1.03_TDP_N0010423NB060.pdf

NAVAL SURFACE WARFARE CENTER

INDIAN HEAD EOD TECHNOLOGY DIV

INDIAN HEAD, MD 20640 (CAGE CODE 14083)

APPROVED BY: BARRETT.KIMBERLY.S.1229428043 APPROVAL DATE: 11/9/2020

DATA LIST: DL520-174-0355 DL REV: - ECP: N/A

NOMENCLATURE: DETONATING CORD ASSEMBLY TOP ASS'Y DWG: 520-174-0355

DODIC: MULTIPLE

CAGE DOCUMENT

NUMBER

REVISION DOCUMENT

DATE

NO.

PGs

DOCUMENT TITLE DOC

SYM

R SC ECP

TOP ASSEMBLY (Total: 1)

14083 520-174-0355 - 8/3/2020 1 DETONATING CORD ASSEMBLY S U U

PRODUCT SPECIFICATIONS (Total: 1)

30003 DTL-WS-36035 - 11/2/2020 13 DETONATING CORD ASSEMBLY (DCA) U

*GOVERNMENT INSPECTION EQUIPMENT DRAWINGS (Total: 5)

30003 841AS150 - 12/23/1976 1 BOSS, SHIELDED MILD DETONATING CORD (SMDC) PORT CONFIGURATION E U U

30003 841AS801 A 1/7/2020 1 FITTING SENSITIVITY TEST E U U

30003 841AS802 - 12/28/1976 1 CONNECTOR, TEE E U U

30003 841AS803 A 8/29/1989 1 DENT BLOCK E U U

30003 841AS804 - 12/23/1976 1 HOLDER, SMDC DENT BLOCK E U U

*WEAPONS REQUIREMENTS (Total: 1)

10001 WR-43 A 6/14/1965 19 PREPARATION OF QUALITY ASSURANCE PROVISIONS (INCLUDING

CLASSIFICATION OF CHARACTERISTICS)

U

*WEAPON SPECIFICATION (Total: 1)

10001 WS5003 HNS EXPLOSIVE U

*MILITARY STANDARDS (BOOK FORM) (Total: 6)

96906 DOD-STD-2101 CLASSIFICATION OF CHARACTERISTICS U

96906 MIL-STD-100 STANDARD PRACTICE FOR ENGINEERING DRAWINGS U

96906 MIL-STD-105 SAMPLING PROCEDURES AND TABLES FOR INSPECTION BY ATTRIBUTES U

96906 MIL-STD-1168 AMMUNITION LOT NUMBERING AND AMMUNITION DATA CARD U

96906 MIL-STD-130 IDENTIFICATION MARKING OF U.S. MILITARY PROPERTY U

Page 1 of 3 DL520-174-0355 11/9/2020 12:40:31 PM

96906 MIL-STD-810 ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY

TESTS

U

*MILITARY SPECIFICATIONS (Total: 5)

81349 MIL-C-83125 CARTRIDGES FOR CARTRIDGE ACTUATED/PROPELLANT ACTUATED

DEVICES, GENERAL DESIGN SPECIFICATION FOR

U

81349 MIL-I-8500 INTERCHANGEABILITY AND REPLACEABILITY OF COMPONENT PARTS FOR

AEROSPACE VEHICLES

U

81349 MIL-L-14758 LEAD AZIDE (SPECIAL PURPOSE) (FOR USE IN AMMUNITION) U

81349 MIL-PRF-46010 LUBRICANT, SOLID FILM, HEAT CURED, CORROSION INHIBITING U

81349 MIL-S-7742 SCREW THREADS, STANDARD, OPTIMUM SELECTED SERIES: GENERAL

SPECIFICATION FOR

U

*FEDERAL SPECIFICATIONS (Total: 1)

81348 QQ-A-225/8 ALUMINUM ALLOY 6061, BAR, ROD, WIRE AND SPECIAL SHAPES; ROLLED,

DRAWN OR COLD FINISHED

U

*AMERICAN NATIONAL STANDARDS INSTITUTE (Total: 1)

80204 ANSI/ASQ-Z1.4 SAMPLING PROCEDURES AND TABLES FOR INSPECTION BY ATTRIBUTES U

*AMERICAN SOCIETY FOR TESTING AND MATERIALS (Total: 5)

81346 ASTM-B117 OPERATING SALT SPRAY (FOG) APPARATUS U

81346 ASTM-D1141 PREPARATION OF SUBSTITUTE OCEAN WATER U

81346 ASTM-

E1742/E1742M

STANDARD PRACTICE FOR RADIOGRAPHIC EXAMINATION U

81346 ASTM-E18 ROCKWELL HARDNESS AND ROCKWELL SUPERFICIAL HARDNESS OF

METALLIC MATERIALS

U

81346 ASTM-E748 THERMAL NEUTRON RADIOGRAPHY OF MATERIALS U

*AMERICAN SOCIETY OF MECHANICAL ENGINEERS (Total: 3)

05047 ASME-Y14.100 -17 11/14/2017 67 ENGINEERING DRAWING PRACTICES U

05047 ASME-Y14.5 -18 2/11/2019 347 DIMENSIONING AND TOLERANCING U

05047 ASME-Y14.5 -09 3/27/2009 227 DIMENSIONING AND TOLERANCING U

*SOCIETY OF AUTOMOTIVE ENGINEERS (Total: 1)

81343 SAE-AMS4117 ALUMINUM ALLOY, ROLLED OR COLD FINISHED BARS, RODS, AND WIRE

AND FLASH WELDED RINGS 1.0MG - 0.60SI - 0.28CU - 0.20CR (6061; -T6, -T651)

SOLUTION AND PRECIPITATION HEAT TREATED - UNS A96061

U

TOTAL DOCUMENTS: 31

Page 2 of 3 DL520-174-0355 11/9/2020 12:40:31 PM

CAGE DOCUMENT REVISION DOCUMENT NO. DOCUMENT TITLE DOC R SC ECP

NUMBER DATE PGs SYM____________________________________________________________________________________________________________________________________________________________________________________________

-------------------------Symbols in DOC SYM Column ------------------------ --------------------------Symbols in R Column ------------------------------

A = ALTERED ITEM S = SOURCE CONTROL L = LIMITED RIGHTS U = UNLIMITED

C = SPEC CONTROL V = VENDOR ITEM GP = GOVT PURPOSE RESTRICTED

E = GAGE & TEST EQPT

F = INTERFACE CONTROL ------------------------- Symbols in SC Column -------------------------

I = PRODUCTION TOOLING C = CLASSIFIED U = UNCLASSIFIED

# INDICATES DATA NOT AVAILABLE

* INDICATES DOCUMENTS NOT SUPPLIED WITH TECHNICAL DATA PACKAGE AND MAY BE OBTAINED THRU THE AGENCY

REF INDICATES DRAWINGS NOT REQUIRED TO DEFINE, PROCURE OR INSPECT THE END ITEM

Page 3 of 3 DL520-174-0355 11/9/2020 12:40:31 PM

CAGE DOCUMENT REVISION DOCUMENT NO. DOCUMENT TITLE DOC R SC ECP

NUMBER DATE PGs SYM____________________________________________________________________________________________________________________________________________________________________________________________

