Attachment 2 - SOW - 70Z03825QJ0000437.pdf
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- Solicitation number
- 70Z03825QJ0000437
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This Statement of Work (SOW) details a repair requirement for the United States Coast Guard (USCG) Aviation Logistics Center's Medium Range Recovery Product Line Division. The solicitation seeks repair of 3 Enhanced Digital Engine Control Units (EDECU), National Stock Number 2995-01-680-3143, for MH-60T aircraft. The components are expected to have corrosion due to saltwater environments, and the contractor must repair them to an airworthy condition following original equipment manufacturer (OEM) specifications and FAA corrosion control guidelines.
The repair process requires a comprehensive evaluation of each component, with provisions for Beyond Economical Repair (BER) scenarios. Specific repair requirements include restoring components to Ready For Issue (RFI) condition, performing thorough inspections, replacing missing or broken parts, and removing foreign matter or corrosion. Pricing for services such as Teardown, Test and Evaluation, BER/Scrap Fee, and firm fixed fee will be determined at the time of contract award. The contract number is 70Z03825QJ0000437, and the repair location is Elizabeth City, North Carolina.
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ATTACHMENT 2 - STATEMENT OF WORK (SOW)
ENHANCED DIGITAL CONTROL UNIT (EDECU) REPAIR
70Z03825QJ0000437
1.0 Contractor Requirements
1.1 The United States Coast Guard (USCG) Aviation Logistics Center (ALC), Medium Range Recovery (MRR) Product Line Division located in Elizabeth City, North Carolina has a requirement to repair the following components quantities specified in the following table:
Description QTY National Stock Number
(NSN)
Part Number (P/N)
Enhanced Digital Engine Control Unit (EDECU)
3 2995-01-680-3143 116007-05C5-17
USCG aircraft operate primarily in a saltwater environment and are subject to corrosion. The Contractor is advised to expect corrosion on the component(s) to be repaired under this order. The component(s) shall be repaired and returned by the Contractor in an airworthy condition suitable for installation on MH- 60T aircraft
1.2 The components are utilized on the MH-60T aircraft. Upon receipt of the components, the Contractor shall perform an evaluation to determine the condition of the components. Any components determined to be Beyond Economical Repair (BER), the Contractor will be allowed one of the following firm-fixed prices only:
Service Total Teardown, Test and Evaluation (TT & E)/ No Fault Found (NFF)
TBD at time of award
BER/Scrap Fee TBD at time of award Firm fixed fee TBD at time of award
1.2.1 When a component is found to be BER, the Contractor shall prepare a failure data report in accordance with (IAW) Section 2.11. This report shall be included with the returned component. The Contracting Officer will provide disposition instructions IAW Section 2.9 via a modification for all parts found to be BER.
2.0 REPAIR
2.1 Not Ready For Issue (NRFI) components shall be repaired and modified to latest configuration and returned to RFI condition in accordance with (IAW) the original equipment manufacturer (OEM) 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-RFI component. The Contractor shall perform an inspection and correct all 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.
2.2 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 OEM specifications and Federal Aviation Administration (FAA) Advisory Circular AC 43-4A, dated 07/24/1991, Corrosion Control for Aircraft.
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