C-17 PSE - kit, wrench - core thrust reverser

Closed Solicitation Posted

Solicitation number
FA8526-24-R-0005
Agency
Lifecycle Management Center Air Force Materiel Command, Department of Defense
Responses due
Set-aside
Total Small Business

Opportunity facts

NAICS code
332216 Saw Blade and Handtool Manufacturing
PSC
5120 Hand Tools, Nonedged, Nonpowered
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 is seeking proposals for a firm-fixed price contract to provide one NSN: 5120-01-500-5497, KIT, WRENCH - CORE THRUST REVERSER, P/N 17G230271-1. The kit must include one First Article, one First Article Test Plan, and one First Article Test Report. The wrench kit is required to remove and install the 60 core thrust reverser interface mount bolts on the F117-PW-100 engines used on C-17A aircraft, with specifications for torque and bolt access. Proposals will be evaluated based on the criteria stated in the Request for Proposal (RFP), and the government will utilize past performance databases to determine contractor status. Proposals are due by April 17, 2024 at 5:00 PM EST.

This is a 100% Small Business Set-Aside requirement. All responsible small business sources may submit a proposal, which will be considered by the agency. The government has not identified any incumbents or current contractors. The contract will be awarded by the Department of the Air Force Materiel Command Lifecycle Management Center, and delivery is FOB Destination within the continental United States.

Notice text

4 versions

Update #4 · Latest ·

*100% Small Business Set-Aside Award*

The C-17 Program Management Office has a requirement that is for a firm-fixed price contract for one (1) each NSN: 5120-01-500-5497, KIT, WRENCH - CORE THRUST REVERSER, P/N 17G230271-1, which includes one (1) First Article, one (1) First Article Test Plan, and one (1) First Article Test Report. The F117-PW-100 engine used on the C-17A are equipped with core thrust reversers (TR’s). The reverser mounts to the AFT engine flange with 60 bolts. The bolts are per DPD Standard 3D0118-1, which has NO. 10 wrenching elements per MS33787. The companion self-locking nuts are located along the rear engine flange. The bolt heads are accessible from the rear (Reverser Side) of the interface plane (the head of the bolt faces rearward, toward the exhaust end of the engine). A means is required to provide a comprehensive set of equipment to remove the core thrust reverser/engine interface mount bolts. The means shall meet the following requirements: Be of adequate strength to overcome a break loose torque (the break loose torque may be as much as 180 IN-LBS; twice the installation value)., Be able to access all 60 mount bolts., Deliver 90 +/- 10 IN-LBS of torque to install the bolts (the tightening value is per DPD DPS 2.70-2 FOR 1/4-28 threaded steel bolts). The means will also be used to run-down the bolts prior to final tightening. Delivery is FOB Destination with shipments in the continental United States. This requirement will be solicited as a competitive 100% Small Business-Set-Aside award. 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 RFP. All data for this weapon system is considered EXPORT CONTROLLED. Proposals are due 12 JUNE 2024 by 5:00 PM EST.

Update #3 ·

*100% Small Business Set-Aside Award*

The C-17 Program Management Office has a requirement that is for a firm-fixed price contract for one (1) each NSN: 5120-01-500-5497, KIT, WRENCH - CORE THRUST REVERSER, P/N 17G230271-1, which includes one (1) First Article, one (1) First Article Test Plan, and one (1) First Article Test Report. The F117-PW-100 engine used on the C-17A are equipped with core thrust reversers (TR’s). The reverser mounts to the AFT engine flange with 60 bolts. The bolts are per DPD Standard 3D0118-1, which has NO. 10 wrenching elements per MS33787. The companion self-locking nuts are located along the rear engine flange. The bolt heads are accessible from the rear (Reverser Side) of the interface plane (the head of the bolt faces rearward, toward the exhaust end of the engine). A means is required to provide a comprehensive set of equipment to remove the core thrust reverser/engine interface mount bolts. The means shall meet the following requirements: Be of adequate strength to overcome a break loose torque (the break loose torque may be as much as 180 IN-LBS; twice the installation value)., Be able to access all 60 mount bolts., Deliver 90 +/- 10 IN-LBS of torque to install the bolts (the tightening value is per DPD DPS 2.70-2 FOR 1/4-28 threaded steel bolts). The means will also be used to run-down the bolts prior to final tightening. Delivery is FOB Destination with shipments in the continental United States. This requirement will be solicited as a competitive 100% Small Business-Set-Aside award. 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 RFP. All data for this weapon system is considered EXPORT CONTROLLED. Proposals are due 23 May 2024 by 5:00 PM EST.

