EN 2884:2024

Aerospace series - Screws, pan head, offset cruciform recess, coarse tolerance normal shank, short thread, in titanium alloy, anodized, MoS2 lubricated - Classification: 1 100 MPa (at ambient temperature)/315 °C

This document specifies the characteristics of screws, pan head, offset cruciform recess, coarse tolerance normal shank, short thread, in titanium alloy, anodized, MoS2 lubricated.
Classification: 1 100 MPa /315 °C ·

Luft- und Raumfahrt - Flachkopfschrauben mit Flügelkreuzschlitz, grobe Schafttoleranz, kurzes Gewinde, aus Titanlegierung, anodisiert, MoS2-geschmiert - Klasse: 1 100 MPa (bei Raumtemperatur)/315 °C

Dieses Dokument legt die Eigenschaften von Flachkopfschrauben mit Flügelkreuzschlitz, grobe Schafttoleranz und kurzem Gewinde, aus Titanlegierung, anodisiert, MoS2-geschmiert, fest.

Série aérospatiale - Vis à tête cylindrique, à empreinte cruciforme déportée, tige normale à tolérance large, filetage court, en alliage de titane, anodisées, lubrifiées au MoS2 - Classification : 1 100 MPa (à température ambiante)/315 °C

Le présent document spécifie les caractéristiques des vis à tête cylindrique, à empreinte cruciforme déportée, tige normale à tolérance large, filetage court, en alliage de titane, anodisées, lubrifiées au MoS2.
Classification : 1 100 MPa /315 °C.

Aeronavtika - Vijaki, z valjasto glavo, križno zarezo, široko toleranco, s kratkim navojem, iz titanove zlitine, anodizirani, mazani z MoS2 - Klasifikacija: 1100 MPa (pri temperaturi okolice)/315 °C

General Information

• Status: Published
• Publication Date: 09-Jul-2024
• Withdrawal Date: 02-May-2022
• ICS: 49.030.20 - Bolts, screws, studs
• Technical Committee: ASD-STAN - Aerospace
• Drafting Committee: ASD-STAN/D 3/S 2 - Fasteners
• Current Stage: 6060 - Definitive text made available (DAV) - Publishing
• Start Date: 10-Jul-2024
• Completion Date: 10-Jul-2024
• Ref Project: SIST EN 2884:2024 - Aerospace series - Screws, pan head, offset cruciform recess, coarse tolerance normal shank, short thread, in titanium alloy, anodized, MoS2 lubricated - Classification: 1 100 MPa (at ambient temperature)/315 °C

Relations

• Replaces: EN 2884:1996 - Aerospace series - Screws, pan head, offset cruciform recess, coarse tolerance normal shank, short thread, in titanium alloy, anodized, MoS2 lubricated - Classification: 1 100 MPa (at ambient temperature)/315 °C
• Effective Date: 04-Feb-2015

Standards Content (Sample)

SLOVENSKI STANDARD
01-oktober-2024
Aeronavtika - Vijaki, z valjasto glavo, križno zarezo, široko toleranco, s kratkim
navojem, iz titanove zlitine, anodizirani, mazani z MoS2 - Klasifikacija: 1100 MPa
(pri temperaturi okolice)/315 °C
Aerospace series - Screws, pan head, offset cruciform recess, coarse tolerance normal
shank, short thread, in titanium alloy, anodized, MoS2 lubricated - Classification: 1 100
MPa (at ambient temperature)/315 °C
Luft- und Raumfahrt - Flachkopfschrauben mit Flügelkreuzschlitz, kurzes Gewinde, aus
Titanlegierung, anodisiert, MoS2 geschmiert - Klasse: 1 100 MPa (bei
Raumtemperatur)/315 °C
Série aérospatiale - Vis à tête cylindrique, à empreinte cruciforme déportée, tige normale
à tolérance large, filetage court, en alliage de titane, anodisées, lubrifiées MoS2 -
Classification : 1 100 MPa (à température ambiante)/315 °C
Ta slovenski standard je istoveten z: EN 2884:2024
ICS:
49.025.30 Titan Titanium
49.030.20 Sorniki, vijaki, stebelni vijaki Bolts, screws, studs
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

