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    SAE ARP 1247D-2010 Aircraft Ground Support Equipment General Requirements《航空器地勤支援设备一般要求》.pdf

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    SAE ARP 1247D-2010 Aircraft Ground Support Equipment General Requirements《航空器地勤支援设备一般要求》.pdf

    1、_SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineering sciences. The use of this report is entirely voluntary, and its applicability and suitability for any particular use, including any patent infringement arising theref

    2、rom, is the sole responsibility of the user.” SAE reviews each technical report at least every five years at which time it may be reaffirmed, revised, or cancelled. SAE invites your written comments and suggestions. Copyright 2010 SAE International All rights reserved. No part of this publication ma

    3、y be reproduced, stored in a retrieval system or transmitted, in any form or by any means, electronic, mechanical, photocopying, recording, or otherwise, without the prior written permission of SAE. TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada) Tel: +1 724-776-4970 (outside US

    4、A) Fax: 724-776-0790 Email: CustomerServicesae.org SAE WEB ADDRESS: http:/www.sae.orgSAE values your input. To provide feedback on this Technical Report, please visit http:/www.sae.org/technical/standards/ARP1247DAEROSPACERECOMMENDEDPRACTICEARP1247 REV. D Issued 1972-04 Revised 2010-07 Superseding A

    5、RP1247C Aircraft Ground Support Equipment General Requirements RATIONALEThis ARP has been revised to define and clarify exsisting requirements, add additional requirements, and to include references to European Standards applicable to GSE manufacturing requirementsTABLE OF CONTENTS 1. SCOPE 32. REFE

    6、RENCES 32.1 Applicable Documents 32.1.1 SAE Publications . 32.1.2 ANSI Publications . 42.1.3 U.S. Government Publications 42.1.4 Other Publications . 53. REQUIREMENTS . 53.1 Performance 53.2 Operability . 53.3 Reliability . 63.4 Maintenance Requirements 63.4.1 Maintainability . 63.4.2 Maintenance Re

    7、pair Cycle 63.4.3 Service and Access 63.5 Total Life . 73.6 Environmental . 73.7 Transportability 83.8 Safety 83.9 Personnel Safety . 83.10 Equipment Safety 103.11 Noise and Vibration . 113.12 Equipment Definition . 113.13 Design and Construction . 123.13.1 General Design Features 123.13.2 Materials

    8、, Parts, and Processes . 243.13.3 Standard and Commercial Parts . 253.13.4 Moisture and Fungus Resistance . 253.13.5 Corrosion of Metal Parts . 253.13.6 Interchangeability and Replaceability . 253.13.7 Workmanship 253.13.8 Electromagnetic Interference 263.13.9 Identification and Marking . 263.13.10

    9、Storage 263.13.11 Exterior Finish . 26SAE ARP1247D Page 2 of 303.13.12 Human Engineering 274. QUALITY ASSURANCE PROVISIONS 274.1 Preliminary Qualification Tests . 274.2 Formal Qualification Tests 274.3 Inspection 274.4 Analyses 274.5 Demonstrations . 284.6 Tests . 284.7 Reliability Test and Analysis

    10、 . 295. INSTRUCTIONS FOR SHIPMENT . 296. DEFINITIONS AND ABBREVIATIONS . 297. DETAILS FOR CONTRACTUAL NEGOTIATIONS 298. NOTES 29SAE ARP1247D Page 3 of 301. SCOPE This SAE Aerospace Recommended Practice (ARP) outlines the basic general design requirements for ground support equipment used in the civi

    11、l air transport industry. It is intended to assist the airlines in standardizing requirements for various configurations of equipment. For procurement of equipment, sections of this document should be specified with due consideration of the functional and environmental requirements of the equipment,

    12、 and to the relative cost of satisfying those requirements. 2. REFERENCES The following publications form a part of this document to the extent specified herein. The latest issue of SAE publications shall apply. The applicable issue of the other publications shall be the issue in effect on the date

    13、of the purchase order. In the event of conflict between the text of this document and references cited herein, the text of this document takes precedence. Nothing in this document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained. 2.1 Applicable Docum

    14、ents 2.1.1 SAE Publications Available from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and canada) or 724-776-4970 (outside USA), www.sae.org. JIO Automotive and Off-Highway Air Brake Reservoir Performance and Identification Requirements Truck

    15、and Bus J377 Vehicular Traffic Sound Signaling Devices (Horns) J512 Automotive Tube Fittings J514 Hydraulic Tube Fittings J517 Hydraulic Hose J524 Seamless Low-Carbon Steel Tubing Annealed for Bending and FlaringJ533 Flares for Tubing J537 Storage Batteries J561 Electrical Terminals Eyelet and Spade

    16、 Type J844 Nonmetallic Air Brake System Tubing J858 Electrical Terminals Blade Type J919 Sound Measurement Off-Road Work Machines Operator Singular Type J928 Electrical Terminals Pin and Receptacle Type J1127 Low Voltage Battery Cable J1128 Low Voltage Primary Cable J1401 Road Vehicle Hydraulic Brak

