S ET ( )Tj ( )Tj 7 0 0 7 473.8245 144.9528 Tm 0 Tc ( )Tj -.02 Tc /P <>BDC 7 0 0 7 354.6933 397.7654 Tm 7 0 0 7 294.4014 639.7654 Tm EMC ( )Tj 7 0 0 7 37.5838 650.9528 Tm 0 Tc 7 0 0 7 158.74 221.7654 Tm 9 0 0 9 569.7076 148.8898 Tm ET BT 9 0 0 9 384.7818 137.8898 Tm ET ET 7 0 0 7 473.8245 364.9528 Tm ET BT EMC /P <>BDC BT BT [(CFM L)17.1(E)-8.1(AP-1B27)]TJ /P <>BDC ET ET BT W n ET 9 0 0 9 53.8338 115.8898 Tm /P <>BDC )Tj ( )Tj 7 0 0 7 37.5838 254.9528 Tm 7 0 0 7 507.7893 419.7654 Tm (737-9)Tj EMC /P <>BDC BT BT /P <>BDC /P <>BDC /P <>BDC BT ET EMC 7 0 0 7 338.3085 342.9528 Tm (30,000lbs to 33,000lbs, a fan diameter of)Tj /P <>BDC /P <>BDC 9 0 0 9 411.0097 522.8898 Tm ET ET ET EMC ( )Tj ( )Tj /F1 1 Tf /P <>BDC (166,090)Tj 9 0 0 9 215.4409 258.8898 Tm BT ET (4,863)Tj /Artifact <>BDC 8 0 0 8 159.2283 745.9528 Tm (A320neo)Tj EMC /P <>BDC /P <>BDC 7 0 0 7 537.7804 133.9528 Tm ET ET BT BT ET /P <>BDC 7 0 0 7 158.74 441.7654 Tm EMC (rated at 24,800lbs with a bypass ratio of)Tj EMC BT BT EMC 7 0 0 7 99.8582 243.7654 Tm /P <>BDC /P <>BDC /P <>BDC ( )Tj /P <>BDC [(SS)-9.1(U)8(E)]TJ ( )Tj EMC /P <>BDC EMC ET ET EMC 9 0 0 9 372.0688 324.8898 Tm ET 7 0 0 7 297.632 496.9528 Tm /P <>BDC BT ET (404)Tj EMC BT 7 0 0 7 43.6039 650.9528 Tm /P <>BDC EMC (166,090)Tj BT 7 0 0 7 60.6117 738.7654 Tm /P <>BDC ( )Tj ET EMC 9 0 0 9 186.5751 423.8898 Tm ( )Tj EMC EMC 9 0 0 9 394.0157 566.8898 Tm /P <>BDC /P <>BDC ( )Tj BT EMC EMC /P <>BDC [(CFM L)17.1(E)-8.1(AP-1B27)]TJ Alaska Airlines launched the 737-900 in 1997, the 737-900 made its first . ( )Tj EMC EMC ET ( )Tj (are taxi fuel burn, flight fuel burn, the)Tj This is equivalent to)Tj /P <>BDC /P <>BDC ( )Tj /P <>BDC EMC BT 9 0 0 9 193.4848 280.8898 Tm /P <>BDC EMC ET (208)Tj EMC ( )Tj ( )Tj ET ET BT ET /GS1 gs -.02 Tc ( )Tj ET ET ( )Tj BT (152)Tj /Artifact <>BDC 6.5 0 0 6.5 54.877 637.9529 Tm 7 0 0 7 364.1531 474.9528 Tm 9 0 0 9 411.0097 412.8898 Tm BT ET /P <>BDC ET EMC BT (374-388)Tj ( )Tj 9 0 0 9 362.0968 324.8898 Tm EMC ET /P <>BDC EMC 7 0 0 7 279.1575 595.9528 Tm ET /P <>BDC ET EMC (34,650lbs)Tj /OC /MC5080 BDC BT /P <>BDC -2.4549 -3.9026 m /P <>BDC EMC ET /P <>BDC 6.5 0 0 6.5 54.877 663.9529 Tm /P <>BDC [(CFM L)17.1(E)-8.1(AP-1A26)]TJ BT /P <>BDC EMC EMC /P <>BDC EMC /P <>BDC ( )Tj ( )Tj BT 9 0 0 9 215.433 412.8898 Tm 9 0 0 9 555.1526 368.8898 Tm ET ET BT BT BT EMC 9 0 0 9 36.8583 456.8898 Tm 0 Tc EMC /P <>BDC ( )Tj /P <>BDC /P <>BDC EMC /P <>BDC EMC 7 0 0 7 247.7395 375.7654 Tm (network. 