EN 3733-001:2009

2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Luft- und Raumfahrt - Optischer Rundsteckverbinder einpolig, Schraubkupplung, Betriebstemperatur 150 °C konstant - Teil 001: Technische LieferbedingungenSérie aérospatiale - Connecteur optique circulaire monovoie, à accouplement par bague filetée, température d'utilisation 150 °C continu - Partie 001: Spécification techniqueAerospace series - Connector, optical, circular, single channel, coupled by self-locking ring, operating temperature up to 150 °C continuous - Part 001: Technical specification49.060Aerospace electric equipment and systemsICS:Ta slovenski standard je istoveten z:EN 3733-001:2009SIST EN 3733-001:2009en01-oktober-2009SIST EN 3733-001:2009SLOVENSKI
STANDARD
EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
EN 3733-001
August 2009 ICS 49.060 English Version
Aerospace series - Connector, optical, circular, single channel, coupled by self-locking ring, operating temperature up to 150 °C continuous - Part 001: Technical specification
Série aérospatiale - Connecteur optique circulaire monovoie, à accouplement par bague filetée, température d'utilisation 150 °C continu - Partie 001 : Spécification technique
Luft- und Raumfahrt - Optischer Rundsteckverbinder einpolig, Schraubkupplung, Betriebstemperatur 150 °C konstant - Teil 001: Technische Lieferbedingungen This European Standard was approved by CEN on 3 July 2009.
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 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 Management Centre has the same status as the official versions.
CEN members are the national standards bodies of Austria, Belgium, Bulgaria, Cyprus, Czech Republic, Denmark, Estonia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom.
EUROPEAN COMMITTEE FOR STANDARDIZATION
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B-1000 Brussels © 2009 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 3733-001:2009: ESIST EN 3733-001:2009

Figures Figure 1 — Plug interface dimensions . 8 Figure 2 — Receptacle interface dimesions . 9 Figure 3 — Key-ways . 10
Aerospace series — Elements of electrical and optical connection — Test methods — Part 100: General1 EN 9133,
Aerospace series - Quality management systems - Qualification procedure for Aerospace Standard Parts EN 3197,
Aerospace series — Installation of aircraft electrical and optical interconnection systems2 EN 3733-002,
Aerospace series — Connectors, optical, circular, single channel, coupled by self-locking ring, operating temperature 150 °C continuous — Part 002: List of product standards2 ISO 1817,
Rubber, vulcanized — Determination of the effect of liquids MIL-STD-810F,
Environmental engineering Considerations and Laboratory Tests3 MIL-PRF-7808L,
Lubricating Oil, Aircraft Turbine Engine, Synthetic Base3 MIL-PRF-23699F,
Lubricating Oil, Aircraft Turbine Engine, Synthetic Base, NATO Code Number O-1563 QPL-5606-31,
Hydraulic Fluid, Petroleum Base; Aircraft; Missile and Ordnance3 SAE-AMS 1424,
Fluid, Deicing/Anti-Icing, Aircraft, SAE Type 13 3 Terminology For the purposes of this standard, the definitions given in EN 2591-100 apply. 4 Description 4.1 General All connectors shall be environmentally sealed to the level specified in Table 2.
1 All parts quoted in Tables 2, 6 and 7. 2 Published as ASD prestandard at the date of publication of this standard. 3 Published by: Department of Defense (DOD), the Pentagon, Washington, DC 20301, USA. SIST EN 3733-001:2009

Key 1 Thread Figure 1 — Plug interface dimensions
Key 1 Thread 2 Elastomeric face seal Figure 2 — Receptacle interface dimensions SIST EN 3733-001:2009

Figure 3 — Key-ways Table 1 – Key positions Dimensions in gradeKey position A B C D Normal 105 140 215 265 A 102 132 248 320 B 80 118 230 312 C 35 140 205 275 D 64 155 234 304 E 91 131 197 240 7 Tests 7.1 Tests according to EN 2591-100 The tests cited in EN 2591-100 are applicable in the context of this standard as well as details necessary for implementing them for inspecting connector characteristics, are given in Table 2. Performance and test method parameters which are fibre and cable dependant, together with environmental testing not applicable to all product standards, are detailed in the appropriate product standards. Tests relating to electrical and multi-way connectors are not applicable to EN 3733 components and are therefore not included in Table 2. SIST EN 3733-001:2009

Method B – 150 °C Time 1 000 h 302 Climatic sequence For performance and test method requirements refer to the applicable product standard for the component and cable under test 6303 Optical elements – Cold/low pressure and damp heat Duration – five cycles Maximum temperature (– 65 ± 2) °C Measurement during test: at each transition point 304 Damp heat steady state For performance and test method requirements refer to the applicable product standard for the component and cable under test. 6305 Optical elements – Rapid change of temperature
TA = (− 6550−) °C TB = (15005+) °C 6306 Optical elements – Mould growth Not applicable 6307 Optical elements – Salt mist The connectors are suspended in the test chamber with non-metallic cords, to prevent accumulation of condensed solution The connectors are subjected to 50 mating/unmating cycles, rate not exceeding to the salt mist: mated for 452 h, then unmated for 48 h 308 Sand and dust Connector mated and positioned such that rear of free plug faces into the wind direction Wind velocity in duct: (3,5 ± 0,5) m/s Number of cycles: one 309 Dry heat For performance and test method requirements refer to the applicable product standard for the component and cable under test. 310 Cold 311 Low air pressure 312 Air leakage Test performed on non-hermetic connectors Method B -
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