Aerospace - Bolts, with MJ threads, made of alloy steel, strength class 1 250 MPa - Procurement specification

ISO 5857:2008 specifies the characteristics and quality assurance requirements for MJ threads bolts made of alloy steel, of strength class 1 250 MPa, for aerospace construction. ISO 5857:2008 is applicable whenever it is referenced in a definition document.

Aéronautique et espace — Vis à filetages MJ, en acier allié, de classe de résistance 1 250 MPa — Spécification d'approvisionnement

General Information

Status
Published
Publication Date
10-Aug-2008
Current Stage
9060 - Close of review
Completion Date
04-Mar-2031

Relations

Effective Date
15-Apr-2008

Overview

ISO 5857:2008 - "Aerospace - Bolts, with MJ threads, made of alloy steel, strength class 1 250 MPa - Procurement specification" defines the procurement, inspection and quality requirements for aerospace bolts with MJ threads manufactured from alloy steel and rated to strength class 1 250 MPa. It is a procurement specification meant to be invoked whenever referenced in a definition document (e.g., drawing or contract). The standard focuses on characteristics, manufacturing controls and quality assurance to ensure safe, repeatable performance in aerospace applications.

Key topics and technical requirements

  • Scope and applicability: Applies to MJ-thread bolts used in aerospace construction; applies when referenced in a definition document.
  • Material and strength: Bolts of alloy steel, strength class 1250 MPa; material conformity is verified per the definition document and material standards.
  • Dimensions and threads: Dimensional and thread limits follow the definition document and related MJ thread standards; threads must be formed by single rolling after full heat treatment.
  • Manufacturing controls:
    • Forging (hot or cold) prior to heat treatment with uniform temperature control for hot forging.
    • Heat treatment rules (limited number of cycles) and stress-relieving after grinding but before thread/fillet rolling.
    • Fillet cold-rolling between head and shank to remove machining marks and produce specified cold work (visual and dimensional checks).
    • Surface roughness and coatings per the definition document and ISO surface texture methods.
  • Mechanical tests: Tensile strength and double-shear strength requirements (referenced test methods such as ISO 7961 and ISO 6892); test temperature is ambient unless otherwise stated.
  • Quality assurance and inspection:
    • Qualification inspection (e.g., 25 bolts by simple random sampling) and production acceptance inspections per lot.
    • Sampling plans and acceptance criteria (AQL, LQ) consistent with ISO 2859-1.
    • Option to use Statistical Process Control (SPC) in lieu of final sampling if validated and approved.
    • Quality records retention for a minimum of 10 years.

Practical applications and users

ISO 5857:2008 is used by:

  • Aerospace fastener manufacturers for production and process control.
  • OEMs, suppliers and procurement teams specifying bolt requirements on drawings and contracts.
  • Quality, inspection and certification authorities responsible for qualification and lot acceptance.
  • Design and structural engineers who require verified mechanical performance data for fastening systems.
  • Maintenance/repair organizations sourcing replacement fasteners to meet aerospace traceability and safety requirements.

Keywords: ISO 5857:2008, aerospace bolts, MJ threads, alloy steel bolts, strength class 1250 MPa, procurement specification, quality assurance, sampling plan, heat treatment, tensile strength, statistical process control (SPC).

Related standards

Normative references include: ISO 2859-1, ISO 4288, ISO 5855-2 (MJ threads limits), ISO 6507-1, ISO 6508-1, ISO 6892, ISO 7961, ISO 7966, ISO 7870-1, ISO 8258 and ISO/TR 13425.

Standard

ISO 5857:2008 - Aerospace -- Bolts, with MJ threads, made of alloy steel, strength class 1 250 MPa -- Procurement specification

English language
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Frequently Asked Questions

ISO 5857:2008 is a standard published by the International Organization for Standardization (ISO). Its full title is "Aerospace - Bolts, with MJ threads, made of alloy steel, strength class 1 250 MPa - Procurement specification". This standard covers: ISO 5857:2008 specifies the characteristics and quality assurance requirements for MJ threads bolts made of alloy steel, of strength class 1 250 MPa, for aerospace construction. ISO 5857:2008 is applicable whenever it is referenced in a definition document.

ISO 5857:2008 specifies the characteristics and quality assurance requirements for MJ threads bolts made of alloy steel, of strength class 1 250 MPa, for aerospace construction. ISO 5857:2008 is applicable whenever it is referenced in a definition document.

ISO 5857:2008 is classified under the following ICS (International Classification for Standards) categories: 49.030.20 - Bolts, screws, studs. The ICS classification helps identify the subject area and facilitates finding related standards.

ISO 5857:2008 has the following relationships with other standards: It is inter standard links to ISO 5857:1988. Understanding these relationships helps ensure you are using the most current and applicable version of the standard.

