( )Tj 9 0 0 9 391.278 313.8898 Tm ( )Tj BT /P <>BDC /P <>BDC /P <>BDC Airbus A330 History How did one of the worlds most popular twin jets evolve. EMC ( )Tj 7 0 0 7 439.7405 584.9528 Tm EMC BT ( )Tj /P <>BDC EMC -.02 Tc 0 Tc 9 0 0 9 555.1324 148.8898 Tm 0 Tc BT BT BT EMC BT 8 0 0 8 225.1837 577.9528 Tm EMC 7 0 0 7 141.7322 177.9528 Tm This makes it more challenging to)Tj EMC ( )Tj ET EMC In this case I believe TUI fly is the main customer. ( )Tj BT /P <>BDC [(CFM L)17.1(E)-8.1(AP-1B27)]TJ EMC (evaluation it has been assumed that the)Tj (136)Tj ET ET /P <>BDC /F6 1 Tf /P <>BDC /P <>BDC EMC EMC EMC -.02 Tc EMC EMC EMC ( )Tj 9 0 0 9 246.6113 247.8898 Tm -.02 Tc EMC EMC following conditions: Takeoff with CSFF on the upper wing surfaces is ET lights were FILTER ICING on the 1/200. 7 0 0 7 439.7405 507.9528 Tm EFVU(eufv7GWgw8HXhx)9IYiy*:JZjz m !1AQa"q2#BRbr3$4CS%cs5DT /P <>BDC EMC ET /P <>BDC ET EMC EMC (128-137)Tj The PPS flight)Tj ET /P <>BDC /P <>BDC ET sectors to ensure an even fuel balance. EMC (39,732)Tj BT 0 Tc EMC (170)Tj ET ET ET /P <>BDC EMC ET BT BT (market. EMC EMC /P <>BDC ET EMC 0 Tc 6.5 0 0 6.5 549.8557 624.9529 Tm BT ( )Tj ET 7 0 0 7 82.8504 188.9528 Tm BT /P <>BDC 0 Tc In contrast, the 737-8s performance)Tj ET (56,901)Tj /P <>BDC (105,000lbs. EMC 7 0 0 7 326.2278 694.9528 Tm EMC 9 0 0 9 549.8481 632.8898 Tm ET EMC /P <>BDC 7 0 0 7 59.2108 11.5129 Tm 137 )Tj 7 0 0 7 241.2727 276.9528 Tm /P <>BDC EMC BT ( )Tj BT BT (CFM56-5B4/P)Tj 6.5 0 0 6.5 64.6596 565.9529 Tm /P <>BDC 7 0 0 7 554.7883 188.7654 Tm EMC /P <>BDC /P <>BDC 7 0 0 7 54.7071 67.7654 Tm EMC EMC q 7 0 0 7 37.6993 375.9528 Tm 6.5 0 0 6.5 244.3364 735.9529 Tm ( )Tj BT ET 13 0 0 13 36.8504 500.8898 Tm BT 9 0 0 9 232.438 335.8898 Tm 9 0 0 9 232.4217 346.8898 Tm ET /P <>BDC (In the same trend as on the A320)Tj ET /P <>BDC 7 0 0 7 380.2788 298.7654 Tm EMC ( )Tj ET /P <>BDC EMC EMC /P <>BDC ET The flight)Tj 7 0 0 7 54.7071 375.7654 Tm BT BT (150)Tj EMC (A320ceo:)Tj /P <>BDC /P <>BDC ET (improvement of 0.58 cents per ASM over)Tj EMC 9 0 0 9 425.183 346.8898 Tm /P <>BDC BT ( )Tj ( )Tj Cruise Speed: 530 mph Propulsion: Two General Electric CFM56-7B24 High Bypass Ratio turbofan engines, rated at 24,200 pounds thrust each. BT EMC 7 0 0 7 535.5029 320.7654 Tm q 7 0 0 7 338.5674 463.9528 Tm BT 7 0 0 7 241.5317 606.9528 Tm EMC ET ( )Tj ET ( )Tj EMC BT /P <>BDC 7 0 0 7 439.2087 67.9528 Tm ET /P <>BDC ET 7 0 0 7 492.5963 584.7654 Tm BT EMC EMC EMC /P <>BDC This study uses a)Tj (A)Tj 0 Tc /P <>BDC BT EMC BT EMC EMC /P <>BDC /P <>BDC warm conditions! [(contempor)10(ary narr)10(o)12(wbodies av)21(ailable on the)]TJ ET ET /P <>BDC BT BT )Tj 9 0 0 9 394.0237 335.8898 Tm /P <>BDC ( )Tj /F1 1 Tf /P <>BDC EMC EMC thank you for stopping by and we appreciate you checking us out on the details. ET (376)Tj -.02 Tc ET /P <>BDC 7 0 0 7 521.4089 11.5132 Tm BT /P <>BDC /P <>BDC /P <>BDC (34,650)Tj ( )Tj /P <>BDC 7 0 0 7 179.5605 716.9528 Tm (141,270)Tj <>stream EMC ET BT BT BT /P <>BDC ET BT ( )Tj -.02 Tc ET /P <>BDC EMC BT BT ET concentration at eight different locations. 9 0 0 9 394.0315 588.8898 Tm ET (CFM56-7B26)Tj ET BT EMC BT 7 0 0 7 54.7071 727.7654 Tm BT /P <>BDC ET ET 9 0 0 9 566.5209 379.8898 Tm EMC BT /F1 1 Tf 7 0 0 7 354.9521 100.7654 Tm /P <>BDC 7 0 0 7 321.4957 430.9528 Tm ET BT BT ET 9 0 0 9 36.8504 302.8898 Tm ( )Tj BT 0 Tc .014984 841.89 609.45 -841.89 re EMC /P <>BDC ( )Tj ET /P <>BDC EMC EMC EMC (pages 23 & 24\))Tj /GS1 gs EMC EMC ET ( )Tj BT 8 0 0 8 439.2348 771.9528 Tm ET EMC EMC 9 0 0 9 203.484 192.8898 Tm (based on the cost index set is different, it)Tj BT BT BT EMC (977)Tj EMC 0 Tc BT EMC (150)Tj 9 0 0 9 147.641 236.8898 Tm BT [(UG)-17.1(U)-8(S)8.1(T)]TJ /P <>BDC EMC EMC EMC ET EMC 7 0 0 7 71.6694 738.9528 Tm (91,300)Tj EMC EMC ET -.02 Tc 9 0 0 9 394.0157 181.8898 Tm BT Digital Fuel Quantity Indicator Error Codes, Missing or disconnected tank 6 0 0 6 316.5908 771.9528 Tm ET ET BT BT EMC BT -.01 Tc ET 6 0 0 6 107.8523 659.9528 Tm BT 9 0 0 9 36.8504 225.8898 Tm EMC (170)Tj EMC ET BT ET /P <>BDC ( )Tj EMC /P <>BDC The NG has 6 dripsticks in each wing tank and 4 in the centre ( )Tj /P <>BDC /P <>BDC ET ET ( )Tj ( )Tj 7 0 0 7 141.7322 661.9528 Tm 6 0 0 6 246.6462 743.9528 Tm BT EMC /P <>BDC BT EMC /P <>BDC EMC 7 0 0 7 141.7322 243.9528 Tm 5.25 0 0 5.25 73.853 11.5132 Tm ET EMC ( N)Tj Hi Andrey, /P <>BDC ET BT EMC (burn comparison. EMC ET BT ET EMC (98,500)Tj EMC ET flammability of fuel tanks in the commercial transport fleet. -.01 Tc 7 0 0 7 241.2727 375.9528 Tm Q EMC The westerly)Tj EMC (\(see table, this)Tj 56.25 0 0 56.25 36.8583 489.8898 Tm 0 Tc EMC -.02 Tc (MTOW and OEW. ET (passenger payload. EMC EMC ET -.02 Tc /P <>BDC EMC /P <>BDC 9 0 0 9 372.8879 412.8898 Tm ET 7 0 0 7 99.8582 298.7654 Tm /P <>BDC /P <>BDC (packages, it will be