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PRECISION MOTOR TACHOMETER GENERATOR
- Aerospace Standard
- ARP667
- Reaffirmed
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
This recommended practice establishes objectives for high performance control motor tachometer generators to be used with aeronautical and associated equipment in protective enclosures or completely within the shell of the aircraft so that they are subjected only to the internal climatic conditions of heat, cold, shock, vibration, and humidity. Control motor tachometer generators larger than size 23 are not covered in this document.
Topic
Data Sets - Support Documents
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TABLE I | Motor Characteristics - Standard Conditions | |
Table II | Motor Tachometer Generator Characteristics - Standard Conditions | |
TABLE III | TACHOMETER GENERATOR CHARACTERISTICS - STANDARD CONDITIONS | |
TABLE IV | TACHOMETER GENERATOR VOLTAGE SENSITIVITY | |
TABLE V | TACHOMETER GENERATOR FREQUENCY SENSITIVITY | |
TABLE VI | TACHOMETER GENERATOR TEMPERATURE SENSITIVITY |
Issuing Committee
A-4 Aircraft Instruments Committee
The A-4 Committee is responsible for mechanical, electromechanical and electronic cockpit instrumentation standards applicable to all civil aircraft, with emphasis on minimum performance standards intended for reference in the Federal Aviation Administration (FAA) Technical Standard Orders (TSO).
A list of the technical reports developed by the A-4 Committee can be obtained by searching on 'aircraft instruments' and selecting 'standards', from the SAE Home Page. A-4 Standards For additional information about the A-4 Committee or SAE, contact Maureen Lemankiewicz mlemank@sae.org Let us contact you about suitable committee participation opportunities. Advise us of an industry issue for an SAE Technical Committee.Reference
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