Attachment_0016_M82E3_Percussion_Primer_Draft_Spec_(Foam_Washer)_Final_Draft_2017_06_20.docx
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- M82 Percussion Primers Federal contract opportunity
- Solicitation number
- W52P1J-17-R-0007
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Attachment 0016 M82E3 Percussion Primer Draft Spec (Foam Washer) Final Draft 2017 06 20
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INCH-POUND
NOTE: This draft 20 June 2017 prepared by U.S. Army ARDEC, RDAR-QES-E, Picatinny Arsenal, NJ has not been approved and is subject to modification. DO NOT USE PRIOR TO APPROVAL. (Project #?)
| MIL-DTL-M82-FW | ||
| (AR) | (AR) |
DRAFT
DETAIL SPECIFICATION-Draft
PRIMER, PERCUSSION, M82-FW
This specification is approved for use by the US Army and is available for use by all Departments and Agencies of the Department of Defense.
1. SCOPE
1.1 Scope. This specification covers the metal parts/loading, assembling and packing for Primer, Percussion, M82-FW (Foam Washer attached to plunger configuration).
2. APPLICABLE DOCUMENTS
2.1 General. The documents listed in this section are specified in sections 3 and 4 of this specification. This section does not include documents in other sections of this specification or recommended for additional information or as examples. While every effort has been made to ensure the completeness of this list, document users are cautioned that they must meet all requirements documents cited in sections 3 and 4 of this specification, whether or not they are listed.
MIL-DTL-82-FW
Comments, suggestions, or questions on this document should be addressed to: Commander, U.S. Army ARDEC, ATTN: AMSRD-AAR-QES-E, Picatinny, New Jersey 07806-5000 or e-mailed to usarmy.picatinny.ardec.list.ardec-stdzn-branch@mail.mil. Since contact information can change, you may want to verify the currency of this information using ASSIST Online database at https:/ /assist.dla.mil.Distribution Statement D- Distribution Authorized to the Department of Defense and U.S. DOD Contractors only (Critical Technology, 01 June 2015). Other requests shall be referred to office of the Project Manager, SFAE-AMO-CAS, ATTN:Conventional Ammo Division, Picatinny Arsenal, NJ 07806.
2.2 Government documents
2.2.1 Specifications, standards, and handbooks. The following specifications, standards, and handbooks form a part of this specification to the extent specified herein. Unless otherwise specified, the issues of these documents are those listed in the issue of the Department of Defense Index of Specifications and Standards (DoDISS) and supplement thereto, cited in the solicitation.
SPECIFICATIONS
STANDARDS
DEPARTMENT OF DEFENSE
MIL-P-223 - Powder, Black
MIL-STD-331 - Fuze and Fuze Component, Environmental and Performance Tests for.
MIL-STD-1168 - Ammunition Lot Numbering and Ammunition Data Card
MIL-STD-1916 - DOD Preferred Methods for Acceptance of Product
| TT-C-490 - Chemical Conversion Coatings and Pretreatments for | |
| Metallic Substrates (Base for Organic Coatings) |
(Copies of these documents are available online at http://quicksearch.dla.mil/ or from the Standardization Document Order Desk, 700 Robbins Avenue, Building 4D, Philadelphia, PA 19111-5094.)
2.2.2 Other Government documents, drawings and publications. The following other Government documents, drawings and publications form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents are those cited in the solicitation (see 6.2).
US ARMY ARMAMENT RESEARCH, DEVELOPMENT AND
ENGINEERING CENTER (ARDEC) DRAWINGS
| 8796535 Carton, packing, domestic | |
| 8796678 Carton, packing, overseas | |
| 8796679 Box, packing, overseas | |
| 8802117 Testing Fixture Primer Sensitivity Sub Assembly & Details | |
| 8861197 Primer, Percussion, M82, Assembly | |
| 8861198-1 Body (external groove) | |
| 8861199 Ignition Element Assembly | |
| 8861200 Cup, Ignition | |
| 8861201 Container, charge assembly | |
| 8861203 Tube, container | |
| 8861204 Container assembly | |
| 8861206 Closure | |
| 8861211-FW Plunger | |
| 8872774 Gage Concentricity | |
| WSHR001 Foam Washer | |
| 10522621 Primer No.34 | |
| DS000515 Packing and Marking for Box, Wirebound for M82 | |
| DS000516 Packing and Marking for Box, Metal, Ammunition, M2A1 for | |
| M82 | |
| DS000517 Packing and Marking for Box, Fiberboard for M82 |
DS000848 Combination of Adopted Items For: M82-FW
U.S. ARMY DEFENSE AMMUNITION CENTER (DAC) DRAWINGS
| 19-48-4116/158G Unitization Procedures for Boxed Ammunition and | |
| Components on 4-Way entry pallets | |
| 19-48-4116-20PA1002 Basic Unitization Procedures | |
| ACV00561 Unit Load Markings | |
| ACV00831 Heat Treatment of Wooden Pallets, Skids, Filler | |
| Assemblies, and Dunnage Assemblies |
Test Operation Procedure (TOP)
| TOP 4-2-602 - Test Operations Procedure 4-2-602 U.S. Army Test and | |
| Evaluation Command |
2.3 Non-Government publications.
| AMERICAN SOCIETY FOR TESTING AND MATERIALS (ASTM |
| INTERNATIONAL) |
| ASTM B154 - Standard Test Method for Mercurous Nitrate Test for Copper | ||
| Alloys | ||
| ASTM E112 - Standard Test Methods for Rockwell Hardness of Metallic | ||
| Materials | ||
| ASTM E18 - Standard Test Methods for Rockwell Hardness of Metallic | ||
| Materials |
| (Copies of ASTM standards may be ordered online at http://www. Astm.org/ or |
| from the ASTM International, 100 Barr Harbor Drive, Conshohocken, PA |
| 19428-2959)’’) |
2.4 Order of precedence. In the event of a conflict between the text of this document and the references cited herein, the text of this document takes precedence. Nothing in this document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained.
3. REQUIREMENTS
3.1 First article. When specified (see 6.2), a sample shall be subjected to first article inspection in accordance with 4.2.
3.2 Conformance. A sample shall be subjected to conformance inspection in accordance with 4.3.
3.3 Materials, components and assemblies. Materials, components, and assemblies shall be in accordance with all requirements specified on drawings 8861197, 8861199, 8861201, WSHR001, DS000515, 19-48-4116/158G.
3.3.1 Primer No. 34. The primer No. 34 shall comply with Drawing 10522621 when tested as Cartridge, 7.62mm, NATO, Ball, M80.
3.4 Ammunition lot numbering. Ammunition lot numbers shall be assigned in accordance with MIL-STD-1168C.
3.5 Moisture content of black powder. The moisture content of the black powder at the loading station, at the time of loading shall not exceed 0.5 percent when determined as specified in 4.4.3.
3.6 Mercurous Nitrate Test. The primer bodies shall exhibit no crack when subjected to the mercurous nitrate test specified in 4.7.9.
3.7 Non-Functioning Test. The primer, without the black powder charge, shall not function under an applied impact energy value of 24.51 inch ounces minimum (min.), when tested as specified in 4.7.1.
3.7.1 Non-Functioning sampling plan. The sampling plan for the non-functioning test shall be in accordance with table III. Any primer which fails to comply with the applicable requirement shall be classified as defective. The test shall be performed as specified in 4.7.1.
