Abs0112 PDF

 

 

ABS0112 Issue 4 Page 1 of 7 October 2014

Aerospace series Rivet, blind 100°, CSK

When this standard is applied, a careful check must be made as to whether any protective rights exist. This standard issuer hereby disclaims any liability for infringement of patent or design rights resulting from the use of this standard.

Published and distributed by : AIRBUS INDUSTRIE AIRBUS S.A.S. ENGINEERING DIRECTORATE 31707 BLAGNAC Cedex FRANCE 

Copyright reserved

Ref. no. ABS0112

 

 ABS0112 Issue 4

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Contents

1  Scope  2  Normative references   3  Requirements  4  Designation  5  Marking 

6  Technical specification 

 

 ABS0112  Issue 4

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1 Scope This standard specifies the dimensions, tolerances, required characteristics and the mass of a blind, 100º flush shear head, self-locking rivet for nut plate installation or tacking purposes in aerospace applications..

2 Normative references This Airbus Standard incorporates by dated or undated reference provisions from other publications. All normative references cited at the appropriate places in the text are listed hereafter. For dated references, subsequent amendments to or revisions of any these publications apply to this Airbus Standard only when incorporated in it by amendment of revision. For undated references, the latest issue of the publication referred to shall be applied.  ASTM A493

Standard Specification for Stainless Steel Wire and Wire Rods for Cold Heading and Cold 1 Forging  

 AMS-QQ-P-416

Plating, Cadmium (Electrodeposited)

 AMS2700

Passivation of Corrosion Resistant Steels  

 AMS5731

Steel, Corrosion and Heat Resistant, Bars, Wire, Forgings, Tubing, and Rings 15Cr 25.5Ni 1.2Mo 2.1Ti 0.006B 0.30V, Consumable Electrode Melted, 1800°F (982°C) 2 Solution Heat Treated  

MIL-PRF-46010

Lubricant, solid film, heat cured, corrosion inhibiting NATO code -S-1738

MIL-STD-129 NASM25027

Military marking for shipment and storage 4 Nut, self-locking, 250°F, 450°F and 800°F  

SAE AS5272

Lubricant, Solid Film, Heat Cured, Corrosion Inhibiting, Procurement Specification

1

2

3

 Published by: American Society for Testing and Materials (ASTM), 100 Barr Harbor Drive, West Conshohocken, PA 194282959, USA 2 Published by: Society of Automotive Engineers (SAE), 400 Commonwealth Drive, Warrendale, PA 15096-0001, USA 3  Published by: Department of Defense (DoD), the Pentagon, Washington, W ashington, D.C., 20307, USA 4  Published by: Aerospace Industries Association of America, Inc. (AIA), 1250 Eye Street, N.W., Washington, D.C. 20005-3924, USA

 

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3 Requirements 3.1

Configuration, dimensions, tolerances and mass

The configuration, dimensions, tolerances and mass shall be in accordance with figure 1, table 1 and table 2..

Z

F L

      °       1      ±

C

        °       0       0       1

not to exceed øD

      D      ø

    R

Head marking

      1

stem

      A       A      ø      ø

B grip

NOTE: When installing, stem pulls completely through and leaves hollow rivet.

Marking see clause 5

sleeve

 

Figure 1  – Configuration

Table 1: Dimensions and tolerances

Diameter code  -24  -32 

Nominal Diameter 2,40

Ø D  Min  2,34

Max  2,46

ØA theoretical  Min  Max  4,45 4,65

Ø A1 

B 

Min  3,84

Ref   0,91

Dimensions in millimeters (inch) Hole C  R  Z  diameter   Min  Max  Min  Max  0,05

0,25

2,34

2,46

(.094) 

(.092)  (.097)  (.175)  (.183)  (.151)  (.036) 

(.092) 

(.097) 

3,20 (.126) 

3,12 3,25 5,62 5,82 5,00 1,07 (.002)  (.010)  3,12 (.123)  (.128)  (.221)  (.229)  (.197)  (.042)  (.123) 

3,25 (.128) 

 

