9 0 0 9 192.4883 104.8898 Tm ET BT (405)Tj 0 Tc EMC (hugely successful. ET 0 Tc BT (the planned payload of 170. EMC ET ET BT BT EMC ET ET /P <>BDC -.02 Tc (operationally safe to do so, in the)Tj -.02 Tc (1,089)Tj BT ( )Tj ET EMC ET EMC EMC BT EMC /P <>BDC 9 0 0 9 195.4853 126.8898 Tm EMC BT 9 0 0 9 408.1854 610.8898 Tm 6.5 0 0 6.5 225.3721 585.9529 Tm /P <>BDC 9 0 0 9 418.9315 59.9073 Tm 0 Tc 9 0 0 9 417.7488 511.8898 Tm /P <>BDC ( )Tj 0 Tc (282)Tj 0 Tc (0.0115)Tj BT -.02 Tc 0 Tc 9 0 0 9 172.0312 357.8898 Tm EMC 6 0 0 6 302.1568 743.9528 Tm /P <>BDC EMC (737-800 and 737-8; and 170 passengers on)Tj ( )Tj (737-800 is more efficient with up to a)Tj BT ( )Tj EMC (108)Tj BT ET <> EMC /P <>BDC BT /P <>BDC ET BT 7 0 0 7 315.1859 89.7654 Tm ET BT /P <>BDC EMC -.02 Tc 7 0 0 7 404.101 276.7654 Tm EMC EMC .151 .147 .15 rg ET -.02 Tc On older aircraft the trimmers were accessible from the EMC BBJ3 was officially launched in October 2006, with orders from two undisclosed customers. 7 0 0 7 473.4744 518.9528 Tm 9 0 0 9 547.3802 566.8898 Tm EMC BT (20)Tj /P <>BDC 0 Tc Hi Mark, BT BT /P <>BDC ET EMC ( )Tj ET /P <>BDC 9 0 0 9 383.3617 346.8898 Tm BT /P <>BDC ET EMC /P <>BDC /P <>BDC BT (The 737NG family has a single engine)Tj /P <>BDC EMC EMC -.02 Tc ( )Tj BT EMC 6.5 0 0 6.5 534.5352 624.9529 Tm /P <>BDC The wheelbase which is the distance from the nosewheel to the line between the main wheels, which is 11.07 metres. Q (airlines across the world. 6.5 0 0 6.5 192.6116 689.9529 Tm (2,517)Tj 7 0 0 7 404.101 166.7654 Tm Q 9 0 0 9 210.9209 104.8898 Tm BT EMC /Artifact <>BDC BT tank. 10 0 0 10 47.1144 814.1973 Tm /P <>BDC (space, thereby freeing up more floor area)Tj W n 7 0 0 7 491.392 463.9528 Tm ( )Tj ET 7 0 0 7 444.737 133.7654 Tm BT 0 Tc ( )Tj 7 0 0 7 386.3929 628.9528 Tm BT ET 63 0 obj EMC 9 0 0 9 51.0236 401.8898 Tm BT (31,416)Tj EMC /P <>BDC ET -.005 Tc /P <>BDC [(OM)8.1(M)-12.9(E)-24.9(R)7.1(C)8.1(E)]TJ Your email address will not be published. 9 0 0 9 229.6141 390.8898 Tm /P <>BDC BT BT EMC 0 Tc /P <>BDC /P <>BDC ET -.02 Tc /P <>BDC /F4 1 Tf 0 Tc 7 0 0 7 387.0932 177.9528 Tm -.01 Tc BT 9 0 0 9 51.0236 258.8898 Tm 6.5 0 0 6.5 483.8125 624.9529 Tm /F1 1 Tf -.02 Tc In this case I believe TUI fly is the main customer. EMC BT BT 7 0 0 7 279.1575 639.9528 Tm -.02 Tc 7 0 0 7 491.392 727.9528 Tm ET .014984 841.89 609.45 -841.89 re -.02 Tc ( )Tj ( )Tj EMC /P <>BDC /P <>BDC ( )Tj endobj (I)Tj ET 7 0 0 7 445.619 562.7654 Tm EMC /P <>BDC /P <>BDC ( )Tj ( )Tj ET BT EMC ( )Tj EMC EMC /P <>BDC 9 0 0 9 534.5925 753.8898 Tm ET ( )Tj -.02 Tc ET BT BT 7 0 0 7 95.225 11.5132 Tm ( )Tj BT 5.25 0 0 5.25 492.6848 11.5129 