3.8 Functioning
3.8.1 Static Test. The primers, without the black powder charge, shall function under an applied impact energy value of 147.06 inch ounces maximum (max.) when tested as specified in 4.7.3.
3.8.2 First Article Ballistic Test. The primers, with the black powder charge, shall fire, with no perceptible hangfires, metal parts separation, or evidence of rupture or erosion and the primer must obturate and shall remain intact upon firing, when tested as specified in 4.7.4.
3.8.3 Chamber gage. The completed primer shall freely enter the prescribed chamber gage and shall be tested according to the requirements in Drawing #8872774.
3.9 Modified Bruceton sensitivity test. A modified Bruceton sensitivity test shall be performed on each lot of No. 34 primers for use in the M82 primers. The test shall be conducted in accordance with 4.7.5 and the test results shall be fully evaluated for acceptance by the Technical Agencies prior to use in the M82 primers.
3.10 Air Pressure test. 150 container assemblies shall be randomly selected for this test.
3.11 Rockwell Hardness test. Ten bodies shall be randomly selected for this test.
3.12 Grain Size test. Ten bodies shall be randomly selected for this test.
3.13 Rupture test. 110 container assemblies shall be randomly selected for this test.
3.14 Workmanship. Components shall be free of burns, sharp edges, cracks, dirt, grease, corrosion, and other foreign matter. Cleaning methods used shall not be injurious to any parts, nor shall the cleaning agents contaminate the parts. All required marking and stamping shall be neat and sharply defined.
4. Verification
Table I. Requirements/verification cross reference matrix
| Method of Verification |
| Classes of Verification |
1- Analysis 2- Demonstration 3- Examination 4- Test
A - First Article
B - Conformance
Section 3 Requirements
| Description |
| Verification |
Method Verification Class Section 4 Verification
| 1 |
| 2 |
| 3 |
| 4 |
| A |
| B |
| 3.1 |
| First Article |
| X |
| X |
| X |
| X |
4.2
| 3.2 |
| Conformance |
| X |
| X |
| X |
| X |
| 4.6 |
| 3.3 |
| Materials, Components and assemblies |
| X |
| X |
| X |
| X |
| 4.6.2.1-4.6.2.23 |
| 3.4 |
| Ammunition lot numbering |
X
| X |
| X |
| 4.6.1 |
| 3.5 |
| Moisture content |
| X |
| X |
| X |
| 4.7.6 |
| 3.6 |
| Mercurous nitrate test |
| X |
| X |
| X |
| X |
| 4.7.9 |
| 3.7 |
| Non- Functioning |
| X |
| X |
| X |
| 4.7.1 |
| 3.8 |
| Functioning |
| X |
| X |
| X |
| 4.7.2 |
| 3.9 |
| Modified bruceton sensitivity test |
| X |
| X |
| X |
| X |
| 4.7.5 |
| 3.10 |
| Air pressure test |
| X |
| X |
| X |
| X |
| 4.7.11 |
| 3.11 |
| Rockwell hardness test |
| X |
| X |
| X |
| X |
| 4.7.14 |
| 3.12 |
| Grain size test |
| X |
| X |
| X |
| X |
| 4.7.15 |
| 3.13 |
| Rupture test |
| X |
| X |
| X |
| X |
| 4.7.10 |
| 3.8.2 |
| Primer assembly first article ballistic test |
X
| X |
| X |
| X |
| 4.7.4 |
| 3.10 |
| Workmanship |
| X |
| X |
| X |
| X |
| 4.6.2.1-4.6.2.23 |
4.1 Classification of inspection. The following types of inspection shall be conducted on this item:
a. First Article inspection (see 4.2)
b. Conformance Inspection (see 4.6)
4.2 First Article inspection. When specified, a sample shall be subjected to first article verification in accordance with Table II.
4.3 First article rejection. If any assembly, component or test specimen fails to comply with any of the applicable requirements, the first article sample shall be rejected.
4.4 No. 34 Primer Qualification. This is a one-time qualification test for new manufacturers of No. 34 primers for use in the M82 primers.
4.4.1 Submission. Test samples shall be randomly withdrawn from the first lot produced by the new manufacturer of No. 34 primers. The test sample shall be tested in accordance with all the requirements of this specification and with 4.4.2, 4.4.2.1 and 4.4.2.2. Until the first article test has been performed and found to be acceptable (the test data will be evaluated by the Technical Agencies), the contractor is in no way authorized by the Government to initiate second lot production unless otherwise directed by the Contracting Officer.
4.4.2 Ignition element assembly vibration test. One thousand (1000) No. 34 primers shall be loaded into ignition element assemblies (Dwg. 8861199) and tested as follows:
4.4.2.1 Five hundred (500) ignition element assemblies from 4.4.2 shall be conditioned at 145 degrees F for 24 hours and tested in accordance with test #119, procedure 2 of MIL-STD-331C vibration frequency 5Hz-500Hz-5Hz in sweep method. Sweep logarithmically in 30 minute cycles for one hour. After the vibration test, all the assemblies shall be subjected to visual inspection. Any evidence of breakup of the cellulose disk or dusting of lead styphnate will be cause for rejection of the first article test samples.
4.4.2.2 Five hundred (500) ignition element assemblies from 4.4.2 shall be conditioned at -65 degrees F for 24 hours and tested in accordance with test #119, procedure 2 of MIL-STD-331C vibration frequency 5Hz-500Hz-5Hz in sweep method. Sweep logarithmically in 30 minute cycles for one hour. After the vibration test, all the assemblies shall be subjected to visual inspection. Any evidence of breakup of the cellulose disk or dusting of lead styphnate will be cause for rejection of the first article test samples.
4.4.3 Loose cargo and functioning test. Four hundred and fifty
| (450) No. 34 primers shall be loaded into M82 primers and tested as |
| follows: |
| 4.4.3.1 145 degrees F. One hundred and fifty (150) M82 |
| primers from 4.4.3 shall be conditioned at 145 degrees F for a |
minimum of 24 hours and subjected to loose cargo test in accordance with TOP 4-2-602. After the loose cargo test, all the M82 primers shall be tested for functioning in a M109 Howitzer with a bump spindle without propelling charge or projectile.
4.4.3.2 70 degrees F. One hundred and fifty (150) M82 primers from 4.4.3 shall be conditioned at 70 degrees F for a minimum of 24 hours and subjected to loose cargo test in accordance with TOP 4-2-602. After the loose cargo test, all the M82 primers shall be tested for functioning in a M109 Howitzer with a bump spindle without propelling charge or projectile.
4.4.3.3 -65 degrees F. One hundred and fifty (150) M82 primers from 4.4.3 shall be conditioned at -65 degrees F for a minimum of 24 hours and subjected to loose cargo test in accordance with TOP 4-2-602. After the loose cargo, all the M82 primers shall be tested for functioning in a M109 Howitzer with a bump spindle without propelling charge or projectile.
4.4.4 M82 primer functioning test. Two thousand (2000) No. 34 primers shall be loaded into M82 primers and tested as follows:
4.4.4.1 145 degrees F. One thousand (1000) M82 primers from 4.4.4 shall be conditioned at 145 degrees F for a minimum of 24 hours and tested for functioning in a M109 Howitzer with a bump spindle without propelling charge or projectile.
