737 800 fuel capacity pounds737 800 fuel capacity pounds

ET EMC EMC /P <>BDC ET /P <>BDC ET Low fuel quantity indication illuminates below BT 6 0 0 6 295.8268 673.9528 Tm )Tj EMC BT 7 0 0 7 539.8962 628.9528 Tm BT ET /P <>BDC 7 0 0 7 99.8582 639.7654 Tm [(Aircr)10(aft)]TJ BT BT ET EMC ( )Tj ET EMC (even though the two have the same)Tj BT /P <>BDC /P <>BDC EMC BT -.02 Tc EMC ET EMC EMC EMC ET EMC BT 0 Tc /P <>BDC ET /P <>BDC /P <>BDC ( The time spent in potential holding)Tj ET /P <>BDC 7 0 0 7 387.619 430.9528 Tm ET EMC -.02 Tc ET /P <>BDC /P <>BDC /F6 1 Tf ( )Tj 0 Tc EMC 9 0 0 9 364.9498 511.8898 Tm (-47)Tj /P <>BDC 0 Tc EMC ET 9 0 0 9 188.8887 60.8898 Tm ET /P <>BDC /P <>BDC /P <>BDC ET (148,592)Tj endobj EMC 10 0 0 10 54.8804 814.1973 Tm ( )Tj (materials. BT ( )Tj ET EMC EMC -.02 Tc /P <>BDC -.02 Tc BT BT ( )Tj /P <>BDC 6.5 0 0 6.5 549.8557 702.9529 Tm 0 Tc ( )Tj /P <>BDC .661 .752 .896 rg 7 0 0 7 230.7317 122.9528 Tm /P <>BDC 9 0 0 9 411.0097 533.8898 Tm (977)Tj (1,272)Tj ET 9 0 0 9 258.18 60.8898 Tm EMC ( )Tj /P <>BDC ET ( )Tj 7 0 0 7 440.3636 474.9528 Tm EMC 7 0 0 7 490.8321 540.7654 Tm BT /P <>BDC BT 9 0 0 9 546.9705 291.8898 Tm BT BT 7 0 0 7 507.7893 507.7654 Tm /P <>BDC ET /P <>BDC BT ET ET ( )Tj /P <>BDC /P <>BDC BT (31,416)Tj ( )Tj BT -.02 Tc (72,450)Tj BT 9 0 0 9 232.438 181.8898 Tm ( )Tj EMC /P <>BDC ET -.02 Tc 8 0 0 8 412.41 771.9529 Tm 0 Tc ET BT /P <>BDC ( )Tj ET ET EMC 0 Tc EMC ET BT each aircraft is sourced from different places. EMC EMC 0 Tc ET (3,535)Tj /P <>BDC BT BT ET (150)Tj ( )Tj -.02 Tc BT EMC 7 0 0 7 124.1242 595.7654 Tm ( )Tj /P <>BDC -.02 Tc EMC EMC EMC ( )Tj q 1 0 0 1 215.433 480.878 cm 0 0 m 9 0 0 9 552.6886 533.8898 Tm BT EMC EMC EMC ET EMC /P <>BDC EMC BT 9 0 0 9 394.0237 423.8898 Tm BT ( )Tj ( )Tj /P <>BDC /P <>BDC BT ( )Tj ( )Tj ET BT EMC 0 Tc EMC (3,031)Tj (A higher engine bypass ratio will result)Tj BT [(I)-33(R)-1(C)7.1(RAF)-21(T)]TJ 7 0 0 7 491.4046 89.9528 Tm 9 0 0 9 344.8161 214.8898 Tm EMC EMC 7 0 0 7 279.1575 485.9528 Tm /P <>BDC ET We dont actually have access to a table of these variants and their features. 7 0 0 7 141.7322 573.9528 Tm -.02 Tc EMC /P <>BDC BT 9 0 0 9 356.4538 258.8898 Tm BT ET /P <>BDC [(P)11(ayload scenario two)]TJ EMC 7 0 0 7 473.8245 375.9528 Tm 6 0 0 6 496.9595 715.9528 Tm (737-9)Tj EMC W n 9 0 0 9 566.5558 544.8898 Tm (evaluate the relative performance of these)Tj BT ( )Tj /P <>BDC BT (economy-plus seats typically offer two to)Tj )Tj EMC 7 0 0 7 491.7142 331.7654 Tm /P <>BDC (A320neo)Tj ( )Tj 7 0 0 7 204.0935 375.7654 Tm BT BT /P <>BDC /P <>BDC EMC EMC BT BT EMC 0 Tc EMC 9 0 0 9 408.1968 159.8898 Tm 9 0 0 9 53.8582 478.8898 Tm )Tj 7 0 0 7 491.4046 397.9528 Tm 7 0 0 7 457.0984 298.7654 Tm ET EMC BT 0 Tc 6.5 0 0 6.5 244.0438 722.9529 Tm /P <>BDC /P <>BDC 9 0 0 9 547.562 126.8898 Tm 9 0 0 9 408.2047 489.8898 Tm (Max payload - lbs)Tj BT EMC /Artifact <>BDC EMC ( )Tj (1,161)Tj 7 0 0 7 363.2711 562.9528 Tm /P <>BDC BT 0 Tc 0 Tc 7 0 0 7 187.0858 408.9528 Tm 7 0 0 7 247.7395 496.7654 Tm ET /P <>BDC ET ET When this runs dry the scavenge ( )Tj EMC y9ou may find what you are looking for by clicking here. ET how can i know the material of 737NGs nose landing gear lower drag strut?thank you. (170)Tj It has a