737 800 fuel capacity pounds

BT 7 0 0 7 456.2165 100.7654 Tm /P <>BDC ET 6.5 0 0 6.5 192.6116 689.9529 Tm ET BT /P <>BDC ET 7 0 0 7 337.4684 738.9528 Tm ET (passengers; thereby giving the A321ceo a)Tj ET BT Have you got any exact places or web address please? ET BT 9 0 0 9 185.4953 214.8898 Tm /P <>BDC EMC /P <>BDC 8 0 0 8 383.8445 771.7654 Tm ET /P <>BDC BT EMC EMC -.02 Tc /P <>BDC BT ET (16,268)Tj 9 0 0 9 522.1112 247.8898 Tm ET ( )Tj BT (737-9)Tj (operational factors that also have to be)Tj BT BT BT 9 0 0 9 195.4853 126.8898 Tm ET ET -.01 Tc /P <>BDC 8 0 0 8 394.0237 38.8898 Tm (112)Tj 6.5 0 0 6.5 90.4525 676.9529 Tm EMC 9 0 0 9 411.0097 181.8898 Tm ET 7 0 0 7 60.6117 540.7654 Tm 9 0 0 9 252.9543 170.8898 Tm BT EMC EMC BT W n EMC ET EMC /P <>BDC EMC BT /F3 1 Tf ET /P <>BDC BT ( )Tj /P <>BDC ( )Tj 19.841 0 l /P <>BDC EMC EMC EMC /F6 1 Tf /P <>BDC EMC BT /P <>BDC (151)Tj BT 9 0 0 9 374.6152 269.8898 Tm EMC ( )Tj BT ET ET ( )Tj 0 Tc ( )Tj 9 0 0 9 36.8504 324.8898 Tm EMC /P <>BDC EMC /P <>BDC BT /P <>BDC BT EMC /P <>BDC EMC 0 Tc BT ( )Tj EMC BT ET EMC 9 0 0 9 187.5717 126.8898 Tm 6.5 0 0 6.5 430.0114 565.9529 Tm (310,080)Tj 9 0 0 9 185.7888 489.8898 Tm ET BT /P <>BDC EMC BT 10 0 0 10 37.304 794.2914 Tm EMC EMC [(SS)-9.1(U)8(E)]TJ ET ( )Tj ET ( )Tj The 737-900 also retains the MTOW and fuel capacity of the 800, trading range for payload. BT [(A3)24.9(20ceo v)12.9(ersus A3)24.9(20neo )]TJ /P <>BDC /P <>BDC 9 0 0 9 246.595 49.8898 Tm /P <>BDC /P <>BDC BT BT /P <>BDC ( )Tj 0 J 0 j .5 w 10 M [] 0 d /P <>BDC 7 0 0 7 508.4124 243.7654 Tm -.02 Tc -.02 Tc EMC /P <>BDC /OC /MC2 BDC ET /Artifact <>BDC (I)Tj The 800 variant is the stretched version of the 737-700. 7 0 0 7 355.5753 584.7654 Tm EMC (. -.01 Tc 6 0 0 6 178.2463 729.9528 Tm EMC /P <>BDC ( )Tj (types will only be made where unrestricted)Tj BT ( )Tj ET ET ET EMC Q BT ET EMC ET 7 0 0 7 508.2252 11.5129 Tm 13 0 0 13 355.5757 115.8898 Tm 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. ET ET 7 0 0 7 387.0932 232.9528 Tm (105,800)Tj /P <>BDC (and Boeing aircraft benefit from the)Tj BT /P <>BDC -.005 Tc BT 10 0 0 10 37.304 794.2914 Tm ET ( )Tj 7 0 0 7 37.5838 639.9528 Tm /P <>BDC BT BT ET EMC /P <>BDC EMC /P <>BDC ET ( )Tj EMC ( )Tj ( )Tj 0 Tc ET ( )Tj 0 Tc ( )Tj 6.5 0 0 6.5 500.4941 565.9529 Tm (9,451)Tj ET BT BT EMC ET ET ( )Tj 9 0 0 9 377.8372 291.8898 Tm -.02 Tc /P <>BDC 5.25 0 0 5.25 100.8225 11.5132 Tm EMC 0 Tc BT safest way forward, but is very expensive and possibly impractical. /P <>BDC 6 0 0 6 174.3402 673.9528 Tm ET /P <>BDC ET /P <>BDC BT EMC -.02 Tc (32,000lbs, down from the 33,000lbs that)Tj 8 0 0 8 159.2283 745.9528 Tm BT EMC ET 1 i /P <>BDC ET Economy-plus is also)Tj !! BT 0 Tc /P <>BDC EMC /P <>BDC ET EMC Cheers Peter, Pingback:Is Covid-19 isolation an opportunity to learn to fly? EMC /P <>BDC ET ET /P <>BDC Thank you. /P <>BDC ET /P <>BDC (over 400 MAXs, and Airbus a similar)Tj ( )Tj EMC -.02 Tc /P <>BDC ( )Tj EMC (464,270)Tj EMC Check