AirSpec.pdf

Brian Umbaugh/OO-ALC/GHGJ

AIRMUNITIONS SPECIFICATIONS

NSN 1377-01-505-52I5ES

PR# FDZ020-II-77059

1. Contractor shall contact their nearest Defense Contract Management Agency (DCMA) Office for transportation guidance and assistance for all Foreign Military Sales (FMS) deliveries prior to shipment; and insure that the DCMA provides one information copy of completed Notice of Availability (NOA) including FMS case and requisition numbers to: 505 CBSS/GBLB Attn:

FMS Transportation by mail to 6043 Elm Lane, Hill AFB, UT 84056-5819 or FAX to (801) 777- 1089 or Email: 784CBSGrrransportation@Hill.af.mil.

2. DODIC Number is: JL70

3. One copy of all shipping documents shall be furnished to 510 CBSS/GBMAC, by mail to:

6038 Aspen Ave., Hill AFB, UT 84056-5805 or FAX to: (801)777-5545, and shall identify requisition number, MIPR number and line item.

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 (DI-MISC-80043).

S. Items shall be marked in accordance with CADIPAD Item Marking Instruction Version 1.1, 01 May 2008, reference attachment 3_

6. HAZARD CLASSIFICA TIOR

1377-01-505-5215ES

Hazard Class Division: 1.4 Storage Compatibility Group: S DOT M",king' CARTRIDGES, POWER DEVICE DOT Class: 1.4S DOT Label: Explosives, ].4S UN Serial Number: 0323 UN Proper Shipping Name: CARTRIDGES, POWER DEVICE

7. All configuration actions shall be in accordance with Industry Standard EIA-649.

8. Class I ECP's and Major/Critical RFD's shall be submitted to the responsible Government Engineering Authority for review/disposition by CCB Approval. Class II ECP's and Minor RFD's shall be dispositioned by the COGNIZANT GOVERNMENT ENGINEER.

9. Electronic Systems to encompass system, subsystems, pieces parts and assemblies shall not contain any Tin-Lead solder substitutes and finishes (Ref. GEIA-STD-0005-1 & -2). The use of Tin-Lead solder substitute requires approval through PCO by OO-ALC-GHGJ, REFERENCE "Airworthiness Advisory (AA-08~02) Lead-Free Electonics".

mailto:784CBSGrrransportation@Hill.af.mil.

Brian Umbaugh/784CBSG/GJ pRJI FD2020-11-77059

10. Item must pass both gross and fine leak checks. MIL-STD-883G, Method 1014.12 may be used as guidance. The existing leak rate limit established for this item(s) will remain the same.

Supplier shall generate a Lot Acceptance Test Plan (LA TP/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 (Dl-QCIC-80553)

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

12. Lot Acceptance Test Requirements are in accordance with the latest government approved

ATP.

13. The contractor shall furnish a TestJInspection Report, Lot Acceptance Test.

(DI-NDTI-80809)

14. LOT ACCEPTANCE TEST: In the event of an end item faiJure, the contractor shall notify the PCOIACO within 1work day and the responsible Air Force Engineering Organization within 1 work day. OO-ALC/GHGJ FAX (801) 777-7052 allen.hancey@hill.af.mil

15. Proposed corrective actions and recommendations shall be furnished in a Failure Analysis and Corrective Action Report (Dl-S£SS-81315).

16. The age of the energetic materials and components (i.e. ALL explosives, propellants, cartridges, and/or initiators) used in the manufacture of these items or sub-components shall not exceed 12 months based on the original manufacturer date. Primers shall have been certified Ire-certified within the past 12 months unless they are Navy certified and have a 2-year certification. Raw (non-blended) ingredients shaU follow established manufacturers shelf life for each ingredient or shall be recertified. All energetic materials and components must be traceable to the original manufacturing source. The government may waive this requirement, or portions thereof, on a case-by-case basis (when advantageous to the government) provided the contractor furnishes all details of the reason for the waiver and the age, lot numbers and COA I COC of the subject components. The waiver (if granted) may be subject to, but not limited to, conditions such as sensitivity testing, stabilizer analysis and/or dehumidification requirements.

17. First Article Test/Inspection Report. FAT-Contractor Test.

(DI-NDTI-80809)

18. First Article Test Plan and Procedures.

(DI-NDTI-81307)

mailto:allen.hancey@hill.af.mil