maximum range of 10,140km. ET EMC BT (150)Tj 9 0 0 9 36.8504 137.8898 Tm (0.0112)Tj BT /P <>BDC 9 0 0 9 203.484 192.8898 Tm /P <>BDC ( )Tj .534 .14 .504 RG (. EMC BT ( )Tj EMC ( )Tj ET BT 9 0 0 9 232.438 126.8898 Tm -.02 Tc ET /P <>BDC /P <>BDC -.02 Tc ( )Tj EMC /P <>BDC The FILTER BYPASS EMC /P <>BDC 6 0 0 6 226.9834 757.9528 Tm BT EMC EMC ( )Tj 9 0 0 9 394.0123 269.8898 Tm ( )Tj /P <>BDC 9 0 0 9 411.0097 148.8898 Tm EMC /P <>BDC BT BT The aircraft broke into 3 pieces after crashing. /P <>BDC 9 0 0 9 411.0097 93.8898 Tm /P <>BDC 7 0 0 7 428.6112 386.9528 Tm /OC /MC3431 BDC ET /P <>BDC EMC ET EMC /P <>BDC 7 0 0 7 539.8962 529.9528 Tm /P <>BDC EMC (39,270)Tj /P <>BDC EMC 7 0 0 7 279.1575 232.9528 Tm BT ( )Tj 9 0 0 9 552.9465 302.8898 Tm EMC /P <>BDC BT EMC 6.5 0 0 6.5 381.6589 624.9529 Tm This maybe? BT ( )Tj BT ( )Tj BT BT ET /P <>BDC ( )Tj -.02 Tc /P <>BDC 7 0 0 7 179.5605 221.9528 Tm /P <>BDC ET ET -.02 Tc (/S)Tj BT /P <>BDC ET 6 0 0 6 322.3867 659.9528 Tm This airliner can hold either 162 first class seats, 175 business class or 189 economy seats in total. EMC EMC ( )Tj ( )Tj EMC ( )Tj EMC /P <>BDC (5.1% benefit in fuel burn with the heavier)Tj ( )Tj ( )Tj EMC ( )Tj BT 8 0 0 8 298.0262 760.9528 Tm /P <>BDC EMC ( )Tj The 737-800 is the most popular variant of the four NG models, with nearly 5,000 aircraft delivered and making up 72% of the NG fleet in service. BT EMC /P <>BDC document.getElementById( "ak_js_1" ).setAttribute( "value", ( new Date() ).getTime() ); Airbus A320 Introduction The very popular short haul airliner. ET 9 0 0 9 36.8504 467.8898 Tm . ( )Tj ET (seat configuration of 16/18/126, giving a)Tj EMC -.02 Tc EMC (1,824)Tj /P <>BDC EMC BT /P <>BDC /P <>BDC ET -.02 Tc ( )Tj EMC ( )Tj 7 0 0 7 445.619 617.7654 Tm /P <>BDC EMC BT ET EMC /P <>BDC 9 0 0 9 385.2246 148.8898 Tm ET ET BT 0 Tc BT (29,432)Tj /P <>BDC EMC 0 Tw ET /P <>BDC ( )Tj EMC EMC 0 Tc /P <>BDC ( )Tj 8 0 0 8 43.6039 731.9528 Tm ( )Tj /P <>BDC /P <>BDC ET EMC (O)Tj /P <>BDC 7 0 0 7 210.1137 265.7654 Tm ET ET ( )Tj 9 0 0 9 542.2972 203.8898 Tm /P <>BDC BT ET BT EMC EMC 7 0 0 7 507.7893 584.7654 Tm /P <>BDC /OC /MC200 BDC BT /P <>BDC EMC ET ( fuel burn benefit to the A320ceo)Tj 0 Tc ET 7 0 0 7 539.8962 540.9528 Tm BT Boeing 737 Assembly, the building of this popular City Jet. 7 0 0 7 247.7395 287.7654 Tm -.02 Tc BT endstream -.02 Tc EMC ET ET In-flight, the GW must be periodically EMC .661 .752 .896 rg ET ET /P <>BDC EMC 0 Tc BT BT BT ET 7 0 0 7 539.8962 639.9528 Tm ET BT 7 0 0 7 473.8245 397.9528 Tm EMC EMC (5,126)Tj ET ET Centre tank pumps EMC EMC EMC /P <>BDC EMC levels in the center fuel tanks. ET (34,650lbs)Tj BT 6 0 0 6 246.7063 757.9528 Tm 9 0 0 9 394.0315 258.8898 Tm 7 0 0 7 247.7395 573.7654 Tm 0 Tc ET EMC (974)Tj (Since all eight aircraft types are in)Tj BT BT BT 9 0 0 9 394.0123 302.8898 Tm /P <>BDC 9 0 0 9 53.8582 720.8898 Tm (\(see table,)Tj 7 0 0 7 490.8321 265.7654 Tm -.02 Tc BT /P <>BDC .008 Tc BT BT 7 0 0 7 355.3163 122.7654 Tm ET /P <>BDC /P <>BDC (improvement of 0.58 cents per ASM over)Tj 6.5 0 0 6.5 379.0655 650.9529 Tm 9 0 0 9 394.0237 203.8898 Tm EMC /P <>BDC BT /P <>BDC (112)Tj ET BT 8 0 0 8 264.6706 619.9528 Tm EMC ET /P <>BDC -.01 Tc /F4 1 Tf ( )Tj BT BT EMC 7 0 0 7 