SAE ARP 6199-2012 Method to Evaluate Aircraft Passenger Seats for the Test Requirements of 14CFR Part 25 Appendix F Parts IV & V《14CFR 第25部分附录F 第IV & V部分的飞机乘客座椅的评价方法用试验方法》.pdf
《SAE ARP 6199-2012 Method to Evaluate Aircraft Passenger Seats for the Test Requirements of 14CFR Part 25 Appendix F Parts IV & V《14CFR 第25部分附录F 第IV & V部分的飞机乘客座椅的评价方法用试验方法》.pdf》由会员分享,可在线阅读,更多相关《SAE ARP 6199-2012 Method to Evaluate Aircraft Passenger Seats for the Test Requirements of 14CFR Part 25 Appendix F Parts IV & V《14CFR 第25部分附录F 第IV & V部分的飞机乘客座椅的评价方法用试验方法》.pdf(30页珍藏版)》请在麦多课文档分享上搜索。
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 revised, reaffirmed, stabilized, or cancelled. SAE invites your written comments and suggestions.Copyright 2012 SAE International All rights reserved. No part of this pub
3、lication may 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
4、(outside USA) 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/ARP6199AEROSPACERECOMMENDEDPRACTICEARP6199 Issued 2012-06 Method to Evaluate Aircraf
5、t Passenger Seats for the Test Requirements of 14CFR Part 25 Appendix F, Parts IV o Items occurring more than once per seat place that have an exposed surface area less than 9 in2(58 cm2) and are at least 12 in (30 cm) apart from each other. NOTE: The above criteria apply to both exposed parts and s
6、mall parts mounted on, or butted up against (with no gap), the unexposed side of exposed panels (see Figure 4). FIGURE 4 - EXAMPLE OF EXPOSED AND UNEXPOSED SMALL PARTS ATTACHED TO A SINGLE PANEL Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networ
7、king permitted without license from IHS-,-,-SAE ARP6199 Page 11 of 30 5.4 Panel Versus Not a Panel A panel is defined as the surface of single or multiple components that may be attached to or be integral to seat structure. Non-metallic seat structure such as shown in Figure 5 is not a panel. FIGURE
8、 5 - EXAMPLES OF NON-METALLIC SEAT STRUCTURE THAT ARE NOT PANELS NOTE: Seat backs, cushions, and seat pans are not addressed by this definition and are addressed separately in this document. This document applies only to metallic structure being replaced by non-metallic components. Fabric (woven or
9、non-woven) or leather coverings are not panels. Construction features of the dress cover materials such as local reinforcement, stitching, surging and welting, are also not panels. Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted
10、 without license from IHS-,-,-SAE ARP6199 Page 12 of 30 5.5 Traditional Versus Non-Traditional 5.5.1 Flight Attendant Seats All flight attendant seats current at the time of initial publication of this document are traditional and do not require evaluation using 14CFR Part 25 Appendix F, Parts IV &
11、V. Flight attendant seats may be a single entity or several assemblies that are separately installed to perform their function (e.g., a wall mounted head rest). Attributes common to traditional flight attendant seats may include but are not limited to: o Standalone (track or floor mounted) or wall m
12、ounted seatso Seats that are sized for their function and locationo Have stowage for emergency equipment (e.g., lifevest, flashlight, handset, smoke hood, PBE, fire extinguisher) o May include miscellaneous stowage Non-traditional flight attendant seats: o Possess a total surface area greater than 2
13、3 ft2(2.14 m2) of exposed non-metallic material. Features covered by a cushion that meets the requirements of 14CFR Part 25 Appendix F, Part II are unexposed. o Are larger than necessary and not located to serve their intended function o Functional design is blended with other interior appliances an
14、d the seat functions as more than a place for an attendant to sit and/or store essential equipment related to their duties (e.g., clothing closet, etc.)o Size of seat is driven by decorative requirementsFIGURE 6 - EXAMPLE OF TRADITIONAL FLIGHT ATTENDANT SEAT HIGH COMFORT SEAT SHOWNFIGURE 7 - EXAMPLE
15、 OF TRADITIONAL FLIGHT ATTENDANT SEAT STANDARD SEAT SHOWN Copyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE ARP6199 Page 13 of 30 5.5.2 Headrests Controlled cushion and structure supporting the pas
16、senger head can be evaluated in the TTL position. If uncontrolled, then evaluation in all positions is necessary. All exposed non-metallic structure and shrouds must be evaluated for 14CFR Part 25 Appendix F, Parts IV & V. Features covered by a cushion that meets the requirements of 14CFR Part 25 Ap
17、pendix F, Part II are unexposed.“Controlled” is defined as a means (e.g., placard, crew instruction) to ensure the headrest is in a specific position for TTL.NOTE: Headrest “ears” must be evaluated in all conditions unless also “controlled”. FIGURE 8 - EXAMPLE OF HEADREST SHROUD FOR EVALUATION 5.5.3
18、 Privacy Dividers Privacy dividers are non-traditional and evaluated in their TTL position. FIGURE 9 - EXAMPLE OF PRIVACY DIVIDERPrivacy Divider HeadrestshroudCopyright SAE International Provided by IHS under license with SAENot for ResaleNo reproduction or networking permitted without license from
19、IHS-,-,-SAE ARP6199 Page 14 of 30 5.5.4 Center Console A calculation of the orthogonally projected area of the center console is used to determine if it is traditional or non-traditional. Alternatively, other more detailed computational methods may be used to calculate the actual surface area of the
20、 exposed surfaces. The purpose of this calculation is to determine the overall size of the feature by surface area without respect to the materials used or the position of the seat cushions. The surface area is calculated using the sum of the projected areas on all sides of the item.Traditional cent
21、er consoles have a surface area of 1008 in2(6503 cm2) or less. Non-traditional consoles have a surface area greater than 1008 in2(6503 cm2) excluding traditional features mounted on the console described in this document.FIGURE 10 - CENTER CONSOLE AREA CALCULATIONIf the bottom of the center console
22、is within 1 inch of the floor, it does not need to be included in the area calculation. If it is greater than 1 inch from the floor, then it should be included in the area calculation. Include aft side ofconsole in calculation Projected area Copyright SAE International Provided by IHS under license
23、with SAENot for ResaleNo reproduction or networking permitted without license from IHS-,-,-SAE ARP6199 Page 15 of 30 5.5.5 Seat End Closeouts (typically used on Economy Class Seats) A calculation of the orthogonally projected area of the item is used to determine if it is traditional or non-traditio
24、nal. Alternatively, other more detailed computational methods may be used to calculate the actual surface area of the non-metallic exposed surfaces.The purpose of this calculation is to determine the overall size of the feature by surface area without respect to the materials used or the position of
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