Aircraft ground support equipment - Specific requirements - Part 6: Deicers and deicing/antiicing equipment

This European standard specifies the safety requirements for deicers and deicing equipment designed for deicing aircraft. It applies to: - self-propelled deicers, - towable deicers, - stationary deicing equipment (e.g. fixed boom, gantry- or tower cranes equipped with aircraft deicing fluid systems).

Luftfahrt-Bodengeräte - Besondere Anforderungen - Teil 6: Enteiser und Enteisungs-/Vereisungsschutzgeräte

Diese Europäische Norm legt die Sicherheitsanforderungen für Enteiser und Enteisungsgeräte fest, die für das Enteisen von Luftfahrzeugen bestimmt sind. Sie ist anzuwenden für: - selbstfahrende Enteiser; - schleppbare Enteiser; - stationäre Enteisungsanlagen ( z.B. mit Enteisungssystemen ausgerüstete Ausleger-, Bock- oder Turmdrehkrane).

Matériel au sol pour aéronefs - Exigences particulieres - Partie 6: Dégivreuses, matériels de dégivrage et d'antigivrage

La présente Norme européenne spécifie les exigences de sécurité pour minimiser les dangers listés a l'Article 4 qui pourraient apparaître lors de la mise en service, de l'exploitation et de la maintenance de dégivreuses et d'équipements de dégivrage conçus exclusivement pour le dégivrage et le lavage des aéronefs avec des liquides de dégivrage/antigivrage/lavage selon les spécifications émises par le constructeur ou son représentant autorisé. Elle prend également en compte certaines exigences de performances reconnues essentielles par les autorités, les fabricants d'aéronefs et de matériels de service au sol, ainsi que par les compagnies aériennes et organismes d'assistance.
NOTE   La sécurité des aéronefs en relation avec les opérations de dégivrage/antigivrage n'est pas traitée dans la présente Norme européenne. Meme mineure, toute opération de dégivrage/antigivrage affecte directement la sécurité au décollage. La prévention des accidents aériens résultants du givrage en vol concerne au premier chef les fluides et méthodes utilisés, mais peut dans certains cas concerner également la conception ou l'exploitation des matériels de dégivrage et d'antigivrage. Ces aspects aéronautiques ne sont pas couverts par la présente Norme européenne (voir également les Joint Aviation authorities (JAA), Joint Aviation Regulations (JAR) JAR-OPS subpart D 1.345 et tous documents associés).
La présente norme s'applique :
-   aux dégivreuses automotrices avec plate-forme fixe ou bras mobile ;
-   aux dégivreuses tractables avec plate-forme fixe ou bras mobile ;
-   aux équipements de dégivrage fixes (tels que bras fixe, grues a portique ou a pylône équipées de circuits de liquide pour le dégivrage/antigivrage des aéronefs).
La présente Norme européenne ne s'applique pas dans les cas suivants :
-   installations fixes, telles que réservoirs de stockage séparés, centrales de chauffage et de remplissage, qui ne sont pas parties intégrantes des équipements de dégivrage fixes.

Talna podporna oprema za letala – Posebne zahteve – 6. del: Sredstva za odstranjevanje ledu in oprema za odstranjevanje/preprečevanje nastanka ledu

General Information

Status
Withdrawn
Publication Date
31-Aug-2004
Withdrawal Date
05-May-2009
Technical Committee
Current Stage
9900 - Withdrawal (Adopted Project)
Start Date
06-May-2009
Due Date
29-May-2009
Completion Date
06-May-2009

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Standards Content (Sample)

SLOVENSKI STANDARD
SIST EN 12312-6:2004
01-september-2004
7DOQDSRGSRUQDRSUHPD]DOHWDOD±3RVHEQH]DKWHYH±GHO6UHGVWYD]D
RGVWUDQMHYDQMHOHGXLQRSUHPD]DRGVWUDQMHYDQMHSUHSUHþHYDQMHQDVWDQNDOHGX
Aircraft ground support equipment - Specific requirements - Part 6: Deicers and
deicing/antiicing equipment
Luftfahrt-Bodengeräte - Besondere Anforderungen - Teil 6: Enteiser und Enteisungs
-/Vereisungsschutzgeräte
Matériel au sol pour aéronefs - Exigences particulieres - Partie 6: Dégivreuses, matériels
de dégivrage et d'antigivrage
Ta slovenski standard je istoveten z: EN 12312-6:2004
ICS:
49.100 Oprema za servis in Ground service and
vzdrževanje na tleh maintenance equipment
SIST EN 12312-6:2004 en
2003-01.Slovenski inštitut za standardizacijo. Razmnoževanje celote ali delov tega standarda ni dovoljeno.

