Aerospace series - General and installation requirements for passenger seat fittings

This European Standard specifies the installation and removal requirements and the space envelopes for passenger seat fittings on aircraft. The purpose is to reduce the installation time and the tooling required for seat installation by standardizing the seat attachment fasteners (fittings).

Luft- und Raumfahrt - Allgemeine und Einbau Anforderungen an Fittinge von Passagiersitzen

Diese Norm legt die Anforderungen an den Einbau und Ausbau sowie die Freigängigkeit für die Fittinge (Sitzbefestigungen) von Passagiersitzen in Luftfahrzeugen fest. Ziel ist es, die Einbauzeit und die Menge der für den Sitzeinbau erforderlichen Werkzeuge zu verringern, indem die Anforderungen an die Fittinge genormt werden.

Série aérospatiale - Exigences générales et d’installation pour siège passager

La présente Norme européenne spécifie les exigences d’installation et de démontage ainsi que les gabarits d'encombrement des ferrures de sièges passagers. Elle a pour but de diminuer le temps d'installation et l'outillage exigé pour réaliser l'installation des sièges en normalisant les éléments de fixation des sièges (ferrures).

Aeronavtika - Splošne zahteve in zahteve za namestitev pritrdilnih elementov potniških sedežev

Ta evropski standard določa zahteve za namestitev in odstranitev ter prostorske okvire za pritrdilne elemente potniških sedežev na letalu. Namen je s standardizacijo sponk za pritrditev sedežev (pritrdilnih elementov sedežev) skrajšati čas namestitve in omejiti orodje, potrebno za namestitev sedeža.

General Information

Status
Withdrawn
Publication Date
15-May-2012
Withdrawal Date
19-Apr-2016
Technical Committee
Drafting Committee
Current Stage
9960 - Withdrawal effective - Withdrawal
Completion Date
20-Apr-2016

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2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Aeronavtika - Splošne zahteve in zahteve za namestitev pritrdilnih elementov potniških sedeževLuft- und Raumfahrt - Allgemeine und Einbau Anforderungen an die Sitzanbindung von PassagiersitzenSérie aérospatiale - Exigences générales et d’installation pour siège passagerAerospace series - General and installation requirements for passenger seat fittings49.095Oprema za potnike in oprema kabinPassenger and cabin equipmentICS:Ta slovenski standard je istoveten z:EN 4697:2012SIST EN 4697:2012en01-september-2012SIST EN 4697:2012SLOVENSKI

STANDARD
SIST EN 4697:2012
EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
EN 4697
May 2012 ICS 49.095 English Version

Aerospace series - General and installation requirements for passenger seat fittings

Série aérospatiale - Exigences générales et d'installation pour siège passager

Luft- und Raumfahrt - Allgemeine und Einbau Anforderungen an Fittinge von Passagiersitzen This European Standard was approved by CEN on 25 February 2012.

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, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and United Kingdom.

EUROPEAN COMMITTEE FOR STANDARDIZATION
COMITÉ EUROPÉEN DE NORMALISATION EUROPÄISCHES KOMITEE FÜR NORMUNG
Management Centre:
Avenue Marnix 17,

B-1000 Brussels © 2012 CEN All rights of exploitation in any form and by any means reserved worldwide for CEN national Members. Ref. No. EN 4697:2012: ESIST EN 4697:2012

EN 4697:2012 (E) 2 Contents Page Foreword ..............................................................................................................................................................31 Scope ......................................................................................................................................................42 Normative references ............................................................................................................................43 Abbreviations .........................................................................................................................................54 Requirements .........................................................................................................................................54.1 General ....................................................................................................................................................54.2 Interface ..................................................................................................................................................84.3 Installation Requirements .................................................................................................................. 104.4 Performance and Safety ..................................................................................................................... 124.5 Stress requirements ........................................................................................................................... 144.5.1 Static requirements ............................................................................................................................ 144.5.2 Dynamic requirements (rear fitting only) ......................................................................................... 164.6 Environmental requirements ............................................................................................................. 214.7 Additional requirements .................................................................................................................... 215 Qualification ........................................................................................................................................ 21 SIST EN 4697:2012

EN 4697:2012 (E) 3 Foreword This document (EN 4697:2012) 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 Standard has received the approval of the National Associations and the Official Services of the member countries of ASD, 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 November 2012, and conflicting national standards shall be withdrawn at the latest by November 2012. Attention is drawn to the possibility that some of the elements of this document may be the subject of patent rights. CEN [and/or CENELEC] shall not be held responsible for identifying any or all such patent rights. According to the CEN/CENELEC Internal Regulations, the national standards organizations of the following countries are bound to implement this European Standard: 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, Romania, Slovakia, Slovenia, Spain, Sweden, Switzerland, Turkey and the United Kingdom. SIST EN 4697:2012

EN 4697:2012 (E) 4 1 Scope This European Standard specifies the installation and removal requirements and the space envelopes for passenger seat fittings on aircraft. The purpose is to reduce the installation time and the tooling required for seat installation by standardizing the seat attachment fasteners (fittings).