interesting to re-)Tj EMC ET BT 9 0 0 9 354.313 236.8898 Tm 9 0 0 9 165.0289 60.8898 Tm /GS2 gs BT EMC 6 0 0 6 271.9128 729.9528 Tm BT BT /P <>BDC -.02 Tc ET 9 0 0 9 203.1969 566.8898 Tm (passenger seat capacity as the older models)Tj (space, thereby freeing up more floor area)Tj /P <>BDC /OC /MC2304 BDC /P <>BDC (34,650)Tj /GS1 gs BT BT 8 0 0 8 474.6331 771.7654 Tm 7 0 0 7 490.5101 485.9528 Tm ET 6.5 0 0 6.5 244.2974 545.9529 Tm 7 0 0 7 508.4124 441.7654 Tm 9 0 0 9 215.4409 412.8898 Tm ( )Tj ET (136)Tj 9 0 0 9 568.1771 115.8898 Tm /P <>BDC /P <>BDC ( )Tj (assumed that no additional cargo is taken)Tj /P <>BDC 8 0 0 8 54.0516 771.7654 Tm EMC (passengers. /P <>BDC 0 Tc BT ( )Tj ( )Tj -.02 Tc BT ( )Tj ET BT ( )Tj BT /P <>BDC /P <>BDC 9 0 0 9 411.0234 698.8898 Tm ET -.02 Tc ( )Tj 7 0 0 7 182.5706 441.9528 Tm The A320ceo and)Tj ET EMC EMC 8 0 0 8 275.1912 745.9528 Tm ET /F7 1 Tf BT 7 0 0 7 474.3564 595.9528 Tm BT 9 0 0 9 394.0315 170.8898 Tm 7 0 0 7 354.6933 276.7654 Tm ET BT 7 0 0 7 508.4124 78.7654 Tm BT ()Tj BT ET EMC (have any payload limitations on the routes)Tj EMC ( )Tj /P <>BDC /P <>BDC ET 7 0 0 7 491.7142 276.7654 Tm BT 9 0 0 9 394.0315 709.8898 Tm BT /P <>BDC (To enable a comparison of the different)Tj EMC 7 0 0 7 490.8321 177.7654 Tm 7 0 0 7 337.9444 617.9528 Tm Q 7 0 0 7 473.8245 210.9528 Tm 7 0 0 7 491.7142 672.7654 Tm EMC ET ( )Tj ET EMC EMC EMC BT BT BT BT /GS2 gs 0 Tc /P <>BDC BT EMC ET The A321neo takes advantage of)Tj BT /P <>BDC /P <>BDC ( )Tj 0 Tc EMC ET EMC .0081 Tc 9 0 0 9 53.8582 49.8898 Tm ET What are the ATR 42 and ATR 72 aircraft made by Arospatiale and Leonardo? /P <>BDC ET -.02 Tc 6 0 0 6 146.7028 743.9528 Tm BT ( )Tj (A)Tj 7 0 0 7 380.2788 276.7654 Tm BT ET 9 0 0 9 535.511 379.8898 Tm testing. ( )Tj BT BT 0 Tc in later aircraft). BT ET 6.5 0 0 6.5 324.4345 650.9529 Tm /P <>BDC EMC /P <>BDC /P <>BDC ( )Tj BT EMC /P <>BDC ET 9 0 0 9 36.8504 49.8898 Tm ET [(A3)24.9(21neo)]TJ ET BT -.02 Tc BT ET ET ET ( )Tj ( )Tj 7 0 0 7 444.737 287.7654 Tm 7 0 0 7 247.7395 122.7654 Tm ET (145,505lbs, and a fuel capacity of 6,303)Tj /P <>BDC ET 7 0 0 7 199.5784 595.7654 Tm (types, but it is worth noting that in)Tj (comparison of the performance of the eight)Tj ET ET BT /P <>BDC EMC ET Today the Next Generation 737 sub-family includes the 700, -800 and 900models. BT ET BT /P <>BDC 7 0 0 7 99.8582 386.7654 Tm ( )Tj /P <>BDC EMC /P <>BDC 7 0 0 7 387.0932 