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EUROPEAN STANDARD
EN 12312-6
NORME EUROPÉENNE
EUROPÄISCHE NORM
May 2004
ICS 49.100
English version
Aircraft ground support equipment - Specific requirements - Part
6: Deicers and deicing/antiicing equipment
Matériel au sol pour aéronefs - Exigences particulières - Luftfahrt-Bodengeräte - Besondere Anforderungen - Teil 6:
Partie 6: Dégivreuses, matériels de dégivrage et Enteiser und Enteisungs-/Vereisungsschutzgeräte
d'antigivrage
This European Standard was approved by CEN on 24 March 2004.
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 Central Secretariat 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 Central Secretariat has the same status as the official
versions.
CEN members are the national standards bodies of Austria, Belgium, Cyprus, Czech Republic, Denmark, Estonia, Finland, France,
Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta, Netherlands, Norway, Poland, Portugal, Slovakia,
Slovenia, 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
© 2004 CEN All rights of exploitation in any form and by any means reserved Ref. No. EN 12312-6:2004: E
worldwide for CEN national Members.

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EN 12312-6:2004 (E)
Contents
page
Foreword.4
1 Scope.6
2 Normative references.6
3 Terms and definitions .7
4 List of significant hazards .8
5 Safety requirements and/or measures .8
5.1 General requirements.8
5.2 Spray system.8
5.3 Stability and strength.8
5.4 Safeguards and safety devices .9
5.5 Emergency systems.9
5.6 Operator's cabin.10
5.7 Controls, monitoring devices and displays .10
5.8 Lights.11
5.9 Fire protection.11
5.10 Protection against heat.11
5.11 Protection against poisoning.11
5.12 Special requirements for deicers.12
5.13 Operating speeds.12
5.14 Warning devices for stationary deicing/antiicing equipment .12
6 Information for use .12
6.1 Marking.12
6.2 Additional marking.12
6.2.2 Additional marking for stationary deicing/antiicing equipment .13
6.3 Instructions.13
7 Verification of requirements.13
Annex A (normative)  List of significant hazards in addition to those of EN 1915-1 .15
Annex B (informative)  Fluid system .17
B.1 General.17
B.2 Functional information.17
B.2.1 General.17
B.2.2 Size/design of deicing equipment.17
B.3 Recommendations for fluid systems.18
B.3.1 General.18
B.3.2 Fluid tanks.18
B.3.3 Pipe and pump system.18
B.3.4 Nozzle, spraying equipment .19
B.3.5 Heating.19
B.3.6 Mixing systems.19
B.4 Verification of fluid system functions.20
B.4.1 General.20
B.4.2 Verification of accuracy of a fluid mixing system .20
B.4.3 Verification of fluid system concerning degradation of Non-Newtonian (pseudoplastic) fluid .20
B.4.4 Verification of accuracy of a fluid metering system .21
Annex C (informative)  Toxicological aspects of using deicing/antiicing equipment.22
C.1 General.22
C.2 Systems and training of operators .22
C.2.1 General.22
C.2.2 Design of the spraying equipment.23
C.2.3 Training of operators.23
C.3 Effects on humans.24
C.3.1 Toxicity of glycols .24
C.3.2 Work environment considerations.24
2

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EN 12312-6:2004 (E)
C.3.3 Aircraft internal environment considerations .25
C.4 Recommendations.25
Annex D (informative)  Environmental aspects of deicing/antiicing at airports.26
D.1 General.26
D.2 Environmental protection.26
D.2.1 General.26
D.2.2 Collection of glycol.27
D.2.3 Treatment of glycol .27
D.3 Environmental effects of deicing/antiicing fluids .29
D.3.1 General.29
D.3.2 Effects on aquatic environment .29
D.3.3 Effects on soil environment .29
D.4 Recommendations.30
Annex E (informative)  Loading control .31
Annex ZA (informative)  Relationship between this European Standard and the Essential
Requirements of EU Directive 98/37/EC, amended by Directive 98/79/EC .32
Bibliography.33