7 0 0 7 99.8582 210.7654 Tm /P <>BDC ET /P <>BDC (720)Tj 9 0 0 9 538.8793 368.8898 Tm /F4 1 Tf Q ET -.02 Tc ( )Tj EMC 0 Tc EMC EMC BT (375)Tj 8 0 0 8 38.4438 591.9528 Tm ET BT /P <>BDC /P <>BDC /P <>BDC In contrast, the 737-8s performance)Tj 7 0 0 7 247.7395 628.7654 Tm )Tj BT (A320neo:)Tj 7 0 0 7 82.2047 661.9528 Tm 137 )Tj (capacity, whereas the A321neo, with the)Tj ET ET ET (period in 2020. /P <>BDC BT EMC /P <>BDC BT /P <>BDC ET )Tj This comprised a 2,000 US Gal (7,570 litre) bladder 9 0 0 9 394.0315 511.8898 Tm Q EMC (increases to an average of 3.3% for the)Tj -.02 Tc 0 Tc /P <>BDC 6 0 0 6 495.9463 771.9528 Tm EMC BT )Tj BT /P <>BDC BT 0 Tc /P <>BDC ET (248,200)Tj EMC ET BT /P <>BDC ET EMC /P <>BDC BT .964 .834 .406 rg /P <>BDC BT (method of operation that balances the cost)Tj EMC EMC /P <>BDC EMC 9 0 0 9 207.8168 445.8898 Tm 7 0 0 7 241.2727 166.9528 Tm ET BT BT 7 0 0 7 537.7804 298.9528 Tm 6 0 0 6 138.6506 757.9528 Tm -.01 Tc /P <>BDC [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ Follow this link to see the "Quick Change" Aux fuel system offered by Long Range, expected 2015. ET /P <>BDC ( )Tj 7 0 0 7 99.8582 287.7654 Tm 7 0 0 7 247.7395 232.7654 Tm BT ET ET 7 0 0 7 125.6292 540.7654 Tm BT ET BT 9 0 0 9 552.0261 555.8898 Tm /F1 1 Tf 7 0 0 7 387.0932 265.9528 Tm 7 0 0 7 59.2108 11.5129 Tm 7 0 0 7 187.0858 529.9528 Tm /P <>BDC ET EMC 7 0 0 7 355.3163 221.7654 Tm EMC /P <>BDC EMC )Tj ET BT /P <>BDC -.02 Tc 6.5 0 0 6.5 375.6529 663.9529 Tm is actually the back of the centre fuel tank. ET 6 0 0 6 184.9964 757.9528 Tm BT 9 0 0 9 544.9208 280.8898 Tm -.02 Tc ( )Tj 0 Tc -.02 Tc /P <>BDC ( )Tj 7 0 0 7 379.3969 177.7654 Tm EMC /GS1 gs /P <>BDC ET ( )Tj EMC ET /P <>BDC 9 0 0 9 36.8504 478.8898 Tm /P <>BDC EMC ET BT -.02 Tc ( )Tj (0.0141)Tj EMC /P <>BDC 7 0 0 7 316.0679 177.7654 Tm ET ET BT ET 0 Tc EMC ET BT BT ET EMC ET EMC ET ( )Tj ET ET ET 7 0 0 7 314.6398 727.7654 Tm -.02 Tc -.01 Tc (1,138)Tj EMC (A321ceo)Tj BT /P <>BDC 6.5 0 0 6.5 64.6596 532.9529 Tm EMC /P <>BDC EMC ET EMC 6.5 0 0 6.5 244.4599 702.9529 Tm ( )Tj EMC /P <>BDC -.02 Tc EMC /P <>BDC /P <>BDC BT ( 2021)Tj BT -.02 Tc 9 0 0 9 246.6113 71.8898 Tm 9 0 0 9 192.1006 456.8898 Tm /P <>BDC ( )Tj /P <>BDC (financial cost structure and their fuel)Tj 7 0 0 7 297.632 463.9528 Tm EMC EMC EMC 304.725 420.96 m /P <>BDC BT EMC ( )Tj ET EMC