287.9528 Tm ET EMC 7 0 0 7 141.7322 584.9528 Tm BT (4,163)Tj /P <>BDC BT (operator. /P <>BDC /P <>BDC 0 Tc BT 9 0 0 9 524.2249 478.8898 Tm ( )Tj (different available options, and gives the)Tj 5.25 0 0 5.25 515.3989 11.5129 Tm ET BT 7 0 0 7 490.5101 705.9528 Tm 7 0 0 7 491.4046 441.9528 Tm endobj /P <>BDC 7 0 0 7 36.8504 155.9528 Tm (0.0111)Tj ET EMC (ASM. 9 0 0 9 341.1717 478.8898 Tm ET EMC EMC /P <>BDC [(OM)8.1(M)-12.9(E)-24.9(R)7.1(C)8.1(E)]TJ BT BT ( )Tj ET BT BT exacerbating the imbalance. BT EMC EMC ET /P <>BDC (1,668)Tj ET ET ET ( )Tj 7 0 0 7 554.7883 177.7654 Tm BT (2,013)Tj EMC EMC BT EMC 7 0 0 7 294.4014 507.7654 Tm (sector. 0 Tc (160)Tj ET -.01 Tc 6 0 0 6 277.7064 715.9528 Tm /P <>BDC /P <>BDC 9 0 0 9 554.4741 412.8898 Tm BT /P <>BDC -.02 Tc BT ( )Tj 0 Tc ET EMC EMC ET EMC ET (2,518)Tj -.01 Tc EMC 8 0 0 8 394.0157 797.8898 Tm BT /P <>BDC ET ET ( )Tj (152)Tj 7 0 0 7 294.4014 375.7654 Tm EMC BT BT ET ET /P <>BDC 9 0 0 9 548.4747 115.8898 Tm ET /P <>BDC BT ( )Tj ET body angle so number 2 engine fuel is drawn from main tank 2, while engine 1 is ( )Tj ( )Tj 6 0 0 6 520.876 743.9528 Tm ET 0 Tc EMC ( )Tj ( )Tj [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ -.02 Tc BT ET (2,349nm because of strong headwind. /P <>BDC 0 Tc ET 9 0 0 9 194.7718 456.8898 Tm /P <>BDC -4.5143 -2.2339 -4.3751 -1.5784 -4.0786 -1.0086 c ET 7 0 0 7 326.2278 463.9528 Tm ( )Tj ET The typical range for this)Tj 8 0 0 8 394.0157 786.8898 Tm ET EMC The use of composite materials in the 737 Next Gen or even the 737 Max is quite conservative. (even though the two have the same)Tj 6 0 0 6 444.4713 757.9528 Tm (1,690)Tj /P <>BDC ET BT ET .0081 Tc ET (132,872)Tj ET BT ET 7 0 0 7 403.478 694.7654 Tm EMC 9 0 0 9 529.8783 621.8898 Tm ( )Tj BT ( )Tj 7 0 0 7 539.8962 705.9528 Tm EMC ET BT EMC /P <>BDC BT BT /P <>BDC (the longest BOS-LAX sector. 0 Tc BT 6 0 0 6 184.9362 743.9528 Tm BT BT /P <>BDC 0 Tc /P <>BDC W* n BT EMC BT /F4 1 Tf 0 Tc /P <>BDC ET ( )Tj ( )Tj BT ET /P <>BDC ET ET /P <>BDC /P <>BDC 9 0 0 9 53.8582 324.8898 Tm ( )Tj (5.1:1)Tj -.01 Tc Q EMC 8 0 0 8 124.845 703.9528 Tm ET /P <>BDC BT 7 0 0 7 337.9444 606.9528 Tm BT BT BT 6.5 0 0 6.5 244.2585 650.9529 Tm /P <>BDC -.02 Tc (The data in the second table is payload)Tj BT (I)Tj EMC EMC 7 0 0 7 519.3773 375.9528 Tm EMC -.02 Tc BT BT EMC EMC BT BT 7 0 0 7 299.0601 342.9528 Tm ( )Tj BT /F1 1 Tf /P <>BDC /P <>BDC 7 0 0 7 473.8245 