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DOD-STD-39 March 1979SUPERSEDINGMIL-STD-35-23(MI)2 JULY 1974

MILITARY STANDARD

FASTEN ERS

AUTOMATED ENGINEERINGDOCUMENT PREPARATION SYSTEM

FSC EDS

Downloaded from http://www.everyspec.com

DOO-STD-35-23A(MI)9 March 1979

DEPARTMENT OF THE ARMYU.S. ARMY MATERIEL

DEVELOPMENT AND REAOINESS COMMANOALEXANDRIA, VA 22333

Fast~nersAutomated EngineeringDocument Preparation System

06D-STD-35-23A(MI)

1. This Mi1itary Standard is approved for use by OARCOM, Department of theArmy and is avai1able for use by al1 Departments and Agencies of the Depart-ment of Defense.

2. Beneficial comnents (recommendations, additions, deletions) and anypertinent data which may be of use in‘improving this document should beaddressed to Commander, U.S. ,AtmyMissi1e Research and Development Comnand,ATTN: DRDMI-ESD, Redstone Krsenal, Alabama 35809, by using the self-addressed Standardization Document Improvement Proposal (DD Form 1426)appearing at the end of this document or by letter.

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DOD-STD-35-23A(MI)9 March 1979

1,.

FOREWORD

The purpose of 00D-STD-35-23A(MI) is to provide instructions for thej;eparation of Specification Requirements Sheets (SRS) in order to produceMilitary Specification Exceptions for Fasteners.

2. In order to properly utilize this document, it is necessary to have acomplete and thorough understanding of the DOD-STD-35.

3. It is important that the procedures described in the basic document(DOD-STD-350 and subsequent revisions) be followed explicitly in order toproduce a document suitable for procurement. Information which is standardfor all dash-numbered parts has been included in the basic document at theissuance of DOD-STD-35D. This infonnation is not repeated in each dash-numbered part.

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CONTENTS

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Paragraph 1. SCOPE --------------- ------- 11.1 General ------------ -------- 11.2 Purpose ------------ -------- 11.3 Utilization -------- ---------- 11.4 Military Specification Exception Title

Index ----------- ---------- 1

2. REFERENCE DOCUNENTS - - - - - - - - - - - - - - 5Issues of documents ---- ----------

$:;5

Other publications- - - - - - - - - - - - - - - 6

3. DEFINITIONS --------- ---------- 8

4. GENERAL REQUIREMENTS - - - - - - - - - - - - - - 9Introduction-------- ----------

f:l9

Specification Requirement Sheet (SRS) - - - - - 94.3 Configuration --------- -------- 94.3.1 Dimensions----------- -------- 94.3.2 Illustrations --------- -------- 94.4 Units of measure-------- -------- 9

5. DETAILED REQUIREMENTS - - - - - - ~~- - - - - - - 105.1 Introduction---------- -------- 105.2 MSE Formats ---------- -------- 105.3 Referenced documents- - - - - - - - - - - - - -

Test matrix ---------- -------- ;:2:2 Tabulation----------- -------- 125.6 Keyword Code Index (KCI) and

Standard Paragraphs - - - - - - - - - - - - - - 155.6.1 Interrelationship of Codes- - - - - - - - - - - 155.6.2 Automatic MSE Data------- -------- 155.6.3 DOD-STD-35 Tables -------- ------- 15

TABLES

Table I. Title Index ---------- --------- 211. Test matrix ---------- --------- 11111. Tabulation candidates - - - - - - - - - - - - - - 13

APPENDICES

Appendix A. Illustrations --------- -----’----B.

118Characteristic Code Index - - - - - - - - - - - - 156

Index -------------- -------- 161

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10DOD-STO-35-23A(MI)9 March 1979

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1. SCOPE

1.1 General. This dash-numbered part of the Automated Engineering OocumentPreparation System (AEOPS), provides detailed requirements for the prepara-tion of Military Specification Exception (MSE) documentation for Fasteners.

‘“2v ~This military standard provides the necessary information toprepare a pacification Requirement Sheet (SRS) which will be used togenerate an MSE by automated data processing.

1.3 Utilization. General instructions, quality assurance provisions,packaging, and notes, applicable to all AEDPS dash-numbered parts have beenincluded in the basic document (DOD-STD-35) to avoid redundancy. Unlessotherwise specified in this dash-numbered part, the following list containsadditional subjects that are applicable to all AEDPS dash-numbered parts andare included in DOD-STD-35:

a. Writing Methodologyb. Document and Part Numberingc. Applicable Oocumentsd. Single and Multi-item Specifications (Tabulation)e. Keyword Code Index (KCI)f. General Requirements of AEDPS

1.4 Military Specification Exception Title Intiex. It is recommended thatMIL-S~nstruction of AerospaceMechanical Systems be reviewed prior to using this dash-numbered part book.

The title code for an MSE shall be selected from one of the MSE titleslisted in the Title Index (see table I). Oata bases have been establishedfor the generation of MSE’S for the MSE titles indicated. If a suitabletitle code is not contained in the Title Index, leave the title code spaceson the SRS blank, and attach a request for the assignment of a title code.Include in the request the desired title and the base document identifier.A code will be assigned and the code, title, and base document will be madea part of the Title Index.

One of the six-digit codes listed in the Title Index, entered on anSRS, will specify that the title of the MSE will be the title shown in theTitle Index.

Each MSE title listed in the Title Index is compatible with the docu-ment(s) listed with that title under base document. The list of base docu-ments may or may not be’a complete listing. The information shown undercoverage is intended for the user’s reference; when mere than one documentis listed for an MSE title. this information will be found useful in deter-mining which of the documents is most suitable for use as the base document.

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The MSE title may or may not be the same as the title used in DODISS,FIIG, or the base document. In general, the MSE title uses the basic fed-eral item name listed in Cataloging Handbook H6. However, titles with addi-tional modifying and identifying words are provided to assist in definingthe scope of the MSE. Also, less restrictive titles are provided to pre-vent exclusion of items.

TABLE I. ILILE.L!25Z:

MSE TITLE.---- —----- —._ —___________FASTENER, BLIND ,

‘FASTENER, CONTAINERCLOSURE

FASTENER, EQUIPAGE

FASTENER, PANEL

FASTENER, PAPER

FASTENER, PARACHUTE PACK

TITLE BASE DOCUMENT—-—--————-_-——--__-—_____—___–scl?&– NUMBER_____ _ COVERAGE ___

1460%9 MIL-F–8975MS21J140

MS211141

NAS1669

NAS1670NAS16711

NASI1672

NAS3673

NASIJ674

146001 MS18015

MS24535

146002 MIL-F–411MIL-F-11698‘MIL-F-43514

146004 MIL–F–5591MI L-F-8490MIL-F-14187MI L-F-25173

lJ46005 FF-F-101FF-F-IJ1FF–F-115

146006 MS70092AN6572

2

HIGH STRENGTH100 DEG FLUSH -.

HEAD MECH LOCKPROTRUDING HEAD ICRESINTLY THREADEDEXT SLEEVEFLUSH HEADHIGH TEMPPROTRUDING HEADHIGH TEMP FLUSHHEAD ●LIGHT WEIGHTPROTRUDING HEADLIGHT WEIGHTMILLABLE HEAD

LATCH ANDSTRIKE ASSY.CONTAINER

BELTQUICK RELEASEEQUIPAGE ITEMS

.;

PANEL ~EQPT RACK ACFTREFRIGERATOR .1CONTROL, ACFT

PRONG TYPECOMPRESSOR TYPE

;

PINCH TYPEI

PACK 1TAB, OVAL

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TABLE I. ~~~L~ INDEX. (CONT)

TITLE B!!~_lqCQHEN1–_--____MSE TITLE CODE NUMBER COVERAGE__________________________ ______ _____________ ___ _____

i’ FASTENER, ROTARY

I FASTENER, SELF-LOCKING

●FASTENER, SLIDE

FASTENER, SNAP

I

FASTENER, QUICK OPERATING,ROTARY %46007 MIL-F-22978

MSl1773L

t4SL7732

NAS67

%46014 MIL-F–22978

1146008 MS143108

MS3J4109

146009 V–F-lIO6AN229

146010 MIL-F–10884t4S27977klS27978MS27979

MS27980

MS2798L

MS27982MS27983MS2798+

MS27985i+IS27986

MI L- F–51184

MI L- F–43573MIL-s-21733

FASTENER, SNAPSLIDE

~ ●✎FASTENER, TAPE, HOOK

146011 MS21324MS21325MS2!J326MS21332

146016 MIL-F-21840

3

SPECIFICATIONFLUSH HEADFLOATING TYPEPROTRUDING HEADFLOATING TYPEGUIDE-FASTENERLOW FORM, COWL

QUICK OPERATINGHIGH STRENGTH

CASE MOUNTINGELECTRONICW/HLDG CLP

INTERLOCKINGINTERLOCKING

SNAP, GENL SPECLARGE CURTAINSMALL CURTAINMUDPRF CURTAINTYPEWIRE SPRINGCLIP, REGULARWIRE SPRINGCLIP, SMALLPRONG RINGTHREE WAY, LKGSCALLOPED,BUTTON HEADFUNL NK, BTNHDRIVET TYPETUBULAR, SOLIDOR BUTTONPLASTICSUPPORT

BRASS STUDCRES STUDCRES STUDCRES

PILE SYNTHETIC


DOD-STO-35-23A(,MI);9 March 1.9.79% ,,..

TABLE I. TITLE INDEX. (CONT)—-—---------,.

TITLE BASE DOCUMENT; MSE ’TITLE

-—-—.--_— ____________________-_ ——_-— —__________________ CODE NUMBER COVERAGE--—----——---- ---——-——---—---FASTENER, TAPE, HOOK ANDPILE L460LZ MIL-F-23J840 SYNTHETIC

FASTENER, TAPE, PILE 146015 MIL-F-23J840 HOOK SYNTHETIC

FASTENER, WOOD JOINT 1460113 FF-F-133 CORRUGATED

HINGE 146017 MS20001 STRUCTURALEXTRUDED

HOLDER, SEMICONDUCTORDEVICE 146018 MIL-S-3t9500 SEMICOND DEVICE

GENL SPEC FOR

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2,, REFERENCE DOCUMENTS

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2.1 Issues of documents. The following documents of the issue in effect ondate of invitation for bids or request for porposal, fonm a part of thisstandard to the extent specified herein.

SPECIFICATIONS

FEDERAL

QQ-P-416

V-F-1D6

MILITARY

MIL-F-5591

MIL-F-8940

MIL-F-10884

MIL-F-21840

MIL-F-22978

MIL-F-25173

MIL-F-43514

MIL-H-6875

Plating, Cadnium (electrodeposited)

Fasteners, Slide, Interlocking

Fasteners, Panel

Fastener, Case, for Equipment RackSystem for Aircraft

Fasteners, Snap

Fastener Tapes, Hook and Pile, Synthetic

Fastener, Rotary, Quick Operating, HighStrength

Fastener, Control Panel, AircraftEquipment

Fastener, Plastic, for Equipage Items

Heat Treatment of Steels (AircraftPractice) Process For

STANDARDS

FEDERAL

FED-STD-H28 Screw-Thread StandardsServices

FED-STD-151 Metal, Test Methods

for Federal

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DDD-STD-35-23A(MI)9 March 1979

FED-STD-191 Textile Test Methods

FED-STD-406 Plastic, Methods of Testing

FED-STD-595 Colors

MILITARY

DDD-STD-35 Automated Engineering DocumentPreparation System

MIL-STD-130 Identification Marking of MilitaryProperty

MIL-STD-186 Protective Finishing Systems for Rockets,Guided Missiles, Support Equipment andRelated Materials

MIL-STD-81O Environmental Test Methods

MIL-STD-1312 Fasteners, Test Methods

(Copies of specifications, standards, drawings, and publicationsrequired by contractors in connection with specific procurement functionsshould be obtained from the procuring activity or as directed by thecontracting officer.)

2.2 Other publications. The following documents form a part of thisstandard to the dxtent specified herein. Unless otherwise indicated, theissue in effect on-date of invitation for bids or request for proposal shallapply.

ANsIB46.1 Surface Texture

(Application for copies should be addressed to American NationalStandards Institute (ANSI), 1430 Broadway, New York, N.Y. 1001B.)

ASTMA370 Method and Definitions for MechanicalTesting of Steel Products

ASTMD2060 (Measuring Zippers, Standard Methods ofTest For)

ASTME8 Tension Testing of Metallic Materials,-Methods Of

ASTME10 Method of Test for 8rinell Hardness ofMetallic Materials

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ASTME18

ASTME151

00D-STD-35-23A(MI)9 March 1979

‘RockwellHardness and Rockwell Super-ficial Hardness of Metallic Materials,Test For

Tension Tests of Material at ElevatedTemperatures with Rapid Heating andConventional or Rapid Strain Rates,RecotmnendedPractice For

ASTME380 Metric Practice Guide

(Application for copies should be addressed to the American Society forTesting and Materials, 1916 Race St., Philadelphia, PA 19103.)1“

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DOD-STD-35-23A(MI)9 March 1979 4!!

3. DEFINITIONS

Definitions contained in 000-STD-35 are applicable to Fasteners,

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4. GENERAL REQUIREMENTS

4.1 Introduction. In order to properly prepare an SRS for Fasteners, it isnecessary to use DOD-STD-35 in conjunction with this dash-numbered part. Inthe event the instructions or the writing methodology are not followed, anAEDPS edit routine will print error messages rather then the desired MSEdocument.

4.2 Specification Requirement Sheet (SRS~. SRS requirements described inDOD-STO-35 are applicable to Fasteners.

4.3 Configuration.

4.3.1 Dimensions. SRS requirements for dimensions described in 00D-STD-35are applicable to Fasteners.

4.3.2 Illustrations. Illustrations applicable to Fasteners are contained inAppendix A to this document.

4.4 Units of measure. The International System of Units (S1) or inch-poundunits (U.S.), may be used to specify characteristics (e.g. weight, dimen-

●sions). Refer to ASTME380 for guidance in using S1. However, whendifferent units of measure are available for specifying a characteristic,only one may be used. Both units of measure cannot appear in the same MSE.

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DOO-STO-35-23A(MI)9 March 1979

5. DETAILEO REQUIREMENTS

5.1 Introduction. This section provides instructions for completion ofthe SRS and references for instructions on specific requirements containedin DOD-STO-35.

5.2 MSE formats. AEDPS has a capability to prepare a six-section or asingle-section document. The six-section document appears similar to a six-section military specification. The single-section document appears similarto a military specification sheet. Specification requirements described inDOO-STD-35 are applicablemandatory that one of theSRS to create the desired

a. 0700 for

b. 0800 for

5.3 Referenced documents.referenced documents within Sections 3, 4, and 5 of-the MSE. Instructionsfor referencing documents to appear in Section 2 of the forthcoming MSE arecontained in 00D-STO-35. ●

to either of the fotmats selected. It istwo following codes and an “X” be entered on theMSE format:

a six-section format

a single-section format

Section 2 of the MSE mav contain a list of all

5.4 Test matrix. A test matrix is supplied as a guide for selecting doku-ments to specify tests (see table II). The test matrix presents documentsMOSt applicable for use to satisfy the statement IITE$T PER (DOC DES)!!.Any document listed in the Title Index may be used to satisfy the statement.However, the selected document from the Title Index must contain the desiredtest. Government test method documents and approved industry standards suchas ASTM test methods may also be used to satisfy the statement !!TEST PER(DOC DES]”.

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[

$

uF’-

t=+=

DOCUMENTS ~0u

V-F-106

MIL-STD-1312

MIL-F-5591

MIL-F-8490

1-

1 MIL-F-21840

I MIL-F-22978

=

MIL-F-25173

FED-STD-151

FEO-STD-191

FEO-STO-406

I ASTM4370

ASTME8

TA8LE II

—

x—

—

—

—

—

—

—

TEST MATRIX.

—

—

—

—

—

—

—

—

—

—

00D-STO-35-23A(MI)9 March 1979

—

—

—

—

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5.5 Tabulation. Instructions for tabulation are provided in DOD-STO-35.Table III pruvides codes for column headings which may be used for Fastenerscharacter sties. When different units of measure within one system (U.S. orS1) are available for specifying a characteristic, only one of the units maybe tabulated; e.g. either ounces or pounds.

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●DOD-STD-35-23A(MI)9 March 1979

TABLE III. TABULATION CANDIDATES_____________________ s

COLUMNHEADING__________

TYPE (DES)

COLUMNHEADING----- ——---

COLUMNHEADING——--------

STYLE DES

CODE----1600

1604

CODE----

16031

%605

CODE----1603

11606

CLASS DES

I SIZE (DES) FINISH DES MIN SHEARLOAD RTGPOUNDS

11607 MIN SHEARLOAD RTGNEWTONS

1608 MIN TNSLLOAD RTGPOUNDS

1609 MIN TNSLLOAD RTGNEWTONS

4905 MAX SERVTEMP RTGDEG C

4904 MIN SERVTEMP RTGDEG C

MAX WT PERUNITOUNCES

MAX WT PERUNITKILOGRAMS

5046 NOM OPERTEMP RTGDEG C

5048 NOM STORTEMP RTGDEG C

7022 7023 MAX WT PERUNITPOUNDS

7021 MAX WT PERUNITGRAMS

7024 7041 MAX WT PERIIooOUNCES

7042 MAX WT PER100POUNDS

7043 MAX WT PER%00GRAMS

NOM WT PER100POUNDS

7044 MAX WT PER100KILOGRAMS

7035 NOM WT PER100OUNCES

7036 7037 NOM WT PER100GRAMS

7038 NOM WT PERLooKILOGRAMS

6996 NOM WT PERUNITOUNCES

6997 NOM WT PERUNITPOUNDS

69’38 NOM WT PERUNITGRAMS

6999 NOM WT PERUNITKILOGRAMS

1750 THREADCALL OUT

1752 THREADDOC DES

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5.6 Keyword Code Index (KCI)and Standard Paragraphs. The KCI providescodes, to be entered on an SRS, that are unique for the type part covered bythis dash-numbered part of DOD-STD-35. The left-hand page presents the in-formation in outline form using keywords and codes. The right-hand pagepresents the words that will appear in the MSE. To find the code to beentered on the SRS, find the subject in the index at the back of this dash-numbered part. Find the keyword on the KCI and its associated code. Enter,on the SRS, the code and the characteristic value required. After the partunique characteristics have been specified, refer to DOD-STD-35 when ex-ceptions are required to Quality Assurance, Packaging, Notes, etc. Instruc-tions are in DOD-STD-35 on how to enter any type characteristic value.Appendix B, Characteristic Code Index,provides a numerical list of codesused in this dash-numbered part. This index identifies the location of codesby page number.

