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§3.355 Reserve energy absorption drop tests.

CAR 3 · Landing Gear Shock Absorbers · Design and Construction · at CAR3-14 (current)

Text in force at CAR3-14: from CAR3-0, effective 1 Nov 1949. OCR text

If compliance with the reserve energy absorption condition specified in § 3.352 (b) is demonstrated by free drop tests, the drop height shall be not less than 1.44 times the drop height specified in § 3.353. In simulating wing lift equal to the airplane weight, the units shall be dropped with an effective mass equal to where the symbols and other details are the same as in § 3.353. RETRACTING MECHANISM

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