EN 12312-19:2005+A1:2009
(Main)Aircraft ground support equipment - Specific requirements - Part 19: Aircraft jacks, axle jacks and hydraulic tail stanchions
Aircraft ground support equipment - Specific requirements - Part 19: Aircraft jacks, axle jacks and hydraulic tail stanchions
This document specifies the technical requirements to minimise the hazards listed in Clause 4 which can arise during the commissioning, operation and maintenance of aircraft jacks, axle jacks and hydraulic tail stanchions when carried out in accordance with the specifications given by the manufacturer or his authorised representative. It also takes into account some performance requirements recognised as essential by authorities, aircraft and ground support equipment (GSE) manufacturers as well as airlines and handling agencies.
This document applies to:
- all types of aircraft jacks;
- axle jacks and hydraulic tail stanchions designed to be used at specific jacking points on the aircraft (examples see Annex A).
NOTE A tail stanchion type is intended to be used with one type of aircraft.
This document does not apply to aircraft recovery equipment.
This document does not establish requirements for noise and vibration.
Noise and vibration are dealt with respectively in EN 1915 4 and EN 1915 3.
This Part of EN 12312 is not applicable to aircraft jacks, axle jacks and hydraulic tail stanchions which are manufactured before the date of publication of this document by CEN.
This part of EN 12312 is intended to be used in conjunction with EN 1915-1, EN 1915-2, EN 1915-3 (for vehicles) and EN 1915-4.
Luftfahrt-Bodengeräte - Besondere Anforderungen - Teil 19: Flugzeugheber, Radwechselheber und hydraulische Heckstützen
Dieses Dokument legt die technischen Anforderungen zur Minimierung der in Abschnitt 4 aufgelisteten
Gefährdungen fest, die bei der Inbetriebnahme, Betrieb und Wartung von Flugzeughebern, Radwechselhebern
und hydraulischen Heckstützen auftreten können, wenn diese in Übereinstimmung mit den
Anweisungen des Herstellers oder seines Beauftragten ausgeführt werden. Es berücksichtigt auch einige
Funktions- und Gestaltungsanforderungen, die von offiziellen Stellen, Luftfahrzeug- und Bodengeräteherstellern
sowie Luftverkehrs- und Abfertigungsgesellschaften als wesentlich erachtet wurden.
Dieses Dokument gilt für:
- alle Bauarten von Flugzeughebern,
- Radwechselhebern und hydraulischen Heckstützen, die für die Verwendung an festgelegten Unterstützungspunkten
am Luftfahrzeug bestimmt sind (Beispiele siehe Anhang A).
ANMERKUNG Heckstützen sind für die Verwendung an nur einem Luftfahrzeugtyp bestimmt.
Dieses Dokument gilt nicht für Bergungsgerät für Luftfahrzeuge.
Dieses Dokument enthält keine Festlegungen hinsichtlich Lärm und Schwingungen.
Lärm und Schwingungen werden in EN 1915-4 bzw. EN 1915-3 behandelt.
Dieser Teil von EN 12312 gilt nicht für Flugzeugheber, Radwechselheber und hydraulische Heckstützen, die
hergestellt wurden, bevor dieses Dokument durch CEN veröffentlicht wurde.
!Es ist beabsichtigt, diesen Teil der EN 12312 in Verbindung mit EN 1915-1, EN 1915-2, EN 1915-3 (für
Fahrzeuge) und EN 1915-4 anzuwenden."
