Special Conditions: Flight Structures, Inc., Boeing Model 777-200 Dynamic Test Requirements for Single-Occupant, Oblique (Side-Facing) Seats With Airbag Devices

AGENCY:

Federal Aviation Administration (FAA), DOT.

ACTION:

Final special conditions; request for comments; correction.

SUMMARY:

This document corrects an error that appeared in Docket No. FAA-2015-3367, Special Conditions No. 25-596-SC, which was published in the Federal Register on September 30, 2015 (80 FR 58597). The error is in a reference to Boeing in a note preceding a section titled, Inflatable Lap Belt Special Conditions. It is being corrected herein.

DATES:

The effective date of this correction is November 20, 2015.

FOR FURTHER INFORMATION CONTACT:

John Shelden, FAA, Airframe and Cabin Safety Branch, ANM-115, Transport Airplane Directorate, Aircraft Certification Service, 1601 Lind Avenue SW., Renton, Washington 98057-3356; telephone 425-227-2785; facsimile 425-227-1149.

SUPPLEMENTARY INFORMATION:

The document designated as “Docket No. FAA-2015-3367, Special Conditions No. 25-596-SC” was published in the Federal Register on September 30, 2015 (80 FR 58597). The document issued special conditions pertaining to dynamic test requirements for single-occupant, oblique (side-facing) seats with airbag devices on Boeing Model 777-200 airplanes.

As published, the document contained one error in a note that refers to Boeing rather than Flight Structures, Inc.

Because no other part of the regulatory information has been changed, the Special Conditions are not being re-published.

Correction

In the Final Special Conditions, Request for Comments document [FR Doc. 2015-24727 filed 9-29-15; 8:45 a.m.] published on September 30, 2015 (80 FR 58597), make the following correction:

On page 58599, column 3, the paragraph marked “Note:” should read:

Note:

Flight Structures, Inc., must demonstrate that the installation of seats via plinths or pallets meets all applicable requirements. Compliance with the guidance contained in FAA Policy Memorandum PS-ANM-100-2000-00123, dated February 2, 2000, titled “Guidance for Demonstrating Compliance with Seat Dynamic Testing for Plinths and Pallets,” is acceptable to the FAA.