MIL-DTL-5421 Revision D:2011
Current
The latest, up-to-date edition.
Tubes, Pitot, Electrically Heated, Aircraft
English
05-04-2011
1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. VERIFICATION
5. PACKAGING
6. NOTES
Specifies all types of two-wire electrically heated pitot tubes for use with airspeed indicators.
| DevelopmentNote |
Inactive for New Design. Supersedes MIL T 5421 (B). (08/2007) NEW CHILD NOT 1 2021 IS ADDED
|
| DocumentType |
Standard
|
| Pages |
11
|
| ProductNote |
NEW CHILD NOT 1 2021 IS ADDED
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
| Supersedes |
This specification covers all types of two-wire electrically heated pitot tubes for use with airspeed indicators.
| AN5811 Revision 7:1988 | Tube, Pitot, Electrically Heated, \"L\" Shaped, Inverted |
| SAE AS5813A | TUBE - PITOT, ELECTRICALLY HEATED |
| MIL-STD-31000 Revision A:2013 | Technical Data Packages |
| MIL A 8625 : F | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
| AN5812 Revision 7:1956 | Tube, Pitot, Electrically Heated, \"L\" Shaped |
| AN3115 Base Document:1941 | Receptacle - Airspeed Tube Electrical |
| MIL-S-7742 Revision D:1991 | Screw Threads, Standard, Optimum Selected Series: General Specification for |
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