419.9528 Tm (31,416)Tj ET ( )Tj 0 Tc ET EMC certain ground and flight cross flow conditions. EMC ( )Tj /P <>BDC (23)Tj 9 0 0 9 216.03 687.8898 Tm BT 7 0 0 7 440.0906 331.9528 Tm EMC 9 0 0 9 112.6132 302.8898 Tm EMC BT ( )Tj ET Hi. EMC BT ( )Tj 7 0 0 7 279.1575 243.9528 Tm 7 0 0 7 343.2355 485.7654 Tm [(BOS-SE)-13.9(A)]TJ /OC /MC5078 BDC 9 0 0 9 36.8504 401.8898 Tm 6 0 0 6 465.9401 729.9528 Tm EMC (operate with first, economy-plus and)Tj ()Tj 7 0 0 7 518.4953 199.9528 Tm EMC /P <>BDC ET BT 9 0 0 9 543.1465 511.8898 Tm /P <>BDC ( )Tj (5,243)Tj At least with the Max 8, looking into the ACAP of Boeing (Rev E), I found it is 2500nm. /P <>BDC /Artifact <>BDC (2,732)Tj 0 Tc /P <>BDC BT /GS1 gs ET ET EMC ET ET 63 0 obj 9 0 0 9 232.4217 170.8898 Tm BT /P <>BDC 7 0 0 7 355.3163 243.7654 Tm ET 0 Tc 9 0 0 9 77.618 82.8898 Tm (72,300)Tj ET EMC /P <>BDC 7 0 0 7 337.6855 408.9528 Tm (on the A320ceo to 11.0:1 on the A320neo. ET BT BT /F4 1 Tf 9 0 0 9 53.8582 269.8898 Tm BT BT BT ET /P <>BDC -.02 Tc ET ET BT ( )Tj BT ( )Tj 7 0 0 7 440.3636 474.9528 Tm (371,416)Tj ET ( )Tj BT /P <>BDC BT EMC /P <>BDC EMC -.02 Tc 0 Tc -.02 Tc 7 0 0 7 507.5303 100.7654 Tm BT BT The accuracy of the fuel flow transmitter is a function of the fuel flow. This compares)Tj ET /P <>BDC (same number of passengers is carried on)Tj [(T)92(axi in time - mins)]TJ (distances, and alternate airports are shown)Tj /GS1 gs 7 0 0 7 247.7395 166.7654 Tm 0 Tc /P <>BDC ET /P <>BDC -.02 Tc BT ( )Tj ET (cost compared to fuel. BT /P <>BDC ET 7 0 0 7 344.1175 584.7654 Tm 7 0 0 7 54.7071 617.7654 Tm BT 9 0 0 9 547.562 126.8898 Tm ET /P <>BDC EMC 7 0 0 7 54.7071 628.7654 Tm EMC 0 Tc BT ET 7 0 0 7 508.4124 320.7654 Tm The three-class cabin)Tj (A320neo:)Tj EMC /P <>BDC ( )Tj ( )Tj BT /P <>BDC -.02 Tc EMC BT BT ET 0 Tc /P <>BDC BT ( )Tj ET /P <>BDC ( )Tj 6 0 0 6 465.1841 743.9528 Tm (831)Tj /P <>BDC /P <>BDC BT EMC 7 0 0 7 278.2756 672.9528 Tm EMC EMC ET ET ET BT ET -.01 Tc EMC ET ET ET -.02 Tc ( )Tj EMC /P <>BDC 7 0 0 7 279.1575 628.9528 Tm BT /P <>BDC BT ET (I)Tj (A320neo:)Tj ET /P <>BDC /P <>BDC ( )Tj /F6 1 Tf /P <>BDC ET BT ET /P <>BDC ( )Tj -.02 Tc (performance improvement over the)Tj EMC -.01 Tc EMC 9 0 0 9 53.8582 445.8898 Tm EMC 9 0 0 9 188.8887 60.8898 Tm (34,650)Tj BT BT /P <>BDC ET BT BT /P <>BDC /P <>BDC /P <>BDC ET ( )Tj BT 7 0 0 7 490.8321 199.7654 Tm /P <>BDC (72,450)Tj /P <>BDC ET 9 0 0 9 232.4217 