1、 g49g50g3g38g50g51g60g44g49g42g3g58g44g55g43g50g56g55g3g37g54g44g3g51g40g53g48g44g54g54g44g50g49g3g40g59g38g40g51g55g3g36g54g3g51g40g53g48g44g55g55g40g39g3g37g60g3g38g50g51g60g53g44g42g43g55g3g47g36g58requirementsICS 49.100; 49.120Aircraft ground equipment Main deck loader Functional BRITISH STANDAR
2、DBS ISO 6967:2006BS ISO 6967:2006This British Standard was published under the authority of the Standards Policy and Strategy Committee on 28 April 2006 BSI 2006ISBN 0 580 48210 3Cross-referencesThe British Standards which implement international publications referred to in this document may be foun
3、d in the BSI Catalogue under the section entitled “International Standards Correspondence Index”, or by using the “Search” facility of the BSI Electronic Catalogue or of British Standards Online.This publication does not purport to include all the necessary provisions of a contract. Users are respon
4、sible for its correct application. Compliance with a British Standard does not of itself confer immunity from legal obligations.Summary of pagesThis document comprises a front cover, an inside front cover, the ISO title page, pages ii to iv, pages 1 to 7 and a back cover.The BSI copyright notice dis
5、played in this document indicates when the document was last issued.Amendments issued since publicationAmd. No. Date CommentsA list of organizations represented on this committee can be obtained on request to its secretary. present to the responsible international/European committee any enquiries on
6、 the interpretation, or proposals for change, and keep UK interests informed; monitor related international and European developments and promulgate them in the UK.National forewordThis British Standard reproduces verbatim ISO 6967:2006 and implements it as the UK national standard. It supersedes BS
7、M 80:1995 which is withdrawn.The UK participation in its preparation was entrusted to Technical Committee ACE/57, Air cargo and ground support equipment, which has the responsibility to: aid enquirers to understand the text;Reference numberISO 6967:2006(E)INTERNATIONAL STANDARD ISO6967Third edition2
8、006-02-01Aircraft ground equipment Main deck loader Functional requirements Matriel au sol pour aronefs Chargeur de pont principal Exigences fonctionnelles BS ISO 6967:2006ii iiiForeword ISO (the International Organization for Standardization) is a worldwide federation of national standards bodies (
9、ISO 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, go
10、vernmental 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/IE
11、C Directives, 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 memb
12、er bodies 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 6967 was prepared by Technical Committee ISO/TC 20, Aircraft and space
13、vehicles, Subcommittee SC 9, Air cargo and ground equipment. This third edition cancels and replaces the second edition (ISO 6967:1994), which has been technically revised. BS ISO 6967:2006iv Introduction This International Standard specifies the functional requirements to be taken into account by m
14、anufacturers for the design of aircraft main deck cargo container and pallet loaders. Throughout this International Standard, the minimum essential criteria are identified by use of the key word shall. Recommended criteria are identified by use of the key word should and, while not mandatory, are co
15、nsidered to be of primary importance in providing safe, economical and usable aircraft main deck loaders. Deviation from recommended criteria should only occur after careful consideration and thorough service evaluation have shown alternative methods to provide an equivalent level of safety. BS ISO
16、6967:20061Aircraft ground equipment Main deck loader Functional requirements 1 Scope This International Standard specifies the functional requirements for a self-propelled loader capable of raising air cargo unit load devices (ULDs) with base dimensions and maximum mass as given in Table 1. Table 1
17、Base dimensions and maximum mass ISO 8097:2001 base size code Length mm (in) Width mm (in) Maximum gross mass kg (lb) A 3 175 (125) 2 235 (88) 6 804 (15 000) M 3 175 (125) 2 438 (96) 6 804 (15 000) R 4 978 (196) 2 438 (96) 11 340 (25 000) G 6 058 (238,5) 2 438 (96) 13 600 (30 000) This International
18、 Standard does not provide all the design requirements applicable for aircraft main deck loaders. Other requirements can be found in separate International Standards: ISO 4116 specifies the additional requirements applicable for conveying surfaces of those pieces of aircraft ground support equipment