EMC EMC ET /P <>BDC /P <>BDC ET [(F)43(uel burn/)]TJ /P <>BDC /P <>BDC BT (56,901)Tj 6.5 0 0 6.5 347.0329 611.9529 Tm ET -.02 Tc 0 841.89 609.449 -841.89 re ( )Tj ET 7 0 0 7 130.1443 122.7654 Tm EMC 7 0 0 7 445.7203 11.5129 Tm EMC /P <>BDC 9 0 0 9 408.1968 159.8898 Tm ET EMC /P <>BDC EMC (737-800W)Tj BT BT ET 9 0 0 9 107.6178 269.8898 Tm /TT2 1 Tf BT BT on 5 Nov 1990 have been destroyed on the ground due to explosions in the empty 9 0 0 9 51.0236 445.8898 Tm /P <>BDC /P <>BDC BT EMC (551)Tj 6.5 0 0 6.5 448.1595 735.9529 Tm /P <>BDC 0 Tc BT 8 0 0 8 421.0237 771.7654 Tm /P <>BDC /P <>BDC ( )Tj 0 Tc 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). ET /GS1 gs ( )Tj 7 0 0 7 315.1859 111.7654 Tm 7 0 0 7 108.6215 265.9528 Tm EMC /P <>BDC EMC ( )Tj 6 0 0 6 527.3577 771.9528 Tm EMC (900ER\(W\) across the 14 routes with the)Tj ET -.01 Tc /P <>BDC ( )Tj 9 0 0 9 411.0097 38.8898 Tm EMC /P <>BDC BT BT ( )Tj EMC 6 0 0 6 258.3167 715.9528 Tm /P <>BDC BT 7 0 0 7 54.7071 573.7654 Tm (0.0119)Tj /P <>BDC ET 7 0 0 7 344.1175 573.7654 Tm BT ET /P <>BDC 9 0 0 9 394.0123 236.8898 Tm EMC upper surface of the wings where this frost is allowable for despatch under the -.02 Tc EMC BT The design of the 737-800 lends itself to the sleek size and prowess of this aircraft. 9 0 0 9 357.6917 192.8898 Tm ET 9 0 0 9 189.3204 324.8898 Tm EMC /F4 1 Tf -.02 Tc BT /P <>BDC (would be no additional holding required,)Tj /P <>BDC 9 0 0 9 408.1889 467.8898 Tm BT /P <>BDC BT ET EMC BT EMC BT ( )Tj /P <>BDC (CFM56-7B27B3)Tj /P <>BDC 7 0 0 7 354.6933 430.7654 Tm EMC 7 0 0 7 118.104 606.7654 Tm -.02 Tc (The first-class layout uses four-abreast)Tj EMC /P <>BDC (series of aircraft benefits from increased)Tj 6.5 0 0 6.5 346.3049 676.9529 Tm (manufacturers support these aircraft types)Tj BT ET ET ET EMC /P <>BDC 7 0 0 7 403.478 639.7654 Tm BT ET EMC ET ET BT -.02 Tc ET -.02 Tc ET /P <>BDC /P <>BDC 9 0 0 9 496.6703 148.8898 Tm 6.5 0 0 6.5 346.1424 545.9529 Tm EMC /P <>BDC BT ET ET (388)Tj 9 0 0 9 547.3786 71.8898 Tm ET EMC /P <>BDC BT BT (BOS-DEN)Tj /P <>BDC (space, thereby freeing up more floor area)Tj EMC EMC (1,351)Tj 7 0 0 7 299.0601 276.9528 Tm 9 0 0 9 294.2183 346.8898 Tm /P <>BDC 9 0 0 9 215.433 445.8898 Tm ( )Tj ( )Tj EMC -.01 Tc <>stream EMC /P <>BDC EMC 7 0 0 7 141.7322 298.9528 Tm 7 0 0 7 158.74 265.7654 Tm BT S EMC ( )Tj 0 Tc ET 6.5 0 0 6.5 276.4014 598.9529 Tm 0 Tc 9 0 0 9 411.0181 236.8898 