5.6.1 Interrelationship of codes, The interrelationship of the codes isshown b~f characteristic names on the KCI. The kindof characteristic value is shown by a colon, parentheses, period or underline.The paragraph, of which the code is a part, is shown by the standard para-graph adjacent to the code on a right-hand page. When a characteristicvalue entered with a code becomes part of the paragraph, the code is shownin the paragraph where the characteristic value will print. The MSE willcontain the exact entry as supplied with the code, except for “X” entries.

5.6.2 Automatic MSE data. Some statements, such as Altitude and Tempera-ture, will appear in the printed MSE without having to make additionalentries. These statements are linked by data base logic to characteristiccodes listed under them and will print when one of the codes listed is used.Other statements may print automatically depending on the type MSE selected.Explanations are noted on the KCI as required.

5.6.3 DOD-STD-35 Tables. The KCI of this document contains references totables in Appendix A of DOD-STO-35. Most of the tables are in preprintedform and should be reproduced, applicable data entered, and attached to theSRS for submittal. Refer to DOD-STO-35 for a general explanation in thegeneration of tables.

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KEYWORD CODE INDEX (KCI)

...CHARACTERISTIC NAME

*REQIJESTERIS NAME

*COMPANY NAME/COMMAND

*STREET/BUILDING

*CITY, STATE, ZIP

*PHONE NUMBER, INCLUDE AREA CODE, AUTOVON IFAPPLICABLE

*DATE

*REQUESTER FSCM

*CONTRACT NUMBER/OFFICE SYMBOL

*BASE DOCUMENT

*SYSTEM APPLICATION

*GOVERNMENT DESIGN ACTIVITY FSCM

*FORMAT (SELECT ONE)

SIX SECTION DOCUMENT

ONE SECTION DOCUMENT

*CONTROL (SELECT ONE)

SOURCE.

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CHAR~

0101

0102

0103

0104

0105

1003

1004

1005

2JO06

1008

6369

0700

0800

‘5i373

●


I

1’

CHAR~

0101

0102

o11o3

0104

o11o5

1003

100+

1005

11006

1008

6369

0700

0800

6873


STANDARD PARAGRA~

~.

~.

~.

~.

Q.

>J .

USER(S) FSCM(SI ~.

CONTRACT NUMBER OR OFFICE SYMBOL ~.

THE COMPLETE REQUIREMENTS FOR PROCURING THE ITEM(S)DESCRIBED HEREIN SHALL BE IN ACCORDANCE WITH THE BASEDOCUMENT(S), ~, EXCEPT AS SPECIFIED IN THIS DOCUMENT.IN THE EVENT OF CONFLICT, THIS DOCUMENT SHALL GOVERN.

SYSTEM APPLICATION ~.

GOVERNMENT DESIGN ACTIVITY FSCM ~.

SOURCE(S).

THE FOLLOWING SOURCE(S) SHOWN WITH THE PART NUMBER(S) IS/ARETHE ONLY APPROVED SOURCE(S) FOR THE ITEM(S) DESCRIBED BYTHIS DOCUMENT. IDENTIFICATION OF THE APPROVED SOURCE(S)HEREIN IS NOT TO BE CONSTRUED AS A GUARANTEE OF PRESENT OR

I

CONTINUED AVAILABILITY AS A SOURCE OF SUPPLY FOR THE ITEMDESCRIBED. I

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CHARACTERISTIC NAME

CONTROL (CONT)

SPECIFICATION.

*SOURCE TABLE

NOTE:

APERTURE

REVISION

~

NOTE :

REFER TO TABLE V

CARDS REQUIRED.

OF AEDPS DOCUMENT

OF DOD-STD–35.

(NUMBER)

THIS ENTRY IS AUTOMATIC ANDDETERMINED BY THE TITLE CODE USED.

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68?4

01107

03108

PART NUMBER

NOTE : AUTOMATIC WITH A SINGLE ITEM MSE.

NOTE : AUTOMATIC WITH A MULTI-ITEM MSE.

UNITS OF MEASURE (SELECT ONE)

Us. -

S1. ,.,

6941

6942

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●

0107

0108 ~.

SCOPE.

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CHAR~ STANDARD PARAGRAPH

6874 THE FOLLOWING SUGGESTED SOURCE(S) SHOWN WITH THEIR PARTNUMBER(SI HAVE BEEN KNOWN TO MEET THE REQUIREMENT(S) OFTHIS DOCUMENT. IDENTIFICATION OF THE, ‘SUGGESTED SOURCE(SIOF SUPPLY! HEREIN IS NOT TO BE CONSTRUED AS A GUARANTEEOF PRESENT OR CONTINUED AVAILABILITY AS A SOURCE OF SUPPLYFOR THE ITEM(S).

SCOPE. THIS DOCUMENT COVERS THE DETAILED REQUIREMENTSFOR TITLE CODE.

PART NUMBER. THE PART NuMBER FOR THE ITEM IS SUPPLIEDBY COMPUTER.

PART NUMBER. THE PART NUMBER FOR THE ITEMS IS THE SAME ASTHE NUMBER OF THIS DOCUMENT PLUS THE SUFFIX NUMBER FROMTHE TABULATED CHARACTERISTIC TABLE. REVISION AND ACTIVITYSYMBOLS ARE NOT INLCUDED IN THE PART NUMBER.

6941 UNIT OF MEASURE. ALL UNITS OFUNITS (U.S.) OR DEGREES UNLESS

MEASURE ARE IN INCH–POUNDOTHERWISE SPECIFIED.

6942 UNIT OF MEASURE. ALL UNITS OF MEASURE ARE IN INTERNATIONALSYSTEM OF UNITS (S1) OR DEGREES UNLESS OTHERWISE SPECIFIED.

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CHARACTERISTIC NAME . ,

CLASSIFICATION

IN ACCORDANCE WITH BASE DOCUMENT

~ (DESIGNATION)

~ (DESIGNATIONI

~ (DESIGNATION)

~ {DES1GNATION}

FINISH (DESIGNATION)

RATINGS

MINIMUM SHEAR LOAD RATING (SELECT ONE)

(POUNDS) I

(NEWTONS) r

MINIMUM TENSILE LOAD RATING (SELECT ONE)

[POUNDS)

(NEWTONS)

TEMPERATURE RATING

MAXIMUM SERVICE

MINIMUM SERVICE

(DEGREES CELSIUS)

(DEGREES CELSIUS)

20

1600

1601

1603

1604

1605

1606

1607

1608

11609

4905

4904



‘o

1600

1601

1603

1604

1605

1606

1607

1608

1609

4905

4904

STANDARD PARAGRAPH

CLASSIFICATION

~ TYPE ~ INAPPLY.

ACCORDANCE wITH THE BASE DOCUMENT SHALL

CLASS. CLASS ~ IN ACCORDANCE WITH THE BASE DOCUMENT SHALLAPPLY.

STYLE . STYLE Q IN ACCORDANCE WITH THE BASE DOCUMENT SHALLAPPLY.

~ SIZE ~ IN ACCORDANCE wITH THEAPPLY.

FINISH. FINISH ~ IN ACCORDANCE WITHSHALL APPLY.

RATINGS.

MINIMUM SHEAR LOAD RATING.

BASE DOCUMENT SHALL

THE BASE DOCUMENT

THE MINIMUM SHEAR LOAD RATING SHALL BE ~ POUNDS.

THE MINIMUM SHEAR LOAD RATING SHALL BE ~ NEWTONS.

MItlIMUN TENSILE LOAD RATING.

THE MINIMUM TENSILE

THE MINIMUM TENSILE

TEMPERATURE RATING.

THE MAXIMUM SERVICECELSIUS.

THE MINIMUM SERVICECELSIUS.

LOAD RATING SHALL BE ~ POUNDS.

LOAD RATING SHALL BE ~ NEWTONS.

TEMPERATURE RATING SHALL BE ~ DEGREES

TEMPERATuRE RATING SHALL BE ~ DEGREES

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DOD-STD-35-23A(MI)9 Narch 1979

KEYWORD CODE INDEX (KCII

CHARCHARACTERISTIC NAME ~

RATINGS (CONTI

TEMPERATURE RATING (CONT)

NOMINAL OPERATING (DEGREES CELSIUS) 5046

NOMINAL STORAGE (DEGREES CELSIUS) 5048

CONFIGURATION

(ILLUSTRATION

,. .?,

NUMBER), SEE APPENDIX A 1009

*UNITS (SELECT ONE)

U.S. (SELECT ONE)

INCHES.

FEET.

S1 (SELECT ONE)

\ CENTIMETERS.,.,

MILLIMETERS.

ILLUSTRATIONS

7572

75-73

7576

7577

.-.

(NUMBER I,t

NOTE:

SEE APPENDIX A .

THIS CODE IS USED TO ENTERAPPLICABLE ILLUSTRATIONS WHICHDO NOT HAVE DIMENSIONS.

4950

22


1

I/

I●

/“

I

‘oI

I,.

1.“

I

“oJ

CHAR~

5046

5048

1009

7572

7573

7576

7577

4950

DOD-STO-35-23A(MI)9 March 1979

STANDARD PARAGRAPH

THE ‘NoMINAL OPERATING TEMPERATURE RATING SHALL BE 5046DEGREES CELSIUS.

THE NOMINAL STORAGE TEMPERATURE RATING SHALL BE MDEGREES CELSIUS.

CONFIGURATION..

CONFIGURATION ILLUSTRATION(S). THE CONFIGURATION SHALL BEAS SHOWN IN ILLUSTRATION(S) ~.

ALL DIMENSIONS, UNLESSINCHES OR DEGREES.

ALL DIMENSIONS, UNLESSFEET OR DEGREES.

ALL DIMENSIONS, UNLESS

OTHERWISE SPECIFIED, SHALL BE IN

OTHERWISE SPECIFIED, SHALL BE IN

OTHERWISE SPECIFIED, SHALL BE INCENTIMETERS OR DEGREES.

ALL DIMENSIONS, UNLESS OTHERWISE SPECIFIED, SHALL BE INMILLIMETERS OR DEGREES.

ILLUSTRATION(S) . ILLUSTRATIONIS) ~ SHALL APPLY TO AIDIN THE DEFINITION OF PARAMETERS.

23



●KEYWORD CODE INDEX (KCI)

CHARCHARACTERISTIC NAME g

TABULATED CHARACTERISTICS (SEE TABLE IV, DOD–STD-35)

MATERIALS (SEE TABLES VI AND VII, DOD-STD-35)

NOTE : AUTOMATIC WHEN TABLE vII IS USED...

FINISHES (SEE TABLES VIII AND IX, DOD-STD-35).

NOTE : AUTOMATIC WHEN TABLE IX IS USED.

METALS

DISSIMILAR METALS.

DESIGN AND CONSTRUCTION

HOOK TAPE (FASTENER TAPE)

PER BASE DOCUMENT EXCEPT

HOOK TAPE CONSTRUCTION AS FOLLOWS:

YARN DIAMETER (SELECT ONEI

(INCH)

[MILLIMETER)

7580

%582

3000

3002

3004

24


II

●DOO-STD-35-23A(MI)9 Narch 1979

.

t)

‘o


MATERIALS). MATERIALS) SHALL BE AS SPECIFIED IN THEMATERIAL TABLE. (NOTE: THE COMPONENT REFERENCE NUMBER(S)ARE ONLY TO REFERENCE THE SAME COMPONENT WHEN TABLECONTINUATION IS NECESSARY.)

FINISH(S). FINISH(S) SHALL BE AS SPECIFIED IN THE FINISHTABLE. (NOTE: THE COMPONENT REFERENCE NUMBER(S) ARE TOREFERENCE THE SAME COMPONENT WHEN TABLE CONTINUATION ISNECESSARY.)

7580 METALS. ALL METALS, WHEN USED, (UNLESS OTHERWISE SPECIFIEDHEREIN) SHALL BE CORROSION-RESISTANT TYPES OR TREATED TORESIST CORROSION. DISSIMILAR METALS SHALL NOT BE USED ININTIMATE CONTACT WITH EACH OTHER UNLESS SUITABLY FINISHEDTO RESIST ELECTROLYTIC CORROSION. CURRENT CARRYING PARTS(WHERE APPLICABLE) SHALL BE NONFERROUS, EXCEPT FOR TERMINALSFORMING PART OF A METAL-TO-GLASS SEAL.

DESIGN AND CONSTRUCTION.

1582 HDfYk TAPE. THE.CONSTRUCTIONBASE DOCUMENT, EXCEPT ~.

3000 HOOK TAPE. THE CONSTRUCTION

SHALL BE IN ACCORDANCE WITH THE

SHALL BE AS FOLLOWS:

3002 THE YARN DIAMETER SHALL BE ~ INCH.

3004 THE YARN DIAMETER SHALL BE ~ MILLIMETER.

25

I



KEYWORD CODE INDEX (KCII

CHARACTERISTIC NAME

DESIGN AND CONSTRUCTION (CONT)

HOOK TAPE CONSTRUCTION AS FOLLOWS: (CONT)

MAXIMUM SELVAGE WIDTH (SELECT ONEI

(INCHES)

(MILLIMETERS)

HOOKS PER LINEAR LENGTH (SELECT I

INCH (QUANTITY OF HOOKS)

MILLIMETER (QUANTITY OF HOOKS

PICKS PER LINEAR LENGTH OF TAPE

INCH (QUANTITY OF PICKS)

NE) “

SELECT ONE)

MILLIMETER (QUANTITY OF PICKS)

GROUND ENDS PER TAPE (QUANTITY)

HOOK ENDS PER TAPE (QUANTITY)

HOOK REPETITION, PICKS BETWEEN HOOKS(QUANTITY)

PILE TAPE (FASTENER TAPE)


PER TAPE “CONSTRUCTION AS

26

FOLLOWS:

CHARg

3006

3007

3008

3010

30112

3014

3016

3018

3020

.,

1602

3030




3006 THE MAXIMUM SELVAGE WIDTH SHALL BE ~ INCH(S).

3007 THE MAXIMUM SELVAGE WIDTH SHALL BE ~ MILLIMETER(S).

3008 THERE SHALL BE 3008 HOOKS PER LINEAR INCH OF TAPE.

30JJ0 THERE SHALL. BE ~ HOOKS PER LINEAR MILLIMETER OF TAPE.

30112 THERE SHALL BE ~ PICKS PER LINEAR INCH OF TAPE.

3014 THERE SHALL BE ~ PICKS PER LINEAR MILLIMETER OF TAPE.

3016 THERE SHALL BE ~ GROUND ENDS PER TAPE.

3018 THERE SHALL BE & HOOK ENDS PER TAPE.

3020 HOOK REPETITION (NUMBER OF PICKS BETWEEN HOOKS) SHALLBE 3020.

1602 PILE TAPE. THE CONSTRUCTION SHALL BE IN ACCORDANCE WITHTHE BASE DOCUMENT, EXCEPT ~. ~

3030 PILE TAPE. THE CONSTRUCTION SHALL BE AS FOLLOWS:

Ip

27

I




CHARACTERISTIC NAME


PER TAPE CONSTRUCTION AS FOLLOWS: (CONT)

YARN DIAMETER (SELECT ONE)

(INCHI

(MILLIMETER)

MAXIMUM SELVAGE WIDTH (SELECT oNE)

(INCHES)

(MILLIMETERS)

PICKS PER LINEAR LENGTH OF TAPE (SELECT ONE)

INCH (QUANTITY OF PICKS)

MILLIMETER (QUANTITY OF PICKS)

GROUND ENDS PER TAPE (QUANTITY)

PILE ENDS PER TAPE (QUANTITY)

LOOP REPETITION, PICKS BETWEEN LOOPS(QuANTITY)

SLIDE FASTENER’ TAPE CONSTRUCTION

PER BASE DOCUMENT

PER V–F–106.

EXCEPT

3032

3034

3036

3038

3040

3042

3044

3046

3048

%6%2

>614

●

(

28


I●DOD-STD-35-23A(MI)9 March 1979

●

CHARg

3032

3034

3036

3038

3040

3042

3044

3046

3048

1612

1614

STANDARD PARAGRAPH

THE YARN DIAMETER SHALL BE 3032 INCH.

THE YARN DIAMETER SHALL BE 3034 MILLIMETER.

THE MAXIMUM SELVAGE WIDTH SHALL BE ~ INCH(S).

THE MAXIMUM 5ELVAGE WIDTH SHALL BE ~ MILLIMETER(5).

THERE SHALL BE ~ PICKS PER LINEAR INCH OF TAPE.

THERE SHALL BE ~ PICKS PER LINEAR MILLIMETER OF TAPE..

THERE SHALL BE ~ GROUND ENDS PER TAPE.

THERE SHALL BE ~ PILE ENDS PER TAPE.

LOOP REPETITION (NUMBER OF PICKS BETWEEN LOOPS) SHALLBE ~.

SLIDE FASTENER TAPE CONSTRUCTION. THE REQUIREMENT(S) SHALLBE IN ACCORDANCE WITH THE BASE DOCUMENT, EXCEPT 1612.