Matériel au sol pour aéronefs - Exigences particulières - Partie 19: Vérins de levage pour aéronefs, vérins de changement de roues et monopoles hydrauliques
Podporna oprema na tleh za letalski promet - Posebne zahteve - 19. del: Dvigovalniki in podporniki za trup letala in (kolesne) osi ter hidravlični podporniki za rep letala
General Information
Relations
Standards Content (Sample)
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.Luftfahrt-Bodengeräte - Besondere Anforderungen - Teil 19: Flugzeugheber, Radwechselheber und hydraulische HeckstützenMatériel au sol pour aéronefs - Exigences particulières - Partie 19: Vérins de levage pour aéronefs, vérins de changement de roues et monopoles hydrauliquesAircraft ground support equipment - Specific requirements - Part 19: Aircraft jacks, axle jacks and hydraulic tail stanchions49.100Oprema za servis in vzdrževanje na tlehGround service and maintenance equipmentICS:Ta slovenski standard je istoveten z:EN 12312-19:2005+A1:2009SIST EN 12312-19:2005+A1:2009en,de01-julij-2009SIST EN 12312-19:2005+A1:2009SLOVENSKI
STANDARD
EUROPEAN STANDARD NORME EUROPÉENNE EUROPÄISCHE NORM
EN 12312-19:2005+A1
April 2009 ICS 49.100 Supersedes EN 12312-19:2005English Version
Aircraft ground support equipment - Specific requirements - Part 19: Aircraft jacks, axle jacks and hydraulic tail stanchions
Matériel au sol pour aéronefs - Exigences particulières - Partie 19: Vérins de levage pour aéronefs, vérins de changement de roues et monopoles hydrauliques
Luftfahrt-Bodengeräte - Besondere Anforderungen - Teil 19: Flugzeugheber, Radwechselheber und hydraulische Heckstützen This European Standard was approved by CEN on 28 February 2005 and includes Amendment 1 approved by CEN on 1 March 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
COMITÉ EUROPÉEN DE NORMALISATION EUROPÄISCHES KOMITEE FÜR NORMUNG
Management Centre:
Avenue Marnix 17,
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 12312-19:2005+A1:2009: ESIST EN 12312-19:2005+A1:2009
Contents Page
Foreword . 3 1Scope . 52Normative references . 53Terms and definitions . 64List of hazards . 65Safety requirements and/or measures . 66Information for use . 77Verification of requirements . 8Annex A (informative)
Typical examples of jacks and stanchions . 9Annex B (normative)
List of hazards in addition to those of EN 1915-1 . 11Annex C (normative)
Manual forces and manual force measurement methods . 13Annex ZA (informative)
Relationship between this European Standard and the Essential Requirements of EU Directive 98/37/EC, amended by Directive 98/79/EC . 14Annex ZB (informative)
!!!!Relationship between this European Standard and the Essential Requirements of EU Directive 2006/42/EC"""" . 15Bibliography . 16
Foreword This document (EN 12312-19:2005+A1:2009) has been prepared by Technical Committee CEN/TC 274 "Aircraft ground support equipment" the secretariat of which is held by DIN. 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 October 2009, and conflicting national standards shall be withdrawn at the latest by December 2009. This document includes Amendment 1, approved by CEN on 2009-03-01. This document supersedes EN 12312-19:2005. The start and finish of text introduced or altered by amendment is indicated in the text by tags ! ". This document has been prepared under a mandate given to CEN by the European Commission and the European Free Trade Association and supports essential requirements of EU Directive(s). !For relationship with EU Directives, see informative Annexes ZA and ZB, which are integral parts of this document." The Parts of EN 12312 — Aircraft ground support equipment — Specific requirements — are: Part 1: Passenger stairs Part 2: Catering vehicles Part 3: Conveyor belt vehicles Part 4: Passenger boarding bridges Part 5: Aircraft fuelling equipment Part 6: Deicers and deicing/antiicing equipment Part 7: Aircraft movement equipment Part 8: Maintenance stairs and platforms Part 9: Container/Pallet loaders Part 10: Container/Pallet transfer transporters Part 11: Container/Pallet dollies and loose load trailers Part 12: Potable water service equipment Part 13: Lavatory service equipment Part 14: Disabled/Incapacitated passenger boarding equipment Part 15: Baggage and equipment tractors Part 16: Air start equipment Part 17: Air conditioning equipment Part 18: Nitrogen or Oxygen units Part 19: Aircraft jacks, axle jacks and hydraulic tail stanchions Part 20: Ground power equipment According to the CEN/CENELEC Internal Regulations, the national standards organizations of the following coun-tries are bound to implement this European Standard: Austria, Belgium, Bulgaria, Cyprus, Czech Republic, Den-mark, 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.
Introduction This document specifies health and safety requirements, as well as some functional and performance requirements for aircraft jacks, axle jacks and hydraulic tail stanchions intended to be used for servicing and handling of all aircraft types commonly in service in civil air transport. The minimum essential criteria are considered to be of primary importance in providing safe, serviceable, economical, and practical aircraft jacks, axle jacks and tail stanchions. Deviations from the recommended criteria should occur only after careful consideration, extensive testing, risk assessment and in service evaluation have shown alternative methods or conditions to be satisfactory. This document is a Type C standard as stated in !EN ISO 12100". The machinery concerned and the extent to which hazards, hazardous situations and events are covered are indicated in the scope of this document. When provisions of this Type C standard are different from those which are stated in Type A or B standards, the provisions of this Type C standard take precedence over the provisions of the other standards, for machines that have been designed and built according to the provisions of this Type C standard. SIST EN 12312-19:2005+A1:2009