out the Boeing 737 Specs tables below to get a clear picture of how these city jets stack up. EMC BT 6.5 0 0 6.5 375.6529 702.9529 Tm 9 0 0 9 382.6039 434.8898 Tm 9 0 0 9 184.2244 203.8898 Tm ET EMC 8 0 0 8 225.1837 717.9528 Tm /P <>BDC BT (cost index calculated by the airline to the)Tj BT EMC 6.5 0 0 6.5 399.2659 565.9529 Tm )Tj /P <>BDC BT /P <>BDC /P <>BDC ET BT EMC (31,416)Tj BT BT EMC -.02 Tc /P <>BDC EMC /P <>BDC EMC 7 0 0 7 54.7071 122.7654 Tm ( )Tj 6 0 0 6 240.5796 729.9528 Tm EMC ET -407.02 814.197 m 0 Tc 7 0 0 7 343.2355 496.7654 Tm 0 Tc EMC In November 2005, Boeing unveiled the BBJ3, based on the 737-900ER. 7 0 0 7 158.74 177.7654 Tm ()Tj BT 10 0 0 10 47.7404 814.1973 Tm BT ET BT /F4 1 Tf 7 0 0 7 297.632 595.9528 Tm /P <>BDC 0 Tc /P <>BDC 9 0 0 9 68.3339 445.8898 Tm ET BT EMC ET EMC EMC (190,800)Tj (36,960)Tj ET 9 0 0 9 356.4538 258.8898 Tm 9 0 0 9 361.9078 401.8898 Tm EMC ( )Tj ( )Tj /P <>BDC .014984 841.89 609.45 -841.89 re ET EMC ( )Tj EMC (5,025)Tj 7 0 0 7 187.0858 529.9528 Tm 9 0 0 9 548.3284 610.8898 Tm BT /P <>BDC ( )Tj /P <>BDC 7 0 0 7 381.1608 573.7654 Tm 431 0 obj ( )Tj (1,272)Tj ( )Tj )Tj EMC ( )Tj EMC EMC EMC BT BT EMC 7 0 0 7 362.3891 287.9528 Tm ET /Im4 Do BT /P <>BDC ET BT EMC ET )Tj /P <>BDC 8 0 0 8 332.978 577.9528 Tm ( )Tj 5.25 0 0 5.25 525.4061 11.5132 Tm /P <>BDC /P <>BDC ET BT ET 0 Tc BT 9 0 0 9 439.4008 324.8898 Tm /P <>BDC /P <>BDC ET ( )Tj ( )Tj ( )Tj ET S BT EMC ET 9 0 0 9 36.8504 38.8898 Tm /P <>BDC /P <>BDC -.02 Tc EMC /P <>BDC BT ( )Tj ET BT /P <>BDC BT 6.5 0 0 6.5 244.2585 637.9529 Tm BT BT /P <>BDC (route structure so these charges would not)Tj EMC /P <>BDC BT ET 9 0 0 9 394.0315 720.8898 Tm BT 7 0 0 7 386.3929 628.9528 Tm ET 9 0 0 9 215.4313 71.8898 Tm BT 7 0 0 7 99.8582 595.7654 Tm ET ET EMC EMC 7 0 0 7 241.2727 166.9528 Tm 9 0 0 9 411.0181 126.8898 Tm /P <>BDC 7 0 0 7 279.1575 243.9528 Tm 7 0 0 7 439.2087 243.9528 Tm 9 0 0 9 393.233 203.8898 Tm (2,732)Tj ( )Tj /P <>BDC /P <>BDC ET ( )Tj ET EMC 9 0 0 9 215.4409 390.8898 Tm -.02 Tc BT EMC (and the A321ceo and A321neo. 9 0 0 9 68.3339 544.8898 Tm EMC EMC /P <>BDC EMC ET ET ET ET BT -.02 Tc ET EMC 9 0 0 9 36.8504 313.8898 Tm 9 0 0 9 421.0664 401.8898 Tm BT BT BT 9 0 0 9 368.9994 225.8898 Tm ( )Tj 7 0 0 7 297.632 518.9528 Tm EMC -.02 Tc /P <>BDC /P <>BDC EMC EMC (832)Tj BT /P <>BDC ET (1B engine as the 737-8. 7 0 0 7 508.4124 78.7654 Tm (3,535)Tj /P <>BDC (737-800W)Tj ET 7 0 0 7 554.7883 375.7654 Tm BT /P <>BDC 7 0 0 7 199.5784 441.7654 Tm Report (DOT/FAA/AR-01/63) (4.8Mb), MAX: 3,869 + 12,990 + 3,869 = 20,729kg, 1/200: 9 0 0 9 411.0181 467.8898 Tm ( )Tj in later aircraft). BT BT ET BT /P <>BDC ET /P <>BDC 7 0 0 7 508.4124 705.7654 Tm /P <>BDC ET ET /P <>BDC (A320neo)Tj 7 0 0 7 279.1575 606.9528 Tm EMC ( )Tj 7 0 0 7 429.157 485.9528 Tm /P <>BDC When this runs dry the scavenge /P <>BDC [(CFM L)17.1(E)-8.1(AP-1B27)]TJ ET ( )Tj 6.5 0 0 6.5 346.3049 676.9529 Tm BT ( )Tj BT BT BT ( )Tj BT BT EMC BT EMC -.02 Tc BT 6 0 0 