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Table 2: Dimensions, tolerances and mass

Length code

Diameter code Grip range

L

-24 F

Min

Max

Max

Max

1,60

3,20

5,16

7,14

(.063) 3,20  

(.126) 4,78  

(.203) 6,73  

(.281) 8,71  

(.126)  4,78

(.188)  6,38

(.265)  8,33

(.343)  10,29

(.188)  6,38

(.251)  7,95

(.328)  9,91

(.405)  11,89

(.251)  7,95

(.313)  9,55

(.390)  11,51

(.468)  13,46

a

(.313)  9,55

(.376)  11,10

(.453)  13,08

(.530)  15,06

 a

(.376)  11,10

(.437)  12,70

(.515)  14,68

(.592)  16,66

 a

(.437)  12,70

(.500)  14,30

(.578)  16,26

(.655)  18,24

 a

(.500)  14,30

(.563)  15,90

(.640)  17,86

(.718)  19,84

 a

(.563)  15,90

(.626)  17,42

(.703)  19,43

(.780)  21,41

 a

(.626)  17,42

(.686)  19,05

(.765)  21,03

(.843)  22,99

(.686) 

(.750) 

(.828) 

(.905) 

02  03  04  05  06  07   08   09   10   11   12  

Dimensions in millimeters (inch)   -32 L F Mass M ass (kg / 1000 Max Max pieces)

Mass M ass (kg / 1000 pieces)

5,89

8,53

(.232) 7,49  

(.318) 10,14  

(.295)  9,07

(.381)  11,71

(.357)  10,67

(.443)  13,31

(.420)  12,24

(.506)  14,88

(.482)  13,84

(.568)  16,49

(.544)  15,42

(.630)  18,06

(.607)  17,02

(.693)  19,66

(.670)  18,59

(.755)  21,23

(.732)  20,19

(.818)  22,84

(.795)  22,23

(.899)  24,41

(.857) 

(.961) 

0,100  0,131  0,163  0,195  0,227  0,258  0,290  0,322  0,354  0,385  0,417 

0,133  0,174  0,217  0,250  0,302  0,344  0,387  0,429  0,472  0,513  0,556 

a These lengths are only available on special order. Consult standards group prior to call up

3.2

Material and surface treatment

The material and surface treatment shall be in accordance with table 3. These blind rivets will be supplied in lubricated condition and must not be degreased prior to installation.

Table 3: Material and surface treatment Material code

Material Sleeve

None

C

T

UNS S66286 corrosion resisting steel per  AMS5731

Finish Stem

Sleeve

Stem

Solid film lubricant per MIL-PRF-46010 or Passivation per SAE AS5272 plus  AMS2700 passivation per  AMS2700 UNS S30500 corrosion Cadmium plating per resisting steel per  AMS-QQ-P-416 type II,  ASTM A493 class 2, dyed green Passivation per plus lubrication  AMS2700. Lubrication optional Passivation per  AMS2700 plus lubrication st

P

Inactive for design as of 1  October 2014, existing stocks may be used until exhausted. Replaced Repla ced by material code “none”  “none”  

 

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4 Designation This type of standard shall be designated according to the philosophy of the following example: Description block Rivet, blind, 100° CSK

Identity block ABS0112

Number of this standard Diameter code (see table 1) Length code (see table 2) Material code (see table 3)

5 Marking MIL-STD-129.

6 Technical specification Torque- and push-out strength to meet or exceed the requirements of NASM25027.

-24

-02

T

 

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RECORD OF REVISIONS

Issue

Clause modified  All 2

4

Description of modification New standard. Revision of normative references.

3.1

Figure 1 modified. Table 1 updated, rounding errors corrected, dimensions A1 and C added. Hole diameters from former separate table added. Dimensions F and L updated. Table 2 updated, rounding errors corrected.

3.2

Table 3: Finish of sleeve and stem s tem revised, code “P” replaced.  replaced.   Revision of normative references. For code “C” the Finish for sleeve: Text “dyed green” added.  added.  

10/14

5

Marking standard added.

6

Technical specification added.