( )Tj BT ET /P <>BDC EMC -.01 Tc BT ET /P <>BDC EMC /P <>BDC BT /P <>BDC ET ( )Tj BT /F4 1 Tf ET 7 0 0 7 403.478 375.7654 Tm Since no two)Tj -407.02 814.197 m /P <>BDC (which is BOS-LAX, whereas the 737-800)Tj ET /P <>BDC 0 Tc 7 0 0 7 247.7395 584.7654 Tm 10 0 0 10 37.304 794.2914 Tm BT (163)Tj EMC /P <>BDC /P <>BDC ( )Tj ET BT 7 0 0 7 315.1859 144.7654 Tm /P <>BDC BT 7 0 0 7 321.6356 276.9528 Tm ( )Tj 0 Tc 7 0 0 7 279.1575 540.9528 Tm 9 0 0 9 51.0236 445.8898 Tm EMC /P <>BDC /P <>BDC /P <>BDC 7 0 0 7 99.8582 540.7654 Tm /P <>BDC (5,279)Tj EMC BT BT EMC BT 7 0 0 7 535.5029 243.7654 Tm /P <>BDC BT /P <>BDC EMC /P <>BDC BT ( )Tj ( )Tj /P <>BDC /P <>BDC 7 0 0 7 365.035 639.9528 Tm BT EMC ( )Tj 8 0 0 8 314.3535 633.9528 Tm BT ET ET (In the 85% passenger payload)Tj The controls for main tanks 1 and 2 change to aft BT BT /P <>BDC ET EMC EMC /P <>BDC 9 0 0 9 68.3339 511.8898 Tm EMC [(T)39.1(OL/57)]TJ ET -.02 Tc EMC EMC /P <>BDC ET BT EMC In-flight, the GW must be periodically ( )Tj Boeing 737 Interior. ( )Tj (176)Tj BT /P <>BDC ET EMC The flight)Tj 6 0 0 6 363.2184 687.9528 Tm /OC /MC5080 BDC 7 0 0 7 521.4928 573.9528 Tm EMC EMC BT BT ( )Tj [(P)11(ayload scenario two)]TJ /P <>BDC /P <>BDC 0 Tc BT BT 6.5 0 0 6.5 192.111 735.9529 Tm (In this comparison the passenger seat)Tj /P <>BDC BT EMC ET ET EMC ET 7 0 0 7 54.7071 529.7654 Tm The 737-900 also retains the MTOW and fuel capacity of the 800, trading range for payload. ( )Tj ( )Tj /P <>BDC 9 0 0 9 187.2749 610.8898 Tm ET 7 0 0 7 554.7883 617.7654 Tm 7 0 0 7 536.3849 111.7654 Tm (is 16/30/114, giving a maximum passenger)Tj ET EMC (150)Tj [(E)-7.8(P)16.1(T)9(E)-13.9(MBE)-16.9(R)]TJ -.02 Tc (burns. ( )Tj EMC 9 0 0 9 232.4217 71.8898 Tm (aircraft types, however, it was decided to)Tj [(CFM L)17.1(E)-8.1(AP-1B27)]TJ -.02 Tc EMC 9 0 0 9 229.6064 335.8898 Tm EMC ET -.02 Tc 0 Tc ( )Tj ET ET /P <>BDC ET 9 0 0 9 411.0097 313.8898 Tm ET BT /P <>BDC BT /F6 1 Tf ET ( )Tj ET 7 0 0 7 444.737 309.7654 Tm /P <>BDC -.02 Tc EMC 6 0 0 6 381.7993 715.9528 Tm BT ( )Tj ET 9 0 0 9 209.6398 489.8898 Tm (3,465)Tj /P <>BDC EMC 7 0 0 7 444.737 210.7654 Tm ET /F4 1 Tf BT ET ( )Tj (engine bypass ratio in the case of the 737)Tj EMC BT BT 8 0 0 8 394.0157 786.8898 Tm EMC EMC 9 0 0 9 36.8583 335.8898 Tm BT 6.5 0 0 6.5 64.6596 565.9529 Tm 9 0 0 9 197.0674 258.8898 Tm EMC /P <>BDC EMC ET /P <>BDC 9 0 0 9 147.641 