4.4.4.2 -65 degrees F. One thousand (1000) M82 primers from 4.4.4 shall be conditioned at -65 degrees F for a minimum of 24 hours and tested for functioning in a M109 Howitzer with a bump spindle without propelling charge or projectile.
Table II. First article inspection.
| Number of FAT Samples |
| Requirement Paragraph |
| Inspection Method |
Cup, Ignition, Dwg. 8861200 Examination for Defects
| 25 |
| 3.3 |
| 4.6.2.5 |
Closure, Dwg. 8861206 Examination for Defects
| 25 |
| 3.3 |
| 4.6.2.3 |
Body, Dwg. 8861198 Examination for Defects
| 3.3 |
| 4.6.2.4 |
Plunger, Dwg. 8861211-FW Examination for Defects
| 25 |
| 3.3 |
| 4.6.2.6 |
Foam Washer, Dwg. WSHR001 Examination for Defects
| 25 |
| 3.3 |
| 4.6.2.16 |
Container Assembly, Dwg. 8861204 Examination for Defects
| 25 |
| 3.3 |
4.6.2.2
Container, charge assembly, prior to sealing closure Dwg. 8861201 Examination for defects
| 25 |
| 3.3 |
| 4.6.2.8 |
Container, charge assembly Dwg. 8861201 Examination for defects
| 25 |
| 3.3 |
| 4.6.2.9 |
Container cup, Dwg. 8861205 Examination for defects
| 25 |
| 3.3 |
| 4.6.2.23 |
Ignition Element Assembly, Dwg. 8861199 Examination for Defects
| 25 |
| 3.3 |
| 4.6.2.7 |
Nonfunctioning test Dwg. 8861197 Examination for defects
| 150 |
| 3.7 |
| 4.7.1 |
Functioning test(without black powder) Dwg. 8861197 Examination for defects
| 900 |
| 3.8 |
| 4.7.2.1 |
Functioning test (with black powder) Dwg. 8861197 Examination for defects
| 25 |
| 3.8 |
| 4.7.2.2 |
Primer, Percussion, M82, Assembly Dwg. 8861197 Examination for Defects
3.3
4.6.2.10-4.6.2.12
Tube,container Dwg. 8861203 Examination for defects
| 25 |
| 3.3 |
| 4.6.2.1 |
Assembly, prior to inserting ignition element Dwg. 8861197 Examination for defects
| 25 |
| 3.3 |
| 4.6.2.10 |
Assembly, prior to assembling container charge assembly Dwg. 8861197 Examination for defects
| 25 |
| 3.3 |
| 4.6.2.11 |
Modified Bruceton Test Examination for defects
| 200 |
| 3.9 |
| 4.7.5 |
Mercurous Nitrate Test Examination for defects
| 25 |
| 3.6 |
| 4.7.9 |
Air Pressure Test Examination for defects
| 150 |
| 3.10 |
| 4.7.11 |
Rockwell Hardness Test Examination for defects
| 10 |
| 3.11 |
| 4.7.14 |
Grain Size Test Examination for defects
| 10 |
| 3.12 |
| 4.7.15 |
Rupture Test Examination for defects
| 110 |
| 3.13 |
| 4.7.10 |
Table III. First article inspection (packaging)
| Examination or Test |
| Number of FAT Samples |
| Requirement Paragraph |
| Inspection Method |
Packing and Marking for box, fiberboard (Sealed Envelope)
DS000517
Examination for defects
| 10 |
| 5.1 |
| 4.6.2.17 |
Packing and Marking for box, fiberboard (Fiberboard Box)
DS000517
Examination for defects
| 8 |
| 5.1 |
| 4.6.2.18 |
Packing and Marking for box, metal, ammunition, M2A1 (prior to closing)
DS000516
Examination for defects
| 8 |
| 5.1 |
| 4.6.2.19 |
Packing and Marking for box, metal, ammunition, M2A1 (closed)
DS000516
Examination for defects
| 8 |
| 5.1 |
| 4.6.2.20 |
Packing and marking for box, wirebound
DS000515
Examination for defects
| 4 |
| 5.1 |
| 4.6.2.21 |
Unitization procedures for boxed ammunition and components on 4-way entry pallets 19-48-4116/158G Examination for defects
| 1 |
| 5.1 |
| 4.6.2.22 |
4.6 Conformance inspection.
4.6.1 Lot formation. Lot formation shall be in accordance with lot formation requirement of MIL-STD-1916 paragraph 4.2, Acceptance by Tables. In addition, each lot of primers shall contain:
a. Percussion primers of one lot interfix number from one manufacturer.
b. Primer metal components of one lot interfix number from one manufacturer.
c. Black powder from not more than two lot numbers with the same interfix number from one manufacturer. A lot of black powder shall be used to completion.
4.6.2 Classification of characteristics
a. Sampling requirements. Inspection sampling requirements for critical, major and minor characteristics are defined in MIL-STD-1916. Unless specified otherwise, Verification Level VII in addition to 100% inspection shall be used for all characteristics defined as Critical, Verification Level IV shall be used for all characteristics defined as Majors and Inspection Level II for all Minor characteristics.
b. Conformance inspection. Conformance inspection shall be performed in accordance with paragraph 4.6.2.1 through 4.6.2.23. For all conformance inspections the same sample specimen may be used for all non-destructive examinations or tests.
c. Alternative inspections. Alternative conformance inspections may be submitted and approved in accordance with MIL-STD-1916.
MIL-P-60318C (AR)
CONFORMANCE INSPECTION
CLASSIFICATION OF CHARACTERISTICS
PARAGRAPH
4.6.2.1
TITLE
Tube, container
DRAWING NUMBER
8861203
CATEGORY
| EXAMINATION OR TEST |
| CONFORMANCE CRITERIA |
| REQUIREMENT |
PARAGRAPH
PARAGRAPH REFERENCE/
INSPECTION METHOD
| Critical |
| None defined |
Major
| 101 |
| Pitch diameter of thread minimum, |
| Level IV |
| 3.3 |
| AIE |
| 102 |
| Major diameter of thread, min |
| Level IV |
| 3.3 |
| AIE |
| 103 |
| Length of effective thread, min |
| Level IV |
| 3.3 |
| AIE |
| 104 |
| Crack or deformation |
| Level IV |
| 3.3 |
| Visual |
Minor
Concentricity of outside diameter with threads Outside diameter Inside diameter of container cup end Inside diameter opposite cup end Concentricity of inside diameter with thread Concentricity of the inside diameter of cup end with thread Total length
Pitch diameter of threads, maximum (max.)