269.8898 Tm -.02 Tc BT BT 9 0 0 9 408.2047 423.8898 Tm /P <>BDC EMC (The A320neo has an average fuel burn)Tj /P <>BDC EMC /P <>BDC BT BT BT BT 7 0 0 7 54.7071 320.7654 Tm BT /P <>BDC ( )Tj panels. [(SS)-9.1(U)8(E)]TJ (126,312)Tj 7 0 0 7 204.0935 111.7654 Tm EMC ET 7 0 0 7 193.1059 287.9528 Tm BT ET /P <>BDC ET ET /P <>BDC Tweet !function(d,s,id){var js,fjs=d.getElementsByTagName(s)[0],p=/^http:/.test(d.location)? EMC /P <>BDC ET EMC ( )Tj /P <>BDC BT /Artifact <>BDC ET /P <>BDC BT ET EMC ET endobj q 1 0 0 1 394.012 447.878 cm 0 0 m ( N)Tj ( )Tj BT BT EMC (fuselage length. BT 6.5 0 0 6.5 448.8744 558.9529 Tm ET 7 0 0 7 491.7142 408.7654 Tm /P <>BDC /P <>BDC /P <>BDC ET /P <>BDC /P <>BDC /P <>BDC ET /P <>BDC EMC ET EMC /P <>BDC BT EMC ET EMC ET -.02 Tc EMC ( )Tj 0 Tc BT EMC 0 Tc ( )Tj /P <>BDC EMC -2.5295 -5.0573 -2.1058 -5.3146 -1.5527 -5.3151 c ET (ratio of 12.5:1; and the CFM LEAP-1A26)Tj BT -.02 Tc -.02 Tc 6 0 0 6 513.0339 701.9528 Tm .023 .567 .626 rg EMC 1 i 9 0 0 9 215.4409 38.8898 Tm 7 0 0 7 247.7395 683.7654 Tm EMC EMC BT EMC /P <>BDC ET ET .534 .14 .504 RG 9 0 0 9 378.9498 335.8898 Tm (288)Tj EMC ET 7 0 0 7 456.4753 738.7654 Tm EMC -.01 Tc ( )Tj (. EMC ET ( )Tj ET BT ( )Tj 0 Tc 9 0 0 9 215.4313 82.8898 Tm (136)Tj ET EMC (prices, and can vary by the aircraft type)Tj BT ( )Tj BT 7 0 0 7 387.0159 606.9528 Tm ()Tj 9 0 0 9 563.4796 324.8898 Tm (0.0171)Tj EMC ( )Tj ET 7 0 0 7 230.7317 727.9528 Tm ET BT ( )Tj EMC .661 .752 .896 rg 5.25 0 0 5.25 40.8474 11.5129 Tm 0 Tc ET 8 0 0 8 191.7259 771.9529 Tm /P <>BDC /F6 1 Tf ET ET 0 Tc -.01 Tc /P <>BDC ET /P <>BDC EMC (The A320ceo is payload-limited to 127)Tj 7 0 0 7 496.3063 705.7654 Tm 0 Tc BT BT -.01 Tc 0 Tc 0 Tc BT BT EMC /P <>BDC /P <>BDC BT /GS1 gs EMC Q 6 0 0 6 320.3167 757.9528 Tm 7 0 0 7 535.5029 496.7654 Tm 0 Tc ()Tj ( )Tj 9 0 0 9 53.8578 302.8898 Tm (and 737-9. BT 7 0 0 7 316.0679 419.7654 Tm EMC 9 0 0 9 212.0769 71.8898 Tm -.02 Tc ( )Tj )Tj EMC /P <>BDC BT 7 0 0 7 404.3599 595.7654 Tm 9 0 0 9 424.4247 764.8898 Tm BT /P <>BDC ET /P <>BDC /P <>BDC -.02 Tc BT 0 Tc ET BT ( )Tj EMC ET ET )Tj 9 0 0 9 555.2855 478.8898 Tm EMC EMC ( )Tj /P <>BDC 0 Tc ET ( )Tj ( )Tj ( )Tj 10 0 0 10 51.9004 814.1973 Tm BT 0 Tc Thank you. 0 Tc ET 7 0 0 7 337.4684 727.9528 Tm 0 Tc 0 Tc ET [(CFM L)17.1(E)-8.1(AP-1A32)]TJ EMC ET BT ET 9 0 0 9 36.8504 379.8898 Tm EMC (might have over an older aircraft would)Tj 7 0 0 7 496.3063 