737 800 fuel capacity pounds
737 800 fuel capacity pounds
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0 Tc ET -.02 Tc BT ET 6.5 0 0 6.5 528.5291 702.9529 Tm BT ( )Tj EMC EMC /P <>BDC 9 0 0 9 215.4409 313.8898 Tm BT ET ET 0 Tc EMC BT -.02 Tc EMC 6.5 0 0 6.5 243.3486 742.9529 Tm ( )Tj (112)Tj 7 0 0 7 60.6117 144.7654 Tm ( )Tj ET ET /P <>BDC ET 0 Tc ( )Tj The Boeing 737-700 is a twin-engined short-to-medium-range narrowbody airliner with a capacity of maximum 149 passengers produced by the American manufacturer Boeing Commercial Airplanes. (ASM benefit over the A320ceo for the)Tj ET /P <>BDC EMC 0 Tc 6.5 0 0 6.5 192.0331 663.9529 Tm 9 0 0 9 394.0157 511.8898 Tm EMC EMC ET -.02 Tc 7 0 0 7 457.0984 287.7654 Tm 7 0 0 7 387.0159 507.9528 Tm /P <>BDC 9 0 0 9 189.8423 467.8898 Tm 0 Tc /P <>BDC BT ( )Tj BT /P <>BDC BT /P <>BDC ET BT BT BT /P <>BDC 0 Tc /P <>BDC (39,270)Tj EMC ET ET -.02 Tc ET EMC ET ET 7 0 0 7 520.6108 595.9528 Tm ( )Tj 7 0 0 7 158.74 364.7654 Tm ET /P <>BDC ET /P <>BDC (371,416)Tj BT /P <>BDC BT BT /P <>BDC The aircraft look like standard -800s, so why the difference? BT ( )Tj BT ( )Tj ( )Tj ET EMC ET ET /P <>BDC BT 7 0 0 7 258.2805 430.7654 Tm ( )Tj 8 0 0 8 141.7322 771.9528 Tm (10)Tj EMC ( )Tj ET 9 0 0 9 546.1516 203.8898 Tm 0 Tc EMC /P <>BDC ET EMC -.02 Tc BT BT /P <>BDC ET BT ET ( )Tj 0 Tc ET (operation the overflight and airport)Tj BT EMC /P <>BDC /P <>BDC They were solenoid held and BT /P <>BDC ET (and in fuel burn per ASM. 9 0 0 9 562.1829 236.8898 Tm 0 Tc /P <>BDC /P <>BDC BT -.02 Tc ET /P <>BDC ET 0 Tc /P <>BDC This would make)Tj The NGS requires no flight or ground crew action for normal system operation and is not dispatch critical. EMC 5.25 0 0 5.25 100.8225 11.5132 Tm ET on board for a late slot. ET /P <>BDC (. ET EMC EMC EMC EMC (150)Tj 7 0 0 7 82.2047 617.9528 Tm 6.5 0 0 6.5 224.5532 598.9529 Tm /P <>BDC BT BT )]TJ BT 7 0 0 7 427.7291 320.9528 Tm EMC BT /P <>BDC BT (31,416)Tj BT Just wondering, where did you get the information about what specific aluminium alloys are used on different parts of the aircraft? EMC -.02 Tc 8 0 0 8 241.2609 771.9528 Tm EMC ET ET (In this comparison the passenger seat)Tj BT 0 Tc ( )Tj EMC BT EMC (1,272)Tj ET ET EMC EMC /P <>BDC EMC BT EMC EMC ET /P <>BDC /P <>BDC ( )Tj 8 0 0 8 187.3427 661.9528 Tm 7 0 0 7 141.7322 276.9528 Tm ET EMC ET 9 0 0 9 537.6038 170.8898 Tm EMC ( )Tj ET EMC (5,394)Tj ( )Tj -.02 Tc /P <>BDC /P <>BDC EMC 9 0 0 9 411.0097 38.8898 Tm BT /P <>BDC BT Q ( )Tj EMC (5,350)Tj ET ET /P <>BDC (number of available seat-miles \(ASM\))Tj Hi Bradley, ET BT -.02 Tc ET 9 0 0 9 388.6428 357.8898 Tm ( )Tj ET ( )Tj (the IAE V2500. ( )Tj /P <>BDC BT ET ( )Tj ET /P <>BDC 8 0 0 8 136.4919 633.9528 Tm BT BT ET BT caused the FAA to issue SFAR88 in June 2001 which mandates improvements to the 0 Tc EMC 7 0 0 7 54.7071 419.7654 Tm BT ( )Tj BT ( )Tj .559 .331 .619 rg ET EMC EMC /P <>BDC 9 0 0 9 196.7724 412.8898 Tm BT /P <>BDC ( )Tj 10 0 0 10 417.91 814.1973 Tm BT Compared with the -400 the -800 is 3.02m (9ft 9in) longer, taking typical two class seating from 146 to 162, while range is significantly increased. /P <>BDC 9 0 0 9 212.7029 390.8898 Tm /P <>BDC (571)Tj /P <>BDC (Block time)Tj ET BT EMC ET BT BT BT EMC /P <>BDC LOW, CONFIG or IMBAL, Digital Fuel Quantity Indicator Error Codes (32,000lbs, down from the 33,000lbs that)Tj 7 0 0 7 241.5317 122.9528 Tm EMC (than the A321ceo. 5.25 0 0 5.25 447.6106 11.5129 Tm 7 0 0 7 474.3564 716.9528 Tm ET EMC /P <>BDC EMC /OC /MC1320 BDC BT 7 0 0 7 379.3969 