AirSpec.doc

AIRMUNITION SPECIFICATION (19 Mar 2018)

FD2020-19-50002

NSN: 1377012348510ES or 1377013849246ES, 1377012449273ES or1377013758919ES, 1377012698061ES or 1377013840106ES

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. DODIC Number: SQ34-1377012348510ES and 1377013849246ES and 1377014320349ES, MT60-1377012449273ES and 1377013758919ES and 1377014368364ES, MT64-1377012698061ES and 1377013840106ES and 1377014300447ES.

3. Government Furnished Material:

NSN: 1376012215665ES, Part number: HES 5808-23

NOUN: Propellant, Qty: 1 lb

4. Ammunition Data Cards (ADC) shall be filled out; input in accordance with Attachment 2, Statement of Work – Ammunition Data Cards; and state quantity/serial number of lot acceptance test Units in the remarks block. One hard copy of the ADC shall accompany shipments to each shipping location. CDRL (DI-MISC-80043B).

5. Items shall be marked in accordance with CAD/PAD Item Marking Instruction Version 1.3, 19 Apr 2016, Reference Attachment.

6. Shelf Life Code Marking NOT required per MIL-STD-129R.

7. For NSNs 1377012348510ES, 1377012698061ES, 1377013840106ES, 1377013849246ES, 1377014300447ES, 1377014320349ES Hazard Class Division: 1.4

Storage Compatibility Group: C DOT Marking: CARTRIDGES, POWER DEVICE DOT Class: 1.4C DOT Label: Explosive 1.4C UN Serial Number: 0276 UN Proper Shipping Name: CARTRIDGES, POWER DEVICE For NSNs 1377012449273ES, 1377003758919ES, 1377014368364ES

Hazard Class Division: 1.4

Storage Compatibility Group: S

DOT Marking: FUZES, DETONATING

DOT Class: 1.4S

DOT Label: Explosive 1.4S

UN Serial Number: 0367

UN Proper Shipping Name: FUZES, DETONATING

Net Explosive Weight NEW 0.002300 lbs for 1377012348510ES and 1377012698061ES, 0.000600 lbs for 1377012449273ES and 1377003758919ES, 0.001300 for 1377013840106ES and 1377013849246ES, 0.001500 lbs for 1377014300447ES and 1377014320349ES, 0.000500 lbs for 1377014368364ES. All packaging/shipping documents shall reflect the NEW identified above per JHCS or IHC. If NEW is altered to adjust item performance and is greater than the weight listed, an ECP shall be submitted to the government prior to manufacturing or at least 60 days prior to shipping and shall include the SDS (formerly MSDS) and applicable supporting documentation.

7. All Engineering Change Proposals (ECP’s), Notice of Revisions(NORs) and Requests for Variances (RFVs formerly RFD/RFW) affecting the approved product baseline configuration, acceptance test procedures, or manufacturing process of any time(s) on this contract shall be in accordance with EIA-649-B. Major ECPs with NORs and Critical/Major RFV’s shall be submitted to the responsible Government Engineering Authority for review/disposition by CCB. Minor/Administrative ECP’s with NOR’s and Minor RFVs shall be processed by the Cognizant Government Engineer, ACO.

ECPs-CDRL (DI-SESS-80639D)

NORs-CDRL (DI-SESS-80642D) RFVs-CDRL (DI-SES-80640D)

Distribution Statement: B, Reason: Administration use only (Engineer – ref. DoD 5230.24)

8. Item(s) must pass both gross and fine checks. MIL-STD-883K, Method 1014.13 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).

9. Lot Acceptance Test requirements are: In accordance with latest government approved ATP. Contractor

10. The contractor shall furnish a Lot Acceptance Test/Inspection Report in WAWF, CDRL: (DI-NDTI-80809B).

11. 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, matthew.tanner.7@us.af.mil.

12. In the event of test failure(s), a Failure Summary and Analysis Report with proposed corrective actions/recommendations is required. CDRL (DI-SESS-80255A).

13. If Hexanitrostilbene (HNS) explosive material is used in the manufacture of this item, the HNS shall meet the requirements of Government Document WS5003F (or latest revision), Purchase Description of HNS Explosive; and maximum particle size shall not exceed 250 microns.

14. The age of energetic materials and components (i.e. ALL explosive, propellants, pyrotechnics, cartridges, and/or initiators) used in the manufacture of these items or sub-components shall not exceed 24 months based on the original manufacturing date. All energetic materials and components must be traceable to the original DoD qualified manufacturer and compliant with the ITAR part 120 and 121 (http:/www.pmddtc.state.gov/regulation_laws/itar_official.html).

15. Raw (non-blended) ingredients and materials used in blended/mixed energetic materials such as, but not limited to: fuels, oxidizers, binders, curatives, sensitizers, plasticizers, stabilizers etc., shall not exceed 24 months since date of manufacture and comply with original manufacture’s MIL-STD. The Government may waive the energetic and constituent material requirements listed above or portions thereof, on a case-by-case basis (when acceptable to the government) provided the contractor furnishes all details of the reason for the variance and the age, lot numbers, traceability, and other pertinent information/test data and Certificate of analysis/Conformance (COA/COC) of the subject materials or components. The variance shall be submitted as a RFV and may be subject to, but not limited to, conditions such as sensitivity testing, stabilizer and analysis and/or dehumidification at vendor’s cost; therefore, vendor must plan accordingly. RFV not required provided vendor has approved energetic material and constituent management and recertification plan approved by HAFB technical authority for this specific contract and contract is executed with materials in compliance with said plan. Recertification test data for materials shall be provided by vendor upon request at no additional charge to the government. All ray ingredients, materials and components must be traceable to the original DoD qualified manufacturer and compliant with the ITAR part 120 and 121

16. Percussion primers shall have been certified/recertified by performing sensitivity (all-fire/no fire) and dud testing per applicable specification within the past 24 months unless they are Navy certified and have a 2 year certification. Primers shall be stored in a temperature and humidity controlled environment and in a sealed container with desiccant from time of primer manufacturing, shipping, storage and through final installation in end item. All primers shall be X-rayed in top and side views for critical defects prior to use.

17. 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.

18. Approval from Government engineer is required prior to rework and repair of nonconforming material (see attachment 5)

19. First Article Test/Inspection Report IAW AFMC Form 260. FAT-Contractor Test. CDRL (DI-NDTI-80603A)

20. Contracts involving ammunition and explosives (AE) will contain:

-DFARS Titles 48 Part 252.223-7002, Safety Precautions for Ammunition and Explosives.

-DFARS Title 48 Part 252.223-7003, change in Place of Performance – Ammunition and Explosives

Additionally, if the scope of work includes air shipment of explosives, the safety specification should require contractor compliance with:

-AFMAN 24-204(1), Preparing Hazardous Materials for Military Air Shipments