236.8898 Tm ET [(E)-7.8(P)16.1(T)9(E)-13.9(MBE)-16.9(R)]TJ (150)Tj ET /P <>BDC ET /F4 1 Tf ( )Tj 10 0 0 10 49.2604 814.1973 Tm ET ( )Tj /P <>BDC BT -.02 Tc BT EMC ET ( )Tj EMC 0 Tc ET 6 0 0 6 427.5796 729.9528 Tm /P <>BDC ( )Tj ET 5.25 0 0 5.25 447.6106 11.5129 Tm ET /P <>BDC BT (/S)Tj -.02 Tc 7 0 0 7 539.8962 474.9528 Tm ( )Tj /P <>BDC BT ET [(Aircr)10(aft type)]TJ ( )Tj /P <>BDC ( )Tj 9 0 0 9 232.438 291.8898 Tm /P <>BDC BT EMC /P <>BDC EMC 9 0 0 9 394.0123 599.8898 Tm /P <>BDC EMC BT BT 7 0 0 7 107.1165 474.9528 Tm /P <>BDC ( )Tj ET ( )Tj BT ET ET 9 0 0 9 53.8582 445.8898 Tm /P <>BDC /P <>BDC ( )Tj EMC ( )Tj (/S)Tj EMC BT 8 0 0 8 38.4438 731.9528 Tm EMC ( )Tj (and in fuel burn per ASM. ET (977)Tj /GS1 gs /P <>BDC 7 0 0 7 490.5101 716.9528 Tm ET ( )Tj BT EMC 7 0 0 7 158.74 210.7654 Tm (difference. ( N)Tj ET BT BT EMC BT ( )Tj /P <>BDC -.02 Tc /P <>BDC 0 Tc ( )Tj BT BT BT /P <>BDC ( )Tj EMC ( )Tj ET ET EMC EMC ( )Tj /GS1 gs -.02 Tc ( )Tj BT (1,913)Tj /P <>BDC 0 Tc EMC EMC but also if a pump is left running dry for over approx 10 minutes it will lose 7 0 0 7 326.2278 716.9528 Tm BT EMC ( )Tj /P <>BDC (The comparison of the two aircraft)Tj 7 0 0 7 158.74 133.7654 Tm BT BT /P <>BDC ET It has a maximum range of 10,140km. 9 0 0 9 445.6725 302.8898 Tm ET 7 0 0 7 82.8504 243.9528 Tm (It was assumed that all flights would)Tj EMC (I)Tj BFE; . 6.5 0 0 6.5 274.6269 689.9529 Tm ( )Tj EMC 9 0 0 9 544.5291 665.8898 Tm 9 0 0 9 362.4471 82.8898 Tm EMC EMC EMC /P <>BDC BT /P <>BDC (have taken advantage of lighter composite)Tj ET /P <>BDC EMC BT /P <>BDC EMC EMC 9 0 0 9 325.0684 434.8898 Tm BT 0 Tc 9 0 0 9 394.0315 390.8898 Tm /P <>BDC (1A26)Tj /P <>BDC (0.0113)Tj /P <>BDC 7 0 0 7 321.6356 100.9528 Tm 6 0 0 6 433.9826 659.9528 Tm [(AS)29(M)21(s)]TJ BT 9 0 0 9 554.9974 456.8898 Tm EMC BT BT ET 9 0 0 9 232.438 423.8898 Tm (CFM56-5B3/P)Tj 9 0 0 9 215.433 346.8898 Tm EMC q 1 0 0 1 53.858 150.878 cm 0 0 m EMC 0 Tc EMC EMC /P <>BDC (SFO \(San Francisco\); and 70 on BOS-LAX. EMC ET ET EMC 0 Tc 9 0 0 9 36.8504 346.8898 Tm -.02 Tc /P <>BDC EMC /P <>BDC f EMC BT 7 0 0 7 429.157 562.9528 Tm /P <>BDC /P <>BDC (O)Tj 0 Tc -.02 Tc ET ( )Tj ET ET /F6 1 Tf ET BT EMC 0 Tc 0 Tc /P <>BDC EMC 8 0 0 8 264.6706 703.9528 Tm EMC The common factor in both accidents was that the centre tank /P <>BDC /P <>BDC (O)Tj EMC ET /P <>BDC EMC BT ( )Tj BT BT BT BT BT BT