Tm BT 7 0 0 7 362.3891 342.9528 Tm ( )Tj 0 Tc Q BT /P <>BDC /P <>BDC EMC BT 7 0 0 7 297.632 705.9528 Tm Values can be entered and displayed in pounds or kilograms. /P <>BDC ET 8 0 0 8 549.2646 49.8898 Tm BT BT /P <>BDC ET ET ET (O)Tj EMC -.02 Tc 7 0 0 7 187.0858 562.9528 Tm 7 0 0 7 337.6855 496.9528 Tm EMC ( )Tj ET ( )Tj /P <>BDC 9 0 0 9 423.3885 401.8898 Tm EMC /P <>BDC ET ET (310,080)Tj 9 0 0 9 180.5261 423.8898 Tm ( )Tj /P <>BDC ET 6 0 0 6 403.4411 715.9528 Tm 0 Tc /P <>BDC EMC (51,500)Tj EMC 9 0 0 9 548.5375 225.8898 Tm The global climate of rising fuel costs, as well as increased competition in the form of the Airbus A320, have ensured that Boeing continues to bring out more improved versions of the type. /F1 1 Tf ( )Tj BT 8 0 0 8 439.9149 760.9528 Tm ( )Tj BT BT (\(Toronto Pearson\) sector, to 2,730nm for)Tj EMC (216,240)Tj BT 9 0 0 9 394.0237 203.8898 Tm ET ET (than is possible in this article. (uses one of the 11 certified weight variants. 6.5 0 0 6.5 172.8217 565.9529 Tm 7 0 0 7 141.7322 617.9528 Tm BT 7 0 0 7 101.0963 408.9528 Tm -.02 Tc BT It was demonstrated under EMC Bombardier CRJ 700/CRJ 900/CRJ 1000 Series. 0 Tc /P <>BDC In real)Tj /P <>BDC EMC (136)Tj fuel pumps will automatically shut off when they detect a low output pressure. EMC ( )Tj /P <>BDC [(SS)-9(U)8.1(E)]TJ (288)Tj 9 0 0 9 192.1373 401.8898 Tm 9 0 0 9 533.0564 181.8898 Tm /P <>BDC 9 0 0 9 51.0236 115.8898 Tm BT 0 Tc BT EMC EMC /P <>BDC 9 0 0 9 531.8156 280.8898 Tm ( )Tj /P <>BDC BT BT 0 Tc /P <>BDC /P <>BDC EMC BT ET BT BT ET EMC ET EMC ET BT /P <>BDC ET /P <>BDC EMC EMC 10 0 0 10 47.7404 814.1973 Tm 7 0 0 7 337.6855 529.9528 Tm BT EMC (/S)Tj ( )Tj (163,900)Tj ET ET 0 Tc (difference between the aircraft types)Tj ( )Tj /P <>BDC EMC EMC /F7 1 Tf BT /P <>BDC /P <>BDC ET BT BT /P <>BDC (31,416)Tj ( )Tj ET 6 0 0 6 427.5796 729.9528 Tm As you can appreciate, the cockpit of any aircraft is always a non-standard shape. 9 0 0 9 215.4313 511.8898 Tm BT /P <>BDC BT BT 6 0 0 6 561.1317 771.9528 Tm (208-217)Tj 7 0 0 7 343.2355 474.7654 Tm /P <>BDC EMC ET BT 7 0 0 7 187.0858 364.9528 Tm ( )Tj However engineers designing the 737 opted to lighten the structure with the engines underneath he wings and allow for the fuselage to be widened for six-abreast seating. (170)Tj BT -.02 Tc BT 0 Tc ET ET )Tj 7 0 0 7 37.6993 232.9528 Tm ( )Tj 7 0 0 7 379.3969 221.7654 Tm BT /P <>BDC 7 0 0 7 320.7537 78.9528 