99.8582 111.7654 Tm ET BT EMC EMC 9 0 0 9 383.6209 423.8898 Tm ( )Tj /P <>BDC ( )Tj EMC EMC 7 0 0 7 404.101 331.7654 Tm BT EMC BT BT ( )Tj The increase in OEW of)Tj ET 7 0 0 7 182.5706 177.9528 Tm 7 0 0 7 141.7322 232.9528 Tm The 800 was developed to replace the 727 on short routes. ET 9 0 0 9 572.0386 115.8898 Tm (1,824)Tj EMC 7 0 0 7 158.74 221.7654 Tm /P <>BDC 9 0 0 9 374.0759 203.8898 Tm BT ( )Tj ET EMC /P <>BDC /P <>BDC The cabin layout used for)Tj /P <>BDC 6 0 0 6 442.408 771.9528 Tm 7 0 0 7 141.7322 540.9528 Tm (31,416)Tj All data presented is for entertainment purposes and should not be used operationally. 7 0 0 7 258.2805 584.7654 Tm 0 Tc ET /P <>BDC EMC (193,344)Tj 7 0 0 7 427.7291 265.9528 Tm 7 0 0 7 241.5317 419.9528 Tm BT -.02 Tc EMC ( )Tj EMC EMC 9 0 0 9 53.8582 368.8898 Tm (I)Tj /P <>BDC .023 .567 .626 rg /P <>BDC 7 0 0 7 141.7322 606.9528 Tm 7 0 0 7 519.3773 276.9528 Tm BT 7 0 0 7 241.5317 441.9528 Tm /P <>BDC EMC 6.5 0 0 6.5 176.1172 585.9529 Tm (483)Tj ET EMC ET 7 0 0 7 554.7883 617.7654 Tm ET EMC EMC EMC 0 Tc EMC [(F)11(uel capacity - U)-8.1(S)0(G)]TJ EMC BT EMC ET ( )Tj /P <>BDC /P <>BDC /Im1 Do BT - Non Perele - News Online, Council Post: Aviation Is The Driving Force Of Hydrogen | QNewsHub, When will the Boeing 737 MAX fly again? BT EMC ET /P <>BDC ET 7 0 0 7 279.1575 89.9528 Tm /P <>BDC (A)Tj /P <>BDC BT /P <>BDC BT /P <>BDC (35,112lbs)Tj /P <>BDC EMC 8 0 0 8 334.994 675.9528 Tm ET /P <>BDC EMC /P <>BDC allowed to run dry or be left running unsupervised. ET 0 Tc EMC -.02 Tc 9 0 0 9 568.555 82.8898 Tm BT ET BT EMC ET ET BT 0 Tc EMC 7 0 0 7 294.4014 584.7654 Tm EMC BT ( )Tj (BOS-DEN)Tj /P <>BDC EMC (A320ceo is limited to 127 passengers on)Tj ET BT ET EMC ET 0 Tc EMC /P <>BDC /GS1 gs (A potential operator would need to)Tj BT /P <>BDC 0 Tc EMC 9 0 0 9 394.0315 38.8898 Tm EMC /P <>BDC EMC EMC BT BT ET .151 .147 .15 rg ET 8 0 0 8 480.7187 771.9529 Tm ( )Tj 9 0 0 9 382.3068 489.8898 Tm 7 0 0 7 537.7804 133.9528 Tm 9 0 0 9 215.433 291.8898 Tm EMC /P <>BDC ( )Tj ET /P <>BDC EMC 9 0 0 9 394.0123 555.8898 Tm /P <>BDC 7 0 0 7 82.8504 331.9528 Tm h /P <>BDC 9 0 0 9 195.0251 434.8898 Tm /P <>BDC ( A)Tj -.02 Tc 7 0 0 7 88.196 11.5129 Tm ET EMC 0 Tc -.01 Tc Cheers Peter. EMC ( )Tj /Figure <>BDC ET ET /P <>BDC 7 0 0 7 247.7395 727.7654 Tm BT BT (reducing their in-flight service offering, this)Tj 7 0 0 7 247.7395 199.7654 Tm EMC BT ET 9 0 0 9 433.2572 104.8898 Tm /P <>BDC /P <>BDC EMC 0 Tc EMC 9 0 0 9 373.9277 478.8898 Tm EMC ET BT BT (with an ESAD of 2,576nm in payload)Tj 9 0 0 9 411.0097 291.8898 Tm /P <>BDC EMC 9 0 0 9 394.0123 49.8898 Tm ET ( )Tj ET BT ET ET (Engine)Tj BT (214)Tj EMC BT ET ET ( )Tj BT /P <>BDC EMC 7 0 0 7 59.2108 11.5129 Tm -.02 Tc BT [(B)-13.9(L)74(V/53)]TJ EMC /P <>BDC (97,700)Tj /P <>BDC 7 0 0 7 258.2805 166.7654 Tm /P <>BDC ET /P <>BDC 0 Tc ( A)Tj 9 0 0 9 393.233 203.8898 Tm 10 0 0 10 54.3039 794.2914 Tm BT EMC 0 Tc BT BT ET 8 0 0 8 43.6039 633.9528 Tm BT EMC 6.5 0 0 6.5 191.942 611.9529 Tm BT 0 Tc BT BT ET )Tj ET BT /P <>BDC 9 0 0 9 545.0725 434.8898 Tm (The second comparison is payload)Tj f /P <>BDC -.02 Tc /P <>BDC /P <>BDC 9 0 0 9 192.1373 401.8898 Tm /F1 1 Tf EMC /P <>BDC 7 0 0 7 54.7071 716.7654 Tm /P <>BDC 7 0 0 7 158.74 