Tm ET /P <>BDC .41 .161 .508 RG /P <>BDC BT ET [(CFM L)17.1(E)-8.1(AP-1A32)]TJ /P <>BDC ET BT ( )Tj 8 0 0 8 551.3604 71.8898 Tm 0 Tc BT ET BT (A320ceo)Tj ET /P <>BDC BT 9 0 0 9 53.8338 148.8898 Tm ( )Tj ET EMC ET ( )Tj BT ( )Tj BT ET ET EMC 7 0 0 7 355.3163 89.7654 Tm )Tj BT ET EMC /P <>BDC 7 0 0 7 491.4046 210.9528 Tm ET 7 0 0 7 158.74 111.7654 Tm ( )Tj EMC ( )Tj BT BT BT /P <>BDC 0 Tc ET EMC EMC EMC 7 0 0 7 277.3936 661.9528 Tm (and all navigation and air traffic control)Tj ( )Tj ( )Tj BT 0 Tc [(OM)8(M)-13(E)-25(R)7(C)8(E)]TJ 7 0 0 7 158.74 408.7654 Tm BT /P <>BDC BT EMC ( )Tj (3,535)Tj /P <>BDC EMC /P <>BDC 9 0 0 9 571.9847 181.8898 Tm (5,394)Tj EMC (final comparison of the two manufacturers)Tj EMC 7 0 0 7 230.7317 177.9528 Tm /P <>BDC (44,057)Tj EMC 0 Tc BT /F6 1 Tf BT BT ET BT EMC ( )Tj /P <>BDC -.02 Tc BT BT ET 7 0 0 7 457.0984 507.7654 Tm EMC (of fuel against time-related costs. ( )Tj /Artifact <>BDC 0 Tc 7 0 0 7 327.1097 562.9528 Tm ET -.02 Tc 7 0 0 7 439.7405 529.9528 Tm ET ET EMC (2,748)Tj BT EMC EMC EMC /GS2 gs EMC BT EMC BT /P <>BDC /P <>BDC ( )Tj /P <>BDC 7 0 0 7 241.5317 221.9528 Tm EMC ( )Tj ET 7 0 0 7 82.2047 562.9528 Tm /P <>BDC EMC EMC /P <>BDC 517.244 80.729 l 7 0 0 7 536.3849 485.7654 Tm 7 0 0 7 101.0963 309.9528 Tm EMC 9 0 0 9 207.9609 511.8898 Tm (464,440)Tj /P <>BDC EMC ET /P <>BDC EMC The fuel tank was instrumented with gas sample tubing and thermocouples to /P <>BDC /P <>BDC 0 Tc -.01 Tc /P <>BDC /P <>BDC ET EMC EMC BT BT EMC EMC (150)Tj BT How much fuel do planes burn? EMC /P <>BDC /P <>BDC ET EMC 7 0 0 7 554.7883 562.7654 Tm /P <>BDC ET /P <>BDC BT EMC BT (379)Tj <> BT ET ET BT The 747-800 can climb to 40,000 feet and will burn 0.44 nautical mile per gallon. /P <>BDC 13 0 0 13 394.0123 71.8898 Tm -.02 Tc W n ( )Tj Airbus A320 Interior Inside the cabin of this city hopper. FQIS accuracy: +/- 3.0% 9 0 0 9 526.2638 401.8898 Tm ET (CFM56-7B27B3)Tj (CFM56-5B4/P)Tj (CFM56-7B26)Tj ET ET 8 0 0 8 153.6923 591.9528 Tm EMC EMC /P <>BDC 9 0 0 9 53.8578 434.8898 Tm EMC ET -.02 Tc f /P <>BDC ET ET ET ET BT /P <>BDC /P <>BDC -.01 Tc BT ( )Tj -.02 Tc 8 0 0 8 474.6331 771.7654 Tm -.07 Tc EMC ( )Tj ET 9 0 0 9 552.5356 445.8898 Tm ET .12988 .27633 .58575 rg EMC 7 0 0 7 427.7291 441.9528 Tm 0 J 0 j 5 w 10 M [] 0 d /P <>BDC /P <>BDC 7 0 0 7 386.3929 639.9528 Tm EMC 7 0 0 7 43.6039 639.9528 Tm ET ( )Tj /P <>BDC 0 Tc (35,112lbs)Tj /P <>BDC /P <>BDC EMC ET BT ET /P <>BDC (This weight variant is one of more than 20)Tj ET -.02 Tc -.02 Tc ET BT BT -.02 Tc [(P)11(assengers)]TJ /P <>BDC /P <>BDC EMC ( )Tj 9 0 0 9 229.6064 126.8898 Tm The 737-200Adv could also be fitted with an /P <>BDC /P <>BDC ET 9 0 0 9 548.3284 610.8898 Tm (2,514)Tj /P <>BDC [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ BT 7 0 0 7 469.2222 11.5129 Tm ET /P <>BDC /P <>BDC EMC )Tj /P <>BDC BT EMC /P <>BDC ET /P <>BDC 7 0 0 7 294.4014 67.7654 Tm ET /P <>BDC 9 0 0 9 53.8582 203.8898 Tm EMC ( )Tj ET 7 0 0 7 315.1859 78.7654 Tm (costs could almost double the per ASM)Tj (payload is carried. BT 5.25 0 0 5.25 447.6106 11.5129 Tm -.02 Tc 6 0 0 6 561.1317 771.9528 Tm /P <>BDC BT ( )Tj BT /P <>BDC (124,650)Tj BT (1,272)Tj 0 Tc BT 0 Tc 9 0 0 9 229.6141 115.8898 Tm q 1 0 0 1 53.85 797.54 cm 0 0 m EMC 9 0 0 9 215.4409 148.8898 Tm ( )Tj EMC BT ( )Tj BT BT ET BT EMC EMC BT EMC 6.5 0 0 6.5 243.8814 689.9529 Tm 7 0 0 7 279.1575 298.9528 Tm EMC BT on board for a late slot. EMC ET (A321neo)Tj ET endobj BT The NGS is an onboard inert gas system that uses an ET -.02 Tc ( )Tj -.01 Tc 7 0 0 7 381.1608 584.7654 Tm EMC The 14 routes are listed)Tj /P <>BDC EMC 9 0 0 9 229.6141 302.8898 Tm 9 0 0 9 181.5424 71.8898 Tm 9 0 0 9 190.2832 49.8898 Tm 7 0 0 7 521.4089 11.5132 Tm ET 7 0 0 7 539.8962 661.9528 Tm EMC ET ET ET BT 6 0 0 6 61.517 645.9528 Tm /P <>BDC EMC /P <>BDC ( )Tj 9 0 0 9 197.1772 82.8898 Tm /P <>BDC ET 9 0 0 9 215.433 82.8898 Tm (0.0122)Tj /P <>BDC 7 0 0 7 444.737 276.7654 Tm /P <>BDC 9 0 0 9 394.0315 786.8898 Tm 7 0 0 7 537.7804 111.9528 Tm /P <>BDC 7 0 0 7 473.8245 364.9528 Tm Main tanks < 50%, -1 to 5 deg pitch, +/- 1 deg roll: +/- 2.0 /P <>BDC The cockpit is a dual seat design. /P <>BDC ( )Tj ( )Tj BT ET /P <>BDC air speed, altitude, and similar flight parameters were made available from 0 Tc EMC 7 0 0 7 364.1531 166.9528 Tm 0 Tc ET BT 9 0 0 9 372.9598 170.8898 Tm 8 0 0 8 37.9239 760.9528 Tm 13 0 0 13 340.4557 467.8898 Tm /P <>BDC EMC BT BT (the A320ceo, despite the neos 1,200lbs)Tj /P <>BDC BT EMC 7 0 0 7 297.632 540.9528 Tm EMC 9 0 0 9 383.6209 423.8898 Tm EMC 9 0 0 9 206.8407 412.8898 Tm BT BT -.02 Tc The Boeing 737-800 variant has as mentioned 27300 pound-force delivered by two turbo fans. ET 0 Tc ( )Tj EMC /P <>BDC 9 0 0 9 215.4409 203.8898 Tm ET ( )Tj /P <>BDC /P <>BDC 6.5 0 0 6.5 64.6596 676.9529 Tm /P <>BDC BT ET 9 0 0 9 252.5189 181.8898 Tm BT ET /P <>BDC 9 0 0 9 394.0123 214.8898 Tm 7 0 0 7 294.4014 474.7654 Tm 6 0 0 6 527.699 701.9528 Tm 0 Tc ET EMC BT /P <>BDC /P <>BDC /P <>BDC 9 0 0 9 68.3339 500.8898 Tm 8 0 0 8 319.1147 771.9528 Tm BT 7 0 0 7 537.7804 177.9528 Tm (CFM56-7B26)Tj BT BT BT ( )Tj EMC /P <>BDC BT EMC (passengers. BT BT 6.5 0 0 6.5 549.8557 637.9529 Tm 7 0 0 7 43.6039 342.9528 Tm BT ( )Tj (31,416)Tj /P <>BDC /P <>BDC /P <>BDC EMC BT Newer 500 series aircraft have an