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本文(BS M 87-1996 Aircraft ground support equipment - Catering vehicle for large capacity aircraft - Functional requirements《航空地面支持设备 大容量飞机用供膳车 功能要求》.pdf)为本站会员(roleaisle130)主动上传,麦多课文库仅提供信息存储空间,仅对用户上传内容的表现方式做保护处理,对上载内容本身不做任何修改或编辑。 若此文所含内容侵犯了您的版权或隐私,请立即通知麦多课文库(发送邮件至master@mydoc123.com或直接QQ联系客服),我们立即给予删除!

BS M 87-1996 Aircraft ground support equipment - Catering vehicle for large capacity aircraft - Functional requirements《航空地面支持设备 大容量飞机用供膳车 功能要求》.pdf

1、BRITISH STANDARD AEROSPACE SERIES BS M 87:1996 ISO 10841: 1996 Aircraft ground support equipment Catering vehicle for large capacity aircraft Functional requirements ICS 49.100BSM87:1996 This British Standard, having been prepared under the direction of the engineering Sector Board, was published un

2、der the authorityof the Standards Board and comes into effect on 15 September 1996 BSI 01-1999 The following BSI references relate to the work on this standard: Committee reference ACE/57 Draft for comment 93/714884 DC ISBN 0 580 26055 0 Committees responsible for this British Standard The preparati

3、on of this British Standard was entrusted to Technical Committee ACE/57, Aircraft cargo systems and ground equipment, upon which the following bodies were represented: Association of Webbing Load Restraint Equipment Manufacturers British Airways British Narrow Fabrics Association Civil Aviation Auth

4、ority (Airworthiness Division) Health and Safety Executive Ministry of Defence Society of British Aerospace Companies Ltd. Society of Motor Manufacturers and Traders Ltd. Amendments issued since publication Amd. No. Date CommentsBSM87:1996 BSI 01-1999 i Contents Page Committees responsible Inside fr

5、ont cover National foreword ii Introduction 1 1 Scope 1 2 Normative references 1 3 Structure and overall dimensions 1 4 Stability 3 5 Controls 3 6 Personnel protection 3 7 Emergency 4 8 Options 4 Annex A (informative) Bibliography 5 List of references Inside back coverBSM87:1996 ii BSI 01-1999 Natio

6、nal foreword This British Standard has been prepared by Technical Committee ACE/57 and is identical with ISO10841:1996 Aircraft Catering vehicle for large capacity aircraft Functional requirements, published by the International Organization for Standardization (ISO). The Technical Committee has rev

7、iewed the provisions of ISO 8058:1985, to which normative reference is made in the text, and has decided that they are acceptable for use in conjunction with this standard. A British Standard does not purport to include all the necessary provisions of a contract. Users of British Standards are respo

8、nsible for their correct application. Compliance with a British Standard does not of itself confer immunity from legal obligations. Cross-references Publication referred to Corresponding British Standard ISO 1496-2:1988 BS 3951 Freight containers Part 2 Specification and testing of series 1 freight

9、containers Section 2.2:1989 Thermal containers (Identical) ISO 6966:1993 BS M 74:1994 Air cargo equipment. Basic requirements for aircraft loading equipment (Identical) ISO 7000:1989 BS 7324:1990 Guide to graphical symbols for use on equipment (Identical) ISO 11995:1996 BS M 89:1996 Aircraft ground

10、support equipment Stability requirements for loading and servicing equipment (Identical) Summary of pages This document comprises a front cover, an inside front cover, pagesi and ii, pages1to6,an inside back cover and a back cover. This standard has been updated (see copyright date) and may have had

11、 amendments incorporated. This will be indicated in the amendment table on theinside front cover.BSM87:1996 BSI 01-1999 1 Introduction The minimum essential criteria are identified by the use of the key word “shall”. Recommended criteria are identified by the use of the key word “should”, and while

12、not mandatory are considered to be of primary importance in providing serviceable, economical, and practical catering vehicles. Deviation from the recommended criteria should occur only after careful consideration, extensive testing, and thorough service evaluation have shown alternate methods to be

13、 satisfactory. 1 Scope 1.1 This International Standard specifies the functional, performance and safety requirements for a vehicle equipped with a liftable van body designed for: cabin resupply and servicing, and/or loading and unloading of catering equipment and supplies on all large capacity aircr

14、aft types commonly in service in international civil air transport with a cabin door sill height equal to or exceeding 2,54m (100in) over the ground. 1.2 The intent of this International Standard is not to specify equipment design, but rather to define minimum functional and performance requirements

15、 and highlight those criteria which are known to be essential to an efficient and safe operation on civil transport aircraft in the environment of international airports by aircraft and vehicle manufacturers as well as airlines and catering agencies. 1.3 It shall be applied with due reference to nat