221.7654 Tm (190,800)Tj 8 0 0 8 38.4438 689.9528 Tm ( )Tj (seats. EMC /P <>BDC BT /P <>BDC BT (410)Tj ET 0 Tc /P <>BDC EMC EMC ET 9 0 0 9 508.4714 38.8898 Tm EMC EMC ET -.01 Tc 0 Tc 7 0 0 7 82.2047 573.9528 Tm EMC 9 0 0 9 394.0123 126.8898 Tm /P <>BDC EMC BT .0161 Tc EMC 7 0 0 7 354.6933 408.7654 Tm (34,650)Tj EMC BT EMC ET BT /P <>BDC (31,416)Tj 7 0 0 7 36.8504 11.5129 Tm ET EMC BT ET BT (381)Tj ET 9 0 0 9 534.5925 753.8898 Tm /P <>BDC EMC /P <>BDC 0 Tc /F4 1 Tf /F1 1 Tf 7 0 0 7 490.8321 265.7654 Tm ET EMC ( )Tj 7 0 0 7 535.5029 397.7654 Tm (difference in fuel cost per ASM, however,)Tj [(E)-7.8(P)16.1(T)9(E)-13.9(MBE)-16.9(R)]TJ /P <>BDC -.02 Tc EMC The FAA Technical Center has determined that an oxygen level /P <>BDC (The aircraft are examined on the basis)Tj 7 0 0 7 241.5317 342.9528 Tm 0 Tc /P <>BDC /P <>BDC )Tj 0 Tc /P <>BDC /P <>BDC ET BT ET BT ET EMC 9 0 0 9 373.9277 478.8898 Tm 9 0 0 9 411.0181 192.8898 Tm ET -.02 Tc EMC BT 8 0 0 8 259.5105 675.9528 Tm ( )Tj ET ( )Tj ET 9 0 0 9 379.5817 577.8898 Tm /GS1 gs ET EMC ET Until its launch on September 5, 1994 the 737-800 was known as the 737-400X Stretch. /P <>BDC BT BT ET ( )Tj 7 0 0 7 445.619 375.7654 Tm /P <>BDC EMC EMC 0 Tc ET ( )Tj ( )Tj ET 9 0 0 9 232.4217 357.8898 Tm 7 0 0 7 403.478 474.7654 Tm /P <>BDC /P <>BDC 7 0 0 7 440.0906 342.9528 Tm /P <>BDC ET EMC EMC BT (airport. BT BT EMC ( )Tj /P <>BDC 9 0 0 9 394.0157 522.8898 Tm ( )Tj 6.5 0 0 6.5 332.0787 545.9529 Tm ET (5B3)Tj /P <>BDC 7 0 0 7 403.478 529.7654 Tm BT 7 0 0 7 387.0932 67.9528 Tm BT (be achieved. /P <>BDC ET Airbus A330 Specs What can this popular long haul twin jet do? EMC ET ET /P <>BDC 8 0 0 8 334.994 675.9528 Tm 7 0 0 7 279.1575 485.9528 Tm 7 0 0 7 491.4046 210.9528 Tm /P <>BDC ET EMC ET EMC ET -.02 Tc BT /P <>BDC BT (375)Tj 0 841.89 609.449 -841.89 re EMC EMC EMC BT BT ET EMC 9 0 0 9 394.0157 390.8898 Tm BT /Artifact <>BDC (2,517)Tj /F4 1 Tf ET EMC (1,058)Tj EMC EMC (CFM56-5B4/P)Tj (when using a cost index. EMC /P <>BDC BT ET ET /P <>BDC EMC (CFM LEAP-1B28B1 rated at 28,000lbs)Tj EMC ET 7 0 0 7 163.8846 11.5132 Tm BT ET 7 0 0 7 338.6433 243.7654 Tm /P <>BDC (410,271)Tj 7 0 0 7 54.7071 375.7654 Tm EMC EMC EMC ( )Tj ET ET 7 0 0 7 99.8582 320.7654 Tm 0 Tc (network. EMC BT BT [(BOS-SE)-13.9(A)]TJ ET -.02 Tc BT ET EMC BT Boeing 737-800 Aircraft type: Commercial airplane Manufacturer: Boeing Maiden flight year: 1997 I have flown in this plane Reports (16) Reviews (2) Photos (333) Forum (8) List of aircraft operators Boeing 737-800 Specifications ET EMC 7 0 0 7 298.1781 67.9528 Tm EMC 9 0 0 9 68.0071 159.8898 Tm /P <>BDC BT BT (payload reduction. ( )Tj ET /P <>BDC /P <>BDC ( )Tj 0 Tc (CFM56-7B26)Tj ET ( )Tj EMC 6 0 0 6 561.1317 771.9528 Tm /P <>BDC 9 0 0 9 394.0315 720.8898 Tm ET EMC ET /P <>BDC 0 Tc 0 J 0 j 5 w 10 M [] 0 d BT ( )Tj /P <>BDC The)Tj 9 0 0 9 367.3702 434.8898 Tm ET 734 0 obj 7 0 0 7 491.7142 606.7654 Tm (cost per ASM for a route is on the)Tj )Tj 9 0 0 9 53.8582 203.8898 Tm -.02 Tc 7 0 0 7 294.4014 122.7654 Tm EMC 7 0 0 7 439.4675 89.9528 Tm (152)Tj BT (207,336)Tj EMC 7 0 0 7 258.2805 265.7654 Tm BT 6.5 0 0 6.5 500.4875 532.9529 Tm ET -.02 Tc BT BT BT /P <>BDC EMC EMC That is because it is an 800. EMC /P <>BDC /P <>BDC ET 7 0 0 7 82.8504 111.9528 Tm /P <>BDC ET EMC 7 0 0 7 158.74 265.7654 Tm (0.0112)Tj 9 0 0 9 550.1644 170.8898 Tm ET BT ET -.02 Tc EMC EMC 9 0 0 9 232.4217 467.8898 Tm /P <>BDC 7 0 0 7 490.5101 705.9528 Tm /P <>BDC [(Alternate airpor)-23(t &)]TJ /P <>BDC (10)Tj /P <>BDC The advanced wing airfoil design