 | Philippines - 2001 - 678 էջ
...VFE with the landing (D) Each system must be arranged, so far as practicable, to prevent malfunction or serious error due to the entry of moisture, dirt, or other substances. (E) Each system must have a heated pitot tube or an equivalent means of preventing malfunction due... | |
 | 1963 - 1044 էջ
...climb-out speed. (5) Arrangement of system. The airspeed indicating system shall be arranged insofar as practicable to preclude malfunctioning or serious...the entry of moisture, dirt, or other substances. (6) Heated pitot tube. The air-speed indicating system shall be provided with a heated pitot tube or... | |
 | 1997 - 1042 էջ
...the landing position. (d) Bach system must be arranged, so far as practicable, to prevent malfunction or serious error due to the entry of moisture, dirt, or other substances. (e) Each system must have a heated pitot tube or an equivalent means of preventing malfunction due... | |
 | 1962 - 898 էջ
...climb-out speed. (5) Arrangement of system. The airspeed indicating system shall be arranged insofar as practicable to preclude malfunctioning or serious...the entry of moisture, dirt, or other substances. (6) Heated pitot tube. The air-speed indicating system shall be provided with a heated pitot tube or... | |
 | 1962 - 902 էջ
...greater, throughout the speed range from Vso to 1.3 Vtj with flaps retracted, and from 1.3 V»0 to VFB with flaps in the landing position. (4) The air-speed...the event of a collision with a bird. (b) Static air vent and pressure altimeter systems. (1) All instruments provided with static air case connections... | |
 | 1961 - 1516 էջ
...greater, throughout the speed range from VA-0 to 1.3 V,, with flaps retracted, and from 1.3 V.0 to V„B with flaps in the landing position. (4) The air-speed...air-speed indicators are required, their respective pilot tubes shall be spaced apart to avoid damage to both tubes in the event of a collision with a... | |
 | 1962 - 966 էջ
...greater, throughout the speed range from 7A.0 to 1.3 Vs, with flaps retracted, and from 1.3 Vi0 to VFB with flaps in the landing position. (4) The air-speed...indicating system shall be provided with a heated pitot tube or equivalent means of preventing malfunctioning due to icing. (6) Where duplicate air-speed... | |
 | 1952 - 1006 էջ
...greater, throughout the speed range from VA-0 to 1.3 V»j with flaps retracted, and from 1.3 V»0 to VFB with flaps in the landing position. (4) The air-speed...indicating system shall be provided with a heated pitot tube or equivalent means of preventing malfunctioning due to icing. (6) Where duplicate air-speed... | |
 | 1964 - 924 էջ
...climb-out speed. (5) Arrangement of system. The airspeed indicating system shall be arranged insofar as practicable to preclude malfunctioning or serious...the entry of moisture, dirt, or other substances. (6) Heated pitot tube. The air-speed indicating system shall be provided with a heated pitot tube or... | |
 | 1963 - 920 էջ
...climb-out speed. (5) Arrangement of system. The airspeed indicating system shall be arranged insofar as practicable to preclude malfunctioning or serious...the entry of moisture, dirt, or other substances. (6) Heated pilot tube. The air-speed indicating system shall be provided with a heated pitot tube or... | |
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... (b) Static air vent and pressure altimeter systems. (1) All instruments provided with static air case connections shall be vented to the outside atmosphere through an appropriate piping system. 