16、ional governmental regulations of the country where the vehicle is to be operated. The main though not exclusive areas in which such national regulations may be more stringent than the requirements of this International Standard are: sanitary requirements regarding design, cleaning and disinfection

17、of vehicles used to carry food for human consumption, stability and other safety requirements applicable to elevating equipment carrying personnel in the elevated position. 2 Normative references The following standards contain provisions which, through reference in this text, constitute provisions

18、of this International Standard. At the time of publication, the editions indicated were valid. All standards are subject to revision, and parties to agreements based on this International Standard are encouraged to investigate the possibility of applying the most recent editions of the standards ind

19、icated below. Members of IEC and ISO maintain registers of currently valid International Standards. ISO 1496-2: 1) , Series 1 freight containers Specification and testing Part 2: Thermal containers. ISO 6966:1993, Aircraft Basic requirements for aircraft loading equipment. ISO 7000:1989, Graphical s

20、ymbols for use on equipment Index and synopsis. ISO 8058:1985, Air cargo equipment Air mode insulated containers Thermal efficiency requirements. ISO 11995:1996, Aircraft Stability requirements for loading and servicing equipment. 3 Structure and overall dimensions 3.1 General 3.1.1 The vehicle shal

21、l be constructed on a standard automotive chassis of appropriate gross weight rating. 3.1.2 The dimensions, laden weight and other characteristics of the vehicle shall satisfy all applicable government regulations for vehicles to be used on public roadways. 3.1.3 The vehicle shall be equipped with a

22、 fully enclosed elevating van body with a front platform, capable of reaching heights between 2,54m (100in) and 5,6m (220in) above the ground. 3.1.4 The allowable load capacity in the elevating van body should be no less than 2700kg (6000lb). A3500kg (7700lb) load capacity is recommended. 3.2 Overal

23、l dimensions 3.2.1 The overall height of the vehicle in the fully lowered position shall not exceed 4m (157in). 3.2.2 The overall width of the vehicle in a driving condition (with stabilizers retracted) shall not exceed 2,5m (98in), or less if so required by locally applicable regulations. 1) To be

24、published. (Revision of ISO 1496-2:1988)BSM87:1996 2 BSI 01-1999 NOTE 1Overall height and width of the vehicle may be further restricted by public roads regulations in certain countries. 3.2.3 The vehicle shall be capable of turning within an overall swept radius of less than 12,2m (40ft). 3.2.4 In

25、order to alleviate aircraft handling difficulties and ramp congestion in the vicinity of an aircraft being serviced, the overall length of the vehicle should be kept to a minimum, consistent with intended van body usable internal length, and other requirements and vehicle equipment (e.g.tailgate). 3

26、.3 Van body 3.3.1 The usable internal length of the van body should be not less than 6m (20ft). 3.3.2 The usable internal width of the van body should be not less than 2,3m (91in). 3.3.3 The minimum clear height at any point within the van body with its doors open or closed shall be1,9m (75in). 3.3.

27、4 The interior of the van body shall be fully lined with a smooth, non-moisture-absorbent, non-toxic material, sanitarily approved for use in vehicles carrying food for human consumption. In addition: the lining material shall be compatible with repeated cleaning with strong detergents and disinfect

28、ing agents, as well as suitable for repeated water pressure cleaning and/or steam cleaning; any joints or appurtenances inside the van body shall be flush, rounded, sloped or otherwise protected to prevent any accumulation of dirt or rubbish and facilitate comprehensive cleaning. 3.3.5 The floor sha

29、ll repeatedly withstand a full complement of catering carts weighing up to80kg(175lb) each on four 50mm (2in) diameter and25mm (1in) width castered wheels located750mm 250mm (30in 10in) apart from each other, without deflecting more than6mm(0,25in). No permanent deflection is allowable. 3.3.6 In add

30、ition, the floor shall: a) be smooth and free from any joint or recess allowing accumulation of dirt or rubbish, and shall meet the cleaning requirements in3.3.4; b) provide an anti-slip surface throughout its whole area; c) provide drainage to cater for elimination of any spilled fluids. 3.3.7 Both

31、 sidewalls shall be equipped with: a) protective devices to avoid deterioration by impact from fully loaded catering carts as defined in3.3.5, and b) quick fastening restraint devices capable of ensuring proper restraint of a full complement of such catering carts under normal over-the-road horizont

32、al and vertical accelerations. 3.3.8 The van body shall be equipped with two doors at the forward and rear ends, with a minimum usable width of 0,8m (31in) and a minimum clear height of 1,9m (75in). 3.3.9 A lighting system shall be fitted within the van body, to provide a minimum illumination of50lx