345678

D

C

B

A

D

C

B

A

L

ALL CHARACTERISTICSMINOR:

NONEMAJOR:

NONECRITICAL:

CLASSIFICATION OF

CHARACTERISTICS (DOD-STD-2101)

REVISION HISTORY

APPROVEDDATEDESCRIPTIONREV

APPLICATION

USED ONNEXT ASSY

AH-64D/E UEES 7-311112017

AH-64/E7-311112017

DO NOT SCALE DRAWING

MATERIAL:

ANGLES �#� �!�

XXX DECIMALS �#� �!�

XX DECIMALS �#� �!�

GENERAL TOLERANCES

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES

DATE

2020/08/03

APPROVED FOR NSWC

DRAWN

CHECKED

ENGINEER

ENGINEER

NAVAL SURFACE WARFARE CENTER

INDIAN HEAD EOD TECHNOLOGY DIVISION

INDIAN HEAD, MD 20640

SHEET 1 OF 1SCALE: .300

520-174-035514083D

DRAWING NUMBERDAISIZE

DETONATING CORD

ASSEMBLY

DEPARTMENT OF THE NAVY

NAVAL SURFACE WARFARE CENTER

INDIAN HEAD, MD 20640-5035

CURRENT DESIGN ACTIVITY CAGE CODE 30003

DEPARTMENT OF THE NAVY

NAVAL AIR SYSTEMS COMMAND

PATUXENT RIVER, MARYLAND 20670

CURRENT DESIGN ACTIVITY CAGE CODE 53711

DEPARTMENT OF THE NAVY

NAVAL SEA SYSTEMS COMMAND

WASHINGTON, D.C. 20362

CURRENT DESIGN ACTIVITY CAGE CODE 14083

DEPARTMENT OF THE NAVY

NAVAL SURFACE WARFARE CENTER

INDIAN HEAD EOD TECHNOLOGY DIVISION

INDIAN HEAD, MARYLAND 20640

APPROVED SOURCE(S) OF SUPPLY

APPLICATION

VENDOR

NAME AND ADDRESS CAGE CODE PART NUMBER

AH-64D/E

AH-64D/E WITH UEES

COLLINS AEROSPACE

3530 BRANSCOMBE ROAD

FAIRFIELD, CA 94533

17610 51960-

TABULATION TABLE

DASH DODIC

VENDOR

P/N

LENGTH "L"

(INCH)

END TIP

"A"

END TIP

"B"

INERT

-1 SP02 51960-1 55.5 3/8-24UNF-3A 3/8-24UNF-3A

-2 NA 51960-2 55.5 3/8-24UNF-3A 3/8-24UNF-3A INERT

-3 NA 51960-3 60.5 3/8-24UNF-3A 3/8-24UNF-3A INERT

-4 SP03 51960-4 60.5 3/8-24UNF-3A 3/8-24UNF-3A

-5 JP01 51960-5 34.5 3/8-24UNF-3A 7/16-20UNF-3A

-6 JP04 51960-6 21.0 1/2-20UNF-3A 3/8-24UNF-3A

-7 JP02 51960-7 42.5 3/8-24UNF-3A 7/16-20UNF-3A

-8 JP03 51960-8 31.5 1/2-20UNF-3A 3/8-24UNF-3A

-9 NA 51960-9 34.5 3/8-24UNF-3A 7/16-20UNF-3A INERT

-10 NA 51960-10 21.0 1/2-20UNF-3A 3/8-24UNF-3A INERT

-11 NA 51960-11 42.5 3/8-24UNF-3A 7/16-20UNF-3A INERT

-12 NA 51960-12 31.5 1/2-20UNF-3A 3/8-24UNF-3A INERT

NOTES:

1. INTERPRET DRAWING IN ACCORDANCE WITH ASME Y14.5-2018 AND

ASME Y14.100-2017 WITH APPENDICES B, C, D, AND E.

2. FOR REQUIREMENTS SEE WS-DTL-36035

3. PERMANENTLY MARK IN ACCORDANCE WITH MIL-STD-130 THE FOLLOWING

INFORMATION:

NSN AND DODIC

DETONATING CORD ASSEMBLY

14083 520-174-0355-X

MANUFACTURER'S CAGE CODE

SERIAL NUMBER

LOT NUMBER PER MIL-STD-1168

4. ONLY ITEMS DESCRIBED ON THIS DRAWING ARE APPROVED FOR USE IN

THE APPLICATIONS SPECIFIED HEREON. A SUBSTITUTE SHALL NOT BE

USED WITHOUT PRIOR APPROVAL BY THE QUALIFYING ACTIVITY.

5. IDENTIFICATION OF THE APPROVED SOURCES OF SUPPLY HEREON IS

NOT TO BE CONSTRUED AS A GUARANTEE OF PRESENT OR CONTINUED

AVAILABILITY AS A SOURCE OF SUPPLY FOR THE ITEM DESCRIBED ON

THE DRAWING.

CAD MAINTAINED, CHANGES SHALL BE

INCORPORATED BY THE DESIGN ACTIVITY

MUST INCLUDE A CURRENT DESIGN ACTIVITY CODE IF

THE DA/CAGE CODE IS NOT ON F OF THE FOLLOWING:

14092 30003 53711 14083

DISTRIBUTION STATEMENT D. DISTRIBUTION AUTHORIZED TO DOD AND DOD CONTRACTORS

ONLY; ADMINISTRATIVE OR OPERATIONAL USE; YYYY-MM-DD. OTHER REQUESTS SHALL BE

REFERRED TO NSWC IHEODTD, INDIAN HEAD, MD 20640. DESTRUCTION NOTICE: DESTROY BY ANY METHOD

THAT WILL PREVENT DISCLOSURE OF CONSTRAINTS

OR RECONSTRUCTION OF THE DOCUMENT.

DISTRIBUTION STATEMENT C: DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT

AGENCIES AND THEIR CONTRACTORS (ADMINISTRATIVE OR OPERATIONAL USE)

(2019/07/30). OTHER REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO

COMMANDER OR TECHNICAL DIRECTOR, NAVAL SURFACE WARFARE CENTER, INDIAN

HEAD EXPLOSIVE ORDNANCE DISPOSAL TECHNOLOGY DIVISION.

PHANTOM PROTECTIVE CAPS

SOURCE CONTROL DRAWING

TIP "A"

TIP "B"

D

C

B

A

D

C

B

A

.485

C

.100 +.005 -.000

HEX STK

.75

1.20

.335

.050

O.D.

