9 0 0 9 394.0157 357.8898 Tm ( )Tj /P <>BDC [(AIRL)8.1(INE & AIR)7.1(CRAF)-12.9(T)18.1( OPERA)56.9(T)-8.1(ION)-13.9(S)]TJ EMC ( )Tj ET BT /P <>BDC EMC ( )Tj (stage lengths or tracked distances of)Tj /P <>BDC BT EMC ET /P <>BDC /P <>BDC /P <>BDC /P <>BDC ET 9 0 0 9 186.8966 357.8898 Tm BT 0 Tc BT 7 0 0 7 403.478 683.7654 Tm ET /P <>BDC 9 0 0 9 526.6688 335.8898 Tm ET /P <>BDC ( )Tj 0 Tc 168 0 obj ET EMC BT EMC (increases to 5.7% in favour of the 737-)Tj ET BT /P <>BDC BT ET /P <>BDC ET 7 0 0 7 247.7395 166.7654 Tm 0 Tc ET EMC 9 0 0 9 394.0315 478.8898 Tm (tracked distance, ESAD, and the difference)Tj ( )Tj /P <>BDC EMC BT ( )Tj 9 0 0 9 36.8504 390.8898 Tm 7 0 0 7 118.104 661.7654 Tm BT EMC ET ( )Tj BT (380-396)Tj ET .151 .147 .15 rg /P <>BDC /P <>BDC /P <>BDC ET BT BT ET (13 seats fewer than the A321neo. /P <>BDC /P <>BDC 9 0 0 9 36.8504 434.8898 Tm ET BT /P <>BDC EMC 9 0 0 9 51.0236 379.8898 Tm (170)Tj 9 0 0 9 36.8504 280.8898 Tm BT ET ( )Tj EMC 0 Tc /P <>BDC /P <>BDC 7 0 0 7 158.74 694.7654 Tm ET /P <>BDC EMC EMC BT (fixed speed of LRC can be applied to all)Tj q 0 Tc /P <>BDC EMC BT EMC BT ET EMC 9 0 0 9 394.0315 434.8898 Tm 7 0 0 7 365.035 606.9528 Tm 7 0 0 7 456.7412 661.7654 Tm 6.5 0 0 6.5 317.7333 742.9529 Tm (150)Tj BT (737-9)Tj EMC ( )Tj 7 0 0 7 355.3163 320.7654 Tm (impacted by external factors such as)Tj BT 7 0 0 7 297.632 705.9528 Tm BT EMC ( )Tj 7 0 0 7 456.2165 397.7654 Tm 9 0 0 9 75.273 511.8898 Tm /P <>BDC Your email address will not be published. /P <>BDC ET endobj [(CFM L)17.1(E)-8.1(AP-1A26)]TJ BT ( )Tj BT 6.5 0 0 6.5 54.877 545.9529 Tm /P <>BDC /P <>BDC /P <>BDC 7 0 0 7 321.6356 386.9528 Tm EMC ET (A321ceo versus the 737-900ER\(W\), in the)Tj 7 0 0 7 118.104 408.7654 Tm 64 0 obj BT BT (1,824)Tj ( )Tj BT /P <>BDC EMC ET ET ET /P <>BDC BT -.02 Tc 7 0 0 7 427.7291 309.9528 Tm /P <>BDC BT 7 0 0 7 337.6855 276.9528 Tm /P <>BDC /P <>BDC ET EMC ET A weight reduction of 700 pounds (320 kg) on a 737-800 results in 0.5% reduction in fuel burn. ET /P <>BDC /P <>BDC BT BT ET BT BT ET BT /P <>BDC .41 .161 .508 RG 6 0 0 6 433.9826 659.9528 Tm /F1 1 Tf /P <>BDC BT BT The accuracy tolerance of the fuel flow transmitter is a function of the fuel flow. ET BT 6 0 0 6 331.4048 687.9528 Tm /P <>BDC 137 )Tj 7 0 0 7 343.2355 716.7654 Tm BT (737-9)Tj ET EMC (same passenger payload. /P <>BDC EMC /P <>BDC EMC BT -.02 Tc EMC 9 0 0 9 190.3733 192.8898 Tm 6 0 0 6 327.5828 701.9528 Tm /P <>BDC (1,272)Tj 7 0 0 7 278.2756 78.9528 Tm ET /P <>BDC ET ET (configurations for these aircraft types. ET ET ( )Tj EMC ( )Tj 6.5 0 0 6.5 448.257 650.9529 Tm 7 0 0 7 258.2805 67.7654 Tm BT -.02 Tc /P <>BDC 7 0 0 7 362.3891 144.9528 Tm ( )Tj /P <>BDC EMC /P <>BDC ( )Tj BT 7 0 0 7 379.3969 89.7654 Tm ( )Tj EMC -.02 Tc /P <>BDC /P <>BDC ET (2,437)Tj ET (190,800)Tj ET /P <>BDC (follow in their footsteps, having already)Tj /P <>BDC ( )Tj /P <>BDC (1,351)Tj EMC ( )Tj /P <>BDC /P <>BDC 0 Tc ( )Tj BT 9 0 0 9 232.438 456.8898 Tm /P <>BDC /P <>BDC /P <>BDC ET ( )Tj EMC ET /GS1 gs /P <>BDC (have won more than 5,600. 