SLIDE FASTENER TAPE CONSTRUCTION. THE SLIDE FASTENER TAPECONSTRUCTION SHALL BE IN ACCOrdanCe WITH v–F-106.

29



KEYWORD CODE INDEX (KCI”)

CHARACTERISTIC NAME


PER V–F-106 (CONT)

WATER RESISTANT TREATED.

MILDEW RESISTANT TREATED.

SLIDE FASTENER TYPE (SELECT ONE)

NONSEPARATING

NONREVERSIBLE.

NONREVERSIBLE, CURVED.

REVERSIBLE.

SEPARATING

NONREVERSIBLE.

REVERSIBLE.

SLIDE FASTENER SIZE

PER V–F–106 (ABBREVIATION)

HEAD -FLUSHNESS

MAXIMUM DEVIATION FROM FLUSHNESS WITH PANEL

(INCH)

(MILLIMETER)

30

1616

l161J8

11620

1622

1624

1626

1628

1630

●

1640

1642



1-1I

10

CHARCODE STANDARD PARAGRAPH

1616

IJ618

1620

1622

1624

11626

1628

11630

1640

1642

THE SLIDE FASTENER TAPE SHALL BE WATER RESISTANT TREATED.

THE SLIDE FASTENER TAPE SHALL BE MILDEW RESISTANT TREATED.

SLIDE FASTENER TYPE.

THE FASTENER SHALL BE THE NONSEPARATING,

THE FASTENER SHALL BE THE NONSEPARATING,CURVED TYPE.

THE FASTENER SHALL BE THE NONSEPARATING,

THE FASTENER SHALL BE THE SEPARATING,

NONREVERSIBLE TYPE.

NONREVERSIBLE

REVERSIBLE TYPE.

NONREVERSIBLE TYPE.

THE FASTENER SHALL BE THE SEPARATING, REVERSIBLE TYPE.

SLIDE FASTENER SIZE. SIZE ~ IN ACCORDANCE WITH V-F-lIO6SHALL APPLY.

HEAD FLUSHNESS.

THE MAXIMUM DEVIATION THE STUD HEAD SHALL RECEDE OR PROTRUDEFROM THE PANEL SURFACE SHALL BE 1640 INCH.

THE MAXIMUM DEVIATION THE STUD HEAD SHALL RECEDE OR PROTRUDEFROM THE PANEL SURFACE SHALL BE 1642 MILLIMETER.

<

31

II




CHARACTERISTIC NAME


HEAD KNURL

TYPE (SELECT ONE)

SPIRAL.

DIAMOND.

90 DEGREE V.

CLASS (SELECT ONE)

FINE.

MEDIUM.

COARSE .

LOCKING

,CLOCKWISE ROTATION OF STUD, VIEWEDFROM HEAD END

MINIMUM (DEGREES)

MAXIMUM [DEGREES)

MALE COMPONENT SHALL TIGHTEN BYIN CLOCKWISE DIRECTION AND LOCK

LOCKED POSITION (SELECT ONE)

MAXIMUM TURN TO LOcK (DEGREES)

1646

1648

1650

1652

1654

1656

● ❉

1660

IJ662

TURNINGuPON RELEASE. 3.1664

1670

32


I

●

‘o

1646

1648

11650

1652

%654

1656

1660


STANDARD PARAGRAPH

HEAD KNURL.

HEAD KNURL SHALL BE THE SPIRAL TYPE.

HEAD KNURL SHALL BE THE DIAMOND TYPE.

HEAD KNURL SHALL BE THE 90 DEGREE V TYPE.

HEAD KNURL SHALL BE FINE CLASS.

HEAD KNURL SHALL BE MEDIUM CLASS.

HEAD KNURL SHALL BE COARSE CLASS.

LOCKING.

THE MINIMUM CLOCKWISE ROTATION OF ~ DEGREES SHALL BEREQUIRED TO POSITIVELY LOCK THE FASTENER WHEN VIEWEDFROM THE STUD END.

1662 THE MAXIMUM CLOCKWISE ROTATION OF ~ DEGREES SHALL BEREQUIRED TO POSITIVELY LOCK THE FASTENER WHEN VIEWED FROMTHE STUD END.

1664 THE MALE COMPONENTDIRECTION AND LOCK

LOCKED POSITION.

SHALL TIGHTEN BY TURNING IN THE CLOCKWISEUPON RELEASE.

1670 THE MAXIMUM TURN TO LOCK THE MALE COMPONENT SHALL BE wDEGREES.



KEYWORD CODE INDEX (KcI)

CHARACTERISTIC NAME


LOCKED POSITION (CONT)

SCREWDRIVER SLOT

ALIGNMENT WITH FASTENER ATTACHMENT RIVETS. 1672

RIGHT ANGLE WITH ATTACHMENT RIVETS. 1674

LOCKED AND UNLOCKED MARKINGS PROVISION. 1676

UNLOCKING

COUNTERCLOCKWISEFROM STUD END

ROTATION OF STUD, VIEWED

MINIMuM (DEGREES) 1680

MAXIMUM (DEGREES) 1682

MALE COMPONENT SHALL UNLOCK BY PUSHINGAND TURNING IN A COUNTERCLOCKWISE DIRECTION. %683

MALE COMPONENT SHALL UNLOCK BY PULLING ANDTURNING IN A COUNTERCLOCKWISE DIRECTION. 1684

ENGAGING OF STUD TO RECEPTACLE

CLOCKWISE

MINIMuM (DEGREES) L690

34

&

‘1‘1


II

1,.

DoD-.sTD-35=z3mMIr9 March 1979


1672 THE SCREWDRIVER SHALL BE IN ALIGNMENT WITH THE ATTACHMENTRIVETS WHEN IN THE LOCKED POSITION.

1674 THE SCREWDRIVER SHALL BE IN AT A RIGHT ANGLE WITH THEATTACHMENT RIVETS WHEN IN THE LOCKED POSITION.

1676 THE LOCKED AND UNLOCKED POSITIONS SHALL BE CLEARLY ANDPERMANENTLY

UNLOCKING.

L680 THE MINIMUMBE REQUIRED

1682 THE ,MAXIMUMBE REQUIRED

MARKED ON THE FASTENER.

COUNTERCLOCKWISE ROTATION OF ~ DEGREES SHALLTO UNLOCK THE STUD WHEN VIEWED FROM THE STUD END.

COUNTERCLOCKWISE ROTATION OF ~ DEGREES SHALLTO UNLOCK THE STUD WHEN VIEWED FROM THE STUD END.

IJ683 THE MALE COMPONENT SHALL UNLOCKCOUNTERCLOCKWISE DIRECTION.

1684 THE MALE COMPONENT SHALL UNLOCKCOUNTERCLOCKWISE DIRECTION.

ENGAGING OF STUD TO RECEPTACLE.

BY PUSHING AND TURNING IN A

BY PULLING AND TURNING IN A

I1690 THE MINIMUM CLOCKWISE ROTATION OF ~ DEGREES SHALL BE

REQUIRED FOR THE STUD TO ENGAGE THE RECEPTACLE.

!●

35

L


DOD>23A(.MI.).=.9 March 1979 ‘=-

1

.0KEYWORD CODE INDEX (KCI)

CHARACTERISTIC NAME


CLOCKWISE (CONT)

MAXIMUM (DEGREES)

COUNTERCLOCKWISE

MINIMUM (DEGREES)

MAXIMUM (DEGREES)

POSITIVE STOP

PROVIDED.

FASTENER INSTALLATION

PER MANUFACTURERS INSTRUCTION.

REPLACEMENT WITH SIMPLE HAND TOOLS.

MAXIMUM SHEET SEPARATION (SELECT ONE)

(INCHES)

(MILLIMETERs)

36

11692

1693

1694

1696

L702

1706

%7%0,,

1712


●DOO-STO-35-23A(MI)9 March 1979

1-1

I

I.0

1692

IJ693

1694

1696

1702

1706

1710

17%2

STANDARD PARAGRAPH

THE MAXIMUM CLOCKWISEREQUIRED FOR THE STUD

ROTATION OF ~ DEGREES SHALL BETO ENGAGE THE RECEPTACLE.

THE MINIMUM COUNTERCLOCKWISE ROTATION OF ~ DEGREES SHALLBE REQUIRED FOR THE STUD TO ENGAGE THE RECEPTACLE.

THE MAXIMUM COUNTERCLOCKWISE ROTATION OF ~ DEGREES SHALLBE REQUIRED FOR THE STUD TO ENGAGE THE RECEPTACLE.

POSITIVE STOP. A POSITIVE STOP SHALL BE PROVIDED TO PREVENTTHE STUD FROM PASSING THE FULL LOCK POSITION.

FASTENER INSTALLATION.

INSTALLATION SHALL BE IN ACCORDANCE WITH THE MANUFACTURER’sINSTRUCTIONS.

REPLACEMENT OF FASTENER SHALL BE PERFORMED WITH SIMPLE HANDTOOLS.

MAXIMUM SHEET SEPARATION.

WHEN THE FASTENER ISTO MAxIMUM OPERATINGBE ~ INCHES.

WHEN THE FASTENER ISTO MAxIMUM OPERATINGBE ~ MILLIMETERS.

INSTALLED, FASTENED, LOCKED OR LOADEDLOAD THE MAXIMUM SHEET SEPARATION SHALL

INSTALLED, FASTENED, LOCKED OR LOADEDLOAD THE MAXIMUM SHEET SEPARATION SHALL

37




CHARACTERISTIC NAME


INTERCHANGEABILITY (SELECT ONEI

SAME Manufacturers PART NUMBER.

SLIDE FASTENER -

FLOATING RECEPTACLE

SAME SIZE AND MANUFACTURE.

MINIMUM LATERAL MOVEMENT (SELEcT ONE)

[INCHES)

(MILLIMETERS)

SURFACE TEXTURE

MAxIMuM fi0uGHNEs5, ARITHMETIcAL AVERAGE

MACHINED SURFACE (SELECT ONEI

(MICROINCHES)

(MICROMETERS)

FAYING SURFACE (SELECT ONE)

(MICROINCHES)

38

CHARCODE

31-120

1-/22

3!730\

0’

1732

1740

1741

3742

I



I

CHARCODE

1720

1722

1730

1732

%740

L741

1742

STANDARD PARAGRAPH

INTERCHANGEABILITY.

PARTS HAVING THE SAME MANUFACTURERVi PART NUMBER SHALL BEINTERCHANGEABLE WITHOUT DEGRADATION OF PERFORMANCE OR EASEOF INSTALLATION.

AN INTERCHANGEABLE SLIDE FASTENER SHALL BE A SEPARATING TYPEWHICH IS SO CONSTRUCTED THAT WHEN THE TWO STRINGERS OF THECHAIN ARE SEPARATED, EACH STRINGER CAN BE JOINED ANDOPERATED WITH THE OPPOSING STRINGER OF OTHER FASTENERSOF THE SAME SIZE AND MANUFACTURE.

FLOATING RECEPTACLE.

THE MINIMUM LATERAL MOVEMENT OF THE RECEPTACLE FROM THENORMAL CENTERLINE OF THE STUD AXIS SHALL BE ~ INCHES.

THE MINIMUM LATERAL MOVEMENT OF THE RECEPTACLE FROM THENORMAL CENTERLINE OF THE STUD AXIS SHALL BE ~ MILLIMETERS.

SURFACE TEXTURE.

THE MAXIMUM SURFACE ROUGHNESS (ARITHMETICAL AVERAGE) OF THEMACHINED SURFACE SHALL BE ~ MICROINCHES.

THE MAXIMUM SURFACE ROUGHNESS (ARITHMETICAL AVERAGE) OF THEMACHINED SURFACE SHALL BE 1741 MICROMETERS.

THE MAXIMUM SURFACE ROUGHNESS (ARITHMETICAL AVERAGE) OF THEFAYING SURFACE SHALL BE ~ MICROINCHES.

!

p39



KEYWORD CODE INDEx (KcI)(

. CHARCHARACTERISTIC NAME ~ I

1DESIGN AND CONSTRUCTION (CONT) ~

.FAyING SURFACE (CONT)I

(MICROMETERS)

MAXIMUM WAVINESS

MACHINED SURFACE

(INCHES)

(MILLIMETERs)

(SELECT ONE)

1744

11745

FAYING SURFACE (SELECT ONE)

(INCHES)

(MILLIMETERS)

SCREW THREADS

THREAD CALLOUT (DESIGNATION)

PER DOCUMENT (DOC DES)

MAXIMUM LONGITUDINAL SHRINKAGE

HOOK TAPE (PERCENT)

PILE TAPE (PERcENT)

TAPE ENDS, ANTI-RAVELING TREATMENT

COATED.

40

1746

1747

1750

1752

%760

11762

1770

1

.,

s,..

‘i

,

1

●“;:,l,.

;1



I

1’

i.


1743 THE MAXIMUM SURFACE ROUGHNESS (ARITHMETICAL AVERAGE) OFTHE FAYING SURFACE SHALL BE ~ MICROMETERS.

1744

17+5

1746

1747

1750

1752

11760

L762

11770

THE MAXIMUM WAVINESS OF THEINCHES.

THE MAXIMUM WAVINESS OF THEMILLIMETERS.

THE MAXIMUM WAVINESS OF THEINCHES.

THE MAXIMUM WAVINESS OF THEMILLIMETERS.

SCREW THREADS.

MACHINED SURFACE SHALL BE ~

MACHINED SURFACE SHALL BE ~

FAYING SURFACE SHALL BE ~

FAYING SURFACE SHALL BE 1747

THE THREAD(S) SHALL BE ~.

SCREW THREADS SHALL BE IN ACCORDANCE WITH 11752.

MAXIMUM LONGITUDINAL SHRINKAGE.

HOOK TAPE LONGITUDINAL SHRINKAGE SHALL BE NOT GREATER THAN~ PERCENT.

PILE TAPE LONGITUDINAL .SHRINKAGE SHALL BE NOT GREATER THAN~ PERCENT.

TAPE ENDS, ANTI-RAVELING TREATMENT.

TAPE ENDS SHALL BE COATED TO PREVENT RAvELING OR FRAYING.

41



KEYWORD CODE INDEx (KcI)0

CHARACTERISTIC NAME


TAPE ENDS, ANTI-RAVELING TREATMENT (CONT)

IMPREGNATED.

PINKED.

FABRIC COLOR

COLOR (NAME)

PER FED-STD-595’ (NUMBER)

PER OTHER _

HAND OF SEPARATING UNIT (SELECT ONE)

SLIDE FASTENER, RIGHT HAND.

SLIDE FASTENER, LEFT HAND.

SPECIAL TOOLS

NOT REQUIRED.

REQUIRED:

FURN15HE,Q BY SUPPLIER.

42

●

CHARCODE

1772

L7T4

1776

1778

1782

1790

1792

>794

1796

1798

o

.


I

‘oDOO-STD-35-23A(MI)9 March 1979

1-1


1772

177+

31776

1778

1782

1790

1792

1794

1796

1798

TAPE ENDS SHALL

TAPE ENDS SHALL

FABRIC COLOR.

BE

BE

IMPREGNATED TO PREVENT RAVELING OR FRAYING.

PINKED TO PREVENT RAVELING OR FRAYING.

THE FABRIC COLOR SHALL BE 1776.

THE FABRIC COLOR SHALL BE NUMBER ~ IN ACCORDANCE WITHFED–STD-595.

THE COLOR SHALL BE 1782.

HAND OF SEPARATING UNIT.

THE SEPARATING UNIT OF THE SLIDE FASTENER SHALL BERIGHT-HAND.

THE separating UNIT OF THE SLIDE FASTENER SHALL BELEFT–HAND.

SPECIAL TOOLS.

SPECIAL TOOLS FOR INSTALLATION OR OPERATION OF THE FASTENERARE NOT REQUIRED.

SPECIAL TOOLS FOR INSTALLATION OR OPERATION OF THE FASTENERARE REQUIRED.

SPECIAL TOOLS FOR INSTALLATION, OPERATION, REMOVAL ORREPLACEMENT SHALL BE FURNISHED BY THE SUPPLIER.

43


DOD-STD-35-23A(MI) ,9 March 1979 ~~


CHARACTERISTIC NAME


WEIGHT/MASS

MAXIMUM wEIGHT/MAss pER UNIT (sELEcT ONE)

U.S. [SELECT ONE)

[OUNCES)

(POUNDS)

S1 (SELECT ONE)

(GRAMS)

(KILOGRAMS)

MAXIMUM WEIGHT/MASS

U.S. (SELECT ONE)

(OUNCES)

[POUNDSI

S1 (SELECT ONE)

(GRAMS)

(KILOGRAMS)

7022

7023

7021

7024

PER 1100 (SELECT ONE)

7041

7042

7043

7044

44

-


o00D-STD-35-23A(MI)9 March 1979

,.

I

‘0


7022

7023

7021

7024

7041

7042

7043

7044

MAxIMUM WEIGHT PER UNIT. THE WEIGHT PER UNIT SHALL BENOT GREATER THAN ~ OUNCE(S).

P.AXIMUM WEIGHT PER UNIT. THE WEIGHT PER UNIT SHALL BENOT GREATER THAN ~ POUND(S).

MAXIMUM MASS PER UNIT. THE MASS PER UNIT 5HALL BENOT GREATER THAN 7021 GRAM(S).

MAXIMUM MASS PER UNIT. THE MASS PER UNIT SHALL BENOT GREATER THAN 7024 KILOGRAM(S).

MAXIMUM WEIGHT PER LOO. THE WEIGHT PER 100 UNITS SHALL BENOT GREATER THAN ~ OUNCE(S).

MAXIMUM WEIGHT PER 100. THE WEIGHT PER IJOO UNITS SHALL BENOT GREATER THAN ~ POUND(S).

MAXIMUM MASS PER 100. THE MASS PER 100 UNITS SHALL BENOT GREATER THAN @ GRAM(S).