provides an economical cruise speed of .789 Mach (530 mph) - compared to .745 Mach for earlier 737 models. -.02 Tc /P <>BDC BT BT BT ( )Tj BT ET BT 7 0 0 7 230.7317 89.9528 Tm 7 0 0 7 99.5912 705.9528 Tm EMC /P <>BDC 7 0 0 7 36.8504 11.5129 Tm 0 Tc ET BT 7 0 0 7 490.8321 199.7654 Tm EMC ET ET EMC 0 Tc ET (I)Tj 9 0 0 9 543.5425 522.8898 Tm BT 9 0 0 9 53.8338 247.8898 Tm EMC /P <>BDC EMC BT 0 Tc /P <>BDC /P <>BDC ET -.02 Tc .001 Tc /P <>BDC BT EMC 7 0 0 7 230.7317 485.9528 Tm BT /P <>BDC ( )Tj 0 Tc ET ET ET ET BT ET EMC BT BT -.01 Tc BT BT 7 0 0 7 490.5101 628.9528 Tm /P <>BDC ( )Tj BT ET ET ET BT EMC /P <>BDC /Artifact <>BDC EMC /P <>BDC EMC EMC EMC ET .151 .147 .15 rg /P <>BDC ET (0.0119)Tj BT EMC (space, thereby freeing up more floor area)Tj 0 Tc Cheers Peter. EMC /P <>BDC 9 0 0 9 232.438 291.8898 Tm /P <>BDC 0 Tc 7 0 0 7 537.7804 342.9528 Tm ET ( )Tj ( )Tj 0 Tc ( )Tj ( )Tj EMC ( )Tj BT 7 0 0 7 247.7395 309.7654 Tm 7 0 0 7 429.157 474.9528 Tm 7 0 0 7 158.74 727.7654 Tm .559 .331 .619 rg /P <>BDC 9 0 0 9 531.4232 159.8898 Tm 9 0 0 9 36.8504 225.8898 Tm ET BT EMC 6 0 0 6 490.4508 729.9528 Tm BT 7 0 0 7 520.6108 694.9528 Tm BT 7 0 0 7 539.9176 11.5129 Tm 9 0 0 9 408.1854 610.8898 Tm /P <>BDC ET EMC ( )Tj ET EMC 0 Tc /P <>BDC EMC 9 0 0 9 36.8504 258.8898 Tm EMC (passenger payload. EMC 7 0 0 7 37.0536 628.9528 Tm .661 .752 .896 rg /P <>BDC BT 7 0 0 7 107.1165 276.9528 Tm For the purposes of)Tj 7 0 0 7 241.5317 683.9528 Tm /P <>BDC 9 0 0 9 197.3398 214.8898 Tm 7 0 0 7 158.74 166.7654 Tm -.02 Tc ( )Tj 7 0 0 7 108.6215 441.9528 Tm 9 0 0 9 339.3695 192.8898 Tm ET /Figure <>BDC EMC .151 .147 .15 rg /F4 1 Tf ET ET BT ET /P <>BDC ( )Tj ( )Tj EMC /P <>BDC BT ( )Tj 9 0 0 9 229.6064 456.8898 Tm (152)Tj EMC 8 0 0 8 225.1837 745.9528 Tm BT EMC EMC ET /P <>BDC -.02 Tc ( )Tj .014984 841.89 609.45 -841.89 re ET ( )Tj EMC /P <>BDC ( )Tj (900ER and 737-9, A320ceo and A320neo,)Tj 9 0 0 9 198.3567 335.8898 Tm ( )Tj ET ( )Tj ET ET ET EMC BT /P <>BDC EMC ET EMC 7 0 0 7 294.4014 595.7654 Tm 8 0 0 8 38.4438 619.9528 Tm [(737-900E)-33(R\(W)-19(\):)]TJ 0 Tc /P <>BDC EMC -.02 Tc /P <>BDC /P <>BDC ( )Tj /P <>BDC ET ET ET EMC /P <>BDC 9 0 0 9 232.4217 93.8898 Tm (revenue benefit of 11 passengers. BT BT 7 0 0 7 193.1059 683.9528 Tm /P <>BDC /P <>BDC ( )Tj ET ET BT BT (The wind speed was based on an 85%)Tj /P <>BDC ET 7 0 0 7 158.74 122.7654 Tm BT BT EMC EMC ET ( )Tj In November 2005, Boeing unveiled the BBJ3, based on the 737-900ER. EMC ( )Tj 7 0 0 7 403.478 463.7654 Tm 7 0 0 7 82.2047 661.9528 Tm EMC 9 0 0 9 455.0733 60.8898 Tm ( )Tj ET ET (the aircraft operator, but in this evaluation)Tj BT /P <>BDC 8 0 0 8 124.845 591.9528 Tm /P <>BDC ET /P <>BDC 9 0 0 9 229.6141 302.8898 Tm ET ET 6.5 0 0 6.5 346.1424 545.9529 Tm 7 0 0 7 440.3636 540.9528 Tm 0 Tc /P <>BDC ( )Tj /P <>BDC /P <>BDC EMC 7 0 0 7 230.7317 419.9528 Tm /P <>BDC (737-900ER\(W\) has an MTOW of)Tj BT 7 0 0 7 554.7883 199.7654 Tm BT ET (It was assumed that all flights would)Tj BT ( )Tj ET /P <>BDC -.02 Tc ET 0 Tc (737-8)Tj ( )Tj 5.25 0 0 5.25 73.853 11.5132 Tm 7 0 0 7 141.7322 243.9528 Tm 9 0 0 9 394.0123 236.8898 Tm 6.5 0 0 6.5 399.2659 565.9529 Tm ET ET ET 6.5 0 0 6.5 280.3794 722.9529 Tm ET EMC ET The APU burns about 160Kgs/hr with electrics and an air-conditioning ( )Tj EMC ET 0 Tc BT ET (0.0160)Tj ET BT ET 9 0 0 9 342.0176 126.8898 Tm 9 0 0 9 394.0237 390.8898 Tm /F6 1 Tf EMC 6.5 0 0 6.5 426.4819 676.9529 Tm (component, while the 737-900ER\(W\) has)Tj .151 .147 .15 rg (0.0149)Tj BT ET /P <>BDC /P <>BDC -.02 Tc /P <>BDC