Repairs of Multiple Composite Components Applicable to the C144 and C27J Aircraft.
SOURCES SOUGHT FOR MARKET RESEARCH PURPOSES ONLY USCG Aircraft Composite Component Repairs NAICS Code: 488190 THIS IS A SOURCES SOUGHT FOR MARKET RESEARCH PURPOSES ONLY. The United States Coast Guard ... SOURCES SOUGHT FOR MARKET RESEARCH PURPOSES ONLY USCG Aircraft Composite Component Repairs NAICS Code: 488190 THIS IS A SOURCES SOUGHT FOR MARKET RESEARCH PURPOSES ONLY. The United States Coast Guard (USCG), Aviation Logistic Command, Medium Range Surveillance Product Line is in the process of developing the acquisition strategy for the award of a requirements contract for repairs of multiple composite components primarily applicable to the C144 and C27J aircraft. This is a Sources Sought Notice and a Request for Information (RFI). This is NOT a solicitation and proposals are not being requested at this time. Information provided to the Government as a result of this posting is strictly voluntary and given with no expectation of compensation and shall be provided at no cost to the Government. Contact with Government personnel other than the Contracting Officer by any potential Offeror or their employees regarding this requirement is strictly prohibited. The purpose of this posting is to locate experienced Offerors capable and interested in providing the services identified herein. Any interested party shall submit a capability statement by the closing date of this notice and will be considered by the Government for the purposes of determining the acquisition strategy for a future solicitation. The capability statement shall outline the potential Offerors’ experience with providing aircraft composite repair services. Please include only capabilities relative to this requirement. Potential Offerors MUST be a certified Federal Aviation Administration (FAA) Part 145 authorized repair center and have experience performing aircraft composite component repairs and have all the necessary provisions to perform the contract requirements for composite repairs, including but not limited to, required tooling, facilities, manuals, test equipment, parts, material, engineering services, management, personnel, documentation, preservation, and shipping. Many of the composite components under this requirement will be removed from the aircraft during the aircraft maintenance cycle and are required for re-install prior to completion of the maintenance cycle. Therefore, the mandatory turn time of 30 days after contractor receipt of the components is required. Component part will be cleaned IAW applicable Component Maintenance Manuals or FAA Advisory Circular 43-205, Guidance for Selecting Chemical Agents and Processes for De-painting and General Cleaning of Aircraft and Aviation Products, to ensure they are as free as practical of all hazardous dust to include Hexavalent chromium, cadmium, lead. Information on these hazards can be found in Occupational Safety and Health Standards 1910.1025 (lead), 1910.1026 (Hexavalent Chromium) and 1910.1027 (Cadmium) Potential Offerors shall not submit proprietary information when responding to this notice. Potential Offerors shall also note that the Government will not return any information submitted in response to this notice. Responses are due no later than 2:00 PM on 20 June 2020. Please send your responses to this RFI via email directly to Theresa.L.Alkeus@uscg.mil. All responses