9 0 0 9 214.4188 478.8898 Tm ET EMC ET BT ET ( )Tj (375)Tj ET 9 0 0 9 554.3696 269.8898 Tm /P <>BDC ET /P <>BDC ET /P <>BDC EMC BT BT *PUUqUef\r+vl ( )Tj BT 9 0 0 9 383.3617 346.8898 Tm /P <>BDC ET (0.0134)Tj EMC (on the same sector is almost the same as)Tj ( )Tj ET BT EMC 7 0 0 7 294.4014 309.7654 Tm ( )Tj EMC EMC 7 0 0 7 230.7317 177.9528 Tm ET 6.5 0 0 6.5 426.4819 689.9529 Tm EMC (176)Tj 7 0 0 7 491.4046 320.9528 Tm EMC ET /P <>BDC BT ( )Tj .0161 Tc ET BT BT 9 0 0 9 232.4217 412.8898 Tm ET /P <>BDC EMC 7 0 0 7 141.7322 694.9528 Tm BT /P <>BDC BT EMC BT EMC /GS2 gs /P <>BDC BT /P <>BDC BT BT /P <>BDC BT BT EMC BT EMC /P <>BDC BT /P <>BDC /P <>BDC -.01 Tc (BOS-DEN)Tj EMC [(CFM L)17.1(E)-8.1(AP-1A26)]TJ 6.5 0 0 6.5 397.1339 689.9529 Tm ET EMC /P <>BDC 7 0 0 7 387.0932 199.9528 Tm BT BT ET 6 0 0 6 130.4965 771.9528 Tm (that a difference in seat capacity has a big)Tj /P <>BDC ET BT 9 0 0 9 536.5664 269.8898 Tm 7 0 0 7 444.737 397.7654 Tm 7 0 0 7 230.7317 331.9528 Tm BT BT /P <>BDC EMC 6 0 0 6 103.8196 757.9528 Tm BT /P <>BDC EMC /P <>BDC EMC 6.5 0 0 6.5 480.4 637.9529 Tm ET EMC ET ( )Tj 9 0 0 9 68.3339 555.8898 Tm EMC BT Each version in the 737 family fills a differ role. /P <>BDC BT EMC 7 0 0 7 519.3773 276.9528 Tm BT ( )Tj EMC 7 0 0 7 519.3773 221.9528 Tm EMC (310,080)Tj EMC /P <>BDC BT EMC /P <>BDC BT /P <>BDC EMC ET EMC 7 0 0 7 387.0159 496.9528 Tm 0 Tc EMC (the fuel burn and operating performance of)Tj (34,650)Tj 6 0 0 6 527.2669 729.9528 Tm 0 Tc <> /P <>BDC q ET BT EMC /OC /MC2287 BDC 9 0 0 9 346.8148 104.8898 Tm 0 Tc ET /P <>BDC /P <>BDC 7 0 0 7 54.7071 331.7654 Tm 6.5 0 0 6.5 500.4875 532.9529 Tm (182,299)Tj /P <>BDC EMC (A potential operator would need to)Tj BT BT 7 0 0 7 247.7395 408.7654 Tm (152)Tj ET 6.5 0 0 6.5 447.8411 663.9529 Tm EMC 7 0 0 7 125.6292 144.7654 Tm /P <>BDC BT 9 0 0 9 294.2183 346.8898 Tm BT /P <>BDC BT EMC recommended many years ago to the FAA that a fuel tank inerting system be made EMC [(R)13.9(OUT)10(E CHARA)16.1(CT)10(ERIS)8.1(T)-8.1(I)0(C)-17.1(S)0( F)8.1(OR ANAL)86.9(YSIS OF AIR)7.1(CRAF)-12.9(T)18.1( PERF)8.1(ORMANCE )]TJ ( )Tj ET /P <>BDC /P <>BDC EMC ET BT W* n BT EMC ET 6.5 0 0 6.5 549.8557 722.9529 Tm ( )Tj .151 .147 .15 rg EMC 6 0 0 6 427.5796 729.9528 Tm (483)Tj 9 0 0 9 53.8582 313.8898 Tm ET (977)Tj BT /P <>BDC ET [(M)-13.9(KE/84)]TJ EMC ET 8 0 0 8 43.6039 633.9528 Tm ( )Tj eight oxygen analyzers, to continuously monitor the ullage oxygen EMC BT (\(Toronto Pearson\) sector, to 2,730nm for)Tj ( )Tj BT 8 0 0 8 74.9636 717.9528 Tm BT ( )Tj ET EMC -.01 Tc EMC EMC EMC ( )Tj /P <>BDC /P <>BDC EMC 9 0 0 9 411.0234 709.8898 Tm ET /P <>BDC EMC ET 7 0 0 7 230.7317 210.9528 Tm /P <>BDC /P <>BDC BT BT ET /P <>BDC BT ET EMC BT BT BT EMC BT [(F)43(uel burn/)]TJ BT Do you have a reference please? BT BT /F6 1 Tf /P <>BDC ET /P <>BDC /P <>BDC (34,650lbs)Tj /P <>BDC ( )Tj (977)Tj 6.5 0 0 6.5 274.6269 689.9529 Tm ET BT /OC /MC1976 BDC BT 9 0 0 9 537.9817 445.8898 Tm BT 2002-19-52 which requires the crew to maintain certain minimum fuel 0 Tc /P <>BDC (31,416)Tj /P <>BDC .014984 841.89 609.45 -841.89 re ET 7 0 0 7 475.2383 639.9528 Tm ET 0 Tc EMC ET 6.5 0 0 6.5 346.7208 624.9529 Tm 7 0 0 7 241.5317 199.9528 Tm 7 0 0 7 124.1242 298.7654 Tm (150)Tj BT BT EMC ET BT W n (A320neo)Tj BT q 1 0 0 1 505.328 82.247 cm 0 0 m BT BT /P <>BDC /P <>BDC ET ( )Tj EMC /P <>BDC EMC 8 0 0 8 74.9636 591.9528 Tm }Qi_I0A"j ET BT /P <>BDC ET ET 0 Tc The NGS is an onboard inert gas system that uses an It provides code tables for aerodromes, air operators including the world's major airlines and for ICAO and IATA codes for aircraft. ET ET EMC BT ET -.02 Tc /P <>BDC 7 0 0 7 444.737 309.7654 Tm (in a more efficient engine. /P <>BDC (737-8)Tj BT BT BT 17 0 0 17 36.8606 775.1944 Tm EMC (As with the comparison of the)Tj 9 0 0 9 232.4217 467.8898 Tm 8 0 0 8 347.1567 771.9529 Tm 0 Tc (aircraft types: the A320ceo, A321ceo,)Tj ET 0 Tc ET BT BT /P <>BDC EMC -.02 Tc BT /P <>BDC /P <>BDC /P <>BDC /P <>BDC 7 0 0 7 355.3163 309.7654 Tm