 | 1957 - 1296 էջ
...recommended. [Supp. 1, 12 FR 3437, May 28, 1947, as amended by Amdt. 1, 14 PR 36, Jan. 5, 1949] § 3.353 Limit drop tests, (a) If compliance with the...drop heights not less than the following : h (inches) =3.8 (W/S)°-° except that the free drop height shall not be less than 9.2 inches and need not be... | |
 | 1964 - 918 էջ
...(1) If compliance with the limit landing conditions specified in paragraph (a) (1) of this section is demonstrated by free drop tests, these shall be...tire, and shock absorber in their proper relation. The free drop heights shall not be less than the following: (1) 18.7 inches for the design landing... | |
 | 2001 - 1132 էջ
...drop tests. (a) If compliance with §23.723(a) is shown by free drop tests, these tests must be made on the complete airplane, or on units consisting of...proper relation, from free drop heights not less than those determined by the following formula: h (Inches) = 3.6 ( W/S) >/i However, the free drop height... | |
 | 1996 - 984 էջ
...prescribed in §§27.725 and 27.727, respectively. These tests must be conducted on the complete rotorcraft or on units consisting of wheel, tire, and shock absorber in their proper relation. 827.726 Limit drop test The limit drop test must be conducted as follows: (a) The drop height must... | |
 | 1962 - 898 էջ
...(1) If compliance with the limit landing conditions specified in paragraph (a) (1) of this section Is demonstrated by free drop tests, these shall be...tire, and shock absorber in their proper relation. The free drop heights shall not be less than the following: (I) 18.7 inches for the design landing... | |
 | 1949 - 582 էջ
...4b.373 Limit drop tests. (a) If compliance with the specified limit landing conditions of § 4b.372 (a) is demonstrated by free drop tests, these shall...from free drop heights not less than the following : (1) 18.7 inches for the design landing weight conditions. (2) 6.7 inches for the design take-off... | |
 | 1961 - 1480 էջ
...(1) If compliance with the limit landing conditions specified in paragraph (a) (1) of this section Is demonstrated by free drop tests, these shall be...tire, and shock absorber in their proper relation. The free drop heights shall not be less than the following: (I) 18.7 Inches for the design landing... | |
 | 1952 - 1006 էջ
...(1) If compliance with the limit landing conditions specified in paragraph (a) (1) of this section is demonstrated by free drop tests, these shall be...tire, and shock absorber in their proper relation. The free drop heights shall not be less than the following: (1) 18.7 Inches for the design landing... | |
 | 1964 - 924 էջ
...(1) If compliance with the limit landing conditions specified in paragraph (a) (1) of this section is demonstrated by free drop tests, these shall be...tire, and shock absorber in their proper relation. The free drop heights shall not be less than the following: (1) 18.7 inches for the design landing... | |
 | 1963 - 920 էջ
...(1) If compliance with the limit landing conditions specified in paragraph (a) (1) of this section is demonstrated by free drop tests, these shall be...tire, and shock absorber in their proper relation. The free drop heights shall not be less than the following: (1) 18.7 inches for the design landing... | |
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If compliance with the limit landing conditions specified in paragraph (a) (1) of this section is demonstrated by free drop tests, these shall be conducted on the complete airplane, or on units consisting of wheel, tire, and shock absorber in their proper... 