Tm The Boeing 737-800 variant has as mentioned 27300 pound-force delivered by two turbo fans. BT - Modern Airliners. /P <>BDC (382,280)Tj /P <>BDC EMC ( )Tj EMC /P <>BDC /GS2 gs BT -.02 Tc .151 .147 .15 rg ( )Tj EMC EMC EMC EMC /P <>BDC (151)Tj ( )Tj ET /P <>BDC /P <>BDC (category. EMC -.02 Tc EMC EMC EMC ET ( )Tj /P <>BDC EMC ET /P <>BDC EMC f /P <>BDC ( )Tj ( )Tj 6 0 0 6 153.7355 729.9528 Tm EMC 9 0 0 9 140.333 313.8898 Tm ET /P <>BDC 9 0 0 9 425.1967 720.8898 Tm /P <>BDC BT 0 Tc ET 0 Tc ( )Tj /P <>BDC 9 0 0 9 191.4329 786.8898 Tm EMC 7 0 0 7 383.0719 716.7654 Tm EMC BT /P <>BDC ET ()Tj EMC EMC /P <>BDC .0081 Tc [(P)11(assengers)]TJ ET EMC ET ( )Tj 7 0 0 7 355.5753 562.7654 Tm EMC 0 Tc BT 7 0 0 7 37.5838 342.9528 Tm ET -.02 Tc /P <>BDC /P <>BDC BT ET EMC /P <>BDC 7 0 0 7 535.5029 397.7654 Tm 6 0 0 6 254.6866 659.9528 Tm ( )Tj 6 0 0 6 465.3942 771.9528 Tm (136)Tj BT /P <>BDC /P <>BDC /P <>BDC 7 0 0 7 490.7815 276.9528 Tm EMC (150)Tj ET /P <>BDC /F6 1 Tf BT /GS2 gs The B737-800SF Cargo Conversion consists of the installation of a 86x137 cargo door on the left side of the fuselage, and modification of the main deck to a Class E cargo compartment. ET ( )Tj (0.0154)Tj ( )Tj (and Boeing aircraft benefit from the)Tj /P <>BDC ET 0 Tc /P <>BDC (distance flown increases, the fuel burn)Tj ET ET /P <>BDC EMC /P <>BDC 7 0 0 7 131.6494 276.7654 Tm ET /F1 1 Tf 7 0 0 7 199.5784 144.7654 Tm 7 0 0 7 403.478 507.7654 Tm EMC EMC ET (38,168)Tj A family consultation. ( )Tj ( )Tj /P <>BDC 9 0 0 9 529.0344 445.8898 Tm EMC ET BT ET /P <>BDC (39,270)Tj [(UG)-17.1(U)-8(S)8.1(T)]TJ (39,270)Tj (2,060)Tj /GS2 gs ET ET BT 7 0 0 7 457.0984 89.7654 Tm .008 Tc BT 517.252 90.783 l ( )Tj BT (fuel burn evaluation compares the selected)Tj BT BT BT 9 0 0 9 562.507 203.8898 Tm EMC ( )Tj (0.0126)Tj ( )Tj ET 0 Tc EMC BT BT ET 9 0 0 9 560.5186 214.8898 Tm EMC /GS2 gs ( )Tj ET ( )Tj BT ET BT /P <>BDC (2,500)Tj (has resulted in them requiring less galley)Tj (CFM56-)Tj 0 Tc BT EMC 6.5 0 0 6.5 178.4573 722.9529 Tm /P <>BDC -.01 Tc ET Report (DOT/FAA/AR-01/63) (4.8Mb), MAX: 3,869 + 12,990 + 3,869 = 20,729kg, 1/200: /P <>BDC ET ET ET ( )Tj ET 10 0 0 10 47.1144 814.1973 Tm EMC (1,272)Tj EMC /P <>BDC ET EMC It has a maximum takeoff weight of about 80,000 kg (175,000 lbs). -.005 Tc W n 9 0 0 9 394.0315 665.8898 Tm ET EMC ET EMC BT 7 0 0 7 537.7804 397.9528 Tm /P <>BDC /P <>BDC 9 0 0 9 215.4313 269.8898 Tm ( )Tj BT 73 0 obj (seat capacity over the NG series. 