Revision_1_PD10WRGBGBEB08.pdf
PDF 17 KB Posted
- Attached to
- Common Multi-Platform Boresight System (CMBS) Federal contract opportunity
- Solicitation number
- FA8533-10-R-22377
About this file
Revision 1 to Purchase Description PD10WRGBFBEB08
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Other files for this federal contract opportunity
| File | Type | Posted |
|---|---|---|
| FA853310R22377______0002.pdf | ||
| Questions and Answers for FBO 28 April 2010.pdf | ||
| 9626025_98752_NULL_E_0001_E_NULL_0001_741_U_N_N_N 1 .pdf | ||
| 9579777_98752_NULL_A_0001_A_NULL_0001_278_U_N_N_N 1 .pdf | ||
| FA853310R22377______0001.pdf | ||
| Revision_1_PD09WRGBGBEB12.pdf | ||
| Revision_1_Statement_of_Work.pdf | ||
| 9579776_98752_NULL_J_0001_J_NULL_0001_741_U_N_N_N 1 .pdf | ||
| Questions and Answers 21 April 2010.pdf | ||
| Attachment2.doc | DOC document | |
| ELINF001.pdf | ||
| Attachment4.doc | DOC document | |
| PD09WRGBGBEB12.DOC | DOC document | |
| ELING001.pdf | ||
| PD10WRGBGBEB08.doc | DOC document | |
| Attachment5.doc | DOC document | |
| StatementWork_1022377_00_1.doc | DOC document | |
| Attachment3.doc | DOC document | |
| FA853310R22377.pdf | ||
| Attachment6.doc | DOC document | |
| ELINH001-H002.pdf | ||
| ELINsA001-E003.pdf |
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Text version
PD10WRGBGBEB08
28 January 2010
CAGE 98752
Revision 1
21 April 2010
The purpose of Revision 1 to Purchase Description PD10WRGBGBEB08 is to change the following sections as identified below.
3.5.11.2 Shock meter. Each adapter shall include a 100G accelerometer (shock meter) to determine abuse in the field or during shipping.
3.7.1 Adapter kit common hardware. The adapter kits shall include all hardware, associated accessories, and handling enclosures required for use with the CMBS. The contractor shall furnish any special tools needed for operation of the adapters as common hardware. Potting fixtures shall not be part of the F-15 or F-16 adapters. No potting adapters shall be used on either the F-15 or F-16 aircraft.
3.11 Basic operation. The adapters shall ensure that the boresight operators will not have to remove the external fuel tank for the boresighting process. The aircraft shall not require jacking, leveling or repositioning. The established aircraft reference centerline shall be used.
The boresight process shall take no more than eight hours or sixteen man-hours from set-up to aircraft returned to mission-ready condition (objective: boresight completion time shall be no more than four hours or eight man-hours). The adapters shall also provide the capability to perform boresight alignment confidence checks or minor boresight alignments without LRU removal.
3.13 Calibration. The adapters shall maintain a calibration cycle no less than 24 months.
The adapters shall be designed to be calibrated by regional PMELs within the Government. The contractor shall provide whatever unique or special hand tools are necessary to calibrate the F-15 and F-16 adapters. The unique tools shall be comprised into a kit and will be ordered as required by the Government for its PMEL facilities.
4.9.1 Examination of preproduction product. Each preproduction adapter kit shall be examined to verify compliance with the requirements herein. Particular attention shall be given to materials, workmanship, dimensions, surface finishes, protective coatings and sealants and their application, welding, fastening, and markings. Proper operation of each adapter function shall be verified. Certifications and analyses shall be provided in accordance with TABLE V.
Compliance with the human engineering requirements of 3.4 shall be demonstrated.
4.9.2 Examination of production product. Each production adapter kit shall be calibrated by the contractor prior to shipment as well as have a marking inspection completed.
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