ET /P <>BDC /P <>BDC BT /P <>BDC ET ET 5.25 0 0 5.25 492.6848 11.5129 Tm BT BT EMC 7 0 0 7 298.1781 144.9528 Tm 0 Tc ET /P <>BDC 7 0 0 7 520.6108 705.9528 Tm [(CFM L)17.1(E)-8.1(AP-1B27)]TJ /P <>BDC BT BT BT /P <>BDC BT ( )Tj ET EMC (170)Tj BT EMC -.01 Tc BT ( )Tj EMC ( )Tj 7 0 0 7 247.7395 485.7654 Tm EMC BT 7 0 0 7 354.6933 639.7654 Tm BT 9 0 0 9 545.546 115.8898 Tm (974)Tj 0 Tc 9 0 0 9 189.8338 49.8898 Tm EMC /P <>BDC /P <>BDC ( )Tj 7 0 0 7 490.8321 441.7654 Tm EMC EMC ET 9 0 0 9 527.3853 709.8898 Tm It works by transferring fuel from the aux 7 0 0 7 354.6933 628.7654 Tm /P <>BDC ( )Tj EMC -.02 Tc ET 9 0 0 9 215.4409 423.8898 Tm ET ( )Tj /P <>BDC /P <>BDC BT 7 0 0 7 107.1165 562.9528 Tm ET ( )Tj 7 0 0 7 456.4753 716.7654 Tm 7 0 0 7 141.7322 738.9528 Tm 9 0 0 9 571.9847 181.8898 Tm 7 0 0 7 445.7203 11.5129 Tm EMC ET 9 0 0 9 381.3998 126.8898 Tm [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ ET /P <>BDC -.02 Tc (direction, so they will use even flight levels)Tj BT /P <>BDC ( )Tj BT BT EMC -.02 Tc /P <>BDC ET 7 0 0 7 537.7804 408.9528 Tm /P <>BDC EMC 9 0 0 9 394.0157 379.8898 Tm /P <>BDC Aircraft must carry enough fuel to taxi, climb, cruise, descent, and mutliple reserves. 9 0 0 9 232.4217 478.8898 Tm BT /P <>BDC ( )Tj -.02 Tc /P <>BDC /P <>BDC BT The Boeing 737-700 is together with the 737-600, 737-800 and 737-900 member of the 737-Next Generation-Family. 0 Tc /P <>BDC EMC EMC [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ EMC EMC In this case I believe TUI fly is the main customer. ET BT ET -.02 Tc BT /P <>BDC ET /P <>BDC (418)Tj /P <>BDC 7 0 0 7 473.8245 298.9528 Tm ET 9 0 0 9 188.0937 115.8898 Tm 7 0 0 7 199.5784 342.7654 Tm ( )Tj ( )Tj 6 0 0 6 434.211 701.9528 Tm ( )Tj ET ET [(BOS-Y)-50(YZ)]TJ ( )Tj EMC BT BT 7 0 0 7 247.7395 199.7654 Tm /P <>BDC BT /P <>BDC 0 Tc 848 0 obj /F6 1 Tf EMC /P <>BDC -.02 Tc 6 0 0 6 495.9463 771.9528 Tm ET (variants increases from 5.1:1 on the 737-)Tj BT BT (34,650)Tj EMC EMC )Tj /P <>BDC BT ET BT .12988 .27633 .58575 rg -.02 Tc ET (208)Tj ET 9 0 0 9 411.0097 214.8898 Tm (for the purposes of this performance)Tj ET -.02 Tc /P <>BDC ET (International Aero Engines V2527-A5)Tj 8 0 0 8 302.5117 717.9528 Tm BT (0.0113)Tj ( )Tj EMC BT ( )Tj ET EMC EMC (135,453)Tj 10 0 0 10 54.1596 794.2914 Tm /P <>BDC BT 6.5 0 0 6.5 244.3754 565.9529 Tm ( )Tj BT /P <>BDC BT ET BT ET BT ET BT ET ET 8 0 0 8 124.845 661.9528 Tm -.02 Tc 9 0 0 9 411.0097 357.8898 Tm EMC /P <>BDC EMC /P <>BDC the two components of the air are separated, the nitrogenenriched air (NEA) is ET BT EMC Q ET /P <>BDC ET -.02 Tc EMC 0 Tc EMC /Artifact <>BDC /P <>BDC 7 0 0 7 113.1366 617.9528 Tm )Tj ET -.02 Tc ET ET /P <>BDC how can i know the material of 737NGs nose landing gear lower drag strut?thank you. EMC /P <>BDC (136)Tj BT [(ar)-22.9(ticles like this, visit: )]TJ /OC /MC200 BDC ET EMC 0 Tc BT /P <>BDC ( )Tj W* n /P <>BDC BT (10)Tj ( )Tj 9 0 0 9 215.433 423.8898 Tm BT BT EMC 7 0 0 7 279.1575 89.9528 Tm 8 0 0 8 531.9995 82.8898 Tm 9 0 0 9 232.438 379.8898 Tm (further improve the fuel cost per ASM)Tj ( )Tj 9 0 0 9 362.0968 324.8898 Tm /P <>BDC /P <>BDC ET ET /P <>BDC 9 0 0 9 53.8582 698.8898 Tm ET ET ET ( )Tj BT 7 0 0 7 82.8504 309.9528 Tm 7 0 0 7 354.4763 672.7654 Tm ET 9 0 0 9 36.8583 456.8898 Tm (150)Tj BT BT /P <>BDC /P <>BDC ET (141,270)Tj BT (1A26-powered aircraft that is used in this)Tj EMC 7 0 0 7 43.6039 650.9528 Tm EMC 9 0 0 9 73.1083 511.8898 Tm ET /Figure <>BDC EMC ( )Tj ET (31,416lbs)Tj BT ET ET (services. BT ET (CFM56-7B26)Tj ET BT -.02 