AIR SPEC.pdf
PDF 106 KB Posted
- Attached to
- Inert Firing Assemblies Federal contract opportunity
- Solicitation number
- FA8213
About this file
This document outlines the requirements for an inert firing assembly sole source contract opportunity with the Department of the Air Force Materiel Command Lifecycle Management Center. The contractor shall provide two inert critical safety items for CAD/PAD functions, including an interseat sequencing valve and a unit firing assembly, with advanced shipment notifications and item markings in accordance with specified standards. Lot acceptance testing is required prior to commencement, with leak checks, failure reporting procedures, and government approval of nonconforming materials and rework. Documentation of critical characteristics must also be provided under the contract.
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Other files for this federal contract opportunity
| File | Type | Posted |
|---|---|---|
| Item Des (0709).pdf | ||
| TransInstruction.pdf | ||
| Special Packing Instructions.pdf | ||
| QAIR (0709) 807.pdf | ||
| Packaging SOW MILB.pdf | ||
| AFMC FORM 158 MIPR.pdf | ||
| Item Des (9367).pdf | ||
| REWORK.pdf | ||
| REPSHIP.pdf | ||
| SOW.pdf | ||
| QAIR (9367) 807.pdf | ||
| AFMC FORM 158 2OF2.pdf | ||
| QALI.pdf | ||
| CADPAD_Marking Instructions.pdf | ||
| DD 1653.pdf | ||
| Packaging SOW SPI.pdf |
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Text version
AIRMUNITION SPECIFICATION
FD2020-20-50064 (USAF)
NSN: 1377-99-148-0709ES
1377-99-998-9367ES
1. The contractor shall provide an advanced Report of Shipment (REPSHIP) to the consignee no later than 24 hours prior to the shipment arrival, and for ammunition shipments no later than two hours after shipment departure. A (REPSHIP) shall include all the following data in accordance with ATTACHMENT 1.
2. Items shall be marked in accordance with CAD/PAD Item Marking Instruction Version 1.5, 1
May 2019, reference attachment.
3. Shelf Life Code marking NOT required per MIL-STD-129R.
4. Items are inert.
5. All Engineering Change Proposals (ECPs), Notice of Revisions (NORs), and Request For
Variances (formerly RFD/RFWs) affecting the approved product baseline configuration, acceptance test procedures, or manufacturing process of any item(s) on this contract shall be in accordance with EIA-649B. Major ECPs with NORs and Critical/Major RFVs shall be submitted to the responsible Government Engineering Authority for review/disposition by CCB.
Minor/Administrative ECPs with NORs and Minor RFVs shall be processed by the:
COGNIZANT GOVERNMENT ENGINEER
ECPs – CDRL (DI-SESS-80639D) – A001
NORs – CDRL (DI-SESS-80642D) – A002
RFVS – CDRL (DI-SESS-80640D) – A003
Distribution Statement B, Reason: Administrative or Operational Use.
6. Item(s) must pass both gross and fine leak checks. MIL-STD-883K, Method 1014.15 may be used as guidance. The existing leak rate limit established for this item(s) will remain the same.
Contractor shall generate a Lot Acceptance Test Plan (LATP/ATP) with an analysis or test results showing compliance for Hill AFB engineering approval at least 90 days prior to commencement of Lot Acceptance Testing allowing for 30 days approval time after submission.
CDRL (DI-QCIC-80553A) – A004
7. Lot Acceptance Test Requirements are: IAW latest Gov’t approved ATP.
Contractor
8. The contractor shall furnish a Lot Acceptance Test/Inspection Report in the following system(s): WAWF
CDRL: (DI-NDTI-80809B) – A005
9. LOT ACCEPTANCE TEST: In the event of an end item failure, the contractor shall notify the
PCO/ACO and Air Force Engineering Organization within 1 business day
Air Force Engineering Organization: AFLCMC/EBHJ
Organization Fax/E-mail: (801) 777-4135 / lawrence.kramer.1@us.af.mil
10. In the event of test failure(s), a Failure Summary and Analysis Report with proposed corrective actions/recommendations is required.
CDRL: (DI-SESS-80255A) – A006
11. This item is designated as a Critical Safety Item (CSI). Documentation for critical characteristics may be found in the contract, TDP, assembly/inspection procedures or QALI.
MRB approval authority shall be retained by government engineer. Other characteristics requiring inspection or special oversight from DCMA:
See attached QALI
12. Approval from government engineer is required prior to rework and repair of nonconforming material (See Attachment #5).
File details come from the government source that posted it. Updated .