6 205.0069 673.9528 Tm /P <>BDC /P <>BDC ( )Tj BT EMC /P <>BDC EMC ET EMC ( )Tj BT ( )Tj ET /P <>BDC BT /P <>BDC ET 0 Tc ET If there is more you want to learn about this airliner, please visit: Boeing 737 Home, Boeing 737 Interior, Boeing 737 Order Book, Boeing 737 History, Boeing 737 Assembly and Boeing 737 Max. /P <>BDC 9 0 0 9 394.0237 379.8898 Tm (additional benefit in this comparison. EMC BT /P <>BDC BT ET ET EMC 7 0 0 7 141.7322 298.9528 Tm EMC 9 0 0 9 394.0123 126.8898 Tm (14 sectors. 0 Tc ET cumulative errors it is recommended that the wings are filled once every few 9 0 0 9 215.4313 478.8898 Tm ( )Tj ( )Tj BT /Artifact <>BDC BT ET 7 0 0 7 554.7883 661.7654 Tm (manufacturers support these aircraft types)Tj /P <>BDC (City-pair)Tj -.02 Tc ET 7 0 0 7 473.8245 243.9528 Tm /P <>BDC EMC EMC EMC ET ( )Tj EMC /P <>BDC (0.0171)Tj 9 0 0 9 394.0123 599.8898 Tm ( )Tj ET /P <>BDC (customers better performance and lower)Tj ET ET EMC BT BT /P <>BDC -.02 Tc EMC ET Boeing 777X The New Triple Seven Family. ET ( )Tj /P <>BDC ET EMC BT 5.25 0 0 5.25 55.7484 11.5132 Tm 7 0 0 7 37.6993 430.9528 Tm /P <>BDC ET (CFM56-5B4/P)Tj /P <>BDC -.02 Tc EMC /P <>BDC ( )Tj /P <>BDC /P <>BDC ET /P <>BDC ET 9 0 0 9 181.0402 335.8898 Tm EMC EMC 5.25 0 0 5.25 525.4061 11.5132 Tm EMC /P <>BDC ET ( )Tj BT ET EMC 6.5 0 0 6.5 433.3069 585.9529 Tm EMC 9 0 0 9 352.4841 313.8898 Tm EMC ET BT 3 i EMC EMC (111)Tj (4,000)Tj ET /P <>BDC BT /P <>BDC 0 Tc 9 0 0 9 215.433 247.8898 Tm 0 Tc 7 0 0 7 298.514 617.9528 Tm ( )Tj 6.5 0 0 6.5 64.6596 715.9529 Tm 6 0 0 6 195.6824 659.9528 Tm ET BT BT /P <>BDC BT 9 0 0 9 36.8583 445.8898 Tm BT endobj 7 0 0 7 258.2805 738.7654 Tm /P <>BDC EMC /P <>BDC ( )Tj ET -.02 Tc /P <>BDC BT BT ET (improvement of 0.58 cents per ASM over)Tj BT BT ET /P <>BDC (166,090)Tj -.02 Tc ET /P <>BDC BT BT EMC EMC 0 Tc ( )Tj /P <>BDC (page\))Tj EMC EMC EMC (34,650lbs)Tj /P <>BDC BT /P <>BDC EMC 7 0 0 7 355.3163 67.7654 Tm 9 0 0 9 548.1057 610.8898 Tm The charges are split by weight)Tj /P <>BDC EMC EMC -.02 Tc EMC 7 0 0 7 387.0932 144.9528 Tm 6 0 0 6 381.7993 757.9528 Tm 9 0 0 9 215.4313 434.8898 Tm BT 7 0 0 7 37.0536 683.9528 Tm /P <>BDC ( )Tj (. -.02 Tc EMC EMC 7 0 0 7 36.8504 155.9528 Tm <>/XObject<>/ExtGState<>/Properties<>>> 9 0 0 9 569.7076 148.8898 Tm BT BT BT (35,112)Tj ET 9 0 0 9 53.8338 115.8898 Tm 9 0 0 9 394.0237 478.8898 Tm BT Cheers Peter. each aircraft is sourced from different places. ET (CFM56-5B4/P)Tj EMC EMC EMC ( fuel burn benefit to the A320ceo)Tj ( )Tj ET /OC /MC3457 BDC EMC ( )Tj /P <>BDC -.02 Tc BT (fuel burn evaluation compares the selected)Tj ET BT EMC ( )Tj BT ( )Tj EMC BT BT -.02 Tc ET ET BT /P <>BDC EMC BT BT EMC 9 0 0 9 376.0986 324.8898 Tm /P <>BDC BT /P <>BDC 9 0 0 9 197.0674 258.8898 Tm BT EMC BT EMC EMC ET 7 0 0 7 247.7395 573.7654 Tm -.02 Tc /P <>BDC 9 0 0 9 53.8578 126.8898 Tm ET 7 0 0 7 316.0679 342.7654 Tm ET ( )Tj s !1AQa"q2B#R3b$r%C4Scs5D'6Tdt& (163)Tj /P <>BDC ET ( )Tj 7 0 0 7 296.1653 100.7654 