Climb from Sample Clauses
The "Climb from" clause defines the minimum altitude or flight level at which an aircraft must begin its ascent after takeoff or when departing from a specific point. In practice, this clause specifies the exact location or condition—such as after passing a runway end or a navigational waypoint—where the climb should commence, ensuring that the aircraft follows a safe and predictable vertical profile. Its core function is to enhance flight safety and airspace management by preventing premature climbs that could conflict with other traffic or terrain.
Climb from pressure altitude up to cruise altitude using maximum climb thrust, cruise at a fixed Mach number of ** at pressure altitudes beween ** and descent to ** pressure altitude are conducted in ** conditions. Climb and descent speeds below ** shall be **. A wind component of ** of cruise wind has been considered during climb and descent.
Climb from pressure altitude up to cruise altitude using maximum climb thrust, cruise at a fixed Mach number of ** at pressure altitudes between ** and descent to ** pressure altitude are conducted in ISA+10°C conditions. Climb and descent speeds below ** shall be **. A wind component of **of cruise wind has been considered during climb and descent. ▇▇▇ — Airbus A330 Purchase Agreement EXECUTION PRIVILEGED AND CONFIDENTIAL **Confidential Treatment Requested.
Climb from pressure altitude up to cruise altitude using maximum climb thrust, cruise at a fixed Mach number of ** at pressure altitudes of ** and descent to ** pressure altitude are conducted in ** conditions. Climb and descent speeds below ** will be ** knots CAS.
Climb from. [DELETED] ft above the departure airport up to optimum cruise altitude using maximum climb thrust, cruise at a fixed Mach number of [DELETED] at a pressure altitude of [DELETED] ft/[DELETED] ft,/ [DELETED] ft, and descent to [DELETED] ft above the destination airport are conducted in [DELETED] conditions. Climb and descent speeds below [DELETED] ft shall be [DELETED] knots CAS.
Climb from above the departure airport up to cruise altitude using maximum climb thrust and cruise at a fixed Mach number of ** at pressure altitudes of ** above the destination airport are conducted in ** conditions. Climb and descent profiles are respectively ** Mach number and **.
Climb from. 2,635 ft pressure altitude up to cruise altitude using maximum climb thrust, cruise at a fixed Mach number of M=0.82 at pressure altitudes of 35,000 ft and 39,000 ft and descent to 1,639 ft pressure altitude are conducted in ISA+10 degrees C conditions. Climb and descent speeds below 10,000 ft will be 250 knots CAS. A wind component of 70% of cruise wind has been considered during climb and descent.