C-17 PSE, Lock, Aircraft Ground Safety

Agency:
State: Georgia
Type of Government: Federal
FSC Category:
  • 17 - Aircraft Launching, Landing, and Ground Handling Equipment
NAICS Category:
  • 336413 - Other Aircraft Parts and Auxiliary Equipment Manufacturing
Set Aside: Total Small Business Set-Aside (FAR 19.5)
Posted Date: Apr 22, 2024
Due Date: May 13, 2024
Solicitation No: FA8526-24-Q-0032
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C-17 PSE, Lock, Aircraft Ground Safety
Active
Contract Opportunity
Notice ID
FA8526-24-Q-0032
Related Notice
Department/Ind. Agency
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General Information
  • Contract Opportunity Type: Presolicitation (Original)
  • All Dates/Times are: (UTC-04:00) EASTERN STANDARD TIME, NEW YORK, USA
  • Original Published Date: Apr 22, 2024 11:50 am EDT
  • Original Response Date: May 13, 2024 04:00 pm EDT
  • Inactive Policy: 15 days after response date
  • Original Inactive Date: May 28, 2024
  • Initiative:
    • None
Classification
  • Original Set Aside: Total Small Business Set-Aside (FAR 19.5)
  • Product Service Code:
  • NAICS Code:
  • Place of Performance:
    Warner Robins , GA 31098
    USA
Description

*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. It is anticipated that the RFQ will be released on or around 20 May 2024.


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