Tm 7 0 0 7 125.6292 441.7654 Tm /P <>BDC BT 7 0 0 7 258.2805 441.7654 Tm /P <>BDC 6.5 0 0 6.5 499.4541 735.9529 Tm EMC ET EMC BT ET ( )Tj 7 0 0 7 363.2711 540.9528 Tm EMC ( )Tj (this evaluation. (. ET EMC EMC ET EMC ( )Tj EMC EMC BT ET EMC EMC ET /P <>BDC ( )Tj ET /P <>BDC ( )Tj ET ET ET 7 0 0 7 379.3969 122.7654 Tm ET pump will also transfer any remaining centre tank fuel into main tank 1, thereby 7 0 0 7 537.7804 419.9528 Tm BT (163)Tj 9 0 0 9 394.0157 126.8898 Tm ET ( )Tj 304.725 420.96 m 0 Tc ET EMC ( )Tj BT ET 7 0 0 7 294.4014 298.7654 Tm /P <>BDC /P <>BDC )Tj 9 0 0 9 36.8504 368.8898 Tm 108 lbs (49 kgs) to the 737-800 basic MEW. EMC 0 Tc ET /P <>BDC -.02 Tc /P <>BDC EMC EMC BT (operating potential for these aircraft. /P <>BDC BT BT EMC /P <>BDC Best of luck. /P <>BDC 5.25 0 0 5.25 549.1047 11.5132 Tm -.02 Tc The trigger for the scavenge pump is different for the series as follows: NB On the classics, when departing with less than 1,000kg of fuel in the centre tank, an imbalance may occur during ( )Tj (126,464)Tj BT BT ( )Tj /P <>BDC EMC (l)Tj ( )Tj -.01 Tc EMC 7 0 0 7 158.74 89.7654 Tm ET /P <>BDC (Boeing aircraft, the 737-800 has a 2.5%)Tj EMC ET (against a headwind component, and give)Tj /P <>BDC /P <>BDC /P <>BDC 6.5 0 0 6.5 549.8557 663.9529 Tm ET EMC /P <>BDC /P <>BDC -.02 Tc 7 0 0 7 363.2711 177.9528 Tm BT 424 0 obj EMC BT ET 9 0 0 9 411.0181 313.8898 Tm /P <>BDC ET BT /P <>BDC BT EMC 0 841.89 609.449 -841.89 re /P <>BDC ET BT EMC ET BT ET 9 0 0 9 53.8582 60.8898 Tm <>/XObject<>/ExtGState<>/Properties<>>> BT 9 0 0 9 194.9803 478.8898 Tm ET /P <>BDC /P <>BDC EMC .151 .147 .15 rg 6.5 0 0 6.5 499.1421 722.9529 Tm BT -.02 Tc (capacity with slimmer seats, and cabin)Tj 518.735 0 l EMC allowed to run dry or be left running unsupervised. /P <>BDC BT /P <>BDC (120-128)Tj ET ET ET EMC ( )Tj 9 0 0 9 191.3244 324.8898 Tm EMC 9 0 0 9 411.0097 500.8898 Tm ( )Tj ET EMC EMC 7 0 0 7 473.4744 540.9528 Tm /F1 1 Tf ET /P <>BDC ET ET (5,466)Tj EMC EMC BT BT ET (78,729)Tj EMC ET 7 0 0 7 141.7322 375.9528 Tm /Artifact <>BDC BT /GS1 gs /P <>BDC EMC /P <>BDC BT /P <>BDC BT (A321neo)Tj /P <>BDC EMC 0 Tc In this)Tj /P <>BDC 9 0 0 9 525.3974 192.8898 Tm 9 0 0 9 394.0123 324.8898 Tm .0081 Tc ET /P <>BDC BT ET (46,900)Tj EMC EMC EMC -.02 Tc BT 8 0 0 8 542.9269 786.8898 Tm BT (483)Tj BT BT /P <>BDC /P <>BDC ET 6 0 0 6 269.4048 687.9528 Tm 0 Tw EMC ET /P <>BDC 8 0 0 8 37.0439 771.9528 Tm BT ( )Tj /P <>BDC EMC 9 0 0 9 209.838 60.8898 Tm BT /P <>BDC EMC 9 0 0 9 382.6146 368.8898 Tm BT /P <>BDC ET ET 7 0 0 7 141.7322 661.9528 Tm 9 0 0 9 563.6848 401.8898 Tm 9 0 0 9 436.7009 104.8898 Tm (831)Tj BT 6 0 0 6 174.3402 701.9528 Tm EMC Fuel temp is taken from main tank 1 because this will be the coldest as it has (248,200)Tj 9 0 0 9 229.6064 456.8898 Tm (34,650)Tj 7 0 0 7 230.7317 133.9528 Tm /P <>BDC 15 w (with a thrust rating of 27,000lbs, an intake)Tj Hiya, (ratio of 11.0:1. 