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consumption at ISA conditions for a reference weight of 60 000 kg
Interpolate the remaining distance of 408 nm at FL 180
Fuel = 2 981 kg
Time = 1 h 11 min
Correction due to actual in-cruise weight :
◂Fuel = +1 kg per 1 000 kg above reference weight
◂Fuel = +1 kg × (74.5 – 60) = 14.5 kg
RESULT :
Total Fuel = 2 981 + 472 + 14.5 = 3 468 kg
Time = 1 h 11 min + 12 min = 1 h 13 min
EXAMPLE
Applicable to:
GIVEN :
GW at engine failure = 70 000 kg
FL at engine failure = 350
Temperature = ISA
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ONE ENGINE INOPERATIVE - GENERAL
A318/A319/A320/A321 FLEET PER-CRZ-OEI-GEN-20 P 3/8
FCOM 19 AUG 10
Distance to diversion airport = 500 nm
Speed selected before dispatch = 350 kt
Cruise level for diversion
Selected before dispatch = FL 180
FIND :
Descent to cruise level :
(Refer to PER-DES-OEI-ETO DESCENT - M.80/350KT - 1 ENGINE OUT)
Distance = 178 - 92 = 86 nm
Fuel = 1 030 - 651 = 379 kg
Time = 24.1 - 13.1 = 11 min
Cruise
Weight = 70 000 - 379 = 69 621 kg
Distance = 500 - 86 = 414 nm
Determine (Refer to PER-CRZ-OEI-ICQ-20 IN CRUISE QUICK CHECK VMO) time and fuel
consumption at ISA conditions for a reference weight of 55 000 kg
Interpolate the remaining distance of 414 nm at FL 180
Fuel = 2 804 kg
Time = 1 h 11 min
Correction due to actual in-cruise weight : no correction here
◂Fuel = +3 kg per 1 000 kg above reference weight
◂Fuel = +3 kg × (69.6 – 55) ~ 44 kg
RESULT :
Total Fuel = 2 804 + 44 + 379 = 3 227 kg
Time = 1 h 11 min + 11 min = 1 h 22 min
EXAMPLE
Applicable to:
GIVEN :
GW at engine failure = 70 000 kg
FL at engine failure = 350
Temperature = ISA
Distance to diversion airport = 500 nm
Speed selected before dispatch = 350 kt
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ONE ENGINE INOPERATIVE - GENERAL
A318/A319/A320/A321 FLEET PER-CRZ-OEI-GEN-20 P 4/8
FCOM 19 AUG 10
Cruise level for diversion
Selected before dispatch = FL 180
FIND :
Descent to cruise level :
(Refer to PER-DES-OEI-ETO DESCENT - M.80/350KT - 1 ENGINE OUT)
Distance = 184 - 94 = 90 nm
Fuel = 1 047 - 651 = 396 kg
Time = 24.8 - 13.3 = 11.5 min
Cruise
Weight = 70 000 - 396 = 69 604 kg
Distance = 500 - 90 = 410 nm
Determine (Refer to PER-CRZ-OEI-ICQ-20 IN CRUISE QUICK CHECK VMO) time and fuel
consumption at ISA conditions for a reference weight of 55 000 kg
Interpolate the remaining distance of 410 nm at FL 180
Fuel = 2 561 kg
Time = 1 h 13 min
Correction due to actual in-cruise weight
◂Fuel = +2 kg per 1 000 kg above reference weight
◂Fuel = +2 kg × (69.6 – 55) ~ 29 kg
RESULT :
Total Fuel = 2 561 + 29 + 396 = 2 986 kg
Time = 1 h 13 min + 12 min = 1 h 25 min
EXAMPLE
Applicable to:
GIVEN :
GW at engine failure = 68 000 kg
FL at engine failure = 350
Temperature = ISA
Distance to diversion airport = 500 nm
Speed selected before dispatch = 350 kt
Cruise level for diversion
Selected before dispatch = FL 180
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
CRUISE
ONE ENGINE INOPERATIVE - GENERAL
A318/A319/A320/A321 FLEET PER-CRZ-OEI-GEN-20 P 5/8
FCOM 19 AUG 10
FIND :
Descent to cruise level :
(Refer to PER-DES-OEI-ETO DESCENT - M.80/350KT - 1 ENGINE OUT)
Distance = 190 - 95 = 95 nm
Fuel = 1 106 - 672 = 434 kg
Time = 25.8 - 13.7 = 12.1 min
Cruise
Weight = 68 000 - 434 = 67 566 kg
Distance = 500 - 95 = 405 nm
Determine (Refer to PER-CRZ-OEI-ICQ-20 IN CRUISE QUICK CHECK VMO) time and fuel
consumption at ISA conditions for a reference weight of 55 000 kg
Interpolate the remaining distance of 405 nm at FL 180
Fuel = 2 669 kg
Time = 1 h 09 min
Correction due to actual in-cruise weight :
◂Fuel = +2 kg per 1 000 kg above reference weight
◂Fuel = +2 kg × (67.6 – 55) ~ 26 kg
RESULT :
Total Fuel = 2 669 + 26 + 434 = 3 129 kg
Time = 1 h 09 min + 12 min = 1 h 21 min
EXAMPLE
Applicable to:
GIVEN :
GW at engine failure = 70 000 kg
FL at engine failure = 350
Temperature = ISA
Distance to diversion airport = 600 nm
Speed selected before dispatch = 350 kt
Cruise level for diversion
Selected before dispatch = FL 180
FIND :
Descent to cruise level :
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
　
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