Update #2 ·

*100% Small Business Set-Aside Award*

The C-17 Program Management Office has a requirement that is for a firm-fixed price contract for one (1) each NSN: 5120-01-500-5497, KIT, WRENCH - CORE THRUST REVERSER, P/N 17G230271-1, which includes one (1) First Article, one (1) First Article Test Plan, and one (1) First Article Test Report. The F117-PW-100 engine used on the C-17A are equipped with core thrust reversers (TR’s). The reverser mounts to the AFT engine flange with 60 bolts. The bolts are per DPD Standard 3D0118-1, which has NO. 10 wrenching elements per MS33787. The companion self-locking nuts are located along the rear engine flange. The bolt heads are accessible from the rear (Reverser Side) of the interface plane (the head of the bolt faces rearward, toward the exhaust end of the engine). A means is required to provide a comprehensive set of equipment to remove the core thrust reverser/engine interface mount bolts. The means shall meet the following requirements: Be of adequate strength to overcome a break loose torque (the break loose torque may be as much as 180 IN-LBS; twice the installation value)., Be able to access all 60 mount bolts., Deliver 90 +/- 10 IN-LBS of torque to install the bolts (the tightening value is per DPD DPS 2.70-2 FOR 1/4-28 threaded steel bolts). The means will also be used to run-down the bolts prior to final tightening. Delivery is FOB Destination with shipments in the continental United States. This requirement will be solicited as a competitive 100% Small Business-Set-Aside award. 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 RFP. All data for this weapon system is considered EXPORT CONTROLLED. Proposals are due 9 May 2024 by 5:00 PM EST.

Update #1 ·

*100% Small Business Set-Aside Award*

The C-17 Program Management Office has a requirement that is for a firm-fixed price contract for one (1) each NSN: 5120-01-500-5497, KIT, WRENCH - CORE THRUST REVERSER, P/N 17G230271-1, which includes one (1) First Article, one (1) First Article Test Plan, and one (1) First Article Test Report. The F117-PW-100 engine used on the C-17A are equipped with core thrust reversers (TR’s). The reverser mounts to the AFT engine flange with 60 bolts. The bolts are per DPD Standard 3D0118-1, which has NO. 10 wrenching elements per MS33787. The companion self-locking nuts are located along the rear engine flange. The bolt heads are accessible from the rear (Reverser Side) of the interface plane (the head of the bolt faces rearward, toward the exhaust end of the engine). A means is required to provide a comprehensive set of equipment to remove the core thrust reverser/engine interface mount bolts. The means shall meet the following requirements: Be of adequate strength to overcome a break loose torque (the break loose torque may be as much as 180 IN-LBS; twice the installation value)., Be able to access all 60 mount bolts., Deliver 90 +/- 10 IN-LBS of torque to install the bolts (the tightening value is per DPD DPS 2.70-2 FOR 1/4-28 threaded steel bolts). The means will also be used to run-down the bolts prior to final tightening. Delivery is FOB Destination with shipments in the continental United States. This requirement will be solicited as a competitive 100% Small Business-Set-Aside award. 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 RFP. All data for this weapon system is considered EXPORT CONTROLLED. Proposals are due 17 April 2024 by 5:00 PM EST.

Attachments

Files attached to this notice, newest first
File Type Posted
FA8526-24-R-0005-0003.pdf PDF
FA8526-24-R-0005-0002.pdf PDF
FA8526-24-R-0005-0001.pdf PDF
FA8526-24-R-0005.pdf PDF
CDRL A003 IUID Marking Plan_EN.pdf PDF
DD1653.pdf PDF
MANDATORY SHIPPING DOCUMENTS.docx DOCX document
FA8526-24-R-0005.pdf PDF
CDRL A001_Inspection Only_17G230271-1.pdf PDF
FORM 158.pdf PDF
EDL.pdf PDF
CDRL A002_Inspection Only_17G230271-1.pdf PDF
NDA.pdf PDF
Show all 13

Notice history

Notices posted for this opportunity, newest first
Notice Type Posted
C-17 PSE - kit, wrench - core thrust reverser This notice · Latest solicitation Solicitation
C-17 PSE - kit, wrench - core thrust reverser Original Pre-Solicitation

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