標(biāo)準(zhǔn)號：SAE AS 1162-1971
中文標(biāo)準(zhǔn)名稱：飛行器飛行傾斜角度和滾轉(zhuǎn)度的測量儀表.第I部分:設(shè)備*低性能標(biāo)準(zhǔn)
英文標(biāo)準(zhǔn)名稱：Attitude Instruments, Pitch and Roll Part I Minimum Performance Standard for Equipment
標(biāo)準(zhǔn)類型：V45
發(fā)布日期：1971/10/1 12:00:00
實(shí)施日期：1999/12/31 12:00:00
中國標(biāo)準(zhǔn)分類號：V45
國際標(biāo)準(zhǔn)分類號：49.090
引用標(biāo)準(zhǔn)：SAE ARP 461;SAE ARP 582;SAE ARP 798-1965;SAE AS 396B-1958;SAE AS 425;SAE AS 441-1964;ARINC 415;MS 33558;NASA D-822;RTCA DO-138;TSO C4a
適用范圍：This Aerospace Standard establishes the essential minimum safe operational performance requirements for gyroscopically stabilized pitch and roll indicating instruments for use with reciprocating and turbine engine powered aircraft. This Aerospace Standard covers two basic types of pitch and roll indicating instruments as follows: Type I: Direct coupled to gyro; Type II: Electrical repeating.