EN 2884
EUROPEAN STANDARD
NORME EUROPÉENNE
July 2024
EUROPÄISCHE NORM
ICS 49.030.20 Supersedes EN 2884:1996
English Version
Aerospace series - Screws, pan head, offset cruciform
recess, coarse tolerance normal shank, short thread, in
titanium alloy, anodized, MoS2 lubricated - Classification:
1 100 MPa (at ambient temperature)/315 °C
Série aérospatiale - Vis à tête cylindrique, à empreinte Luft- und Raumfahrt - Flachkopfschrauben mit
cruciforme déportée, tige normale à tolérance large, Flügelkreuzschlitz, kurzes Gewinde, aus
filetage court, en alliage de titane, anodisées, lubrifiées Titanlegierung, anodisiert, MoS2 geschmiert - Klasse: 1
au MoS2 - Classification : 1 100 MPa (à température 100 MPa (bei Raumtemperatur)/315 °C
ambiante)/315 °C
This European Standard was approved by CEN on 26 May 2024.

CEN members are bound to comply with the CEN/CENELEC Internal Regulations which stipulate the conditions for giving this
European Standard the status of a national standard without any alteration. Up-to-date lists and bibliographical references
concerning such national standards may be obtained on application to the CEN-CENELEC Management Centre or to any CEN
member.
This European Standard exists in three official versions (English, French, German). A version in any other language made by
translation under the responsibility of a CEN member into its own language and notified to the CEN-CENELEC Management
Centre has the same status as the official versions.

CEN members are the national standards bodies of Austria, Belgium, Bulgaria, Croatia, Cyprus, Czech Republic, Denmark, Estonia,
Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway,
Poland, Portugal, Republic of North Macedonia, Romania, Serbia, Slovakia, Slovenia, Spain, Sweden, Switzerland, Türkiye and
United Kingdom.
EUROPEAN COMMITTEE FOR STANDARDIZATION
COMITÉ EUROPÉEN DE NORMALISATION

EUROPÄISCHES KOMITEE FÜR NORMUNG

CEN-CENELEC Management Centre: Rue de la Science 23, B-1040 Brussels
© 2024 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 2884:2024 E
worldwide for CEN national Members.

Contents Page
European foreword . 3
1 Scope . 4
2 Normative references . 4
3 Terms and definitions . 4
4 Required characteristics . 5
4.1 Configuration – Dimensions – Mass . 5
4.2 Tolerances of form and position . 7
4.3 Materials . 7
4.4 Surface treatment . 7
5 Designation . 7
6 Marking . 8
7 Technical specification . 8
7.1 General . 8
7.2 Approval of manufacturers . 8
7.3 Qualification of screws . 8
Annex A (informative) Evolution sheet . 9
Bibliography. 10

European foreword
This document (EN 2884:2024) has been prepared by the Aerospace and Defence Industries
Association of Europe — Standardization (ASD-STAN).
After enquiries and votes carried out in accordance with the rules of this Association, this document has
received the approval of the National Associations and the Official Services of the member countries of
ASD-STAN, prior to its presentation to CEN.
This European Standard shall be given the status of a national standard, either by publication of an
identical text or by endorsement, at the latest by January 2025, and conflicting national standards shall
be withdrawn at the latest by January 2025.
Attention is drawn to the possibility that some of the elements of this document may be the subject of
patent rights. CEN shall not be held responsible for identifying any or all such patent rights.
This document supersedes EN 2884:1996.
This document includes the following significant technical changes with respect to EN 2884:1996:
— normative references updated;
— Clause 3 “terms and definitions” added;
— in Table 3, “Drive” was changed according to ISO 14275 and ISO 14276;
— 7.2 “
...