19、 intended for handling and loading of baggage and cargo unit load devices; 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 genera
20、lly recognized assumptions with regard to a) the normally intended use of 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 rule
21、s, staff qualification, etc.) conditions prevailing on the ramp area of the majority of international civil airports. It is assumed the manufacturers of aircraft main deck loaders define in the relevant documentation the specifically intended conditions of use and environment for each item of equipm
22、ent, and the purchasers systematically review their 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. BS ISO 6967:20062 2 Normative references The following referenc
23、ed 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. ISO 4116, Air cargo equipment Ground equipment requirements for compati
24、bility with aircraft unit load devices ISO 6966-1, Aircraft ground equipment Basic requirements Part 1: General design requirements ISO 6966-2, Aircraft ground equipment Basic requirements Part 2: Safety requirements ISO 7000, Graphical symbols for use on equipment Index and synopsis ISO 8097:2001,
25、Aircraft Minimum airworthiness requirements and test conditions for certified air cargo unit load devices ISO 11995:1996, Aircraft Stability requirements for loading and servicing equipment 3 Requirements 3.1 General 3.1.1 On an adequate chassis, the loader shall provide two platforms: a) a front pl
26、atform capable of operating between 2 100 mm (83 in) and 5 600 mm (221 in), which is positioned at the applicable aircraft door and remains at this position during the loading/unloading operation; b) a main platform for up and down movement between 508 mm (20 in) and 5 600 mm (221 in). 3.1.2 The ove
27、rall dimensions of the loader shall be kept to a minimum. 3.1.3 The overall height of the entire loader should not exceed 3 600 mm (142 in) when being driven. 3.1.4 The loader shall support simultaneously, at their maximum gross mass, two 2 438 mm 3 175 mm (96 in 125 in) ULDs on the main platform an
28、d one 2 438 mm 3 175 mm (96 in 125 in) ULD on the front platform. 3.1.5 When negotiating two ramps that intersect at 3 (5 %), the loader shall have adequate underneath clearance from any portion of the equipment to the ground. 3.1.6 The length of the front platform shall be adequate to accept one 2
29、438 mm 3 175 mm (96 in 125 in) ULD lengthwise. 3.1.7 The length of the main platform shall be adequate to accept two 2 438 mm 3 175 mm (96 in 125 in) ULDs lengthwise on the platform. 3.1.8 The width of both platforms shall be adequate to accept a ULD with its 3 175 mm (125 in) dimension across the p
30、latforms. 3.1.9 The surface of both platforms shall allow for longitudinal and lateral movement of ULDs. BS ISO 6967:200633.1.10 The front platform shall be adjustable to changes in aircraft attitude with an accuracy of a) 2,0 in pitch and roll; b) 6,4 mm (0,25 in) in height. 3.1.11 The front platfo
31、rm shall be designed not to interfere with the opening and closing of the aircraft door. All component parts that may come into contact with the aircraft should be covered with a protective material, e.g. rubber D section (see 7 in the Bibliography). 3.1.12 Safety guard-rails shall be fitted to both
32、 sides of the front platform and have a minimum height of 1 100 mm (43 in). These rails shall be adjustable to close the gap between the loader and the aircraft. 3.1.13 The front platform shall be accessible from the ground at all times. 3.1.14 Platform safety supports for maintenance purposes shall
33、 be provided. 3.1.15 The loaders design shall meet all applicable requirements of ISO 6966-1 and ISO 6966-2. 3.2 Guide rails and stops 3.2.1 Longitudinal (retractable) guide rails shall be provided on the main platform and adjustable on the front platform to the following ULD widths and as indicated
34、 in a) and b): 2 438 mm (96 in) + 25 mm to 50 mm (1 in to 2 in) clearance; 3 175 mm (125 in) + 25 mm to 50 mm (1 in to 2 in) clearance. a) Front platform: guide rails along the whole length of both sides of the platform to accurately guide ULDs into the aircraft. They shall be adjustable laterally t
35、o align with the appropriate in-aircraft guides. b) Main platform: guide rails 3 175 mm (125 in) + 25 mm to 50 mm (1 in to 2 in) clearance apart along the full length of both sides of the platform. The guide rails shall consist of two sections positioned adjacent to the powered sections of the platf