OF MATING PART

.5640 +.0000 -.0005

.38

.400

.400

ALL CHARACTERISTICSMINOR:

NONEMAJOR:

NONECRITICAL:

CLASSIFICATION OF

CHARACTERISTICS (DOD-STD-2101)

REVISION HISTORY

APPROVEDDATEDESCRIPTIONREV

2020/07/01 REDRAWN WITH CHANGE SEE ECP18-0303R1A

APPLICATION

USED ONNEXT ASSY

DL841AS800841AS800

DL841AS806841AS806

DL841AS807841AS807

DO NOT SCALE DRAWING

MATERIAL:

ANGLES �#� 5.0

XXX DECIMALS �#� .005

XX DECIMALS �#� .01

GENERAL TOLERANCES

UNLESS OTHERWISE SPECIFIED

DIMENSIONS ARE IN INCHES

DATEAPPROVED FOR NAVAIR

DRAWN

CHECKED

ENGINEER

ENGINEER

NAVAL ORDNANCE STATION

INDIAN HEAD, MD 20640

SHEET 1 OF 1SCALE: 4.000

841AS80130003D

DRAWING NUMBERDAISIZE

FITTING

SENSITIVITY TEST

DEPARTMENT OF THE NAVY

NAVAL AIR SYSTEMS COMMAND

WASHINGTON, D.C. 20361

CURRENT DESIGN ACTIVITY CAGE CODE 30003

DEPARTMENT OF THE NAVY

NAVAL AIR SYSTEMS COMMAND

PATUXENT RIVER, MARYLAND 20670

CURRENT DESIGN ACTIVITY CAGE CODE 53711

DEPARTMENT OF THE NAVY

NAVAL SEA SYSTEMS COMMAND

WASHINGTON, D.C. 20362

CURRENT DESIGN ACTIVITY CAGE CODE 14083

DEPARTMENT OF THE NAVY

NAVAL SURFACE WARFARE CENTER

INDIAN HEAD EOD TECHNOLOGY DIVISION

INDIAN HEAD, MARYLAND 20640

DASH NO. A

PORT DETAIL DRAWING

B

PORT DETAIL DRAWING

C

DIMENSION

-1 30003-841AS150-1 30003-841AS150-1 .958

-2 30003-841AS150-1 30003-841AS150-2 .958

-3 30003-841AS150-1 30003-841AS150-3 .958

-4 30003-841AS150-2 30003-841AS150-1 1.017

-5 30003-841AS150-2 30003-841AS150-2 1.017

-6 30003-841AS150-2 30003-841AS150-3 1.017

-7 30003-841AS150-3 30003-841AS150-1 1.017

-8 30003-841AS150-3 30003-841AS150-2 1.017

-9 30003-841AS150-3 30003-841AS150-3 1.017

NOTES:

1. INTERPRET DRAWING IN ACCORDANCE WITH ASME Y 14.5-2009

AND ASME Y14.100-2017 WITH APPENDICES B THRU E.

2. UNLESS OTHERWISE SPECIFIED:

REMOVE ALL BURNS AND BREAK SHARP EDGES .02 FILLET R.01 MAX.

3. SENSITIVITY TEST FITTINGS, PART NUMBERS 80017-1 THRU-9,

MANUFACTURED BY UNITED PROPULSION COMPANY, UPCO,

FAIRFIELD, CALIFORNIA, CODE IDENT NO. 17610 ARE APPROVED

SUBSTITUTES FOR THE PARTS DEPICTED HEREON. MANUFACTURER'S

PART DASH NUMBERS CORRESPOND TO THE DASH NUMBERS DEPICTED

ON THIS DRAWING.

4. THE FOLLOWING ITEM IDENTIFICATION MARKINGS SHALL BE APPLIED

TO EACH PART, EITHER BY IMPRESSION STAMPING, ETCHING, OR AN

ADHESIVE BACKED DECAL: NAVAIR DRAWING NUMBER AND DASH NUMBER,

LOT NUMBER- MFR'S SYMBOL- MONTH AND YEAR OF MANUFACTURE,

AN ARROW INDICATING DIRECTION OF FLOW (FROM PORT A TO PORT B).

5. MATERIAL: ALUMINUM ALLOY 6061-T6, SAE-AMS4117

CAD MAINTAINED, CHANGES SHALL BE

INCORPORATED BY THE DESIGN ACTIVITY

DISTRIBUTION STATEMENT C:

DISTRIBUTION AUTHORIZED TO U.S. GOVERNMENT AGENCIES AND THEIR

CONTRACTORS (ADMINISTRATIVE OR OPERATIONAL USE) (2019/07/30). OTHER

REQUESTS FOR THIS DOCUMENT SHALL BE REFERRED TO NSWC IHEODTD CODE E26.

WARNING - THIS DOCUMENT CONTAINS TECHNICAL DATA WHOSE EXPORT IS RESTRICTED BY

THE ARMS EXPORT CONTROL ACT (TITLE 22, U.S.C., SEC 2751, ET SEQ.) OR THE EXPORT

ADMINISTRATION ACT OF 1979 (TITLE 50, U.S.C., APP. 2401 ET SEQ.), AS AMENDED.

VIOLATIONS OF THESE EXPORT LAWS ARE SUBJECT TO SEVERE CRIMINAL PENALTIES.

DISSEMINATE IN ACCORDANCE WITH PROVISIONS OF DOD DIRECTIVE 5230.25.

MUST INCLUDE A CURRENT DESIGN ACTIVITY CODE IF

THE DA/CAGE CODE IS NOT ON F OF THE FOLLOWING:

14092 30003 53711 14083

DISTRIBUTION STATEMENT D. DISTRIBUTION AUTHORIZED TO DOD AND DOD CONTRACTORS

ONLY; ADMINISTRATIVE OR OPERATIONAL USE; YYYY-MM-DD. OTHER REQUESTS SHALL BE

REFERRED TO NSWC IHEODTD, INDIAN HEAD, MD 20640.

+.0005 -.0000

A

B

.03X45�$�

AU

TH

EN

TI

CA

TE

D

/2 3/

AMSC N/A FSC 1377

DTL-WS-36035 (OS)

CAGE Code 30003

DETAIL SPECIFICATION

FOR THE AH-64 HELICOPTER

DETONATING CORD ASSEMBLY (DCA)

Prepared for:

Program Manager Apache Attack Helicopter

Redstone Arsenal Huntsville, AL 35898

Prepared by:

Naval Surface Warfare Center Indian Head Division

(NSWC IHD)

4393 Benson Road, Code E2

Indian Head, MD 20640

SUBMITTED BY: ________________________________________ DATE: __________________

Philip A. Renn Aerospace Engineer, Technology Development Branch, Code E24PR

NSWC IHD

REVIEWED BY: _________________________________________ DATE: __________________

Armen G. Malkasian Manager, Technology Development Branch, Code E24

APPROVED FOR USE AS

PRODUCT BASELINE BY: ________________________________ DATE: __________________

Robert Hastings CAD/PAD Division Senior Engineer

DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited.

INCH-POUND

RENN.PHILIP.

A.1229315362

Digitally signed by

RENN.PHILIP.A.1229315362

Date: 2020.10.27 08:25:18 -04'00'

MALKASIAN.ARM

EN.G.1228654716

Digitally signed by

MALKASIAN.ARMEN.G.122865471

Date: 2020.11.02 10:08:47 -05'00'

HASTINGS.ROBER

T.C.JR.1228788097

Digitally signed by

HASTINGS.ROBERT.C.JR.12287

88097 Date: 2020.11.02 14:13:46 -05'00'

27-Oct-2020

2-Nov-2020

2-Nov-2020

AMSC N/A 2 FSC 1377

DTL-WS-36035 (OS)

CAGE Code 30003

DETAIL SPECIFICATION

ITEM SPECIFICATION

FOR THE

DETONATING CORD ASSEMBLY (DCA)

This specification is approved for use by the Naval Sea Systems Command, Department of the Navy, and is available for use by all Departments and Agencies of the Departments of Defense.

