SOW.pdf

This is a Statement of Work (SOW) for HC-144 Flight Control Repair dated 24 June 2024. The contract concerns the inspection, repair, and restoration of the RH Elevator, P/N 35-32001-0009, which has sustained corrosion and fatigue damage on internal ribs. The work references a prior contract for HC-144 Elevator P/N 35-32001-0009 corrosion and damage repair.

ADSMA (the contractor) will perform comprehensive services at its OEM repair facility in Mobile, Alabama. The contractor must conduct a complete inspection and execute all necessary repairs per IAW AIRBUS ON-236 Aircraft Structural Repair Manual, including applicable Rib Replacement procedures (IAW SB235-55-0009) and Rear Spar Service Bulletins (SB-235-55-0011M). ADSMA is responsible for providing facilities, manpower, tooling, special equipment, hardware, hazmat, and materials. The contractor must contact the Point of Contact (CWO Lance Godfrey) if additional damage is discovered during repair. All work must include additional protections per Marinization Drawing 35-94463-00 (reference NT-3-DCO-03162), mid-life inspections documented on AIRBUS Work Cards, primer protection per IAW CN235-23-2, bonding jumper testing with resistance measurement documentation, corrosion control preservation per IAW CN-235 Sea Patrol Version, and bonding jumpers/wires per USCG publication MPC 200001.0.

Deliverables include a detailed proposal with estimated costs broken down by engineering, labor, and materials with calendar day completion timeline; detailed drawings and diagrams of work performed; cost breakdown for submission to ALC in Elizabeth City, NC; bonding jumper test documentation; and completion documentation via FAA 8130-3 or COC with NDI deposition reports.