 | 1939 - 1520 էջ
...safe operation. §03.1331 Static longitudinal stability. In the configurations outlined in § 03.13310 and with the airplane trimmed as indicated, the characteristics...released from any speed within the limits defined In (a) above. § 03.13310 Specific conditions. In conditions (a) , (b) , and <c) below, within the speeds... | |
 | 1961 - 1484 էջ
...necessary for safe operation. § 3.1 14 Static longitudinal stability. In the configurations outlined in § 3.115 and with the airplane trimmed as indicated,...force is slowly released from any speed within the its defined in paragraph (a) of this tion. §3.115 Specific conditions. In conditions set forth in... | |
 | 1964 - 918 էջ
...is appropriate, or need not be less than the minimum speed in steady unstalled flight. (b) The ah1 speed shall return to within 10 percent of the original...the limits defined In paragraph (a) of this section. (c) The stable slope of the stick force versus speed curve shall not be less than 0.5 pound per 3 knots... | |
 | 1965 - 480 էջ
...is appropriate, or lower than the minimum speed for steady, unstalled flight. (b) The airspeed must return to within 10 percent of the original trim speed...force is slowly released from any speed within the range specified in paragraph (a) of this section. (c) The stable slope of the stick force versus speed... | |
 | 1965 - 1938 էջ
...is appropriate, or lower than the minimum speed for steady, unstalled flight. (b) The airspeed must return to within 10 percent of the original trim speed...force is slowly released from any speed within the range specified in paragraph (a) of this section. (c) The stable slope of the stick force versus speed... | |
 | 1973 - 966 էջ
...the minimum speed for steady unstalled flight. (b) The airspeed must return to within plus or minus 10 percent of the original trim speed when the control force is slowly released at any speed within the speed range specified in paragraph (a) of this section. (c) The stick force... | |
 | United States. Flight Standards Service - 1962 - 170 էջ
...airspeed should return to within 10 percent or 5 mph of the original trim speed, whichever is greater, when the control force is slowly released from any speed within the limits defined in paragraph a, above. c. Any short period oscillations occurring between stalling speed and maximum permissible speed... | |
 | 1962 - 898 էջ
...necessary for safe operation. § 3.114 Static longitudinal stability. In the configurations outlined in § 3.115 and with the airplane trimmed as indicated,...is slowly released from any speed within the limits denned in paragraph (a) of this section. §3.115 Specific conditions. In conditions set forth in this... | |
 | 1962 - 902 էջ
...necessary for safe operation. §3.114 Static longitudinal stability. In the configurations outlined in § 3.115 and with the airplane trimmed as indicated,...is slowly released from any speed within the limits denned in paragraph (a) of this section. §3.115 Specific conditions. In conditions set forth in this... | |
 | 1952 - 1006 էջ
...except that such speeds need not be greater than the appropriate operating limit speed or need not be less than the minimum speed in steady unstalled flight....the limits defined in paragraph (a) of this section. (c) The stable slope of stick force curve versus speed shall be such that any substantial change in... | |
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This shall be so at any speed which can be obtained without excessive control force, except that such speeds need not be greater than the appropriate maximum permissible speed or less than the minimum speed in steady unstalled flight. (b) The air speed... 