1. SCOPE

1.1 Scope. This specification covers the requirements for the AH-64 Helicopter types of detonating cord assemblies commercially known as Thin Layer Explosives or TLX ® (see 6.1).

1.2 Classification. Detonating cord assemblies will be of the same configuration, varying in length and end-fitting connections, as specified (see 6.2).

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 cited 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 specified requirements of documents cited in sections 3 and 4 of this specification, whether or not they are listed.

2.2 Government documents.

2.2.1 Specifications, standards, and handbooks. The following specifications, standards, and handbooks 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 or contract.

DEPARTMENT OF DEFENSE SPECIFICATIONS

MIL-I-8500 Interchangeability and Replaceability of Component Parts for Aerospace Vehicles

MIL-L-14758 Lead Azide (Special Purpose) (For use in Ammunition)

MIL-PRF-46010 Lubricant, Solid Film, Heat Cured, Corrosion Inhibiting NATO

Code S-1738

MIL-C-83125 Cartridge for Cartridge Actuated/Propellant Actuated Devices, General Design Specification for

Comments, suggestions, or questions should be addressed to: Commander, Naval Surface Warfare Center Indian Head Division, Attn: CAD/PAD Division (Code E2), Indian Head, MD 20640 or emailed to IHDIV_Standardization_Team@navy.mil.

INCH-POUND

DTL-WS 36035 (OS)

DEPARTMENT OF DEFENSE STANDARDS

MIL-STD-810 Environmental Engineering Considerations and Laboratory Tests

MIL-STD-1168 Ammunition Lot Numbering and Ammunition Data Card

(Copies of these documents are available online at http://quicksearch.dla.mil/.)

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 are those cited in the solicitation or contract.

NAVAL SEA SYSTEMS COMMAND (CODE IDENT 53711)

SPECIFICATIONS

WS 5003 Hexanitrostilbene (HNS), Explosives

NAVAL AIR SYSTEMS COMMAND (CODE 30003)

DRAWINGS

841AS801 Fitting, Sensitivity Test 841AS802 Connector, Tee 841AS803 Block, Dent 841AS804 Holder, Dent Block

NSWC INDIAN HEAD DIVISION (CODE 14083)

DRAWING

520-174-0355 Detonating Cord Assembly

(Commander, Naval Surface Warfare Center Indian Head Division, Attn: CAD/PAD Division (Code E2), Indian Head, MD 20640)

2.3 Non-Government publications. The following documents 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 or contract.

ASTM INTERNATIONAL

ASTM B 117 Standard Practice for Operating Salt Spray (Fog)

Apparatus

ASTM E 748 Standard Practices for Thermal Neutron Radiography of Materials

ASTM D 1141 Standard Practices for the Preparation of Substitute

Ocean Water ASTM E 1742 Standard Practices for Radiographic Examination

(Copies of this document are available from ASTM International online at www.astm.org.)

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 from the Contracting Officer or their representative.

3. REQUIREMENTS

3.1 Inspections. The contract or purchase order will specify whether, a sample shall be subjected to lot acceptance inspections or first article inspections (see 4.3 and 4.4). A first article inspection shall be required if 2 years or more have passed since the item was manufactured, major turn over in personnel, major changes to the production facility, or transfer of production to a new facility or site.

3.2 Conformance to documents. All materials used in the manufacture of the Detonating Cord Assembly (DCA) shall conform to the specifications referenced unless specific approval in writing covering a departure therefrom has been obtained from the Government cognizant field activity for these DCAs prior to manufacture.

DCA design and construction shall be identical to that approved for service use by the Government. Any design changes affecting the interchangeability or performance of these items shall be subject to approval by the cognizant governmental design activity.

3.2.1 Interchangeability. Each line shall be interchangeable with its corresponding part number per 4.2.1.

3.2.2 Halar integrity. The Halar tubing with the energetic material loaded shall have no leaks per 4.2.2.

3.2.3 DCA cord velocity. The spool of cord used in production shall be tested on each end and every 500 feet to meet the detonation velocity requirements of 1400 meters per second minimum (see 4.2.3).

3.2.4 End fitting tensile test. The end-fitting joint between the outer ferrule and the braided stainless-steel casing shall be capable of withstanding a tensile load of 150 pounds minimum (see 4.2.4).

3.2.5 Corrosion. All components used in production shall be free of corrosive products (see 4.2.5). The threads shall be coated with a dry film lubricant per MIL-PRF-46010.

3.2.6 End fittings leakage. Each end fitting will be leak tested in a dry gas leak tester. End fittings which exhibit a leak rate in excess of 10-5 cc/sec of air at a pressure differential of 1 ± 0.1 atmosphere, when tested in accordance with paragraph 4.2.6, shall be considered defective and shall be rejected.

3.2.7 Explosive weight. Every 1,000 feet a 1-meter section of cord shall be taken to verify the requirement of 20 +/- 10 mg of ignition material per meter (see 4.2.7).

3.2.8 Primary components. For the purpose of this specification, the thin layer explosive loaded cord, the cord energetic ignition materials, the booster tip explosive (HNS, WS5003), and transfer charge (Lead Azide, MIL-L-14758) are considered primary components.

3.3 First article inspection. If a first article test is invoked by the contract or purchase order then the first article inspections in 4.3 apply.

3.4 First article testing. Following the successful completion of the first article inspection per 4.3, the test samples shall be exposed to the environmental tests in the sequence stated in Table I.

TABLE I. First article inspection

TESTS Reqmnt Para Test Para

Group Number Total per test I

II

III

IV

V

VI

VII

Length stabilization 3.4.1 4.4.1 5 5 5 3 3 3 3 27 X-ray 3.4.2.1 4.4.2 5 5 5 3 3 3 3 27 N-ray 3.4.2.2 4.4.2 5 5 5 3 3 3 3 27 Visual 3.4.3 4.4.3 5 5 5 3 3 3 3 27 Temp Shock, Humidity and altitude 3.4.4 4.4.4 5 5 5 15 20 G Shock 3.4.5 4.4.5 5 5 5 15 Vibration 3.4.6 4.4.6 5 5 5 15 Pressure cycling 3.4.7 4.4.7 5 5 5 15 Temperature cycling 3.4.8 4.4.8 5 5 5 15 Minimum bend/flex 3.4.9 4.4.9 3 3 6 Salt fog 3.4.10 4.4.10 5 5 5 15

Ballistics -65 oF 3.4.11 4.4.11 5 3 3 11 Ballistics 70 oF 3.4.11 4.4.11 5 5 Ballistics 175 oF 3.4.11 4.4.11 5 3 3 11

3.4.1 Length Stabilization. Per 4.4.1 the cord shall be annealed to stabilize cord length prior to use. The minimum percent shrinkage achieved when first annealed shall not be less than 1.25% of the cord total length.

When retested in accordance with 3.4.1, the maximum shrinkage shall be 0.2% of the sample length.

3.4.2 Radiographic inspection. Radiographic inspections, both N-ray and X-ray shall be performed in accordance with 4.4.2.