33、(4,65ftcd) at any point on the floor. 3.4 Front platform 3.4.1 The vehicle shall be equipped with a front platform to be level with the van body floor within the specified working height range, consisting of: a) a fixed platform over the full width of the van, the length of which should be a minimum

34、 of1,6m(63in), and b) a sliding bridge to allow alignment with the aircraft door. The width of the sliding bridge should be at least 0,8m (31in) and shall not exceed 1m (39in). 3.4.2 The fixed front platform shall repeatedly withstand a distributed load of 600kg (1320lb), or a 300kg (660lb) concentr

35、ated load at either forward quarter area, without deflecting more than6mm(0,25in). No permanent deflection is allowable. 3.4.3 A suitable safety shield shall be fitted vertically in front of the van body, the function of this shield being to close the gap between the body floor in the lowered positi

36、on and the upper floor line of the front platform. The safety shield shall be flush mounted, with a maximum 6mm (0,25in) clearance from the forward edge of the van bodys floor. 3.4.4 The platform floor shall provide an anti-slip surface throughout its whole area. 3.4.5 A spotlight or equivalent shal

37、l be fitted on the front end of the van body to light the platform, and provide a minimum illumination of 50lx (4,65ftcd) at any point on its floor and the floor of the sliding bridge. 3.4.6 The sliding bridge shall: a) be adjustable over the whole width of the fixed front platform, and lockable at

38、intermediate positions, and b) have telescopic extension and retraction capability over a minimum length of0,5m(20in).BSM87:1996 BSI 01-1999 3 3.4.7 The sliding bridge shall repeatedly withstand a distributed load of 350kg (770lb), or a100kg(220lb) concentrated load at its forward end when fully ext

39、ended, without deflecting more than 6mm (0,25in). No permanent deflection is allowable. 3.4.8 The area directly below the sliding bridge shall be free from any components or protrusions within at least 0,3m (12in) from its forward end. The bridges thickness in this area shall be kept to a minimum. 3

40、.4.9 The forward edge of the sliding bridge shall be protected at aircraft interface by a full-width cylindrical rubber bumper. 4 Stability 4.1 A minimum of four stabilizers shall be provided for van body elevation. The stabilizers in the retracted position shall not protrude from the vehicles overa

41、ll width as specified in3.2.2. In addition, the stabilizers in the extended position should preferably not protrude from the overall width. 4.2 When supported by the fully extended stabilizers, the vehicle in both the maximum gross weight and empty conditions shall meet the static and wind stability

42、 criteria of ISO11995. 4.3 It shall not be possible: a) to raise the van body beyond 2,54m (100in) height when the stabilizers are not fully extended and supporting the vehicles weight against a supporting surface. b) to retract the stabilizers under normal conditions until the van body has been low

43、ered to2,54m (100in). (See7.2 for emergency conditions.) c) to drive the vehicle when the stabilizers are not fully retracted or the van body is not in the fully down position. Manual override of the latter interlock shall be possible for emergency conditions. (See7.3.) d) for the stabilizers to col

44、lapse in case of a system failure. 5 Controls 5.1 Controls for raising and lowering the van body and the front platform shall be located in the van body and the vehicle cabin. 5.2 The control panel in the van body shall be located at the forward end. 5.3 Controls for extending and retracting the sta

45、bilizers shall be located in the vehicle cabin only, and shall be protected against inadvertent activation. Positive confirmation by a warning light or equivalent device indicating that the stabilizers are either fully retracted or fully extended and supporting the vehicles weight against a supporti

46、ng surface shall be provided next to the controls. 5.4 Emergency stop buttons which kill the engine shall be provided at both control panels. 5.5 It shall be possible to start and stop the engine from both the vehicle cabin and the van body control panels. 5.6 The engine shall be equipped with a dem

47、and throttle providing high idle whenever one of the hydraulic functions is actuated. 5.7 All controls shall be identified by the appropriate pictographic symbols as described inISO7000. 5.8 The control panels layout should insofar as practical meet the requirements of IATAAHM915, section2. 6 Person

48、nel protection 6.1 The equipment shall meet the appropriate requirements of ISO6966. 6.2 A ladder shall be provided to give access from the ground to the front platform when in the lowered position. The ladder shall not extend beyond the overall width of the vehicle as specified in3.2.2. It shall be

49、 fitted with anti-slip rungs and adequate handholds. 6.3 Steps shall be provided at the rear of the body to allow easy access to and from the body in the lowered position. The steps shall have an anti-slip surface and be fitted with adequate handholds. 6.4 Rigid handrails including knee rails and footrails shall be provided on both sides of the front platform. They shall include: a) adjustable elements between the platform and the sliding bridge. b) extendable elements along both sides of the sliding bridge. c) an adequate opening to g

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