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.
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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, ft and descent to [DELETED] ft above the destination airport are conducted in [DELETED] ISA conditions. Climb and descent speeds below [DELETED] ft shall be [DELETED] knots CAS.
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