You can purchase ISO 5857:2008 directly from iTeh Standards. The document is available in PDF format and is delivered instantly after payment. Add the standard to your cart and complete the secure checkout process. iTeh Standards is an authorized distributor of ISO standards.

Standards Content (Sample)


INTERNATIONAL ISO
STANDARD 5857
Second edition
2008-08-15
Aerospace — Bolts, with MJ threads,
made of alloy steel, strength class
1 250 MPa — Procurement specification
Aéronautique et espace — Vis à filetages MJ, en acier allié, de classe
de résistance 1 250 MPa — Spécification d'approvisionnement

Reference number
©
ISO 2008
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ii © ISO 2008 – All rights reserved

Contents Page
Foreword. iv
1 Scope . 1
2 Normative references . 1
3 Terms and definitions. 2
4 Quality assurance. 3
4.1 General. 3
4.2 Qualification inspection conditions. 4
4.3 Acceptance inspection conditions . 4
4.4 Use of “statistical process control (SPC)”. 4
5 Requirements . 5
Annex A (informative) Cross-sectional areas and formulae for tensile, tension fatigue and stress
durability loads . 21
Annex B (informative) Cross-sectional areas and formulae for double shear loads . 23

Foreword
ISO (the International Organization for Standardization) is a worldwide federation of national standards bodies
(ISO member bodies). The work of preparing International Standards is normally carried out through ISO
technical committees. Each member body interested in a subject for which a technical committee has been
established has the right to be represented on that committee. International organizations, governmental and
non-governmental, in liaison with ISO, also take part in the work. ISO collaborates closely with the
International Electrotechnical Commission (IEC) on all matters of electrotechnical standardization.
International Standards are drafted in accordance with the rules given in the ISO/IEC Directives, Part 2.
The main task of technical committees is to prepare International Standards. Draft International Standards
adopted by the technical committees are circulated to the member bodies for voting. Publication as an
International Standard requires approval by at least 75 % of the member bodies casting a vote.
Attention is drawn to the possibility that some of the elements of this document may be the subject of patent
rights. ISO shall not be held responsible for identifying any or all such patent rights.
ISO 5857 was prepared by Technical Committee ISO/TC 20, Aircraft and space vehicles, Subcommittee SC 4,
Aerospace fastener systems.
This second edition cancels and replaces the first edition (ISO 5857:1988) which has been technically revised.

iv © ISO 2008 – All rights reserved

INTERNATIONAL STANDARD ISO 5857:2008(E)

Aerospace — Bolts, with MJ threads, made of alloy steel,
strength class 1 250 MPa — Procurement specification
1 Scope
This International Standard specifies the characteristics and quality assurance requirements for MJ thread
bolts made of alloy steel, of strength class 1 250 MPa, for aerospace construction.
It is applicable whenever it is referenced in a definition document.
2 Normative references
The following referenced documents are indispensable for the application of this document. For dated
references, only the edition cited applies. For undated references, the latest edition of the referenced
document (including any amendments) applies.
ISO 2859-1:1999, Sampling procedures for inspection by attributes — Part 1: Sampling schemes indexed by
acceptance quality limit (AQL) for lot-by-lot inspection
ISO 4288, Geometrical Product Specifications (GPS) — Surface texture: Profile method — Rules and
procedures for the assessment of surface texture
ISO 5855-2, Aerospace — MJ threads — Part 2: Limit dimensions for bolts and nuts
ISO 6507-1, Metallic materials — Vickers hardness test — Part 1: Test method
ISO 6508-1, Metallic materials — Rockwell hardness test — Part 1: Test method (scales A, B, C, D, E, F, G, H,
K, N, T)
ISO 6892, Metallic materials — Tensile testing at ambient temperature
ISO 7870-1, Control charts — Part 1: General guidelines
ISO 7961, Aerospace — Bolts — Test methods
ISO 7966, Acceptance control charts
ISO 8258, Shewhart control charts
ISO/TR 13425, Guidelines for the selection of statistical methods in standardization and specification
3 Terms and definitions
For the purposes of this document, the following terms and definitions apply.
3.1
production batch
quantity of finished bolts, manufactured using the same process, from a single material cast (single heat of
alloy), having the same definition document number, the same thread and diameter code, heat-treated
together to the same specified condition and produced as one continuous run
3.2
inspection lot
quantity of bolts from a single production batch having the same definition document number
3.3
definition document
document specifying directly or indirectly all the requirements for bolts
NOTE The definition document may be an International Standard, an in-house standard or a drawing.
3.4
crack
rupture in the material which may extend in any direction and which may be intercrystalline or transcrystalline
in character
3.5
seam
open surface defect
3.6
lap
surface defect caused by folding over metal fins or sharp corners and then rolling or forging them into the
surface
3.7
crevice
hollow area at thread crest
3.8
inclusions
non-metallic particles originating from the material manufacturing process
NOTE These particles can be isolated or arranged in strings.
3.9
sampling plan
plan according to which one or more samples are taken in order to obtain information and possibly reach a
decision
NOTE In this International Standard, each sampling plan specifies the number of bolts to be inspected as a function
1)
of the size of the batch and the acceptance number [number of defective items acceptable (Ac) ].
3.10
simple random sampling
sampling of n items from a population of N items in such a way that all possible combinations of n items have
the same probability of being chosen