MAXIMUM MA5s PER 100. THE MASS PER 1100 UNITS SHALL BENOT GREATER THAN 7044 KILOGRAM(S).

45



KEYWORD CODE INDEX (KC1)

CHARACTERISTIC NAME


WEIGHT/MASS (cONT)

NOMINAL WEIGHT/MASS PER UNIT (SELECT ONE)

us. (sELEcT oNE)

(OUNCES)

(POUNDS)

S1 (SELECT ONE)

(GRAMs)

(KILoGRAM5)

NOMINAL WEIGHT/MASS

us. (5ELECT oNE)

(0uNcE51

(POUNDS)

S1 (SELECT ONE)

[ GRAMS)

(KILOGRAMS):,

PER 100 (sELEcT ONE)

46

6996 .

6997

6998 ●l

6999

7035

7036

7037 :

7038 4

1?

●1,/,\

,;

I


oDOD-STD-35-23A(MI)9 March 1979

CHARg

6996

6997

6998

6999

7035

7036

7037

7038

STANDARD PARAGRAPH

fJOMINAL WEIGHT PER UNIT. THE WEIGHT PER UNIT SHALL BE6996 OUNCE(S).

NOMINAL WEIGHT PER UNIT. THE WEIGHT PER UNIT SHALL BE6997 POUND(S).

NOMINAL MASS PER UNIT.6998 GRAM(S).

NOMINAL MASS PER UNIT.6999 KILOGRAM(S).

THE MASS PER UNIT SHALL BE

THE MASS PER.UNITLSHALL BE

NOMINAL WEIGHT PER 300. THE HEIGHT PER 100 UNITS SHALL BE7035 OUNCE(S).

NOMINAL WEIGHT PER 100. THE WEIGHT PER 100 UNITS SHALL BE7036 POUND(S).

NOMINAL MASS PER 1100. THE MASS PER 100 UNITS SHALL BE~ GRAM(S).

NOMINAL MASS PER 100. THE MASS PER 100 UNITS SHALL BE~ KILOGRAM(S).

47





CHAIN UNIFORMITY

REQUIREMENTS (SELECT ONE),

PER BASE DOCUMENT EXCEPT _ 1812

AS FOLLOWS: 1813

CHAIN CENTER LINE DEVIATIONFROM STRAIGHT LINE (SELECT ONE)

MAXIMUM (INCH)*LENGTH OVER WHICH DEVIATION IS MEASURED 1834

(INCHES) 1816

MAXIMUM (MILLIMETERS)*LENGTH OVER WHICH DEVIATION IS MEASURED 1815

(MILLIMETERS) 1817

CURVED FASTENER RADIUS SHALL CONFORM TOSPECIFIED DIMENSIONS. 1818

TEST METHODS (SELECT

PER BASE DOCUMENT

PER ASTMD2060

ONE)

EXCEPT _

MEASURE CURVED CHAIN RADIuS TODETERMINE CONFORMANCE TO LIMITS.

1802

IJ804

3!806

48


,

,0DOO-STD-35-23A(MI)9 March 1979

)

.’

1“I10

L


1806

CHAIN UNIFORMITY. THE REQUIREMENT(S)WITH THE BASE DOCUMENT, EXCEPT ~.

CHAIN UNIFORMITY. HE REQUIREMENT(S)

SHALL BE IN ACCORDANCE

SHALL BE AS FOLLOWS:

THE CHAINSURFACE.THAN ~

THE CHAINSURFACE.THAN ~

THE CHAIN

WHEN MEASURED SHALL LIE FLAT ON A HORIZONTALCHAIN CENTERLINE DEVIATION SHALL NOT BE GREATERINCHES IN = INCHES OF LENGTH.

WHEN MEASURED SHALL LIE FLAT ON A HORIZONTALCHAIN CENTERLINE DEVIATION SHALL NOT BE GREATERMILLIMETERS IN ~ MILLIMETERS OF LENGTH.

OF THE CURVED FASTENER, WITHOUT TENSION SHALL LIEFLAT ON THE HORIZONTAL SURFACE. THE RADIUS OF THE CHAINCENTERLINE SHALL CONFORM TO SPECIFIED DIMENSIONS.

CHAIN UNIFORMITY. TESTING SHALL BE PERFORMED IN ACCORDANCEWITH THE BASE DOCUMENT, EXCEPT ~.

CHAIN UNIFORMITY. TESTING SHALL BE PERFORMED IN ACCORDANCEWITH ASTMD2060.

MEASURE CURVED CHAIN RADIUS AND DETERMINE CONFORMANCE TOSPECIFIED LIMITS.

49



KEYWORD CODE INDEX

CHARACTERISTIC NAME

CHAIN WAVINESS (SLIDE FASTENERS)

REQUIREMENTS (SELECT

PER BASE DOCUMENT

NO.,WAVINESS.


PER.BASE DOCUMENT

PER ASTMD2060.

CLEANLINESS

REQUIREMENTS .(SELECT

PER BASE DOCUMENT

AS FOLLOWS:

ONE )

EXCEPT _

ONE )

EXCEPT _

ONE )

EXCEPT

KCI)

4

IJ828

1830

1822

1824

“1I

● ,

PER MIL-STD–1246 (CLEANLINESS LEVEL)

PER MIL-S-23192.

TEST METHODS (SELECT ONE)

PER BASE DOCUMENT EXCEPT _

PER MIL–STD-186

(PROCEDUREI

2202

2203

2204

2206

21192

2194

21196

50



G-1ARSTANDARD PARAGRAPH

.

1’).

.

io

II

1.

I

i●

I

1828

%830

1822

1824

2202

2203

2204

2206

2192

2194

21196

CHAIN WAVINESS. THE REQUIREMENT(S) SHALL BE IN ACCORDANCEWITH THE BASE DOCUMENT, EXCEPT ~.

CHAIN WAVINESS. THE CHAIN SHALL LIE FLAT WITHOUT WAVINESS.

CHAIN WAVINESS. TESTING SHALL BE PERFORMED IN ACCORDANCEWITH THE BASE DOCUMENT, EXCEPT ~.

CHAIN WAVINESS. TESTING SHALL BE PERFORMED IN ACCORDANCEWITH ASTMD2060.

CLEANLINESS. THE REQUIREMENT(S) SHALL BE IN ACCORDANCE WITHTHE BASE DOCUMENT, EXCEPT ~.

CLEANLINESS. THE REQUIREMENT(S) SHALL BE AS FOLLOWS:

CLEANLINESS LEVEL ~ IN ACCORDANCE WITH MIL-STD-1246SHALL APPLY.

CLEANLINESS REQUIREMENTS IN ACCORDANCE WITH MIL-S-23J92SHALL APPLY.

CLEANLINESS. TESTING SHALL BE PERFORMED IN ACCORDANCE WITHTHE BASE DOCUMENT, EXCEPT ~.

CLEANLINESS. TESTING SHALL BE PERFORMED IN ACCORDANCE WITHMIL-STD-L86.

THE CLEANING PROCEDURE SHALL BE 2196.

51




CHARACTERISTIC NAME

CLEANLINESS (CONT)

PER MIL-STD-186. (CONT)

CLEANING MATERIAL (SPECIFY)

CLINCH FORCE

REQUIREMENTS (SELECT ONE)


MINIMUM CLINCH FORCE (SELECT ONE)

(PouNDS)

(NEWTONS)


PER BASE DOCUMENT

PER MIL-F–43514.

COLORFASTNESS


PER BASE DOCUMENT

AS FOLLOWS:

ONE )

EXCEPT _

ONE )

EXCEPT _

NO DULLING OR FADING.

DULLING OR FADING PERMITTED.

●

CHAR

.

21198

2348

2350

2352

2342

2344

2066

2069

2071

2072

52



,,


2198

2348

2350

2352

2342

2344

2068

2069

207%

2072

THE CLEANING MATERIAL SHALL BE ~.

CLINCH FORCE.WITH THE BASE

THE REQUIREMENT(S) SHALL BE IN ACCORDANCEDOCUMENT, EXCEPT ‘~.

CLINCH FORCE. THE FASTENER SHALL WITHSTAND A CLINCH FORCEOF NOT LESS THAN 2350 POUNDS.

CLINCH FORCE. THE FASTENER SHALL WITHSTAND A CLINCH FORCE ,OF NOT LESS THAN ~ NEWTONS.

CLINCH FORCE. TESTING SHALL BE PERFORMED IN ACCORDANCE WITHTHE BASE DOCUMENT, EXCEPT ~.

CLINCH FORCE. TESTING SHALL BE PERFORMED IN ACCORDANCE WITHMIL–F-43514.

COLORFASTNESS. THE REQUIREMENT(S) SHALL BE IN ACCORDANCEWITH THE BASE DOCUMENT, EXCEPT ~.

COLORFASTNESS. THE REQUIREMENT(S) SHALL BE AS FOLLOWS:

THERE SHALL BE NO DULLING OR FADING OF THE COLOR.

DULLING OR FADING OF THE COLOR IS PERMISSIBLE.

53





COLORFASTNESS (CONT)

AS FOLLOWS: (CONT)

DULLING OR FADING PER STANDARD SAMPLE, 2074


PER BASE DOCUMENT

PER FED-STD-191.

ONE )

EXCEPT —’. 2052

2053

METHOD (NUMBER) 2054

DECARBURIZATION


PER BASE DOCUMENT EXCEPT _ 2%08

AS FOLLOWS: ,, 2109

MAXIMUM DEPTH (SELECT. ONE)

(INCHES) 2110

(MILLIMETERS) 2111

/ MAXIMUM LIMITS OF MIL-H-6875c 2112



54●


?

,,

I



2074 DULLING OR FADING SHALL BE IN ACCORDANCE WITH THE STANDARDSAMPLE .

2052

2053

2054

2108

2109

231110

21!llll

21112

2102

COLORFASTNESS. TESTINGWITH THE BASE DOCUMENT,

COLORFASTNESS. TESTINGWITH FED-STD-L9L.

TEST METHOD NUMBER ~

SHALL BE PERFORMEDEXCEPT ~.

SHALL BE PERFORMED

SHALL APPLY.

IN ACCORDANCE

IN ACCORDANCE

DECARBURIZATION. THE REQUIREMENT(S) SHALLWITH THE BASE DOCUMENT, EXCEPT ~.

DECARBURIZATION. THE REQUIREMENT(S) SHALL

DECARBURIZATION DEPTH SHALL BE NOT GREATER

DECARBURIZATION DEPTH SHALL BE NOT GREATERMILLIMETERS.

MAXIMUM DECARBURIZATION LIMITS SHALL BE INMIL–H-6875.

BE IN ACCORDANCE

BE AS FOLLOWS:

THAN ~ INCHES.

THAN ~

ACCORDANCE WITH

DECARBURIZATION. TESTING SHALL BE PERFORMED IN ACCORDANCEWITH THE BASE DOCUMENT, EXCEPT ~.

55




CHARACTERISTIC NAME

DECARBURIZATION (CONT)

TEST METHODS (CONT)

PER MIL–H–6875.

EMBRITTLEMENT RELIEF


PER BA5E DOCUMENT

AS FOLLOWS:

ONE )

EXCEPT _

NO EMBRITTLEMENT FROM PLATING PROCESS.

EMBRITTLEMENT RELIEF PER PLATING DOCUMENT.

EMBRITTLEMENT SHALL BE MINIMIZED.

SUPPLIER CERTIFICATION.

No’ CRACKS OR FRACTURES.




BAKING TEMPERATURE (DEGREES CELSIUS)

.,TEMPERATURE TOLERANCE (DEGREES CELSIUS)

BAKING DURATION (HOURS)

2104

2134

21J35

2137

21/39

21411

21147

2149

2122

2123

2125

2L27

21129

56



CHAR~

21J04

2134

2135

2137

21139

2141

2147

21149

2122

2123

2125

2127

2%29

STANDARD PARAGRAPH

DECARBURIZATION. TESTING SHALL BE PERFORMED IN ACCORDANCEWITH MIL–H-6875.

EMBRITTLEMENT RELIEF. THE REQUIREMENT(S) SHALL BE INACCORDANCE WITH THE BASE DOCUMENT, EXCEPT ~.

EMBRITTLEMENT RELIEF. THE REQUIREMENT(S) SHALL BE ASFOLLOWS:

THERE SHALL BE NO EMBRITTLEMENT FROM THE PLATING PROCESS.

EMBRITTLEMENT RELIEF SHALL BE IN ACCORDANCE WITH THE PLATINGDOCUMENT.

EMBRITTLEMENT OF THE PART SHALL BE MINIMIZED.

CERTIFICATION OF EMBRITTLEMENT RELIEF OF PARTS SHALL BEPROVIDED BY SUPPLIER.

THE TEST SPECIMEN SHALL NOT CRACK OR FRACTURE.

EMBRITTLEMENT RELIEF. TESTING SHALL BE PERFORMED!INACCORDANCE WITH THE BASE DOCUMENT, EXCEPT ~.

EMBRITTLEMENT RELIEF. TESTING SHALL BE PERFORMED” INACCORDANCE WITH ~.

THE BAKING TEMPERATURE SHALL BE @ DEGREES CELSIUS.

THE TEMPERATURE TOLERANCE SHALL BE ~ DEGREES CELSIUS.

THE DURATION OF TEST SHALL BE ~ HOURS.

57




CHARACTERISTIC NAME

ENDURANCE


PER BASE DOCUMENT

AS FOLLOWS:

NO FAILURE.

NO DEGRADATION


PER BASE DOCUMENT

PER DOCUMENT (DOC

MOUNT FASTENER

MINIMUM NUMBER

LOCKING AND

CLOSING AND

ONE)

EXCEPT

OF PERFORMANCE.

ONE)

EXCEPT _

DES)

IN TYPICAL FIXTURE.

OF TEST CYCLES (SELECT ONE)

UNLOCKING (CYCLES)

OPENING (CYCLES)

COMPLETE OPERATIONAL (CYCLES)

NOMINAL, CYCLE RATE (CYCLES PER MINUTE)

CYCLE TOLERANCE (CYCLES PER MINUTE)

SPECIMEN TEMPERATURE (DEGREES ’CELSIUS)

2472

2473

2475

2477

2442

2444

2446

2448

2450

2452 .

2454

2456

2458

58




2472 ENDURANCE. THE REQUIREMENT(S) SHALL BE IN ACCORDANCE WITHTHE BASE DOCUMENT, EXCEPT 2472.

2473 ENDURANCE. THE REQUIREMENT(S) SHALL BE AS FOLLOWS:

2475 THERE SHALL BE NO FAILURE AS A RESULT OF THE TEST.

2477 THERE SHALL BE NO DEGRADATION OF PERFORMANCE AS A RESULTOF THE TEST.

2442 ENDURANCE. TESTING SHALL BE PERFORMED IN ACCORDANCE WITHTHE BASE DOCUMENT, EXCEPT ~.

2444 ENDURANCE. TESTING SHALL BE PERFORMED IN ACCORDANCE WITH~.

2446 FASTENER SPECIMEN SHALL BE MOUNTED IN A TYPICAL TEST FIXTURE.

2448 THE NUMBER OF LOCKING AND UNLOCKING TEST CYCLES SHALL BENOT LESS THAN ~ CYCLES.

2450 THE NUMBER OF CLOSING AND OPENING TEST CYCLES SHALL BE NOTLESS THAN ~ CYCLES.

2452 THE NUMBER OF COMPLETE OPERATIONAL TEST CYCLES SHALL BE NOTLESS THAN ~ CYCLES.

2454 THE

2456 THE

2458 THE

CYCLE RATE SHALL BE ~ CYCLES PER MINUTE.

CYCLE RATE TOLERANCE

SPECIMEN TEMPERATURE

SHALL BE ~ CYCLES PER MINUTE.

SHALL BE ~ DEGREES CELSIUS.

59


I



CHARACTERISTIC NAME

ENDURANCE (CONTI

SPECIMEN TEMPERATURE (CONT)

TEMPERATURE TOLERANCE (DEGREES CELSIUS) 2460

TEST MEDIA (SELECT ONE)

AIR RELATIVE HUMIDITY (PERCENT) 2462

AIR AT AMBIENT CONDITIONS. 2464

NOMINAL WATER TEMPERATURE(DEGREES CELSIUS) 2466

TEMPERATURE TOLERANCE(DEGREES CELSIUS) “2468

FUNGUS

REQUIREMENTS (SELECT ONEI

‘.


FUNGUS RESISTANT BY CERTIFICATION OR BY TEST. 4761

NO EVIDENCE OF FUNGUS GROWTH WHEN TESTED. 4762

60


CHARCODE

i

0

2462

)2464

2466

,0 2468

4760

4761

4762


STANDARD PARAGRAPH

THE SPECIMEN TEMPERATURE TOLERANCE SHALL BE ~ DEGREESCELSIUS.

THE TEST MEDIA~ PERCENT.

THE TEST MEDIA

SHALL BE AIR AT

SHALL BE AIR AT

THE WATER TEMPERATURE

THE WATER TEMPERATURE

SHALL BE

A RELATIVE HUMIDITY

AMBIENT CONDITIONS.

OF

& DEGREES CELSIUS.

TOLERANCE SHALL BE ~ DEGREES

FUNGUS . THE REQUIREMENT(S)BASE DOCUMENT, EXCEPT ~.

CELSIUS.

SHALL BE IN ACCORDANCE WITH THE

FUNGUS . ALL EXTERNAL MATERiALS SHALL BE NONNUTRIENT TOFUNGUS GROWTH OR SHALL BE SUITABLY TREATED TO RETARD FUNGUSGROWTH . THE MANUFACTURER SHALL VERIFY BY CERTIFICATION THATALL EXTERNAL MATERIALS ARE FUNGUS RESISTANT OR SHALL PERFORMTHE FUNGUS TEST. WHEN THE FUNGUS TEST IS PERFORMED, THERESHALL BE NO EVIDENCE OF FUNGUS GROWTH ON THE EXTERNALSURFACES.