3

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EN 12312-6:2004 (E)
Foreword
This document (EN 12312-6:2004) has been prepared by Technical Committee CEN/TC 274 "Aircraft ground sup-
port 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 November 2004, and conflicting national standards shall be withdrawn at the latest
by November 2004.
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 annex ZA, which is an integral part 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
Annex A is normative. Annexes B, C, D and E are informative.
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, Cyprus, Czech Republic, Denmark, Esto-
nia, Finland, France, Germany, Greece, Hungary, Iceland, Ireland, Italy, Latvia, Lithuania, Luxembourg, Malta,
Netherlands, Norway, Poland, Portugal, Slovakia, Slovenia, Spain, Sweden, Switzerland and United Kingdom.

4

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EN 12312-6:2004 (E)
Introduction
This European Standard specifies health and safety requirements, as well as some functional and performance
requirements, for deicers and equipment intended for deicing/antiicing of all aircraft types commonly in service in
civil air transport. It contains functional and environmental aspects of deicing in the informative annexes B, C
and D.
The minimum essential criteria are considered to be of primary importance in providing safe, serviceable, economical,
and usable deicers and deicing/antiicing equipment. Deviation from the recommended criteria should occur only after
careful consideration, extensive testing, risk assessment and thorough service evaluation have shown alternative
methods or conditions to be satisfactory.
This document is a Type C standard as stated in EN 1070:1998.
The machinery concerned and the extent to which hazards, hazardous situations and events are covered are indi-
cated 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 pro-
visions 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.
5

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EN 12312-6:2004 (E)

1 Scope
This European Standard specifies the technical requirements to minimise the hazards listed in clause 4 which can
arise during the commissioning, operation and maintenance of deicers and equipment designed exclusively for
deicing and washing of aircraft with deicing/antiicing/washing liquids 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 GSE manufacturers as well as
airlines and handling agencies.
NOTE Safety of aircraft in connection with deicing/antiicing operations is not dealt with in this European Standard. Any,
even minor, aircraft deicing or antiicing operation directly affects flight safety on take-off. Prevention of aeronautical accidents
resulting from in-flight icing principally concerns the fluids and methods used, but it may in certain cases also concern deicing or
antiicing equipment design or operation. These aeronautical aspects are not covered in this European Standard (see also Joint
Aviation authorities (JAA), Joint Aviation Regulations (JAR) JAR-OPS subpart D 1.345 and any associated material).
This standard applies to:
 self-propelled deicers with fixed platform or hinged boom;
 towable deicers with fixed platform or hinged boom;
 stationary deicing/antiicing equipment (e.g. fixed boom, gantry or tower cranes equipped with aircraft
deicing/antiicing fluid systems).
This standard does not apply to:
 fixed installations, such as separate storage tanks or heating and filling stations, which are not an integrated
part of the stationary deicing equipment;
 hydraulic control systems;
 pneumatic systems;
 flow generating systems as such.
This standard does not establish requirements for noise and vibration.
Noise and vibration are dealt with respectively in prEN 1915-4 and prEN 1915-3.
This standard is not dealing with hazards in respect to a standard automotive chassis and the traffic on the apron.
This part of EN 12312 is not applicable to deicers and deicing/antiicing equipment which are manufactured before
the date of publication by CEN of this standard.

