SOW Repair Kit Brake.pdf
PDF 166 KB Posted
- Attached to
- Brake Line Repair Kit - Tyndall AFB Federal contract opportunity
- Solicitation number
- FA481921QA005
About this file
This statement of work outlines requirements for a brake line repair kit for Tyndall Air Force Base. The contractor shall provide 100 each Repair Kit, Brake with part number 9843442-1 per the attached drawings. First article testing will be required for any contractor who has not produced the item for the Air Force within the last 60 months. The contractor must submit the first article for testing within 180 days, with 30 days allowed for Air Force review and 150 days to deliver remaining items thereafter. The first article must pass third party verification of dimensions, materials, welds and components. Tyndall Air Force Base will inspect the first article and documentation for form, fit and function. Conditionally approved first articles will be retained by the Air Force. All items shall be delivered to Tyndall Air Force Base by the specified dates.
View the file
Other files for this federal contract opportunity
| File | Type | Posted |
|---|---|---|
| Combined Synopsis Solicitation Brake Line Repair.docx | DOCX document | |
| Attachment 2 - Stator Plate Assembly Repair Kit Brake Drawing 9843443-10.pdf | ||
| Attachment 5 - Backing Plate Assembly Repair Kit Brake Drawing 9843446-10.pdf | ||
| Attachment 3 - Pressure Plate Assembly Repair Kit Brake Drawing 9843444-10.pdf | ||
| Combined Synopsis Solicitation Brake Line Repair.docx | DOCX document | |
| Attachment 1 - Repair Kit Brake Drawing 9843442-1.pdf | ||
| Attachment 4 - Rotor Plate Assembly Repair Kit Brake Drawing 983445-10.pdf |
On GovTribe
Work with this file on GovTribe
- Download the original file
- Contacts named in this file
- Similar government files
- Ask GovTribe AI about this file
Text version
22 October 2020
Statement of Work CEMIRT BAK-12 Parts and Equipment
1. PURPOSE: The contractor shall furnish all required parts, equipment, material, and labor to provide the following items in accordance with (IAW) all applicable codes, specifications, and industry/federal standards to CEMIRT at Tyndall AFB, Florida.
2. SCOPE:
1. Repair Kit, Brake – P/N: 9843442-1 – 100 Each:
a. See attachments 1 thru 5.
3. First Article Testing (FAT):
1. The purpose of this section is to detail the work required to fulfill the First Article Testing component of this contract.
a. FAT shall be required of any contractor who has not undergone, completed and received FAT approval for the item purchased under this contract, and has produced it for the USAF within the last 60 months.
2. This is an Air Force designated Critical Safety Item (CSI). All requests for waivers or deviations must be forwarded to the contracting officer for review and approval.
3. FAT shall be coordinated through the Air Force AAS Engineer, Mr. Christopher Peisher. Contact information is listed below:
a. AAS Engineer Point of Contact Christopher S. Peisher Aircraft Arresting Systems Engineer
WRLCMC/WNZEC
235 Byron St., Suite 19A Robins AFB GA 31098-1813 christopher.peisher@us.af.mil 478-222-1371
4. The Delivery Period shall be adjusted if a FAT is required. The timeline to conduct the FAT shall be as follows:
a. Submit First Article to CEMIRT: 180 days Government Review: 30 days Delivery Period for Remaining Balance: 150 days
b. The contractor shall have a total of 180 days to produce their first article for government testing. Should the contractor produce this article prior to the completion of this 180 day period, the contractor will have the remaining time to correct any deficiencies noted during the FAT. For example, if the first article is produced within 120 days, the contractor will have 60 days to correct any deficiencies identified and return the item for additional testing. This total period shall not exceed 180 days.
i. The first article shall be considered as having been provided to the government for FAT on the date that it arrives at Tyndall CEMIRT for testing. Additionally, the date that notification of First Article deficiencies is provided to the contractor shall be considered the date that the contractors period for FAT submittal recommences.
c. Any return of a First Article for correction of deficiencies shall be at the Contractor’s expense.
mailto:chr mailto:chr
5. First Article Testing shall be conducted as follows:
a. Testing will be in accordance with applicable drawings, specifications and/or engineering instructions. The First Article offered shall be manufactured at the facilities in which production quantities are procured and produced under this contract.
b. Third Party Verification – The contractor shall be responsible for providing third party lab verification of all characteristics of the item to include all dimensions, materials, welds, hardware and components. These shall be verified by visual inspection, inspection of material certifications, inspection of welder’s certifications and inspection of shipment invoices.
Documentation of successful third party verification shall be included with the First Article.
c. Form, Fit and Function and Configuration Conformity Check – The contractor shall provide the First Article Tyndall CEMIRT for inspection.
When submitting the First Article for government testing, a copy of the contract and all applicable drawings, specifications, engineering instructions, certifications and inspection sheets (to include all applicable data identified during third party verification) shall be provided.
Additionally, First Article packaging must be clearly marked as “FIRST ARTICLE TEST EXHIBIT.” Tyndall CEMIRT shall perform a form, fit and function check verifying all operational aspects of the first article.
6. Approved and conditionally approved First Articles shall be retained by the government for use. Retention of this item will qualify as the first production item.
7. Deliver Government First Article to:
a. CEMIRT
Attn: Bruce Goodwill 100 Mississippi Road Bldg. 1141 Tyndall AFB, FL 32403-5318
Attachments
1. - Repair Kit, Brake Drawing #: 9843442-1
2. - Stator Plate Assembly, Repair Kit, Brake Drawing #: 9843443-10
3. - Pressure Plate Assembly, Repair Kit, Brake Drawing #: 9843444-10
4. - Rotor Plate Assembly, Repair Kit, Brake Drawing #: 983445-10
5. - Backing Plate Assembly, Repair Kit, Brake Drawing #: 9843446-10
| Statement of Work CEMIRT BAK-12 Parts and Equipment |
| 2. SCOPE: |
| 3. First Article Testing (FAT): |
File details come from the government source that posted it. Updated .