SAE ARP5497A
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.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
Hardcopy , PDF
21-10-2019
English
06-02-2018
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Withdrawn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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