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 amendment or revision. For undated references the latest edition of the
publication referred to applies (including amendments).
EN 418:1992, Safety of machinery — Emergency stop equipment, functional aspects — Principles for design.
EN 795:1996, Protection against falls from a height — Anchor devices — Requirements and testing.
EN 1050:1996, Safety of machinery — Principles for risk assessment.
6

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EN 12312-6:2004 (E)
EN 1070:1998, Safety of machinery — Terminology.
EN 1915-1:2001, Aircraft ground support equipment — General requirements — Part 1: Basic safety requirements.
EN 1915-2:2001, Aircraft ground support equipment — General requirements — Part 2: Stability and strength
requirements, calculations and test methods.
ISO 4305:1991, Mobile cranes — Determination of stability.
ISO 11076:2000, Aerospace — Aircraft de-icing/anti-icing methods with fluids.
3 Terms and definitions
For the purposes of this European Standard, the terms and definitions given in EN 1070:1998, EN 1915-1:2001
and ISO 11076:2000 and the following apply.
3.1
deicing/antiicing equipment
piece of equipment, mobile or stationary, used for performing deicing/antiicing/washing operations on aircraft on the
ground
3.2
deicer
entire mobile unit, including the chassis and any structures mounted thereon
3.3
self-propelled deicer
deicer able to move by an own power source and to operate without a constant connection to external energy or
fluid supply
3.4
towable deicer
deicer not able to move by an own power source
3.5
stationary deicing/antiicing equipment
permanently installed equipment, e.g. gantry, fixed boom or other crane types
3.6
boom
moveable hinged beam attached to the integral frame carrier to support the lifting/work platform
3.7
chassis cabin
driver's cabin mounted on the chassis of a self-propelled deicer
3.8
operator's cabin
boom mounted, enclosed lifting/work platform
3.9
basket
boom mounted, open lifting/work platform
3.10
harness anchorage point
point for attaching the operator's safety harness
7