BT BT (737-8)Tj (0.0112)Tj EMC -.02 Tc /P <>BDC (1,683)Tj The airliner was attempting to land at Amsterdams Schiphol Airport. /P <>BDC (carried - lbs)Tj ET BT /P <>BDC 6 0 0 6 372.3969 729.9528 Tm BT ET 7 0 0 7 439.2087 67.9528 Tm BT ET EMC 9 0 0 9 215.4409 500.8898 Tm EMC -.02 Tc EMC 0 Tc -.02 Tc BT (carried - lbs)Tj EMC 9 0 0 9 194.6103 401.8898 Tm .0081 Tc BT 9 0 0 9 215.4409 104.8898 Tm EMC 9 0 0 9 388.4178 49.8898 Tm EMC 9 0 0 9 539.8684 280.8898 Tm 0 Tc ET 7 0 0 7 299.0601 133.9528 Tm 0 Tc 9 0 0 9 36.8504 214.8898 Tm /P <>BDC (4,218)Tj ET ( )Tj BT 7 0 0 7 179.5605 122.9528 Tm 9 0 0 9 246.595 423.8898 Tm 9 0 0 9 232.4217 434.8898 Tm 9 0 0 9 360.5848 104.8898 Tm ( )Tj 7 0 0 7 294.4014 617.7654 Tm /P <>BDC EMC BT ET If you like us, please share with your followers. /P <>BDC -.02 Tc ( )Tj ET BT 9 0 0 9 191.0032 225.8898 Tm BT ET 6.5 0 0 6.5 426.4819 663.9529 Tm BT ET 6.5 0 0 6.5 346.7208 624.9529 Tm /P <>BDC EMC ET /F6 1 Tf /P <>BDC 7 0 0 7 444.737 133.7654 Tm (capacity, so that payload is reduced to)Tj W n BT /P <>BDC /OC /MC1976 BDC BT BT ET ET ( )Tj BT Main tanks < 50%, -1 to 5 deg pitch, +/- 1 deg roll: +/- 2.0 ET 8 0 0 8 187.3427 591.9528 Tm BT /P <>BDC ET BT (O)Tj /P <>BDC /P <>BDC BT BT /P <>BDC EMC -.02 Tc (A321ceo)Tj EMC endstream BT the two components of the air are separated, the nitrogenenriched air (NEA) is ET BT 0 Tc 7 0 0 7 456.2165 111.7654 Tm ET 9 0 0 9 394.0123 379.8898 Tm (3,021)Tj .151 .147 .15 rg /P <>BDC to the centre tank through a manual valve by cabin pressure. 9 0 0 9 536.1277 247.8898 Tm BT .0161 Tc 0 Tc ( )Tj (135,453)Tj ( )Tj EMC 7 0 0 7 82.8504 375.9528 Tm EMC EMC /P <>BDC BT ET 7 0 0 7 338.6433 430.7654 Tm 7 0 0 7 54.7071 232.7654 Tm BT (192)Tj EMC EMC EMC BT BT EMC 7 0 0 7 114.6416 397.9528 Tm ( )Tj EMC /P <>BDC BT /P <>BDC BT ( )Tj ( )Tj 0 Tc 10 0 0 10 422.8 814.1973 Tm ( )Tj /P <>BDC ET /P <>BDC /P <>BDC vlXf6.vlWfvlXyeb/k/+6**]CR$2T*+-t=* (&g@a};z53I$]I\+eSE_ >YXKt87^-+ L%!'W+6Q8P8s' ( )Tj EMC ET BT 0 Tc BT /P <>BDC 9 0 0 9 68.0314 302.8898 Tm /P <>BDC 7 0 0 7 439.2087 144.9528 Tm BT ( )Tj EMC According to Boeing.com, the 737-600/-700/-800/-900ER models have a maximum fuel capacity of 6,875 gallons. /P <>BDC BT [(CFM L)17.1(E)-8.1(AP-1A32)]TJ /P <>BDC (388)Tj ET ( )Tj ET ET Q (172,992)Tj /P <>BDC 0 Tc ET EMC 6.5 0 0 6.5 549.8557 676.9529 Tm EMC BT ET 10 0 0 10 49.3644 814.1973 Tm 9 0 0 9 182.0906 467.8898 Tm BT (163)Tj /P <>BDC EMC EMC <>stream /P <>BDC EMC 6.5 0 0 6.5 448.257 637.9529 Tm (shorter sectors. BT /P <>BDC /P <>BDC /P <>BDC ET (170)Tj BT ET (improvement of 17.7% compared to the)Tj EMC 9 0 0 9 369.406 104.8898 Tm 9 0 0 9 548.4747 115.8898 Tm BT 8 0 0 8 302.5117 619.9528 Tm ( )Tj ET 9 0 0 9 421.0664 401.8898 Tm -.02 Tc 7 0 0 7 338.5674 122.9528 Tm /P <>BDC /P <>BDC ET BT /P <>BDC 7 0 0 7 379.3969 78.7654 Tm -.02 Tc 7 0 0 7 279.1575 243.9528 Tm ET BT EMC 7 0 0 7 199.5784 243.7654 Tm ET 7 0 0 7 297.632 540.9528 Tm EMC EMC /P <>BDC EMC EMC BT BT 7 0 0 7 338.6433 287.7654 Tm ( )Tj BT ( )Tj (passenger payload. ( )Tj 7 0 0 7 54.7071 111.7654 Tm ( )Tj ET 7 0 0 7 158.74 78.7654 Tm BT EMC 7 0 0 7 108.6215 628.9528 Tm /P <>BDC ( )Tj BT ET 6.5 0 0 6.5 273.8079 676.9529 Tm ET EMC ET EMC BT EMC ET -.02 Tc (reducing their in-flight service offering, this)Tj 6 0 0 6 184.0127 771.9528 Tm EMC /P <>BDC EMC BT ET 0 Tc )Tj BT ( )Tj /P <>BDC (evaluation that are payload-limited on the)Tj ET /P <>BDC ET 6.5 0 0 6.5 375.6529 689.9529 Tm (greater improvement in fuel burn on the)Tj /P <>BDC BT -.02 Tc EMC BT /P <>BDC EMC BT 0 