MIL-A-27261 Revision A:1966
Current
The latest, up-to-date edition.
Accelerometer, Aircraft
08-11-1966
1 SCOPE
2 APPLICABLE DOCUMENTS
3 REQUIREMENTS
4 QUALITY ASSURANCE PROVISIONS
5 PREPARATION FOR DELIVERY
6 NOTES
Describes integrally lighted, 1-7/8-inch dial aircraft accelerometers having a range of -2 to +4g's.
| DevelopmentNote |
A NOTICE 1 - Notice of Inactivation for new design. (05/2004) A NOTICE 2 - Notice of Validation but remains Inactive for New Design. (08/2008) A NOTICE 3 - Notice of Validation but remains Inactive for New Design. (05/2014)
|
| DocumentType |
Standard
|
| Pages |
28
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
This specification covers integrally lighted, 1-7/8-inch dial aircraft accelerometers having a range of -2 to +4g\'s.
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| MIL-P-116 Revision J:1988 | PRESERVATION, METHODS OF (S/S BY MIL-STD-2073-1) |
| QQ-P-416 Revision F:1991 | Plating, Cadmium (Electrodeposited) (S/Sby SAE-AMS-QQ-P-416) |
| MIL-L-25467 Revision D:1977 | Lighting, Integral, Red, Aircraft Instrument, General Specification for |
| FED-STD-595 Revision C:2008 | Colors Used in Government Procurement (S/S By SAE-AMS-STD-595) |
| MIL-STD-781 Revision D:1986 | RELIABILITY TESTING FOR ENGINEERING DEVELOPMENT, QUALIFICATION AND PRODUCTION |
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