must include the following information: Company Name Company Address Company Business Size/Socio-economic category (if applicable) DUNS Number Point of Contact (POC) name, phone number and email address Responses shall not exceed fifteen (15) single-sided pages. Email submissions are subject to size and type restrictions (typically limited to less than 5MB in size and only executable attachments such as .doc and .pdf files) as well as any other appropriate network measures. It is the potential Offeror’s responsibility to verify email submissions have been received and can be viewed. The following is a brief example of a few of the items that may be included for composite repair under this contracting effort. IT IS NOT ALL INCLUSIVE and does NOT constitute the entire schedule of requirements. Nomenclature Part Number PANEL, VERT STAB 35-33235-0001 PANEL, VERT STAB 35-33236-0003 PANEL, VERT STAB 35-33237-0003 PANEL, VERT STAB 35-33238-0003 PANEL, VERT STAB 35-33239-0003 TURTLE BACK TOP CVR 35-22842-0003 TOP COVER 35-22817-0003A01 ACCESS DOOR-LH 35-11724-0007A01 TIP ASSY RH 35-31302-0006A04 PANEL ASSY-ACCESS LH 35-11720-0011A01 ACCESS DOOR-RH 35-11724-0008 NEL ASSY ACCESS RH 35-11771-0010-51-MTA PANEL ACCESS LH 35-11771-0009-51-MTA PANEL ASSY ACCESS LH 35-11726-0005 NEL ASST ACCESS RH 35-11726-0006 TRAILING CURVE 1-LH 35-31331-0005 PANEL ASSY-ACCES LH 35-11728-0005 ACCESS DOOR 5210 RH 35-11770-0006 COVER ASSY LH 35-13664-0009A03-MTA COVER ASSY LH 35-13666-0011A03-MTA COVER ASSY RH 35-13666-0012A04-MTA ACCESS DOOR 500-980 35-11722-0007 PANEL ASSY-ACCESS RH 95-11763-0002-MTA COVER ASSY RH 35-13664-0010A04-MTA COVER RH 35-13659-0008A04-MTA COVER ASSY LH 35-13659-0007A03-MTA TIP ASSY-LH 35-31302-0005 PANEL ASSY-ACCESS RH 35-11720-0010 COVER ASSY-RH 35-13656-0008A04-MTA PANEL ASSY-ACCESS RH 35-11728-0006 COVER ASSY 35-13656-0007 PANEL ASSY RH 95-11722-0002-MTA PANEL ASSY RH 95-11767-0002-MTA PANEL ASSY-ACCESS LH 35-11773-0009A03 COVER ASSY 35-13661-0009A03-MTA COVER 35-13661-0010A04-MTA ACCESS DOOR 35-11773-0012 TIP ASSY 35-33302-0003A01 FAIRING 35-22837-0006-01 COUPLING, LOWER LH 35-31244-0011 FAIRING 35-22837-0005-01 ACCESS DOOR LH 35-11766-0005 ACCESS DOOR LH 35-11770-0005 PANEL ASSY-ACCESS RH 95-11773-0006 COVER ACCESS 35-24063-0005-MTA FAIRING HOR STAB RH 35-24076-0008A02-MTA FAIRING HOR STAB LH 35-24076-0007A01-MTA DOOR, AVIONIC RH 95-21160-0002A02 DOOR, AVIONIC LH 95-21160-0001A01 COUPLING UPPER, LH 35-31247-0011A01 FAIRING W/F, LH 35-22839-0007A01 FAIRING W/F, RH 35-22839-0008A02 PANEL ASSY ACCESS LH 35-11767-0011 COVER-RH (FAIRING) 35-33322-0002A02-SUBC NEL ASSY ACCESS LH 95-11763-0001-MTA COMPLETE FAIRING LH 35-15053-0004-MTA ADAPTER 35-33312-0009 WINT TIP ASSY, RH 35-11021-0006C02 COVER - LH 35-33322-0001A01 COWL 35-53333-0007-01 LH WING TIP RIB 35-11467-0001A01 RH WING TIP RIB 35-11467-0002A02 WING TIP ASSY. LH 35-11021-0005C01 TRAILING CURVE 1-RH 35-31331-0006 COUPLING LOWER RH 35-31244-0012A02 COUPLING UPPER RH 35-31247-0012A02 TIP ASSY,RUDDER G1335531040-001 LH FAIRING G2219249209-001 RH FAIRING G2219249209-002 LH,MLG SPONSON G1255391109-001 NLG LH DOOR, ASSY G1413221006-009 NLG RH DOOR,ASSY G1413221006-010 TAIL CONE ASSY G1265362055-001 LH HORIZONTAL TIP 13479-001 RH HORIZONTAL TIP 13479-002 LH TRAIL EDGE ASSY 66571-001 RH,TRAIL EDGE ASSY 66571-002 LEADING EDGE ASSY 66570-001 TIP ASSEMBLY 13635-001
Data sourced from SAM.gov.
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