EN 4022:2001
(Main)Aerospace series - Pipe coupling 8°30' in titanium alloy - Elbows 90° bulkhead, welded end
Aerospace series - Pipe coupling 8°30' in titanium alloy - Elbows 90° bulkhead, welded end
This standard specifies the characteristics of elbows 90°, bulkhead, welded end, for pipe couplings 8°30', in titanium alloy,
for aerospace applications.
Nominal pressure: up to 28 000 kPa
Temperature range: 55 °C to 135 °C
Luft- und Raumfahrt - Rohrverschraubung 8°30' aus Titanlegierung - Winkelverschraubungen 90° mit Anschweißende
Diese Norm legt die Eigenschaften von Winkel-Schottverschraubungen 90° mit Anschweißende, für Rohrverschraubungen
8°30', aus Titanlegierung, zur Verwendung in der Luft- und Raumfahrt fest.
Nenndruck: bis 28 000 kPa
Temperaturbereich: 55 °C bis 135 °C
Série aérospatiale - Système de raccordement 8°30' en alliage de titane - Raccords coudés à 90° pour traversée de cloison, à souder
La présente norme spécifie les caractéristiques des raccords coudés à 90° à souder, pour traversée de cloison, pour les
systèmes de raccordement 8°30', en alliage de titane, pour applications aérospatiales.
Pression nominale: jusqu'à 28 000 kPa
Plage de température: 55 °C à 135 °C
Aerospace series - Pipe coupling 8°30' in titanium alloy - Elbows 90° bulkhead, welded end
General Information
- Status
- Published
- Publication Date
- 23-Oct-2001
- Withdrawal Date
- 29-Apr-2002
- Technical Committee
- ASD-STAN - Aerospace
- Drafting Committee
- ASD-STAN/D 3 - Mechanical
- Current Stage
- 9093 - Decision to confirm - Review Enquiry
- Start Date
- 31-May-2017
- Completion Date
- 14-Apr-2025
Overview
EN 4022:2001 (CEN) covers aerospace series pipe coupling 8°30' – 90° bulkhead elbows with welded ends in titanium alloy. The standard defines the characteristics, dimensional data and manufacturing/acceptance requirements for these elbows used in aerospace fluid systems. It applies to fittings rated for nominal pressures up to 28 000 kPa and a published temperature range of 55 °C to 135 °C. (Verify the full standard text for temperature limits applicable to your program.)
Key topics and technical requirements
- Configuration & dimensions: Detailed geometry, mass and dimensional tables for multiple MJ thread sizes (per EN 3274 and EN 2656). Many dimensions are given before lubrication; unspecified dimensions may be at the manufacturer’s option when qualification/acceptance is met.
- Threads: MJ thread forms and limit dimensions referenced to ISO 5855‑3 (Aerospace MJ threads).
- Materials: Titanium alloys specified by related aerospace titanium standards (EN 3311 / EN 3314 / EN 3312 / EN 3315 referenced).
- Surface treatment and lubrication:
- Welded end without surface treatment for a minimum 10 mm (outside and bore).
- Thread and sealing face lubrication per EN 2491; film thickness 0.005–0.013 mm.
- Surfaces to be abrasive-blasted with non-metallic grit prior to lubricant application.
- Internal finishing: Bore radius R = 0.3 mm to 1.0 mm and surface roughness 0.8 μm; hand deburring is not permitted.
- Marking & designation: Marking requirements follow EN 2424 (style A) and the standard includes designation examples and coding practice.
- Technical specification & acceptance: Conformance and inspection requirements refer to EN 3275, type II.
- Installation: Bulkhead installation details (washer per EN 3267, grip length, thread engagement allowances) are included.
Applications and users
EN 4022:2001 is intended for:
- Aerospace design and stress/fluids engineers specifying titanium 90° bulkhead elbows for hydraulic and pneumatic lines.
- Manufacturers and suppliers of aerospace pipe fittings and welded-end elbows.
- Quality, procurement and certification personnel ensuring components meet aerospace coupling, pressure and temperature requirements.
- Maintenance organizations and MROs replacing or inspecting bulkhead fittings in aircraft fluid systems.
Typical use cases: high-pressure aircraft hydraulic lines, fuel and pneumatic tubing where lightweight titanium fittings and reliable bulkhead penetration are required.
Related standards
Key normative references linked to EN 4022 include:
- ISO 5855‑3 (MJ threads)
- EN 2656, EN 3274, EN 3275 (coupling geometry and seals)
- EN 2424 (marking)
- EN 2491 (dry lubricant/coating)
- EN 3267 (bulkhead washers)
- EN 3311 / EN 3312 / EN 3314 / EN 3315 (titanium alloy material specifications)
For procurement or design use, consult the full EN 4022:2001 document and the referenced standards for complete, authoritative requirements.
