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CS 29.61 Take-off distance: Category A
Available versions for ERULES-1963177438-5469
ED Decision 2003/16/RM
found in: CS-29 Amdt 11 - Large Rotercraft (Feb 2023)
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CS-29 Amdt 12 - La... (Mar 2026)
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CS 29.61 Take-off distance: Category A ED Decision 2003/16/RM (a) The normal take-off distance is the horizontal distance along the take-off path from the start of the take-off to the point at which the rotorcraft attains and remains at least 11 m (35 ft) above the take-off surface, attains and maintains a speed of at least VTOSS; and establishes a positive rate of climb, assuming the critical engine failure occurs at the engine failure point prior to the TDP. (b) For elevated heliports, the take-off distance is the horizontal distance along the take-off path from the start of the take-off to the point at which the rotorcraft attains and maintains a speed of at least VTOSS and establishes a positive rate of climb, assuming the critical engine failure occurs at the engine failure point prior to the TDP.
CS 29.61 Take-off distance: Category A ED Decision 2003/16/RM (a) The normal take-off distance is the horizontal distance along the take-off path from the start of the take-off to the point at which the rotorcraft attains and remains at least 11 m (35 ft) above the take-off surface, attains and maintains a speed of at least VTOSS; and establishes a positive rate of climb, assuming the critical engine failure occurs at the engine failure point prior to the TDP. (b) For elevated heliports, the take-off distance is the horizontal distance along the take-off path from the start of the take-off to the point at which the rotorcraft attains and maintains a speed of at least VTOSS and establishes a positive rate of climb, assuming the critical engine failure occurs at the engine failure point prior to the TDP.
#### CS 29.61 Take-off distance: Category A *ED Decision 2003/16/RM* (a) The normal take-off distance is the horizontal distance along the take-off path from the start of the take-off to the point at which the rotorcraft attains and remains at least 11 m (35 ft) above the take-off surface, attains and maintains a speed of at least VTOSS; and establishes a positive rate of climb, assuming the critical engine failure occurs at the engine failure point prior to the TDP. (b) For elevated heliports, the take-off distance is the horizontal distance along the take-off path from the start of the take-off to the point at which the rotorcraft attains and maintains a speed of at least VTOSS and establishes a positive rate of climb, assuming the critical engine failure occurs at the engine failure point prior to the TDP.