7 0 0 7 383.0719 705.7654 Tm ET BT ( )Tj 9 0 0 9 370.2844 489.8898 Tm 7 0 0 7 53.8582 11.5132 Tm /P <>BDC ET 6.5 0 0 6.5 376.7644 742.9529 Tm /P <>BDC 9 0 0 9 553.7373 225.8898 Tm (US gallons \(USG\) )Tj -.02 Tc BT -.02 Tc 9 0 0 9 232.4217 148.8898 Tm /P <>BDC EMC 7 0 0 7 158.74 485.7654 Tm ET EMC EMC EMC ( )Tj (25,160)Tj ( )Tj EMC ET EMC (2,514)Tj BT BT EMC 9 0 0 9 215.4409 478.8898 Tm (2,732)Tj ( )Tj 7 0 0 7 554.7883 705.7654 Tm 7 0 0 7 54.5916 243.7654 Tm EMC EMC /P <>BDC BT 7 0 0 7 537.267 133.7654 Tm EMC /P <>BDC BT 7 0 0 7 490.5101 518.9528 Tm ET 7 0 0 7 439.2087 221.9528 Tm ET /F1 1 Tf ET .1202 .4955 .3052 1.277 y ET ( )Tj EMC Engine size (A321neo)Tj ET EMC EMC 9 0 0 9 203.484 192.8898 Tm ET EMC EMC /P <>BDC (fan diameter of 68 inches and a bypass)Tj BT EMC EMC BT 6.5 0 0 6.5 172.7047 598.9529 Tm ET /P <>BDC ET EMC BT BT /P <>BDC 7 0 0 7 554.7883 408.7654 Tm BT ( )Tj 0 Tc ET ( )Tj BT (484)Tj .661 .752 .896 rg EMC BT BT 7 0 0 7 554.7883 419.7654 Tm 8 0 0 8 187.3427 577.9528 Tm BT The 737-200Adv could also be fitted with an EMC EMC /P <>BDC BT BT thank you for stopping by. /P <>BDC ET /P <>BDC (passenger payload - nm)Tj ET 7 0 0 7 99.8582 485.7654 Tm BT ET 7 0 0 7 54.5916 254.7654 Tm BT -.02 Tc ET 10 0 0 10 408.1099 814.1973 Tm 505.331 89.873 m /P <>BDC )Tj -.02 Tc ET 9 0 0 9 36.8504 214.8898 Tm EMC 6.5 0 0 6.5 64.6596 689.9529 Tm 9 0 0 9 36.8504 247.8898 Tm /P <>BDC 9 0 0 9 411.0097 423.8898 Tm EMC ET 9 0 0 9 198.8517 280.8898 Tm /P <>BDC /P <>BDC 0 Tc ( )Tj 0 Tc 7 0 0 7 343.2355 694.7654 Tm ET /P <>BDC /P <>BDC /P <>BDC 9 0 0 9 394.0157 225.8898 Tm ET ET EMC /P <>BDC 7 0 0 7 518.4953 133.9528 Tm ( )Tj EMC BT 7 0 0 7 241.5317 518.9528 Tm EMC 6.5 0 0 6.5 94.8855 689.9529 Tm 7 0 0 7 277.3936 265.9528 Tm 7 0 0 7 491.4046 397.9528 Tm /P <>BDC EMC ( )Tj EMC EMC EMC ET /P <>BDC ET There are many variants of the 737. /P <>BDC BT BT BT EMC 7 0 0 7 241.5317 243.9528 Tm /P <>BDC /P <>BDC 5.25 0 0 5.25 64.5461 11.5129 Tm EMC ( )Tj BT /P <>BDC ET (hour and per mile reduces . (block fuel burn performance of up to)Tj /P <>BDC 0 Tc BT ( )Tj BT 9 0 0 9 392.5848 379.8898 Tm /P <>BDC BT ET /P <>BDC EMC (evaluation, the 737-8 and 737-9 are 2.2%)Tj /P <>BDC 9 0 0 9 527.3954 313.8898 Tm /P <>BDC BT ET EMC EMC ( )Tj EMC EMC EMC 0 Tc (carriers. EMC /P <>BDC ET ET BT It provides code tables for aerodromes, air operators including the world's major airlines and for ICAO and IATA codes for aircraft. ET BT ET ET (A321ceo)Tj ET 8 0 0 8 158.74 760.7654 Tm EMC 6.5 0 0 6.5 330.4406 624.9529 Tm /P <>BDC BT ( )Tj BT ET -2.4549 -3.9026 l ET ET /P <>BDC BT /P <>BDC (2,498)Tj 9 0 0 9 232.4408 753.8898 Tm /F4 1 Tf 7 0 0 7 241.5317 122.9528 Tm 6.5 0 0 6.5 382.9199 735.9529 Tm BT /P <>BDC /P <>BDC /P <>BDC ET 9 0 0 9 232.438 478.8898 Tm /P <>BDC EMC /P <>BDC /P <>BDC EMC /P <>BDC EMC 6.5 0 0 6.5 64.6596 722.9529 Tm /P <>BDC 7 0 0 7 294.4014 606.7654 Tm ( )Tj ET EMC /P <>BDC 9 0 0 9 411.0181 148.8898 Tm EMC 0 Tc EMC /P <>BDC BT /P <>BDC /P <>BDC EMC BT BT BT ET ET 5.25 0 0 5.25 492.6848 