SAE AS1162-1971
Attitude Instruments, Pitch and Roll Part I Minimum Performance Standard for Equipment
- Standard No.
- SAE AS1162-1971
- Release Date
- 1971
- Published By
- Society of Automotive Engineers (SAE)
- Status
- 2001-07
- Replace By
- SAE AS1162-1996
- Latest
- SAE AS1162-2008
- Scope
- 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.
SAE AS1162-1971 Referenced Document
- SAE ARP461 Synchros
- SAE ARP582 Lighting, Integral, for Aircraft Instruments; Criteria for Design
- SAE ARP798-1965 Design Criteria for White Incandescent Lighted Aerospace Instruments
- SAE AS396B-1958 Bank and Pitch Instruments (Indicating Stabilized Type) (Gyroscopic Horizon, Attitude Gyro)
- SAE AS425 AS425 Bottom Bracket - Parachute Stowage
- SAE AS441-1964 BANK AND PITCH INSTRUMENTS (Indicating Stabilized Type)(Gyroscopic Horizon, Attitude Gyro)(Turbine-Powered Subsonic Aircraft)
SAE AS1162-1971 history
- 2008 SAE AS1162-2008 Attitude Instruments, Pitch and Roll Part I Minimum Performance Standard for Equipment
- 1996 SAE AS1162-1996 Attitude Instruments@ Pitch and Roll Part I: Minimum Performance Standard for Equipment (Reaffirmed Noncurrent July 2001)
- 1971 SAE AS1162-1971 Attitude Instruments, Pitch and Roll Part I Minimum Performance Standard for Equipment
- 1945 SAE AS1162-2-1945 AS1162 Clips, 360°, with Pressed Ends (Aluminium Alloy)
