Text in force at CS29-12: from CS29-0, effective 14 Nov 2003.
The landing inertia load factor and the reserve energy absorption capacity of the landing gear m ust be substantiated by the tests prescribed in CS 29.725 and 29.727, respectively . These tests m ust be conducted on the complete rotorcraft or on units consisting of wheel, ty re, and shock absorber in their proper relation.
ED Decision 2003/016/RM · Source