11.5129 Tm -.02 Tc how can i know the material of 737NGs nose landing gear lower drag strut?thank you. ( )Tj BT ( )Tj 7 0 0 7 492.5963 738.7654 Tm /P <>BDC ET EMC (44,057)Tj .559 .331 .619 rg ET -.02 Tc EMC (1,272)Tj 7 0 0 7 230.7317 210.9528 Tm /P <>BDC ( )Tj BT ET ET 7 0 0 7 258.2805 584.7654 Tm BT ET ET EMC /P <>BDC (comparative performance. (0.0149)Tj -.02 Tc ET /P <>BDC /P <>BDC EMC /P <>BDC EMC ET BT 9 0 0 9 204.9867 214.8898 Tm BT (188,400)Tj EMC 9 0 0 9 417.7488 511.8898 Tm ET /P <>BDC 6.5 0 0 6.5 448.1595 735.9529 Tm /P <>BDC (evaluate the physical configuration of the)Tj /P <>BDC -.02 Tc /P <>BDC Q [(M)-9(L)51(W - lbs)]TJ 8 0 0 8 43.6039 771.9528 Tm ET EMC (2,517)Tj 7 0 0 7 535.5029 518.7654 Tm /P <>BDC /P <>BDC ET ( )Tj ET aux tanks to push the aux fuel into the centre tank. 0 841.89 609.449 -841.89 re 9 0 0 9 571.1344 742.8898 Tm EMC (\(Toronto Pearson\) sector, to 2,730nm for)Tj /P <>BDC ( )Tj EMC /P <>BDC 9 0 0 9 372.8879 412.8898 Tm .0081 Tc /P <>BDC ( )Tj ET ( )Tj 6 0 0 6 538.428 771.9528 Tm EMC BT (248,064)Tj ET 8 0 0 8 181.9279 771.7654 Tm 7 0 0 7 380.2788 419.7654 Tm BT /P <>BDC EMC ET /P <>BDC EMC ( )Tj BT 6 0 0 6 389.0654 673.9528 Tm /P <>BDC -.01 Tc /GS2 gs 7 0 0 7 298.3957 430.9528 Tm 9 0 0 9 411.0097 71.8898 Tm 9 0 0 9 190.2715 38.8898 Tm BT (12,549)Tj 7 0 0 7 457.0984 188.7654 Tm EMC ET hi! 7 0 0 7 258.2805 188.7654 Tm ( )Tj ET (includes checked and carry-on luggage. /P <>BDC -.02 Tc 5 0 0 5 484.5872 11.5129 Tm BT BT ET ET EMC (737-9)Tj ET ET EMC 7 0 0 7 337.4684 705.9528 Tm BT ( )Tj /P <>BDC EMC 9 0 0 9 68.9175 247.8898 Tm 0 Tc S BT 9 0 0 9 546.1516 203.8898 Tm (149,300)Tj EMC ET /P <>BDC BT /P <>BDC ET /P <>BDC BT ET ET (2,517)Tj EMC /P <>BDC 8 0 0 8 74.9636 591.9528 Tm (0.0117)Tj ET BT /P <>BDC /P <>BDC BT EMC BT 9 0 0 9 394.0157 456.8898 Tm BT 9 0 0 9 76.2256 412.8898 Tm BT 7 0 0 7 279.1575 738.9528 Tm ( )Tj BT /P <>BDC 7 0 0 7 131.6494 309.7654 Tm 9 0 0 9 232.4217 555.8898 Tm (900ER and 737-9, A320ceo and A320neo,)Tj /P <>BDC /P <>BDC ET EMC ET 8 0 0 8 136.4919 703.9528 Tm -.01 Tc EMC EMC 0 Tc 9 0 0 9 394.0315 225.8898 Tm ET During cruise, the tolerance is less than 1.5%. ET I would like to know what is the AOA during cruise for B737 NG and also the Fuel Flow cruise. /P <>BDC EMC BT ET -.01 Tc BT (150)Tj ET ( )Tj -.02 Tc EMC BT 7 0 0 7 241.5317 397.9528 Tm BT 9 0 0 9 369.3136 698.8898 Tm EMC /P <>BDC ( )Tj 7 0 0 7 487.0872 11.5129 Tm ET ( )Tj -.02 Tc /P <>BDC EMC BT BT ET BT BT ET 7 0 0 7 554.7883 584.7654 Tm ( )Tj BT EMC EMC q 7 0 0 7 43.6039 254.9528 Tm EMC -.02 Tc EMC EMC 0 Tc EMC /P <>BDC 0 Tc BT ( )Tj EMC 7 0 0 7 321.6356 166.9528 Tm BT EMC 6 0 0 6 489.6948 743.9528 Tm BT (0.0129)Tj 0 Tc 7 0 0 7 247.7395 331.7654 Tm (0.0139)Tj /P <>BDC EMC ET BT EMC -.02 Tc EMC /P <>BDC BT BT BT EMC EMC (cost per ASM ranges from 0.06 to 0.16)Tj EMC EMC /P <>BDC BT ET BT (The A320 and 737 families have been)Tj ET EMC -.02 Tc ( )Tj /P <>BDC 7 0 0 7 445.619 463.7654 Tm BT ET /P <>BDC ET BT