BS ISO 27471-2012 Aircraft ground equipment Upper deck loader Functional requirements《航空地勤支援设备 上层甲板装载机 功能要求》.pdf

1、raising standards worldwideNO COPYING WITHOUT BSI PERMISSION EXCEPT AS PERMITTED BY COPYRIGHT LAWBSI Standards PublicationBS ISO 27471:2012Aircraft ground equipment Upper deck loader Functional requirementsBS ISO 27471:2012 BRITISH STANDARDNational forewordThis British Standard is the UK implementat

2、ion of ISO 27471:2012.The UK participation in its preparation was entrusted to TechnicalCommittee ACE/57, Air cargo and ground support equipment.A list of organizations represented on this committee can beobtained on request to its secretary.This publication does not purport to include all the neces

3、saryprovisions of a contract. Users are responsible for its correctapplication. The British Standards Institution 2012. Published by BSI StandardsLimited 2012ISBN 978 0 580 56929 6ICS 49.100Compliance with a British Standard cannot confer immunity fromlegal obligations.This British Standard was publ

4、ished under the authority of theStandards Policy and Strategy Committee on 30 June 2012.Amendments issued since publicationDate Text affectedBS ISO 27471:2012 ISO 2012Aircraft ground equipment Upper deck loader Functional requirementsMatriel au sol pour aronefs Chargeur de pont suprieur Exigences fo

5、nctionnellesINTERNATIONAL STANDARDISO27471First edition2012-06-15Reference numberISO 27471:2012(E)BS ISO 27471:2012ISO 27471:2012(E)ii ISO 2012 All rights reservedCOPYRIGHT PROTECTED DOCUMENT ISO 2012All rights reserved. Unless otherwise specified, no part of this publication may be reproduced or ut

6、ilized in any form or by any means, electronic or mechanical, including photocopying and microfilm, without permission in writing from either ISO at the address below or ISOs member body in the country of the requester.ISO copyright officeCase postale 56 CH-1211 Geneva 20Tel. + 41 22 749 01 11Fax +

7、41 22 749 09 47E-mail copyrightiso.orgWeb www.iso.orgPublished in SwitzerlandBS ISO 27471:2012ISO 27471:2012(E) ISO 2012 All rights reserved iiiContents PageForeword iv1 Scope 12 Normative references . 13 Terms and definitions . 24 Requirements . 34.1 General . 34.2 Guide rails and stops . 54.3 Conv

8、eyor surface 64.4 Platform operation and loading . 74.5 Mobility and stability 74.6 Controls . 84.7 Emergency 95 Options . 9Bibliography . 11BS ISO 27471:2012ISO 27471:2012(E)ForewordISO (the International Organization for Standardization) is a worldwide federation of national standards bodies (ISO

9、member bodies). The work of preparing International Standards is normally carried out through ISO technical committees. Each member body interested in a subject for which a technical committee has been established has the right to be represented on that committee. International organizations, govern

10、mental and non-governmental, in liaison with ISO, also take part in the work. ISO collaborates closely with the International Electrotechnical Commission (IEC) on all matters of electrotechnical standardization.International Standards are drafted in accordance with the rules given in the ISO/IEC Dir

11、ectives, Part 2.The main task of technical committees is to prepare International Standards. Draft International Standards adopted by the technical committees are circulated to the member bodies for voting. Publication as an International Standard requires approval by at least 75 % of the member bod

12、ies casting a vote.Attention is drawn to the possibility that some of the elements of this document may be the subject of patent rights. ISO shall not be held responsible for identifying any or all such patent rights.ISO 27471 was prepared by Technical Committee ISO/TC 20, Aircraft and space vehicle

13、s, Subcommittee SC 9, Air cargo and ground equipment.iv ISO 2012 All rights reservedBS ISO 27471:2012INTERNATIONAL STANDARD ISO 27471:2012(E)Aircraft ground equipment Upper deck loader Functional requirements1 ScopeThis International Standard specifies the functional and performance requirements for

14、 a self-propelled container/pallet loader capable of raising air cargo unit load devices (ULDs) to the upper deck of very large capacity freighter (VLCF) aircraft and also to the main deck of any main-line freighter aircraft.This International Standard does not intend to provide all the design requi

15、rements applicable for aircraft upper-deck loaders. Other requirements can be found in separate standards which are also applicable: ISO 4116 specifies the additional requirements applicable for conveying surfaces of aircraft ground support equipment intended for handling and loading of baggage and

16、cargo ULDs; ISO 6966-1 and ISO 6966-2 specify, respectively, the general and safety-related requirements applicable to all aircraft ground support equipment.The requirements of this International Standard were determined based on generally recognized assumptions as to:a) the normally intended use of

