MIL-DTL-32183 Base Document:2004
Current
The latest, up-to-date edition.
Catapult, Aircraft Ejection Seat: CKU-5C/A Rework Assembly
English
21-12-2004
1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. VERIFICATION
5. PACKAGING
6. NOTES
Describes the requirement for the refurbishment (rework) of the CKU-5C/A rocket catapults (ROCAT) for aircraft ejection seat assemblies.
| DocumentType |
Standard
|
| Pages |
15
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
This specification establishes the requirement for the refurbishment (rework) of the CKU-5C/A rocket catapults (ROCAT) for aircraft ejection seat assemblies. This specification includes only the requirements for restoration of salvageable hardware. All other requirements for the CKU-5C/A ROCAT are specified in the new unit specification, MIL-DTL-32127 and drawing 512-174-0068. The earlier versions of the CKU-5C/A ROCAT, the CKU-5/A/A and CKU-5B/A, may be converted to the CKU-5C/A configuration during the rework.
| ASME B46.1 : 2009 | SURFACE TEXTURE (SURFACE ROUGHNESS, WAVINESS, AND LAY) |
| DOD-STD-2101 Base Document:1979 | Classification of Characteristics |
| MIL-DTL-32127 Revision A:2005 | Catapult, Aircraft Ejection Seat, CKU-5C/A Assembly |
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