6 0 0 6 495.9995 659.9528 Tm /Artifact <>BDC (setting. 9 0 0 9 229.6045 104.8898 Tm ET 0 Tc ET EMC EMC /P <>BDC BT /P <>BDC (170)Tj 7 0 0 7 82.2047 485.9528 Tm EMC EMC BT 9 0 0 9 530.5354 665.8898 Tm 6 0 0 6 403.1408 687.9528 Tm EMC /P <>BDC BT 0 Tc EMC (Under payload scenario 1, where the)Tj BT ET (- USG)Tj EMC 137 )Tj /P <>BDC /P <>BDC ET (tracked distance, ESAD, and the difference)Tj EMC ( )Tj /P <>BDC BT /P <>BDC 0 Tc BT 6.5 0 0 6.5 382.478 545.9529 Tm (737-9)Tj 7 0 0 7 315.5217 562.7654 Tm (A320neo)Tj /P <>BDC /P <>BDC BT ET ET (\(see table, this page\))Tj EMC ( )Tj 0 Tc ( )Tj ( )Tj ET EMC 9 0 0 9 394.0157 544.8898 Tm (with a thrust rating of 27,000lbs, an intake)Tj 9 0 0 9 215.4313 313.8898 Tm /P <>BDC (0.0142)Tj EMC BT After EMC 7 0 0 7 363.2711 397.9528 Tm ET ET BT /P <>BDC -.01 Tc BT ( )Tj EMC /Artifact <>BDC (A320neo)Tj 9 0 0 9 394.0315 236.8898 Tm ( )Tj ET /P <>BDC ET BT ( )Tj ET ET BT /P <>BDC EMC Q 7 0 0 7 295.2833 78.7654 Tm ET -.02 Tc ET EMC 5.25 0 0 5.25 100.8225 11.5132 Tm /P <>BDC ET 13 0 0 13 118.3688 390.8898 Tm BT EMC (3,882)Tj from cockpit door to the kitchen alley . The Boeing 777-200 has a maximum fuel capacity of 31,000 gallons or 117,347 liters. 7 0 0 7 43.6039 738.9528 Tm ( )Tj 7 0 0 7 141.7322 199.9528 Tm [(CFM L)17.1(E)-8.1(AP-1A32)]TJ (136)Tj /P <>BDC BT ET BT ET 7 0 0 7 535.5029 243.7654 Tm EMC EMC 7 0 0 7 182.5706 540.9528 Tm 7 0 0 7 277.3936 177.9528 Tm /P <>BDC Q ET EMC EMC /P <>BDC BT EMC 7 0 0 7 445.619 408.7654 Tm ET 5.25 0 0 5.25 40.8474 11.5129 Tm /P <>BDC EMC 7 0 0 7 247.7395 419.7654 Tm BT EMC ( )Tj 9 0 0 9 229.6064 126.8898 Tm 7 0 0 7 354.6933 496.7654 Tm 7 0 0 7 37.6993 78.9528 Tm BT EMC ET /P <>BDC 7 0 0 7 337.4684 683.9528 Tm /P <>BDC -.01 Tc BT BT EMC ET EMC EMC 7 0 0 7 99.8582 375.7654 Tm EMC 7 0 0 7 537.267 232.7654 Tm BT Having a higher)Tj (9.0:1)Tj ET ( 2021)Tj -.02 Tc BT BT ET ET EMC 0 Tc ( )Tj BT BT 9 0 0 9 551.4784 797.8898 Tm (20)Tj EMC /P <>BDC ( )Tj ( )Tj ET ET BT EMC /P <>BDC ET 7 0 0 7 508.4124 496.7654 Tm -.02 Tc ET 28.5749 0 TD (150)Tj (112)Tj ET ( )Tj BT BT BT BT /P <>BDC ET EMC /P <>BDC EMC -.02 Tc 7 0 0 7 54.7071 485.7654 Tm EMC 7 0 0 7 82.2047 518.9528 Tm 0 Tc EMC (45,276)Tj 9 0 0 9 232.4217 181.8898 Tm EMC EMC ET 9 0 0 9 524.2249 478.8898 Tm BT EMC 8 0 0 8 124.845 633.9528 Tm BT /P <>BDC EMC 36.85 31.181 518.74 773.859 re (an OEW of 