1 Scope This document specifies the technical requirements to minimise the hazards listed in Clause 4 which can arise during the commissioning, operation and maintenance of aircraft jacks, axle jacks and hydraulic tail stanchions when carried out in accordance with the specifications given by the manufacturer or his authorised representative. It also takes into account some performance requirements recognised as essential by authorities, aircraft and ground support equipment (GSE) manufacturers as well as airlines and handling agencies. This document applies to: all types of aircraft jacks; axle jacks and hydraulic tail stanchions designed to be used at specific jacking points on the aircraft (examples see Annex A). NOTE A tail stanchion type is intended to be used with one type of aircraft. This document does not apply to aircraft recovery equipment. This document does not establish requirements for noise and vibration. Noise and vibration are dealt with respectively in EN 1915-4 and EN 1915-3. This Part of EN 12312 is not applicable to aircraft jacks, axle jacks and hydraulic tail stanchions which are manufactured before the date of publication of this document by CEN. !This part of EN 12312 is intended to be used in conjunction with EN 1915-1, EN 1915-2, EN 1915-3 (for vehicles) and EN 1915-4." 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. !deleted text" EN 1050:1996, Safety of machinery — Principles for risk assessment EN 1915-1:2001, Aircraft ground support equipment — General requirements — Part 1: Basic safety requirements EN 1915-2, Aircraft ground support equipment — General requirements — Part 2: Stability and strength requirements, calculations and test methods !EN 1915-3, Aircraft ground support equipment — General requirements — Part 3: Vibration measurement methods and reduction" !EN 1915-4, Aircraft ground support equipment — General requirements — Part 4: Noise measurement methods and reduction" EN ISO 12100-1:2003, Safety of machinery — Basic concepts, general principles for design — Part 1: Basic termi-nology, methodology (ISO 12100-1:2003) EN ISO 12100-2:2003, Safety of machinery — Basic concepts, general principles for design — Part 2: Technical principles (ISO 12100-2:2003). !EN ISO 13850:2008, Safety of machinery — Emergency stop — Principles for design (ISO 13850:2006)" SIST EN 12312-19:2005+A1:2009
3 Terms and definitions For the purposes of this document, the terms and definitions given in EN ISO 12100:2003 and EN 1915-1:2001 and the following apply. 3.1 aircraft jack lifting device to support and/or raise an aircraft via its fuselage and wings 3.2 axle jack lifting device used to support and/or raise an aircraft via its axles 3.3 hydraulic tail stanchion device used to support an aircraft at its tail during loading and unloading operations 4 List of hazards The list of risks and hazards (see Annex B) is based on EN 1050 and contains the hazards and hazardous situa-tions, as far as they are dealt with in this document, identified by risk assessment as significant for aircraft jacks, axle jacks and hydraulic tail stanchions and which require action to eliminate or reduce risks. 5 Safety requirements and/or measures 5.1 General requirements 5.1.1 !!!!Aircraft jacks, axle jacks and hydraulic tail stanchions shall conform to the relevant requirements of EN 1915-1, EN 1915-2, EN 1915-3 and EN 1915-4 unless otherwise specified in this standard." They shall also conform to the specific requirements of this document. 5.1.2 Stability and strength calculations shall be carried out in accordance with EN 1915-2. 5.1.3 Where a pressure relief valve is used for overload protection, it shall not be positioned between the ram and its control device. The pressure relief valve shall be adjusted to the lowest possible value but not exceeding 125 % of the rated load. 5.1.4 On jacks it shall be possible for the operator to control the lowering speed or stop the lowering at any load up to the rated load, e.g. on manually operated jacks, by a finely controllable valve. 5.1.5 Maximum admissible forces for manual operation and translation of jacks and stanchions and the methods to measure it are given in Annex C. 5.2 Specific requirements for aircraft jacks and hydraulic tail stanchions 5.2.1 Aircraft jacks and hydraulic tail stanchions shall be designed to enable safe and easy steering, e.g. one steering wheel out of three. 5.2.2 Permanent access shall be provided on aircraft jacks and hydraulic tail stanchions to enable positioning and adjustment of the upper load support point. Where this is only a ladder, the maximum distance between the fourth tread counting from the top of the ladder and the maximum extended position of the support point shall not exceed 2,0 m. 5.2.3 On power operated aircraft jacks and tail stanchions, emergency stops shall be installed at each operator's panel. !They shall meet the requirements in EN ISO 13850:2008, Category 0 or 1." SIST EN 12312-19:2005+A1:2009
5.2.4 Adjustable stabilisers may be considered as equivalent devices to fulfil the requirements in EN 1915-1:2001, 5.7.2. 5.2.5 The lifting system of aircraft jacks shall be equipped so that failure in the lifting device does not generate any hazardous movement of the lifting point/load. 5.2.6 Where more than one jack is intended to be used to lift an aircraft: failure of one drive shall induce stopping of all the jacks; monitoring of the movement shall be provided, in accordance with EN 1915-1:2001, 5.1; differences in height up to 100 mm shall be automatically corrected and differences in height of more than 100 mm shall lead to immediate stop of all jacks; manual lowering shall not be used. The device to fulfil the requirements in EN 1915-1:2001, 5.20.3, shall be a pilot-operated check valve (see Clause 0 of EN 1915-1:2001 — negotiation). 5.2.7 The upper load support point of hydraulic tail stanchions, when connected to the a
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