    17、e Hose Assemblies for Use With Nonpetroleum-Base Hydraulic Fluids J1402 Automotive Air Brake Hose and Hose Assemblies J1403 Vacuum Brake Hose SAE ARP1247D Page 4 of 302.1.1 (Continued) J1703 Motor Vehicle Brake Fluid J2031 High Tension Ignition Cable ARP836 Design and Safety Criteria for Passenger B

    18、oarding Stairways ARP1052 Selection Criteria for Internal Combustion Engines Used in Ground Support Equipment ARP1328 Aircraft Ground Support Equipment - Wind Stability Determination ARP1330 Welding of Structures for Ground Support Equipment AIR1336 Vehicle Electric Systems AIR1375 Minimum Safety Re

    19、quirements for Special Purpose Airline Ground Support EquipmentAIR 1558 AircraftInterface Protective Devices ARP1801 Measurement of Exterior Sound Level of Specialized Aircraft Ground Support Equipment 2.1.2 ANSI Publications Available from American National Standards Institute, 25 West 42ndStreet,

    20、New York, NY 10036-8002, Tel: 212-642-4900, www.ansi.org. ANSI B56.1 Safety Standard for Powered Industrial Trucks ANSI A92.7 Airline Ground Support Vehicle Mounted Vertical Lift Devices 2.1.3 U.S. Government Publications Available from Document Automation and Production Service (DAPS), Building 4D,

    21、 700 Robbins Avenue, Philadelphia, PA 19111-5094, Tel: 215-697-6257, http:/assist.daps.dla.mil/quicksearch/.MIL-STD-461 Electromagnetic Interference Characteristics Requirements for Equipment MIL-STD-1472 Human Engineering Design Criteria for Military Systems, Equipment, and Facilities MlL-DTL-3950

    22、Switch, Toggle, General Specification for A-A-870 Antifreeze, Ethylene Glycol, Inhibited Various Standards United States Public Health Service Standards Code of Federal Regulations- Title 29, Part 1910 - 0ccupational Safety and Health Standards (OSHA) - Title 49, Part 393 - Parts and Accessories Nec

    23、essary for Safe Operation - Title 49, Part 571 - Federal Motor Vehicle Safety Standards (FMVSS) SAE ARP1247D Page 5 of 302.1.4 Other Publications American Welding Society Applicable chapters/sections of welding codes Section VIII ASME Unfired Pressure Vessel CodeATA Spec. 101 Specification for Groun

    24、d Equipment Technical Data E.U. Machinery Directive NOTE: For intended GSE operation in Europe, EU Machinery Directive (Directive 2006/42/EC of 17 May 2006) requirements apply. They can be met by complying with the general requirements of the EN 1915 Parts as well as requirements specific to each GS

    25、E type covered by EN 12312-1 to -20 standards. ISO 6966-1 and 6966-2 provide general requirements common to ARP 1247D and the ENs for worldwide application. However, they are not sufficient to ensure compliance with the E.U. Machinery Directive.a) EN 1915-1:2001 Aircraft ground support equipment Gen

    26、eral requirements Part 1: Basic safety requirements b) EN 1915-2:2001 Aircraft ground support equipment General requirements Part 2: Stability and strength requirements, calculations and test methods c) EN 1915-3:2004 Aircraft ground support equipment - General requirements - Vibration measurement m

    27、ethods and reductiond) EN 1915-4:2005 Aircraft ground support equipment General requirements - Part 4: Noise measurement methods and reduction e) ISO 6966-1:2005 Aircraft ground equipment Basic requirements Part 1: General requirements f) 6966-2:2005 Aircraft ground equipment Basic requirements Part

    28、 2: Safety requirements g) EU Low Voltage Directive - LV 72/23/EEC NFPA No. 70 National Fire Prevention Association Standard No. 70, “National Electric Code“NFPA No. 505 Standard for the Use, Maintenance and Operation of Industrial Trucks. Fire Safety for Powered Industrial TrucksVarious Standards C

    29、aster i.e., major component overhaul or removal, may be designed to be removed from the equipment when hinging or pinning is not practical.3.4.3.5 All hinged doors shall be provided with devices to secure them in the open and closed positions such that they will not be blown by jet blast or ambient

    30、winds. Stops or bumpers shall be installed so that the doors (or stops), do not mark or scratch the paint work. Where possible, at least 8 inches (203 mm) of clearance above the ground shall exist when any door is open. 3.4.3.6 Major assemblies and components shall be capable of being disconnected a

    31、nd removed from the equipment without the necessity for extensive disassembly of other components. Standard automotive practice is acceptable.3.4.3.7 Parts requiring removal for replacement, service, or maintenance shall be fastened with removable fasteners or latching devices. 3.4.3.8 Weight of rem