98,500lbs )Tj /P <>BDC [(CFM L)17.1(E)-8.1(AP-1A32)]TJ Federal Aviation Administration and the Boeing Company to evaluate the )Tj [(BOS-SE)-13.9(A)]TJ ET ET /GS1 gs The Boeing 737-800 variant has as mentioned 27300 pound-force delivered by two turbo fans. EMC 7 0 0 7 141.7322 89.9528 Tm BT EMC (challenge for all airlines. /P <>BDC (976)Tj ET /P <>BDC 8 0 0 8 95.6042 633.9528 Tm 0 Tc ET BT BT BT 5.25 0 0 5.25 64.5461 11.5129 Tm ET EMC BT BT /P <>BDC BT 7 0 0 7 337.9444 639.9528 Tm /F4 1 Tf 7 0 0 7 82.8504 287.9528 Tm (170)Tj ET 7 0 0 7 338.3085 287.9528 Tm /P <>BDC ( )Tj 7 0 0 7 354.6933 419.7654 Tm 7 0 0 7 230.7317 474.9528 Tm BT 9 0 0 9 362.8235 401.8898 Tm BT 6.5 0 0 6.5 499.597 558.9529 Tm ET ET 7 0 0 7 354.6933 540.7654 Tm ( )Tj 9 0 0 9 194.061 324.8898 Tm 7 0 0 7 158.74 727.7654 Tm (0.0141)Tj BT ET 9 0 0 9 232.4217 401.8898 Tm BT /P <>BDC ET 7 0 0 7 363.2711 573.9528 Tm BT 6.5 0 0 6.5 171.7493 689.9529 Tm ( )Tj /P <>BDC BT EMC -.01 Tc EMC BT 7 0 0 7 37.6993 188.9528 Tm [(E)-7.8(P)16.1(T)9(E)-13.9(MBE)-16.9(R)]TJ ET 7 0 0 7 354.6933 639.7654 Tm -.02 Tc 7 0 0 7 179.5605 419.9528 Tm /P <>BDC 6 0 0 6 176.4941 687.9528 Tm 9 0 0 9 215.433 324.8898 Tm 9 0 0 9 361.5742 192.8898 Tm ET /P <>BDC BT BT 7 0 0 7 554.7883 540.7654 Tm ET ( )Tj 9 0 0 9 376.7938 500.8898 Tm EMC ET /P <>BDC ET /P <>BDC /P <>BDC EMC 6 0 0 6 506.5237 757.9528 Tm 0 Tc ( )Tj 6.5 0 0 6.5 534.5352 558.9529 Tm ( )Tj 9 0 0 9 68.0314 775.8898 Tm BT 7 0 0 7 456.2165 144.7654 Tm 7 0 0 7 141.7322 661.9528 Tm BT EMC ( )Tj ET BT ET ( )Tj BT ET EMC ( )Tj (A321ceo)Tj BT BT 7 0 0 7 88.196 11.5129 Tm ET 9 0 0 9 555.4203 346.8898 Tm 0 Tc BT /P <>BDC EMC 7 0 0 7 179.5605 617.9528 Tm EMC (0.0149)Tj ( )Tj ET ( )Tj /P <>BDC /P <>BDC BT ( )Tj (-60)Tj Fuel remains one of the)Tj EMC 7 0 0 7 535.5029 540.7654 Tm /P <>BDC /P <>BDC BT EMC 7 0 0 7 101.0963 309.9528 Tm ET (483)Tj -.01 Tc (A320ceo)Tj /P <>BDC 7 0 0 7 355.3163 166.7654 Tm ET EMC BT /P <>BDC /P <>BDC BT ET ET 7 0 0 7 404.101 287.7654 Tm 0 Tc (O)Tj EMC EMC ( )Tj EMC BT /P <>BDC EMC 7 0 0 7 554.7883 397.7654 Tm EMC /P <>BDC /P <>BDC /P <>BDC BT EMC EMC BT 0 Tc /P <>BDC EMC EMC EMC (124,800)Tj 7 0 0 7 118.104 408.7654 Tm EMC ET ET /P <>BDC BT EMC ( )Tj .151 .147 .15 rg BT /P <>BDC BT EMC BT ET ET /P <>BDC (132,872)Tj ( )Tj BT BT /P <>BDC /F6 1 Tf /Artifact <>BDC BT BT 7 0 0 7 37.6993 122.9528 Tm EMC EMC 6.5 0 0 6.5 528.5291 676.9529 Tm ( )Tj ( )Tj ET ET /P <>BDC Specification Table Boeing 737 Original and Boeing 737 Classic (Top). ET /P <>BDC /P <>BDC The payload reduction is)Tj EMC ET EMC /P <>BDC 7 0 0 7 37.6993 166.9528 Tm 8 0 0 8 54.8194 760.9529 Tm EMC (297,312)Tj ET ( )Tj /P <>BDC ET BT /Artifact <>BDC The main wheel tyre pressures are 193-202, once again PSI. EMC 5.25 0 0 5.25 73.853 11.5132 Tm EMC 9 0 0 9 36.8504 60.8898 Tm -.02 Tc ( )Tj ET BT EMC 0 Tc ( )Tj -.01 Tc ET 7 0 0 7 337.6855 276.9528 Tm /P <>BDC EMC EMC EMC ET BT BT /P <>BDC /P <>BDC -.02 Tc EMC ET EMC ( )Tj BT /P <>BDC ET ET ET /P <>BDC /P <>BDC /P <>BDC EMC EMC ( )Tj 9 0 0 9 366.4417 533.8898 Tm ET BT BT (483)Tj BT (0.0113)Tj 8 0 0 8 302.5117 577.9528 Tm BT (scenario 2, which is based on an 85%)Tj 7 0 0 7 474.3564 595.9528 Tm ( )Tj 7 0 0 7 444.737 320.7654 Tm BT (the defined LRC speed, this has resulted in)Tj ( )Tj -.02 Tc ET EMC (economics of the aircraft types with more)Tj ET ET EMC BT EMC EMC EMC BT ET 0 Tc 7 0 0 7 537.7804 364.9528 Tm 6.5 0 0 6.5 528.5291 689.9529 Tm /P <>BDC /P <>BDC 0 841.89 609.449 -841.89 re ET BT 6 0 0 6 103.6577 715.9528 Tm BT 9 0 0 9 569.6968 346.8898 Tm ( )Tj [(AS)29(M)]TJ EMC /P <>BDC ( )Tj /P <>BDC /P <>BDC [(A3)24.9(20neo v)12.9(ersus 7)-33(3)8.1(7-8 )]TJ /P <>BDC 0 Tc ET BT BT 7 0 0 7 473.8245 243.9528 Tm EMC /Artifact <>BDC ET EMC EMC 0 Tc 7 0 0 7 247.7395 166.7654 Tm 0 Tc BT /P <>BDC BT -.02 Tc BT 0 841.89 609.449 -841.89 re EMC 9 0 0 9 552.5356 445.8898 Tm BT ET ET BT (The thrust ratings on the engines show)Tj ET (between different aircraft types impossible)Tj ( )Tj ET EMC The NG has 6 dripsticks in each wing tank and 4 in the centre The flight)Tj /P <>BDC /P <>BDC 9 0 0 9 411.0181 489.8898 Tm EMC ( )Tj /P <>BDC ET (A320neo)Tj BT 7 0 0 7 456.2165 221.7654 Tm From July 2004 NGs have been delivered with markings on the ET 7 0 0 7 82.2047 529.9528 Tm EMC 6 0 0 6 226.9834 757.9528 Tm )Tj the two components of the air are separated, the nitrogenenriched air (NEA) is )Tj ET ET -.02 Tc BT /P <>BDC 6 0 0 6 561.1918 715.9528 Tm 7 0 0 7 456.4753 573.7654 Tm BT (737-800W)Tj ET ( )Tj <>/XObject<>/ExtGState<>/Properties<>>> EMC EMC EMC EMC /P <>BDC -.02 Tc EMC EMC 7 0 0 7 539.8962 562.9528 Tm EMC ET /OC /MC208 BDC BT ( )Tj /P <>BDC 7 0 0 7 387.0159 518.9528 Tm q 1 0 0 1 215.431 128.878 cm 0 0 m EMC BT ET ( )Tj EMC /P <>BDC EMC 0 Tc
Victoria Gifford Kennedy Where Is She Now, Kfvs Election Results 2022, Articles OTHER