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Using this procedure, the fuel required is the greatest of:
F1 = taxiA + tripAC + 10% Trip timeBC + alternateCD + holdingD + Additional
F2 = taxiA + tripAE + 10% Trip timeAE + alternateEF + holdingF + Additional
When comparing standard fuel planning to the redispatch procedure fuel planning, the maximum contingency fuel reduction is 10% of the trip time between A and B.
F1 = taxiA + tripAC + 10% Trip timeBC + alternateCD + holdingD + Additional
STD= taxiA + tripAC + 10% Trip timeAC + alternateCD + holdingD + Additional
2.2.6. ETOPS Procedure
Similar to JAR ETOPS Procedure (chapter 1.1.6)
2.2. Fuel Management
FAR 121 does not provide fuel management rules, but the operating manual has to address appropriate procedures. Operators usually adopt the following rules:
2.2.1 Minimum Fuel at Landing Airport
The remaining fuel in flight must be sufficient to proceed to an airport where a safe landing can be made. The minimum quantity of remaining fuel at landing is defined in the operating manual, and is usually equivalent to the final reserve (fuel quantity necessary to fly for a period of 30 to 45 minutes at 1,500 feet above the airport in ISA conditions at holding speed).
This rule applies to the destination airport, the destination alternate airport, or any en route alternate airport.
J. APPENDIX
1. APPENDIX 1 : ALTIMETRY - TEMPERATURE EFFECT
Here’s a concrete example: Consider the case of Switzerland’s Sion airport.
During an ILS approach on Runway 26, it is required to overfly given waypoints at given geometrical altitudes, whatever the temperature conditions (Figure J1). For example, at 21 Nm from the glide antenna, the aircraft must be at a height of 8,919 feet above the runway, or at a true altitude of 10,500 feet above mean sea level.
The transition altitude shown on Figure J1 is 16,000 feet, corresponding to a height of 14,419 feet.
Figure J2 provides the indicated altitude values to maintain the required true altitude for different temperature conditions:
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