ALL EXTERNAL MATERIALS SHALL BE NONNUTRIENT TOFUNGUS .FUNGUS GROWTH OR 5HALL BE SUITABLY TREATED TO RETARD FUNGUSGROWTH . THERE SHALL BE NO EVIDENCE OF FUNGUS GROWTH ON THEEXTERNAL SURFACES.

PI

61




CHARACTERISTIC NAME

FUNGUS (CONT)


PER BASE DOCUMENT

ONE)

EXCEPT

PER MIL–STD-81O, METHOD

TEST PERIOD (DAYS)

HARDNESS


508.

PER BASE DOCUMENT EXCEpT _

HARDNESS (DESIGNATION)



PER DOCUMENT (DOC .DES)

TEST METHOD (DESIGNATION)

HUMIDITY .


PER BASE DOCUMENT EXCEPT .

NO EVIDENCE OF CORROSION OR PHYSICAL DAMAGE..

NO DEGRADATION OF PERFORMANCE.

REMAIN WITHIN SPECIFIED TOLERANCE.

4754

4755

4756

2770

2772

2780

2782

270.4

4798

4799

4815

4791

‘.

62


I

●DOD-STD-35-23A(MI)9 March 1979

CHARg

475+

4755

4756

2770

2772

2780

2782

2784

4798

4799

4815

479>

STANDARD PARAGRAPH

FUNGUS TESTING SHALL BE PERFORMED IN ACCORDANCE WITH THE-BASE DOCUMENT, EXCEPT 4=.

FUNGUS . TESTING SHALL BE PERFORMED IN ACCORDANCE WITHMETHOD 508 OF MIL–STD-810.

TEST PERIOD SHALL BE & DAY(S).

HARDNESS. THE REQUIREMENT(S) SHALL BE IN ACCORDANCE wITH,THE BASE DOCUMENT, EXCEP7 ~.

HARDNESS. THE HARDNESS OF THE ITEM SHALL 3E ~.

HARDNESS. TESTING SHALL BE PERFORMED IN ACCORDANCE WITHTHE BASE DOCUMENT, EXCEPT ~.

HARDNESS. TESTING SHALL BE PERFORMED IN ACCORDANCE WITH ~.

THE HARDNESS TEST METHOD SHALL BE ~.

HUMIDITY. THE REQUIREMENT(S) SHALL BE IN ACCORDANCE WITHTHE BASE DOCUMENT, EXCEPT ~.

HUMIDITY. THERE SHALL BE NO EVIDENCE OF CORROSION ORPHYSICAL DAMAGE.

THERE SHALL BE NO DEGRADATIONOF PERFORMANCE.

ITEM(S) SHALL REMAIN WITHIN SPECIFIED TOLERANCE.

63

I




CHARACTERISTIC NAME

HUMIDITY (CONT)’


PER BASE DOCUMENT

ONE )

EXCEPT _

PER MIL-STD-810, METHOD 507.

*PROCEDURE NUMBER (SELECT ONE)

TEST PROCEDURE I.

EXTREME TEMPERATURE BEFORE TESTING(DEGREES CELSIUS)

*DURATION OF TEMPERATUREEXPOSURE IHOURS)

TEST PROCEDURE 11.

CYCLE LIMITED TO 24 HOURS DURATION.

TEST PROCEDURE 111.

TEST PROCEDURE IV.

TEST PROCEDURE V.

NUMBER oF CYCLES (NUMBER)

WATER ‘PURITY BY CONDUCTIVITY METHOD.

OPERATION AND. MEASUREMENT AT HIGHTEMPERATURE PORTION OF CYCLE(S) (NuMBERi

CHAR~

4788

48711

4767

4777

4778

6334

4716

6335

6336

6337

4800

4764

491J6

.

64 ●


I

I



4788

487L

4767

4777

4778

6334

4736

6335

6336

6337

4800

4764

4916

HUMIDITY. TESTINGTHE BASE DOCUMENT,

SHALL BE PERFORMED IN ACCORDANCE WITHEXCEPT ~.

HUMIDITY. TESTING SHALL BE PERFORMED IN ACCORDANCE WITHMETHOD 507 OF MIL–STD–81O.

PROCEDURE NUMBER I SHALL APPLY.

SPECIMEN(S) SHALL BE EXPOSED TO ~ DEGREES CELSIUSBEFORE TESTING.

DURATION OF EXPOSURE TO EXTREME TEMPERATURE SHALL BE~ HOUR(S).

PROCEDURE NUMBER II SHALL APPLY.

CYCLES SHALL BE LIMITED TO 24 HOURS DURATION.

PROCEDURE NUMBER 111 SHALL APPLY.

PROCEDURE NUMBER IV SHALL APPLY.

PROCEDURE NUMBER V SHALL APPLY.

THERE

WATER

SHALL BE ~ CYCLE(S).

PURITY SHALL BE DETERMINED

OPERATION AND MEASUREMENTSTEMPERATURE DURING CYCLE(S’

SHALL~.

65

BY THE CONDUCTIVITY METHOD.

BE PERFORMED AT HIGH




CHARACTERISTIC NAME

HUMIDITY (CONT)

PER MIL-STD-810, METHOD 507. (CONT)

OPERATION AND MEASUREMENT AT LOWTEMPERATURE PORTION OF CYCLE(S) (NUMBER) 1554

INITIAL TENSION



MAXIMUM INITIAL TENSION

(POUNDS)

(NEWTONS)



SELECT ONE

PER DOCUMENT [DOC DES)

MATERIAL ANALYSIS



AS FOLLOWS:

SUPPLIER CERTIFICATION.



2228

2230

2232

2222

2224

38731

3873

%882

L872

.

1

66


oDOD-STD-35-23A(MI)9 March 1979

!01

I

l“’i:~‘o

CHAR~

1554

2228

2230

2232

2222

2224

%871

1873

1882

1872

STANDARD PARAGRAPH

OPERATION AND MEASUREMENTS SHALL BE PERFORMED AT LOWTEMPERATURE, DURING CYCLE(S) 1554.

INITIAL TENSION. THE REQUIREMENT(S) SHALL BE IN ACCORDANCEWITH THE BASE DOCUMENT, EXCEPT ~.

INITIAL TENSION. THE INITIAL TENSION SHALL BE NOT GREATERTHAN @ POUNDS.

INITIAL TENSION. THE INITIAL TENSION SHALL BE NOT GREATERTHAN 2232 NEWTONS.

\

INITIAL TENSION. TESTING SHALL BE PERFORMED IN ACCORDANCEWITH THE BASE DOCUMENT, EXCEPT 2222.

INITIAL TENSION. TESTING SHALL BE PERFORMED IN ACCORDANCEWITH ~.

MATERIAL ANALYSIS. THE REQUIREMENT(SI SHALL BE IN ACCORDANCEWITH THE BASE DOCUMENT, EXCEPT ~.

MATERIAL ANALYSIS. THE REQUIREMENT(S) SHALL BE AS FOLLOWS:

CERTIFICATION BY SUPPLIER THAT THE ITEM MEETS MATERIALREQUIREMENTS, IN LIEU OF A TEST.

MATERIAL ANALYSIS. TESTING SHALL BE PERFORMED IN ACCORDANCEWITH THE BASE DOCUMENT, EXCEPT 1872.

67


-.‘DOD-STD-35-23A( MI)

9 March 1979



MATERIAL ANALYSIS (CONT)

TEST METHODS [CONT)

PER DOCUMENT (DOC DES) 1878

METHOD (NUMBER) 1880

DETERMINE PRESENCE OF IRON WITH MAGNET. 1884

MILDEW RESISTANCE TREATMENT



NO EVIDENCE OF MILDEW.

TEST METHODS [SELECT ONEI


PER V-F–106

RECEPTACLE PUSH-OUT


PER’ BASE DOCUMENT EXCEPT _

NO DISENGAGEMENT OR DEFORMITY.

68

2>78

2179

2172

2174

2397

2398

:, II

0:1,!

.


1

I

I

.

CHAR~

1878

1880

1884

I

21178

21J79

2172


STANDARD PARAGRAPH

MATERIAL ANALYSIS. TESTING SHALL BE PERFORMED IN ACCORDANCEWITH ~.

THE TEST METHOD SHALL BE NUMBER ~.

DETERMINE THE PRESENCE OF IRON BY USING A MAGNET.

MILDEW RESISTANCE TREATMENT. THE REQUIREMENT(SI SHALL BEIN ACCORDANCE WITH THE BASE DOCUMENT, EXCEPT 2178.

MILDEW RESISTANCE TREATMENT. THERE SHALL BE NO EVIDENCE OFMILDEW AS A RESULT OF THE TEST.

MILDEW RESISTANCE TREATMENT. TESTING SHALL BE PERFORMED INACCORDANCE WITH THE BASE DOCUMENT, EXCEPT ~.

MILDEW RESISTANCE TREATMENT.ACCORDANCE WITH V–F–106.

TESTING SHALL BE PERFORMED IN

2397 RECEPTACLE PUSH-OUT. THE Retirement sHALL BE INACCORDANCE WITH THE BASE DOCUMENT, EXCEPT 2397.

2398 RECEPTACLE PUSH–OUT. THERE SHALL BE NO DISENGAGEMENT ORDEFORMITY OF THE STUD AS A RESULT OF TESTING.

I

I69




CHARACTERISTIC NAME

RECEPTACLE PUSH-OUT (CONT)


PER BASE DOCUMENT

PER MIL-F-22978.

ONE)

EXCEPT _

MINIMUM PUSH-OUT TEST LOAD (SELECT ONE)

[POUNDS)

(NEWTONS)

RESISTANCE TO ATTACHMENT WEAR



NO EVIDENCE OF ‘PAINT LOSS.



PER MIL–F–10884.

RESISTANCE TO BRITTLENESS



NO JAGGED FURROW EDGES.

CHAR~

2392

2394

2395

2399

2040

2042

2034

2036

2028

2030

70


●

II

I

L“

‘o

CHARg

2392

2394

2395

2399

2040

2042

2034

2036

2028

2030


STANDARD PARAGRAPH

RECEPTACLE PUSH–OUT. TESTING SHALL BE PERFORMEDACCORDANCE WITH THE BASE DOCUMENT, EXCEPT 2392.

RECEPTACLE PUSH–OUT. TESTING SHALL BE PERFORMEDACCORDANCE WITH MIL-F–22978.

IN

IN

THE PUSH-OUT TEST LOAD SHALL BE NOT LESS THAN ~ POUNDS.

THE PUSH-OUT TEST LOAD SHALL BE NOT LESS THAN ~ NEWTONS.

RESISTANCE TO ATTACHMENT WEAR. THE REQUIREMENT(S) SHALL BEIN ACCORDANCE WITH THE BASE DOCUMENT, EXCEPT ~.

RESISTANCE TO ATTACHMENT WEAR. THE FASTENER FINISH SHALLSHOW NO EVIDENCE OF PAINT LOSS.

RESISTANCE TO ATTACHMENT WEAR. TESTING SHALL BE PERFORMEDIN ACCORDANCE WITH THE BASE DOCUMENT, ExCEPT 2034.

RESISTANCE TO ATTACHMENT WEAR.IN ACCORDANCE WITH MIL-F-L0884.

TESTING SHALL BE PERFORMED

RESISTANCE TO BRITTLENESS. THE REQUIREMENT(S) SHALL BE INACCORDANCE WITH THE BASE DOCUMENT, EXCEPT ~.

RESISTANCE TO BRITTLENESS. THE FASTENER FINISH SHALL SHOWNO EVIDENCE OF BRITTLENESS SUCH AS JAGGED FURROW EDGES.

‘o 71



I● :

KEYWDRD CODE INDEX IKCI)

CHARACTERISTIC NAME

RESISTANCE TO BRITTLENESS (CONT)

TEST METHODS [SELECT

PER BASE DOCUMENT

PER MIL–F-10884.

ONE )

EXCEPT

RESISTANCE TO CHEMICAL REAGENTS



NO DAMAGE TO FINISH OR BASE MATERIAL.



PER FED–STD-406, METHOD 7011.

REAGENTS (DESIGNATION)

RESISTANCE TO HOT SOAP SOLUTION



AS FOLLOWS:

No DE7’ERrORATION OF PAINTED SURFACE.

72

2022

2024

2486

2488

2479

2480

2482

, 2010

2011

2012

I●,!

,-.

,,’,

0I


I

I

.I

~

:0

t

I

1:)I

I

‘o

CHAR~

2022

2024

2486

2488

2479

2480

2482

2010

2011

20%2


>

STANDARD PARAGRAPH

RESISTANCE TO BRITTLENESS. TESTING SHALL BE PERFORMED INACCORDANCE WITH THE BASE DOCUMENT, EXCEPT ~.

RESISTANCE TO BRITTLENESS. TESTING SHALL BE PERFORMED INACCORDANCE WITH MIL-F-10884.

RESISTANCE To CHEMICAL REAGENTS. THE REQUIREMENT(SI SHALLBE IN ACCORDANCE WITH THE BASE DOCUMENT, EXCEPT ~.

RESISTANCE TO CHEMICAL REAGENTS. THERE SHALL BE NO DAMAGETO, FINISH OR BASE MATERIAL.

RESISTANCE TO CHEMICAL REAGENTS. TESTING SHALL BE PERFORMEDIN ACCORDANCE WITH THE BASE DOCUMENT, ExCEPT ~.

RESISTANCE TO CHEMICAL REAGENTS. TESTING SHALL BE PERFORMEDIN ACCORDANCE WITH METHOD 70111 OF FED-STD-406.

THE REAGENT(S) SHALL BE 2482.

RESISTANCE TO HOT SOAP SOLUTION. THE REQUIREMENT(S) SHALLBE IN ACCORDANCE wITH THE BASE DOCUMENT, EXCEPT ~.

RESISTANCE TO HOT SOAP SOLUTION. THE REQUIREMENT(SI SHALLBE AS FOLLOWS:

THERE SHALL BE NO DETERIORATION OF THE PAINTED SURFACE.

73


DOD-STD-35-23A(MI )9 March 1979


CHARACTERISTIC NAME

RESISTANCE TO HOT SOAP SOLUTION (CONT)

AS FOLLOWS: (CONT)

NO THUMBNAIL FURROWS

TEST METHODS (SELECT ONEI

IN FILM.


PER MIL–F–10884.

NOMINAL SOAP SOLUTION (PERCENT)

TOLERANCE (PERCENT)

NOMINAL SOLUTION TEMPERATURE(DEGREES CELSIUS)

TOLERANCE (DEGREES CELSIUS)

NOMINAL TEST PERIOD (HOURS)

TOLERANCE (HOURS)

RESISTANCE TO SOLVENTS


PER BASE DOCUMENT EXCEPT -

AS FOLLOWS:.

NO DIFFERENCE OF FINISH EXCEPTSLIGHT LOSS OF GLOSS.

IJ992 i

11994

11996

1998

2000

2002

2004

2006

1984

11985

1986

74



CHAR~

2013

1992

%s’s’4

>’396

3990

2000

2002

2004

2006

STANDARD PARAGRAPH

PAINTED SURFACE’ SHALL NOT BE AFFECTED WHEN ATTEMPTING TOFURROW THROUGH THE FILM WITH THE THUMBNAIL.

RESISTANCE-TO HOT SOAP SOLUTION. TESTING SHALL BE PERFORMEDIN ACCORDANCE WITH THE BASE DOCUMENT, EXCEPT ~.

RESISTANCE TO HOT SOAP SOLUTION. TESTING SHALL BE PERFORMED)IN ACCORDANCE WITH MIL-F-10884.

THE SOAp SOLUtION SHALL CONSIST OF 1996 pERc131T SOAPi

THE SOAP SOLUTION TOLERANCE SHALL BE ~ PERCENT.*

THE SOLUTION TEMPERATURE SHALL BE ~ DEGREES CELSIUS.

THE SOLUTION TEMPERATURE TOLERANCE SHALL BE q DEGREESCELSIUS. \

THE TEST PERIOD SHALL BE ~ HOURS.

THE TEST PERIOD TOLERANCE SHALL BE ~ HOURS.

RESISTANCE TO SOLVENTS. THE REQUIREMENT(S) SHALL BE INACCORDANCE WITH THE BASE DOCUMENT, EXCEPT 1984.

RESISTANCE TO SOLVENTS. THE REQUIREMENT(S) SHALL BE ASFOLLOWS:

THERE SHALL BE NO DIFFERENCE IN FINISH APPEARANCE AFTERTEST, EXCEPT FOR A SLIGHT LOSS OF GLOSS.

75

.


DOD-STD-35-23A(MIJ9 March 1979 ,


CHARACTERISTIC NAME

RESISTANCE TO SOLVENTS ICONT)

AS FOLLOWS: (CONT)

NO SOFTENING OF PAINT.



PER MIL-F-10884.

SOLVENT TEMPERATURE (DEGREES CELSIUS) ‘

TOLERANCE (DEGREES CELSIUS)

NOMINAL TEST DURATION (MINUTES)

DURATION TOLERANCE

1908

1972

3J974

11975

%976

1978

31980

0

,



C14AR~ STANDARD PARAGRAPH

I!, 1988

1. 1972

I 1974

1975

1976

1978

1980

THERE SHALL BE NO SOFTENING OF THE PAINT AS A RESULT OFTHE TEST.

RESISTANCE TO SOLVENTS. TESTING SHALL BE PERFORMED INACCORDANCE WITH THE BASE DOCUMENT, EXCEPT 1972.

RESISTANCE TO SOLVENTS. TESTING SHALL BE PERFORMED INACCORDANCE WITH MIL–F-10884.

THE TEST SOLVENT TEMPERATURE SHALL BE ~ DEGREES CELSIUS.

THE TEST SOLVENT TEMPERATURE TOLERANCE SHALL BE 1976DEGREES CELSIUS.

THE TEST DURATION

THE TEST DURATION

SHALL BE ~ HOURS.

