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CS 27.337 Limit manoeuvring load factor
Available versions for ERULES-1963177438-4892
ED Decision 2003/15/RM
found in: CS-27 Amdt 10 - Small Rotorcraft (Feb 2023)
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CS 27.337 Limit manoeuvring load factor ED Decision 2003/15/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 27.337 Limit manoeuvring load factor ED Decision 2003/15/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.