C-17 PSE - Sling, Beam Type

Closed Solicitation Posted

Solicitation number
FA8526-24-Q-0028
Agency
AFLCMC Robins AFB Lifecycle Management Center, Department of Defense
Responses due
Set-aside
Total Small Business

Opportunity facts

NAICS code
333923 Overhead Traveling Crane, Hoist, and Monorail System Manufacturing
PSC
3940 Blocks, Tackle, Rigging, And Slings
Place of performance
Warner Robins, Georgia 31098, United States
Points of contact

Notice details come from SAM.gov. Updated .

About this opportunity

The Department of the Air Force Materiel Command Lifecycle Management Center at Robins Air Force Base is seeking to procure one Sling, Beam Type (NSN 3940-01-267-0618, P/N 17G130026-1) for the C-17 aircraft Main Landing Gear system. The requirement includes one First Article, one First Article Test Plan, and one First Article Test Report. The device must interface with a crane to remove and replace the shock strut on the aircraft and in the maintenance shop. Proposals will be evaluated based on the criteria stated in the Request for Quotation (RFQ), and are due by 27 May 2024 at 5:00 PM EST.

This opportunity is a 100% Small Business Set-Aside. Delivery is FOB Destination within the continental United States. The award will be a firm-fixed price contract. The requirement is classified as NAICS 333923 - Overhead Traveling Crane, Hoist, and Monorail System Manufacturing, and PSC 3940 - Blocks, Tackle, Rigging, And Slings. Proposals were originally due on 27 May 2024 but have been extended to 6 August 2024 by 5:00 PM EST via Amendment.

Notice text

*Small Business Set-Aside*

The C-17 Program Management Office has a requirement that is for a firm-fixed price contract for one (1) NSN: 3940-01-267-0618, Sling, Beam Type, P/N: 17G130026-1, which includes one Frist Article, one Frist Article Test Plan, and one First Article Test Report. The C-17 A/C Main Landing Gear (MLG) utilizes a shock strut, connected between the axle beam and post, for absorbing landing loads. The strut is located between the center and outboard tires on each MLG. The strut uses a mixed air/fluid arrangement for pressurization with a 12-gallon fluid capacity. The empty weight of the strut is approximately 312 lbs. The O.D. of the cylindrically shaped strut is approximately 11” and the compressed and extended lengths of the strut are approximately 44” and 66” respectively. One end of the strut incorporates a clevis which is attached to the axle beam using a 2.5” O.D. pin. The other end of the strut incorporates a self-aligning bearing for attachment to a 3.4” O.D. pin on the post.

A device is required to interface a crane, (P/N: TBD), to the shock strut in order to remove and replace the strut on the A/C and move the strut about the shop; at the organizational, intermediate and depot levels of maintenance. The device must provide a means of hoisting the strut in the compressed position and prevent the strut from extending, which could cause handling problems. The A/C must be jacked to relieve the A/C load from the strut, and then the strut must be depressurized before being removed.

Delivery is FOB Destination with shipments in the continental United States. This requirement will be solicited as a Small Business Set-Aside. All responsible sources may submit a quotation which shall be considered by the agency. The Government will utilize the Past Performance Information Retrieval System (PPIRS), Excluded Parties List System (EPLS), and other Government databases to determine contractor status before evaluating proposals. Proposals will be evaluated based on the criteria stated in the RFQ. All data for this system is considered EXPORT CONTROLLED. Proposals are due by 27 May 2024 by 5:00 PM EST.

Attachments

Files attached to this notice, newest first
File Type Posted
FA852624Q0028 Amend2.pdf PDF
FA852624Q0028 Amend1.pdf PDF
CDRL_A003_IUID_Marking_Plan_EN_17G130026-1.pdf PDF
Use_and_Non-Disclosure_Agreement.docx DOCX document
FD2060-24-30167_FORM_1653.pdf PDF
C-17_PSE_Solicitation_Template-FA8526-XX-Q-XXXX-Rev_B.xlsx XLSX spreadsheet
FA852624Q0028.pdf PDF
CDRL_A001_Test_Inspection_17G130026-1.pdf PDF
CDRL_A002_Test_Inspection_17G130026-1.pdf PDF
EDL_Rev05.pdf PDF
MANDATORY_SHIPPING_DOCUMENTS.docx DOCX document
FD2060-24-30167_FORM_158.pdf PDF
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