Tc BT EMC EMC ET (. EMC 9 0 0 9 544.0105 258.8898 Tm EMC /P <>BDC BT EMC /P <>BDC 7 0 0 7 258.2805 474.7654 Tm -.02 Tc BT 9 0 0 9 186.5751 423.8898 Tm BT /P <>BDC EMC /P <>BDC BT ( )Tj ET EMC ET /P <>BDC BT BT 8 0 0 8 43.6039 771.9528 Tm EMC ET ET 9 0 0 9 146.3 346.8898 Tm ET /P <>BDC BT 7 0 0 7 554.7883 496.7654 Tm 7 0 0 7 508.4124 320.7654 Tm (28,000lbs compared to 27,000lbs for the)Tj ( )Tj ET BT EMC ET /P <>BDC 8 0 0 8 258.7094 760.9528 Tm BT ( )Tj (up to 3,200nm when equipped with)Tj ET 0 Tc 7 0 0 7 314.6398 727.7654 Tm 7 0 0 7 241.5317 243.9528 Tm ET 9 0 0 9 215.4409 280.8898 Tm ET /P <>BDC BT (comparison focused on the fuel burn)Tj (market. (benefits from improved propulsive)Tj 7 0 0 7 490.5101 738.9528 Tm 9 0 0 9 408.1968 236.8898 Tm 8 0 0 8 302.5117 703.9528 Tm /P <>BDC (152)Tj BT EMC The typical range for this)Tj ( )Tj /P <>BDC ET -.02 Tc /P <>BDC 7 0 0 7 337.6855 529.9528 Tm /GS1 gs EMC 10 0 0 10 422.8 814.1973 Tm 7 0 0 7 508.2252 11.5129 Tm ( )Tj -.02 Tc 0 Tc BT ET ET (737-8 has a 0.8-3.0% higher trip fuel burn than)Tj ET 9 0 0 9 368.7299 346.8898 Tm BT EMC /P <>BDC ET ( )Tj 6.5 0 0 6.5 54.877 585.9529 Tm ET ET 0 Tc EMC 6 0 0 6 459.5796 729.9528 Tm /P <>BDC 9 0 0 9 232.4217 126.8898 Tm 9 0 0 9 53.8582 566.8898 Tm ET (31,416)Tj ET EMC EMC /P <>BDC EMC /P <>BDC /P <>BDC /P <>BDC ( )Tj BT 9 0 0 9 53.8338 247.8898 Tm EMC (209)Tj -.02 Tc 7 0 0 7 519.3773 166.9528 Tm /P <>BDC /P <>BDC ET [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ (this evaluation. ET BT BT BT ET ET 7 0 0 7 294.4014 672.7654 Tm 7 0 0 7 537.7804 397.9528 Tm 7 0 0 7 316.0679 364.7654 Tm ET EMC /P <>BDC 7 0 0 7 554.7883 397.7654 Tm ( )Tj ET ET (39,270)Tj 8 0 0 8 225.1837 661.9528 Tm (the aircraft types. EMC /P <>BDC /P <>BDC EMC /P <>BDC ( )Tj BT 7 0 0 7 82.8504 177.9528 Tm /P <>BDC ( )Tj (1B engine as the 737-8. BT ET EMC ( )Tj BT ET BT (0.0177)Tj 9 0 0 9 387.3578 258.8898 Tm 9 0 0 9 354.463 49.8898 Tm ( )Tj ( )Tj Boeing 737 History, the story behind this hugely successful City Jet. EMC ET -.02 Tc BT (orders, while the 737-800 and 737-900ER)Tj (900ER and 737-9, A320ceo and A320neo,)Tj (comparison of the fuel burn performance. ( )Tj EMC 9 0 0 9 53.8582 588.8898 Tm EMC /P <>BDC BT BT BT 7 0 0 7 294.4014 342.7654 Tm ET BT EMC BT /P <>BDC /P <>BDC BT EMC 0 Tc 0 Tc (this evaluation are all in the same weight)Tj -.02 Tc ( )Tj ( )Tj -.01 Tc (2,349)Tj 36.85 541.416 340.159 263.624 re (CFM56-)Tj ( )Tj 9 0 0 9 369.2608 38.8898 Tm EMC (on these flights. ET /P <>BDC /P <>BDC Q 6 0 0 6 61.517 701.9528 Tm BT ET 9 0 0 9 212.2888 93.8898 Tm 9 0 0 9 53.8578 93.8898 Tm /P <>BDC 9 0 0 9 394.0315 170.8898 Tm ET /P <>BDC 9 0 0 9 312.9828 38.8898 Tm ET EMC /P <>BDC ET BT ET EMC (operator. /P <>BDC ET 9 0 0 9 394.0315 786.8898 Tm (36,960)Tj 9 0 0 9 408.2047 489.8898 Tm 8 0 0 8 287.7892 771.7654 Tm EMC ET /P <>BDC BT EMC 0 Tc BT ( )Tj (1,272)Tj 9 0 0 9 195.69 181.8898 Tm (113,016)Tj BT /P <>BDC /P <>BDC EMC BT ( )Tj /P <>BDC sorry that is way out of our knowledge here. /P <>BDC EMC ET According to Boeing.com, the 737-600/-700/-800/-900ER models have a maximum fuel capacity of 6,875 gallons. EMC -.02 Tc Cheers Peter. I know the 787 is moving toward using more composite materiel instead of aluminum. 