2 Normative references The following documents, in whole or in part, are normatively referenced in this document and are indispensable for its application. For dated references, only the edition cited applies. For undated references, the latest edition of the referenced document (including any amendments) applies. EN 9100, Aerospace series — Quality Management Systems — Requirements for Aviation, Space and Defence Organizations EN 9133, Aerospace series — Quality management systems — Qualification procedure for aerospace standard parts AMS 1424J, Aircraft Deicing/Anti-icing Fluids 1) AMS 1428F, Fluid, Aircraft De-icing/Anti-Icing, Non-Newtonian, (Pseudoplastic) 1) AMS 1550B, Cleaner, Water Base, Aircraft Interior Hard Surface Materials 1) AMS 1630C, Cleaner, Carpet, Shampoo Type 1) AMS 1631C, Cleaner, Carpet Water Extraction Type 1) AS8049B, Performance Standard for Seats in Civil Rotorcraft, Transport Aircraft and General Aviation A/C 1) CS-25 Amendment 5, 5 September 2008, Certification Specification for Large Aeroplanes 2) FAR 25 Amendment 127, 28 October 2008, Airworthiness Standards: Transportation Category Airplanes 3) RTCA DO-160F 6 December 2007, Environmental Conditions and Test Procedures for Airborne Equipment 4)

1) Published by: SAE National (US) Society of Automotive Engineers http://www.sae.org/ 2) Published by: European Aviation Safety Agency (EASA), Postfach 101253, D-50452 Koeln, Germany 3) Published by: FAA National (US) Federal Aviation Administration http://www.faa.gov/ 4) Published by: Radio Technical Commission for Aeronautics (RTCA), 1828 L Street, NW, Suite 805 Washington, DC 20036, USA

SIST EN 4697:2012
EN 4697:2012 (E) 5 3 Abbreviations

For the purposes of this standard, the following abbreviations apply. A/C Aircraft. Acc. According. Fwd Forward. SLD Shear Locking Device. 4 Requirements 4.1 General The fitting design shall fit within the given space envelope, according to Figure 1 and Figure 6.

Key 1 Monument 2 Fitting body 3 Carpet 4 Floor panel 5 Seat rail 6 Raceway Figure 1 — Fitting environment 1 All fittings attached to seat legs shall be pre-set to the correct seat track dimensions with fine adjustment of the fitting during installation not being necessary. Minimum front to rear fitting distance shall be 482,6 mm (19”) between the extreme studs of each fitting.

Figure 2 — Aircraft Coordinate System SIST EN 4697:2012

EN 4697:2012 (E) 6 The front attachment fasteners shall cover the tolerances in X-direction (see Figure 2) that might occur due to installation tolerances (of the seat leg and of the A/C structure). The fitting weight shall be according to Table 1. Table 1 — Fitting classes Fitting class Fitting Weight

g A Rear triple stud fitting ≤ 150 B ≤ 250 C Rear quadruple stud fitting ≤ 200 D ≤ 290 E Forward single stud fitting ≤ 50 F ≤ 90

Maintenance or repair work on the seat track shall be taken into account during fitting design. Details see Figure 3. Dimensions in millimetres

Figure 3a — Seat track top view Figure 3b — Seat track 3 D view continued SIST EN 4697:2012

EN 4697:2012 (E) 7

Figure 3c — Damage repair cross section 1 Figure 3d — Damage repair cross section 2

Figure 3e — Damage repair top view Key 1 If the amount of material removed on one side of a seat track exceeds 0,3 mm (0.012 inch) maximum in depth, it is necessary to remove the same amount from the other side, so that a level surface is achieved 2 Minimum remaining thickness after rework 3 Maximum rework depth as reference to nominal thickness Figure 3 — Seat track allowable damage limits and repair solutions The fitting design shall show no evidence of any movement/rattling of the fitting-track combination. A continuous load path shall be ensured at all times. A shear-locking device should only be incorporated in the rear fitting. Fitting design and performance shall be validated incorporating the fitting-seat combination. SIST EN 4697:2012

EN 4697:2012 (E) 8 4.2 Interface The fitting shall be compatible with the standard seat track concept, see Figure 4 and detail.

Dimension A Tolerance of ± 0,1 mm (0.004 inch) on 1 pitch Tolerance of ± 0,5 mm (0.020 inch) on 100 pitches Figure 4 — Seat rail top view

Detailed seat rail dimensions, see Table 2. Figure 5 — Seat rail cross section
SIST EN 4697:2012

EN 4697:2012 (E) 9 Table 2 — Seat rail dimensions Dimensions in millimetres (in inches) A B C D E H α° R1 R2 R3 min. max. min. max. min. max. min. max. min. max. min. max. min. max. min. max. min. max.

25,3 25,5 19,7 20,0 10,7 11,0 20,5 21,0 7,8 8,0 2,3 2,7 13,75 14,25 0 1,0 0,8 1,8 Full 1.0040.996 

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