78.7654 Tm EMC EMC 7 0 0 7 320.7537 144.9528 Tm BT ET [(TU)-8.1(S/101)]TJ EMC EMC (3,443)Tj 9 0 0 9 526.8993 643.8898 Tm /P <>BDC ET 6.5 0 0 6.5 500.4875 532.9529 Tm -.02 Tc ET 9 0 0 9 184.215 478.8898 Tm /P <>BDC BT BT ET /P <>BDC BT )Tj /P <>BDC /P <>BDC ET 0 Tc EMC 9 0 0 9 75.273 445.8898 Tm -.02 Tc BT /P <>BDC ( )Tj /P <>BDC ET BT EMC 9 0 0 9 207.0841 203.8898 Tm S BT /P <>BDC /P <>BDC (41,289)Tj ET EMC /P <>BDC BT -.02 Tc ET EMC EMC ET /P <>BDC /P <>BDC -.02 Tc /P <>BDC ET BT /P <>BDC EMC /P <>BDC /P <>BDC /P <>BDC I started of using with this image. ET /P <>BDC BT 7 0 0 7 355.5753 562.7654 Tm BT EMC ET BT EMC ( )Tj 6 0 0 6 481.8528 701.9528 Tm q 1 0 0 1 36.85 469.878 cm 0 0 m q 1 0 0 1 394.016 758.971 cm 0 0 m /P <>BDC ET /P <>BDC ( )Tj -.02 Tc BT 0 Tc BT /P <>BDC /P <>BDC (with the newer types it is expected that)Tj ET BT 5.25 0 0 5.25 123.5367 11.5132 Tm BT ET EMC -.02 Tc ( C)Tj 9 0 0 9 532.5876 137.8898 Tm -.02 Tc EMC Q BT ( )Tj BT ( )Tj /P <>BDC EMC /P <>BDC EMC BT EMC BT EMC 9 0 0 9 394.0315 654.8898 Tm EMC ET EMC /P <>BDC BT 7 0 0 7 116.3631 11.5132 Tm /P <>BDC /P <>BDC BT EMC EMC Q BT /P <>BDC EMC 6 0 0 6 153.0397 715.9528 Tm ( )Tj 7 0 0 7 439.2087 298.9528 Tm (136)Tj (174,606)Tj (10)Tj /P <>BDC ET /P <>BDC /P <>BDC /P <>BDC ET ( )Tj /P <>BDC EMC (rating on the CFM LEAP-1A32 to)Tj ET /P <>BDC /P <>BDC ET ( )Tj /P <>BDC (capacity, whereas the A321neo, with the)Tj /P <>BDC EMC ( )Tj 7 0 0 7 354.6933 628.7654 Tm 0 Tc /P <>BDC -.02 Tc -.01 Tc BT ( N)Tj ( )Tj -.02 Tc ( )Tj BT ET 9 0 0 9 394.0123 137.8898 Tm /P <>BDC 7 0 0 7 490.8321 166.7654 Tm EMC ET (. BT ET 7 0 0 7 326.2278 672.9528 Tm /P <>BDC 7 0 0 7 337.7614 144.7654 Tm [(737-900E)-33(R)]TJ BT -.02 Tc EMC (performance. EMC ET ( )Tj 7 0 0 7 490.8321 375.7654 Tm /P <>BDC ET BT ( )Tj EMC BT ET EMC /P <>BDC -.02 Tc BT [(P)11(assenger payload - lbs )]TJ ET EMC 0 Tc 9 0 0 9 209.838 60.8898 Tm /F6 1 Tf 6.5 0 0 6.5 399.2659 565.9529 Tm (136)Tj 13 0 0 13 411.0234 786.8898 Tm BT ET ( )Tj /P <>BDC 6.5 0 0 6.5 346.9224 585.9529 Tm 6.5 0 0 6.5 104.3885 722.9529 Tm ( )Tj ET (2,013)Tj ET /P <>BDC BT BT 0 Tc 0 Tc 7 0 0 7 379.3969 320.7654 Tm ET /P <>BDC ET ( )Tj 9 0 0 9 51.0236 258.8898 Tm 0 Tc /P <>BDC -.02 Tc -.02 Tc [(A3)24.9(20neo v)12.9(ersus 7)-33(3)8.1(7-8 )]TJ (1,751)Tj EMC BT ET ET /P <>BDC ( )Tj ET ( )Tj EMC ET ET 0 J 0 j 15 w 10 M [] 0 d ET ( )Tj ( )Tj EMC BT BT ET /P <>BDC EMC BT ET ET (The spot fuel price for the US aviation)Tj ( )Tj EMC -.01 Tc /P <>BDC 6 0 0 6 237.4295 701.9528 Tm EMC /P <>BDC ET BT ( )Tj EMC EMC (A321neo)Tj EMC BT 9 0 0 9 53.8582 93.8898 Tm ET ET /P <>BDC ET BT 304.725 420.96 m -.005 Tc ( )Tj EMC 7 0 0 7 298.514 573.9528 Tm /P <>BDC BT /P <>BDC /P <>BDC 0 Tc BT BT EMC ( )Tj /P <>BDC ET /P <>BDC EMC (The main operating parameters are: )Tj ET BT BT ET -.02 Tc ET /Artifact <>BDC ET EMC ( )Tj BT BT EMC For the wheels, I will give you two measurements. ET (The comparison of the two aircraft)Tj ET EMC ET 0 J 0 j 5 w 10 M [] 0 d 9 0 0 9 199.5582 38.8898 Tm EMC /P <>BDC There are two AC powered fuel pumps in each tank; there are also EDPs at ( )Tj EMC (369-383)Tj EMC 7 0 0 7 125.6292 628.7654 Tm ( )Tj (market. )Tj BT 9 0 0 9 394.0237 181.8898 Tm ( )Tj 7 0 0 7 187.0858 562.9528 Tm ET These are: Below is a table of the main features and specifications for the Boeing 737 family of aircraft. The)Tj ET 7 0 0 7 141.7322 276.9528 Tm ( )Tj 9 0 0 9 196.1514 390.8898 Tm ET BT ( )Tj ET (The three main operational costs for)Tj -.02 Tc (50,800)Tj BT EMC ET 7 0 0 7 456.7412 661.7654 Tm BT BT 7 0 0 7 247.7395 419.7654 Tm ET BT EMC 0 Tc ET 7 0 0 7 491.7142 298.7654 Tm BT ET BT (182,200lbs, an MLW of 152,800lbs, and)Tj /P <>BDC /P <>BDC BT EMC 9 0 0 9 376.0468 401.8898 Tm EMC ET ET ET EMC EMC ( )Tj /P <>BDC /P <>BDC /P <>BDC EMC ET /P <>BDC BT 0 Tc 6.5 0 0 6.5 296.4841 663.9529 Tm 9 0 0 9 394.0123 577.8898 Tm BT Q -.01 Tc -.02 Tc (0.0133)Tj 7 0 0 7 326.2278 529.9528 Tm ET /P <>BDC 9 0 0 9 73.1083 489.8898 Tm 7 0 0 7 247.7395 628.7654 Tm EMC ET 7 0 0 7 439.8175 727.9528 Tm 0 Tc /P <>BDC 9 0 0 9 394.0315 214.8898 Tm BT /P <>BDC BT /P <>BDC EMC /P <>BDC EMC EMC EMC BT /P <>BDC EMC BT BT ( )Tj BT BT EMC [(AIRL)8.1(INE & AIR)7.1(CRAF)-12.9(T)18.1( OPERA)56.9(T)-8.1(ION)-13.9(S)]TJ .151 .147 .15 rg ET EMC BT ( )Tj /P <>BDC ET BT (176)Tj EMC ET BT ( )Tj EMC 9 0 0 9 215.4409 379.8898 Tm ET 0 Tc 0 Tc Q 7 0 0 7 537.267 232.7654 Tm EMC EMC EMC ( )Tj /P <>BDC /Artifact <>BDC ( )Tj 0 Tc /P <>BDC /P <>BDC ( )Tj /OC /MC2304 BDC 0 Tc /P <>BDC BT -.02 Tc 9 0 0 9 36.8504 192.8898 Tm ET BT (comparison focused on the fuel burn)Tj 10.479 -.009 l ( )Tj 9 0 0 9 420.5961 38.3073 Tm BT 0 Tc ( )Tj ( )Tj EMC q EMC EMC (0.0134)Tj BT ET ( )Tj ET BT ( )Tj BT BT 0 Tc /P <>BDC ( )Tj BT f /P <>BDC /P <>BDC EMC EMC ET 0 Tc EMC /P <>BDC EMC ( )Tj ET EMC (study has been configured with the same)Tj 0 Tc 6 0 0 6 477.5682 659.9528 Tm /P <>BDC 7 0 0 7 386.3929 628.9528 Tm ET (MTOW. ET 7 0 0 7 344.1175 595.7654 Tm but also if a pump is left running dry for over approx 10 minutes it will lose EMC ET ET BT BT EMC BT ET ET 7 0 0 7 163.8846 11.5132 Tm EMC BT (. ET ET (direction lead to a headwind component)Tj .151 .147 .15 rg 0 Tc (4,514)Tj BT BT -.02 Tc ( )Tj 7 0 0 7 124.1242 397.7654 Tm EMC /P <>BDC /P <>BDC ET /P <>BDC ET ET (based on the cost index set is different, it)Tj BT )Tj /P <>BDC EMC ( )Tj 9 0 0 9 186.0514 60.8898 Tm /P <>BDC ET ( )Tj BT BT /P <>BDC EMC BT ET EMC 6 0 0 6 247.4022 729.9528 Tm ( )Tj EMC 9 0 0 9 198.8517 280.8898 Tm [(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 ET 9 0 0 9 374.2479 71.8898 Tm BT 8 0 0 8 543.5282 797.8898 Tm /P <>BDC (have any payload limitations on the routes)Tj 0 Tc /Artifact <>BDC 7 0 0 7 241.2727 276.9528 Tm BT BT /P <>BDC /P <>BDC /P <>BDC /P <>BDC ( )Tj EMC (571)Tj BT /P <>BDC ET ET BT 7 0 0 7 520.6108 529.9528 Tm BT ET ET ( )Tj EMC (which has the lowest fuel burn rate per)Tj (and A321neo respectively. BT 9 0 0 9 551.4604 269.8898 Tm ET BT ET 9 0 0 9 543.0273 192.8898 Tm ET BT BT (The equivalent still air distance \(ESAD\))Tj /P <>BDC 9 0 0 9 36.8583 478.8898 Tm BT ET ET 7 0 0 7 473.8245 199.9528 Tm ( )Tj 9 0 0 9 368.2199 247.8898 Tm EMC EMC ET 0 Tc -.02 Tc EMC EMC ET /P <>BDC ( )Tj 9 0 0 9 496.6703 148.8898 Tm (family, Airbus has reduced the thrust)Tj 6 0 0 6 147.4588 729.9528 Tm BT ET BT 0 Tc EMC The 737-900ER's successor is set to be the MAX 10, which will have a maximum capacity of 230 passengers and can fly 3,300 nautical miles (narrowly beating its