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SAE ARP5497A

Withdrawn

Withdrawn

A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.

Modification or Replacement of Components on Dynamically Certified Seat Systems

Available format(s)

Hardcopy , PDF

Withdrawn date

21-10-2019

Language(s)

English

Published date

06-02-2018

€108.76
Excluding VAT

FOREWORD
1. SCOPE
2. REFERENCES
3. PRIMARY COMPONENT EVALUATION
4. SECONDARY COMPONENT EVALUATION
5. ANCILLARY COMPONENT EVALUATION
6. FLOWCHART FOR EVALUATION OF POTENTIAL
   MODIFICATION

Gives engineering evaluation appropriate for modifying or replacing components of a previously certified seat when the certification process is based on qualification to the requirements of AS8049, which includes dynamic testing.

DocumentType
Standard
Pages
14
PublisherName
SAE International
Status
Withdrawn
Supersedes

This document outlines the engineering evaluation appropriate for modifying or replacing components of a previously certified seat when the certification process is based on qualification to the requirements of AS8049, which includes dynamic testing. The engineering evaluation presented in this document may be used to determine if a modification (including replacement of a component) is a minor change with respect to meeting the dynamic testing requirements described in AS8049.Whenever a modification is considered, the ability to meet all requirements of the applicable Federal Aviation Regulation (FAR) must be verified. For example, this would include the capability to meet requirements such as flammability and flotation. Analysis and/or test data supporting the ability of the new materials and/or configuration to meet the applicable requirements must be submitted with the change documentation.This document addresses the evaluation of seat pan cushions, secondary components, and ancillary components. Other primary components such as restraint systems and primary structural components are not considered.

FAA AC 20-137 : 0 DYNAMIC EVALUATION OF SEAT RESTRAINT SYSTEMS & OCCUPANT RESTRAINT FOR ROTORCRAFT (NORMAL AND TRANSPORT)
SAE AS8049C Performance Standard for Seats in Civil Rotorcraft, Transport Aircraft, and General Aviation Aircraft
FAA AC 23.562-1 : 0 DYNAMIC TESTING OF PART 23 AIRPLANE SEAT/RESTRAINT SYSTEMS AND OCCUPANT PROTECTION
FAA 8150.1 : 2017 TECHNICAL STANDARD ORDER PROGRAM
FAA AC 25.562-1 : 2006 DYNAMIC EVALUATION OF SEAT RESTRAINT SYSTEMS AND OCCUPANT PROTECTION ON TRANSPORT AIRPLANES
FAA AC 21-25 : 2016 APPROVAL OF MODIFIED SEATING SYSTEMS INITIALLY APPROVED UNDER A TECHNICAL STANDARD ORDER
FAA AC 25-17 : 2009 TRANSPORT AIRPLANE CABIN INTERIORS CRASHWORTHINESS HANDBOOK

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