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EN 12312-6:2004 (E)
3.11
deicing pad
dedicated area on an airport specially designed for deicing
4 List of significant hazards
The list of hazards (see annex A) is based on EN 1050:1996 and contains the hazards and hazardous situations,
as far as they are dealt with in this European Standard, identified by risk assessment as significant for deicers and
deicing equipment and which require action to eliminate or reduce risks.
5 Safety requirements and/or measures
5.1 General requirements
5.1.1 Deicers and deicing/antiicing equipment shall conform to the relevant requirements of EN 1915-1:2001
unless otherwise specified in this standard. They shall also conform to the specific requirements of this standard.
5.1.2 The operating conditions shall be given by the manufacturer. Deicers shall be designed to operate safely in
a continuous relative humidity of 94 %.
Materials and devices used shall take into account the environmental conditions intended to be encountered by
deicing equipment, e.g. with respect to temperature, sun, precipitation and freezing effects.
NOTE The operating conditions and the materials chosen are depending on the airport of use (see clause 0 of
EN 1915-1:2001 — negotiation).
5.1.3 The design of deicers and deicing/antiicing equipment shall take into account the operational conditions for
deicing/antiicing as given in ISO 11076:2000.
5.2 Spray system
5.2.1 The control of hand held spray guns shall be of the hold-to-run type.
5.2.2 Fixed spray guns of deicers shall be prevented from spraying directly towards the operator's position, e.g.
by means of a positive fit.
5.2.3 In case of spray gun failure it shall be possible to stop the fluid flow by means of an additional shut-off
valve.
5.3 Stability and strength
5.3.1 Calculation of stability and strength shall be carried out according to EN 1915-2:2001. Deicing equipment
shall be stable under all working conditions.
Any life limited components shall be calculated for a foreseeable lifetime of 10 000 hours of operating taking into
account foreseeable wear and corrosion.
5.3.2 Deviating from 5.2.2.3 of EN 1915-2:2001 the maximum number of persons in the cabin/basket shall be
two. The maximum rated load shall be 205 kg.
5.3.3 Where intended operation includes deicing/antiicing with aircraft engines running, the additional forces
shall be taken into account.
5.3.4 Spraying forces are considered as being dynamic forces (see 5.2.2.4 of EN 1915-2:2001).
5.3.5 Special attention shall be given to the calculation of telescopic boom joints.
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EN 12312-6:2004 (E)
5.3.6 The design of deicers shall not need stabilizers to ensure stability.
Where chassis spring locks or torsion bars are used, they shall automatically be engaged when the cabin/basket is
moved out of the base position.
5.3.7 Where open baskets are used, the nozzle and hose(s) shall be considered as structural parts for calcula-
tion purposes.
5.3.8 For fatigue stress analysis, the factor for the intended load spectrum shall not be less than one and the
4
amount of load cycles never less than 2 × 10 (see also 5.2.6 of EN 1915-2:2001).
5.3.9 The maximum overturning and corresponding stabilizing moments shall be calculated about the most unfa-
vourable tipping lines and with empty tanks.
Tipping lines shall be determined as shown in ISO 4305:1985.
NOTE For solid and foam-filled tyres the tipping lines may be taken at 1/4 of the tyre ground contact width from the outside
of the ground contact width.
5.3.10 In addition to the verification of stability and strength in accordance with EN 1915-2:2001 the following tests
shall be done:
 vehicle driving over a test fixture at maximum allowable speed (6 km/h) in forward and reverse directions. The
wheels driving over test fixture shall be the ones giving highest stresses in boom structure. The test fixture
shall be a device used to simulate obstacles that may be encountered on an airport ramp (e.g. wheel chocks,
storm drains, fuel pit lids, snow and ice ruts, etc.). The test fixture shall be made out of wood or any other simi-
lar material measuring 100 mm (4 in) high, 150 mm (6 in) wide and 600 mm (24 in) long. The top corners shall
be symmetrically cut at 45° angles along the longitudinal length of the member providing a top flat surface
measuring 50 mm (2 in) in width. The test fixture shall be secured in such a manner that prevents sliding or
overturning as the vehicle is driven over it during dynamic load testing.
 vehicle driving at maximum allowable speed (6 km/h) in forward and reverse directions and suddenly applying
brakes to simulate emergency (panic) stops.
Both tests shall incorporate boom orientation and fluid tank level which generate maximum stress on the structural
boom components. The basket/enclosed cabin shall be loaded at maximum rated capacity. In addition to these
loads the windload shall be incorporated by calculation afterwards. During the tests the stress levels shall be
measured using strain gauge or equivalent measurement techniques. How and where to mount the strain gauges
shall be done in accordance with relevant industry practices.
NOTE Relevant recommendations for the mounting of strain gauges can be found e.g. in IIW (International Institute of
weldings) publications (see Bibliography).
The design verification shall be done comparing measured stresses (with incorporated wind loads) and yield
strength of the material in question. To pass the tests the minimum acceptable safety factors are as stated in
Table 1 in EN 1915-2:2001.
5.4 Safeguards and safety devices
5.4.1 Operator's seats shall be provided with 3 point type inertial reel seat belts as used on standard automotive
vehicles.
5.4.2 Harness anchorage points for each person in accordance with EN 795:1996 Class A shall be provided at
baskets.
5.5 Emergency systems
5.5.1 Deicers shall be fitted with:
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EN 12312-6:2004 (E)
 an emergency lowering control at ground level or at an accessible position (see 5.13 of EN 1915-1:2001 for
access). The design and position of this control shall ensure visibility on the movement of the cabin/basket.
This control device shall override the control devices for lifting and lowering;
 an emergency control system in the cabin/basket to move the boom in case of primary power loss;
 an emergency valve at the base lifting cylinder. Provision shall be made for safe access, e.g. portable ladder,
and for use of personal protective equipment against falling.
5.5.2 Emergency stops shall meet the requirements of EN 418 category 0 (see 4.1.5 of EN 418:1992). At least
one shall be provided in the cabin/basket on deicers. Additional emergency stops shall be installed on the outer
contour reachable from ground level, e.g. on each longitudinal side.
5.5.3 Emergency stops on deicers shall:
 stop and hold all boom and cabin/basket movements;
 shut down the fluid pump and heater;
 apply parking brakes.
Emergency stops on deicers shall not:
 impede the emergency lowering function;
 stop the function of communication systems;
 switch off working lights;
 shut down fire extinguisher systems, where applicable.
5.5.4 Emergency stops on stationary systems shall be installed at operator's position(s) as well as on the
structure and reachable from ground level, e.g. on each travelling gear or fundament.
5.5.5 On stationary deicing/antiicing equipment emergency stops shall stop all motions, the fluid supply and the
spraying system.
5.5.6 To prevent overheating and overpressure, the fluid heater shall be equipped with safety devices. As a
minimum, two independent overheat thermo-swit
...

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