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OPERATING MANUAL
PERFORMANCE
TWO ENGINES INOPERATIVE
DESCENT - STANDARD STRATEGY
A330/A340 FLEET PER-TEI-DES-10 P 3/4
FCOM 19 AUG 10
DESCENT AT GREEN DOT SPEED - ISA + 15
Applicable to:
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
TWO ENGINES INOPERATIVE
DESCENT - STANDARD STRATEGY
A330/A340 FLEET PER-TEI-DES-10 P 4/4
FCOM 19 AUG 10
DESCENT AT GREEN DOT SPEED - ISA + 20
Applicable to:
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
TWO ENGINES INOPERATIVE
DESCENT - DESCENT TO LANDING
A330/A340 FLEET PER-TEI-DES-20 P 1/2
FCOM 19 AUG 10
DESCENT TO LANDING
Applicable to:
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
TWO ENGINES INOPERATIVE
DESCENT - DESCENT TO LANDING
Intentionally left blank
A330/A340 FLEET PER-TEI-DES-20 P 2/2
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
TWO ENGINES INOPERATIVE
DESCENT - GENERAL
A330/A340 FLEET PER-TEI-DES-GEN P 1/2
FCOM 19 AUG 10
GENERAL
Applicable to:
Descent tables are established for normal descent speed M .82/300 kt/250 kt and emergency
descent at MMO/VMO with airbrakes extended down to 1 500 ft with :
• Normal air conditioning (Packs NORM/Cargo cooling OFF or Packs LO/Cargo cooling NORM)
• CG = 30 %
• Anti ice OFF
For normal descent, cabin vertical speed is limited to 350 ft/min.
GENERAL
Applicable to: ,
Descent tables are established for normal descent speed M .80/300 kt/250 kt and emergency
descent at MMO/VMO with airbrakes extended down to 1 500 ft with :
Normal air conditioning (Packs NORM/Cargo cooling OFF ‐ or Packs LO/Cargo cooling NORM)
‐ CG = 30 %
‐ Anti ice OFF
For normal descent, cabin vertical speed is limited to 350 ft/min.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
TWO ENGINES INOPERATIVE
DESCENT - GENERAL
Intentionally left blank
A330/A340 FLEET PER-TEI-DES-GEN P 2/2
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
TWO ENGINES INOPERATIVE
DESCENT - ALL ENGINES OPERATIVE
A330/A340 FLEET PER-TEI-DES-AEO-STD P 1/2
FCOM 19 AUG 10
STANDARD
DESCENT
Applicable to:
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
TWO ENGINES INOPERATIVE
DESCENT - ALL ENGINES OPERATIVE
A330/A340 FLEET PER-TEI-DES-AEO-STD P 2/2
FCOM 19 AUG 10
DESCENT
Applicable to: ,
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
TWO ENGINES INOPERATIVE
DESCENT - ALL ENGINES OPERATIVE
A330/A340 FLEET PER-TEI-DES-AEO-EMG P 1/2
FCOM 19 AUG 10
EMERGENCY
EMERGENCY DESCENT
Applicable to:
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
TWO ENGINES INOPERATIVE
DESCENT - ALL ENGINES OPERATIVE
A330/A340 FLEET PER-TEI-DES-AEO-EMG P 2/2
FCOM 19 AUG 10
EMERGENCY DESCENT
Applicable to: ,
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
TWO ENGINES INOPERATIVE
DESCENT - ONE ENGINE INOPERATIVE
A330/A340 FLEET PER-TEI-DES-OEI-STD P 1/4
FCOM 19 AUG 10
STANDARD
EXAMPLE
Applicable to:
GIVEN
GW at engine failure = 200 000 kg
FL at engine failure = 350
Temperature = ISA
Distance to destination
airport
= 2 500 nm
No wind
FIND
LRC ceiling : FL 330
(Refer to PER-CRZ-OEI-ALT-10 GROSS CEILINGS AT LONG RANGE AND GREEN DOT
SPEEDS)
Descent to cruise
level
: (FL 310)
Refer to PER-TEI-DES-OEI-STD DESCENT - M.82/300KT - 1 ENGINE OUT
Distance = 223 – 160 = 63 nm
Fuel = 2 732 – 1 958 = 774 kg
Time = 30 – 22 = 8 min
Cruise at long range speed (FL 310) to landing.
(Weight = 200 000 – 774= 199 226 kg : Distance = 2 500 – 63 = 2 437 nm)
Determine on (Refer to 00002633 **Not found**) time and fuel consumption at ISA conditions
for a reference weight of 160 000 kg. Interpolate the remaining air distance of 2 437 nm at
FL 310.
Fuel : 28 531 kg
Time : 6 h 16 min
Correction due to actual in-cruise weight
▹Fuel􀀃=􀀃+89.1􀀃kg􀀃per􀀃1􀀃000􀀃kg􀀃above􀀃reference􀀃weight􀀃
▹Fuel􀀃=􀀃+89.1􀀃kg􀀃×􀀃(199􀀃–􀀃160)􀀃▹􀀃3􀀃475􀀃kg􀀃
RESULT
Total Fuel = 28 531 + 3 475 + 774 = 32 780 kg
A330/A340 FLIGHT CREW
OPERATING MANUAL
PERFORMANCE
　
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