80969_DID.pdf
PDF 160 KB Posted
- Solicitation number
- FA811824R0043
About this file
This document is a Detailed Interface Description (DID) for the KC-135 flap drive ballscrew assembly. It provides detailed technical specifications and requirements for the remanufacturing of this aircraft component. The KC-135 flap drive ballscrew assembly is a mechanically driven gearbox/ball screw assembly used to extend and retract the wing flaps on the KC-135 aircraft. The Air Force is seeking contractors to provide remanufacturing services for this assembly, both with and without replacement of the ball screw. Key requirements include the ability to repair and overhaul the assembly to restore it to full operational capability. This opportunity is being issued under Solicitation Number FA811824R0043 by the Department of the Air Force Materiel Command Air Force Sustainment Center.
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Other files
| File | Type | Posted |
|---|---|---|
| 80441_DID.pdf | ||
| 81838_DID.pdf | ||
| 81995A_DID.pdf | ||
| Transportation.pdf | ||
| SpecialPackagingInstruction.pdf | ||
| FA811824R0043 SOLICITATION.pdf | ||
| Packaging.pdf | ||
| CDRL.pdf | ||
| CAVAF.pdf | ||
| GFP.pdf | ||
| SOW.pdf |
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Text version
Source: http://assist.dla.mil -- Downloaded: 2019-02-14T15:58Z Check the source to verify that this is the current version before use.
Source: http://assist.dla.mil -- Downloaded: 2019-02-14T15:58Z Check the source to verify that this is the current version before use.
File details come from the government source that posted it. Updated .