17、 aircraft ground support equipment, when used on the ramp of international civil airports in order to handle, service or maintain civil transport aircraft;b) the environmental (surface, slope, weather, lighting, operating rules, traffic infrastructure, staff qualification, etc.) conditions prevailin

18、g on the ramp area of the majority of international civil airports.It is assumed that the manufacturers of aircraft upper-deck loaders define in the relevant documentation the specifically intended conditions of use and environment for each model, and that the purchasers systematically review their

19、own specific conditions of use and environment in order to determine whether those stated are adequate, or negotiate with the manufacturer appropriate modifications to ensure they are.This International Standard does not specify requirements applicable to: any adapters or ancillary/supplemental equi

20、pment additions to in-service main-deck loaders in order to allow their occasional upper-deck use; any main-deck loaders fitted with optional access to upper-deck height of the front platform only (ISO 6967:2006, 4.8).2 Normative referencesThe following referenced documents are indispensable for the

21、 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.ISO 4116, Air cargo equipment Ground equipment requirements for compatibility with aircraft unit load devicesI

22、SO 6966-1, Aircraft ground equipment Basic requirements Part 1: General design requirementsISO 6966-2, Aircraft ground equipment Basic requirements Part 2: Safety requirementsISO 7000, Graphical symbols for use on equipment Registered symbolsISO 8097:2001, Aircraft Minimum airworthiness requirements

23、 and test conditions for certified air cargo unit load devicesISO 11532, Aircraft ground equipment Graphical symbols ISO 2012 All rights reserved 1BS ISO 27471:2012ISO 27471:2012(E)ISO 11995:1996, Aircraft Stability requirements for loading and servicing equipmentISO 14122-3, Safety of machinery Per

24、manent means of access to machinery Part 3: Stairs, stepladders and guard-railsISO 21100, Air cargo unit load devices Performance requirements and test parameters3 Terms and definitionsFor the purposes of this document, the following terms and definitions apply.3.1cycle timetime elapsed between the

25、moment the loader reaches any reference position (e.g. ground level) and the next moment it reaches the same position, after transferring a full complement of unit load devices (ULDs) on the ground level, raising, transferring the ULDs to the aircraft, and coming down againNOTE 1 Cycle time depends

26、on loader performance.NOTE 2 The addition of the necessary loader cycles constitutes the (offloading and loading) aircraft turnaround time.3.2cycle timeloader cycle time divided by the number of ULDs carried in one cycleNOTE 1 ULD cycle time represents the mean time to load or offload a ULD into or

27、from the aircraft.NOTE 2 ULD cycle time depends on both loader performance and size.3.3lower decklowest deck of either a two-deck or a three-deck very large capacity (VLCA) main-line aircraft3.4main deckthe highest deck of a two-deck main-line aircraft, or the intermediate deck of a three-deck very

28、large capacity aircraft (VLCA)3.5main-line aircraftcivil passenger and/or freight transport aircraft with a maximum ramp mass over 50 000 kg (110 000 lb)3.6turnaround timetotal elapsed time between the moment a fully loaded aircraft starts being offloaded and the moment it is fully loaded againNOTE

29、Turnaround time constitutes the primary economic objective of the operating airline.3.7unit load deviceULDdevice for grouping, transferring and restraining cargo for transitNOTE A ULD may consist of a pallet with a net or it may be a container.3.8upper deckhighest deck of a three-deck very large cap

30、acity aircraft (VLCA)2 ISO 2012 All rights reservedBS ISO 27471:2012ISO 27471:2012(E)3.9very large capacity aircraftVLCAmain-line aircraft with three decks and a maximum ramp mass over 453 600 kg (1 000 000 lb)3.10very large capacity freighterVLCFfreighter version of a very large capacity aircraft,

31、including an upper deck load of unit load devices (ULDs)4 Requirements4.1 General4.1.1 Upper deck loaders defined by this International Standard shall be capable of raising and transferring air cargo ULDs with base dimensions and maximum massesas follows:ISO 8097/ISO 21100Base size codeLength mm (in

32、)Width mm (in)Max. gross mass kg (lb) Main deckMax. gross mass kg (lb) Upper deckA 3 175 (125) 2 235 (88) 6 804 (15 000) 4 080 (9 000)M 3 175 (125) 2 438 (96) 6 804 (15 000) 4 445 (9 800)Na2 438 (96) 1 562 (61,5) 3 402 (7 500) 2 220 (4 900)R 4 978 (196) 2 438 (96) 11 340 (25 000) 8 980 (19 800)Sa2 2

