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PURCHASE DESCRIPTION

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A PDF document (216 KB) attached to L7WC02 B670 Paint Booth and HVAC, from the Department of the Air Force. Due Nov 12, 2026, 3:00 PM (UTC-5).

File name: PURCHASE DESCRIPTION (PD) 20_Oct 26.pdf

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PURCHASE DESCRIPTION

FOR
Building 2390 and Building 91 Fall Protection System
(CIP Projects: L6WA18/L7WA05)

21 October 2026

1.0

Description: The Contractor shall provide all materials, parts, equipment, engineering, labor, shipping and travel necessary to provide fabrication, installation, and integration of a fall protection/fall arrest system (FAS) for C-130 programmed depot maintenance (PDM) performed in B2390 (See Table 1: Summary of Requirements), plus an option for B91 (See Table 2: Summary of Requirements). The system shall provide fall protection for maintenance operations performed on the C-130 wing, center-wing box, empennage, and horizontal stabilizer. The installed FAS shall accommodate non-stretched and stretched C-130 fuselage variants. The Government prefers one FAS that provides fall protection for both variants. The contractor shall use passive systems, such as guard rails, fall restraint, and fall arrest means in this order of government preference. The system shall not contact any aircraft components. Delivery shall include operation manuals, maintenance manuals, recommended preventive maintenance, drawings, SolidWorks models and training of 402d Aircraft Maintenance Group (AMXG) at Robins Air Force Base (AFB), Georgia.
Table 1: Summary of Requirements

4 Each

4 Each

Fabrication of FAS for Base/Stretched Model (C-130),
B2390
FAS Installed in Four B2390 Bays for Base/Stretched Model (C-130)

Table 2: Summary of Requirements

7 Each

Fabrication of FAS for Base/Stretched Model (C-130), B91

7 Each

FAS Installed in Four B91 Bays for Base/Stretched Model (C-130)

1.1 SELF RETRACTING LIFELINES (SRL): The Contractor shall provide: 1.1.1 An electronic document the SRL’s can fully arrest a fall in compliance with the requirements and include make, model, length, location and serial number of each SRL. (CDRL A001 DI-MGMT-80368A/T, Status Report)
1.1.2 Each SRL shall have a 316 stainless steel cable lifeline connected to a swivel snap hook which attaches to the user’s D-ring.
1.1.3 Each SRL shall have a visual impact indicator on the hook to notify the user if the SRL has been “impacted” and requires servicing prior to use. 1.1.4 Each SRL shall be connected directly to a trolley. There shall not be any cables between the SRL housings and the trolleys.
1.1.5 SRL’s installed over the wings, aft fuselage and horizontal stabilizers shall

have enough cable to extend to the floor of the maintenance stand. 1.1.6 SRL’s installed over the fuselage shall have enough cable to extend to the floor

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