1) Ac = acceptance number (supplementary information taken from ISO 2859-1).
2 © ISO 2008 – All rights reserved

3.11
critical defect
defect that, according to judgement and experience, is likely to result in hazardous or unsafe conditions for
individuals using, maintaining or depending upon the considered product (bolt), or that is likely to prevent
performance of the function of a major end item
3.12
major defect
defect, other than critical, that is likely to result in failure or to reduce materially the usability of the considered
product (bolt) for its intended purpose
3.13
minor defect
defect that is not likely to materially reduce the usability of the considered product (bolt) for its intended
purpose, or that constitutes a departure from the established specification, having little bearing on the effective
use or operation of this product
3.14
limiting quality
LQ
〈sampling plan〉 quality limit which corresponds to a specified and relatively low probability of acceptance
NOTE 1 It is the limiting lot quality characteristic that the consumer is willing to accept with a low probability that a lot of
this quality would occur.
NOTE 2 For the purposes of this International Standard, the limiting quality quoted in Table 4 corresponds to a
probability of acceptance of 10 %.
3.15
acceptable quality limit
AQL
maximum percent defective (or maximum number of defects per hundred units) that, for purposes of sampling
inspection, can be considered satisfactory as a process average
NOTE Variant: quality limit which, in a sampling plan, corresponds to a specified but relatively high probability of
acceptance.
4 Quality assurance
4.1 General
The manufacturer shall be capable of providing a continuous production of bolts complying with the quality
requirements specified in this International Standard. It is recommended that the manufacturer be certified to a
recognized quality management system. The certification authority may be the prime contractor.
2)
The purpose of qualification inspections of bolts is to check that the design and manufacturing conditions of
a bolt allow it to satisfy the requirements of this International Standard.
Quality documentation for parts produced in accordance with this International Standard shall be maintained
for a minimum period of 10 years.
Qualification of the bolts shall be granted by the Certification Authorities in the purchaser's country, or their
appointed representative, who may be the prime contractor.

2) In order to simplify the text, the term “inspections” used in this International Standard also refers to “inspections and
tests”.
The purpose of a production acceptance inspection of a bolt is to check, as simply as possible, using a
method which is inexpensive but representative of the actual conditions of use, with the uncertainty inherent in
statistical sampling, that the bolt satisfies the requirements of this International Standard.
Production acceptance inspections shall be carried out by the manufacturer or under his responsibility.
4.2 Qualification inspection conditions
Unless otherwise specified, the inspection shall be carried out on:
⎯ each type and diameter of bolt;
⎯ 25 bolts selected from a single inspection lot by simple random sampling.
The test programme may possibly be reduced, or the qualification granted, without inspection: any such
decision shall be based on the results obtained on similar types and diameters of bolts provided that the
design and manufacturing conditions are identical.
The inspections shall be repeated on any bolt if the manufacturing conditions have been modified.
Table 2 indicates the allocation of bolt samples for the inspections.
4.3 Acceptance inspection conditions
Inspections shall be carried out on each production batch or inspection lot. Bolts from the batch or lot to be
inspected shall be selected by simple random sampling.
Each bolt may be submitted to several inspections, provided that none of characteristics to be verified has
been previously altered during any of these inspections.
The bolts to be subjected to destructive inspections may be those on which non-destructive inspections have
been carried out.
If a more stringent inspection is deemed necessary, all or part of the qualification inspections may be
performed during the acceptance inspections. In this case, the number of bolts submitted is the same as that
submitted for the qualification inspection.
Production batches or inspection lots declared unacceptable after the production acceptance inspections shall
be submitted for re-inspection only after all the defective units have been removed and/or defects have been
corrected. In this case, the attribute(s) that caused the rejection shall be verified using a sample of twice the
normal size with the same number of defective items acceptable.
4.4 Use of “statistical process control (SPC)”
When a characteristic is obtained by a controlled statistical process, the manufacturer has the option, in order
to declare conformity of the characteristic, to forgo the final systematic sampling provided in this International
Standard, if he is capable of formally justifying this choice by using ISO/TR 13425 and the standards quoted
in it as a basis.
This justification will include the following phases:
⎯ analysis of the key characteristics of the product;
⎯ analysis of the risks for each implemented process;
⎯ determination of the parameters and/or characteristics to be respected under SPC;
⎯ determination of the capabilities of each process;
4 © ISO 2008 – All rights reserved