0 Tc ( )Tj ET (1.5 mm) thick, the extent of the frost is similar on both wings, the frost is on or between the black lines defining /P <>BDC BT /P <>BDC 7 0 0 7 77.36 11.5132 Tm ET EMC EMC 8 0 0 8 334.994 717.9528 Tm 0 Tc BT 0 Tc ET /P <>BDC ET EMC 19.841 0 l ET /P <>BDC /TT2 1 Tf -.02 Tc ET (compares to a tracked distance of)Tj /P <>BDC 7 0 0 7 187.0858 496.9528 Tm EMC EMC 0 Tc EMC BT EMC /P <>BDC 7 0 0 7 279.1575 287.9528 Tm BT ET BT BT ( )Tj /P <>BDC 7 0 0 7 158.74 716.7654 Tm ET /P <>BDC BT ET -.02 Tc EMC 0 Tw ET ET (these aircraft, two different payload)Tj 7 0 0 7 315.5217 617.7654 Tm BT BT EMC /P <>BDC EMC BT 8 0 0 8 95.6042 633.9528 Tm 0 J 0 j 15 w 10 M [] 0 d ET BT BT 0 Tc ET 0 Tc BT /P <>BDC ET .023 .567 .626 rg ( )Tj /P <>BDC BT 7 0 0 7 362.3891 342.9528 Tm 6 0 0 6 208.9129 729.9528 Tm 0 Tc BT 7 0 0 7 327.1097 584.9528 Tm The aircraft also features)Tj BT /P <>BDC EMC BT /P <>BDC (404)Tj 9 0 0 9 274.8953 93.8898 Tm ET ( )Tj ( )Tj EMC /P <>BDC BT 9 0 0 9 388.8047 390.8898 Tm EMC 9 0 0 9 389.0497 445.8898 Tm ET 7 0 0 7 125.6292 287.7654 Tm 9 0 0 9 53.8578 390.8898 Tm EMC EMC EMC ET EMC (. BT BT ET ET ET 7 0 0 7 327.1097 573.9528 Tm ET EMC EMC /P <>BDC .0161 Tc /P <>BDC 202.559 814.197 m 7 0 0 7 315.1859 100.7654 Tm 9 0 0 9 213.8067 159.8898 Tm (35,112)Tj EMC EMC BT 9 0 0 9 36.8504 445.8898 Tm EMC ET ET /P <>BDC BT BT [(CFM L)17.1(E)-8.1(AP-1B27)]TJ 8 0 0 8 187.3427 633.9528 Tm /P <>BDC (1,202)Tj (170)Tj EMC /P <>BDC (payload on any sector in this evaluation. ET next aircraft W n 9 0 0 9 408.1854 511.8898 Tm ( )Tj ET .534 .14 .504 RG BT BT BT EMC /P <>BDC ET 9 0 0 9 376.579 434.8898 Tm /P <>BDC ET BT BT 9 0 0 9 544.921 225.8898 Tm EMC ET ET 0 Tc 7 0 0 7 299.0601 331.9528 Tm BT BT EMC ET (163)Tj EMC (160)Tj ( )Tj 7 0 0 7 99.8582 199.7654 Tm BT /P <>BDC In this)Tj BT ET /P <>BDC /P <>BDC BT EMC ( )Tj (the A321neo offers a better fuel cost per)Tj [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ 9 0 0 9 528.0345 511.8898 Tm -.02 Tc 0 Tc EMC /P <>BDC ( )Tj S 7 0 0 7 316.0679 265.7654 Tm -.01 Tc BT EMC -.02 Tc ET ( )Tj [(F)-21(LL/47)]TJ BT /P <>BDC /P <>BDC BT ET 7 0 0 7 241.5317 485.9528 Tm (heavier than the A320ceo. EMC 0 Tc /P <>BDC EMC EMC ( )Tj ( )Tj ET (160)Tj BT 7 0 0 7 554.7883 210.7654 Tm 7 0 0 7 82.8504 408.9528 Tm ( )Tj (. BT /P <>BDC BT (destination airport are listed )Tj EMC BT BT EMC BT 0 Tc /P <>BDC 8 0 0 8 439.2348 771.9528 Tm ET (158)Tj 13 0 0 13 162.9571 181.8898 Tm BT 10 0 0 10 278.2126 794.2914 Tm BT /P <>BDC BT ( )Tj (seat count of 179. ( )Tj EMC BT 5.25 0 0 5.25 515.3989 11.5129 Tm /P <>BDC BT (CFM56-7B27B3)Tj ( )Tj ET /P <>BDC ET ET /P <>BDC ET 9 0 0 9 433.2572 104.8898 Tm 7 0 0 7 114.6416 298.9528 Tm EMC ET (CFM56-5B3/P)Tj (0.0124)Tj ET 9 0 0 9 215.4313 170.8898 Tm (124,800)Tj 7 0 0 7 82.8504 353.9528 Tm BT [(A3)24.9(20ceo v)12.9(ersus A3)24.9(20neo )]TJ 0 Tc BT BT 7 0 0 7 387.0932 210.9528 Tm (24)Tj EMC EMC [(A3)24.9(21neo)]TJ EMC BT EMC BT EMC /P <>BDC EMC 7 0 0 7 124.1242 595.7654 Tm ET BT 7 0 0 7 247.7395 67.7654 Tm BT ET 0 Tc BT /P <>BDC 0 Tc 0 Tc ET 9 0 0 9 36.8504 104.8898 Tm /OC /MC202 BDC (2,500)Tj 7 0 0 7 294.4014 595.7654 Tm BT BT 7 0 0 7 321.6356 298.9528 Tm EMC (282)Tj 9 0 0 9 246.6113 71.8898 Tm (maximum fuel capacity, the A320neo)Tj -.02 Tc /P <>BDC 6.5 0 0 6.5 346.5844 735.9529 Tm BT (3,069)Tj /P <>BDC BT BT ET 0 Tc ET -.02 Tc ( )Tj BT 8 0 0 8 258.2687 771.7654 Tm /Artifact <>BDC 0 Tc /P <>BDC (150)Tj BT EMC /P <>BDC ET EMC ET EMC BT 0 Tc /P <>BDC ET ET BT BT BT 6.5 0 0 6.5 488.8955 532.9529 Tm 7 0 0 7 130.1443 419.7654 Tm (2,154)Tj ET 6.5 0 0 6.5 438.3899 611.9529 Tm ET EMC (load factor, the A321neo carries a heavier)Tj EMC BT 8 0 0 8 43.6039 591.9528 Tm EMC The BBJ is based on the 737-700 airliner and the BBJ2 on the 737-800. 