EMC EMC The fuel flow indication is integrated over time to calculate the fuel used for each engine. ( )Tj EMC ET EMC BT ( )Tj EMC /F1 1 Tf /P <>BDC EMC /P <>BDC [(CFM L)17.1(E)-8.1(AP-1A26)]TJ ET 9 0 0 9 518.9756 49.1073 Tm /P <>BDC (equipped with the more fuel-efficient CFM)Tj 6.5 0 0 6.5 296.3606 735.9529 Tm 6 0 0 6 277.7064 715.9528 Tm EMC EMC ( )Tj ( )Tj /P <>BDC ET BT 0 Tc /P <>BDC ET ET BT BT EMC BT BT ET 0 Tc ( )Tj EMC BT BT -.02 Tc EMC ET BT ET ( )Tj BT -.02 Tc Im glad you got something out of our site that was helpful. ET )Tj 0 Tc 7 0 0 7 158.74 441.7654 Tm (directly compare the fuel burn and)Tj BT /P <>BDC -.005 Tc 7 0 0 7 456.2165 441.7654 Tm BT ( )Tj .0081 Tc -.02 Tc BT 0 Tc ET (or comfort plus, depending on the airline. BT (132,872)Tj EMC 9 0 0 9 194.9803 478.8898 Tm ( )Tj 7 0 0 7 95.225 11.5132 Tm ET ET ET ET -.02 Tc ET ET /P <>BDC ET 7 0 0 7 230.7317 672.9528 Tm ET -.02 Tc ET /P <>BDC ET EMC 7 0 0 7 230.7317 276.9528 Tm 7 0 0 7 404.101 430.7654 Tm /Artifact <>BDC ET /P <>BDC EMC EMC 7 0 0 7 53.8582 749.7654 Tm 7 0 0 7 380.2788 287.7654 Tm ( )Tj BT ET /P <>BDC 9 0 0 9 532.3544 214.8898 Tm BT 9 0 0 9 362.6813 357.8898 Tm EMC ET /P <>BDC ( )Tj EMC ( )Tj 7 0 0 7 82.8504 320.9528 Tm /P <>BDC (96,500)Tj EMC .023 .567 .626 RG EMC (CFM56-7B27B3)Tj ET BT ET The aircraft look like standard -800s, so why the difference? /P <>BDC EMC (the BOS-LAX \(Los Angeles\) route. ET q -.02 Tc EMC ET Can you confirm if Im right or wrong? ( )Tj .014984 841.89 609.45 -841.89 re BT BT /P <>BDC BT /P <>BDC 7 0 0 7 491.7142 518.7654 Tm ET 7 0 0 7 362.3891 364.9528 Tm 0 Tc ( )Tj EMC BT 7 0 0 7 338.6433 441.7654 Tm ( )Tj EMC BT ET -.01 Tc ET 0 Tc 7 0 0 7 446.5009 672.7654 Tm ET ET 9 0 0 9 68.0314 401.8898 Tm BT BT BT /P <>BDC 7 0 0 7 380.2788 298.7654 Tm /P <>BDC BT /P <>BDC /P <>BDC 6.5 0 0 6.5 477.8064 702.9529 Tm 9 0 0 9 408.1889 192.8898 Tm (l)Tj 0 Tc ET (65,688)Tj ET EMC ET The website is currently in the process of optimizing and will have further functions added in order to improve the usability. /P <>BDC /P <>BDC ET /P <>BDC 0 Tc BT ET -.01 Tc ET BT /P <>BDC ET less heating from the smaller hydraulic system A. ET 0 Tc ET BT BT 7 0 0 7 60.6117 342.7654 Tm ET EMC 0 Tc EMC ET ( )Tj ( )Tj ET EMC /P <>BDC /Artifact <>BDC 7 0 0 7 439.7405 595.9528 Tm ( )Tj ( )Tj BT /P <>BDC /P <>BDC 6 0 0 6 340.4597 743.9528 Tm BT /P <>BDC 0 Tc ET from cockpit door to the kitchen alley . .151 .147 .15 rg /P <>BDC /P <>BDC ET BT EMC (they are replacing. BT BT /P <>BDC ET .41 .161 .508 RG ( )Tj ( )Tj -.02 Tc EMC (the 737-9 reduces the block fuel burn)Tj ET 9 0 0 9 184.4215 434.8898 Tm BT (190,800)Tj EMC (scenario 2, where all types carry an 85%)Tj EMC /P <>BDC BT ( )Tj BT 6 0 0 6 389.8214 701.9528 Tm /P <>BDC /P <>BDC /P <>BDC BT ( )Tj /P <>BDC /P <>BDC /P <>BDC ET ET BT EMC EMC 7 0 0 7 338.6433 397.7654 Tm 6.5 0 0 6.5 397.0428 532.9529 Tm EMC ET EMC The Boeing 777-200 has a maximum fuel capacity of 31,000 gallons or 117,347 liters. BT EMC (between different aircraft types impossible)Tj (The 737-9 has an 11.2% to 12.7%)Tj ( )Tj 0 Tc 0 Tc EMC EMC /P <>BDC (2,376)Tj ( )Tj /GS1 gs -.01 Tc ET BT ( )Tj BT ET EMC ET EMC 0 Tc /P <>BDC ET /P <>BDC (339-353)Tj EMC (11.0:1)Tj ( )Tj BT (\(see table, page 21\))Tj 6.5 0 0 6.5 233.8677 532.9529 Tm BT 9 0 0 9 394.0123 467.8898 Tm /P <>BDC EMC EMC 9 0 0 9 346.8148 104.8898 Tm (A potential operator would need to)Tj BT ET Therefore, the Boeing 777-200 can carry 24,125 more gallons of fuel than the Boeing 737-800. /P <>BDC ET /Artifact <>BDC ET BT EMC -.02 Tc /P <>BDC ET EMC 7 0 0 7 196.5683 221.7654 Tm ET ET BT EMC ET /P <>BDC -.01 Tc /P <>BDC /P <>BDC BT 7 0 0 7 473.8245 309.9528 Tm 0 Tc ET BT EMC 0 Tc EMC ET [(M)21(T)39.1(O)7.1(W)0( - lbs)]TJ 7 0 0 7 355.5753 573.7654 Tm /P <>BDC In contrast, the 737-8s performance)Tj ( )Tj EMC ( )Tj (141,270)Tj EMC ET BT ET ( )Tj EMC (performed with both engines operating to)Tj ET ET BT 6 0 0 6 215.373 715.9528 Tm Therefore,)Tj -.02 Tc ET EMC EMC ( )Tj 7 0 0 7 230.7317 100.9528 Tm 9 0 0 9 530.5354 665.8898 Tm EMC BT ( )Tj EMC /P <>BDC /P <>BDC ET /P <>BDC EMC /P <>BDC (38,168)Tj /P <>BDC /P <>BDC ( )Tj /P <>BDC EMC 9 0 0 9 199.3017 401.8898 Tm (120-128)Tj ET ET (720)Tj 7 0 0 7 199.5784 496.7654 Tm /P <>BDC /P <>BDC If you switch on the centre tank pumps and the LP lights /P <>BDC ET EMC ( )Tj 7 0 0 7 158.74 166.7654 Tm EMC EMC ET EMC /P <>BDC ( )Tj ET /P <>BDC ET ( )Tj 1 i .001 Tc EMC /P <>BDC ET 7 0 0 7 536.3849 111.7654 Tm five ground) under different ground and flight conditions to demonstrate the EMC /P <>BDC 0 Tw BT /P <>BDC ET The aux tanks are located at EMC ET /P <>BDC /P <>BDC ( )Tj EMC ET /P <>BDC (The later generation aircraft are set to)Tj BT BT 0 Tc /P <>BDC /P <>BDC EMC ET BT BT 515.808 82.238 l BT EMC ET EMC (1,824)Tj /P <>BDC 7 0 0 7 430.039 683.9528 Tm ET ET BT ET BT BT (0.0117)Tj /P <>BDC /P <>BDC ( )Tj (A321neo)Tj (\(see table, page 19\))Tj ET It has a maximum takeoff weight of about 80,000 kg (175,000 lbs). ( )Tj EMC ( )Tj BT /P <>BDC EMC 0 Tc (The overflight and airport charges are)Tj BT ET BT ET EMC BT ET EMC 9 0 0 9 411.0097 104.8898 Tm ET ( )Tj BT ( )Tj EMC BT 0 Tc BT (0.0149)Tj BT BT 7 0 0 7 337.6855 518.9528 Tm BT /P <>BDC ET tank. /P <>BDC EMC -.02 Tc EMC 9 0 0 9 53.8578 423.8898 Tm /P <>BDC ET -.01 Tc BT EMC ( )Tj BT The engine)Tj 9 0 0 9 36.8504 302.8898 Tm ET 0 Tc /P <>BDC ET 7 0 0 7 491.7142 529.7654 Tm 7 0 0 7 490.7815 221.9528 Tm EMC BT BT ET 0 Tc /P <>BDC EMC /P <>BDC (1,089)Tj ET (A321neo)Tj EMC 7 0 0 7 539.9176 11.5129 Tm ET ( )Tj ET [(v)21(ariant)]TJ Our Math Says It Isn't. /P <>BDC BT ( )Tj ( )Tj /P <>BDC /OC /MC4769 BDC ET ET /P <>BDC /P <>BDC -.02 Tc BT ( )Tj BT /P <>BDC EMC EMC (aircraft types, all the flights were evaluated)Tj -.02 Tc /P <>BDC BT (39,270)Tj BT BT /P <>BDC 9 0 0 9 394.0237 423.8898 Tm EMC (382)Tj BT ET /P <>BDC ET ET S BT EMC BT ET 9 0 0 9 411.0181 236.8898 Tm ET (component, while the 737-900ER\(W\) has)Tj ET /P <>BDC /P <>BDC EMC EMC ET 7 0 0 7 487.0872 11.5129 Tm BT /P <>BDC It is produced in the Renton plant in Washington by Boeing Commercial Airplanes. /P <>BDC 8 0 0 8 38.4438 661.9528 Tm 0 Tc /P <>BDC /P <>BDC EMC 6 0 0 6 365.7265 729.9528 Tm ET /P <>BDC ET 7 0 0 7 439.7405 463.9528 Tm /P <>BDC ET 9 0 0 9 36.8504 280.8898 Tm EMC /P <>BDC EMC EMC 0 Tc (172,992)Tj BT This fuel would give a ET 7 0 0 7 518.4953 287.9528 Tm )Tj EMC EMC BT EMC 7 0 0 7 199.5784 694.7654 Tm 7 0 0 7 456.2165 166.7654 Tm 9 0 0 9 181.8233 49.8898 Tm 9 0 0 9 209.6398 489.8898 Tm (0.0113)Tj (this evaluation. /P <>BDC EMC /GS2 gs /P <>BDC ET ET ( )Tj EMC ET EMC Hello! (0.0124)Tj /GS2 gs ET 7 0 0 7 387.0932 441.9528 Tm ( )Tj 0 Tc BT /P <>BDC /P <>BDC ET 0 Tc EMC ET EMC (2,094)Tj (150 passengers on the A320ceo, A320neo,)Tj ET /P <>BDC /P <>BDC ET /P <>BDC BT ( )Tj ( )Tj ET 7 0 0 7 439.7405 705.9528 Tm /P <>BDC ET ( )Tj BT EMC BT 9 0 0 9 394.0157 390.8898 Tm 7 0 0 7 118.104 606.7654 Tm EMC [(BOS-L)-31(A)-24.9(X)]TJ ET 0 Tc ET ET EMC ET BT .151 .147 .15 rg BT 7 0 0 7 241.5317 408.9528 Tm 7 0 0 7 37.6993 221.9528 Tm ET ( )Tj -.02 Tc EMC (CFM56-7B27B3 installed on the 737-)Tj 9 0 0 9 215.4409 412.8898 Tm ( )Tj 7 0 0 7 355.5753 584.7654 Tm /P <>BDC BT 0 Tc BT 0 Tc (127)Tj (415,112)Tj (0.0126)Tj /P <>BDC /P <>BDC /P <>BDC EMC EMC ET ( )Tj /P <>BDC BT ET 9 0 0 9 232.4217 324.8898 Tm ( )Tj BT ( )Tj fuel pumps will automatically shut off when they detect a low output pressure. ET EMC /P <>BDC BT EMC EMC BT /P <>BDC /P <>BDC 9 0 0 9 531.3621 148.8898 Tm EMC BT (2,347)Tj ( )Tj ET (148,504)Tj EMC BT /P <>BDC ET BT -.02 Tc BT 0 Tc EMC EMC (payload carried. ET EMC BT BT 9 0 0 9 528.248 643.8898 Tm 9 0 0 9 394.0315 555.8898 Tm ET EMC EMC 8 0 0 8 43.6039 745.9528 Tm 7 0 0 7 457.0984 408.7654 Tm /P <>BDC /P <>BDC (and in fuel burn per ASM. /P <>BDC ET BT ET 9 0 0 9 252.5351 214.8898 Tm ( )Tj 6.5 0 0 6.5 129.3816 598.9529 Tm 7 0 0 7 456.4753 617.7654 Tm waiting with pax EMC EMC /P <>BDC EMC ET BT 7 0 0 7 158.74 617.7654 Tm 7 0 0 7 539.8962 716.9528 Tm ( )Tj (170)Tj -.02 Tc BT BT BT 0 Tc ( )Tj 7 0 0 7 403.478 562.7654 Tm (166-175)Tj EMC EMC 9 0 0 9 372.2987 181.8898 Tm EMC ET (even though the two have the same)Tj /P <>BDC 0 Tc -.02 Tc ( )Tj EMC BT BT EMC BT ET EMC ET BT -.02 Tc /P <>BDC BT BT BT /P <>BDC ( )Tj EMC /P <>BDC ( )Tj ET -.02 Tc ( )Tj ( )Tj BT ET 7 0 0 7 490.8321 199.7654 Tm ET (bypass ratio than the A320/321neo. 0 Tc EMC -.01 Tc 7 0 0 7 354.7351 683.7654 Tm BT /P <>BDC /P <>BDC BT ET 6.5 0 0 6.5 448.8744 624.9529 Tm BT EMC 7 0 0 7 158.74 89.7654 Tm 6.5 0 0 6.5 225.3721 585.9529 Tm /P <>BDC -.01 Tc /P <>BDC 8 0 0 8 141.7322 760.9528 Tm ET 9 0 0 9 176.5402 280.8898 Tm This)Tj ( )Tj Economy-plus is also)Tj BT BT EMC ( )Tj -.02 Tc EMC BT ET ET /P <>BDC <>/ExtGState<>/Properties<>>> EMC EMC EMC ( )Tj ET 9 0 0 9 53.8338 82.8898 Tm 13 0 0 13 53.8582 137.8898 Tm /P <>BDC ET BT BT ( )Tj /P <>BDC 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. (economics of the aircraft types with more)Tj /P <>BDC (1,161)Tj /P <>BDC EMC EMC ET 6.5 0 0 6.5 192.3255 742.9529 Tm (capacity, so that payload is reduced to)Tj EMC EMC 7 0 0 7 158.74 397.7654 Tm ET (20)Tj [(OM)8(M)-13(E)-25(R)7(C)8(E)]TJ ( )Tj ( )Tj ET BT (1,800 - )Tj ET 7 0 0 7 508.4124 188.7654 Tm /P <>BDC EMC BT ET 0 Tc [(CFM L)17.1(E)-8.1(AP-1B27B1)]TJ /P <>BDC /P <>BDC EMC 0 Tc 9 0 0 9 181.2747 170.8898 Tm BT 7 0 0 7 230.7317 573.9528 Tm 9 0 0 9 215.433 357.8898 Tm BT (0.0177)Tj (to in-flight service levels will increase seat)Tj 7 0 0 7 543.7693 11.5132 Tm ET /P <>BDC EMC BT EMC /P <>BDC /P <>BDC BT /P <>BDC (larger engines, but again the aircraft)Tj 9 0 0 9 75.3887 489.8898 Tm 6.5 0 0 6.5 296.4841 663.9529 Tm (2,517)Tj (2,013)Tj ( )Tj EMC .0081 Tc ET BT ( )Tj ET [(Seat configur)10(ation)]TJ /P <>BDC /F1 1 Tf ET BT 7 0 0 7 