The instrument system specified shall accept an input of static pressure and in some equipment other inputs that contribute altitude information to provide a visual indication of pressure altitude. If equipped with an automatic correction mechanism, it shall indicate by a positive means when the automatic correction mechanism is not in use. If the static source pressure error compensating mechanism is operational it shall be functional throughout the required operating envelope of the particular aircraft. Each aircraft type has its own static source error data which shall be obtained from the airframe manufacturer's certified data. When a Central Air Data Computer is used in the altimeter system, the CADC shall be certified to its own governing document and the altimeter system (CADC and display) shall comply with the requirements of this document.
PRESSURE ALTMETER SYSTEM MINIMUM SAFE PERFORMANCE STANDARD
01.06.1971
Aufsatz (Konferenz)
Englisch
PRESSURE ALTIMETER SYSTEM MINIMUM SAFE PERFORMANCE STANDARD
SAE Technical Papers | 1996
Minimum Performance Standard for Automatic Pressure Altitude Digitizer Equipment
SAE Technical Papers | 2008
MINIMUM STANDARD FOR OXYGEN PRESSURE REDUCERS
SAE Technical Papers | 1991
Minimum Safe Performance Over Speed Warning Instruments
SAE Technical Papers | 2023
MINIMUM PERFORMANCE STANDARD TEMPERATURE INSTRUMENTS
SAE Technical Papers | 1996