EMC ( )Tj ET ET 0 Tc ( C)Tj ET ET ET 7 0 0 7 36.8504 11.5129 Tm (shorter sectors, the A320ceo has a better)Tj EMC 9 0 0 9 53.8578 82.8898 Tm EMC 6.5 0 0 6.5 335.5237 532.9529 Tm 7 0 0 7 314.6398 507.7654 Tm ( )Tj 6.5 0 0 6.5 176.1172 558.9529 Tm (configuration, because this study shows)Tj /P <>BDC BT EMC (737-8)Tj /P <>BDC (-59)Tj EMC ( )Tj /P <>BDC /P <>BDC BT BT ( )Tj (route structure so these charges would not)Tj 7 0 0 7 380.2788 540.7654 Tm EMC 0 Tc EMC BT /P <>BDC 7 0 0 7 474.3564 617.9528 Tm 7 0 0 7 491.392 727.9528 Tm BT ET BT 7 0 0 7 204.0935 89.7654 Tm 0 Tc 9 0 0 9 394.0123 390.8898 Tm 9 0 0 9 183.0113 214.8898 Tm /P <>BDC ET 7 0 0 7 427.7291 188.9528 Tm ( )Tj ( )Tj -.02 Tc ET I already checked in the AMM, SRM. ( )Tj /P <>BDC (273,600)Tj ( )Tj /P <>BDC ET BT 6.5 0 0 6.5 477.8064 702.9529 Tm /P <>BDC ET ( )Tj 0 Tc (977)Tj ET /P <>BDC BT 6.5 0 0 6.5 244.2585 637.9529 Tm ET ( )Tj BT BT BT 7 0 0 7 258.2805 342.7654 Tm ET -.02 Tc (342,312)Tj BT EMC /P <>BDC ET ET 6.5 0 0 6.5 448.4195 722.9529 Tm BT /P <>BDC 7 0 0 7 379.3969 331.7654 Tm BT 9 0 0 9 200.4401 258.8898 Tm BT BT /P <>BDC /F5 1 Tf 6.5 0 0 6.5 54.877 742.9529 Tm EMC BT BT EMC ET BT Due to the additional structural)Tj 9 0 0 9 384.7818 137.8898 Tm EMC /P <>BDC 5.25 0 0 5.25 549.1047 11.5132 Tm 7 0 0 7 428.6112 397.9528 Tm EMC ( )Tj /P <>BDC 7 0 0 7 326.2278 540.9528 Tm BT 9 0 0 9 232.4217 566.8898 Tm 9 0 0 9 543.1342 192.8898 Tm EMC ET EMC /P <>BDC EMC EMC EMC ( )Tj BT /P <>BDC ( )Tj EMC EMC 0 Tc -.02 Tc ET 0 Tc ( )Tj EMC BT EMC BT BT 0 Tc EMC EMC EMC the climb. 9 0 0 9 36.8504 181.8898 Tm ET ET EMC /P <>BDC (\(ATC\) charges. /P <>BDC BT ET /P <>BDC ET ET /P <>BDC EMC 9 0 0 9 53.8578 49.8898 Tm BT 9 0 0 9 229.6064 456.8898 Tm EMC BT ( )Tj EMC ET ( )Tj BT EMC ( )Tj 7 0 0 7 294.4014 529.7654 Tm ( )Tj (136)Tj /P <>BDC ET ET EMC EMC ET EMC -.02 Tc EMC /P <>BDC 0 Tc /P <>BDC /P <>BDC /GS2 gs /P <>BDC 6.5 0 0 6.5 227.9655 565.9529 Tm EMC ( )Tj ET 9 0 0 9 169.0072 511.8898 Tm /P <>BDC ( )Tj BT ET 0 Tc /P <>BDC .014984 841.89 609.45 -841.89 re -.02 Tc BT ET 9 0 0 9 354.313 236.8898 Tm Worlds Most Popular Passenger Airplane for $ 89.1 million. (difference in fuel cost per ASM, however,)Tj /P <>BDC 7 0 0 7 141.7322 166.9528 Tm ( )Tj EMC /P <>BDC -.02 Tc ET EMC /Artifact <>BDC ET BT (136)Tj EMC (have therefore been removed from the)Tj EMC (cents, with a network