3.4.2.1 X-ray examination. Each DCA end assembly and approximately 3 inches of line behind the tips shall be X-rayed. All defects shall be identified on the film and defective DCAs removed from the lot (see 4.4.2).

3.4.2.2 N-ray examination. Each DCA assembly end tips shall be N-rayed. All defects shall be identified on the film and the defective DCAs removed from the lot (see 4.4.2).

3.4.3 Visual inspection. DCAs shall pass the inspection per 4.4.3 and be free of visual defects such as, but not limited to, burrs, deep scratches, defective ferrules and fittings, corrosion, chipped surfaces, or other defects that may prevent assembly or affect the environmental stability of the line. The threads of the DCA end fittings shall be dry film lubricated with MIL-PRF-46010. The dash number tape, identification tape and identification plate shall be verified to comply with 14083-520-174-0355.

3.4.4 Temperature, humidity, shock, and altitude. Per 4.4.4, the DCAs subjected to temperature, humidity, shock, and altitude environments shall meet the performance requirements of 3.4.11.

3.4.5 20 G shock. DCAs shall meet the performance requirements of 3.4.11 after being exposed to the shock environment of 4.4.5.

3.4.6 Vibration. DCAs shall meet the performance requirements of 3.4.11 after being exposed to random sinusoidal vibration environments of 4.4.6.

3.4.7 Pressure cycling. DCAs shall meet the performance requirements of 3.4.11 after pressure cycling from

6.76 inches of mercury to 29.92 inches of mercury at temperatures of -65°F to 160°F (see 4.4.7).

3.4.8 Temperature cycling. DCAs shall meet the performance requirements of 3.4.11 after temperature cycling between -65°F and 160°F per 4.4.8.

3.4.9 Minimum bend/flex. Six lines shall be wrapped a minimum of four turns on a 1-inch-diameter helix along the centerline for 4 hours minimum and meet the requirements of 3.4.11 per 4.4.9.

3.4.10 Salt fog. DCAs shall meet the performance requirements of 3.4.11 after exposure to salt/fog environments (see 4.4.10).

3.4.11 Ballistic requirements. The DCA ballistic sample shall meet the requirements of 3.4.11 when tested per 4.4.11.

3.4.11.1 Sensitivity. DCAs shall be fired per 4.4.11 through a sensitivity connector (Drawing 841AS801) into a sensitivity fixture from a tee (Drawing 841AS802) that is fired from one of two SMDC or TLX test tips. Each assembly shall have a 1-inch-diameter loop in the assembly when tested. The assembly, when conditioned at - 65°F, 70°F or 175°F, shall propagate and produce an indent of at least 0.040 inch in a 6061-T6 aluminum dent block (Drawing 841AS803) secured in a dent block holder (Drawing 841AS804).

3.5 Lot acceptance testing. Lot acceptance testing shall be conducted in accordance with 4.5.

3.5.1 Lot size. Lot size shall be per 4.5.1 unless otherwise specified in the contract or purchase order.

3.5.2 Lot sampling. The selection of test samples shall be performed per 4.5.2.

3.5.3 Conformance to documents. All materials used in the manufacture of the DCA shall conform to 4.2 and the specifications referenced unless specific approval in writing covering a departure therefrom has been obtained from the Government cognizant field activity for these DCAs prior to manufacture. DCA design and construction shall be identical to that approved for service use by the Government. Any design changes affecting the interchangeability or performance of these items shall be subject to approval by the cognizant governmental design activity.

3.5.4 Length stabilization. The cord shall be annealed to stabilize cord length prior to use. The minimum percent shrinkage achieved when first annealed shall not be less than 1.25% of the cord total length. When retested in accordance with 4.4.1, the maximum shrinkage shall be .2% of the sample length.

3.5.5 Visual inspection. DCAs shall pass the inspection per 4.4.3 and be free of visual defects such as, but not limited to, burrs, deep scratches, defective ferrules and fittings, corrosion, chipped surfaces, or other defects that may prevent assembly or affect the environmental stability of the line. The threads of the DCA end fittings shall be dry film lubricated with MIL-PRF-46010. The dash number tape, identification tape and identification plate shall be verified to comply with 14083-520-174-0355.

3.5.6 X-ray examination. Each DCA end assembly and approximately 3 inches of line behind the tips shall be X-rayed. All defects shall be identified on the film and defective DCAs removed from the lot (see 4.4.2).

3.5.7 N-ray examination. Each DCA end assembly and approximately 3 inches of line behind the tips shall be N-rayed. All defects shall be identified on the film and the defective DCAs removed from the lot (see 4.4.2).

3.5.8 Ballistic requirements. The ballistic sample shall meet the requirements of 3.4.11.1.

3.6 Workmanship. DCAs shall be constructed and finished in a manner to assure compliance with all requirements of this specification. Particular attention shall be directed to dimensions, finishes, crimping, sealing, and assembly operations.

4. VERIFICATION

4.1 Classification of inspections. The inspection requirements specified herein are classified as follows:

a. First article inspection (see 4.3)

b. Lot acceptance inspection (see 4.5)

4.1.1 Inspection conditions. Unless otherwise specified (see 6.2), all inspections shall be performed in accordance with the test conditions specified in 4.3 and 4.4.

4.2 Material conformance. All materials and their certifications used in the manufacture of these DCAs shall be identified in the Ammunition Data Cards per MIL-STD-1168 as specified in the contract.

4.2.1 Interchangeability. The contractor shall conduct inspections of the production lot to verify total interchangeability per MIL-I-8500 of the lines and end fittings with their corresponding part number per 3.2.1.

4.2.2 Halar integrity. One end of the tube will be sealed and a + 1 atmosphere of air pressure applied to the other end for 5 minutes with no pressure loss per 3.2.2.

4.2.3 Cord velocity. Each end and every 500 feet of planned cord production shall be tested for velocity measurement per 3.2.3 prior to actually producing any DCAs.

4.2.4 End fitting strength. Five DCAs from the lot acceptance test sample shall be subjected to the 150-pound load test per 3.2.4 to verify the fitting strength. The 150-pound load shall be reached by applying the load at a rate of 6 pounds per second. The load shall be maintained for 60 seconds minimum. The lines shall be radiographed per 3.4.2 and any units showing a gap greater than 0.050 inch between the bottom center bore and the Halar shall reject the lot. If it is decided to ballistically test the rejects and they meet the requirements of

3.4.11 the lot may be considered for acceptance depending on the rest of the testing.

4.2.5 Corrosion. All parts shall be visually inspected to assure there are no corrosion products on the hardware per 3.2.5 and that the threads are coated with dry film lubricant.

4.2.6 End fitting leakage. Each end fitting shall be tested in a dry gas leakage tester to demonstrate that the requirement of 3.2.6 is met.

4.2.7 Explosive weight. The explosive shall meet the requirements of 3.2.7 when removed from the cord and the residue weighed to the nearest milligram to verify explosive weight.

4.2.8 Primary components. The primary components shall be verified by inspection of the Ammunition Data Cards, as identified in the contract to validate component single lot composition.

4.3 First article inspection. First article inspection per 3.3 shall be performed after award of contract and prior to production at a location acceptable to the Government (see 6.3). First article inspection shall be performed, as specified in Table I, on sample units, which have been produced with equipment and procedures normally used in production. First article approval is valid only on the contract under which it is granted, unless extended by the Government to other contracts.