Tc (136)Tj EMC BT /P <>BDC EMC BT /P <>BDC EMC (A320neo)Tj BT on 5 Nov 1990 have been destroyed on the ground due to explosions in the empty ET BT BT BT BT ET (1,272)Tj [(looks at the performance of eight Airbus and Boeing narr)10(o)12(wbody types)]TJ ET EMC ET (A321ceo, in contrast to the A320neo over)Tj (A320ceo)Tj 0 Tc /P <>BDC 8 0 0 8 163.4218 771.9529 Tm EMC /P <>BDC EMC ET BT BT ET EMC EMC EMC /P <>BDC ( )Tj 0 Tc 9 0 0 9 36.8504 236.8898 Tm ET ( )Tj -.02 Tc EMC /P <>BDC ( )Tj /P <>BDC -.01 Tc -9.719 805.04 386.723 -270.624 re /P <>BDC BT ( )Tj BT BT 0 Tc 6 0 0 6 146.7028 743.9528 Tm (doors configuration. ( )Tj (I)Tj BT BT EMC /P <>BDC /P <>BDC BT 0 Tc BT ET -.02 Tc -.02 Tc /P <>BDC EMC (31,416)Tj 9 0 0 9 551.0015 291.8898 Tm ( )Tj /P <>BDC BT 9 0 0 9 543.1465 511.8898 Tm 8 0 0 8 471.0755 760.9528 Tm EMC EMC /F2 1 Tf ET 0 Tc EMC BT 5 0 0 5 92.725 11.5132 Tm BT EMC ET EMC BT EMC (or scenarios in this study. unit, Open or short in ET BT /P <>BDC 9 0 0 9 299.3893 478.8898 Tm 6.5 0 0 6.5 295.8145 611.9529 Tm ET 7 0 0 7 491.4046 408.9528 Tm /P <>BDC ET ET ET 7 0 0 7 88.196 11.5129 Tm /P <>BDC ET .1202 .4955 .3052 1.277 y [(UG)-17.1(U)-8(S)8.1(T)]TJ /P <>BDC -.02 Tc (10)Tj BT ET BT EMC 7 0 0 7 125.6292 628.7654 Tm /P <>BDC 6 0 0 6 236.6735 673.9528 Tm EMC -.02 Tc /P <>BDC ( )Tj ( )Tj /P <>BDC EMC EMC 9 0 0 9 197.7229 522.8898 Tm BT EMC /P <>BDC 7 0 0 7 554.7883 122.7654 Tm /P <>BDC ( )Tj /Artifact <>BDC /P <>BDC BT EMC ( )Tj /P <>BDC /P <>BDC BT EMC 7 0 0 7 508.4124 221.7654 Tm 9 0 0 9 394.0123 478.8898 Tm (482)Tj BT BT 7 0 0 7 537.7804 144.9528 Tm ET 7 0 0 7 474.7064 276.9528 Tm ET (On the sectors where the A321ceo and)Tj ET EMC ET EMC BT ET /P <>BDC -.01 Tc ( )Tj /P <>BDC 8 0 0 8 187.3427 703.9528 Tm ET /GS1 gs EMC ET 7 0 0 7 338.5674 166.9528 Tm ET (\(see table, this)Tj BT ET ET 7 0 0 7 298.1781 111.9528 Tm BBJ style winglets are offered as an optional feature for the -800. /P <>BDC (1,091)Tj /P <>BDC EMC ( )Tj ( )Tj (172,992)Tj (I)Tj /P <>BDC ( )Tj BT 7 0 0 7 258.2805 529.7654 Tm EMC (158)Tj EMC EMC EMC -.02 Tc /P <>BDC BT (performance. BT EMC BT /P <>BDC EMC 7 0 0 7 258.2805 672.7654 Tm 7 0 0 7 445.7203 11.5129 Tm ET EMC ET EMC ET EMC 0 Tc EMC 7 0 0 7 37.8848 452.9528 Tm The same alternate airport was)Tj (As with the comparison of the)Tj BT 0 Tc EMC 9 0 0 9 553.271 434.8898 Tm (airport charges, while the time-dependent)Tj 0 Tc 10 0 0 10 54.2544 814.1973 Tm (comparative performance. 7 0 0 7 54.7071 221.7654 Tm /P <>BDC 9 0 0 9 126.1392 522.8898 Tm 0 Tc ET 9 0 0 9 369.3136 698.8898 Tm ( )Tj /P <>BDC BT ( )Tj 9 0 0 9 411.0181 269.8898 Tm BT ( )Tj ET EMC 9 0 0 9 53.8578 434.8898 Tm I found this image that might have some of the answers you need. ( )Tj EMC ( )Tj /P <>BDC )Tj 9 0 0 9 197.3123 379.8898 Tm 7 0 0 7 99.8582 738.7654 Tm 7 0 0 7 537.7804 364.9528 Tm 6 0 0 6 226.9834 757.9528 Tm ET BT BT ( )Tj /P <>BDC (\(see table, page 19\))Tj /P <>BDC -.02 Tc ET ( )Tj /P <>BDC /P <>BDC (377,550)Tj ( )Tj ET EMC ET ( )Tj /P <>BDC BT BT BT ET (or any airborne or ground delays. (. /P <>BDC EMC 9 0 0 9 571.3269 38.8898 Tm BT ET EMC /P <>BDC 9 0 0 9 232.438 225.8898 Tm BT 6 0 0 6 506.5237 757.9528 Tm BT BT /P <>BDC (4,615)Tj 7 0 0 7 130.1443 716.7654 Tm ET /P <>BDC /P <>BDC BT 9 0 0 9 246.6113 71.8898 Tm /P <>BDC EMC ( )Tj EMC -.02 Tc 9 0 0 9 252.5189 181.8898 Tm ( )Tj /P <>BDC EMC 0 Tc 7 0 0 7 445.619 540.7654 Tm /F1 1 Tf EMC BT 7 0 0 7 99.8582 144.7654 Tm The 737-9 has a)Tj ET BT /P <>BDC /P <>BDC 9 0 0 9 515.4913 555.8898 Tm [(OM)8(M)-13(E)-25(R)7(C)8(E)]TJ 0 