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
Issued by
Department of the Army Materiel Command Joint Munitions Command

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Attachment 0016 M82E3 Percussion Primer Draft Spec (Foam Washer) Final Draft 2017 06 20

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Attachment_0012_DS000848_-_COAI_M82-FW.PDF PDF
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Attachment_0006_Address_Code_Distribution_for_ECP__RFV__RFD__VECP.pdf PDF
Attachment_0003_Government_Point_of_Contact_List.pdf PDF
Attachment_0015_DS000516_FW_P&M_Metal.pdf PDF
Exhibit_A_Contract_Data_Requirements_List.pdf PDF
Attachment_0018_WSHR001_draft.pdf PDF
Attachment_0009_Non_Disclosure_Agreement_(NDA).pdf PDF
Attachment_0007_ACQUISITION_OPSEC_PLAN.pdf PDF
Attachment_0011_DS000515_FW_P&M_Wirebound.pdf PDF
Attachment_0019_DS000517_FW_P&M_Fiber.pdf PDF
Attachment_0014_MIL-DTL-46610_Revision_F.pdf PDF
Attachment_0010_8861211-FW_Draft.pdf PDF
Attachment_0005_PPI_ADDRESS_2015.pdf PDF
W52P1J17R0007.pdf PDF
Attachment_0008_Instructions_for_Completing_DD_Form_1423.pdf PDF
Attachment_0017_8861200E.PDF PDF
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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
CustodianPreparing activity
Army-ARArmy-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.

File details come from the government source that posted it. Updated .