Frequently Asked Questions
EN 4022:2001 is a standard published by the European Committee for Standardization (CEN). Its full title is "Aerospace series - Pipe coupling 8°30' in titanium alloy - Elbows 90° bulkhead, welded end". This standard covers: This standard specifies the characteristics of elbows 90°, bulkhead, welded end, for pipe couplings 8°30', in titanium alloy, for aerospace applications. Nominal pressure: up to 28 000 kPa Temperature range: 55 °C to 135 °C
This standard specifies the characteristics of elbows 90°, bulkhead, welded end, for pipe couplings 8°30', in titanium alloy, for aerospace applications. Nominal pressure: up to 28 000 kPa Temperature range: 55 °C to 135 °C
EN 4022:2001 is classified under the following ICS (International Classification for Standards) categories: 49.080 - Aerospace fluid systems and components. The ICS classification helps identify the subject area and facilitates finding related standards.
EN 4022:2001 is available in PDF format for immediate download after purchase. The document can be added to your cart and obtained through the secure checkout process. Digital delivery ensures instant access to the complete standard document.
Standards Content (Sample)
SLOVENSKI STANDARD
01-maj-2004
Aerospace series - Pipe coupling 8°30' in titanium alloy - Elbows 90° bulkhead,
welded end
Aerospace series - Pipe coupling 8°30' in titanium alloy - Elbows 90° bulkhead, welded
end
Luft- und Raumfahrt - Rohrverschraubung 8°30' aus Titanlegierung -
Winkelverschraubungen 90° mit Anschweißende
Série aérospatiale - Systeme de raccordement 8°30' en alliage de titane - Raccords
coudés a 90° pour traversée de cloison, a souder
Ta slovenski standard je istoveten z: EN 4022:2001
ICS:
49.080 /HWDOVNLLQYHVROMVNL Aerospace fluid systems and
KLGUDYOLþQLVLVWHPLLQGHOL components
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.
EUROPEAN STANDARD
EN 4022
NORME EUROPÉENNE
EUROPÄISCHE NORM
October 2001
ICS 49.080
English version
Aerospace series - Pipe coupling 8°30' in titanium alloy - Elbows
90° bulkhead, welded end
Série aérospatiale - Système de raccordement 8°30' en Luft- und Raumfahrt - Rohrverschraubung 8°30' aus
alliage de titane - Raccords coudés à 90° pour traversée de Titanlegierung - Winkelverschraubungen 90° mit
cloison, à souder Anschweißende
This European Standard was approved by CEN on 29 December 2000.
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 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 Management Centre has the same status as the official
versions.
CEN members are the national standards bodies of Austria, Belgium, Czech Republic, Denmark, Finland, France, Germany, Greece,
Iceland, Ireland, Italy, Luxembourg, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland and United Kingdom.
EUROPEAN COMMITTEE FOR STANDARDIZATION
COMITÉ EUROPÉEN DE NORMALISATION
EUROPÄISCHES KOMITEE FÜR NORMUNG
Management Centre: rue de Stassart, 36 B-1050 Brussels
© 2001 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 4022:2001 E
worldwide for CEN national Members.
Foreword
This European Standard has been prepared by the European Association of Aerospace Manufacturers (AECMA).
After inquiries and votes carried out in accordance with the rules of this Association, this Standard has received the
approval of the National Associations and the Official Services of the member countries of AECMA, 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 April 2002, and conflicting national standards shall be withdrawn at the latest by April 2002.
According to the CEN/CENELEC Internal Regulations, the national standards organizations of the following countries are
bound to implement this European Standard: Austria, Belgium, Czech Republic, Denmark, Finland, France, Germany,
Greece, Iceland, Ireland, Italy, Luxembourg, Netherlands, Norway, Portugal, Spain, Sweden, Switzerland and the United
Kingdom.
1 Scope
This standard specifies the characteristics of elbows 90°, bulkhead, welded end, for pipe couplings 8°30', in titanium alloy,
for aerospace applications.
Nominal pressure: up to 28 000 kPa
Temperature range: 55 °C to 135 °C
2 Normative references
This European Standard incorporates by dated or undated reference provisions from other publications. These normative
references are cited at the appropriate places in the text and the publications are listed hereafter. For dated references,
subsequent amendments to or revisions of any of these publications apply to this European Standard only when
incorporated in it by amen
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