Tc BT BT BT /P <>BDC 8 0 0 8 302.5117 717.9528 Tm )Tj 7 0 0 7 326.2278 694.9528 Tm 0 Tc BT BT /P <>BDC BT ET /GS1 gs 6.5 0 0 6.5 192.5726 722.9529 Tm ( )Tj EMC /P <>BDC ET ET /P <>BDC /P <>BDC 9 0 0 9 408.2047 93.8898 Tm ( )Tj ET EMC EMC BT 7 0 0 7 70.8101 243.9528 Tm [(AIRL)8.1(INE & AIR)7.1(CRAF)-12.9(T)18.1( OPERA)56.9(T)-8.1(ION)-13.9(S)]TJ BT BT EMC ET ET BT BT BT EMC ( )Tj ( )Tj /P <>BDC /P <>BDC EMC BT /P <>BDC /P <>BDC 0 Tc ET 9 0 0 9 36.8504 38.8898 Tm ( )Tj EMC 7 0 0 7 354.4763 727.7654 Tm ET /P <>BDC (lower fuel burn compared to the 737-)Tj BT BT /P <>BDC 10 0 0 10 36.8504 814.1973 Tm ET (financing. 0 Tc 9 0 0 9 190.2832 49.8898 Tm EMC ET ET 0 Tc /F8 1 Tf /P <>BDC (39,270)Tj /P <>BDC -.02 Tc /P <>BDC BT 7 0 0 7 247.7395 716.7654 Tm -.02 Tc 0 Tc (486)Tj /P <>BDC /P <>BDC (31,416)Tj EMC 6 0 0 6 268.0069 701.9528 Tm 9 0 0 9 394.0123 313.8898 Tm 10 0 0 10 359.2822 794.2914 Tm 9 0 0 9 394.0157 610.8898 Tm ET BT /P <>BDC BT EMC (0.0113)Tj BT BT ET (These are the 737-800 and 737-8, 737-)Tj 5.25 0 0 5.25 465.7151 11.5129 Tm BT /P <>BDC 9 0 0 9 195.231 423.8898 Tm (737-800:)Tj /P <>BDC ET ( )Tj BT /P <>BDC ET ability of GBI to reduce fuel tank flammability. S ( )Tj 7 0 0 7 99.5912 485.9528 Tm /P <>BDC /P <>BDC Boeing 737 History, the story behind this hugely successful City Jet. EMC EMC 9 0 0 9 542.4784 115.8898 Tm BT .023 .567 .626 rg ET [(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 7 0 0 7 279.1575 309.9528 Tm EMC EMC /P <>BDC ET /P <>BDC ET (282-294)Tj 7 0 0 7 99.8582 232.7654 Tm ( )Tj 13 0 0 13 340.4557 467.8898 Tm ( )Tj 8 0 0 8 394.0157 775.8898 Tm (190,800)Tj 9 0 0 9 195.4853 126.8898 Tm 7 0 0 7 457.0984 298.7654 Tm ET EMC in later aircraft). BT 7 0 0 7 456.2165 375.7654 Tm BT /P <>BDC 7 0 0 7 141.7322 441.9528 Tm /P <>BDC (the relative fuel costs between the aircraft)Tj ( )Tj (aircraft operators fly their aircraft based on)Tj 7 0 0 7 77.36 11.5132 Tm ET ET EMC BT 9 0 0 9 359.0967 786.8898 Tm ET BT EMC BT centre fuel tanks. EMC 7 0 0 7 473.8245 67.9528 Tm BT ET ET BT EMC BT ( )Tj With the tapering of the aircraft nose, it is hard to give any one clear answer. EMC ( )Tj BT BT 0 Tc 9 0 0 9 394.0157 313.8898 Tm 9 0 0 9 212.5107 313.8898 Tm BT BT /P <>BDC BT (214)Tj (160)Tj ET 0 Tc ET /P <>BDC ( )Tj /P <>BDC ET 7 0 0 7 403.478 540.7654 Tm ET ET 6 0 0 6 246.9464 659.9528 Tm BT BT ( )Tj /P <>BDC BT /P <>BDC /P <>BDC BT Note: The gauges are still considered to be operating normally with BT BT BT 9 0 0 9 36.8504 247.8898 Tm EMC /P <>BDC 6.5 0 0 6.5 335.5237 532.9529 Tm EMC EMC BT EMC ET BT /P <>BDC 0 Tc ET (150)Tj EMC 7 0 0 7 107.1165 562.9528 Tm BT EMC 6.5 0 0 6.5 243.7903 611.9529 Tm 7 0 0 7 247.7395 386.7654 Tm (The 737-9 has an 11.2% to 12.7%)Tj ( )Tj /P <>BDC -.02 Tc 0 Tc BT (2,517)Tj (A320neo:)Tj /P <>BDC BT EMC ET Perhaps somebody has experience in shipment of landing gear. BT /P <>BDC -.02 Tc EMC EMC EMC ET ( )Tj EMC ( )Tj Main tanks < 50%, -1 to 5 deg pitch, +/- 1 deg roll: +/- 1.0% ET ET ( )Tj EMC 9 0 0 9 68.0071 357.8898 Tm ET /P <>BDC BT /P <>BDC BT BT ( )Tj )Tj /P <>BDC 9 0 0 9 53.8582 225.8898 Tm ( )Tj EMC EMC ET EMC ( )Tj EMC EMC BT /P <>BDC (and the 737 MAX family with the CFM)Tj ET ET BT (38,168)Tj (A)Tj /P <>BDC 0 Tc 6.5 0 0 6.5 539.6182 532.9529 Tm 0 Tc BT -.02 Tc /P <>BDC 9 0 0 9 555.1324 148.8898 Tm ( )Tj EMC <> EMC ET 9 0 0 9 53.8582 390.8898 Tm 7 0 0 7 355.3163 320.7654 Tm 7 0 0 7 456.2165 474.7654 Tm -.02 Tc 9 0 0 9 411.0234 698.8898 Tm EMC 7 0 0 7 37.6993 331.9528 Tm EMC EMC EMC ET BT 0 Tc BT BT /P <>BDC ET 6 0 0 6 