36、orm and shall be able to operate independently. All sections shall automatically extend when the main platform starts moving upward and remain in this position. When the main platform is being lowered and reaches the height of 1 520 mm (60 in) from the ground, it should be possible for the operator
37、to control the retraction of the guide rails. For a unit with ULD rotation capability (see 4.3), the guide rails shall be able to be operated independently and/or simultaneously, and shall automatically arise when the main platform starts moving upward and remain in this position. 3.2.2 Automatic UL
38、D stops shall be provided as follows. a) Front platform: At the end adjacent to the main platform. These stops shall arise at the moment the main platform starts moving down and shall fully retract when the upcoming main platform is level with the front platform. These stops shall remain raised at a
39、ny position other than level with the main platform. b) Main platform: 1) At the forward and aft ends. 2) Side guide rails that function as stops and guide rails. 3.2.3 The stops adjacent to the front platform shall automatically retract as the main platform lines up with the front platform. These s
40、tops shall start rising the moment the main platform starts moving down and remain raised at any position other than level with the front platform. BS ISO 6967:20064 3.2.4 The rear stops and side guide rails shall automatically arise when the platform is raised above 559 mm (22 in) from the ground,
41、and remain raised while the main platform is not aligned with the front platform. 3.2.5 The operating mode of the rear stops and side guide rails shall be selected by the operator. 3.2.6 If the operator selected the end loading mode and the main platform reaches the height of 1 520 mm (60 in) from t
42、he ground when being lowered, it should be possible for the operator to control the retraction of the rear stops by continuous intentional action. When the platform descends below 559 mm (22 in) from the ground, the rear stops shall automatically retract but the side guide rails shall remain in the
43、raised position. 3.2.7 If the operator selected the side loading mode and the main platform reaches the height of 1 520 mm (60 in) from the ground when being lowered, it should be possible for the operator to control the retraction of the side guide rails by continuous intentional action. When the p
44、latform descends below 559 mm (22 in) from the ground, the selected side guide rails shall automatically retract but the rear stops shall remain in the raised position. 3.2.8 All fixed or removable guide rails and retractable stops shall have a minimum height of 100 mm (4 in). Retractable guide rail
45、s shall have a height of not less than 50 mm (2 in). 3.3 Conveyor surface 3.3.1 The loader shall be designed for powered end and side loading of ULDs. On the front platform, the longitudinal and lateral movement shall be effected by means of a powered system. On the main platform, the longitudinal a
46、nd lateral movement shall be effected by means of a powered system. The main platform powered system shall be divided into two sections, each of which will accept one 3 175 mm 2 438 mm (125 in 96 in) ULD longitudinally. It shall be possible to control these sections individually or simultaneously. 3
47、.3.2 The powered system shall be able to drive ULDs at a speed of approximately 0,3 m/s (60 ft/min). 3.3.3 It shall not be possible to transfer loaded ULDs from either platform when the stops are not properly operated. 3.3.4 The platforms conveying surfaces shall meet all applicable requirements of
48、ISO 4116. 3.4 Platform operation and loading 3.4.1 It shall be possible to adjust the position of the ULD in a lateral direction on the front platform. 3.4.2 Platform elevating systems shall be able to hold both platforms at maximum height with full specified continuous lift capacity with no noticea
49、ble height decrease for 30 min, with and without the engine running. 3.4.3 Both the front and main platform elevating mechanisms shall incorporate safety features to prevent sudden collapse in the event of system failure. 3.4.4 The operator shall be able to a) open and close the aircraft door from the front platform; b) simultaneously operate the loader and in-aircraft systems. 3.4.5 The time taken for the main platform to reach maximum height from the lowered position a