TOLERANCE SHALL BE ~ HOURS.

I

,.

i

77


DOD-STD-35-23A(MI )9 March 19.79


CHARACTERISTIC NAME

SALT FOG



NO EVIDENCE OF CORROSION, PHYSICAL DAMAGEOR DEGRADATION OF PERFORMANCE.



PER MIL–STD-81J0, METHOD 509.

SALT SOLUTIIJN (PERCENT)

EXPOSURE PERIOD (HOURS)

DRYING PERIOD (HOURS)

OPERATE (SELECT ONE)

OPERATE

OPERATE

OPERATE

OPERATE

ONLY AFTER DRYING.

ONLY AFTER EXPOSURE.

AFTER EXPOSURE AND AFTER DRYING.

AFTER 24-HOURS OF EXPOSURE,

*

4998

4999

4779

4780

4T86

4783

4775

6245

6246

6247

6248

78

1‘.

I

01


oI

1:

,, .-

1 ‘


CHAR~

4998

4999

4779

4780

4786

4783

4775

6245

6246

6247

6248

STANDARD PARAGRAPH

SALT FOG. THE RECNJIREMENT[S) SHALL BE IN AccordanceWITH THE BASE DOCUMENT, EXCEPT ~.

SALT FOG. THERE SHALL BE NO EVIDENCE OF CORROSION,PHYSICAL DAMAGE OR DEGRADATION OF PERFORMANCE.

SALT FOG. TESTING SHALL BE PERFORMED IN ACCORDANCE WITHTHE BASE DOCUMENT, EXCEPT ~.

SALT FOG. TESTING SHALL BE PERFORMED IN ACCORDANCE WITHMETHOD 509 OF MIL-STD-810.

SOLUTION SHALL BE ~ PERCENT SALT.

DURATION OF THE TEST SHALL BE ~ HOUR(S).

DRYING PERIOD SHALL BE ~7~ HOUR(S).

ITEM(S) SHALL BE OPERATED ONLY AFTER DRYING.

ITEM(S) SHALL BE OPERATED ONLY AFTER EXPOSURE.

ITEM(S) SHALL BE OPERATED AFTER EXPOSURE AND AFTER DRYING.

ITEM(SI SHALL BE OPERATED AFTER 24 HOURS OF EXPOSURE.

79



KEYWORD CODE INDEX IKCI)

CHARACTERISTIC NAME

SHEAR FATIGUE \



NO CRACKS, FRACTURES OR DAMAGE.



PER NIL-F-22978

MINIMUM ULTIMATE LOAD (SELECT ONEI

(POUNDs) ,

(NEWTONS)

(PERCENT OF RATEDI

MAXIMUM ULTIMATE LOAD

(POUNDS)

(NEWTONS)

(PERCENT OF RATED)

MINIMUM NUMBER OF CYLCES (QUANTITY)

CYCLE RATE (CYCLES PER MINUTEI

CYCLE RATE TOLERANCE (CYCLES PER MINUTE)

2598

2S99 .

2582

2583

02584

2585

2586

2587

2588

2590:,

2592

2594

80!!,



1.

I


2598

2599

2582

2583

2584

2585

2586

2587

2588

2589

2596

2592

2594

SHEAR FATIGUE. THE REQUIREMENT(S) SHALL BE IN ACCORDANCEWITH THE BASE DOCUMENT, EXCEPT ~.

SHEAR FATIGUE. THERE SHALL BE NO CRAcK5, FRAcTuRE5 OR

DAMAGE .

SHEAR FATIGUE. TESTING SHALL BE PERFORMED IN ACCORDANCEWITH THE BASE DOCUMENT, EXCEPT ~.

SHEAR FATIGUE. TESTING SHALL BE PERFORMED IN ACCORDANCEWITH MIL-F-22978.

THE ULTIMATE LOAD SHALL BE NOT LESS THAN ~ POUNDS.

THE ULTIMATE LOAD SHALL BE NOT LESS THAN ~ NEWTONS.

THE ULTIMATE LOAD SHALL BE NOT LESS THAN ~ PERCENTOF RATED LOAD.

THE ULTIMATE LOAD SHALL BE NOT GREATER THAN ~ POUNDS.

THE uLTIMATE LOAD SHALL BE NOT GREATER THAN * NEwToN5.

THE ULTIMATE LOAD SHALL BE NOT GREATER THAN 2589 PERcENTOF RATED LOAD.

THE NUMBER OF CYCLES SHALL BE NOT LESS THAN ~ CYCLES.

THE CYCLE RATE

THE CYCLE RATE

SHALL BE ~ CYCLES PER MINUTE.

TOLERANCE SHALL BE ~ CYCLES PER MINUTE.

81


DDD-STD-35-23A(MI )9 March 1979


CHARACTERISTIC NAME

SHEAR STRENGTH


PER. BASE DOCUMENT

AS FOLLOWS:

MAXIMUM OPERATING

(POUNDS)

(NEWTONS)

CHAR,,.,,.,-.,,....,, ~

ONE)

-,’ ,“,. .:’;, ,’, , 2268,..:. ~;,,, ,

. . . . :.,:: ,. ;,~?.”.’ j.,+)’,; ,, . .226I3

SHEAR LOAD

2271

ULTIMATE SHEAR LOAD

(POUNDS) 2272

(NEWTONS) 2273,.. L ,.


PER BASE DOCUMENT EXCEPT ,— , 2262

(!tiif-it::? ... . .. . . . .-J-,. ..: ~,!.?,

PER DOCUMENT (DOC. DES) ..,, ..,. 226+“...

82


DOD-STD-35-Z!3A (MI)9 March 1979

,

,1

!

o

II:It..

●

CHAR~

2268

2269

2270

2271

2272

2273

2262

2264

STANDARD PARAGRAPH

.“;

SHEAR STRENGTH. THE REQUIREMENT(S) SHALL BE IN ACCORDANCEWITH THE BASE DOCUMENT? EXCEPT ~.

SHEAR STRENGTH. THE REQUIREMENT(S) SHALL BE AS FOLLOWS:

THE OPERATING SHEAR LOAD SHALL BE NOT GREATER THAN 2270PoUNDS .

,THE OPERATING SHEAR LOAD SHALL BE NOT GREATER THAN ~NEWTONS.

THE ULTIMATE SHEAR LOAD SHALL BE ~ POUNDS.

THE ULTIMATE SHEAR LOAD SHALL BE ~ NEWTONS.

SHEAR STRENGTH. TESTING SHALLWITH THE BASE DOCUMENT, EXCEPT

SHEAR STRENGTH. TESTING SHALL

83

BE PERFORMED IN ACCORDANCE~.

BE ‘IN ACCORDANCE WITH ~.




CHARACTERISTIC NAME

SHEET PULL-UP


PER BASE DOCUMENT

ONE )

EXCEPT

MAX MUM INITIAL SHEET SEPARATION.

(INCHESI

(Millimeters)


PER ’BASE DOCUMENT

PER MIL-F–22978.

SHEET SEPARATION


PER BAkE DOCUMENT

,

ONE )

EXCEPT —,

ONE )

EXCEPT

CHARCODE

2408

0

,24310

24311

“o2402

2404

2432

.!

=.

84 II(1t,1


CHAR~

2408

24%0

2411

2402

2404

2432


STANDARD PARAGRAPH

SHEET PULL-UP. THE REQUIREMENT(S) SHALL BE IN ACCORDANCEWITH THE BASE DOCUMENT, EXCEPT ~.

SHEET PULL-UP; THE FASTENER SHALL ENGAGE AND PULL

TOGETHER SHEETS WITH AN INITIAL SEPARATION OF ~ INCHES.

SHEET PULL-UP. THE FASTENER SHALL ENGAGE AND PULLTOGETHER SHEETS WITH AN INITIAL SEPARATION OF &&MILLIMETERS.

SHEET PULL-UP. TESTING

WITH THE BASE DOCUMENT,

SHEET PULL-UP. TESTING

WITH MIL–F–22978.

SHALL BE PERFORMEDEXCEPT ~.

SHALL BE PERFORMED

IN ACCORDANCE

IN ACCORDANCE

SHEET SEPARATION. THE REQUIREMENT(S) SHALL BE INACCORDANCE WITH THE BASE DOCUMENT, EXCEPT ~.

85




CHAR,CHARACTERISTIC NAME g

SHEET SEPARATION (CONT)

REQUIREMENTS (CONT)

MAXIMUM SHEET SEPARATION (SELECT ONE)<,

(INCHES)

(MILLIMETERS)


PER BASE DOCUMENT,.

PER DOCiJMENT (DOC

2433

!,

,2435

ONE)

EXCEPT _

DES)

NOMINAL TENSILE LOAD

(POUNDS)

(NEWTONS)

(SELECT ONEI

(PERCENT OF TENSILE..RATING)

2422

2424

2426

2427

2429

,,::;

86


.1

I

2433

1?

2435

I 2422

[ 2426

I 2427

I2429


STANDARD PARAGRAPH

SHEET SEPARATION. THE SHEET SEPARATION SHALL BE NOT GREATERTHAN ~ INCHES.

SHEET SEPARATION. THE SHEET SEPARATION SHALL BE NOT GREATERTHAN ~ MILLIMETERS.

SHEET SEPARATION. TESTING SHALL BE PERFORMED IN ACCORDANCEWITH THE BASE DOCUMENT! EXCEPT 2422.

SHEET SEPARATION. TESTING SHALL BE PERFORMED IN ACCORDANCEWITH 2424.

THE TENSILE LOAD SHALL BE 2426 POUNDS.

THE TENSILE LOAD SHALL BE ~ NEWTONS.

THE TENSILE LOAD SHALL BE ~ PERCENT OF,RATED TENSILESTRENGTH.

I

II ;

1,.:

i

I87




CHARACTERISTIC NAME

m


PER BASE DOCUMENT

AS FOLLOWS:

NO FAILURES.

NO LOOSENESS.

NO UNLOCKING.


PER BASE DOCUMENT

ONE )

EXCEPT

ONE)

EXCEPT _

PER MIL-STD-810, METHOD 516.

*pRoCEDURE

PROCEDURE

*FIGURE

1.

(SELECT ONE)

FIGURE 5116-I APPLIES.

FIGURE 516–2 APPLIES.

*AMPLITUDE, A OR B (LETTER)

*DURATIONt C OR D (LETTER)

PROCEDURE 11.

PROCEDURE 111.

7315

2870

2872

2874

2876

733.!3!

7312

7313

733!7

73%8

7305

7306

6327

6338

I

●

“

I

88


CHAR~

7315

2870

2872

2874

2876

7311

7312

7313

7317

7318

7305

7306

6327

6338


STANDARD PARAGRAPH

SHOCK . THE REQUIREMENT(S) SHALL BE IN ACCORDANCE WITHTHE BASE DOCUMENT, EXCEPT ~.

SHOCK. THE REQUIREMENT(S) SHALL BE:AS FOLLOWS:

THE FASTENER SHALL NOT FAIL AS A RESULT OF THE TEST.

THE FASTENER SHALL NOT LOOSEN DURING TEST.

THE FASTENER SHALL NOT BECOME UNLOCKED DURING TEST.

SHOCK . TESTING SHALL BE PERFORMED IN ACCORDANCE WITH THEBASE DOCUMENT, EXCEPT ~.

SHOCK. TESTING SHALL BE PERFORMED IN ACCORDANCE WITHMETHOD 516 OF MIL-STD-81O.

PROCEDURE NUMBER I SHALL APPLY.

THE SHOCK PULSE SHAPE SHALL BE SAWTOOTH IN ACCORDANCE WITHFIGURE 516-1 OF METHOD 516 OF MIL–STD–8L0.

THE SHOCK PULSE SHAPE SHALL BE HALF SINE WAVE IN ACCORDANCEWITH FIGURE 516-2 OF METHOD 516 OF MIL-STD-810.

AMPLITUDE LETTER ~ SHALL APPLY.

DURATION LETTER 7306 SHALL APPLY.

PROCEDURE NUMBER II SHALL APPLY.

PROCEDURE NUMBER III SHALL APPLY.

89

I

I




/..’

●

I

CHARACTERISTIC NAME

= (CONT)

PROCEDURE 111. (CONT)

*FIGURE (SELECT ONE)

FIGURE 5116-1 APPLIES.

FIGURE 516-2 APPLIES.

*AMPLITUDE A OR B (LETTER)

*DURATION C OR D (LETTER)

PROCEDURE IV.

*FIGURE (SELECT ONE)

FIGURE 516–L APPLIES.

FIGURE 516–2 APPLIES.

*AMPLITUDE, A OR B (LETTER)

*DURATION, C OR D (LETTER)

PROCEDURE V.

PROCEDURE VI.

TEST TEMPERATURE (DEGREES CELSIUS)

TEMPERATURE TOLERANCE (DEGREES CELSIUS)

OPERATION DURING TEST REQUIRED.

90

6339

6340

634L

6342

6343

6344

6345

6346

6347

6348

6349

7307

7308

7309




6339 THE SHOCK PULSE SHAPE SHALL BE SAWTOOTH IN ACCORDANCE WITHFIGURE 516-1 OF METHOD 516 OF MIL-STD–810.

6340 THE SHOCK PULSE SHAPE SHALL BE HALF SINE WAVE IN ACCORDANCEWITH FIGURE 516–2 OF METHOD 516 OF MIL-STD-810.

6341 AMPLITUDE LETTER 6341 SHALL APPLY.

6342 DuRATION LETTER ~ SHALL APPLY.

6343 PROCEDURE NUMBER IV SHALL APPLY.

63+4

6345

6346

6347

6348

6349

7307

7308

7309

THE SHOCK PULSE SHAPE SHALL BE SAWTOOTH IN ACCORDANCE WITHFIGURE 516-1 OF METHOD 516 OF MIL-STD-810.

THE SHOCK PULSE SHAPE SHALL BE HALF SINE WAVE IN ACCORDANCEWITH FIGURE 516-2 OF METHOD 516 OF MIL–STD-81O.

AMPLITUDE LETTER & SHALL APPLY.

DURATION LETTER ~ SHALL APPLY.

PROCEDURE NUMBER V SHALL APPLY.

PROCEDURE NUMBER VI SHALL APPLY.

THE TEST TEMPERATURE SHALL BE ~ DEGREES CELSIUS.

THE TEST TEMPERATURE TOLERANCE SHALL BE PLUS OR MINUS ~

DEGREES CELSIUS.

OPERATION ’DURING THE TEST IS REQUIRED.

91




CHARACTERISTIC NAME

STRESS CORROSION


PER BASE DOCUMENT

NO CRACKS, DAMAGE


PER BASE DOCUMENT

PER MIL-STD-IJ312,

ONE)

EXCEPT _

OR CORROSIOH,

ONE)

EXCEPT _

METHOD 9.

PER FED–STD–151, METHOD 823.

STUD PUSH–OUT



NO DISENGAGEMENT OR DEFORMITY.


PER

PER

BASE DOCUMENT

MIL-F-22978.

ONE)

EXCEPT _

92

2504

2506

2492

2494

245’6

2384

2386

●

23768,

2378


●

CHARg

.. 2504

2492

2494

●2496

2384

I2386

I>I

2376

1’I 2378

0’


STANDARD PARAGRAPH

STRESS CORROSION. THE REQUIREMENT(S) SHALL BE IN ACCORDANCEWITH THE BASE DOCUMENT, EXCEPT ~.

STRESS CORROSION. THERE SHALL BE NO CRACKS, PHYSICAL DAMAGEOR CORROSION.

STRESS CORROSION. TESTING SHALL BE PERFORMED IN ACCORDANCEWITH THE BASE DOCUMENT, EXCEPT ~.

STRESS CORROSION. TESTING SHALL BEPERFORMED IN ACCORDANCEWITH METHOD 9 OF MIL-STD–1312.

STRESS CORROSION. TESTING SHALL BE PERFORMED IN ACCORDANCEWITH METHOD 823 OF FED-STD-151.

STUD PUSH-OUT. THE REQUIREMENT(S) SHALL BE IN ACCORDANCEWITH THE BASE DOCUMENT, EXCEPT ~.

STUD PUSH-OUT. THERE SHALL BE NO DISENGAGEMENT OR DEFORMITYOF THE FASTENER.

STUD PUSH-OUT. TESTING SHALL BE PERFORMED IN ACCORDANCEWITH THE BASE DOCUMENT, EXCEPT ~.

STUD PUSH-OUT. TESTING SHALL BE PERFORMED IN ACCORDANCEWITH MIL-F-22978.

93



●KEYWORD CODE INDEX (KCI)

CHARACTERISTIC NAME

STUD PUSH–OUT (CONT)

PER MIL-F–22978. (CONT)

MINIMUM TEST LOAD (SELECT ONE)

(POUNDS)

(NEWTONS)

SUREACE ROUGHNESS



AS FOLLOWS:

MAXIMUM ROUGHNESS HEIGHT, ARITHMETICALAVERAGE (SELECT ONE)

(MICROINCHES)

(MICROMETERS)

‘ cOMPONENTS (WRITE-IN)


PER BASE DOCUMENT

PER ANSIB46.I.

ONE )

EXCEPT _

94

2380

2379

27001

:1

2702 ● 1

2704

2706

1’

2708,1(

s i’;!

2720I

. !;

2722!,

:;1

‘,I

I

● II

i

11

“! I


DOO-,STD-35-23A(MI )9 March 1979

. .

CHARg

2380

2379

2700

2702

270+

2706

2708

2720

2722

STANDARD PARAGRAPH

THE TEST LOAD SHALL

THE TEST LOAD SHALL

SURFACE ROUGHNESS.ACCORDANCE WITH THE

SURFACE ROUGHNESS.FOLLOWS:

BE NOT LESS THAN ~ POUNDS.

BE NOT LESS THAN 2379 NEWTONS.

THE REQUIREMENT(S) SHALL BE INBASE DOCUMENT, EXCEPT ~.

