PMDG 747-400 fuel planning
1 kg = 2.2 lb
Weights Pound (LB) Dry operation weight (DOW)= 394088 Maximum zero-fuel weight (MZFW)= 542500 Maximum Take-off weight (MTOW)= 875000 Maximum Landing weight (MLW)= 630000 Payload = Pax-weight + Cargo-weight ZFW= DOW + Payload < MZFW ================================================== ============ OSDI: Damascus OYSN: Sanaa Alternate: OYHD Distance:1155nm, Time:03:15, weather: calm ,Pressure altitude: FL390 ft From OSDI to OYSN Alt OYHD ================================================== ============ # Calculate ZFW Pax-weight=46620 lbs Cargo-weight=73500 lb - Payload=46620 + 73500 PAYLOAD = ((120120 lb)) - ZFW=394088 + 120120 ZFW=((514208 lb)) < 542500 we are ok ================================================== ============ # Calculate Trip fuel * For much better understanding please print out PMDG 02- Cruise and fuel planning manual ( Cruise and fuel planning 2-7 Table) Trip length Pressure altitude(feet) FL390 ______________________________________________ 1400 3:21 72.6 ______________________________________________ ==Trip Fuel for 3:21 min = ((72600 lb)) ================================================== ============ # Calculate Minimum landing fuel ( Cruise and fuel planning 2-13) - Minimum landing fuel international = 24000 lb - Minimum landing fuel domestic short haul = 19000 lb Landing weight = ZFW + Minimum landing fuel == Landing weight = 514208 + 19000 == Landig weight = ((533208 lb)) at OYSN ================================================== ============ # Calculate Alternate Fuel ( Cruise and fuel planning 2-9) Nam to Alternate Time to alternate Landing weight at Alternate __________________________________________________ _____________________ 100 0:30 541 lb to 630 lb __________________________________________________ ______________________ 8800 lb __________________________________________________ ______________________ == Alternate Fuel = ((8800 lb)) ================================================== ================= # Calculate Contingency fuel ( Cruise and fuel planning 2-14) Holdig fuel 60 min = 18000 lb 60 ------------------ 18000 45 ------------------ ? 45 x 18000 __________ = 13500 lb easy way to do it 60 == Holding fuel = ((13500 lb)) ================================================== =================== Now - Planned landig weight= ZFW + Minimum landing weight + Alternate fuel + Contingency fuel == Planned landing weight = 514208 + 19000 + 8800 + 13500 == Planned landing weight = ((555508 lb)) < 630000 we are ok ================================================== ==================== # Calculate Adjustment fuel ( Cruise and fuel planning 2-14) - adjustment fuel = Planned landing weight - Table discription weight == Adjustment fuel = 555508 - 475000 == Adjustment fuel = 80508 == Adjustment fuel = 80508 % 10000 == Adjustment fuel = 8.0508 ( Cruise and fuel planning 2-7 Table) FL390 _____ 880bs/hr == Adjustment fuel = 8.0508 X 880 == Adjustment fuel = ((7084.704 lb)) ================================================== ======================= # Calculate Total fuel - Total fuel= Trip fuel + Minimum landing fuel + Alternate fuel + Holding fuel + Adjustment fuel + Taxi fuel == Total fuel = 72600 + 19000 + 8800 + 13500 + 7084.704 + 2200 == Total fuel = ((123184.7 lb)) ================================================== ======================= # Calculate Take-off gross weight Taxi out weight = Total fuel + ZFW == Taxi out weight = 123184.7 + 514208 == Taxi out weight = ((637392.7 lb)) < 875000 lb we are ok to taxi out - Take-off gross weight = Taxi out weight - 2200 == TOGW = 637392.7 - 2200 == TOGW = ((635192.7 lb)) ================================================== ======================== # Calculate Reserves fuel - Reserves fuel= Minimum landing fuel + Alternate fuel + Holding fuel + 1/2 Contingency fuel == Reserves fuel = 19000 + 8800 + 6750 == Rserves fuel = ((34550 lb)) So please type in the fmc 34.55 for reserve. ================================================== ========================== # Calculate Intial Cruise alititude Eastbound = odd altitudes Wesbond = even altitudes Important TOGW= ((635192.7 lb)) ( Cruise and fuel planning 2-9) Maximum & Optimum Cruise Altitude Altiude optimum Wt Maximum Wt Time to burn fuel Wt FL370 600,000 lb 670,000 lb 1:22 So far our Intial altitude will be fl370 and after 1:22 we could make step climb to fl390 Tips fmc ICAO type 2000 VNAV information about optimum Altitudes Progress information about T/C , T/D , E/D, Step climb So please make it your own way Please take it or leave it |
رد: PMDG 747-400 fuel planning
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