8 0 0 8 124.845 619.9528 Tm EMC BT 6 0 0 6 320.3167 757.9528 Tm 0 Tc /P <>BDC 7 0 0 7 387.0932 78.9528 Tm ET /P <>BDC ET EMC EMC ET 0 Tc 7 0 0 7 141.7322 133.9528 Tm ET -.02 Tc /P <>BDC /P <>BDC ( )Tj ( )Tj BT 9 0 0 9 360.0909 115.8898 Tm EMC EMC [(SS)-9.1(U)8(E)]TJ /P <>BDC BT 9 0 0 9 545.4755 654.8898 Tm 5 0 obj EMC ( )Tj 9 0 0 9 112.3045 346.8898 Tm /F6 1 Tf 6 0 0 6 520.876 743.9528 Tm /P <>BDC ( )Tj (149,300)Tj (minutes between aircraft types or 3.7% on)Tj /P <>BDC 7 0 0 7 363.2711 408.9528 Tm /P <>BDC ( )Tj EMC EMC 7 0 0 7 230.7317 364.9528 Tm EMC (The fuel cost per ASM improves with)Tj /P <>BDC /P <>BDC 9 0 0 9 394.0123 599.8898 Tm /P <>BDC EMC ( )Tj /P <>BDC 7 0 0 7 299.0601 188.9528 Tm /P <>BDC 7 0 0 7 294.4014 188.7654 Tm -.02 Tc BT ET /P <>BDC (on the A320ceo to 11.0:1 on the A320neo. 7 0 0 7 490.7815 67.9528 Tm 0 Tc 9 0 0 9 420.5961 38.3073 Tm ET 6.5 0 0 6.5 244.2585 598.9529 Tm BT /P <>BDC EMC ET BT (A320ceo)Tj EMC ET )Tj 9 0 0 9 537.6038 170.8898 Tm /P <>BDC ET ET ET BT BT BT /P <>BDC /P <>BDC ET ET Jump to Specification Table Boeing 737 Original and Boeing 737 Classic. ET /P <>BDC BT BT /P <>BDC EMC 6.5 0 0 6.5 375.6529 702.9529 Tm (98,500)Tj EMC 9 0 0 9 394.0157 566.8898 Tm ET 7 0 0 7 326.2278 474.9528 Tm EMC ET BT EMC BT (0.0141)Tj 7 0 0 7 343.2355 683.7654 Tm EMC EMC BT /P <>BDC ( )Tj ET EMC BT 9 0 0 9 191.7472 379.8898 Tm (when using a cost index. 7 0 0 7 474.3564 595.9528 Tm /P <>BDC BT 7 0 0 7 491.7142 287.7654 Tm ( )Tj ET EMC /P <>BDC 9 0 0 9 210.9209 104.8898 Tm EMC /P <>BDC ET /P <>BDC ET ( )Tj (31,416)Tj ( )Tj ET ET 10 0 0 10 425.05 814.1973 Tm BT 6 0 0 6 195.6824 659.9528 Tm ET 0 Tc BT ET ( )Tj -.02 Tc ET ET EMC 8 0 0 8 153.6923 591.9528 Tm BT 7 0 0 7 507.7893 639.7654 Tm BT .014984 841.89 609.45 -841.89 re 6.5 0 0 6.5 330.4406 565.9529 Tm 8 0 0 8 354.3239 771.7654 Tm 529.065 38.307 m (11,593)Tj .151 .147 .15 rg 0 Tc /P <>BDC ET /P <>BDC /P <>BDC 0 Tw /P <>BDC BT /P <>BDC 0 Tc (36,960)Tj ()Tj 6 0 0 6 144.9509 687.9528 Tm ET 0 Tc ET EMC 7 0 0 7 338.3085 342.9528 Tm BT .008 Tc ( )Tj /P <>BDC ( )Tj ET BT ET EMC EMC ET /P <>BDC 9 0 0 9 232.4217 225.8898 Tm /GS1 gs 7 0 0 7 279.1575 331.9528 Tm /P <>BDC /P <>BDC [(UG)-17.1(U)-8(S)8.1(T)]TJ ET -.02 Tc /P <>BDC -.02 Tc .1334 -5.7288 l /P <>BDC )Tj EMC BT /P <>BDC EMC 7 0 0 7 258.2805 265.7654 Tm BT 7 0 0 7 37.6993 111.9528 Tm -.02 Tc /P <>BDC ET 9 0 0 9 53.8582 49.8898 Tm BT /F1 1 Tf -.02 Tc (the relative fuel costs between the aircraft)Tj ( )Tj BT EMC BT ET )Tj /P <>BDC ET BT BT ET /P <>BDC EMC -.02 Tc BT ET /P <>BDC ( )Tj EMC (the aircraft in this study are shown )Tj /P <>BDC EMC 17 0 0 17 560.3929 742.1944 Tm /F4 1 Tf 9 0 0 9 534.2559 302.8898 Tm (The A320 analysed here is powered by)Tj ET ( )Tj (charges combined with the time-related)Tj 0 Tw ET 9 0 0 9 372.2987 181.8898 Tm ( )Tj (248,064)Tj /P <>BDC /P <>BDC 9 0 0 9 363.9759 115.8898 Tm EMC EMC -.02 Tc (seat capacity of 179. 858 0 obj 6 0 obj /P <>BDC -.02 Tc ( )Tj (All the flights were in a westerly)Tj ( )Tj ET EMC ET EMC /P <>BDC ET ET EMC /P <>BDC ( )Tj /P <>BDC 9 0 0 9 36.8504 60.8898 Tm ( )Tj (A321neo)Tj /P <>BDC EMC 7 0 0 7 258.2805 705.7654 Tm /P <>BDC ET BT BT BT The Boeing 737-800 variant has as mentioned 27300 pound-force delivered by two turbo fans. BT ET 0 Tc ET /P <>BDC /P <>BDC EMC 9 0 0 9 394.0237 181.8898 Tm 6.5 0 0 6.5 64.6596 611.9529 Tm BT 6 0 0 6 309.5222 701.9528 Tm EMC /P <>BDC /P <>BDC /P <>BDC EMC EMC (generated per route. /P <>BDC EMC (112)Tj ( )Tj ( A)Tj 7 0 0 7 539.8962 639.9528 Tm EMC 0 Tc EMC EMC /P <>BDC ET (208-217)Tj /P <>BDC BT 7 0 0 7 445.7203 11.5129 Tm 9 0 