ET /P <>BDC /P <>BDC ( )Tj ( )Tj BT -.02 Tc ET 9 0 0 9 373.9458 159.8898 Tm EMC 0 Tw BT ET BT ET I already checked in the AMM, SRM. 0 Tc /P <>BDC /P <>BDC -.02 Tc .151 .147 .15 rg BT /P <>BDC (A320neo, A321neo, 737-800, 737-)Tj BT ET 9 0 0 9 270.2513 93.8898 Tm I know the 787 is moving toward using more composite materiel instead of aluminum. -.02 Tc EMC [(CFM L)17.1(E)-8.1(AP-1A26)]TJ BT ( )Tj ( )Tj 6.5 0 0 6.5 64.6596 532.9529 Tm 7 0 0 7 338.5674 463.9528 Tm 7 0 0 7 535.5029 276.7654 Tm EMC EMC /P <>BDC ET BT waiting with pax endobj ET ET EMC /P <>BDC (In both cases, the A320neo has a lower)Tj /P <>BDC 7 0 0 7 141.7322 419.9528 Tm ET ET During cruise, the tolerance is less than 0.5%. BT 5.25 0 0 5.25 447.6106 11.5129 Tm /P <>BDC /P <>BDC ( )Tj /P <>BDC ET ET BT /P <>BDC BT /P <>BDC 8 0 0 8 90.0179 771.7654 Tm EMC 7 0 0 7 387.0932 199.9528 Tm EMC ET EMC (36,960)Tj 9 0 0 9 551.4784 797.8898 Tm 7 0 0 7 158.74 617.7654 Tm BT BT ET 7 0 0 7 321.6356 177.9528 Tm ( )Tj ( )Tj /P <>BDC FQIS accuracy: +/- 1.0% overall Main tanks smaller at 3900kg each but centre tank much larger giving total fuel capacity of 20,800kg. EMC (passengers and 163 passengers on the)Tj /P <>BDC 9 0 0 9 192.1913 38.8898 Tm /P <>BDC /P <>BDC 0 Tc ( )Tj EMC 9 0 0 9 215.4409 269.8898 Tm EMC ET 7 0 0 7 363.2711 419.9528 Tm 0 Tc EMC /P <>BDC EMC /P <>BDC 9 0 0 9 550.3618 324.8898 Tm /P <>BDC /OC /MC4777 BDC ET 9 0 0 9 370.7977 236.8898 Tm /P <>BDC EMC EMC 7 0 0 7 258.2805 111.7654 Tm )Tj /P <>BDC ET f (9 has no payload limitation on any of the)Tj /P <>BDC BT ( )Tj 9 0 0 9 36.8504 225.8898 Tm ET BT EMC 7 0 0 7 537.7804 364.9528 Tm 7 0 0 7 456.4753 738.7654 Tm EMC ET ET 8 0 0 8 43.6039 731.9528 Tm ( )Tj EMC BT 0 Tc EMC /P <>BDC 7 0 0 7 54.7071 364.7654 Tm 0 Tc BT ET EMC ET /P <>BDC 7 0 0 7 520.6108 595.9528 Tm 7 0 0 7 427.7291 188.9528 Tm 10.479 -.009 l BT 9 0 0 9 522.5095 181.8898 Tm ET EMC EMC EMC 9 0 0 9 53.8582 82.8898 Tm /P <>BDC 7 0 0 7 258.2805 683.7654 Tm 6 0 0 6 214.7788 729.9528 Tm EMC EMC 0 Tc ( )Tj /P <>BDC BT BT 8 0 0 8 404.5618 771.9528 Tm 9 0 0 9 411.0097 225.8898 Tm /P <>BDC /P <>BDC 0 Tc /P <>BDC (170)Tj BT ET ( )Tj BT EMC ( )Tj EMC 9 0 0 9 534.7515 599.8898 Tm ET (2,376)Tj EMC 7 0 0 7 182.5706 441.9528 Tm ET 7 0 0 7 82.8504 430.9528 Tm 0 Tc 9 0 0 9 544.5291 665.8898 Tm /P <>BDC EMC How much fuel do planes burn? 9 0 0 9 53.8582 269.8898 Tm BT ET The)Tj /P <>BDC BT /Artifact <>BDC /OC /MC4794 BDC /P <>BDC ( )Tj (20)Tj 9 0 0 9 394.0123 302.8898 Tm I suppose you have to look at the 737 as an aircraft class that is targeting a certain segment of the market. /P <>BDC (194,700)Tj BT BT BT 9 0 0 9 68.0314 775.8898 Tm ( )Tj BT ( )Tj BT BT BT /P <>BDC -.02 Tc ( )Tj ET /P <>BDC EMC (207,336)Tj 9 0 0 9 379.7168 225.8898 Tm 9 0 0 9 411.0097 269.8898 Tm 7 0 0 7 247.7395 221.7654 Tm BT ET /P <>BDC ( )Tj ET ET (70)Tj EMC /P <>BDC BT Each version in the 737 family fills a differ role. ET -.02 Tc (/S)Tj ET BT EMC 9 0 0 9 232.4217 544.8898 Tm EMC