average)Tj -.01 Tc BT (550)Tj /P <>BDC (bypass ratio than the A320/321neo. /P <>BDC ( )Tj 19.843 0 l /P <>BDC ET ET (aircraft an economic advantage in terms of)Tj BT ET ET BT EMC The PPS flight)Tj ET EMC 0 Tc BT BT BT ET 7 0 0 7 141.7322 89.9528 Tm 6.5 0 0 6.5 243.3486 742.9529 Tm /OC /MC1320 BDC /P <>BDC EMC 7 0 0 7 294.4014 562.7654 Tm EMC 7 0 0 7 321.6356 309.9528 Tm ET 7 0 0 7 125.6292 584.7654 Tm ET EMC (152)Tj ET EMC /P <>BDC ( )Tj BT /P <>BDC 13 0 0 13 215.4313 115.8898 Tm /P <>BDC EMC /P <>BDC ET BT BT BT 7 0 0 7 278.9827 430.9528 Tm 7 0 0 7 355.3163 89.7654 Tm 7 0 0 7 508.4124 287.7654 Tm EMC ET 9 0 0 9 394.0157 357.8898 Tm -.02 Tc EMC ( )Tj 9 0 0 9 215.433 104.8898 Tm ET EMC ( )Tj (than is possible in this article. ET BT ET ET ET /P <>BDC (11,593)Tj EMC ET Firstly, thank you for reply. W n EMC BT ( )Tj ET ET EMC ET ET ET 6.5 0 0 6.5 225.3721 637.9529 Tm EMC 9 0 0 9 206.355 214.8898 Tm (of being configured like those of the)Tj EMC /P <>BDC BT ET -.02 Tc 7 0 0 7 82.8504 342.9528 Tm 7 0 0 7 490.5101 529.9528 Tm ET /P <>BDC /P <>BDC /P <>BDC /P <>BDC /P <>BDC 9 0 0 9 411.0097 126.8898 Tm BT 13 0 0 13 36.8504 456.8898 Tm BT (0.0142)Tj /P <>BDC 9 0 0 9 232.4217 588.8898 Tm ( )Tj 7 0 0 7 37.5838 441.9528 Tm /P <>BDC (2,500)Tj EMC 0 Tc 9 0 0 9 376.579 434.8898 Tm ET BT /P <>BDC ( in absolute terms in USG,)Tj (fuel capacity of 6,303USG )Tj /P <>BDC BT 7 0 0 7 179.5605 320.9528 Tm EMC EMC BT 9 0 0 9 53.8578 126.8898 Tm 0 Tc 7 0 0 7 247.7395 529.7654 Tm 7 0 0 7 141.7322 441.9528 Tm .964 .834 .406 rg 7 0 0 7 297.632 518.9528 Tm /P <>BDC BT /P <>BDC 7 0 0 7 241.5317 606.9528 Tm ET -.01 Tc EMC 9 0 0 9 372.6154 236.8898 Tm ( )Tj ET EMC /P <>BDC BT 6 0 0 6 55.0668 701.9528 Tm (283)Tj ( )Tj /P <>BDC /P <>BDC ET ET (types, but it is worth noting that in)Tj /P <>BDC (20)Tj ( )Tj EMC 9 0 0 9 544.5056 302.8898 Tm EMC EMC (I)Tj ET ET EMC /P <>BDC 7 0 0 7 457.0984 133.7654 Tm (flight levels )Tj ET BT BT EMC ( )Tj EMC BT This)Tj /P <>BDC 7 0 0 7 54.7071 419.7654 Tm ( )Tj EMC ET BT BT ET EMC EMC (66,096)Tj 7 0 0 7 537.7804 177.9528 Tm EMC /P <>BDC 0 841.89 609.449 -841.89 re /P <>BDC /P <>BDC 6 0 0 6 61.517 729.9528 Tm (831)Tj /GS1 gs ( )Tj 9 0 0 9 181.2747 170.8898 Tm ET BT ( )Tj EMC -.02 Tc BT BT /P <>BDC (at 27,000lbs thrust compared to the)Tj /P <>BDC BT -.02 Tc ET BT ( )Tj EMC BT ET EMC ET /P <>BDC /P <>BDC ET ET 9 0 0 9 356.4538 