C-17 PSE - Towbar, Aircraft

Agency: DEPT OF DEFENSE
State: Georgia
Level of Government: Federal
Category:
  • 17 - Aircraft Launching, Landing, and Ground Handling Equipment
Opps ID: NBD00159332374975877
Posted Date: Apr 19, 2024
Due Date: May 6, 2024
Solicitation No: FA852624Q0039
Source: Members Only
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C-17 PSE - Towbar, Aircraft
Active
Contract Opportunity
Notice ID
FA852624Q0039
Related Notice
Department/Ind. Agency
DEPT OF DEFENSE
Sub-tier
DEPT OF THE AIR FORCE
Major Command
AIR FORCE MATERIEL COMMAND
Sub Command
AIR FORCE LIFE CYCLE MANAGEMENT CENTER
Sub Command 2
MOBILITY AIRCRAFT
Office
FA8526 AFLCMC WLMKA
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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 19, 2024 11:02 am EDT
  • Original Response Date: May 06, 2024 04:00 pm EDT
  • Inactive Policy: 15 days after response date
  • Original Inactive Date: May 21, 2024
  • Initiative:
    • None
Classification
  • Original Set Aside: Total Small Business Set-Aside (FAR 19.5)
  • Product Service Code: 1730 - AIRCRAFT GROUND SERVICING EQUIPMENT
  • NAICS Code:
    • 336413 - Other Aircraft Parts and Auxiliary Equipment Manufacturing
  • Place of Performance:
    Warner Robins , GA 31098
    USA
Description

*100% Total Small Business Set-Aside*



The C-17 Program Management Office has a requirement that is for a firm-fixed price contract for four (4) each NSN: 1730-01-534-6421, Towbar, Aircraft, P/N 17G013043-501, which includes one First Article, one First Article Test Plan, and one First Article Test Report.



Towing or pushing the C-17 aircraft, either forward or backward, is normally accomplished through the nose landing gear (NLG). The NLG incorporates a tow lug design similar to the lug on the KC-10 and having design maximum allowable torsional load of 273,000 in-lbs and maximum axial load of 90,000 lbs. A means is required at the organizational and depot levels of maintenance to interface between the NLG tow lug and the tow tractor while towing and/or positioning the aircraft, at its gross takeoff weight of 586,000 lbs., up a 3 percent grade. The means must provide adequate clearance between the aircraft and the tow tractor. In addition, the means must have an effective length (aircraft interface to tractor interface) of approximately 174”. The commercially developed contractor furnished aircraft towbar, Specification Control Drawing P/N 17G013043-501 or equivalent, is recommended to fulfill the requirements identified in the functional analysis. The towbar will interface between the aircraft towing tractor, P/N: 0404-48980 (SERD 010002) and the aircraft NLG towing lug and tow a 586,000 lb. aircraft.



Delivery is FOB Destination with shipments in the continental United States. This requirement will be solicited as 100% 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. If you desire to obtain a copy of the RFQ, your emailed request must be submitted to kathryn.ferguson.4@us.af.mil and aliscia.pitts@us.af.mil. It is anticipated that the RFQ will be released on or around 10 May 2024.


Attachments/Links
Contact Information
Contracting Office Address
  • CP 478 327 8694 660 ELEVENTH STREET
  • ROBINS AFB , GA 31098-2428
  • USA
Primary Point of Contact
Secondary Point of Contact
History
  • Apr 19, 2024 11:02 am EDTPresolicitation (Original)

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