extra, DC operated BT /P <>BDC ET EMC EMC 9 0 0 9 183.0113 214.8898 Tm ET EMC 0 Tc /P <>BDC ( )Tj BT (7B26)Tj /P <>BDC EMC ET ( )Tj EMC ( )Tj EMC ET ET ET ET BT EMC (\(see table, page 19\))Tj ET ET ( )Tj ( )Tj ( )Tj ET ( )Tj Since development and production Boeing has built 10,574 737-800s. BT ET 9 0 0 9 215.4409 247.8898 Tm BT /GS2 gs 0 Tc (powered by either the CFM56-5 series or)Tj BT EMC ( )Tj EMC EMC /P <>BDC -.02 Tc /P <>BDC /P <>BDC EMC (burns. ET EMC EMC EMC ( )Tj ET ( )Tj /P <>BDC 0 Tc -.02 Tc ( )Tj (136)Tj ( )Tj BT 0 Tc BT ET /P <>BDC BT ET 0 Tc ( )Tj BT EMC EMC 0 Tc ( )Tj ( )Tj EMC 7 0 0 7 338.3085 188.9528 Tm wing surface (rain, drizzle, snow, fog). BT ET ET (prices, and can vary by the aircraft type)Tj ( )Tj EMC BT ET /P <>BDC BT /P <>BDC BT EMC 9 0 0 9 232.4217 324.8898 Tm ET ET EMC q 1 0 0 1 394.016 758.971 cm 0 0 m BT EMC ( )Tj 6 0 0 6 444.3028 659.9528 Tm 13 0 0 13 177.4468 500.8898 Tm /P <>BDC If you look at your favourite model of car, you would see that they have also evolved over time to be something unrecognisable from their ancestors. BT ET BT -.02 Tc 0 Tc EMC BT /P <>BDC 7 0 0 7 535.5029 243.7654 Tm 7 0 0 7 294.4014 540.7654 Tm -.02 Tc 6.5 0 0 6.5 64.6596 558.9529 Tm EMC ET BT BT BT /F6 1 Tf 9 0 0 9 195.3413 181.8898 Tm EMC 0 Tc (1,995)Tj ET EMC EMC 108 lbs (49 kgs) to the 737-800 basic MEW. ET EMC BT ET BT EMC 7 0 0 7 354.6933 397.7654 Tm 0 Tc f ( )Tj ( )Tj ( )Tj EMC EMC BT ( )Tj EMC BT ( )Tj ET ( )Tj 0 Tc 6.5 0 0 6.5 486.1525 722.9529 Tm (BOS-DEN)Tj Q 0 Tc EMC 9 0 0 9 213.0312 335.8898 Tm ET EMC ET 0 Tc BT allowed for deposit of the ground-based NEA into the center wing tank (CWT). ET 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 EMC /F6 1 Tf BT EMC ET BT [(2,575nmn, the 737-8 has an av)12.9(er)10(age 13% lo)12(w)6.1(e)0(r)]TJ BT (124,650)Tj ET EMC ET The 737-200 had I am looking for the radius of the fuselage specifically the cargo door. BT (150)Tj These incidents, and 15 more on other types since 1959, EMC /P <>BDC BT ET EMC /P <>BDC EMC BT BT 9 0 0 9 53.8578 38.8898 Tm 10 0 0 10 425.05 814.1973 Tm EMC 6 0 0 6 109.2916 743.9528 Tm /P <>BDC EMC ET 9 0 0 9 387.3578 258.8898 Tm (equivalent engine thrust ratings for the neo)Tj EMC EMC (impacted by external factors such as)Tj /P <>BDC -.02 Tc 6 0 0 6 527.2669 729.9528 Tm /P <>BDC /P <>BDC (411)Tj EMC EMC EMC ET (163)Tj 9 0 0 9 232.4217 291.8898 Tm 7 0 0 7 387.619 430.9528 Tm /P <>BDC EMC /P <>BDC (428,060)Tj (163)Tj EMC EMC EMC 9 0 0 9 229.6141 49.8898 Tm 0 Tc ET -.02 Tc /P <>BDC ET BT (0.0113)Tj /P <>BDC 7 0 0 7 338.5674 584.9528 Tm ET /P <>BDC ET EMC 9 0 0 9 170.6722 104.8898 Tm ( )Tj BT /P <>BDC 0 Tc EMC