4.3.1 Sample size. Unless otherwise specified (see 6.3), 27 DCA lines representative of the planned production shall be sequentially conditioned and ballistically tested with the exception that one shall be kept as a retain sample for investigative purposes.

4.3.2 Inspection routine.

4.3.2.1 Detonating cord assemblies. The samples shall undergo the non-destructive examinations and tests of

3.2 prior to environmental exposure as described in Table I. The tolerance on temperatures shall be ± 5°F. The environmental exposures shall be sequential as shown in Table I. The conditioning temperatures for ballistic testing are -65°F, 70°F and 175°F with a third fired at each temperature. Any remaining samples shall be fired at 175°F. Temperature conditioning at the extremes shall be no less than 4 hours and no more than 24 hours.

4.3.2 Failures. The failure of any DCA to meet the requirements of 3.4.11 shall cause rejection of the first article sample.

4.4 First article test. The first article tests shall validate the requirements of 3.4.

4.4.1 Length stabilization. The TLX cord, prior to its use in TLX manufacture, shall be annealed at a stabilized temperature of 300 ± 5°F for 60 to 65 minutes continuous. For every continuous length of cord annealed (approximately 1,000 ft. max.), 3 samples (36 ± .10 inches per sample) shall be cut from the cord. These samples shall be annealed to the time and temperature described above and shall meet the requirement of 3.4.1 for retest.

4.4.2 Radiographic examination. All DCAs in the first article sample or production lot shall be radio-graphically examined in accordance with ASTM E1742 and ASTM E 748. Any observable imperfections in components or assembly of the DCA lines shall be cause for rejection. The DCAs shall be positioned on their sides for the most revealing exposure. DCAs shall be arranged on trays or boards in consecutive numerical order and each radiograph shall carry a permanent identification displayed thereon. The radiographic identification shall include the complete lot number in accordance with MIL-STD-1168, the contract number, drawing number, and the span of serial numbers displayed. Defective DCAs found by the vendor shall be clearly identified on the X- ray and those defective DCAs removed from the production lot. The serial numbers shall be located apart from other markings.

4.4.3 Visual inspection. The external condition and appearance of the DCA shall be determined by comparison to Drawing 520-174-0355. Specific inspections to the labels, outer covering, B-nut threads, end tip appearance, no dent or scratches, proper color, correct data on label and shipping caps shall be conducted at a minimum.

4.4.4 Temperature, humidity, shock and altitude. Fifteen assemblies shall be subjected to the 28-day exposure to temperature, humidity, shock, and altitude environments per 3.4.4 as detailed in MIL-C-83125.

4.4.5 20 G shock. The 20 G shock test per 3.4.5 shall be conducted on fifteen assemblies to ensure that the requirements of MIL-STD-810, method 516, Procedure I is met. The shock pulse waveform shall be terminal peak saw tooth. The amplitude shall be 20 G and the duration 11 msec. Tips and centers of the lines shall be supported as in actual installation.

4.4.6 Vibration (sinusoidal). To meet the requirements of 3.4.6 the equipment shall be verified in accordance with MIL-STD-810, Method 514.5, Procedure I and Annex A, Para. 2.3.3, Category 14 (for equipment in helicopters) and Figure 1 with the following clarifications:

FIGURE 1. Non-gunfire flight vibration test spectrum subject to main rotor influence

The main rotor influences all areas of the fuselage. The main rotor fundamental frequency f1 in Table 514.5C-IV for this region is 4.86 Hz. Four harmonics of the main rotor are superimposed on the random background at 4.86, 19.5, 38.9, and 58.4 Hz. The complete sine-on-random test spectrum for this region is shown in Figure 1. Pre-and post-resonance scan shall be ran to the profile in Figure 2. After testing, the DCA shall meet the requirements of 3.4.11.

FIGURE 2. Acceleration input profile for use in resonance scans before and after testing

4.4.7 Pressure cycling. Ten assemblies shall be subjected to a minimum of 100 pressure cycles with 50 cycles conducted at 160°F and 50 cycles at -65°F. One pressure cycle shall consist of the following sequence: the pressure shall be 29.92 inches mercury (Hg) and held for 5 minutes and then reduced to 6.76 inches Hg (20,000 feet) in less than 5 minutes. The absolute pressures shall be maintained at 6.76 inches Hg for 25 minutes then increased to 29.92 inches Hg in less than 5 minutes and maintained at 29.92 inches Hg for 25 minutes. One cycle shall have a 60-minute duration. There shall be no withdrawals during the pressure cycling. The requirements of

3.4.7 shall be met after exposure to pressure cycling.

4.4.8 Temperature cycling. After pressure cycling, the ten DCAs shall be subjected to a minimum of 100 temperature cycles. One temperature cycle shall consist of the following sequence: The temperature shall be stabilized at -65°F and maintained for 55 minutes. The temperature shall then be raised to 160°F in 5 minutes and maintained for 55 minutes and then lowered to -65°F in 5 minutes. One cycle shall have a 2-hour duration. The assemblies shall meet the requirements of 3.4.11 when tested.

4.4.9 Minimum bend/flex. Six DCAs shall be wrapped in a 1-inch-diameter helix along the centerline for four complete revolutions and shall remain in that configuration for 4 hours minimum. The assemblies shall meet the requirements of 3.4.11 when tested.

4.4.10 Salt fog. The salt fog test shall be conducted in accordance with ASTM B 117 except that seawater per ASTM D 1141 shall be used in place of a 5 percent salt solution. The control of pH and salt impurity requirements per ASTM B 117 shall not apply. Test duration shall be 168 hours.

4.4.11 Ballistic testing. After successfully completing the above examinations, the assemblies shall be conditioned as specified in 4.3.2.1. Assemblies shall be removed from the conditioning chamber and tested per

3.4.11.1 within 5 minutes after removal from the conditioning chamber. If this time is exceeded, the test samples shall be removed from the test fixture and reconditioned for 1 hour minimum as the specified temperature. The DCAs shall be grouped into three equal sections with one group conditioned at -65 + 5°F , the second at 70 + 5°F, the other group conditioned at 175 + 5°F for 4 hours minimum to 24 hours maximum. The DCAs shall then be functionally tested in accordance with 3.4.11 using a number 8 blasting cap on the test tip. The lot shall be accepted if the requirements of 3.4.11.1 have been met with an accept of zero and a reject of one or more criteria.

4.4.11.1 Retest. There shall be no retests.

4.4.11.2 Test failure. If a test failure is attributable to an assignable cause, excluding the DCA's, the original test results shall be discarded and that portion of the test reconducted using a retain sample from the lot.

4.5 Lot acceptance inspection. Conformance inspection shall consist of verification of the characteristics listed in Table II.

