SOW.pdf
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- Solicitation number
- 70Z03825QL0000130
About this file
This Statement of Work (SOW) details the repair requirements for an HC-144 Elevator (Part Number 35-32001-0009, Right Hand) with corrosion and fatigue damage. The United States Coast Guard has contracted ADSMA in Mobile, AL to perform a comprehensive repair and inspection of the elevator component. The scope includes a complete inspection, necessary repairs according to AIRBUS CN-235 Aircraft Structural Repair Manual, rib replacement, rear spar reinforcement, and mid-life inspections.
Key requirements include providing facilities, manpower, tooling, and materials for repair, documenting any additional damage discovered, applying marinization protections, completing specific mid-life inspections, and ensuring primer and bonding protections. ADSMA must deliver a detailed proposal with estimated costs, completion timeline, repair process description, and supporting documentation. The deliverables include detailed drawings, a cost breakdown for engineering, labor, and materials, and proper documentation of all repair work via FAA 8130-3 or Certificate of Conformity (COC).
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| File | Type | Posted |
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| Solicitation Terms and Conditions.pdf | ||
| Redacted J A.pdf |
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Text version
STATEMENT OF WORK
HC-144 Flight Control Repair
24 June 2024
Reference Contract No: 70Z03819PA0000389
HC-144 ELEVATOR, P/N 35-32001-0009 (RH) Corrosion and Damage Repair
A. General: HC144 Elevator control surfaces are consistently found to have corrosion and fatigue damage during scheduled PDM inspections. Repair of corrosion and fatigue damage on internal ribs requires a significant amount of effort and disassembly. ALC does not have the repair resource capacity to support field level and PDM demands. The USCG has deemed that organic repair of this component is BER.
B. Scope: This SOW shall establish services from the OEM repair facility, ADSMA in Mobile AL via the reference contract to inspect, repair and restore the RH Elevator P/N 35-32001-0009 to airworthy condition.
Your Point of Contact is: CWO Lance Godfrey, lance.l.godfrey@uscg.mil telephone 252 335- 7308.
C. Requirement:
1. ADSMA shall perform a complete inspection and complete the necessary repairs IAW AIBUS CN-235 Aircraft Structural Repair Manual to include the applicable Rib Replacement IAW SB235-55-0009 for the respective Elevator(s) and Elevator Reinforcement of the Rear Spar Service Bulletin NR. SB-235-55-0011 M for the respective elevator(s).
2. ADSMA shall provide the facilities, manpower, tooling, special equipment, hardware, hazmat, and materials necessary to remove/replace affected parts.
3. If additional damage or corrosion is discovered during the repair process, ADSMA shall contact the POCs listed in paragraph B.
4. ADSMA shall provide a detailed list of any additional damage and repair requirements to restore airworthiness to the respective Elevator(s).
5. All work performed by ADSMA shall include the additional protections cited in "Marinization" Drawing 35-94453-00 of reference NT-3-DCO-03162.
6. All of the following mid-life inspections shall be completed and documented on the AIRBUS Work Card IAW AIRBUS TEA-3-DT-180072 for RH Elevator, P/N 35-32001-0009: EL0101, EL0102, EL0201, EL0202, EL0301, EL0401, EL0402 and SV0102 for Elevator tabs to include all NDI deposition reports where required.
7. All components shall receive primer protections IAW CN235-23-2, Table 2-5 and Section 2.8.
8. All bonding jumper tests shall be documented on the Work Card IAW AMM Chapter 20-28-00 to include the measured resistance value(s).
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