727.7654 Tm EMC BT EMC /P <>BDC EMC (737-8)Tj EMC ET BT /P <>BDC 0 Tc EMC /P <>BDC ( )Tj EMC ( )Tj BT (CFM56-7B26)Tj 8 0 0 8 91.2605 771.9529 Tm [(M)21(T)39.1(O)7.1(W)0( - lbs)]TJ EMC 9 0 0 9 394.0157 522.8898 Tm ET /P <>BDC EMC EMC BT available a Boeing 737 for modification and testing. /P <>BDC 0 Tc EMC 0 Tc Boeing 737 Assembly, the building of this popular City Jet. )Tj /P <>BDC 7 0 0 7 114.6416 298.9528 Tm The total tolerance for the FQIS system is based on a full tank. /P <>BDC /P <>BDC ET /P <>BDC (A320ceo is limited to 127 passengers on)Tj 0 Tc (158)Tj BT ET BT ET /P <>BDC -.02 Tc (326-339)Tj 9 0 0 9 548.1057 610.8898 Tm 6 0 0 6 258.3167 757.9528 Tm BT EMC /P <>BDC EMC ET Q 7 0 0 7 258.2805 474.7654 Tm EMC (flight levels )Tj BT (977)Tj 9 0 0 9 215.4409 522.8898 Tm ( )Tj 0 Tc EMC 6.5 0 0 6.5 54.877 565.9529 Tm 8 0 0 8 43.6039 633.9528 Tm EMC (1,089)Tj 8 0 0 8 549.2646 49.8898 Tm The aircraft also features)Tj ET ( )Tj (170)Tj ( )Tj /P <>BDC of the fuel gauges is done by capacitance trimmers, these are adjusted 9 0 0 9 565.8376 577.8898 Tm BT 9 0 0 9 362.4471 82.8898 Tm 7 0 0 7 108.6215 243.9528 Tm BT ET (1,945)Tj 9 0 0 9 53.8582 720.8898 Tm EMC BT 7 0 0 7 299.0601 100.9528 Tm ET ET 9 0 0 9 192.5225 489.8898 Tm -.02 Tc 9 0 0 9 532.5876 137.8898 Tm 9 0 0 9 215.4313 170.8898 Tm /P <>BDC ( )Tj ( )Tj EMC EMC ET /P <>BDC /P <>BDC ( )Tj ( )Tj BT /P <>BDC 0 Tc -.02 Tc ET /P <>BDC 9 0 0 9 211.7668 225.8898 Tm ET EMC ET /P <>BDC EMC (160)Tj ( )Tj (differences in the flight times. /P <>BDC EMC BT /P <>BDC ET BT EMC BT 424 0 obj 7 0 0 7 354.6933 529.7654 Tm EMC BT [(SS)-9.1(U)8(E)]TJ EMC 9 0 0 9 411.0097 291.8898 Tm .151 .147 .15 rg /P <>BDC EMC 7 0 0 7 36.8504 11.5129 Tm 0 Tc 9 0 0 9 408.1889 137.8898 Tm As stated, this makes a fair)Tj 7 0 0 7 491.4046 210.9528 Tm ET /P <>BDC (The three main operational costs for)Tj ET ET BT ET 0 Tc BT 7 0 0 7 439.2087 419.9528 Tm ( )Tj /P <>BDC /P <>BDC BT ( )Tj BT /P <>BDC 7 0 0 7 294.4014 485.7654 Tm ET EMC (payload is carried. BT 7 0 0 7 279.1575 320.9528 Tm BT ET 7 0 0 7 363.2711 386.9528 Tm BT (CFM56-7B27B3)Tj 6 0 0 6 309.2107 771.9528 Tm BT 0 Tc BT 7 0 0 7 508.2252 11.5129 Tm /P <>BDC BT EMC BT -.02 Tc EMC 6 0 0 6 450.9814 701.9528 Tm EMC q BT 9 0 0 9 360.9639 192.8898 Tm (0.0135)Tj 0 Tc ET /P <>BDC (955)Tj /P <>BDC /P <>BDC BT (170)Tj [(SS)-9(U)8.1(E)]TJ BT 7 0 0 7 321.6356 309.9528 Tm 7 0 0 7 490.8321 386.7654 Tm /P <>BDC 6 0 0 6 465.8383 673.9528 Tm 7 0 0 7 362.3891 331.9528 Tm (Since all eight aircraft types are in)Tj ET 9 0 0 9 267.0826 500.8898 Tm BT EMC /P <>BDC EMC BT ( )Tj ET ET /P <>BDC 7 0 0 7 37.0536 617.9528 Tm 7 0 0 7 37.6993 397.9528 Tm EMC /P <>BDC ET (0.0122)Tj EMC EMC 7 0 0 7 491.392 672.9528 Tm /P <>BDC /P <>BDC -.02 Tc 6 0 0 6 466.0123 687.9528 Tm ET ET EMC 9 0 0 9 215.433 214.8898 Tm -.02 Tc /P <>BDC (carried - lbs)Tj BT ET 7 0 0 7 187.0858 298.9528 Tm BT /P <>BDC BT /P <>BDC BT ET ( )Tj ET ( )Tj 7 0 0 7 518.4953 232.9528 Tm ET -.01 Tc /P <>BDC 9 0 0 9 232.438 181.8898 Tm 7 0 0 7 554.7883 298.7654 Tm /P <>BDC -.01 Tc I not sure what you mean by a and b basis allowable. BT /P <>BDC ET 8 0 0 8 259.5105 675.9528 Tm BT 9 0 0 9 232.4217 544.8898 Tm 13 0 0 13 205.5668 412.8898 Tm EMC BT ET 9 0 0 9 36.8504 511.8898 Tm ET ET BT BT BT ( )Tj EMC 9 0 0 9 341.4411 247.8898 Tm 6.5 0 0 6.5 296.4841 689.9529 Tm EMC ET EMC ( )Tj ( )Tj (831)Tj ( )Tj BT Thai Airways on 3 Mar 2001 and 737-300 EI-BZG operated by Philippine Airlines ET EMC ET 9 0 0 9 411.0181 390.8898 Tm 9 0 0 9 232.438 390.8898 Tm /P <>BDC EMC 7 0 0 7 316.0679 177.7654 Tm (I)Tj BT ET 9 0 0 9 215.4313 214.8898 Tm 9 0 0 9 548.3644 533.8898 Tm (127)Tj 9 0 0 9 53.8578 60.8898 Tm (range for both the A320ceo and A320neo. 6.5 0 0 6.5 243.4784 585.9529 Tm EMC /P <>BDC BT EMC )Tj ET 7 0 0 7 363.2711 221.9528 Tm 9 0 0 9 408.2047 313.8898 Tm EMC ET ET EMC (at 27,000lbs thrust compared to the)Tj .151 .147 .15 rg ( )Tj 9 0 0 9 411.0234 764.8898 Tm EMC BT ET S EMC EMC BT Over the nine)Tj EMC (of fuel against time-related costs. 9 0 0 9 518.9185 401.8898 Tm EMC 7 0 0 7 554.7883 364.7654 Tm ET 9 0 0 9 550.3666 247.8898 Tm BT BT EMC (20/29/143, giving a maximum capacity of)Tj (the CFM56-5B with thrust ratings of)Tj BT 9 0 0 9 126.1392 522.8898 Tm (\(Toronto Pearson\) sector, to 2,730nm for)Tj -.02 Tc /P <>BDC That is because it is an 800. -.02 Tc (1465,400)Tj ET -.02 Tc EMC /P <>BDC EMC 6.5 0 0 6.5 531.9417 637.9529 Tm /P <>BDC EMC ET EMC /P <>BDC 7 0 0 7 403.478 375.7654 Tm 0 Tc (total seat count for these two types. 7 0 0 7 536.3849 595.7654 Tm ET /P <>BDC ET BT 10 0 0 10 312.5146 771.9528 Tm 6 0 0 6 396.1516 743.9528 Tm EMC BT BT (1,272)Tj EMC EMC EMC -.02 Tc EMC ET /P <>BDC (39,270lbs)Tj (would need to consider many more factors)Tj /P <>BDC W n /P <>BDC

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