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Aircraft Seat Design Guidance and Clarifications
- Aerospace Standard
- ARP5526C
- Revised
Downloadable datasets available
Annotation ability available
Sector:
Issuing Committee:
Language:
English
Scope
This Aerospace Recommended Practice (ARP) documents a common understanding of terms, compliance issues and design criteria to facilitate certification of seat installations specific to Part 25 aircraft. This ARP provides general guidance for seats to be installed in Part 23 aircraft and Parts 27 and 29 rotorcraft and does not specify specific designs or design methods for such certification.
Rationale
The change in this revision represent the latest agreement obtained by the SAE SEAT Committee to integrate the new paragraph ยง3.18 Electrically Actuation Feature.
Recommended Content
Topic
Data Sets - Support Documents
Title | Description | Download |
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TABLE 2 | MAXIMUM FORCE VALUES | |
TABLE 3 | HAZARD LEVEL EVALUATION | |
TABLE 4 | EXAMPLES OF HAZARD MODIFYING FACTOR VALUES | |
TABLE 5 | HAZARD VALUE AND RECOMMENDED ACTIONS | |
TABLE 6 | CAESAR ANTHROPOMETRIC DATABASE SITTING AND STANDING HEIGHT | |
TABLE B1 | SEAT SECONDARY STRUCTURE HANDLING AND SERVICE LOADS | |
TABLE B2 | SEAT SECONDARY STRUCTURE FATIGUE LIFE |
Issuing Committee
The Aerospace Council of SAE established the Aircraft Seat Committee (SEAT) in 1997 to address technical issues related to the design and/or performance of aircraft seating systems. The seating systems include crew, flight attendants, and passenger seats installed in Civil Rotorcraft, Transport Aircraft, and General Aviation Aircraft.
A list of the technical reports developed by the SEAT Committee can be obtained by searching on 'aircraft seat' and selecting 'standards', from the SAE Home Page. SEAT StandardsReference
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