MISSION DESCRIPTION Sample Clauses

MISSION DESCRIPTION. The equivalent still air distance is the actual route distance (range) corrected for the average winds. Head winds are negative. [***] have been used. The maximum take-off weight for each departure airport is based on the conditions specified in paragraph 2.0 and is in compliance with FAR 25 take-off requirements. The missions are flown in ISA conditions throughout. A fixed allowance of fuel dependent on take-off weight is considered for take-off and acceleration to initial climb speed at [***] ft above the airport elevation. Climb is made starting [***] ft above the airport elevation to the initial cruise pressure altitude specified in the table above using a climb speed schedule of [***] KCAS/ [***] M.
Sample 1
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MISSION DESCRIPTION. The equivalent still air range (stage length) is the actual route distance corrected for the average winds. Head winds are negative. The maximum take-off weight for each departure airport ("from") is based on the conditions specified in paragraph 2.0 and is in compliance with FAR 25 take-off requirements. The missions are flown in ISA conditions throughout. Climb is made starting at the airport elevation to the initial cruise pressure altitude specified in Table 1 above using a climb speed schedule of [***] KCAS/ [***] M. Cruise is at the pressure altitude specified in Table 1 at an average cruise Mach number of [***] M. Thrust during cruise is not to exceed maximum cruise thrust.
Sample 1
MISSION DESCRIPTION. The equivalent still air range (stage length) is the actual route distance corrected for the average winds. Head winds are negative. The maximum take-off weight for each departure airport ("from") is based on the conditions specified in paragraph 2.0 and is in compliance with FAR 25 take-off requirements. The missions are flown in ISA conditions throughout. Climb is made starting at the airport elevation to the initial cruise pressure altitude specified in Table 1 above using a climb speed schedule of [***] KCAS/ [***] M. Cruise is at the pressure altitude specified in Table 1 at an average cruise Mach number of [***] M. Thrust during cruise is not to exceed maximum cruise thrust. When a second cruise pressure altitude is specified in Table 1, a [***] ft step climb from the first to the second pressure altitude is made using a climb speed schedule of [***] KCAS/ [***] M. It is followed by a cruise at the second pressure altitude at an average cruise Mach number of [***] M.
Sample 1
MISSION DESCRIPTION. The equivalent still air range (stage length) is the actual route distance corrected for the average winds. The missions are flown in *** conditions throughout. Take-off is made with engines at full take-off thrust. Climb is made starting at *** above the airport elevation to the initial cruise pressure altitude specified in the table above using a climb speed schedule of ***. Cruise is at the pressure altitude specified in the table above at cruise Mach number of ***. Thrust during cruise is not to exceed *** thrust. When a second cruise pressure altitude is specified in Table 1, a step climb from the first to the second pressure altitude is made using a climb speed schedule of ***. It is followed by a cruise at the second pressure altitude at cruise Mach number of ***. Descent is made from the final cruise pressure altitude in the table above *** using a descent speed schedule of ***.
Sample 1
MISSION DESCRIPTION. The equivalent still air distance is the actual route distance (range) corrected for the average winds. Head winds are negative. 85% average winter winds (Boeing model) have been used. The maximum take-off weight for each departure airport is based on the conditions specified in paragraph 2.0 and is in compliance with FAR 25 take-off requirements. The missions are flown in ISA conditions throughout. A fixed allowance of fuel dependent on take-off weight is considered for take-off and acceleration to initial climb speed at 1500 ft above the airport elevation. Climb is made starting 1500 ft above the airport elevation to the initial cruise pressure altitude specified in the table above using a climb speed schedule of 250 KCAS/ 0.70 M. Cruise is at the pressure altitude specified in the table at an average cruise Mach number of 0.74 M. Thrust during cruise is not to exceed maximum cruise thrust.
Sample 1

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