predecessor). BT -.02 Tc Modern Airliners and Civil Aviation Aircraft. /P <>BDC 7 0 0 7 363.2711 573.9528 Tm (1,823)Tj BT 7 0 0 7 141.7322 375.9528 Tm 7 0 0 7 101.0963 89.9528 Tm EMC EMC EMC (operator with additional savings in)Tj /F7 1 Tf /P <>BDC /P <>BDC -.01 Tc 7 0 0 7 108.6215 364.9528 Tm ET 0 Tc 0 Tc 7 0 0 7 490.5101 661.9528 Tm ET -.02 Tc EMC ( )Tj EMC BT BT [(737-900E)-33(R)]TJ 9 0 0 9 189.3204 324.8898 Tm ET 0 Tc /P <>BDC 6.5 0 0 6.5 484.6315 545.9529 Tm ET ET /P <>BDC ET ( )Tj /P <>BDC ( )Tj 8 0 0 8 43.6039 591.9528 Tm (has resulted in them requiring less galley)Tj BT (cabin interior enhancements and changes)Tj ( )Tj 9 0 0 9 368.2867 357.8898 Tm (types over a wide range of mission lengths)Tj /P <>BDC ET The Boeing 737 is a narrow-body aircraft produced by Boeing at its Renton Factory in Washington.Developed to supplement the Boeing 727 on short and thin routes, the twinjet retains the 707 fuselage width and six abreast seating with two underwing turbofans.Envisioned in 1964, the initial 737-100 made its first flight in April 1967 and entered service in February 1968 with Lufthansa. 9 0 0 9 354.313 236.8898 Tm 7 0 0 7 355.5753 573.7654 Tm (Improvements introduced to the)Tj ( )Tj EMC ( )Tj EMC BT 7 0 0 7 204.0935 507.7654 Tm ET (1465,400)Tj (with a thrust rating of 26,000lbs, an intake)Tj BT 6 0 0 6 146.7028 743.9528 Tm BT /P <>BDC EMC ET 6.5 0 0 6.5 534.5352 624.9529 Tm EMC BT /P <>BDC EMC 7 0 0 7 37.6993 408.9528 Tm BT /P <>BDC ET /P <>BDC BT 9 0 0 9 377.4586 676.8898 Tm BT BT 7 0 0 7 490.8321 320.7654 Tm ET ( )Tj /P <>BDC (113,016)Tj ET /P <>BDC ET (1,690)Tj 9 0 0 9 536.1277 247.8898 Tm /P <>BDC ( )Tj 6 0 0 6 191.3929 771.9528 Tm BT ( )Tj 7 0 0 7 380.2788 606.7654 Tm EMC /P <>BDC ET ( )Tj -.02 Tc ET BT ET EMC 9 0 0 9 182.0906 467.8898 Tm ( )Tj -.02 Tc 0 Tc EMC /P <>BDC BT /P <>BDC BT ET BT ET BT ET ET ( )Tj ( )Tj /P <>BDC BT BT BT 9 0 0 9 544.9208 280.8898 Tm [(UG)-17.1(U)-8(S)8.1(T)]TJ ET (5.7:1)Tj ( )Tj 9 0 0 9 68.3339 555.8898 Tm ET 9 0 0 9 380.2477 247.8898 Tm BT /P <>BDC 7 0 0 7 179.5605 716.9528 Tm EMC 7 0 0 7 354.4763 672.7654 Tm (of 170 passengers, the A321neo burns an)Tj 0 Tc EMC /P <>BDC EMC BT 7 0 0 7 37.0536 705.9528 Tm the aircraft data bus. W n ET ( )Tj 0 Tc 0 Tc ET /F1 1 Tf EMC (will take into account the additional)Tj ET W n 7 0 0 7 439.7405 595.9528 Tm (aircraft types; and with no additional cargo)Tj ( )Tj BT BT EMC (405)Tj ET EMC ( )Tj EMC ET ET EMC EMC 9 0 0 9 53.8578 115.8898 Tm EMC ET FQIS accuracy: +/- 1.0% overall 0 Tc -.02 Tc ( )Tj /P <>BDC ( )Tj /GS1 gs EMC -.02 Tc (CFM56-5B3/P)Tj BT /P <>BDC ET ET /P <>BDC BT EMC 7 0 0 7 386.3929 683.9528 Tm 7 0 0 7 491.4046 210.9528 Tm BT /P <>BDC ( )Tj (trip-?? BT [(differ)10(ences in fuel burn betw)6.1(een the types ar)10(e examined by Ian Britchfor)7.1(d. )]TJ -.02 Tc 9 0 0 9 394.0123 313.8898 Tm -.01 Tc Cheers Peter, Pingback:Is Covid-19 isolation an opportunity to learn to fly? f ET (1,272)Tj BT /P <>BDC BT EMC Heres the list of Boeing Customer Codes: https://en.m.wikipedia.org/wiki/List_of_Boeing_customer_codes. 