0 9 214.7728 247.8898 Tm ET EMC /P <>BDC EMC EMC /P <>BDC ( N)Tj -.02 Tc /P <>BDC ( )Tj ET EMC BT EMC /P <>BDC EMC W n /GS2 gs 9 0 0 9 53.8338 181.8898 Tm ( )Tj ET EMC .0161 Tc /P <>BDC BT ( 2021)Tj 7 0 0 7 380.2788 474.7654 Tm BT 7 0 0 7 204.0935 430.7654 Tm ET /P <>BDC BT Download the Final 0 Tc ( )Tj /P <>BDC (1,547)Tj BT ET /P <>BDC EMC 8 0 0 8 394.0157 797.8898 Tm ET BT EMC ( )Tj (409,650)Tj 7 0 0 7 445.619 518.7654 Tm .023 .567 .626 rg ( )Tj 7 0 0 7 444.737 232.7654 Tm EMC 9 0 0 9 552.5356 445.8898 Tm 9 0 0 9 394.0123 247.8898 Tm 7 0 0 7 158.74 89.7654 Tm ET ET ET BT ET (177)Tj 9 0 0 9 394.0237 247.8898 Tm /P <>BDC /P <>BDC 5.25 0 0 5.25 55.7484 11.5132 Tm BT -.02 Tc BT /P <>BDC 0 Tc (976)Tj /P <>BDC ET ( )Tj EMC ( )Tj ET EMC /P <>BDC EMC 9 0 0 9 232.438 412.8898 Tm ET (\(neo\) families, and the 737NG family. BT 7 0 0 7 535.5029 221.7654 Tm 9 0 0 9 555.1594 379.8898 Tm EMC 9 0 0 9 68.3339 445.8898 Tm BT ( )Tj BT Q EMC (difference between the aircraft types)Tj /P <>BDC EMC 7 0 0 7 521.4928 727.9528 Tm BT EMC -.02 Tc 6 0 0 6 255.8802 771.9528 Tm BT -.02 Tc EMC -.005 Tc EMC EMC 0 Tc EMC BT 7 0 0 7 99.8582 518.7654 Tm ET ET 7 0 0 7 131.6494 265.7654 Tm EMC 0 Tc EMC EMC ( )Tj /P <>BDC ( )Tj tank. ET ET /P <>BDC 0 Tc (977)Tj ET 9 0 0 9 425.183 544.8898 Tm 7 0 0 7 490.8321 419.7654 Tm /P <>BDC /P <>BDC 6 0 0 6 396.9076 729.9528 Tm 9 0 0 9 215.4313 148.8898 Tm 0 Tc ET EMC BT EMC EMC .0161 Tc BT /P <>BDC BT BT /P <>BDC BT /P <>BDC ( )Tj 19.843 0 l ( )Tj ET BT /P <>BDC 0 Tc ( )Tj /OC /MC3451 BDC ET ( )Tj BT BT ( )Tj 7 0 0 7 54.7071 683.7654 Tm /P <>BDC ET (1,622)Tj 378 0 0 271.8 -.30716 30.902 cm BT BT BT /P <>BDC -.02 Tc BT EMC -407.02 814.197 m (- USG)Tj 7 0 0 7 199.5784 144.7654 Tm 0 Tc (1,824)Tj ET BT /P <>BDC BT ( )Tj /P <>BDC /P <>BDC ET EMC /OC /MC1183 BDC EMC (294)Tj /P <>BDC 0 Tc /P <>BDC ET BT 7 0 0 7 54.7071 287.7654 Tm BT ET ( )Tj ET BT ET ( )Tj EMC ET /P <>BDC EMC /P <>BDC EMC 6.5 0 0 6.5 397.0428 532.9529 Tm EMC /P <>BDC 7 0 0 7 279.1575 441.9528 Tm /GS2 gs 7 0 0 7 536.3849 639.7654 Tm ( )Tj 9 0 0 9 379.7078 588.8898 Tm (6,820)Tj Hello, do you know the meaning of the 737-8K5 designation and its background? Q BT ( )Tj /P <>BDC /P <>BDC ET 7 0 0 7 141.7322 78.9528 Tm )Tj ET ET (sectors, particularly the shorter ones,)Tj /P <>BDC ET /P <>BDC EMC /P <>BDC /P <>BDC EMC BT ET -.02 Tc /P <>BDC ( )Tj 7 0 0 7 539.8962 529.9528 Tm /P <>BDC EMC EMC BT 9 0 0 9 232.438 49.8898 Tm EMC /P <>BDC 0 Tc EMC EMC 8 0 0 8 38.4438 675.9528 Tm 0 Tc ET /P <>BDC /P <>BDC 0 Tc BT ET EMC /P <>BDC EMC /P <>BDC (192)Tj ET (405)Tj ( )Tj BT EMC EMC 7 0 0 7 82.2047 727.9528 Tm (direction, with an initial heading ranging)Tj EMC 9 0 0 9 411.0181 236.8898 Tm ET BT /P <>BDC /P <>BDC /P <>BDC EMC EMC EMC /P <>BDC /P <>BDC /P <>BDC EMC /P <>BDC ET [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ ( )Tj 9 0 0 9 421.0664 401.8898 Tm /P <>BDC 0 Tc 9 0 0 9 51.0236 159.8898 Tm (163)Tj (35,112)Tj ( )Tj ET (1,060)Tj -.02 Tc 0 Tc (1,059)Tj ( )Tj (the IAE V2533-A5 engine, rated at)Tj /P <>BDC 0 Tc EMC 6 0 0 6 277.9531 771.9528 Tm EMC BT BT oxygen in the air. /P <>BDC ET 6 0 0 6 107.8523 659.9528 Tm ( )Tj 7 0 0 7 53.8582 11.5132 Tm BT ET ET EMC EMC 9 0 0 9 547.2866 390.8898 Tm BT EMC /P <>BDC /P <>BDC BT (170)Tj BT -.02 Tc EMC /P <>BDC EMC aux (AA) and fwd aux (FA) respectively. BT ET 7 0 0 7 537.7804 67.9528 Tm ET /P <>BDC 7 0 0 7 99.8582 386.7654 Tm /P <>BDC ET 7 0 0 7 60.6117 540.7654 Tm ET -.02 Tc -.02 Tc BT ( )Tj (1,824)Tj EMC 6.5 0 0 6.5 191.63 624.9529 Tm BT ET /P <>BDC EMC