33、35 (88) 1 562 (61,5) 3 402 (7 500) 2 040 (4 500)G 6 058 (238,5) 2 438 (96) 13 600 (30 000)bNot allowableaOptional (see 5.11).bOr higher, on customer request (see 5.13 and 5.14).4.1.2 On an adequate chassis, the loader shall provide at least two platforms, and may provide three:a) an aircraft interfa

34、ce platform capable of operating between 2 590 mm (102 in) to at most 2 900 mm (114 in) (see 4.1.4 and 4.1.9) and 8 380 mm (330 in) above the ground, which is positioned at the applicable aircraft door and shall remain at this position during the complete loading/unloading operation;b) optionally, a

35、n intermediate platform shuttling between the aircraft interface and main platforms;c) a main platform for up and down movement between 480 mm (19 in) and either 8 380 mm (330 in) or, if an intermediate shuttling platform is provided, 5 540 mm (218 in) above the ground.4.1.3 The overall dimensions o

36、f the unit shall be kept to a minimum consistent with its intended use and performance. See 4.5.6 for turning-radius requirements.4.1.4 The overall height of the entire unit when being driven should not exceed 4 000 mm (157 in), in order to be compatible with usually encountered airport infrastructu

37、re. See 4.1.9 for foldable guard-rails if needed.It is recommended not to exceed this value. Loaders may however exceed it, subject to verification of available height clearances in the intended movement zone at the airport of use, but should not in any event exceed 5 000 mm (197 in), in order to pr

38、event the risk of interference with the aircraft wing trailing edge while positioning at main-deck doors aft of it.4.1.5 The loader shall simultaneously support, at their maximum gross mass, at least: one 2 438 mm 3 175 mm (96 in 125 in) ULD in either direction on the aircraft interface platform; IS

39、O 2012 All rights reserved 3BS ISO 27471:2012ISO 27471:2012(E) two 2 438 mm 3 175 mm (96 in 125 in) ULDs in either direction on the main platform; where applicable, one 2 438 mm 3 175 mm (96 in 125 in) ULD in either direction on an intermediate platform.Where the intermediate platform provides more

40、than one ULD position, the aircraft interface platform may be smaller than one position. However, in such a case, an increased hazard may result from personnel working near to the aircraft door area being too close to the platforms edge: a retractable safety barrier (see 5.9) shall then be provided

41、aft of the platform as a guard-rail across the whole width whenever the adjacent platform is not level with the aircraft interface platform.4.1.6 The aircraft interface platform shall be adjustable to changes in aircraft attitude:a) pitch and roll: within a minimum range of 2 (3,5 %);b) height: with

42、 an accuracy of 6 mm (0,25 in).4.1.7 The aircraft interface platform shall be designed not to interfere with the opening and closing of the aircraft doors, either from a safe position on the loader or from inside the aircraft, up to a door width of 4 320 mm (170 in), with no less than 100 mm (4 in)

43、clearance on each side. All component parts that may come into contact with the aircraft should be covered with protective padding, e.g. rubber tube or “D” section. See Reference 12 for information on protective materials.4.1.8 The aircraft interface platform shall include adjustable side guides tha

44、t can be aligned with those of the aircraft and locked into position. The platform should be: either overhanging by at least 305 mm (12 in) forward of the front vertical end of the chassis;or fitted on its forward edge with a telescoping element with rollers, in order to bridge the gap to the aircra

45、ft door sill where this is not achieved by an aircraft cargo door sill folding-out element.The telescopic element extension, if applicable, shall have a minimum 3 300 mm (130 in) width, be powered and extend no less than 305 mm (12 in) forward of the fixed platform edge. It shall not be possible to

46、lift or lower the platform, except for small adjustments to aircraft door sill height, prior to the telescopic element being fully retracted.4.1.9 Fixed safety guard-rails (side panels) shall be fitted to both outer sides of the aircraft interface platform and shall have a minimum height of 1 100 mm

47、 (43 in), in accordance with ISO 14122-3, up to 1 400 mm (55 in). Guard-rails shall be adjustable to fully close any gap between the loader and the aircraft, including when the platforms telescopic element (see 4.1.8), if provided, is fully extended, and on the aircraft door opening.Safety guard-rai

48、ls/side panels shall be lockable in either deployed or stored position and provide a continuous kick plate at least 150 mm (6 in) high. They should preferably be filled with continuous material.When the guard-rails are higher than 1 100 mm (43 in), a continuous hand rail should be provided along the

49、 inner sides at a 1 000 mm (40 in) height. Where necessary, to meet the overall driving height objective (see 4.1.4), the top part of the guard-rails may fold down in the driving mode. In such a case, the top part of the guard-rails shall fold down inward, fail-safe mechanical locking shall be provided for each guard-rail section in the deployed position, and the drivers position shall remain protected.4.1.10 Where an intermediate platform is provided and is authorized for use in lifting personne