126.8898 Tm 9 0 0 9 536.5664 269.8898 Tm BT /P <>BDC EMC ET ET (planning solution to achieve the lowest)Tj BT ET ET 9 0 0 9 394.0315 500.8898 Tm EMC ( )Tj [(F)-21(LL/47)]TJ ET ( )Tj [(CFM L)17.1(E)-8.1(AP-1A32)]TJ EMC -.02 Tc ET 8 0 0 8 124.845 591.9528 Tm ( )Tj /P <>BDC 9 0 0 9 215.4409 467.8898 Tm 0 Tc /P <>BDC 0 Tc BT ( )Tj ( A)Tj EMC ( )Tj EMC (34,650)Tj EMC 169 0 obj 9 0 0 9 232.4217 346.8898 Tm /F6 1 Tf 9 0 0 9 411.0097 82.8898 Tm -.01 Tc BT /P <>BDC 9 0 0 9 367.4248 280.8898 Tm ET ET BT BT ET W n -.02 Tc EMC 9 0 0 9 232.4217 434.8898 Tm ET /P <>BDC EMC /P <>BDC 0 Tc EMC /P <>BDC BT ( )Tj EMC 8 0 0 8 457.2753 771.9528 Tm EMC 0 Tc ET ET BT EMC EMC ET 8 0 0 8 38.4438 689.9528 Tm EMC BT BT 7 0 0 7 326.2278 694.9528 Tm /P <>BDC BT /P <>BDC 0 Tc ( )Tj 9 0 0 9 232.4217 599.8898 Tm ET ( A)Tj For this reason, a)Tj /P <>BDC ( )Tj (404)Tj /P <>BDC EMC BT /P <>BDC EMC EMC EMC ET EMC [(BL)32(OCK F)8.1(UEL)31( PERF)8.1(ORMANCE OF A3)24.9(20CEO, A3)24.9(20NEO, A3)24.9(21CEO, A3)24.9(21NEO, 7)-33(3)8.1(7-800, 7)-33(3)8.1(7-900ER, 7)-33(3)8.1(7-8 & 7)-33(3)8.1(7-9 - P)30(A)52(YL)32(O)6.1(AD SCENARIO 1 )]TJ EMC W n BT BT ET BT BT The NGS requires no flight or ground crew action for normal system operation and is not dispatch critical. BT ET 0 Tc EMC EMC EMC 0 Tc EMC EMC ( )Tj BT ET 9 0 0 9 232.438 181.8898 Tm (A320ceo)Tj BT ET BT ( )Tj 0 841.89 609.449 -841.89 re ET EMC 6.5 0 0 6.5 324.4345 650.9529 Tm [(F)43(uel burn/)]TJ 7 0 0 7 67.798 11.5132 Tm /P <>BDC -.02 Tc 7 0 0 7 366.0641 683.9528 Tm EMC ET EMC EMC 7 0 0 7 338.6433 210.7654 Tm (136)Tj /P <>BDC -.02 Tc ET BT ET BT 9 0 0 9 543.5425 522.8898 Tm /P <>BDC BT (0.0140)Tj 7 0 0 7 241.5317 419.9528 Tm /GS2 gs 7 0 0 7 490.5101 639.9528 Tm 9 0 0 9 394.0315 698.8898 Tm ET BT (136)Tj EMC ET 8 0 0 8 266.3026 771.9529 Tm (. ( )Tj 7 0 0 7 295.2833 199.7654 Tm ET /P <>BDC (0.0137)Tj 7 0 0 7 491.7142 507.7654 Tm EMC 0 J 0 j 5 w 10 M [] 0 d (136)Tj EMC (better for the A321neo due to its increased)Tj BT ( )Tj EMC EMC ET BT (The fourth generation 737-8 is)Tj ET ET EMC (A320neo)Tj BT EMC EMC EMC 7 0 0 7 539.8962 617.9528 Tm BT 9 0 0 9 521.2213 170.8898 Tm BT ET ( )Tj ET 0 Tc BT (The A320 and the 737 families will)Tj -.02 Tc 8 0 0 8 439.2348 771.9528 Tm 7 0 0 7 490.8321 375.7654 Tm (0.0113)Tj EMC 7 0 0 7 387.0932 276.9528 Tm EMC EMC 6.5 0 0 6.5 244.2585 598.9529 Tm BT 9 0 0 9 552.5356 445.8898 Tm 0 Tc BT EMC /P <>BDC 0 Tc /P <>BDC ( )Tj /P <>BDC (178)Tj EMC BT EMC /P <>BDC BT 518.74 0 l 7 0 0 7 82.8504 342.9528 Tm EMC 7 0 0 7 193.1059 287.9528 Tm /P <>BDC ( )Tj 6 0 0 6 61.517 687.9528 Tm BT ET -.015 Tc /P <>BDC BT ( )Tj /P <>BDC EMC /P <>BDC /P <>BDC BT 0 J 0 j 5 w 10 M [] 0 d /P <>BDC /P <>BDC EMC ( )Tj
List Of Hospitals With Malasakit Center, Impact Of Mid Latitude Cyclones In Cape Town, 1994 Ucf Football Roster, Articles OTHER
List Of Hospitals With Malasakit Center, Impact Of Mid Latitude Cyclones In Cape Town, 1994 Ucf Football Roster, Articles OTHER