Major diameter of threads, max Width of slots, min Depth of slots Depth to interior shoulder, max Finish improper Evidence of poor workmanship
Level II
Level II Level II Level II Level II Level II
Level II Level II Level II Level II Level II Level II
3.3 3.3 3.3 3.3 3.3
3.3 3.3 3.3 3.3 3.3 3.3
AIE
AIE
AIE
AIE
AIE
AIE
AIE
AIE
AIE
AIE
AIE
AIE
AIE
Visual
PARAGRAPH
4.6.2.2
TITLE
Container Assembly
DRAWING NUMBER
8861204
CATEGORY
| EXAMINATION OR TEST |
| CONFORMANCE CRITERIA |
| REQUIREMENT |
PARAGRAPH
PARAGRAPH REFERENCE/
| Critical |
| None defined |
Major
Minor
Cup ruptured Air pressure test
Depth to cup, max Braze not 360° Freedom from oil and grease Freedom from alkalies and strong acids Evidence of poor workmanship Level IV Level IV
Level II Level II Level II Level II
Level II 3.3 3.3
3.3 3.3 3.3 3.3
3.14
AIE
AIE(4.7.11)
AIE
Visual Visual Manual(4.7.12)
Manual(4.7.13)
PARAGRAPH
4.6.2.3
TITLE
Closure
DRAWING NUMBER
8861206
CATEGORY
| EXAMINATION OR TEST |
| CONFORMANCE CRITERIA |
| REQUIREMENT |
PARAGRAPH
PARAGRAPH REFERENCE/
| Critical |
| None defined |
| Major |
| None defined |
Minor
Disc ruptured
Disc not completely fastened to washer Level II
Visual
| 203 |
| Washer split |
| Level II |
| 3.3 |
| Visual |
| 204 |
| Evidence of poor workmanship |
| Level II |
| 3.3 |
| Visual |
| 4.6.2.4 |
| Body(external groove) |
| Drawing Number |
8861198-1(Draft)
| Classification |
| Examination Or Test |
| Conformance |
| Requirement |
| Inspection Method |
| Criteria |
| Paragraph |
| Critical |
| None defined |
Major
| 101 |
| Concentricity of thread with outside surface |
| Level IV |
| 3.3 |
| AIE |
| 102 |
| Concentricity of hole through base with outside surface |
| Level IV |
| 3.3 |
| AIE |
| 103 |
| Concentricity of interior surface above hole through base with outside surface |
| Level IV |
| 3.3 |
| AIE |
| 104 |
| Concentricity of large inside diameter with outside diameter |
| Level IV |
| 3.3 |
| AIE |
| 105 |
| Pitch diameter of threads, max |
| Level IV |
| 3.3 |
| AIE |
| 106 |
| Minor diameter of thread, max |
| Level IV |
| 3.3 |
| AIE |
| 107 |
| Thickness of flange |
| Level IV |
| 3.3 |
| AIE |
| 108 |
| Length of groove |
| Level IV |
| 3.3 |
| AIE |
| 109 |
| Distance of groove |
| Level IV |
| 3.3 |
| AIE |
| 110 |
| Diameter of groove |
| Level IV |
| 3.3 |
| AIE |
| 111 |
| Chamfer to groove |
| Level IV |
| 3.3 |
| AIE |
Minor
| 201 |
| Length to datum diameter |
| Level II |
| 3.3 |
| AIE |
| 202 |
| Thickness from base to bottom of igniter |
Seat
| Level II |
| 3.3 |
| AIE |
| 203 |
| Concentricity of flange with outside surface |
| Level II |
| 3.3 |
| AIE |
| 204 |
| Thickness from base to shoulder below igniter seat |
| Level II |
| 3.3 |
| AIE |
| 205 |
| Diameter of plunger hole through base |
| Level II |
| 3.3 |
| AIE |
| 206 |
| Diameter of cavity above hole through base |
| Level II |
| 3.3 |
| AIE |
| 207 |
| Diameter of flange |
| Level II |
| 3.3 |
| AIE |
| 208 |
| Large inside diameter |
| Level II |
| 3.3 |
| AIE |
| 209 |
| Pitch diameter, min |
| Level II |
| 3.3 |
| AIE |
| 210 |
| Total length |
| Level II |
| 3.3 |
| AIE |
| 211 |
| Length to thread, max |
| Level II |
| 3.3 |
| AIE |
| 212 |
| Length to end of thread, min |
| Level II |
| 3.3 |
| AIE |
| 213 |
| Finish improper |
| Level II |
| 3.3 |
| Visual |
| 214 |
| Evidence of poor workmanship |
| Level II |
| 3.3 |
| Visual |
| Cup, Ignition |
| Drawing Number |
4.6.2.5
8861200
| Classification |
| Examination Or Test |
| Conformance |
| Requirement |
| Inspection Method |
| Criteria |
| Paragraph |
| Critical |
| None defined |
Major
| 101 |
| Depth of primer cavity |
| Level IV |
| 3.3 |
| AIE |
| 102 |
| Diameter of primer cavity |
| Level IV |
| 3.3 |
| AIE |
| 103 |
| Concentricity of primer cavity and thread |
| Level IV |
| 3.3 |
| AIE |
| 104 |
| Concentricity of flash hole and thread |
| Level IV |
| 3.3 |
| AIE |
| 105 |
| Total Length |
| Level IV |
| 3.3 |
| AIE |
| 106 |
| Flash hole obstructed |
| Level IV |
| 3.3 |
| Visual |
| 107 |
| Chamfer missing from end of flash hole |
| Level IV |
| 3.3 |
| Visual |
Minor
| 201 |
| Pitch diameter of thread |
| Level II |
| 3.3 |
| AIE |
| 202 |
| Major diameter of thread, min |
| Level II |
| 3.3 |
| AIE |
| 203 |
| Diameter of pilot, max |
| Level II |
| 3.3 |
| AIE |
| 204 |
| Length of pilot |
| Level II |
| 3.3 |
| AIE |
| 205 |
| Diameter of flash hole |
| Level II |
| 3.3 |
| AIE |
| 206 |
| Depth of slot |
| Level II |
| 3.3 |
| AIE |
| 207 |
| Width of slot, min |
| Level II |
| 3.3 |
| AIE |
| 208 |
| Chamfer missing from bottom of primer cavity at mouth of flash hole |
| Level II |
| 3.3 |
| Visual |
| 209 |
| Finish improper |
| Level II |
| 3.3 |
| Visual |
| 210 |
| Evidence of poor workmanship |
| Level II |
| 3.3 |
| Visual |
| Plunger |
| Drawing Number |
4.6.2.6
8861211-FW(Draft)
| Classification |
| Examination Or Test |
| Conformance |
Criteria Requirement Paragraph Inspection Method
| Critical |
| None defined |
Major
| 101 |
| Total Length |
| Level IV |
| 3.3 |
| AIE |
| 102 |
| Length to shoulder |
| Level IV |
| 3.3 |
| AIE |
| 103 |
| Diameter and profile of firing point |
| Level IV |
| 3.3 |
| AIE |
| 104 |
| Length of firing point |
| Level IV |
| 3.3 |
| AIE |
Minor
| 201 |
| Large diameter |
| Level II |
| 3.3 |
| AIE |
| 202 |
| Small diameter |
| Level II |
| 3.3 |
| AIE |
| 203 |
| Radius or chamfer missing |
| Level II |
| 3.3 |
| Visual |
| 204 |
| Finish improper |
| Level II |
| 3.3 |
| Visual |
| 205 |
| Evidence of poor workmanship |
| Level II |
| 3.3 |
| Visual |
| Ignition element assembly |
| Drawing Number |
4.6.2.7
8861199
| Classification |
| Examination Or Test |
| Conformance |
| Requirement |
| Inspection Method |
| Criteria |
| Paragraph |
| Critical |
| Total Length (over primer) max. |
| Level VII |
| 3.3 |
| AIE |
Major
| 101 |
| Primer missing or damaged |
| Level IV |
| 3.3 |
| Visual |
| 102 |
| Seal missing or incomplete at joint between primer and cup sidewall |
| Level IV |
| 3.3 |
| Visual |
| 103 |
| Primer inverted |
| Level IV |
| 3.3 |
| Visual |
| 104 |
| Cellulose disk missing |
| Level IV |
| 3.3 |
| See Note 1 |
Minor
| 201 |
| Evidence of poor workmanship |
| Level II |
| 3.3 |
| AIE |
Note 1: Ignition element assemblies shall be either visually or automatically inspected 100% for the presence of the cellulose disk. Any sample which is found to have the disk missing inside the ignition element assembly shall be removed from the lot. Inspection may be performed immediately prior to inserting the primer or after the primer is inverted.
