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SAE AS8049 Rev D

Current Revision

Performance Standard for Seats in Civil Rotorcraft, Transport Aircraft, and General Aviation Aircraft

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This SAE Aerospace Standard (AS) defines minimum performance standards, qualification requirements, and minimum documentation requirements for passenger and crew seats in civil rotorcraft, transport aircraft, and general aviation aircraft. The goal is to achieve comfort, durability, and occupant protection under normal operational loads and to define test and evaluation criteria to demonstrate occupant protection when a seat/occupant/restraint system is subjected to statically applied ultimate loads and to dynamic impact test conditions set forth in Title 14, Code of Federal Regulations (14 CFR) parts 23, 25, 27, or 29 (as applicable to the seat type, see Table 1 ). Guidance for test procedures, measurements, equipment, and interpretation of results is also presented to promote uniform techniques and to achieve acceptable data. While this document addresses system performance, responsibility for the seating system is divided between the seat supplier and the installation applicant. The seat supplier's responsibility consists of meeting all the seat system performance requirements and obtaining and supplying to the installation applicant all the data prescribed by this document. The installation applicant has the ultimate system responsibility in assuring that all requirements for safe seat installation have been met.

SDO SAE: SAE International
Document Number AS8049
Publication Date Nov. 2, 2020
Language en - English
Page Count 71
Revision Level D
Supercedes
Committee
Publish Date Document Id Type View
Nov. 2, 2020 AS8049D Revision
Aug. 14, 2015 AS8049C Revision
Jan. 25, 2005 AS8049B Revision
Sept. 1, 1997 AS8049A Revision
July 1, 1990 AS8049 Revision