⎯ drawing up of an inspection plan and integration in the manufacturing process;
⎯ drawing up of routes and control charts (ISO 7966, ISO 7870-1, ISO 8258);
⎯ use of control charts for data consolidation;
⎯ determination of the audits to be run and the control to be carried out to ensure reliability of the device.
To be usable in production, this process shall be validated beforehand by the qualifying body, either during the
qualification phase, or a posteriori according to the case, by analysing the justificatory file and the results of
the qualification inspections such as provided in Clause 5. Such an SPC process is not applicable to
destructive tests apart from the stress durability test.
5 Requirements
The requirements of this International Standard are given in Table 1 and, unless otherwise specified, they
apply to bolts that are ready for use. The test temperature, unless otherwise specified, shall be the ambient
temperature. These requirements complement the requirements of all other standards or specifications
referenced in the definition document.
Table 1 — Requirements and test methods
Inspection and Desig- Sample
Subclause Characteristic Requirement
a
test method nation size
5.1 Material In accordance with the definition See material standard. As required
document by semi-
finished
product
5.2 Dimensions In accordance with the definition Standard gauging Q 20
document
A
Tables 3
and 4
5.3 Manufacturing
5.3.1 Forging The heads of the bolts shall be According to the Q
formed by a hot or cold forging manufacturing route

process before heat treatment.
In the case of hot forging, the The equipment used
equipment shall ensure an shall be approved.
adequate and uniform temperature
throughout the production batch.
5.3.2 Heat treatment The forged blanks shall be heat- According to the Q
treated to produce the properties process route

required by the definition
The equipment used
document. Blanks shall not be
shall be approved.
heat-treated more than twice.
5.3.3
Removal of If machining is required, it is
surface necessary to respect the
contamination requirements of 5.5.1.
(bearing face
and shank)
5.3.4 Stress-relieving After grinding, but before thread
and fillet rolling, bolts shall be
stress-relieved at a temperature
higher than 190 °C and (20 to
30) °C below the final tempering
temperature for at least 2 h.
Table 1 (continued)
Inspection and Desig- Sample
Subclause Characteristic Requirement
a
test method nation size
5.3.5 Fillet between The fillet radius shall be cold-rolled Visual examination at Q 5
head and shank after heat treatment and machining a suitable
A Tables 3
so as to remove all visual signs of magnification of
and 4
machining and to create superficial 10× to 20× and
cold working. dimensional check
The deformation shall not exceed
the values given in Figure 1.
The requirements apply to bolts
except the following:
a) bolts threaded to head;
b) bolts with a nominal diameter
< 5 mm.
5.3.6 Threads Formed by a single rolling process According to the Q
after full heat treatment manufacturing route

5.3.7 Surface In accordance with the definition ISO 4288 Q 5
roughness document
Visual examination
A Tables 3
and 4
5.3.8 Surface coating In accordance with the definition See surface coating Q 5
document standard.
A Tables 3
and 4
5.4 Mechanical
properties
5.4.1 Tensile strength See Table 5. On bolts: ISO 7961 Q 5
The requirements apply to bolts On test specimen A for bolts, Table 6
except the following: (when tests do not not for or Table 7
apply to bolts as specimens
a) protruding head bolts of grip
indicated in
length < twice the nominal shank
“Requirement”
diameter;
column): ISO 6892
b) countersunk head bolts of grip
The test specimens
length < two and a half times the
are to be produced
nominal shank diameter;
from the same
c) bolts threaded to head of overall
material batch as the
length < three times the nominal
...

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記事タイトル:ISO 5857:2008 - 航空宇宙 - 合金鋼製,1,250 MPa 強度クラスのMJスレッドボルト - 調達仕様 記事内容:ISO 5857:2008は、航空宇宙構造に使用される合金鋼製、1,250 MPaの強度クラスを備えたMJスレッドボルトの特性と品質保証要件を規定しています。ISO 5857:2008は、定義文書で参照される場合に適用されます。

ISO 5857:2008 is a procurement specification that outlines the characteristics and quality assurance requirements for MJ thread bolts made of alloy steel, specifically those with a strength class of 1 250 MPa, for use in aerospace construction. This standard applies when referenced in any definition document.

기사 제목: ISO 5857:2008 - 항공우주 - 1,250 MPa 인장강도의 합금강 MJ 나사 볼트 - 조달 사양 기사 내용: ISO 5857:2008은 항공우주 건설을 위해 1,250 MPa의 인장강도를 가지는 합금강 MJ 나사 볼트의 특성과 품질 보증 요구사항을 규정합니다. ISO 5857:2008은 정의 문서에서 참조될 때 적용됩니다.