    32、ovable enclosures, or replaceable units, designed for one-man handling must be less than 30 pound (14 kg). Units exceeding 30 pound (14 kg) to a maximum of 80 pound (36 kg) must be designed for two-man handling.SAE ARP1247D Page 7 of 303.4.3.9 All components that exceed 80 pound (36 kg), or that exc

    33、eed 30 pound (14 kg) if only one man has access to the unit for handling, shall have provisions for attaching lifting or handling devices such as slings, hoists, or forklift tines. The minimum design safety factor of such provisions, based on the ultimate strength of the material shall be 5 to 1.3.4

    34、.3.10 Any vital, unattached parts such as tractor hitch pins and lock pins which might otherwise be easily lost shall be secured to the equipment with cable or chain of durable size and material. 3.4.3.11 Pressure lubrication fittings shall be provided at all points where heavy loads, close toleranc

    35、e, relative rotary or linear motion of parts occurs. This will normally include pivots, guides, bearings, and journals except sealed ball and roller bearings. Where access to the fittings is difficult, they shall be brought to a common lubrication panel. 3.4.3.12 Fastener heads and nuts shall be pro

    36、vided with adequate clearance for wrenches and drivers. 3.4.3.13 A means of positively securing lift devices at a convenient height for service and access shall be provided with each unit. 3.4.3.14 On lift types of equipment, the manufacturer shall provide alternate means of raising the hoist in eve

    37、nt of failure of the primary power source if any components that could cause failure are not accessible while the hoist is in the down position. 3.4.3.15 On lift bed types of equipment a means shall be provided for a mechanic to raise and lower the hoist while working at ground level. 3.4.3.16 Chain

    38、 and belt drives shall have provisions for adjusting the tension to the manufacturers specified value. A positive means to hold the adjustment shall be provided. 3.5 Total Life “Total Life“ is defined to be the hours of use from time of delivery of the equipment to the using activity until its ident

    39、ity isdestroyed by classifying it as salvage and/or subject to cannibalization. The “Total Life“ for which the equipment is designed, assuming it is used and maintained in accordance with the manufacturers recommendation, shall be specified. 3.6 Environmental 3.6.1 The entire unit shall be designed

    40、and equipped to start easily and operate satisfactorily under temperature conditions ranging from -20 to +123 F (-29 to +52 C) after soaking at either of the stated temperature extremes for 24 h. For vehicles to be routinely operated at higher and/or lower temperatures, applicable operating temperat

    41、ure limits should be specified in the procurement document. 3.6.2 The equipment shall be designed to operate satisfactorily after exposure to the following sequence of conditionsa. 4 hours soak at +20 F (-6.7 C) b. Thorough wetting of the exterior of the equipment with a fine spray of +40 F (4.4 C)

    42、water c. 4 hours soak at +20 F (-6.7 C) 3.6.3 The equipment and all its components shall be designed to operate satisfactorily after 6 hours exposure to heavy rainfall (0.30 in/h) (0.76 cm/h) driven by a 25 mph (4002 km/h) wind in any horizontal direction. 3.6.4 Components shall be protected from me

    43、chanical, electrical, and corrosion damage and impairment of operation due to rain, snow, ice, sand, grit, and deicing fluids. 3.6.5 Operators compartments shall be designed to preclude excessive temperature from heat sources such as engine and exhaust system. Insulation and ventilation shall be pro

    44、vided, if necessary, to limit compartment temperatures in any operational mode, to a maximum of 100 F (37.8 C) on a calm, 85 F (29.4 C), full sunlight day. SAE ARP1247D Page 8 of 303.7 Transportability 3.7.1 The unit shall be designed for over-the-road unrestricted transportation insofar as possible

    45、. The manufacturer shall identify any constraints applicable to transportation or shipment of the unit or any subassemblies. 3.7.2 Units required, as outlined in the controlling specification, to operate on public highways or to be capable of being licensed for use on public highways shall meet the

    46、requirements of Chapter V National Highway Safety Bureau, Department of Transportation, Title 49 of the Code Federal Regulations in effect on the date of manufacture. The unit shall be manufactured in a manner and equipped to be capable of operation in accordance with Part 393, subparts A, B, C, D,

    47、E, and G of Chapter III Federal Highway Administration, Department of Transportation, Title 49 of the Code of Federal Regulations. 3.7.3 Units which may be licensed to operate on public highways shall have the minimum capability to accelerate on a level surface, from 0 to 40 mph (0 to 64.4 km/h) wit

    48、hin 60 s with full payload. 3.8 Safety 3.8.1 It shall be the responsibility of the manufacturer to ensure that the equipment contains all the safety features required to protect the equipment, the operator(s), the load, and the aircraft serviced, in accordance with AIR1375 - Minimum Safety Requirements for Special Purpose Airline Ground Support Equipment, and Title 29 CFR Part 1910 - 0ccupational Safety and Health Standards (OSHA). 3.8.2 Powered Industrial Trucks (as de


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