3680_Price_List_Phosphate_Flouride_Coating.xlsx
XLSX spreadsheet 19 KB Posted
- Attached to
- Phosphate Flouride Coating Federal contract opportunity
- Solicitation number
- FA8224-18-Q-COAT
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Price List
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Other files for this federal contract opportunity
| File | Type | Posted |
|---|---|---|
| Combined_Synopsis_and_Solicitation_-_Phosphate_Flouride_Coating.doc | DOC document | |
| 3680_Phosphate_-_PWS.docx | DOCX document | |
| 3680_Phosphate_-_CDRL_A001.pdf | ||
| 3680_Phosphate_-_PWS.docx | DOCX document | |
| 3680_Phosphate_-_CDRL_A001.pdf | ||
| 3680_Price_List_Phosphate_Flouride_Coating.xlsx | XLSX spreadsheet | |
| Combined_Synopsis_and_Solicitation_-_Phosphate_Flouride_Coating.doc | DOC document |
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Text version
Bomb Lift Repairs
| Part number Breakdown | Year 2018-2019 | Year 2019-2020 | Year 2020-2021 | Year 2021-2022 | Year 2022-2023 | |
| Services / Parts Required | Order Period 1 - Price (Each) | Order Period 2 - Price (Each) | Order Period 3 - Price (Each) | Order Period 4 - Price (Each) | Order Period 5 - Price (Each) | |
| DAA3222A220-001 1620-01-297-3695 | B2 M Upper Drag Brace | |||||
| DAA3222A221-001 1620-01-297-6591 | B2 M Lower Drag brace | |||||
| DAA3221A227-001 3040-01-284-1637 | B2 Nose Mount | |||||
| DAA3221A140-001 1620-01-128-6366 | NLG Torsion Link | |||||
| DA3222A136-015 1620-01-383-3535 | MLG Stiker Titanium | |||||
| DAA3222A136-013 1620-01-297-1520 | Fitting Assy- Truck Tilt Actuator MLG |
The contractor shall prepare the surfaces and apply phosphate-fluoride coating to the B-2 landing gear components in accordance with (IAW) Aerospace Material Specification (AMS) 2486.
The contractor shall prime the components with MIL-PRF-23377 TYPE I, CLASS C (primer coating, epoxy, high solids) or MIL-PRF-85582 TYPE I, CLASS C2 (primer coating, epoxy, waterborne). The primer thickness shall be 0.0006-0.0013”. Parts must be primed within 24 hours of completing the phosphate fluoride coating process. The applied primer shall be free of runs, wrinkling, crazing, blistering, lifting, pitting, cupping or other defects. Lubrication holes and noted interior diameters (see drawings below, areas to be omitted have been highlighted) shall not be coated with primer.
Individual part requirements: Many of the figures below (see Appendix B) show the entire assembly including bushings, springs, screws, nuts, etc. All components will require removal of the old phosphate-fluoride coating and application of the new phosphate-fluoride coating to the entire surface of the part (unless otherwise noted in the drawing). The government will disassemble all assemblies into individual components at Hill AFB. Paint and primer will also be removed by Hill AFB. The phosphate fluoride coating is only required on the titanium components in the assembly. Masking may be required as specified in the attached drawings for paint. The contractor shall provide Certificate of Compliance with each returned component and a copy including the following: (CDRL A001)
The time and date the phosphate-fluoride process was completed.
Dry film thickness of applied primer.
The time and date the primer was applied.
This documentation shall be provided to Hill AFB with the shipment of each component.
This documentation shall be maintained by the contractor for two years from when the parts are processed.
It shall be made available to Hill AFB personnel on request.
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