TABLE II. Lot acceptance testing

Requirement Rqmnt Para Test para Conformance to documents

3.2 4.2

Length Stabilization 3.4.1 4.4.1

Visual inspection 3.4.3 4.4.3

X-ray 3.4.2.1 4.4.2 N-ray 3.4.2.2 4.4.2

Ballistics 3.4.11 4.4.11

4.5.1 Lot size. Unless otherwise specified in the contract (see 6.2), the DCA production lot size shall be as defined in the contract. DCAs required for all test purposes shall be randomly selected from the production lot and shall not be applied as a part of the quantity specified for delivery by the contract. Only primary components from a single lot shall be used in a production lot of DCAs, however, one primary component production lot may be used in more than one DCA production lot. DCAs for the ballistic tests shall be delivered to the activity designated by the contracting agency (see 6.2).

4.5.2 Sampling. Lot sampling size shall be to general inspection level II in accordance with ASQ Z1.4. Two additional samples shall be retained regardless of lot size. End fitting tensile tests shall require five (5) samples per lot.

5 PACKAGING

5.1 Packaging. For acquisition purposes, the packaging requirements shall be as specified in the contract or purchase order (see 6.2). When packaging of materiel is to be performed by DoD or in-house contractor personnel, these personnel need to contact the responsible packaging activity to ascertain packaging requirements.

Packaging requirements are maintained by the Inventory Control Point’s packaging activities within the Military Service or Defense Agency, or within the military service’s system commands. Packaging data retrieval is available from the managing Military Department or Defense Agency’s automated packaging files, CD-ROM products, or by contacting the responsible packaging activity.

6 NOTES

(This section contains information of a general or explanatory nature that may be helpful but is not mandatory.)

6.1 Intended use. Generally, the DCAs are intended as a rapid energy source to provide an explosive release signal in the aircraft emergency systems. Specifically, they are used in areas requiring more flexure during their life cycle but can be used in static installations. They have a protective coating to prevent damage and are required to pass additional cycling tests. These items were specifically designed for use in these military aircraft, and thus have no commercial application.

6.2 Ordering data. Acquisition documents should specify the following:

a. Title, number and date of this specification.

b. Issue of DODISS to be cited in the solicitation, and if required, the specific issue of individual documents referenced (see 2.2.1, 2.2.2, and 2.4).

c. Type of DCA required (see 1.2).

d. Whether first article inspection is required and if so, specify the test activity (see 3.1 and 4.3).

e. Inspection conditions if other than as specified in 4.2.

f. Sample size if other than as specified in 4.3.1.

g. Production lot size and test activity (see 4.5.1).

h. Marking if other than as specified in 5.1and 6.4.1.

i. That the safety precaution requirements of the "Contractors' Safety Manual for Ammunition, Explosives and Related Dangerous Material," DOD 4145.26M are applicable. NOTE: When this specification is used as a part of the description of work to be accomplished by a Government activity the safety precaution requirements of "Ammunition and Explosives," OP 5, are applicable.

6.3 First article. When a first article inspection is required, the items should be a first article lot. The first article lot should consist of 27 DCAs. The contracting officer should include specific instructions in acquisition documents regarding arrangements for examinations, approval of first article test results and disposition of the lot.

Invitations for bids should provide that the Government reserves the right to waive the requirement for samples for first article inspection to those bidders offering a product which has been previously acquired or tested by the Government and that bidders offering such products, who wish to rely on such previous production or tests, must furnish evidence with the bid that prior Government approval is presently appropriate for the pending contract.

6.4 Contract packaging and marking. The following marking requirements should be specified in the contract.

6.4.1 Markings.

6.4.1.1 Special markings. Marking of interior, intermediate and exterior containers should be in accordance with 49 CFR 171-178 and MIL-STD-129.

6.4.1.2 Normal markings. Unless otherwise specified in the contract or order, the marking information on unit packages and shipping containers should be as specified below. The specified marking information should be applied to the containers in accordance with the applicable provisions of MIL-STD-129.

Inner Container Marking

a. National Stock Number and DODIC

b. Nomenclature: Cord Assembly, Detonating

c. Drawing Number

d. Quantity: One

e. Lot Number in accordance with MIL-STD-1168

f. Dash Number

g. Warning: Ammunition, Non-explosive

Outer Container Marking

a. National Stock Number and DODIC

b. Nomenclature: Cord Assembly, Detonating

c. Drawing Number

d. Quantity

e. Lot Number in accordance with MIL-STD-1168

f. Dash Number

g. Gross weight and Cube

h. Contract or Purchase Order

i. Warning: Ammunition, Non-explosive

6.4.1.3 Explanation of terms. For the purpose of this specification, NAVSUPINST 4030.28B should be used to clarify terms.

6.5 Subject term (keyword) list.

Aluminum Halar ®

HMX

HNS

Lead Azide Shielded Mild Detonating Cord (SMDC)

6.6 Changes from previous issue.

Custodian: Preparing activity:

Navy – OS Navy - OS

SPECIAL PACKAGING INSTRUCTION

Form Approved OMB No. 0704-0188

Public reporting burden for this collection of information is estimated to average 30 days per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing the collection of information. Send comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing this burden, to Washington Headquarters Services, Directorate for Information Operations and Reports, 1215 Jefferson Davis Highway, Suite 1204, Arlington, VA 22202-4302, and to the Office of Management and Budget, Paperwork Reduction Project(0704-0188). Washington, DC 20503. Please do not return your form to either of these addresses.

1. PART OR DRAWING NO. NOMENCLATURE 2. CODE INDENT 3. SPI NO.

Cord Assembly: Detonating 59678 (AD) P 1377- 7

4. NATIONAL STOCK NO. 5.DATE OF DRAWING/SPI

(YYMMDD)

6. REVISION / ERR NO.

SEE TABLE 1 200831 C

7. QUP / UNIT OF ISSUE 8. ICQ 9. UNIT PACK WT. (LB) (0.0) 10. UNIT PACK CU (CU.

FT.)(0.000)

11. UNIT PACK SIZE (INCHES)(00.0)

SEE TABLE 1 N/A SEE TABLE 1 0.326 12.1 X 7.5 X 6.2

18.

STEPS

19.

REQD

20.

DESCRIPTION

12. MILITARY PRESERVATION 1 1 Barrier Bag, MIL-DTL-117, TY I, CL F, ST 1 12.2" x 8.8” 2 AR Filler, ASTM D4727 MIL-STD-2073-1 3 AR Cushioning, A-A-59135 (SEE NOTE (B))

13. CLEANING 4 1 Inner Carton ASTM D5118, STYLE RSC, TYPE CF 11.0” X 6.8

X 5.6”

* 5 1 M2 Series Metal Container, M2A1 Metal Container (7553296) or

M2A2 Metal Container (13032542)

14. DRYING 6 AR Tape, Pressure-Sensitive, ASTM D5330, 1" Width, TY I

* 7 1 Metallic Seal (8794342)

15. PACKING

a. LEVEL A

MIL-STD-2073-1

b. LEVEL B

MIL-STD-2073-1

16. MARKING

MIL-STD-129, PARA 5.14 AND NOTE G BELOW

17. NOTES/DRAWING * THESE BLOCKS WILL CHANGE DEPENDING UPON THE ITEM BEING PACKED.

(A) THIS DOCUMENT CONTAINS PACKAGING INSTRUCTIONS FOR THE PREPARATION OF LIGHT BOXES FOR SHIPMENT OF CAD/PAD ITEMS IDENTIFIED IN TABLE 1, PACKED IN M2 SERIES METAL CONTAINERS (STEP 5). THE M2 SERIES METAL CONTAINER (STEP 5) MAY BE USED AS THE PRIMARY SHIPPING CONTAINER, IF THE WEIGHT DOES NOT EXCEED 45 LBS WHEN PACKED. THIS SPI UTILIZES THE M2 SERIES METAL CONTAINER (STEP 5) FOR LIGHT BOX APPLICATIONS AND APPLIES TO ANY NSN THAT MEETS THE REQUIREMENTS OF NOTE B. INSPECT M2 SERIES METAL CONTAINER (STEP 5) TO

ENSURE IT IS CLEAN AND SERVICEABLE PRIOR TO USE.