BT BT /P <>BDC /P <>BDC ET ET -.02 Tc 9 0 0 9 215.4313 247.8898 Tm ET 7 0 0 7 473.8245 243.9528 Tm 8 0 0 8 339.6345 760.7654 Tm BT (A320neos 7,000lbs higher MTOW. BT 9 0 0 9 354.313 236.8898 Tm EMC -.02 Tc EMC ET 7 0 0 7 507.7893 67.7654 Tm BT ET BT /P <>BDC ET (CFM56-5B4/P)Tj ET ( )Tj -.02 Tc /P <>BDC 7 0 0 7 321.6356 287.9528 Tm EMC BT 7 0 0 7 380.2788 287.7654 Tm ET BT BT /P <>BDC /P <>BDC 6.5 0 0 6.5 429.8944 598.9529 Tm EMC W n BT EMC /P <>BDC ET ET ET 9 0 0 9 534.7515 599.8898 Tm /P <>BDC must be determined by using the dripsticks (floatsticks 9 0 0 9 68.3339 533.8898 Tm ET /P <>BDC ET ET (29,432)Tj BT ET /P <>BDC ( )Tj BT 7 0 0 7 54.7071 111.7654 Tm ET ( )Tj EMC /P <>BDC BT EMC 7 0 0 7 473.8245 111.9528 Tm BT EMC 0 Tc 9 0 0 9 408.2047 313.8898 Tm /P <>BDC 7 0 0 7 444.737 386.7654 Tm EMC ET (A320neo)Tj 7 0 0 7 539.8962 606.9528 Tm Greetings. Thanks. BT ( )Tj ET 9 0 0 9 203.511 621.8898 Tm 0 Tc ET EMC 9 0 0 9 394.0315 335.8898 Tm EMC /P <>BDC 9 0 0 9 361.1316 214.8898 Tm BT ( )Tj EMC 9 0 0 9 555.1526 368.8898 Tm 8 0 0 8 225.1837 619.9528 Tm (0.0141)Tj ET /P <>BDC (remain competitive aircraft. EMC /P <>BDC ET EMC ET /P <>BDC ET EMC 10 0 0 10 425.05 814.1973 Tm ET /P <>BDC /P <>BDC BT ET 7 0 0 7 343.2355 694.7654 Tm /P <>BDC 7 0 0 7 230.7317 540.9528 Tm BT EMC 6 0 0 6 115.1719 701.9528 Tm to standardise the total tank capacitance and allows for the replacement EMC EMC BT EMC 9 0 0 9 170.752 368.8898 Tm EMC EMC ( )Tj ET EMC /P <>BDC -.02 Tc ET 9 0 0 9 36.8504 126.8898 Tm )Tj 0 Tc .41 .161 .508 rg 7 0 0 7 54.7071 320.7654 Tm 6 0 0 6 174.3402 701.9528 Tm ET (bypass ratio of 5.7:1, and is rated at)Tj BT 7 0 0 7 446.5009 672.7654 Tm ( )Tj (l)Tj 0 Tc [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ ET EMC ET ( )Tj (same maximum fuel capacity, had no)Tj /P <>BDC 6 0 0 6 239.8235 743.9528 Tm /P <>BDC ET (passengers on BOS-LAX, whereas the)Tj EMC ( 2021)Tj ( )Tj BT BT EMC ( )Tj /P <>BDC EMC 13 0 0 13 36.8583 390.8898 Tm 9 0 0 9 392.5128 236.8898 Tm EMC 7 0 0 7 535.5029 716.7654 Tm EMC /P <>BDC (manufacturers support these aircraft types)Tj ET ( )Tj BT /P <>BDC (405)Tj ( )Tj (152)Tj EMC /P <>BDC -.02 Tc BT 8 0 0 8 43.6039 661.9528 Tm 7 0 0 7 439.2087 111.9528 Tm /P <>BDC -.02 Tc BT 9 0 0 9 411.0181 225.8898 Tm EMC BT EMC BT ET BT ET BT -.02 Tc /F1 1 Tf ET /P <>BDC )Tj (1,668)Tj /P <>BDC /P <>BDC ET EMC (of 170 passengers, the A321neo burns an)Tj BT -.01 Tc (\(see table, page 19\))Tj EMC /P <>BDC BT (from Boston \(BOS\) Logan International)Tj ET (208)Tj -.02 Tc /P <>BDC BT ET (difference to an average of 2.1% over the)Tj EMC /P <>BDC /P <>BDC /P <>BDC ET (manufacturers, with Airbus reducing the)Tj 9 0 0 9 366.7762 390.8898 Tm 9 0 0 9 385.653 71.8898 Tm 9 0 0 9 394.0315 60.8898 Tm BT /P <>BDC ( )Tj ET 0 841.89 609.449 -841.89 re ET EMC EMC /GS2 gs BT EMC /P <>BDC EMC 262 0 obj /P <>BDC EMC 0 Tc /P <>BDC 7 0 0 7 491.4046 111.9528 Tm (number for the neo family. -2.5295 -5.0573 -2.1058 -5.3146 -1.5527 -5.3151 c )Tj EMC ET ET EMC 6.5 0 0 6.5 557.8578 742.9529 Tm /P <>BDC EMC (flight relate to fuel burn, overflight and)Tj ( )Tj BT ET 0 Tc The pumps should be switched off and considered inop until they can be /P <>BDC 9 0 0 9 394.0157 621.8898 Tm (176)Tj 7 0 0 7 387.0159 727.9528 Tm /P <>BDC EMC ( )Tj EMC BT EMC ET /P <>BDC 7 0 0 7 141.7322 188.9528 Tm BT ET ( )Tj 7 0 0 7 279.1575 639.9528 Tm ET BT BT /F1 1 Tf (2,042)Tj 0 Tc ET /P <>BDC /P <>BDC EMC q BT /P <>BDC /P <>BDC ET ( )Tj BT /P <>BDC 9 0 0 9 551.8838 324.8898 Tm
737 800 fuel capacity pounds
13
Mar