ET 7 0 0 7 107.1165 276.9528 Tm BT BT (The in-service fleet of the newer)Tj ET BT ET 6.5 0 0 6.5 449.7715 565.9529 Tm ET /P <>BDC ET ( )Tj EMC /P <>BDC /P <>BDC 7 0 0 7 535.5029 177.7654 Tm ET (capacity, so that payload is reduced to)Tj /P <>BDC 7 0 0 7 539.8962 738.9528 Tm EMC (4,163)Tj 8 0 0 8 314.3535 661.9528 Tm 9 0 0 9 36.8504 335.8898 Tm 9 0 0 9 53.8582 104.8898 Tm 7 0 0 7 158.74 320.7654 Tm ( )Tj BT (2,481)Tj BT \p+\rWef6lfL6;U1E5/6lUYyVebaHfQM]$q|L>_ SO9_sXa 3@"G;C=zlPY[?B 7 0 0 7 519.3773 166.9528 Tm ( )Tj -.01 Tc EMC 529.065 38.307 m 0 Tc 9 0 0 9 374.887 346.8898 Tm BT ET EMC BT BT /P <>BDC ( )Tj BT 7 0 0 7 279.1575 111.9528 Tm 7 0 0 7 101.0963 386.9528 Tm 7 0 0 7 326.2278 463.9528 Tm (20)Tj /OC /MC2279 BDC ET /P <>BDC ( )Tj 0 Tc BT ET /P <>BDC 17 0 0 17 36.8606 742.1944 Tm EMC 0 Tc EMC 9 0 0 9 545.537 390.8898 Tm EMC ()Tj (39,270)Tj ET EMC /P <>BDC ( )Tj 0 Tc ET /P <>BDC ( )Tj BT ( )Tj BT ET /P <>BDC 9 0 0 9 564.8296 82.8898 Tm ET EMC -.02 Tc 9 0 0 9 394.0315 291.8898 Tm ET ( )Tj /F6 1 Tf [(AIRL)8.1(INE & AIR)7.1(CRAF)-12.9(T)18.1( OPERA)56.9(T)-8.1(ION)-13.9(S)]TJ ( )Tj EMC EMC 6 0 0 6 237.4295 701.9528 Tm 9 0 0 9 534.6934 82.8898 Tm BT BT 9 0 0 9 552.0261 555.8898 Tm 0 Tc ET ET (for the purposes of this performance)Tj 7 0 0 7 508.6712 430.7654 Tm EMC 0 Tc ET 0 Tc EMC 9 0 0 9 346.8148 104.8898 Tm As an Amazon Associate I earn from qualifying purchases. (114)Tj EMC ET EMC ( )Tj -.02 Tc (3,691)Tj ( )Tj EMC ET )Tj BT 9 0 0 9 349.6767 335.8898 Tm ET /P <>BDC ET ET ET (evaluation that are payload-limited on the)Tj ( )Tj 6 0 0 6 295.8268 673.9528 Tm 9 0 0 9 270.2513 313.8898 Tm endobj BT ( )Tj /P <>BDC 9 0 0 9 373.1937 357.8898 Tm ( )Tj EMC /P <>BDC ( )Tj 7 0 0 7 124.1242 199.7654 Tm /P <>BDC 7 0 0 7 179.5605 221.9528 Tm /P <>BDC EMC 7 0 0 7 474.3564 507.9528 Tm 7 0 0 7 230.7317 177.9528 Tm (stated maximum still air passenger range of)Tj ET ET BT 304.725 420.96 m [(W)7.1(ind component - kts)]TJ BT (burn and operating)Tj BT 0 Tc EMC While the MAX 10 is still yet to be certified, the legacy of the -900ER lives on, and the type will likely continue to fly for many more years before retirement. /P <>BDC (operation. 7 0 0 7 387.3522 122.9528 Tm /P <>BDC BT [(Engine b)6.1(ypass)]TJ BT ( )Tj 6.5 0 0 6.5 397.9138 722.9529 Tm ET /P <>BDC BT (374)Tj 9 0 0 9 187.8443 346.8898 Tm EMC EMC -.02 Tc BT (number of seats as the A320ceo; and the)Tj 7 0 0 7 116.3631 11.5132 Tm ET /P <>BDC q /P <>BDC BT EMC ET EMC 9 0 0 9 261.8182 225.8898 Tm 7 0 0 7 338.3085 320.9528 Tm /P <>BDC 7 0 0 7 338.6433 320.7654 Tm EMC 7 0 0 7 520.6108 694.9528 Tm ( )Tj BT (with the newer types it is expected that)Tj 7 0 0 7 363.2711 529.9528 Tm EMC /P <>BDC /P <>BDC The)Tj ( )Tj EMC /P <>BDC /P <>BDC ( N)Tj BT ( )Tj ET ET BT 7 0 0 7 258.2805 386.7654 Tm 7 0 0 7 294.4014 287.7654 Tm /F4 1 Tf (. BT ET 0 Tc /P <>BDC -.02 Tc (342,312)Tj /P <>BDC /P <>BDC BT ( )Tj /P <>BDC /P <>BDC /P <>BDC

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