| Container, charge assembly, prior to sealing closure |
| Drawing Number |
4.6.2.8
8861201
| Classification |
| Examination Or Test |
| Conformance Criteria |
| Requirement Paragraph |
| Inspection Method |
| Critical |
| None defined |
Major
| 101 |
| Weight of charge, min. |
| Level IV |
| 3.3 |
| AIE |
Minor
| 201 |
| Foreign matter in charge or on interior surface of container |
| Level II |
| 3.3 |
| Visual |
| Container, charge assembly |
| Drawing Number |
4.6.2.9
8861201
| Classification |
| Examination Or Test |
| Conformance Criteria |
| Requirement Paragraph |
| Inspection Method |
| Critical |
| None defined |
Major
| 101 |
| Closure assembly above flush |
| Level IV |
| 3.3 |
| Visual |
| 102 |
| Closure disc ruptured |
| Level IV |
| 3.3 |
| Visual |
Minor
| 201 |
| Closure assembly incompletely sealed (not 360 degrees) |
| Level II |
| 3.3 |
| Visual |
| 202 |
| Evidence of poor workmanship |
| Level II |
| 3.14 |
| Visual |
| Assembly, prior to inserting ignition element |
| Drawing Number |
4.6.2.10
8861197
| Classification |
| Examination Or Test |
| Conformance Criteria |
| Requirement Paragraph |
| Inspection Method |
| Critical |
| None defined |
| Major |
| None defined |
Minor
| 201 |
| Foreign matter on interior surface |
| Level II |
| 3.14 |
| Visual |
| Assembly, prior to assembling container charge assembly |
| Drawing Number |
4.6.2.11
8861197
| Classification |
| Examination Or Test |
| Conformance Criteria |
| Requirement Paragraph |
| Inspection Method |
| Critical |
| None defined |
Major
| 101 |
| Ignition element assembly inverted |
| Level IV |
| 3.3 |
| Visual |
| 102 |
| Lacquer missing between ignition element assembly and body |
| Level IV |
| 3.3 |
| See Note 1 |
| 103 |
| Depth of plunger, max |
| Level IV |
| 3.3 |
| AIE |
Minor
| 202 |
| Foreign matter on interior surface |
| Level II |
| 3.14 |
| Visual |
Note 1: One sample shall be randomly withdrawn from each ½ hour accumulated production prior to insertion of the container charge assembly. The ignition element assembly shall be unscrewed and extracted from the primer body for inspection. Failure to find evidence of lacquer on the ignition assembly seat or thread shall be cause for rejection of entire production run represented by the sample.
| Assembly |
| Drawing Number |
4.6.2.12
8861197
| Classification |
| Examination Or Test |
| Conformance Criteria |
| Requirement Paragraph |
| Inspection Method |
| Critical |
| Plunger above flush when it is touching ignition element |
| Level VII |
| 3.3 |
| AIE |
Major
| 101 |
| Body and container joint seal incomplete |
| Level IV |
| 3.3 |
| Visual |
| 102 |
| Container cup cracked or punctured |
| Level IV |
| 3.3 |
| Visual |
| 103 |
| Container charge assembly below flush max. |
| Level IV |
| 3.3 |
| AIE |
| 104 |
| Container charge assembly above flush |
| Level IV |
| 3.3 |
| Visual |
| 105 |
| Nonfunctioning |
| Level IV |
| 3.3 |
| AIE-4.7.1 |
| 106 |
| Functioning |
| Level IV |
| 3.3 |
| AIE-4.7.2 |
Minor
| 201 |
| Total length, max. |
| Level II |
| 3.3 |
| AIE |
| 202 |
| Coating missing from container assembly (rear surface) |
| Level II |
| 3.3 |
| Visual |
| 203 |
| Marking misleading or unidentifiable |
| Level II |
| 3.3 |
| Visual |
| 204 |
| Evidence of poor workmanship |
| Level II |
| 3.14 |
| Visual |
| Carton, packing, domestic |
| Drawing Number |
4.6.2.13
8796535
| Classification |
| Examination Or Test |
| Conformance Criteria |
| Requirement Paragraph |
| Inspection Method |
| Critical |
| None defined |
Major
| 101 |
| Strapping missing, broken or loose |
| Level IV |
| 3.3 |
| Visual-Manual |
| 102 |
| Board broken or split |
| Level IV |
| 3.3 |
| Visual |
| 103 |
| Contents exposed |
| Level IV |
| 3.3 |
| Visual |
Minor
| 201 |
| Strapping improperly assembled |
| Level II |
| 3.3 |
| Visual-Manual |
| 202 |
| Contents move when shaken |
| Level II |
| 3.3 |
| Manual |
| 203 |
| Marking misleading or unidentifiable |
| Level II |
| 3.3 |
| Visual |
| Carton, packing, overseas |
| Drawing Number |
4.6.2.14
8796678
| Classification |
| Examination Or Test |
| Conformance Criteria |
| Requirement Paragraph |
| Inspection Method |
| Critical |
| None defined |
Major
| 101 |
| Assembly damaged so that contents are exposed or liable to become exposed |
| Level IV |
| 3.3 |
| Visual |
| 102 |
| Sealing strip incomplete, badly wrinkled, or not in contact with surface of box for at least ½ inch around entire box |
| Level IV |
| 3.3 |
| Visual |
Minor
| 201 |
| Contents move when shaken |
| Level II |
| 3.3 |
| Manual |
| 202 |
| Label missing (when applicable) |
| Level II |
| 3.3 |
| Visual |
| 203 |
| Marking misleading or unidentifiable |
| Level II |
| 3.3 |
| Visual |
| Box, packing, overseas |
| Drawing Number |
4.6.2.15
8796679
| Classification |
| Examination Or Test |
| Conformance Criteria |
| Requirement Paragraph |
| Inspection Method |
| Critical |
| None defined |
Major
| 101 |
| Hardware or strapping missing, broken or loose |
| Level IV |
| 3.3 |
| Visual-Manual |
| 102 |
| Board broken or split |
| Level IV |
| 3.3 |
| Visual |
| 103 |
| Contents exposed |
| Level IV |
| 3.3 |
| Visual |
Minor
| 201 |
| Hardware or strapping improperly assembled |
| Level II |
| 3.3 |
| Visual-Manual |
| 202 |
| Car seal missing, unsealed or improperly positioned |
| Level II |
| 3.3 |
| Visual-Manual |
| 203 |
| Handle missing or insecure |
| Level II |
| 3.3 |
| Visual-Manual |
| 204 |
| Contents move when shaken |
| Level II |
| 3.3 |
| Manual |
| 205 |
| Marking misleading or unidentifiable |
| Level II |
| 3.3 |
| Visual |
| Foam Washer |
| Drawing Number |
4.6.2.16
WSHR001(Draft)
| Classification |
| Examination Or Test |
| Conformance Criteria |
| Requirement Paragraph |
| Inspection Method |
| Critical |
| None defined |
Major
| 101 |
| Thickness of washer |
| Level IV |
| 3.3 |
| AIE |
| 102 |
| Outside diameter |
| Level IV |
| 3.3 |
| AIE |
| 103 |
| Inside diameter |