THE REQUIREMENT(S) SHALL BE AS

THE ROUGHNESS HEIGHT (ARITHMETICAL AVERAGE) SHALL BE NOTGREATER THAN ~ MICROINCHES.

THE ROUGHNESS HEIGHT (ARITHMETICAL AVERAGE) SHALL BE NOTGREATER THAN ~ MICROMETERS.

THE COMPONENTS SHALL BE 2708.

SURFACE ROUGHNESS. TESTING SHALL BE PERFORMED IN ACCORDANCEWITH THE BASE DOCUMENT, EXCEPT 2720.

SURFACE ROUGHNESS. TESTING SHALL BE PERFORMED IN ACCORDANCEWITH ANSIB46.L.

95




CHARACTERISTIC NAME

TEMPERATURE, HIGH


PER BASE DOCUMENT

ONE 1

EXCEPT _

NO EVIDENCE OF PHYSICAL DAMAGE.



PER MIL-STD-810, METHOD 501L.

*PROCEDURE (ROMAN NUMERAL)

STORAGE TEMPERATURE (DEGREES CELSIUS)

STORAGE DURATION [HOURS)

HIGHEST OPERATING TEMPERATURE(DEGREES CELSIUS)

OPERATION TIME (SELECT ONE)

(MINUTES)

( HOURS)

6228

6229

,.

6217

6218

621J9

6220

6221

6222

6224

, 6225

96


1

●


6228

6229

62%7

62118

6219

6220

6221

6222

6224 .

6225

TEMPERATURE, HIGH.ACCORDANCE WITH THE

TEMPERATURE, HIGH.DAMAGE.

TEMPERATURE, .HIGH.ACCORDANCE WITH THE


THE REQUIREMENT(S) SHALL BE INBASE DOCUMENT, EXCEPT ~.

THERE SHALL BE NO EVIDENCE OF PHYSICAL

TESTING SHALL BE PERFORMED INBASE DOCUMENT, EXCEPT ~.

TEMPERATURE, HIGH. TESTING SHALL BE PERFORMED INACCORDANCE WITH METHOD 501 OF MIL-STD-810.

PROCEDURE NUMBER & SHALL APPLY.

STORAGE TEMPERATURE SHALL BE ~ DEGREES CELSIUS.

STORAGE DURATION SHALL BE ~ HOUR(S).

HIGHEST OPERATING TEMPERATURE SHALL BE ~ DEGREES CELSIUS.

OPERATING TIME SHALL BE ~ MINUTE(S).

OPERATING TIME SHALL BE ~ HOUR(S).

L

97




CHARACTERISTIC NAME

TEMPERATURE, LOW



NO EVIDENCE OF PHYSICAL DAMAGE.


PER BASE DOCUMENT EXCEP”

PER MIL-STD-81O, METHOD 502.

CHAR~

63118

6319

STORAGE TEMPERATURE (DEGREES CELSIUS) 6234

STORAGE DURATION (HOURS) 6235

LOWEST OPERATING TEMPERATURE [DEGREESCELSIUS) 6236

CHAMBER AIR VELOCITY (SELECT ONE)

(FEET PER SECOND) 6237

(METERS PER SECOND) 6238

OPERATION TIME (SELECT ONE)

[MINUTES) 6315

(HOURS) 6316

.,

.

●

98



i’~

o

1,,

!

10L-

CHARg

6318

6319

6231

6232

6234

6235

6236

6237

6238

6315

6316

.,

STANDARD PARAGRAPH

TEMPERATURE, LOW. THE REQUIREMENT(S) SHALL BE INACCORDANCE WITH THE BASE DOCUMENT, EXCEPT ~.

TEMPERATURE, LOW. THERE SHALL BE NO EVIDENCE OFPHYSICAL DAMAGE.

~&MPERATURE, LOW. TESTING SHALL BE PERFORMED INACCORDANCE WITH THE BASE DOCUMENT, EXCEPT ~.

TEMPERATURE, LOW. TESTING SHALL BE PERFORMED INACCORDANCE WITH METHOD 502 OF MIL-STD–810.

STORAGE TEMPERATURE SHALL BE ~ DEGREES CELSIUS.

STORAGE DURATION SHALL BE ~ HOUR(S).

LOWEST OPERATING TEMPERATURE SHALL BE @ DEGREES CELSIUS.

CHAMBER AIR VELOCITY SHALL BE ~ FEET PER SECOND.

CHAMBER AIR VELOCITY SHALL BE ~ METERS PER SECOND.

OPERATING TIME SHALL BE ~ MINUTE(S).

OPERATING TIME SHALL BE ~ HOUR(S).

99




CHARACTERISTIC NAME

TENSILE STRENGTH



AS FOLLOWS:

MAXIMUM OPERATING TENSILE LOAD (SELECT ONE)

(POUNDS)

(NEWTONS)

(PERCENT OF RATED)

ULTIMATE TENSILE LOAD (SELECT ONE)

(POUNDS)

(NEWTONS

(PERCENT

TEST METHODS (SELl

OF RATED)

CT ONE)



2248

2249

2250

2245

2247

2252

2253

2254

2242

2244

100

‘ !



2248,’

I2249

II 2250

I 2245

I●2247

2252

2253

2254

2242

,2244

.,

STANDARD PARAGRAPH

TENSILE STRENGTH. THE REQUIREMENT(SI SHALL BE INACCORDANCE WITH THE BASE DOCUMENT, EXCEPT ~.

TENSILE STRENGTH. THE REQUIREMENT(S) SHALL BE AS FOLLOWS:

THE OPERATING TENSILE LOAD SHALL BE NOT GREATER THAN~ POUNDS.

THE OPERATING TENSILE LOAD SHALL BE NOT GREATER THAN~ NEWTONS.

THE OPERATING TENSILE LOAD SHALL BE NOT GREATER THAN~ PERCENT OF RATED TENSILE STRENGTH.

THE ULTIMATE TENSILE LOAD SHALL BE ~ POUNDS.

THE ULTIMATE TENSILE LOAD SHALL BE ~ NEWTONS.

THE ULTIMATE TENSILE LOAD SHALL BE ~ PERCENT OFRATED TENSILE STRENGTH.

TENSILE STRENGTH. TESTING SHALL BE PERFORMED INACCORDANCE WITH THE BASE DOCUMENT, EXCEPT ~.

TENSILE STRENGTH. TESTING SHALL BE PERFORMED INACCORDANCE WITH ~.

101



KEYWORD

CHARACTERISTIC NAME

TENSILE STRENGTH (CONT)

PER, DOCUMENT (CONT)

CODE INDEX (KCI)

NOMINAL TENSION LOAD RATE (SELECT ONE)

‘(POUNDS PER SQUARE INCH PER MINUTE) 2233

(KILOPASCALS pER MIyuTE) 2234

SPECIMEN DESCR1PTION (k/RITE-IN) 2235

TEST TEMPERATURE (DEGREES CELSIUS) 2236

TEMPERATURE TOLERANCE (DEGREES CELSIUS) 2237

TEMPERATURE DURATION ‘(MINUTES) 2238

TEST FIXTURE TYPE” (DESIGNATION) 2239

THICKNESS OF METALLIC COATINGS



NOTE; REQUIREMENTS FOR PLATING THICKNESSAND OTHER PARAMETERS MAY BE

SPECIFIED IN THE FINISH TABLE OF DOD-STD-35.



PER MIL-STD-1312, TEST 12.

.

:.

2740

2742

102


,0

,’

I

1

CHAR~

2233

2234

2235

2236

2237

2238

2239

2730

.

2740

----L [4L


STANDARD PARAGRAPH

THEPER

THE

THE

THE

THE

TENSION LOAD SHALL BE ~ POUNDS PER SQUARE INCHMINUTE.

TENSION LOAD SHALL BE ~ KILOPASCALS PER MINUTE.

SPECIMEN SHALL BE ~.

TEST TEMPERATURE SHALL BE & DEGREES CELSIUS.

TEST TEMPERATURE TOLERANCE SHALL BE ~ DEGREES--.-.,.-LEL>lU>.

THE TEST TEMPERATURE DURATION SHALL BE @ DEGREESCELSIUS.

THE TEST FIXTURE TYPE SHALL BE ~.

THICKNESS OF METALLIC COATINGS. THE REQUIREMENT(S) SHALLBE IN ACCORDANCE WITH THE BASE DOCUMENT, EXCEPT ~.

THICKNESS OF METALLIC COATINGS. TESTING SHALL BE PERFORMEDIN ACCORDANCE WITH THE BASE DOCUMENT, EXCEPT ~.

THICKNESS OF METALLIC COATINGS. TESTING SHALL BE PERFORMEDIN ACCORDANCE WITH TEST NUMBER 12 OF MIL-STD-1312.

103


DOD-STD-35-23A(MIJ9 March 1979


CHARACTERISTIC NAME..

THICKNESS OF METALLIC COATINGS (CONT)

PER MIL–STD-1312, TEST 12.

METHODS

DROP .

MAGNETIC.

EDDY CURRENT.

MICROSCOPIC.

DIMENSIONAL CHANGE.

ANODIC DISSOLUTION.

STRIP AND WEIGH.

TORQUE



AS FOLLOWS:

LOCKING TORQUE

MINIMUM (SELECT ONE)

(POUND-INCHES )

(NEWTON METERS)

CHARCODE

CONT

274+ ;

2746

2748

2750

2752

2754

2756

/’,’

0

●

2Z88

2289

c ,:

2290

2291

104


DOO-STD-35-23A(MI )9 March 1979

.

CHARg

2744

2746

2748

2750

2752

2754

2756

2288

2289

2290

2291

STANDARD PARAGRAPH

TEST METHOD SHALL BE







DROP.

MAGNETIC.

EDDY CURRENT.

MICROSCOPIC.

DIMENSIONAL CHANGE.

ANODIC DISSOLUTION.

STRIP AND WEIGH.

TORQUE . THE REQUIREMENT(S) SHALL BE IN ACCORDANCE WITH THEBASE DOCUMENT, EXCEPT ~.

TORQUE . THE REQUIREMENT(S) SHALL BE AS FOLLOWS:

THE LOCKING TORQUE SHALL BE NOT LESS THAN @ POUND-INCHES.

THE LOCKING TORQUE SHALL BE NOT LESS THAN 2291 NEWTON METERS.

105



.

KEYWORD CODE INDEX [KCII

CHARACTERISTIC NAME

TORQUE (CONT)

LOCKING TORQUE (CONT)

MAXIMUM [SELECT ONE)

(POUND-INCHES)

(NEWTON METERS)

UNLOCKING TORQUE


(POUND-INCHES)

(NEWTON METERS)

MAXIMUM (SELECT ONE)

(POUND-INCHES)

(NEWTON METERSI

FASTENER TORQUE STRENGTH


(POUND-INCHES)

(NEWTON METERS)

2292

2293

2294

2295

2296

2297

2299

2298

● ’

106



I

.

I ●I

,

,>

●


2292

2293

2294

2295

2296

2297

2299

2298

THE LOCKING TORQUE SHALL BE NOT GREATER THAN 22.9’2POUND–INCHES.

THE LOCKING TORQUE SHALL BE NOT GREATER THAN w

NEWTON METERS.

THE UNLOCKING TORQUE SHALL BE NOTPOUNDS–INCHES.

THE UNLOCKING TORQUE SHALL BE NOTNEWTON METERS.

THE UNLOCKING TORQUE SHALL BE NOTPOUND-INCHES.

THE UNLOCKING TORQUE SHALL BE NOTNEWTON METERS.

LESS THAN ~.

LESS THAN ~

GREATER THAN’Lfi

GREATER THAN ~

THE FASTENER TORQUE STRENGTH SHALL BE NOT LESS~THAN 2299POUND-INCHES.

THE FASTENER TORQUE STRENGTH SHALL BE NOT LESS-THAN 2298NEWTON METERS.

107


DOD-STD-35-23A(MI):. ,,:9 March 1979 ,.:


CHARACTERISTIC NAME

TORQUE (CONT)

AS FOLLOWS:

LOCK STOP TORQUE STRENGTH

MINIMUM

(POUND-INCHES)

[NEWTON METERS)


PER BASE DOCUMENT

PER DOCUMENT (DOC

VIBRATION


PER’BASE DOCUMENT

ONE )

EXCEPT _

DES)

ONE )

EXCEPT _

AS FOLLOWS: ... ,.

NO LOOSENESS, FAILURE OR DEGRADATIONOF PERFORMANCE.

NO UNLOCKING.


PER BASE DOCUMENT

ONE)

EXCEPT

108

2360

2362

2366

2368

46%3

2890

2892

2894

1

;, \


CHARg

2360

2362

2366

2368

4681,

2890

2892

2894

1505


STANDARD PARAGRAPH

THE LOCK STOP TORQUE STRENGTH SHALL BE NOT LESS THAN 2360POUND–INCHES.

THE LOCK STOP TORQUE STRENGTH SHALL BENEWTON METERS.

TORC!UE . TESTING SHALL BE PERFORMED INBASE DOCUMENT, EXCEPT 2366.

TORQUE . TESTING SHALL BE PERFORMED IN

NOT LESS THAN ~

ACCORDANCE WITH THE

ACCORDANCE WITH ~.

VIBRATION. THE REQUIREMENT(S) SHALL BE IN ACCORDANCE WITHTHE BASE DOCUMENT, EXCEPT ~.

VIBRATION. THE REQUIREMENT(S) SHALL BE AS FOLLOWS:

THE FASTEFJER SHALL NOT BECOME LOOSE, FAIL OR DEGRADE INPERFORMANCE.

THE FASTENER SHALL NOT BECOME UNLOCKED.

VIBRATION. TESTING SHALL BE PERFORMED IN ACCORDANCE WITHTHE BASE DOCUMENT, EXCEPT ~.

109


.DOD-STD-35-23A(MI)9 March 1979


CHARACTERISTIC NAME

VIBRATION (CONT)

TEST METHODS (CONT)

PER MIL–STD-810, METHOD 514.

*PROCEDURE NUMBER (ROMAN NUMERAL)

EQUIPMENT (CATEGORY) .,.:,,,,

CURVE. (LETTERS)

APPLICABLE TABLE (NUMBER)

APPLICABLE TABLE (FIGURE)..

OPERATION NOT REQUIRED.

TEMPERATURE (DEGREES CELSIUS)

TEMPERATURE TOLERANCE (DEGREES

DURATION AT TEMPERATURE (HOURS

PER MIL-STD–1312.

WATER RESISTANCE TREATMENT



MAXIMUM TApE WEIGHT INcREA5E (pERCENT)

CELSIUSI

110

IJ525

1532

11559

1424

1542

1543

1544

2898

2358

2160


1-—●.

i:

“o

1“

!’.

i

1

●

CHARg

1514

15%8

1540

%525

1532

1559

1424

1542

L543

1544

2898


STANDARD PARAGRAPH

VIBRATION. TESTING SHALL BE PERFORMED IN ACCORDANCE WITHMETHOD 514 OF MIL-STD-81O.

PROCEDURE NUMBER ~ SHALL APPLY.

THE EQUIPMENT CATEGORY SHALL BE ~ IN ACCORDANCE WITHMETHOD 514 OF MIL-STD-8%0.

CURVE ~ SHALL APPLY.

PROCEDURE AND TIME SCHEDULE SHALL BE AS SHOWN ON TABLE WOF METHOD 514 OF MIL-STD-810.

TEST CURVES SHALL BE AS SHOWN IN FIGURE ~ OF METHOD 514OF MIL-STD–810.

OPERATION DURING THE TEST 1S NOT REQUIRED.

VIBRATION TEST SHALL BE PERFORMED AT ADEGREES CELSIUS.

TEMPERATURE TOLERANCE SHALL BE PLUS ORCELSIUS.

THE TEMPERATURE TIME DURATION SHALL BE

VIBRATION. TE5TING SHALL BE PERFORMEDMIL–STD-IJ312.

TEMPERATURE OF ~

MINUS ~ DEGREES

& HOUR(S).

IN ACCORDANCE WITH

2158 WATER RESISTANCE TREATMENT. THE REQUIREMENT(S) SHALL BE INACCORDANCE WITH THE BASE DOCUMENT, EXCEPT 2158.

2160 MATER RESISTANCE TREATMENT. THE WEIGHT INCREASE OF THE TAPESHALL NOT BE GREATER THAN ~ PERCENT AS A RESULT OF THETEST.

111




CHARACTERISTIC NAME

WATER RESISTANCE TREATMENT (CONT)



PER FED-STD-191, METHOD 5502.

WIRE STAKING STRENGTH (RECEPTACLE STRIP FASTENER)



AS FOLLOWS:

NO LOAD SLIPPAGE IN LONGITUDINAL DIRECTION.

NO DISLOCATION


PER BASE DOCUMENT

PER MIL-F-25173.

FROM STAKED POSITION.

ONE )

EXCEPT _

NOMINAL LOAD PARALLEL TO WIRE AXIS

‘: (POUNDS)

r,’ (NEWTONS)

21152

2154

23%2

23%3

233I4

2336

2302

2304

2305

2306!

112


oDOD-STO-35-23A(MI)9 March 1979

.

CHAR~

21152

21154

2312

2313

2314

2316

2302

2304

2305

2306

STANDARD PARAGRAPH

MATER RESISTANCE TREATMENT. TESTING SHALL BE PERFORMEDIN ACCORDANCE WITH THE BASE DOCUMENT, EXCEPT ~.

WATER RESISTANCE TREATMENT. TESTING SHALL BE PERFORMEDIN ACCORDANCE WITH METHOD 5502 OF FED-STD-191.

WIRE STAKING STRENGTH. THE REQUIREMENT(S) SHALL BE INACCORDANCE WITH THE BASE DOCUMENT, EXCEPT 2312.

WIRE STAKING STRENGTH. THE REQUIREMENT(S) SHALL BE ASFOLLOWS:

THERE SHALL BE NO WIRE SLIPPAGE WHEN THE LOAD IS APPLIEDIN THE LONGITUDINAL DIRECTION.