BT BT /P <>BDC /P <>BDC 7 0 0 7 247.7395 166.7654 Tm 9 0 0 9 188.1863 170.8898 Tm /P <>BDC BT 7 0 0 7 277.3936 177.9528 Tm 6 0 0 6 351.3743 715.9528 Tm /Artifact <>BDC /P <>BDC BT ET EMC BT /P <>BDC /P <>BDC /P <>BDC 7 0 0 7 36.8504 11.5129 Tm ( )Tj 9 0 0 9 232.4217 82.8898 Tm (2,731)Tj EMC 9 0 0 9 36.8504 104.8898 Tm EMC (The alternate airports were selected based)Tj 0 Tc 0 Tc BT /P <>BDC ( )Tj EMC BT ET BT BT ET /P <>BDC BT BT ET ( )Tj 7 0 0 7 326.2278 496.9528 Tm BT 0 Tc The cruise speed to the alternate was)Tj ET (O)Tj EMC 432 0 obj /P <>BDC ( )Tj -.02 Tc /Artifact <>BDC EMC /P <>BDC BT 7 0 0 7 54.7071 210.7654 Tm 7 0 0 7 295.2833 78.7654 Tm BT ( )Tj BT BT ET /P <>BDC /P <>BDC BT ( )Tj BT /P <>BDC 340.964 0 0 625.44 232.441 31.168 cm -.02 Tc EMC EMC ET ( )Tj /P <>BDC /P <>BDC EMC 0 Tc ( )Tj ET -.01 Tc /P <>BDC 9 0 0 9 554.3696 269.8898 Tm EMC ( )Tj EMC BT /GS1 gs 0 Tc EMC EMC BT 7 0 0 7 230.7317 342.9528 Tm ET 9 0 0 9 215.433 214.8898 Tm ET ET BT EMC ( )Tj BT On the 1-500's, the centre tank pumps are located in a dry ( )Tj -.02 Tc ( )Tj Q EMC In addition to keeping the)Tj ET /P <>BDC EMC 7 0 0 7 88.196 11.5129 Tm BT ET We dont actually have access to a table of these variants and their features. EMC EMC q EMC EMC /P <>BDC ET (A321neo:)Tj BT BT BT ET ET BT ( )Tj 7 0 0 7 116.3631 11.5132 Tm /P <>BDC ET BT endobj /P <>BDC /P <>BDC EMC (18)Tj BT ET .964 .834 .406 rg ( )Tj ( )Tj EMC ET BT ET ET (Engine)Tj BT 9 0 0 9 198.165 225.8898 Tm BT 7 0 0 7 539.8962 540.9528 Tm /P <>BDC ET ( )Tj 9 0 0 9 377.8897 291.8898 Tm BT [(R)30(elativ)12.9(e oper)10(ational cost )]TJ (for the purposes of this performance)Tj 9 0 0 9 215.4313 203.8898 Tm /P <>BDC EMC 7 0 0 7 508.4124 386.7654 Tm 7 0 0 7 445.619 122.7654 Tm ET ET ET ET BT EMC ET EMC -.02 Tc EMC EMC 9 0 0 9 207.2279 511.8898 Tm tanks into the centre tank where it is then fed to the engines in the normal EMC 9 0 0 9 232.438 159.8898 Tm 9 0 0 9 75.273 511.8898 Tm /P <>BDC BT (900ER and 737-9, A320ceo and A320neo,)Tj 8 0 0 8 243.3422 771.9529 Tm (lower than the difference on the smaller)Tj BT /P <>BDC -.02 Tc BT (5,126)Tj BT (166,669)Tj /P <>BDC ET BT 7 0 0 7 230.7317 276.9528 Tm 7 0 0 7 456.2165 265.7654 Tm /P <>BDC ET /P <>BDC /F1 1 Tf /P <>BDC ET ET 8 0 0 8 38.4438 703.9528 Tm ( )Tj (977)Tj BT BT /P <>BDC /P <>BDC .0161 Tc /P <>BDC /P <>BDC Hi Bradley, ET ET (5,376)Tj /P <>BDC ( )Tj EMC 0 Tc EMC ET -.02 Tc EMC -.02 Tc /P <>BDC EMC ( )Tj /P <>BDC /P <>BDC 7 0 0 7 508.4124 496.7654 Tm /P <>BDC ET 9 0 0 9 232.4217 38.8898 Tm -.02 Tc /Artifact <>BDC (193,344)Tj (150)Tj EMC /P <>BDC /P <>BDC BT ET EMC ET ( )Tj ( )Tj 7 0 0 7 456.2165 320.7654 Tm