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CS 29.337 Limit manoeuvring load factor
Available versions for ERULES-1963177438-5604
ED Decision 2003/16/RM
found in: CS-29 Amdt 10 - Large Rotercraft (Jan 2023)
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CS 29.337 Limit manoeuvring load factor ED Decision 2003/16/RM The rotorcraft must be designed for – (a) A limit manoeuvring load factor ranging from a positive limit of 3.5 to a negative limit of -1.0; or (b) Any positive limit manoeuvring load factor not less than 2.0 and any negative limit manoeuvring load factor of not less than –0.5 for which: (1) The probability of being exceeded is shown by analysis and flight tests to be extremely remote; and (2) The selected values are appropriate to each weight condition between the design maximum and design minimum weights.
CS 29.337 Limit manoeuvring load factor ED Decision 2003/16/RM The rotorcraft must be designed for – (a) A limit manoeuvring load factor ranging from a positive limit of 3.5 to a negative limit of -1.0; or (b) Any positive limit manoeuvring load factor not less than 2.0 and any negative limit manoeuvring load factor of not less than –0.5 for which: (1) The probability of being exceeded is shown by analysis and flight tests to be extremely remote; and (2) The selected values are appropriate to each weight condition between the design maximum and design minimum weights.