THERE SHALL BE NO DISLOCATION OF THE WIRE WHEN IN THESTAKED POSITION.

WIRE STAKING STRENGTH. TESTING SHALL BE PERFORMED INACCORDANCE WITH THE BASE DOCUMENT, EXCEPT 2302.

WIRE STAKING STRENGTH. TESTING SHALL BE PERFORMED INACCORDANCE WITH MIL-F-25173.

THE LOAD PARALLEL TO THE WIRE

THE LOAD PARALLEL TO THE WIRE

113

AXIS SHALL BE ~ POUNDS.

AXIS SHALL BE ~ NEWTONS.


DOD-STD-35-23A(MI) ,,9 March 1979 ,,

KEYWORD CODE INDES (KCII

CHARCHARACTERISTIC NAME . . . ~

WIRE STAKING STRENGTH (RECEPTACLE STRIP FASTENER) (CONT)

PER MIL-F-25L73. (CONT)

NOMINAL LOAD PERPENDICULAR TO WIRE AXIS

(POUNDS)

(NEWTONS)

MOUNTING HARDWARE (SEE

,

. . /,

,,, -, l,!,,,,L ,, >.,.,,.. ,. .,,

TABLE X, DOD-STD-35)

NOTE : AUTOMATIC WHEN TABLE X IS USED. -,,’..

WORKMANSHIP

(DOC DES)

ADDITIONAL REQUIREMENTS ,,

A_

B_

c_

D

E—.

PART MARKING (SELECT ONE)

[DOC DES)

2307

2308

6870 ●

7oo.11

7002

7003

7004

7005,

6372 ?,

!!MIL-STD–130. 7629

,: I

o ~j114 1!,,t

1!


‘oI

I.



2307

2308

6870

7001

7002

7003

7004

7005

6372

7629

THE LOADPOUNDS .

THE LOADNEWTONS.

PERPENDICULAR

PERPENDICULAR

TO THE WIRE AXIS SHALL BE ~

TO THE WIRE AXIS SHALL BE ~

MOUNTING HARDWARE. MOUNTING HARDWARE IDENTIFIED IN THEFOLLOWING TABLE SHALL BE FURNISHED WITH EACH ITEM.

WORKMANSHIP . WORKMANSHIP

ADDITIONAL REQUIREMENTS.

(A) ~.

(B) ~.

(c) ~.

(D) ~.

(E) ~.

SHALL BE IN ACCORDANCE WITH ~.

PART MARKING. PART IDENTIFICATION MARKING SHALL BE INACCORDANCE WITH ~, USING THE PART NUMBER AS THEIDENTIFYING NUMBER.

PART MARKING. PART IDENTIFICATION MARKING SHALL BE INACCORDANCE WITH MIL-STD-130.

115




CHARACTERISTIC NAME

ADDITIONAL PART MARKING

A_

B_

c_

D_

E_

Applicable DocuMENTs (SEE DCID-STD-35)

QUALITY ASSURANCE PROVISIONS (SEE DOD-STD-35)

PAcKAGING (sEE DoD-sTD-35)

~ (SEE DoD-sTD-35)

NOMENCLATURE (sEE DoD-sTD-35)

SUPERSEDED DOCUMENT (SEE DOD-STD-35)

PART NUMBER CROSS–REFERENCE (SEE DOD-STD-35)

6991

6992 .

6993

6994

6995

116


(

I

i

1

I

I

I

I

I

I

I

●

✎

●

✎‘

●


ADDITIONAL PART MARKING.

6991 (A) ~.

6992 (B) ~.

6993 (C) ~.

6994 (D) ~.

6995 (E) ~.

Custodians:AtTIY-MI

Review activities:AtTILv-ATArmy-AVArmy-ELArmy-MEArmy-MRAtmy-SGArmy-WC


User activity:Army-MU

Preparing activity:Army-MI

(Project EDS-A285)

117


00D-sTD-35-23A(M1)9 March 1979

APPENDIX A

ILLUSTRATIONS


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146-05-1

124



146-05-5

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146-09-12

132

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DOD-STD-35-23A(MI]9 March 1979

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146-1+27

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146-14-28

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+-,,-4

146-1+29

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146


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146-10-42

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146-14-43

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155



APPENDIX B

CHARACTERISTIC CODE INDEX

156


DOD-STO-35-23A(NI )9 March 1979

0

.

1604

151815251532154J15421543i5b41554i5591582

16!70ieili1662i6u3

PAGE.NQa

16ib161616lb181016161616101622ii:108ii.11<iioiiuii G

Iii

lib

ii u

6611.24202J262020Zu202.2J

2JJ2828

CHAFACTEFISTIC CODE INDEx

CHAR.CQ.Ci

16161616ifi2ui6Z?162416261628i63iiit4ii t421646iE4816561652i65&it5bi66G1EE2166+i67iliE72i67k1676iteai6e216e3168+i69J16921~931~941696

17Li21700171$1?12172L1722i>~-)

1732

PAGE.ML

3036303113Q303rA303C3U3232323232323232323234343*343434343636363b363636363638302838

157

CHARLQrk

174i3i?ki174217431744176517461747i75u17521?601762i77a17721?74177617781782179d17921794i79617981802i8C41806181218131814iai518161817li?181822le241828183318711.S721873

PAGE-Ma

383838404040404G4G40404G4(I424242424242424.24242be484848$84848464848

;;5050666666

CHAR

1878t88G18821884197219741975197619781980i98k1985198619681’3921994199619982000200220042~G6

2010Ziiii20122G13Zil222024202821)302L3420362L4Uzok220522253205+2i682L692071

PAGE-l&

68606668767676767676.74747*767474747474747474727272747272707070707070545454525252

—



c~4GAcTERIsTIc coo: INOEX (CONT)

~iJ~~

2C7+21.221r,4Z1L821U32Ali.2311Ziiz212221Z321252iZ72129213$2135.21372139.214121+721492152215+2158.216JZ172217421782179Z19Z219421962198ZZ;222;322;*2.?J6Zl?ziZ22Z2224

52545.+56545454545+5056565656;b56505656565011z11z11u11i686868685J5G5b5Z5d50s$’i-.Jd666666

22282Z.322233223422352236

2237zz~~

Z2392242Z244Z2452Z4722482Z4922s.Z25222532254226222 e*Z2fi82269227:22712Z7Z2273Z2882Z89Z29U229122922293229422<5

22962z97Z298Z29923CZ

6666.

162102~J2

1321C2lizi32lililldll10Ci!lolJG100i-b1(JG100lIJO8282e28282828Z82

104li14164lii4I(J61:6106iG61061061~6

la6112

CHARG~Q~

z~~+23G523u62311723G8231223i3Z314231623422344Z348Z35J2352Z36022622366.75&3237623782379238023b42Z8623922394

2395z39r23982399241122*O+Zkt 8241J24iiZ422242424262427Z429

P&G:

-M.

114;112’112114114112ilz11211252525Z5252

138108io81089Z9294’34929Z707il?G68

%8484!3484846686868686

CHAP.

GQQL

243Z243324352k422++42+462448Z*5C24522.+5424562458246u24622*6*Z4b6z*D1324722+73247524772479248024822486248824922*942+962504256625622585256425852586258725882589259.2

PAGE

.NQA

848686585858585858585858606063606058 ●5858587272727Z729292929292808080 /1

80 .,,

8080808960

158


●DOO-STD-35-23A(MI)9 March 1979

.

1.

0

CHAR PAGE

fiQQi .LiQ~

259+2555

259927tiJ27.22?;427u62?i132?232722273U27+327422?4427462746275!32752275.+275627702?72

C!+ARACTEfiISTIC

PAGE

-fw

26

26

26

26

26

26

28

28

28

28

2e

28

28

2e

28

Iia

6*

62

62

62

60

E&

60

04

c+

78

0+

Ck

76

76

78

78

04

62

62

62

64

62

64

20

159

CCDE INCEX (CONT}

CHAR

LiQQE

49G54916495J4’s9845995a4652b8621762186219622J62216222622*6.2256228622’362316232623462356236623?0238024562*c62476243b.?i56316631a63196327633W

63356336633763386339634cI

PAGE

-MI

20642276762222’36969696969696969696989898’389B98?e75

?e

?@

?d

99

58

9e

98

8a

64

64

64

64

86

90

90

CHAR PAGELURE _BQA

6341 906342 906343 906344 906345 9063+6 906347 906348 906349 906369 166372 1146870 ii46873 16687L 1869+1 1869426991 lit6992 1166993 1166994 1166995 1166996 466997 4669’38 466999 -67 .,1 1147c~2 lIL

7?C3 114,GL+ It+7GI15 1147u21 LA7022 447023 b47924 447(I35 467036 467037 467038 467G417042 ::



CHARixE

7(J43764473357.3G67zi77308

733’37311

731273137315731773~~

?5727573?5767577753376.29

4*4488889!i9G9U88888888808822222222“24114

CHARACTERISTIC CCJIE INOEX (CONTJ

Ct?fll? PAGE GHA? PAGE CHAR PAGE

fiuz .Juh Mix Jd.k CQQE _tiQa

o

160


●DOD-STO-35-23A(MI)9 March 1979

,.INDEXI

1

I

I

I

r

I

Additional Part Marking ------ ----------------AdditionalRequirements----- -----------------Aperture Cards Required ----- -----------------Applicable Documents------- -----------------

.Base Document ---------- -----------------

.

●

Chain Uniformity--------- -----------------Chain Waviness (Slide Fasteners)- - - - - - - - - - - - - - - - - -City, State, Zip---------- ----------------Class -------------- -----------------Classification--------- ---------------- --Cleanlinens ---------- ---------------- --Clinch Force---------- ---------------- --Colorfastness --------- ---------------- --Company Name/Conunand-------- ----------------Configuration ---------- -----------------Contract Number/Office Symbol - - - - - - - - - - - - - - - - - - -Control, Source -------- ----------------- --Control, Specification------ -----------------

Date--------------- -----------------Decarburization -------- ---------------- --Design and Construction ----- -----------------

Embrittlement Relief------ ---------------- --Endurance ----------- ------------------Engaging of Stud to Receptacle- - - - - - - - - - - - - - - - - - -

Fabric Color---------- ---------------- --Fastener Installation ----- ---------------- --

. Finish-------------- -----------------Finishes------------ ---------------- --Floating Receptacle ------- -----------------Format-------------- -----------------

[~”’ Fungus------------- ---------------- --

I Government Design Activity FSCM - - - - - - - - - - - - - - - - - -

Hand of Separating Unit----- -----------------Hardness---------- -------------- ------Head Flushness------- -------------- ------Head Knurl---------- --------------- ----

●Hook Tape (Fastener Tape)--- ------ ---------- -.Humidity----------- ------- -------- ----

161

Q

116114

II:

16

4850

::

H52521622161618

::24

565834

42

:;24381660

16

426230

%62



INDEX (CCINT)

#Pagg!

Illustrations --------- ---------------- --Initial Tension -------- ---------------- -- ::Interchangeability-------- ----------------- 38

Locked Position -------- ---------------- -- 32Locking ----------- --------------- ---- 32

Material Analysis ------ --------------- ---- 66Materials ---------- --------------- ---- 24Maximum Longitudinal Shrinkage- - - - - - - - - - - - - - - - - - - 40Maximum Sheet Separation-- -------------- ------Metals------------ --------------- ---- ::Mildew Resistance Treatment - - - - - - - - - - - - - - - - - - - - 68Minimum ShearLoadRating- -------------- ------ 20MinimumTensile Load Rating -------------- ------Mounting Hardware ----- -------------- ------ 1::

Nomenclature-------- -------------- ------ 116Notes ----------- -------------- ------ 116

:

*,

●Packaging --------- -------------- ------ 116 I

Part Marking-------- -------------- ------ 114Part Number -------- - ---’ ---------- ------Part Number Cross-Reference - - - - - - - - - - - - - - - - - - - - 1;:Phone Nurrber-------- -------------- ------ 16 - “’-Pile Tape (Fastener Tape)--- ---------------- -- 26Positive Stop ------- -------------- ------ 36

Quality Assurance Provisions- - - - - - - - - - - - - - - - - - - - 116

Ratings ---------- -------------- ------ 20Receptacle Push-Out,----- --------------- ---- 68Requester FSCM--------- ---------------- --Requester’s Name------ -------------- ------ 1:Resistance toAttachmentWear -------------- ----- 70Resistance to Brittleness- -------------’- ------ 70Resistance to Chemical Reagents - - - - - - - - - - - - - - - - - -Resistance to Hot Soap Solution - - - -“- - - - - - - - - - - - - - ;;Resistance to Solvents----- ---------------- -- 74Revision of AEDPS Document.(Number) - - - - - - - - - - - - - - - - 18

Salt Fog-------------- ---------------- 78Scope -------------- ----------------- 18Screw Threads ---------- -----------------Shear Fatigue ---------- ----------------- ::

*

162


1


INDEX (CONT)

F’acJg

I

,

●

10

Shear Strength ---------- --------------::-Sheet Pull-Up----------- -----------------Sheet Separation ------ -------------- ------Shock------------- --------------- -;--Size ------------ -------------- ----=-Slide Fastener Size---- -------------- ----:;-Slide Fastener Tape Construction - - - - - - - - - - - - - - - - .--Slide Fastener Type-Source Table - - - -Special Tools- - - -Street/Building- - -Stress Corrosion - -Stud Push-Out- - - -Style--------Superseded Document-Surface Roughness- -Surface Texture- - -System Application -

---- ---- ---- ---- ---- -.------- ---- ---- ---- ---- -------- ---- ---- ---- ---- ---- ----- ---- ---- ---- ---- -------- ---- ---- ---- ---- -------- ---- ---- ---- ---- -------- ---- ---- ---- ---- -------- ---- ---- ---- ---- -------- ---- ---- ---- ---- -------- ---- ---- ---- ---- -------- ---- ---- ---- ---- ----

Tabulated Characteristics- - - - - - - --- - - - - - - - - - --- - -Tape Ends, Anti-Raveling Treatment - - - - - - - - - - - - - ----- -Temperature, High--------- -------------------Temperature, Low -------- ---------------- --Temperature Rating ------- ----------------- -Tensile Strength --------- -----------------Thickness of Metallic Coatings - - - - - - - - - - - - - - - - - - -Torque ------------- ---------------- --Type ------------- --------------- ----

8284

;:2030283018421692

%116943616

::9698

1;:10210420

Units of Measure ----- -- ------------ ------18,22Unlocking---------- -------------- ------ 34

Vibration--------- -------------- ------- 108

Water Resistance Treatment- -------------- ------ 110Weight/Mass---------- --------------- ----Wire Staking Strength (Receptacle Strip Fastener)- - - - - - - -- - 1;;Workmanship--------- ------ -------- ------ 114

w.S. GOVERNMENT PRINTINQWWE 1979-3J32z1m3

163


DOD-STD-35-23A(MI)

The digital copy of DOD-STD-35-23A(MI), dated 9 March 1979 does not include the foldout page for theSpecification Requirement Sheet (SRS). If you need a copy it must be ordered separately, please fax thispage to 215-697-9398 and include your complete mailing address below.

165-166


DOD-STD-35-23A (MI)

Thedigital copyof DOD. STD-35-23A(MI), dated 9March 1979does notinclude the foldout page for theSpecification Requirement Sheet (SRS).Ifyou need a copy it must be ordered separately, please fax thispage to 215-697-9398 and include your complete mailing address below.

167-168


;

3

iTANDARDIZATION DOCUMENT IMPROVEMENT PROPOSAL I OMB ApprovalNo. 22-R255

{STRUCTIONS Thepurpo$e of this form is to solicit beneficial comments which will help achieve procure.mt of suitable products at reasonable cost and minimum delay, or will otherwise enhance use of the documentOD contractors, government activities, m manufacturers/ ve.dors who are prospective suppliers of the productr. invited m submit comments to the go.emrne.t, Fold on lines o. reverse side, staple i. comer, and se.d torepari. g activity. Comments submitted on this form do not constitute or imply authorization m waive any.rtio. of the referenced document(s) or t. amend . ..tractuel requirements. Attach any pertinent data whichw be of .s. i. improving this document. If there are additional papers, attach to form and place both in . .n.cloy addressed to preparing activity.

CUMENT ,cIENT, FIER AND TITLE

Fasteners DOD-STD-35-23A(MI)ME OF ORGANIZATION AND ADDRESS CONTRACT NUMBER

MATERIAL PROCURED UNDER A

DolREc TGOvERNM=. TcONTRAc T Os. BcO. Te. c’

HAS ANY PART OF THE DOCUMENT CREATED I= ROBLEMSOR REQUIRED IN TERPRETS. TIO’NIN PROCUREMENT

uSE?

A. GIVE . . . . . . . . . .“Me. R A.. .0,.,. .,

,. ,6. OMM. NO AT, ONS ,0. con.,.,,.. ,“, .6,,.,,..,. s

COMMENTSON ANY DOCUMENT REQUIREMENT CO WDERED TOO RIGID

IS THE DO CUMENr RESTRICTIVE,

o ... D .0 (If<<i’.s,s,in what way?)

REMARKS

i3Ml TTED BY (Pr)n,, do, ,,ped name ar, daddr., s - 0.,,...,) TELEPHONE NO.

DATE

m ,..,, . .--

u ,;;:”,214<0 ..,, ..,, ..,,,0. 0. , ,.. s, ... ,,” MA” ., “s,.


‘ ,/

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OFFICIAL BuSINESSPENALTY FOR PRl VATEUSES300

Commander,J, U.S. Army Missile

ATTN: DRDMI-ESDRedstone Arsenal,

o~* t

PoSTAGE AND FEES PAID

DEPARTMENT OF THE ARMY

DOD–314 ~

R & D Command

AJabama 35809

.:’:-’\ ‘ - ‘“””w“, --- ,

.

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