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This Solicitation opportunity from Department Of Defense was posted on March 6, 2023. The submission period has ended. Browse the details below for market research, or find similar active opportunities.

C-17 PSE - Bracket Angle, Mounting-Accelerometer

Closed
FA8526-23-Q-0012Federal

Contract Overview

Solicitation details, issuing organization, response deadlines, documents, and interested companies for this government contract opportunity.

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General Info

Contract Value

$19,382

NAICS

332510 - Hardware Manufacturing

Place of Performance

GA

Set-Aside

SBA

Award Issued Date

Documents

7

EDL Rev 2 - Bracket, Angle (NSN 5340013033614BA)

PDF, High priority: read this firstspecifications
High

FA8526-23-Q-0012 Request for Quotation

PDF, High priority: read this firstrfq
High

FD2060-23-30196 CDRL A001 - First Article Test/Inspection Procedures and Plan

PDF, High priority: read this firstcdrl
High

FD2060-23-30196 CDRL A002 - First Article Test/Inspection Procedures and Report

PDF, High priority: read this firstcdrl
High

FD2060-23-30196 CDRL A003 IUID Marking Plan

PDF, High priority: read this firstsow
High

FD2060-23-30196 Transportation Requirements (DD Form 1653)

PDF, High priority: read this firstspecifications
High

Packaging_Requirements_Form158.pdf

PDF

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Timeline

PhaseClosed
Posted

Solicitation

Response Deadline

Deadline has passed

Submission Closed

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Organization & Contact Information

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AgencyDepartment Of Defense → FA8526 Aflcmc Wlmka
Contacts2 people available
OfficeROBINS AFB, GA, 31098-2428, USA
Office AddressROBINS AFB, GA, 31098-2428, USA
Contacts
Philip Earthly
Kathryn Ferguson

Full Description

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** This is a 100% Small Business Set-Aside ** This requirement is for a firm-fixed price contract for two (2) each NSN: 5340-01-303-3614BA, Bracket Angle, Mounting-Accelerometer, P/N 17G230052-1, which includes one First Article and one production asset, one First Article Test Plan, one First Article Test Report, and one IUID Marking Plan. This requirement also includes three annual options containing a quantity of 3 each. The C-17 aircraft is powered by four (4) Pratt & Whitney F117-PW-100 high-bypass turbofan engines enclosed in isolated nacelles suspended below the wings. Part of the procedure for fault isolating the F11-PW-100 engine is to perform a vibration monitoring test while the engine, installed on the aircraft, is operated. Among the causes of excessive vibration is imbalance, bearing wear, and other types of mechanical deterioration. The vibration amplitude will be measured through the use of P/N 303-07C5 accelerometers mounted on the - B and - P flanges of the engine. The - B flange is located near the front of the engine, on the fan case. The - P flange is located near the back of the engine, on the engine turbine exhaust case. Am means is required at the organizational- and depot-level of maintenance to mount the accelerometer at the 12 o'clock position on the - B engine flange. The means for the - P flange will be documented separately. The mounting pad on the accelerometer has four (4) holes, 0.282 diameter, in a square pattern, 1.88 between adjacent holes. The hole spacing between bolts on the - B flange is approximately 2.508. The holes on the flanges will accommodate 0.250 diameter bolts. The means must be rigid enough to transmit the vibrations from the engine flange to the accelerometer without distorting the vibration signal. This will be a 100% Small Business Set-Aside. Offerors shall prepare their proposals in accordance with the mandatory, explicit, and detailed instructions contained in the RFQ. All responsible small business sources may submit a proposal to be considered by the contracting 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.

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