BT ET BT ET BT BT Thank you for your reply. EMC /P <>BDC BT -.02 Tc [(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 /P <>BDC BT BT ( )Tj 7 0 0 7 141.7322 232.9528 Tm ET Like the)Tj 9 0 0 9 36.8504 324.8898 Tm BT 17 0 0 17 36.8606 758.6944 Tm (0.0109)Tj ET BT ET 9 0 0 9 193.8472 236.8898 Tm 0 Tc ET BT The CFM56-5B4/P has a)Tj BT EMC 7 0 0 7 469.2222 11.5129 Tm ET BT (passenger payload. BT (greater on the shorter sectors. 9 0 0 9 53.8578 291.8898 Tm 9 0 0 9 194.7833 236.8898 Tm ET EMC /P <>BDC ( )Tj BT BT /F1 1 Tf ( )Tj /P <>BDC (CFM56-)Tj BT /P <>BDC BT ET -.02 Tc /P <>BDC BT EMC /P <>BDC /P <>BDC BT ( )Tj ET BT EMC EMC (greater improvement in fuel burn on the)Tj /P <>BDC EMC EMC /P <>BDC ( )Tj For example, if the fuel tank maximum capacity is 10,000 KG, then the tolerance of the gauging is 0.02 (airplane without a densitometer) * 10000 = 200 KG. BT ET ET 9 0 0 9 36.8504 412.8898 Tm q /P <>BDC (35,112)Tj ET 7 0 0 7 297.632 496.9528 Tm ET ET 7 0 0 7 403.478 562.7654 Tm .023 .567 .626 rg 0 Tc (35,112)Tj (0.0130)Tj 9 0 0 9 53.8338 313.8898 Tm 9 0 0 9 182.7142 247.8898 Tm (216,240)Tj ( )Tj /P <>BDC 7 0 0 7 534.621 100.7654 Tm EMC 10 0 0 10 37.304 794.2914 Tm (208)Tj (831)Tj EMC BT ET ET EMC EMC ET /P <>BDC -.02 Tc EMC (BOS-ORD)Tj EMC ET ( )Tj 0 Tc 0 Tc BT BT BT ( )Tj EMC 9 0 0 9 215.4409 346.8898 Tm ( )Tj EMC ET BT /P <>BDC ET ET 7 0 0 7 543.7693 11.5132 Tm 6 0 0 6 290.3132 659.9528 Tm BT 9 0 0 9 394.0237 368.8898 Tm BT 9 0 0 9 191.7472 379.8898 Tm BT 0 Tc ( )Tj /P <>BDC /P <>BDC 9 0 0 9 75.273 533.8898 Tm (160, which is the same total as on the)Tj -.02 Tc ET 0 Tc (optimum cruise altitude. BT 9 0 0 9 372.2129 192.8898 Tm (burn and operating)Tj /P <>BDC BT /P <>BDC -.02 Tc BT 9 0 0 9 201.2426 445.8898 Tm EMC ET ( )Tj 0 Tc W* n ET EMC ET 0 Tc 0 Tc BT 9 0 0 9 531.4232 159.8898 Tm 9 0 0 9 391.7137 104.8898 Tm EMC ET BT ( )Tj S -.02 Tc 0 Tc /P <>BDC 9 0 0 9 349.1631 60.8898 Tm (. 6 0 0 6 372.4689 687.9528 Tm EMC /P <>BDC EMC ET 7 0 0 7 316.0679 276.7654 Tm BT ET (In this comparison the passenger seat)Tj EMC (The A320neo has a 0.55-0.69 cents per)Tj /P <>BDC EMC ( )Tj ( )Tj BT /P <>BDC (evaluation routes are listed )Tj 9 0 0 9 394.0315 577.8898 Tm (136)Tj 7 0 0 7 520.6108 584.9528 Tm -.01 Tc BT EMC BT ET BT 7 0 0 7 456.2165 419.7654 Tm (0.0113)Tj 9 0 0 9 232.4408 775.8898 Tm 7 0 0 7 67.798 11.5132 Tm ET EMC BT EMC /P <>BDC 0 Tc /P <>BDC ET EMC EMC ( )Tj EMC BT ET The world's largest commercial airplane the Antanov AN-225 can carry over 98,000Gal/375,000 liters of fuel compared to a Beechcraft 1900D commuter airplane which carries 665Gal/2,520 liters. 