Solicitation, total small business set-aside, first published as presolicitation
C-17 PSE, Lock, Aircraft Ground Safety
FA8526-24-Q-0032
Department of the Air Force, FA8526 AFLCMC WLMK. Other Aircraft Parts and Auxiliary Equipment Manufacturing.
Response deadline
July 31, 2024 at 4:00 PM EDT
Closed 779 days ago. Posted July 12, 2024, first published April 22, 2024. Scheduled to archive August 15, 2024.
Description
As published on SAM.gov.
*100% Small Business Set Aside* The C-17 Program Management Office has a requirement that is for a firm-fixed price contract for NSN:
1730-01-246-1540, Lock, Aircraft Ground Safety, P/N: 17G140004-1, which includes one First Article, one First Article Test Plan, and one First Article Test Report. The C-17 aircraft rudder pedals are used to position the rudder control surfaces, steer the aircraft, and to activate the brake system. At the organizational and depot levels of maintenance, there is a requirement to remove and replace the rudder pedal force transducer.
Prior to performing this task, the rudder pedal assy, which controls rudder control surface motions, must be made inoperative. A device is required which will lock the rudder pedals to make them inoperative when work is being performed to remove and replace the rudder pedal transducer. The following data pertains to the system:
Applicable LCN:
C57AAD MTBF: 68,160 Operating Hours To meet the requirements of Part I, Functional Analysis, the newly developed CFE rudder pedals aircraft ground safety lock, part number 17G140004-1 is recommended. The lock is designed so that when attached to both pedals, the rudder control surfaces cannot be repositioned by an input from the pedals. The aircraft braking system can still be used while the locks are installed.
The lock will have adjustment capabilities, using captive adjustment screws, to compensate for accumulative tolerances which may occur between various rudder pedal assys. The lock is intended to be installed when work is being performed on the rudder system upstream of the hydraulic control valve.
When working downstream of the hydraulic control valve all hydraulic systems shall be depressurized, all hydraulic pump circuit breakers shall be pulled and tagged and the rudder trim circuit breakers shall be pulled and tagged. Delivery is FOB Destination with shipments in the continental United States. This requirement will be solicited as a Total 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 weapon system is considered EXPORT CONTROLLED.
Publications
Every notice SAM.gov issued under this solicitation number, oldest first. Each is a separate record on SAM.
April 22, 2024
Presolicitation
Due May 13, 2024 at 4:00 PM EDT. SAM.gov, notice 509ae479bfb7495787d28222a7aa43d1
May 17, 2024
Solicitation
Due June 17, 2024 at 4:00 PM EDT. SAM.gov, notice 852db047b5d24cb48beff4f6e65fc78b
June 20, 2024
Solicitation
Due July 11, 2024 at 4:00 PM EDT. SAM.gov, notice 199af87b2d9b45a9b8f42a48503db0e5
July 12, 2024
Solicitation
Due July 31, 2024 at 4:00 PM EDT. SAM.gov, notice 86ac1205afdb4ecc89bf46ef8c141476
Points of contact
- Theresa Youncetheresa.younce@us.af.mil
- Aliscia Pittsaliscia.pitts@us.af.mil