| Level IV |
| 3.3 |
| AIE |
| 104 |
| Material Certification |
| Level IV |
| 3.3 |
| Visual |
| Minor |
| None defined |
Drawing Number
| 4.6.2.17 |
| Packing and marking for box, fiberboard (Sealed Envelope) |
DS000517(Draft)
Conformance
Requirement Next higher assembly DS000516(Draft)
| Classification |
| Examination Or Test |
| Criteria |
| Paragraph |
| Inspection method reference |
| Critical |
| None defined |
Major
| Waterproofness of bag destroyed by rip, tear, puncture, or separation of heat seal. |
| Level IV |
| 3.3 |
| Visual |
Minor Heat Seal Test
| Level IV |
| 3.3 |
| 4.7.16 |
| 201 |
| Barrier bag improperly marked, marking missing, or marking illegible |
| Level II |
| 3.3 |
| Visual |
| 202 |
| Evidence of poor workmanship |
| Level II |
| 3.10 |
| Visual |
Drawing number
| 4.6.2.18 |
| Packing and marking for box, fiberboard (Fiberboard Box) |
DS000517(Draft)
Next higher assembly DS000516(Draft)
| Classification |
| Examination or Test |
| Criteria |
| Paragraph |
| Inspection method reference |
| Critical |
| None defined |
Major
| Assembly damaged so that contents are exposed or liable to become exposed |
| Level IV |
| 5.1 |
| Visual |
| Sealing strip incomplete, badly wrinkled or not in contact with surface of box for at least ½ inch around body |
| Level IV |
| 5.1 |
| Visual |
| 103 |
| Incorrect number of primers |
| 100% |
| 5.1 |
| 4.4.13 |
Minor
| 201 |
| Contents move when shaken |
| Level II |
| 5.1 |
| Visual |
| 202 |
| Evidence of poor workmanship |
| Level II |
| 3.10 |
| Visual |
Packing and marking for box, metal, ammunition, M2A1 (prior to closing)
Drawing number
4.6.2.19
DS000516(Draft)
Next higher assembly DS000515(Draft)
| Classification |
| Examination or Test |
| Criteria |
| Paragraph |
| Inspection Method Reference |
| Critical |
| None defined |
Major
| 101 |
| Separator missing |
| Level IV |
| 5.1 |
| Visual |
| 102 |
| Interior Dimensions |
| Level IV |
| 5.1 |
| AIE |
Minor
| 201 |
| Evidence of poor workmanship |
| Level II |
| 3.10 |
| Visual |
Drawing number
| 4.6.2.20 |
| Packing and marking for box, metal, ammunition, M2A1 (closed) |
DS000516 (Draft)
Next higher assembly DS000515(Draft)
| Classification |
| Examination or Test |
| Criteria |
| Paragraph |
| Inspection method reference |
| Critical |
| None defined |
Major
| 101 |
| Hardware improperly engaged |
| Level IV |
| 5.1 |
| Visual |
| 102 |
| Box dented or deformed |
| Level IV |
| 5.1 |
| Visual |
| 103 |
| Marking incomplete, misleading or unidentifiable |
| Level IV |
| 5.1 |
| Visual |
| 104 |
| Contents loose when box is tilted |
| Level IV |
| 5.1 |
| Visual |
| 105 |
| Outside Dimensions (max) |
| Level IV |
| 5.1 |
| AIE |
Minor
| 201 |
| Bare spot on exterior |
| Level II |
| 5.1 |
| Visual |
| 202 |
| Metallic seal missing, unsealed or improperly positioned |
| Level II |
| 5.1 |
| Visual |
| 203 |
| Evidence of poor workmanship |
| Level II |
| 3.10 |
| Visual |
Drawing number
| 4.6.2.21 |
| Packing and marking for box, wirebound |
DS000515(Draft)
Next higher assembly
| Classification |
| Examination or Test |
| Criteria |
| Paragraph |
| Inspection method reference |
| Critical |
| None defined |
Major
DOT marking missing, incorrect, or illegible (when applicable) Contents loose when box is tilted
Level IV
Level IV
5.1
5.1
Wire missing, broken, or loose Wire improperly secured Level IV Level IV 5.1 5.1 Visual/Manual Visual
| 105 |
| Board broken or split |
| Level IV |
| 5.1 |
| Visual |
| 106 |
| Outside Dimensions |
| Level IV |
| 5.1 |
| AIE |
Minor
Marking (other than DOT) incomplete, misleading or unidentifiable Metallic seal missing, unsealed or improperly positioned Evidence of poor workmanship Level II
Level II Level II 5.1
5.1 3.10 Visual
Visual
NOTES:
Unitization Procedures For Boxed Ammunition and Components on 4-Way Entry Pallets
Drawing number
4.6.2.22
19-48-4116/158G
Next higher assembly
| Classification |
| Examination Or Test |
| Criteria |
| Paragraph |
| Inspection method reference |
| Critical |
| None defined |
Major
DOT marking missing, incorrect, or illegible (when applicable) Skids missing, broken or loose Strapping missing, loose, engaged improperly or mislocated Boards broken or split full length Number of containers incorrect
Level IV
Level IV Level IV Level IV Level IV
5.2
5.2 5.2 5.2 5.2
Visual
Visual Visual Visual
Minor
Skids partially split Boards partially split Marking (other than DOT) incomplete, misleading or unidentifiable Evidence of poor workmanship Level II Level II Level II
Level II 5.2 5.2 5.2
3.10 Visual Visual Visual
NOTES:
| Cup, Container |
| Drawing Number |
4.6.2.23
8861205
| Classification |
| Examination Or Test |
| Conformance Criteria |
| Requirement Paragraph |
| Inspection Method |
| Critical |
| None defined |
Major
| 101 |
| Overall diameter |
| Level IV |
| 3.3 |
| AIE |
| 102 |
| Inside radius |
| Level IV |
| 3.3 |
| AIE |
| 103 |
| Front thickness |
| Level IV |
| 3.3 |
| AIE |
| 104 |
| Sidewall minimum thickness |
| Level IV |
| 3.3 |
| AIE |
| 104 |
| Outside length |
| Level IV |
| 3.3 |
| AIE |
| 105 |
| Position of grooves |
| Level IV |
| 3.3 |
| AIE |
| 106 |
| Depth of groove |
| Level IV |
| 3.3 |
| AIE |
| 107 |
| Width of groove |
| Level IV |
| 3.3 |
| AIE |
| 108 |
| Material Certification |
| Level IV |
| 3.3 |
| AIE |
| 109 |
| Depth of vee-groove must extend over entire length of groove |
| Level IV |
| 3.3 |
| Visual |
| 110 |
| The maximum width of the flat at the bottom of the vee-groove is not to exceed .005 |
| Level IV |
| 3.3 |
| Visual |
| Minor |
| None defined |
4.7 Testing.
4.7.1 Nonfunctioning
4.7.1.1 A steel ball approximately 1-19/32 inches in diameter and weighing 16.34 plus or minus
0.02 ounces shall be dropped on the firing pin from a height of 1 ½ inches minimum. The drop height shall be measured as the distance between the bottom of the ball and the top of the firing Pin. Any primer assembly that fires shall be classified as defective.