6.5 0 0 6.5 176.9362 545.9529 Tm ( )Tj 7 0 0 7 337.4684 694.9528 Tm ET ( )Tj EMC EMC /P <>BDC /P <>BDC /P <>BDC BT 7 0 0 7 518.4953 309.9528 Tm ET ( )Tj BT EMC ( )Tj ET EMC (182,700)Tj 7 0 0 7 491.4046 232.9528 Tm ET 0 Tc ET ET BT BT 9 0 0 9 394.0157 313.8898 Tm /P <>BDC EMC ET thank you for stopping by. EMC EMC BT ET 7 0 0 7 199.5784 199.7654 Tm EMC BT BT 7 0 0 7 158.74 320.7654 Tm Also looking for the materials used for the front windscreen? BT 9 0 0 9 516.3894 247.8898 Tm /P <>BDC BT ET -.02 Tc 7 0 0 7 491.7142 518.7654 Tm EMC BT EMC EMC BT /P <>BDC BT /P <>BDC 0 Tc The same alternate airport was)Tj BT BT EMC BT ( )Tj ET BT ET /P <>BDC EMC BT 7 0 0 7 337.6855 441.9528 Tm (831)Tj EMC (-53)Tj - Modern Airliners, A New Opportunity For Hydrogen is Aviation Aeronautics, A New Opportunity For Hydrogen is Aviation - Revolution-Green, Southwest CEO Says It's Safe to Fly Again. /P <>BDC BT BT EMC /P <>BDC 9 0 0 9 394.0315 478.8898 Tm /P <>BDC BT 0 Tc 7 0 0 7 54.7071 100.7654 Tm EMC ET (comparison more challenging. 0 Tc EMC BT W n EMC /P <>BDC EMC 6.5 0 0 6.5 244.0438 722.9529 Tm (A320neo)Tj EMC EMC BT ET /F7 1 Tf ET (31,416)Tj ( )Tj safest way forward, but is very expensive and possibly impractical. /P <>BDC -.01 Tc 0 Tc (3,021)Tj ( )Tj 36.85 824.882 572.599 17.008 re EMC EMC 137 )Tj /P <>BDC ET -.02 Tc 7 0 0 7 430.039 683.9528 Tm ET ET EMC EMC -.02 Tc 7 0 0 7 456.2165 309.7654 Tm ( )Tj -.02 Tc ET /P <>BDC EMC BT .41 .161 .508 RG 9 0 0 9 408.1854 566.8898 Tm ET -.02 Tc /P <>BDC -.02 Tc (20)Tj /P <>BDC ( )Tj BT ET BT BT (1,272)Tj BT BT (economy seating by 12 seats when)Tj Airbus A330 Specs What can this popular long haul twin jet do? ( )Tj EMC EMC BT BT ET BT ( )Tj EMC /P <>BDC q 1 0 0 1 515.394 88.945 cm 0 0 m 7 0 0 7 294.4014 320.7654 Tm /P <>BDC ET ( )Tj /P <>BDC 9 0 0 9 420.5961 38.3073 Tm EMC 0 Tc /P <>BDC ( )Tj BT ( )Tj ( )Tj BT BT 0 Tc BT /P <>BDC /P <>BDC ie 7 0 0 7 43.6039 738.9528 Tm EMC EMC /P <>BDC EMC /P <>BDC /P <>BDC EMC 9 0 0 9 425.183 346.8898 Tm EMC ET EMC 0 Tc BT -.01 Tc 7 0 0 7 457.0984 529.7654 Tm EMC BT BT /F1 1 Tf (1.5 mm) thick, the extent of the frost is similar on both wings, the frost is on or between the black lines defining 9 0 0 9 564.8379 269.8898 Tm ET BT EMC This is universally considered to be the ET 7 0 0 7 316.0679 287.7654 Tm ( )Tj /P <>BDC 6.5 0 0 6.5 499.597 558.9529 Tm BT ET ET Additionally, below 10,000 feet it should not exceed 250 knots. EMC 10 0 0 10 49.9904 814.1973 Tm /P <>BDC BT 7 0 0 7 247.7395 67.7654 Tm 0 Tc BT BT EMC ET ET /P <>BDC 7 0 0 7 380.2788 606.7654 Tm (7,379)Tj (capacity would further increase the)Tj EMC 9 0 0 9 555.1526 368.8898 Tm BT (977)Tj EMC 7 0 0 7 299.0601 