(B) INSERT ANY NSN LISTED IN TABLE 1 INTO BARRIER BAG (STEP 1). REMOVE EXCESS AIR AND CLOSE BY HEAT SEALING.

WRAP BARRIER BAG WITH A MINIMUM OF TWO WRAPS OF CUSHIONING MATERIAL (STEP 3). PLACE BAGGED AND WRAPPED ITEM IN INNER CARTON (STEP 4) AND FILL ANY VOIDED AREAS WITH CUSHIONING MATERIAL (STEP 3).

(C) IN LIEU OF STEP 2 AND 3 ABOVE, THE FOLLOWING ALTERNATIVE MATERIALS MAY BE USED TO ENSURE A TIGHT PACK:

PPP-C-1797 OR A-A-59136. CLOSE CARTON USING TAPE (STEP 6).

(D) INSERT CARTON (STEP 4) INTO M2 SERIES METAL CONTAINER (STEP 5). ADD FILLER MATERIAL (STEP 2) TO FILL ANY VOIDS ON THE SIDES, ENDS AND TOP OF THE M2 SERIES METAL CONTAINER (STEP 5) TO ENSURE A TIGHT PACK.

(E) CLOSE AND SEAL THE M2 SERIES METAL CONTAINER (STEP 5) LATCH WITH METALLIC SEAL (STEP 7).

(F) UNIT PACK MEETS LEVEL A PACK REQUIREMENTS. THE M2 SERIES METAL CONTAINER (STEP 5) MAY BE USED AS

SHIPPING CONTAINER BY APPLYING REINFORCED TAPE (STEP 6) AROUND THE CIRCUMFERENCE BETWEEN THE END OF THE HANDLE AND THE LATCH (SEE FIGURE 1 ON PAGE 3). THE REINFORCED TAPE IS NOT INTENDED FOR LONG TERM

STORAGE.

(G) MARK IN ACCORDANCE WITH MIL-STD-129, PARA 5.14 AND AS A MINIMUM:

NSN/DODIC

UNITED NATION IDENTIFICATION NUMBER/PROPER SHIPPING NAME

QTY

NOMENCLATURE

LOT NUMBER

PACKAGE GROSS WEIGHT

SPI NO (AD) P 1377-7

PERFORMANCE ORIENTED PACKAGING (POP) MARKINGS

HAZARD LABEL

WSC: ITEM SIZE: * ITEM WEIGHT: * DMW APPROVED:

DISTRIBUTION STATEMENT A; APPROVED FOR PUBLIC RELEASE; DISTRIBUTION IS UNLIMITED.

DD Form 2169C, JUN 97 Previous editions are obsolete Page 1 of 3 Pages

HANSSEN.JOSEP

H.W.1376495538

Digitally signed by

HANSSEN.JOSEPH.W.1376495538

Date: 2020.09.01 13:10:00 -05'00'

DD Form 2169C, JUN 97 Previous editions are obsolete Page 2 of 3 Pages

1. PART OR DRAWING NO. NOMENCLATURE 2. CODE INDENT 3. SPI NO.

Cord Assembly: Detonating 59678 (AD) P 1377- 7

4. NATIONAL STOCK NO. 5.DATE OF SPI

(YYMMDD)

6. REVISION / ERR NO.

SEE TABLE 1 200831 C

17. NOTES/DRAWING

(H) THE PROPER SHIPPING NAME WILL COMPLY WITH THE JOINT HAZARD CLASSIFICATION SYSTEM (JHCS) FOR THE

TYPE CLASSIFIED ITEMS.

(I) UNITIZATION PROCEDURES:

1. A PALLETIZED LOAD SHALL NOT EXCEED 4,000 POUNDS AND SHOULD NOT EXCEED 52 INCHES IN LENGTH

OR WIDTH, OR 54 INCHES IN HEIGHT. WHEN THE ITEM BEING PALLETIZED IS AMMUNITION/EXPLOSIVE, AT

LEAST ONE OF THE HORIZONTAL DIMENSIONS MUST BE LESS THAN 47 INCHES. WHEN LEVEL A

PACKAGING IS REQUIRED, A FOUR-WAY ENTRY PALLET SHALL BE USED. ALL PALLET LOADS SHALL CONTAIN THE LOAD IN A MANNER THAT WILL PERMIT SAFE, MULTIPLE REHANDLING DURING STORAGE

AND SHIPMENT.

2. PALLET MARKING: MARK PALLETIZED LOAD IAW MIL-STD-129, PARA 5.14

(J) THE PERFORMANCE ORIENTED PACKAGING MARKING FOR THE APPLICABLE OPTIONS ARE AS FOLLOWS:

M2 SERIES METAL CONTAINER (STEP 5) 4A/Y21/S/** **INSERT YEAR PACKED

WITH TAPE CLOSURE: USA/DOD/AYA

TABLE 1 – ITEM CHART

NSN DODIC ITEM SIZE ITEM WT/LBS. PART NUMBER

1377-01-356-7841 SP02 55.5 X .26 INCHES 0.26 51960-1

1377-01-356-7842 SP03 60.5 X .26 INCHES 0.26 51960-4

1377-01-685-6574 JP01 34.5 X .19 INCHES 0.08 51960-5

1377-01-685-6603 JP02 42.5 X .19 INCHES 0.10 51690-7

1377-01-685-6606 JP03 31.5 X .19 INCHES 0.08 51960-8

1377-01-685-6581 JP04 21.0 X .19 INCHES 0.06 51960-6

u n

DD Form 2169C, JUN 97 Previous editions are obsolete Page 3 of 3 Pages

1. PART OR DRAWING NO. NOMENCLATURE 2. CODE INDENT 3. SPI NO.

Cord Assembly: Detonating 59678 (AD) P 1377- 7

4. NATIONAL STOCK NO.

5.DATE OF SPI

(YYMMDD)

6. REVISION / ERR NO.

SEE TABLE 1 200831 C

FIGURE 1

NOTE: ITEMS SHIPPED WITH THIS SPECIAL PACKAGING INSTRUCTION MUST PASS QUALITY ASSURANCE

INSPECTION CRITERIA.

POP MARKING

PLACE ON THE BACK SIDE OF

CLOSURE:

1 REQUIRED

1” WIDE X LENGTH

TO OVERLAP ITSELF

PROPER SHIPPING

NAME &

ID NUMBER

IDENTIFICATION

MARKINGS

HERE

EXPLOSIVE LABEL

Place on the End of the box

Controlled by: NSWC IHD/Code E26 CUI Category: CTI Distribution/Dissemination Control: DISTRO C