Statement of Work
Updated
A PDF document (1.2 MB) attached to MH-65 Power Supply Assembly Repair, from the US Coast Guard. Due Nov 10, 2026, 1:00 PM (UTC-5).
File name: Statement of Work - 70Z03827QB0000018.pdf
The full file is for paid members, or buy this bid alone.
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STATEMENT OF WORK (SOW)
70Z03827QB0000018
Contractor Requirement
I. This requirement is for the repair of the items listed in the following table utilized on the United States Coast Guard (USCG)'s MH-65 helicopter. Upon receipt of the components, the contractor shall perform a test and evaluation to determine the condition of the items. Description
Quantity
ASSY,PWR SUPPLY
l0+OPTQTY
(+22)
National Stock Number
(NSN)
6130-01-424-4931
Part Number(s)
(PIN)
171BS101-1
2. If, after visual and functional inspections, an item is found to meet manufacturer's minimum performance specifications and considered to be Ready for Installation (RPI) or is considered to be Beyond Economical Repair (BER) in accordance with (IAW) paragraph 11, the contractor will be allowed the firm fixed price for test and evaluation only. The contractor shall prepare a failure data report IAW paragraph 13 which shall be included with the returned component. The parts shall be marked "RPI" or "BER" and returned as-is. All other items shall be major repaired IAW this Statement of Work (SOW). 3. Non-RPI components shall be modified and returned to RPI condition IAW the OEM minimum functional performance specifications. Components shall be repaired for the specific fault noted on the DD Form 1577-2, Unserviceable (Repairable) Tag-Material, or CG-1577-A (11-90), Unsatisfactory Report Tag, which will be attached to each non-RPI item. The contractor shall perform additional inspections and correct deficiencies found. This shall include, but is not limited to, replacement of missing or broken parts and the removal of any foreign matter or corrosion.
4. During inspection and functional test, the presence of corrosion in a component shall constitute reason for a more thorough disassembly and inspection. Should corrosion be found, disassembly shall be made to the extent necessary to remove corrosion or replace the part, or parts, affected. Corroded parts shall be replaced, except in those cases where removal of corrosion from a part will not impair efficiency or safe operation of the part. Corrosion removal and treatment of affected areas will be accomplished IAW Original Equipment Manufacturer (OEM) specifications or Federal Aviation Administration (FAA) Advisory Circular AC 43-4B, dated 09/11/2018, Corrosion Control for Aircraft. 5. Work under this purchase order shall be performed at the contractor's facility or USCG approved facility. The contractor shall provide all necessary parts, materials, labor, tooling,
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