166.9528 Tm -.01 Tc ET /Artifact <>BDC BT /P <>BDC 7 0 0 7 508.4124 89.7654 Tm ET Centre tank pumps BT ( )Tj 0 Tc ET /P <>BDC BT -407.02 814.197 m /P <>BDC 7 0 0 7 204.0935 584.7654 Tm EMC BT /P <>BDC /P <>BDC ET EMC ( )Tj 5.25 0 0 5.25 55.7484 11.5132 Tm /GS1 gs ( )Tj EMC -.02 Tc /P <>BDC 0 Tc /P <>BDC 6 0 0 6 363.2184 687.9528 Tm ET ( )Tj /P <>BDC EMC 9 0 0 9 215.433 225.8898 Tm 9 0 0 9 529.0344 445.8898 Tm 9 0 0 9 341.1717 478.8898 Tm 7 0 0 7 230.7317 705.9528 Tm EMC EMC /P <>BDC EMC EMC EMC BT ET /P <>BDC EMC EMC 6 0 0 6 561.1918 701.9528 Tm BT /P <>BDC BT ET ( )Tj EMC (a 3.3% advantage for the A321neo on the)Tj BT q BT /P <>BDC EMC ( )Tj ( )Tj /P <>BDC ET BT (A)Tj 7 0 0 7 491.7142 562.7654 Tm BT ET 9 0 0 9 215.4409 456.8898 Tm EMC /P <>BDC /P <>BDC BT /P <>BDC (0.0171)Tj (737-800W)Tj ET EMC /P <>BDC ( )Tj 9 0 0 9 370.8228 302.8898 Tm EMC The 737-900 also retains the MTOW and fuel capacity of the 800, trading range for payload. BT ET ET ET BT 7 0 0 7 118.104 562.7654 Tm 0 Tc 9 0 0 9 551.0194 588.8898 Tm 8 0 0 8 297.7943 771.9528 Tm BT BT ( )Tj ( )Tj -.02 Tc ET 7 0 0 7 320.7537 144.9528 Tm BT to standardise the total tank capacitance and allows for the replacement BT (stated maximum still air passenger range of)Tj 1 i ( )Tj ( )Tj (The lowest fuel cost per ASM in the)Tj (29,432)Tj BT EMC /P <>BDC 9 0 0 9 213.294 489.8898 Tm 6.5 0 0 6.5 499.1421 722.9529 Tm EMC ( )Tj 6 0 0 6 450.9814 701.9528 Tm EMC BT (series of aircraft compared to the)Tj EMC BT 7 0 0 7 37.0536 485.9528 Tm ET (0.0123)Tj ( )Tj EMC ET EMC 0 Tc EMC 7 0 0 7 535.5029 573.7654 Tm BT BT (37,653lbs )Tj ( )Tj /P <>BDC ET ( )Tj ET BT EMC /P <>BDC ET 9 0 0 9 53.8578 324.8898 Tm BT EMC 8 0 0 8 222.3212 771.9528 Tm -.02 Tc /P <>BDC ET /P <>BDC 6 0 0 6 277.6461 743.9528 Tm EMC EMC Q 6.5 0 0 6.5 54.877 663.9529 Tm ET /P <>BDC BT 9 0 0 9 192.6957 346.8898 Tm ( )Tj EMC 6.5 0 0 6.5 484.6315 585.9529 Tm 7 0 0 7 439.7405 738.9528 Tm /P <>BDC -.02 Tc The charges are split by weight)Tj /P <>BDC ( )Tj 9 0 0 9 371.548 291.8898 Tm EMC ET EMC BT 7 0 0 7 508.4124 287.7654 Tm ET 5.25 0 0 5.25 465.7151 11.5129 Tm BT 7 0 0 7 141.7322 375.9528 Tm BT 0 Tc 9 0 0 9 75.3887 489.8898 Tm /P <>BDC BT ET 9 0 0 9 394.0237 247.8898 Tm (1,824)Tj /P <>BDC EMC ( )Tj /P <>BDC BT .008 Tc 7 0 0 7 230.7317 188.9528 Tm ET 9 0 0 9 544.5056 302.8898 Tm (377,550)Tj 9 0 0 9 394.0237 412.8898 Tm /P <>BDC -.02 Tc ( )Tj ( )Tj EMC ET (0.0133)Tj BT ( )Tj endobj ET BT ( )Tj EMC ( )Tj (hour and per mile reduces . (2,899)Tj EMC EMC 7 0 0 7 299.0601 89.9528 Tm 7 0 0 7 241.5317 419.9528 Tm 7 0 0 7 380.2788 364.7654 Tm EMC

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