 | 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...tire, and shock absorber, in their proper relation, from free drop heights not less than those determined by the following formula: h (Inches) = 3.6 (... | |
 | 2000 - 1128 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...tire, and shock absorber, in their proper relation, from free drop heights not less than those determined by the following formula: A (inches) = 3.6 (W/S)... | |
 | 1964 - 1108 էջ
...simulating an airplane descent velocity of 12 fps at design landing weight, assuming wing lift not greater than the airplane weight acting during the landing...conditions specified in paragraph (a) (1) of this ;ection is demonstrated by free drop lests, these shall be conducted on the :omplete airplane, or on... | |
 | 1962 - 898 էջ
...3.353 Limit drop testa. (a) If compliance with the specified limit landing conditions of § 3.352 (a) is demonstrated by free drop tests, these shall be...tire, and shock absorber in their proper relation, from free drop heights not less than the following: h. (inches) =3.6 (W/S)'-* except that the free... | |
 | 1963 - 908 էջ
...simulating an airplane descent velocity of 12 fps at design landing weight, assuming wing lift not greater than the airplane weight acting during the landing impact. In this test the landing gear shall not fall. (See paragraph (c) of this section.) (b) Limit drop tests. (1) If compliance with the limit landing... | |
 | 1962 - 966 էջ
...simulating an airplane descent velocity of 12 fps at design landing weight, assuming wing lift not greater than the airplane weight actIng during the landing...by free drop tests, these shall be conducted on the jomplete airplane, or on units consisting >f wheel, tire, and shock absorber in their proper relation.... | |
 | 1961 - 1480 էջ
...§3.353 Limit drop tests. (a) If compliance with the specified limit landing conditions of § 3.352 (a) is demonstrated by free drop tests, these shall be...tire, and shock absorber in their proper relation, from free drop heights not less than the following: h. (inches) =3.6 (W/S)"> except that the free drop... | |
 | 1952 - 1006 էջ
...3.353 Limit drop tests, (a) If compliance with the specified limit landing conditions of § 3.352 (a) is demonstrated by free drop tests, these shall be...tire, and shock absorber in their proper relation, from free drop heights not less than the following : h (inches) =3.6 (W/S)°° except that the free... | |
 | 1964 - 924 էջ
...3.353 Limit drop tests. (a) If compliance with the specified limit landing conditions of § 3.352(a) is demonstrated by free drop tests, these shall be...tire, and shock absorber in their proper relation, from free drop heights not less than the following: h. (inches) =3.6 (W/S)« except that the free drop... | |
 | 1963 - 920 էջ
...3.353 Limit drop tests. (a) If compliance with the specified limit landing conditions of § 3.352 (a) is demonstrated by free drop tests, these shall be...tire, and shock absorber in their proper relation, from free drop heights not less than the following: ft (inches) =3.6 (W/S)" except that the free drop... | |
| |
If compliance with the specified limit landing conditions of § 3.352 (a) 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 relation, from free... 