54.7071 573.7654 Tm /P <>BDC ( )Tj BT 6.5 0 0 6.5 499.597 558.9529 Tm /P <>BDC ( )Tj )Tj BT /P <>BDC 7 0 0 7 37.0536 606.9528 Tm 9 0 0 9 215.4409 423.8898 Tm BT ET BT BT 0 Tc EMC /P <>BDC EMC BT (The block- and flight- \(take-off to)Tj /P <>BDC 7 0 0 7 535.5029 78.7654 Tm ET EMC [(SS)-9.1(U)8(E)]TJ ( )Tj EMC 7 0 0 7 158.74 364.7654 Tm BT 5.25 0 0 5.25 64.5461 11.5129 Tm (Both the A321ceo and 737-900ER\(W\))Tj After -.02 Tc BT ET EMC ( )Tj /P <>BDC 7 0 0 7 337.4684 661.9528 Tm ( A)Tj (carried - lbs)Tj /P <>BDC .559 .331 .619 rg (170)Tj 7 0 0 7 507.7893 111.7654 Tm ET 7 0 0 7 337.6855 276.9528 Tm ET /P <>BDC BT EMC /P <>BDC BT /P <>BDC 0 Tc EMC (The A320 family is offered with the)Tj (CFM56-5B3/P)Tj ( )Tj ( )Tj /P <>BDC /P <>BDC EMC BT /P <>BDC ( )Tj ( )Tj (10)Tj BT the climb. EMC (283)Tj BT ET ET ET ET /P <>BDC EMC 9 0 0 9 373.87 258.8898 Tm Whilst bigger than the Embraer E-Jets, Boeing feels this is an optimum size range for a small city jet which can also be used for medium-haul international services. 7 0 0 7 125.6292 584.7654 Tm BT EMC 7 0 0 7 474.7064 342.9528 Tm /P <>BDC -.01 Tc .023 .567 .626 rg 0 Tc /P <>BDC EMC BT ET BT ET [(E)-7.8(P)16.1(T)9(E)-13.9(MBE)-16.9(R)]TJ 7 0 0 7 67.798 11.5132 Tm 9 0 0 9 36.8504 456.8898 Tm BT 7 0 0 7 354.6933 287.7654 Tm (379)Tj /P <>BDC f (the shorter sectors at 4.6%, and reduces to)Tj ET EMC /P <>BDC 7 0 0 7 387.0159 518.9528 Tm BT 7 0 0 7 141.7322 419.9528 Tm ( )Tj BT EMC EMC EMC ET ET BT ET /P <>BDC .41 .161 .508 rg EMC /P <>BDC (economy seats are at six-abreast. ( )Tj 7 0 0 7 158.74 67.7654 Tm (operational factors that also have to be)Tj EMC EMC /P <>BDC ( )Tj EMC -.02 Tc (lighter aircraft. EMC ET /P <>BDC EMC EMC (A321ceo)Tj BT (310,080)Tj BT BT 7 0 0 7 241.5317 507.9528 Tm ET 7 0 0 7 230.7317 529.9528 Tm ET /P <>BDC BT -.02 Tc BT BT BT /P <>BDC )Tj BT /P <>BDC BT EMC EMC BT /P <>BDC (follow in their footsteps, having already)Tj -.01 Tc /F6 1 Tf EMC EMC EMC /P <>BDC .41 .161 .508 rg ET ( )Tj /F4 1 Tf ET 7 0 0 7 241.5317 89.9528 Tm EMC BT BT BT ET 7 0 0 7 294.4014 628.7654 Tm EMC /P <>BDC EMC EMC -.02 Tc ( )Tj 6 0 0 6 418.9814 701.9528 Tm /P <>BDC (A320neo at 2.30 cents per ASM )Tj 56 0 0 56 36.8606 622.1944 Tm EMC -.02 Tc EMC BT The 747-800 can climb to 40,000 feet and will burn 0.44 nautical mile per gallon. EMC ET ( )Tj /P <>BDC 8 0 0 8 298.0262 760.9528 Tm 6.5 0 0 6.5 347.0393 565.9529 Tm 7 0 0 7 37.6993 364.9528 Tm BT BT ET ET ET EMC 0 Tc