507.2798 715.9528 Tm ET EMC S ( )Tj EMC EMC ET EMC ET ( )Tj 7 0 0 7 386.4701 89.9528 Tm 9 0 0 9 215.433 71.8898 Tm .023 .567 .626 rg ET ( )Tj 7 0 0 7 241.5317 529.9528 Tm ET /P <>BDC EMC ET EMC BT (which could reduce this difference. BT BT 8 0 0 8 474.6331 771.7654 Tm ET /P <>BDC /P <>BDC /P <>BDC BT ET EMC BT EMC 7 0 0 7 247.7395 331.7654 Tm EMC 7 0 0 7 508.4124 78.7654 Tm /P <>BDC ( )Tj 7 0 0 7 520.6108 485.9528 Tm BT /P <>BDC 7 0 0 7 108.6215 540.9528 Tm ET The 737-8 offers)Tj ET /P <>BDC ( )Tj 9 0 0 9 392.5848 379.8898 Tm ET ET BT [(737-900E)-33(R)]TJ BT BT /P <>BDC 9 0 0 9 207.5339 280.8898 Tm 9 0 0 9 485.5482 500.8898 Tm 7 0 0 7 193.1059 188.9528 Tm (141,757)Tj /P <>BDC 529.065 38.307 m /P <>BDC 6.5 0 0 6.5 540.4371 611.9529 Tm /F6 1 Tf BT 9 0 0 9 408.1854 159.8898 Tm 0 Tc EMC 0 Tc /P <>BDC /F4 1 Tf 0 Tc BT ET 9 0 0 9 53.8582 643.8898 Tm ( )Tj .014984 841.89 609.45 -841.89 re -.02 Tc BT ( )Tj ET (\(Miami\) sector, to 299 degrees on the)Tj ET 7 0 0 7 427.7291 100.9528 Tm /P <>BDC (560)Tj ET ET EMC 7 0 0 7 99.8582 111.7654 Tm ET (A320, the A321 neo is significantly heavier)Tj Boeing 737 MAX 9 pictures, specifications, cabin configuration. (4,514)Tj 7 0 0 7 125.6292 232.7654 Tm EMC BT /P <>BDC ET EMC 7 0 0 7 124.1242 397.7654 Tm ET BT EMC -.02 Tc EMC 6 0 0 6 309.2404 715.9528 Tm EMC EMC /P <>BDC https://www.markuspilot.com/download/BOEING%20737%20MEASUREMENTS.pdf, Perhaps you will build a cockpit and use it with the new Flight Sim 2020. 7 0 0 7 343.2355 474.7654 Tm 7 0 0 7 520.6108 540.9528 Tm ( )Tj S /P <>BDC ( )Tj BT /P <>BDC /P <>BDC BT These sectors)Tj EMC BT [(A3)24.9(21neo)]TJ EMC ET 6 0 0 6 132.3631 659.9528 Tm (payload is carried. /P <>BDC ET EMC /P <>BDC BT /P <>BDC /P <>BDC endobj /P <>BDC /P <>BDC BT EMC /P <>BDC BT ET (170)Tj .014984 824.882 572.583 17.008 re BT /P <>BDC EMC ( )Tj ET ET ( )Tj ET ET ET 0 Tc 6 0 0 6 309.5222 701.9528 Tm EMC 7 0 0 7 380.2788 474.7654 Tm BT /P <>BDC EMC EMC EMC /P <>BDC BT /P <>BDC BT ET 7 0 0 7 279.1575 727.9528 Tm ET 9 0 0 9 394.0157 434.8898 Tm ( )Tj 9 0 0 9 511.3603 412.8898 Tm /P <>BDC 7 0 0 7 427.7291 210.9528 Tm BT ( )Tj EMC 7 0 0 7 204.0935 276.7654 Tm BT /P <>BDC BT BT BT 9 0 0 9 511.9579 335.8898 Tm BT EMC ET /P <>BDC EMC 789 0 obj 9 0 0 9 555.4203 346.8898 Tm (34,650)Tj EMC ET 9 0 0 9 187.5717 126.8898 Tm /P <>BDC (977)Tj EMC -.02 Tc ( )Tj ( )Tj /P <>BDC /P <>BDC 9 0 0 9 165.5977 478.8898 Tm EMC f ET /P <>BDC (with a thrust rating of 26,000lbs, an intake)Tj /P <>BDC ( )Tj -.02 Tc ET BT ET ET 9 0 0 9 53.8578 313.8898 Tm EMC EMC (371,416)Tj 680kg; All other series: 453kg, Main tanks to be full if centre contains over 453kg, If a fuel gauge is u/s the quantity BT /P <>BDC ET /P <>BDC BT /P <>BDC BT BT ( )Tj ET -.02 Tc /P <>BDC EMC Q 7 0 0 7 199.5784 342.7654 Tm ALERT light illuminates on the main panel. 6.5 0 0 6.5 376.7644 742.9529 Tm BT BT ( )Tj ET 7 0 0 7 247.7395 595.7654 Tm BT 7 0 0 7 517.6133 78.9528 Tm BT EMC BT ET EMC BT ET EMC ( )Tj -.01 Tc EMC ET /P <>BDC /P <>BDC ET EMC 7 0 0 7 508.4124 199.7654 Tm ( )Tj (170)Tj 9 0 0 9 392.7317 742.8898 Tm BT ET 9 0 0 9 391.7137 104.8898 Tm BT ( )Tj 9 0 0 9 112.6132 302.8898 Tm [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ 7 0 0 7 491.7142 408.7654 Tm The cockpit is a dual seat design. /P <>BDC (CFM56-5B3/P)Tj 432 0 obj /OC /MC5061 BDC (140-148)Tj EMC 0 Tc ET /F1 1 Tf ET /P <>BDC EMC /P <>BDC ET /P <>BDC 7 0 0 7 404.101 276.7654 Tm The analysis, however,)Tj ET 7 0 0 7 539.8962 738.9528 Tm BT ( )Tj 0 Tc /P <>BDC -.02 Tc of gauges. EMC (37,416)Tj /P <>BDC BT BT EMC /P <>BDC 7 0 0 7 381.1608 595.7654 Tm EMC -.02 Tc /P <>BDC EMC The fuel was fed /P <>BDC 7 0 0 7 87.8179 441.7654 Tm BT EMC Boeing 787 Dreamliner Orders and Deliveries. Any help would be greatly appreciated and thank you for all your work its extremely helpful! BT BT BT ( )Tj ET ( )Tj /P <>BDC 9 0 0 9 394.0123 577.8898 Tm EMC EMC /P <>BDC ( )Tj EMC /P <>BDC BT /P <>BDC (other seven aircraft types. 