258.8898 Tm 7 0 0 7 491.4046 386.9528 Tm EMC At least with the Max 8, looking into the ACAP of Boeing (Rev E), I found it is 2500nm. BT 6.5 0 0 6.5 76.9446 715.9529 Tm BT EMC BT ( )Tj BT BT ET /P <>BDC 0 Tc 9 0 0 9 211.1071 764.8898 Tm ET ET EMC BT -.02 Tc /P <>BDC BT 7 0 0 7 321.6356 320.9528 Tm /P <>BDC BT /P <>BDC (288)Tj (2,313)Tj /P <>BDC /P <>BDC 8 0 0 8 539.8061 771.9528 Tm ET EMC BT EMC 8 0 0 8 435.4879 760.7654 Tm BT BT BT 0 Tc BT ( )Tj /P <>BDC BT /P <>BDC -.01 Tc BT EMC /P <>BDC ( )Tj /P <>BDC 7 0 0 7 519.3773 67.9528 Tm /P <>BDC /OC /MC834 BDC BT 5.25 0 0 5.25 549.1047 11.5132 Tm BT (0.0139)Tj /P <>BDC /P <>BDC /P <>BDC ET 0 Tc ET EMC ET ( )Tj (-54)Tj (A321ceo)Tj s !1AQa"q2B#R3b$r%C4Scs5D'6Tdt& EMC ET 6.5 0 0 6.5 426.4819 663.9529 Tm 0 Tc 5.25 0 0 5.25 123.5367 11.5132 Tm 9 0 0 9 411.0181 379.8898 Tm EMC EMC /P <>BDC (1,272)Tj ET EMC BT BT ET ( )Tj EMC EMC /P <>BDC 9 0 0 9 423.3885 401.8898 Tm BT BT (4,863)Tj /P <>BDC 7 0 0 7 54.5916 738.7654 Tm /P <>BDC /P <>BDC ( )Tj ET 7 0 0 7 490.8321 540.7654 Tm BT -.01 Tc EMC EMC EMC Your email address will not be published. -.02 Tc ET ( )Tj ( )Tj BT (37,653lbs )Tj 7 0 0 7 508.4124 661.7654 Tm ET This narrow body jet airliner had first rolled out on June 30, 1997 and shortly after was had its first test flight with he pilot Jim McRoberts in the cockpit. BT /P <>BDC 9 0 0 9 351.8271 203.8898 Tm ET ET The 800 is mainly used for passenger transport with its 526 seating capacity. EMC BT ET EMC BT BT EMC (Since all eight aircraft types are in)Tj ET EMC )Tj /P <>BDC especially during start. 9 0 0 9 394.0315 291.8898 Tm /P <>BDC (132,872)Tj -.02 Tc (7B27B3)Tj ET EMC Hi and thanks for stopping by. BT EMC /P <>BDC /P <>BDC BT 9 0 0 9 36.8504 456.8898 Tm ET (second payload scenario using the 85%)Tj (37,653)Tj BT 0 Tc ( )Tj ET EMC 7 0 0 7 54.7071 562.7654 Tm ET EMC ET EMC 6.5 0 0 6.5 347.0329 611.9529 Tm ( )Tj EMC 7 0 0 7 403.478 474.7654 Tm EMC /P <>BDC 0 Tc ( )Tj ET ( )Tj ( )Tj /P <>BDC EMC (family of aircraft, despite increases in)Tj -.02 Tc EMC ET 7 0 0 7 187.0858 199.9528 Tm -.02 Tc ( )Tj 6.5 0 0 6.5 376.7644 742.9529 Tm BT 9 0 0 9 394.0123 588.8898 Tm 0 Tc EMC ET 9 0 0 9 232.4217 236.8898 Tm ET BT (163)Tj EMC ET 10 0 0 10 407.56 814.1973 Tm 0 Tc ET EMC /P <>BDC ET BT BT 9 0 0 9 420.5961 38.3073 Tm 9 0 0 9 564.4508 324.8898 Tm Neither the 737-800 nor the 737-8)Tj 9 0 0 9 