6 0 0 6 309.4863 659.9528 Tm 0 Tc EMC /P <>BDC /P <>BDC EMC /P <>BDC 13 0 0 13 36.8583 390.8898 Tm 7 0 0 7 241.5317 111.9528 Tm EMC /P <>BDC EMC BT /P <>BDC EMC 6.5 0 0 6.5 221.1405 702.9529 Tm 7 0 0 7 535.5029 397.7654 Tm (difference. ET EMC .41 .161 .508 rg The website has also a photo gallery and gives you an overview of all aviation museums worldwide. The payload reduction is)Tj [(A3)24.9(20neo)]TJ EMC 7 0 0 7 457.0984 694.7654 Tm ET /P <>BDC BT /P <>BDC ET EMC BT (used in flight planning, the scenarios use a)Tj EMC -.02 Tc .151 .147 .15 rg BT ET ET ET EMC /P <>BDC ( )Tj 7 0 0 7 343.2355 683.7654 Tm ET ( )Tj /GS2 gs /P <>BDC ET 9 0 0 9 232.4217 412.8898 Tm ET ET BT EMC ( )Tj /P <>BDC 7 0 0 7 210.1137 364.7654 Tm -.07 Tc ( )Tj ( )Tj /P <>BDC 7 0 0 7 37.5838 639.9528 Tm EMC 0 Tc design and maintenance of fuel tanks to reduce the chances of such explosions in 7 0 0 7 295.2833 78.7654 Tm 7 0 0 7 241.5317 133.9528 Tm ( )Tj BT /P <>BDC EMC 7 0 0 7 258.2805 573.7654 Tm (The 737-800 is the most popular)Tj BT EMC 6 0 0 6 308.7063 757.9528 Tm 7 0 0 7 554.7883 309.7654 Tm .151 .147 .15 rg EMC 361 0 obj (lighter aircraft. BT (the engine option chosen for this study is)Tj 13 0 0 13 162.9571 181.8898 Tm /P <>BDC BT ET /P <>BDC ET /P <>BDC ET /P <>BDC ET BT BT ET /P <>BDC [(Alternate airpor)-23(t &)]TJ EMC ET EMC BT -.02 Tc EMC 7 0 0 7 279.1575 100.9528 Tm BT ET ET /P <>BDC ( )Tj /P <>BDC ET ( )Tj BT 7 0 0 7 355.3163 232.7654 Tm BT ( )Tj EMC -.5815 -.9071 l EMC /P <>BDC -27.729 805.04 404.737 -303.307 re /GS2 gs BT BT 6 0 0 6 444.4713 757.9528 Tm [(P)11(assengers)]TJ (full passenger payload. 7 0 0 7 354.4763 716.7654 Tm EMC EMC /P <>BDC BT /P <>BDC 6 0 0 6 547.0496 673.9528 Tm ET EMC /P <>BDC /P <>BDC EMC /P <>BDC 7 0 0 7 247.7395 705.7654 Tm 6 0 0 6 208.9129 729.9528 Tm 7 0 0 7 241.5317 639.9528 Tm /P <>BDC /P <>BDC ET EMC BT ET EMC BT /P <>BDC BT ET The Boeing 777-200 has a maximum fuel capacity of 31,000 gallons or 117,347 liters. BT EMC (is 0.01 to 0.15 cents better than the)Tj BT 9 0 0 9 325.0684 434.8898 Tm 7 0 0 7 158.74 133.7654 Tm /P <>BDC BT EMC EMC EMC ET ( )Tj 9 0 0 9 571.1344 742.8898 Tm ET EMC /P <>BDC 9 0 0 9 211.8361 577.8898 Tm EMC EMC 1 1 1 rg 6 0 0 6 115.2799 687.9528 Tm ET EMC /P <>BDC BT BT EMC 7 0 0 7 326.2278 683.9528 Tm EMC /P <>BDC (economics of the aircraft types with more)Tj BT ( )Tj /P <>BDC 9 0 0 9 211.0829 379.8898 Tm BT BT BT LO-Z wiring, Open or short circuit in a LO-Z to a tank unit, Calibration unit does not operate correctly. /P <>BDC /P <>BDC ET ET ET BT BT EMC (in ASMs between the eight aircraft types. EMC BT Thank you so much. 9 0 0 9 411.0097 599.8898 Tm ET ET EMC ( )Tj /Artifact <>BDC 7 0 0 7 337.6855 507.9528 Tm (The later generation aircraft are set to)Tj ET ET BT 9 0 0 9 185.7888 489.8898 Tm 9 0 0 9 232.438 346.8898 Tm 9 0 0 9 163.2471 269.8898 Tm BT 9 0 0 9 197.3303 170.8898 Tm BT 36.85 824.882 572.599 17.008 re 9 0 0 9 36.8504 181.8898 Tm /P <>BDC ET (1,162)Tj BT ( )Tj BT BT /P <>BDC BT (PPS flight planning software is used to)Tj The 800 variant is the stretched version of the 737-700. EMC /P <>BDC /P <>BDC ( )Tj /P <>BDC /P <>BDC ET ET BT /P <>BDC ET 9 0 0 9 425.1913 181.8898 Tm /P <>BDC BT EMC endstream EMC EMC (hugely successful. EMC 9 0 0 9 68.3339 544.8898 Tm /P <>BDC 6.5 0 0 6.5 191.7926 702.9529 Tm EMC 0 Tc )Tj (135,453)Tj BT BT 0 Tc (0.0110)Tj BT ET -.02 Tc BT BT BT ( )Tj EMC ( )Tj 0 Tc ET /P <>BDC 7 0 0 7 404.101 210.7654 Tm /P <>BDC ET (152)Tj ET EMC 0 Tc 7 0 0 7 445.619 562.7654 Tm ( )Tj EMC -.01 Tc 6.5 0 0 6.5 274.6269 689.9529 Tm -.02 Tc -.02 Tc ET ET ( )Tj ET BT ET EMC 9 0 0 9 565.8376 577.8898 Tm EMC /P <>BDC (final comparison of the two manufacturers)Tj 9 0 0 9 202.0349 753.8898 Tm /P <>BDC EMC ET EMC BT BT 7 0 0 7 474.3564 496.9528 Tm BT EMC /P <>BDC /P <>BDC EMC q 1 0 0 1 394.024 91.644 cm 0 0 m EMC EMC Q /P <>BDC ET 7 0 0 7 337.9444 628.9528 Tm (105)Tj EMC ET /P <>BDC BT ET W n ( )Tj EMC 9 0 0 9 215.433 346.8898 Tm BT 0 Tc 7 0 0 7 440.0906 276.9528 Tm ET /P <>BDC ET 9 0 0 9 229.6064 126.8898 Tm /P <>BDC EMC /P <>BDC ( )Tj BT 7 0 0 7 446.5009 672.7654 Tm /P <>BDC 7 0 0 7 457.0984 672.7654 Tm ET EMC ( )Tj 9 0 0 9 215.4409 104.8898 Tm ET EMC (150)Tj EMC ET 7 0 0 7 535.5029 276.7654 Tm /P <>BDC ET ET ET 0 Tc ET BT EMC BT ET /OC /MC19 BDC 0 Tc .151 .147 .15 rg /P <>BDC /P <>BDC (this study, the 737-9 is operated with the)Tj EMC BT BT (block fuel burn performance of up to)Tj ET BT (and their operational use by mainline)Tj 0 Tc ET (34,650)Tj (0.0141)Tj EMC (0.0123)Tj ET EMC ET BT ET ( )Tj ET ( )Tj ( )Tj ( )Tj BT BT /P <>BDC EMC 7 0 0 7 158.74 672.7654 Tm BT ET ( )Tj ET (31,416)Tj 7 0 0 7 338.3085 243.9528 Tm .151 .147 .15 rg ET BT BT /P <>BDC EMC 7 0 0 7 387.0159 529.9528 Tm BT (propulsive efficiency. ( )Tj BT /P <>BDC BT BT 8 0 0 8 124.845 675.9528 Tm -.02 Tc ET /P <>BDC BT (737-800W)Tj ( )Tj 9 0 0 9 53.8338 346.8898 Tm ET 6.5 0 0 6.5 433.3069 585.9529 Tm ET ET BT BT ET BT BT EMC ( )Tj /P <>BDC /P <>BDC ( )Tj ET /P <>BDC ( )Tj ( )Tj ET EMC BT 7 0 0 7 543.7693 11.5132 Tm EMC EMC EMC BT BT ET ET (burn difference is 2.2%, and results in an)Tj BT 7 0 0 7 294.4014 595.7654 Tm 9 0 0 9 362.6813 357.8898 Tm 9 0 0 9 571.9847 181.8898 Tm 0 Tc EMC ( )Tj 5.25 0 0 5.25 40.8474 11.5129 Tm BT ( )Tj (34,650)Tj /P <>BDC ET 17 0 0 17 526.2604 775.1944 Tm /P <>BDC 7 0 0 7 456.2165 111.7654 Tm ET /P <>BDC EMC ET EMC ( )Tj (11,593)Tj ET BT BT ET BT /Artifact <>BDC 0 Tc ET ET BT /GS2 gs 7 0 0 7 474.7064 188.9528 Tm EMC 8 0 0 8 270.7815 771.9528 Tm EMC /P <>BDC 9 0 0 9 36.8504 456.8898 Tm BT (377,550)Tj 304.725 420.96 m 0 Tc -.02 Tc EMC BT ET EMC /P <>BDC 6 0 0 6 527.8009 743.9528 Tm BT /P <>BDC 0 Tc EMC -.02 Tc /P <>BDC (1,824)Tj The total tolerance for the FQIS system is based on a full tank. BT ET /P <>BDC 8 0 0 8 419.0258 760.9528 Tm ( )Tj BT BT 7 0 0 7 99.8582 122.7654 Tm BT /P <>BDC ( )Tj EMC /F4 1 Tf BT /P <>BDC BT BT endobj /P <>BDC 7 0 0 7 456.4753 738.7654 Tm ET EMC BT EMC ( )Tj ( )Tj EMC ET 13 0 0 13 530.7245 434.8898 Tm ET q 1 0 0 1 215.441 73.878 cm 0 0 m W n ET (. BT ET ET ( )Tj /P <>BDC BT EMC /P <>BDC ET /P <>BDC ET ET 394.516 71.673 160.63 -39.992 re -.02 Tc ET 9 0 0 9 425.1913 93.8898 Tm BT 0 Tc ( )Tj EMC ( )Tj 0 841.89 609.449 -841.89 re 9 0 0 9 215.4409 489.8898 Tm 0 Tc ET ET BT -.02 Tc ET EMC EMC BT ( )Tj ( )Tj 7 0 0 7 294.4014 364.7654 Tm BT 9 0 0 9 375.3516 335.8898 Tm EMC ET 9 0 0 9 36.8504 379.8898 Tm 7 0 0 7 430.039 639.9528 Tm ET ET ET /P <>BDC BT 9 0 0 9 53.8582 192.8898 Tm ( )Tj 9 0 0 9 411.0097 269.8898 Tm /P <>BDC EMC BT /P <>BDC ET -.02 Tc 0 Tc BT q EMC ET 9 0 0 9 394.0157 423.8898 Tm
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