4.7.1.2 Beginning with the first lot produced and continuing until three consecutive lots have complied with the acceptance criteria specified, a sample of 150 head assemblies shall be randomly selected from each lot for the test. The head assembly includes the plunger, body, and ignition element assembly without the container charge assembly (see Dwg. 8861197). If any sample fails to comply with the requirements the lot shall be rejected. The test shall be performed as specified in 4.7.1.1.
4.7.1.3 After three consecutive lots have met the criteria of 4.7.1.2, a sample of 50 head assemblies shall be randomly selected from each lot for this test. If one or more primers fails to comply with the applicable requirement, the lot shall be rejected. The test shall be performed as specified in 4.7.1.1. Primers subject to this test shall be destroyed.
4.7.2 Functioning
4.7.2.1 Without black powder charge
| 4.7.2.1.1 Beginning with the first lot produced and continuing until three consecutive lots |
| have complied with the acceptance criteria specified, three hundred primers shall be |
| selected from each lot for this test. If five or more primers fail to comply with the |
| specified requirements the lot shall be rejected. If two, but less than five, defectives are |
| found a second sample of 600 primers shall be tested. If the combined number of |
| deficiencies in both the first and second sample is 5 or more the lot shall be rejected. The |
| test shall be performed as specified in 4.7.3. |
| 4.7.2.1.2 After three consecutive lots have met the criteria of 4.7.2.1.1, one hundred and |
| twenty-five primers shall be selected from each subsequent production lot for this test. If |
| 2 or more primers fail to comply with the specified requirement the lot shall be rejected. If |
| only one defective is found, a second sample of 250 primers shall be tested. If the |
| combined number of defective in both the first and second sample is 2 or more, the lot |
| shall be rejected. The test shall be performed as specified in 4.7.3. |
4.7.2.2 With black powder charge.
4.7.2.2.1 This test is required for ballistic first article only and shall be performed as specified in 4.7.4.
4.7.3 Static Test. The primer assembly less the black powder charge shall be tested as specified
| 4.7.1.1 except that the drop height shall be increased to 9 inches maximum. Any primer assembly |
| that fails to fire shall be classed defective. |
| 4.7.4 First Article Ballistic Test. The primers shall be assembled with a projectile and propelling charge |
| system at a Government proving ground, and fired from a gun for which the primer is standard. |
| 4.7.5 Modified Bruceton sensitivity test. Approximately two hundred (200) No. 34 primers |
| shall be loaded into M82 primers without container charge assembly and tested as follows and |
| the test result shall be submitted to the Technical Agency (see 6.11) for evaluation prior to loading |
| of M82 primers: |
| 4.7.5.1 50% point phase. |
| 1. Set height to 5 inches and drop a steel ball with approximately 1 19/32 inches in |
| diameter and weighing 16.34 plus or minus 0.02 ounces on a primer. |
| 2. If primer fires, record result and lower height by ½ inch. |
| 3. If primer does not fire, record result and raise height by ½ inch. |
| 4. Repeat steps 2 and 3 until 8 reversals in direction of height adjustment between |
| drops are performed. A reversal occurs whenever the height is adjusted in a |
| direction opposite that of the previous adjustment. |
| 4.7.5.2 No-fire phase. | |
| 1. Set height to ½ inch below the lowest fire which occurred during the 50% point | |
| phase. | |
| 2. If 5 consecutive primers do not fire, record results and raise height by ½ inch. | |
| 3. If any primer fires prior to the 5th consecutive no-fire at the set height, record | |
| the results and lower the height by ½ inch. | |
| 4. Repeat steps 2 and 3 until 5 reversals in direction of height adjustment are | |
| performed. |
| 4.7.5.3 All-fire phase. | |
| 1. Set height to ½ inch above the highest no-fire which occurred during the 50% | |
| point phase. | |
| 2. If 5 consecutive primers fire, record results and lower height by ½ inch. | |
| 3. If any primer no-fires prior to the 5th consecutive fire at the set height, record | |
| the results and raise the height by ½ inch. | |
| 4. Repeat steps 2 and 3 until 5 reversals in direction of height adjustment are | |
| performed. |
4.7.6 Moisture content of black powder. The moisture content of the black powder shall be determined in accordance with the procedure specified in Specification MIL-P-223. A sample of one container charge assembly, prior to assembly to the primer body shall be randomly selected from each eight hours production. The black powder shall be randomly selected from each eight hours production. Any failure to comply with the applicable requirement shall be cause for rejection of eight hours production represented by the sample.
| 4.7.7 Grade of powder (see dwg. 8861201). The contractor shall select approximately 100 grams of black | |
| powder from each container for this test. If any sample fails to comply with granulation requirement, the | |
| container form which it was taken shall not be used in the loading of the primers. The grade of black | |
| powder shall be determined as specified in Specification MIL-P-223. |
| 4.7.8 Check test for deterioration (not applicable to new production). This test is intended to prevent the | |
| loading of major ammunition items with primers that have deteriorated. The tests shall be performed on | |
| primers from each lot which has been stored under normal conditions for more than two years, or under | |
| adverse conditions for any period of time. If the specification for the ammunition item | |
| into which the primers are loaded does not require performance of the check test, the contracting officer | |
| should insert a check test requirement in the contract. |
| 4.7.9 Mercurous nitrate test. (see 3.6) 25 bodies shall be randomly selected for this test. If any sample | |
| fails to comply with the requirement the lot shall be rejected. The primer shall be tested in accordance | |
| with ASTM B154. Each body shall be examined for cracks. |
| 4.7.10 Rupture Test (see dwg. 8861204). 110 container assemblies shall be randomly selected for this test, | |
| if any sample fails to comply with the requirement the lot shall be rejected. |
| 4.7.11 Air Pressure Test (see dwg. 8861204). 150 container assemblies shall be randomly selected for this | |
| test. If two or more samples fail to comply with the requirement the lot shall be rejected. |
| 4.7.12 Freedom from alkalies and strong acids. 3 sample containers from each four hours production | |
| shall be selected for this test. The container assemblies shall be tested in accordance with Specifications | |
| TT-C-490. If the limits specified herein have not been complied with, inspection for acceptance shall be | |
| stopped until corrective action has been taken. After corrective action, sampling shall be resumed as | |
| normal. |
| 4.7.13 Freedom from oil and grease. 3 sample containers from each four hours production shall be | |
| selected for this test. The container assemblies shall be tested and action taken in accordance with | |
| specification TT-C-490. |
| 4.7.14 Rockwell Hardness test (see dwg. 8861198). Ten bodies shall be randomly selected for this test; | |
| if any sample fails to comply with the requirement the lot shall be rejected. The primer bodies shall be | |
| tested in accordance with ASTM E18. |
| 4.7.15 Grain size test (see dwg. 8861198). Ten bodies shall be randomly selected for this test; if any | |
| sample fails to comply with the requirement the lot shall be rejected. Primer bodies used in this test shall | |
| not be returned to the lot. The primer bodies shall be tested in accordance with ASTM E112. |
4.7.16 Heat Seal Test- The seals shall comply with the test specified in MIL-STD-2073, paragraph G.4.3.
| 4.7.17 Correct number of primers- The number of primers in each pack shall be verified 100%. This may |
| be accomplished by any applicable approved method, such as visual inspection, weight, or x-ray. |
5. PACKAGING
5.1 Packaging. The primers shall be packed and marked in accordance with drawing DS000515, DS000516 and DS000517.
5.2 Unitization. Boxes shall be unitized in accordance with drawing 19-48-4116/158G.
6. NOTES
(This section contains information of a general or explanatory nature that may be helpful, but is not mandatory.)