562.8273 764.8898 Tm -.02 Tc BT BT /P <>BDC ET EMC ET /P <>BDC EMC ( )Tj BT 7 0 0 7 508.4124 375.7654 Tm /Artifact <>BDC .014984 824.882 572.583 17.008 re 7 0 0 7 521.4089 11.5132 Tm Flight crew can select fwd or aft tanks but normal practice is to use both ET BT /P <>BDC /P <>BDC ( )Tj ET ( )Tj ET /P <>BDC /P <>BDC ET ET (passenger seat capacity as the older models)Tj BT BT /P <>BDC (136)Tj EMC ET ( )Tj f ET ET BT EMC 9 0 0 9 326.8538 60.8898 Tm EMC EMC /P <>BDC ( )Tj EMC ( )Tj 9 0 0 9 394.0315 181.8898 Tm ET ( A)Tj BT BT ET BT 7 0 0 7 125.6292 89.7654 Tm ET /P <>BDC ( C)Tj BT 9 0 0 9 339.3695 192.8898 Tm ET ( )Tj BT EMC 8 0 0 8 124.845 577.9528 Tm EMC BT BT 6.5 0 0 6.5 191.63 624.9529 Tm (better for the A321neo due to its increased)Tj ET BT ET (484)Tj EMC 9 0 0 9 550.3917 456.8898 Tm ET 0 Tc BT /P <>BDC 9 0 0 9 209.2378 324.8898 Tm ( )Tj 7 0 0 7 141.7322 276.9528 Tm ET ET EMC 10 0 0 10 54.3039 794.2914 Tm BT 0 Tc (0.0113)Tj 0 Tc It works by transferring fuel from the aux /GS2 gs /P <>BDC /P <>BDC EMC /P <>BDC EMC 6.5 0 0 6.5 331.0061 722.9529 Tm /P <>BDC EMC 15 w BT On older aircraft the trimmers were accessible from the ( )Tj ( )Tj EMC (The block- and flight- \(take-off to)Tj BT 9 0 0 9 394.0123 654.8898 Tm (7,379)Tj ET 0 Tc (page 21\))Tj -.01 Tc 9 0 0 9 554.0057 566.8898 Tm ET ET 7 0 0 7 158.74 496.7654 Tm /P <>BDC /Artifact <>BDC ET EMC ET BT BT BT BT ET -.02 Tc ( )Tj 7 0 0 7 429.157 738.9528 Tm ( )Tj 0 Tc Can you please tell me where to look for the cabin height,width, seat height, width and door to door length. 0 Tc /P <>BDC BT 7 0 0 7 456.2165 540.7654 Tm EMC 0 Tc EMC EMC 9 0 0 9 382.7137 93.8898 Tm ( )Tj ( )Tj BT ET BT 9 0 0 9 392.5848 346.8898 Tm EMC -.02 Tc -.02 Tc /P <>BDC EMC /P <>BDC BT BT ET ( )Tj (0.0127)Tj 7 0 0 7 82.8504 386.9528 Tm BT /P <>BDC EMC 9 0 0 9 429.7348 104.8898 Tm 0 Tc ET EMC ET (342,312)Tj 0 Tc EMC /P <>BDC W n /P <>BDC ( )Tj 7 0 0 7 381.1608 562.7654 Tm /P <>BDC 7 0 0 7 427.7291 232.9528 Tm 9 0 0 9 53.8578 291.8898 Tm /P <>BDC 0 Tc ET 7 0 0 7 113.1366 221.9528 Tm ( )Tj /P <>BDC ET 9 0 0 9 542.7234 489.8898 Tm ET /P <>BDC S ET ET 7 0 0 7 141.7322 144.9528 Tm EMC ( )Tj ( )Tj ( )Tj ( )Tj /P <>BDC ET 9 0 0 9 418.1167 335.8898 Tm BT 0 Tc 7 0 0 7 403.478 639.7654 Tm 7 0 0 7 37.5838 254.9528 Tm 36.85 541.416 340.159 263.624 re ( )Tj /P <>BDC
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