6 0 0 6 195.6824 659.9528 Tm q (bypass ratio than the A320/321neo. 9 0 0 9 394.0123 621.8898 Tm ET BT /P <>BDC ( )Tj 0 Tc BT ET ET (170)Tj ET /P <>BDC -.01 Tc 5.25 0 0 5.25 549.1047 11.5132 Tm /P <>BDC 9 0 0 9 469.0061 423.8898 Tm EMC BT -.02 Tc ( )Tj ET ( )Tj ET #"""#'''''''''' EMC /P <>BDC BT EMC (20)Tj ET /P <>BDC /P <>BDC /P <>BDC ET BT [(R)13.9(ange with full)]TJ EMC EMC ET 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. [(737-900E)-33(R)]TJ BT /P <>BDC BT /P <>BDC /P <>BDC /P <>BDC 7 0 0 7 326.2278 463.9528 Tm 9 0 0 9 232.4217 82.8898 Tm BT Irkut MC-21, Russias homegrown modern airliner. 7 0 0 7 316.0679 408.7654 Tm BT /P <>BDC /P <>BDC 26.0355 0 TD 9 0 0 9 193.0552 434.8898 Tm The main wheel tyre pressures are 193-202, once again PSI. -.02 Tc /P <>BDC [(CFM L)17.1(E)-8.1(AP-1A26)]TJ (Like the A321neo, the 737-9 has a)Tj ET 304.725 420.96 m 7 0 0 7 321.6356 89.9528 Tm /P <>BDC /P <>BDC EMC ET (3,078)Tj ( )Tj ET BT 7 0 0 7 354.4763 672.7654 Tm /P <>BDC -.02 Tc ( )Tj -.01 Tc /P <>BDC /P <>BDC BT ET EMC /P <>BDC ET EMC /P <>BDC /P <>BDC 9 0 0 9 394.0237 467.8898 Tm EMC BT BT ET 7 0 0 7 354.6933 474.7654 Tm BT -.02 Tc EMC 7 0 0 7 141.7322 342.9528 Tm EMC (0.0157)Tj EMC (second payload scenario using the 85%)Tj BT BT BT ET EMC ( )Tj 137 )Tj EMC ET ET BT EMC BT 0 Tc (0.0130)Tj BT (CFM56-5B4/P)Tj /P <>BDC (72,450)Tj BT 0 Tc ET - 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. ( )Tj BT /P <>BDC /P <>BDC /P <>BDC EMC /P <>BDC BT /P <>BDC EMC ( )Tj EMC ET EMC 8 0 0 8 394.0157 797.8898 Tm 0 Tc ET ET ET BT 9 0 0 9 73.1083 511.8898 Tm (0.0177)Tj 9 0 0 9 68.0071 291.8898 Tm BT EMC ( )Tj EMC 9 0 0 9 177.8457 82.8898 Tm ( )Tj EMC BT EMC ( )Tj EMC 0 Tc BT (10)Tj (CFM56-5B4/P)Tj EMC EMC EMC 7 0 0 7 241.5317 408.9528 Tm ET /P <>BDC 28.5749 0 TD BT /P <>BDC 10 0 0 10 38.6761 771.9528 Tm EMC BT What is the History behind the Airbus A380 Super Jumbo? /P <>BDC -.02 Tc BT ( )Tj EMC (CFM56-5B3/P)Tj BT /P <>BDC EMC 7 0 0 7 82.2047 595.9528 Tm 0 841.89 609.449 -841.89 re EMC 7 0 0 7 387.0932 342.9528 Tm EMC ET BT -.02 Tc EMC 6 0 0 6 561.1918 715.9528 Tm BT 9 0 0 9 215.4409 423.8898 Tm /P <>BDC 9 0 0 9 394.0157 456.8898 Tm ET ( )Tj ET EMC /P <>BDC /P <>BDC /P <>BDC EMC ( )Tj BT BT EMC 7 0 0 7 520.6108 661.9528 Tm ( )Tj EMC EMC 6.5 0 0 6.5 324.4345 650.9529 Tm /P <>BDC More Economical Dash Speed Capacity; Lower Landing . .0081 Tc BT BT (737-800W)Tj )Tj ET /P <>BDC EMC /P <>BDC EMC 9 0 0 9 232.4217 324.8898 Tm 6.5 0 0 6.5 484.6315 585.9529 Tm EMC /P <>BDC )Tj ET 7 0 0 7 381.1608 573.7654 Tm /OC /MC2287 BDC -.02 Tc 9 0 0 9 565.1979 478.8898 Tm EMC 9 0 0 9 229.6064 49.8898 Tm EMC 7 0 0 7 37.5838 144.9528 Tm ( )Tj ( )Tj However, it was also shown that the dual venting configuration of some ( )Tj 9 0 0 9 394.0123 137.8898 Tm /Figure <>BDC ET 9 0 0 9 363.4443 390.8898 Tm EMC ET /P <>BDC /P <>BDC (cost of aviation fuel increases the operating)Tj 7 0 0 7 355.3163 122.7654 Tm ET 0 Tc ET ET 0 Tc BT EMC EMC 7 0 0 7 60.6117 639.7654 Tm EMC ET 9 0 0 9 189.3204 324.8898 Tm ( )Tj EMC The A320neo in this study)Tj ET BT 0 Tc (2,347)Tj
737 800 fuel capacity pounds