6.1 Intended use. The components and assemblies covered by this specification are intended for use on all M82 series percussion primers.
6.2 Acquisition requirements. Acquisition documents must specify the following:
a. Title, number and date of this specification.
b. Packaging requirements (see 5 and 6.3).
c. Requirements for submission of first article sample.
d. Requirement for submission of acceptance inspection equipment.
e. Check Test for possible deterioration of M82 Primer.
f. Primer Qualification.
6.3 Packaging drawings. Drawings listed in this section are for reference only. The government's current packaging for the M82 Percussion Primers as defined by Technical Data Package (TDP) 8796535 and 8796679, is included for reference. The contractor may use the information contained in the TDP as guidance for its own design. If the contractor chooses to build to the current approved TDP (8796535 and 8796679) the Government will waive the testing required to meet the First Article performance test requirements of the packaging specification, except for Performance Oriented Packaging (POP) testing which is still required to transport hazardous materials in accordance with Code of Federal Regulations (CFR), Title 49. Unless otherwise noted, the custodian of the following drawings is the U.S. Army Armament Research, Development and Engineering Center, Picatinny Arsenal, NJ 07806-5000;
a. 8796535 Box, Packing, Ammunition, for Primers, Percussion-Electric M75 or Percussion M82.
b. 8796679 Box, Set-up, Packing, Ammunition, for Primers, Percussion-Electric M75 or Percussion M82.
6.4 Visual standards. Visual standards for evaluation of defects will be established for each contract after the first month’s production. However, establishment of visual standards will not waive the requirements for compliance with the requirements of the applicable drawing.
6.5 Check test for possible deterioration of M82 series artillery primers. The following tests are designed to prevent the loading of deteriorated artillery primers into a major ammunition item. The test should be performed on artillery primers from each lot which has been stored under normal conditions for more than three years or under adverse conditions for any period of time. If the specification for the ammunition item into which the artillery primers are loaded does not require that a check test be performed, the contracting officer should insert a provision for the performance of the check tests in the contract.
6.6 Nonfunctioning. The Sampling plan for the non-functioning test shall be in accordance with table III. Any primer which fails to comply with the applicable requirement shall be classified as defective. The test shall be performed as specified in 4.7.1.
Table IV. Nonfunctioning Test Samples
| Sample |
| Sample size |
| Combined |
| Acceptance |
| Rejection |
| Sample Size |
| Number |
| Number |
| First |
| 20 |
| 20 |
| * |
| 2 |
| Second |
| 20 |
| 40 |
| * |
| 2 |
| Third |
| 20 |
| 60 |
| 0 |
| 2 |
| Fourth |
| 20 |
| 80 |
| 1 |
| 3 |
| Fifth |
| 20 |
| 100 |
| 1 |
| 3 |
| Sixth |
| 20 |
| 120 |
| 1 |
| 3 |
| Seventh |
| 20 |
| 140 |
| 2 |
| 3 |
*No acceptance on first or second sample.
6.7 Functioning. The sampling plan for this test shall be in accordance with table IV. Any primer which fails to comply with the applicable requirements shall be classed as defective. The test shall be performed as specified in 4.7.2.
Table V. Functioning Test Samples
| Sample |
| Sample size |
| Combined |
| Acceptance |
| Rejection |
| Sample Size |
| Number |
| Number |
| First |
| 75 |
| 75 |
| * |
| 2 |
| Second |
| 75 |
| 150 |
| * |
| 3 |
| Third |
| 75 |
| 225 |
| 0 |
| 3 |
| Fourth |
| 75 |
| 300 |
| 1 |
| 4 |
| Fifth |
| 75 |
| 375 |
| 2 |
| 5 |
| Sixth |
| 75 |
| 450 |
| 2 |
| 5 |
| Seventh |
| 75 |
| 525 |
| 4 |
| 5 |
*No acceptance on first or second sample
6.8 Moisture content of black powder. A sample of 25 primers shall be selected for this test. The black powder shall be removed from the flash tube by any suitable means. The moisture content of the powder should
| be determined in accordance with the method specified in Specification MIL-P-223. If the moisture content of |
| any of the powder tested exceeds 0.7 percent, the lot of primers should be rejected. Since black powder is |
| hygroscopic, it is advisable to place the powder in a dry, airtight container immediately upon removal, and to |
| run the determination as soon as possible thereafter. |
| 6.9 Cost of check test. The contracting officer will arrange for the contractor to be reimbursed for the expense | |
| incurred in the performance of the check test. |
| 6.10 Metal parts separation. Missing metal from the lip area (mouth of the primer) is considered a “burned | |
| through” area and not metal parts separation provided that such an area is not greater than 1/4 –inch wide at the | |
| lip and does not extend more than 1/4 –inch back from the lip. |
| 6.11 Modified Bruceton sensitivity test. All the modified Bruceton sensitivity test results shall be submitted to | |
| Commander, ARDEC, ATTN: AMSTA-AR-QAT-P, Picatinny Arsenal, NJ 07806-5000 for evaluation prior to | |
| loading of M82 primers using a new lot of No. 34 primers. In order to expedite the evaluation of the new lot of | |
| No. 34 primers. In order to expedite the evaluation of the new lot of No. 34 primers, the test data should be | |
| Datafaxed to AMSTA-AR-QAT-P. |
| 6.12 Lot formation. Allowance for two black powder lots is for the purpose to facilitate LAP when a black | |
| powder lot is depleted and a new lot is introduced. |
6.13 Critical classification notes.
| 6.13.1 Total length (over primer) max. If the total length over primer exceeds the allowable maximum |
| value, it will cause improper functioning of the primer. This is likely to cause injury or death to troops |
| firing the howitzer. |
| 6.13.2 Plunger above flush when it is touching ignition element. If the plunger is above the flush, it will |
| cause unintended initiation of the primer which can cause injury or death to troops firing the howitzer. |
| 6.14 Acceptance Inspection Equipment (AIE). Any measuring device that is traceable to the national or | |
| international standard used to assure conformance of material to the contract requirements. |
6.15 Subject term (key word) listing.
| Artillery | |
| Cartridge | |
| Check Test |
| Custodian | Preparing activity | |||
| Army-AR | Army-AR | |||
| (Project#) |
NOTE: The activities listed above were interested in this document as of the date of this document. Since organizations and responsibilities can change, you should verify the currency of the information above using the ASSIST Online database at https://assist.dla.mil.
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