80 FR 72561 - Special Conditions: Flight Structures, Inc., Boeing Model 777-200 Dynamic Test Requirements for Single-Occupant, Oblique (Side-Facing) Seats With Airbag Devices
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 80, Issue 224 (November 20, 2015)
Federal Aviation Administration
Federal Register Volume 80, Issue 224 (November 20, 2015)
| Page Range | 72561-72561 | |
| FR Document | 2015-29624 |
[Federal Register Volume 80, Number 224 (Friday, November 20, 2015)] [Rules and Regulations] [Page 72561] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2015-29624] [[Page 72561]] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 25 [Docket No. FAA-2015-3367; Special Conditions No. 25-596-SC] 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. Issued in Renton, Washington, on November 11, 2015. Michael Kaszycki, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2015-29624 Filed 11-19-15; 8:45 am] BILLING CODE 4910-13-P
![Federal Register / Vol. 80, No. 224 / Friday, November 20, 2015 / Rules and Regulations 72561
DEPARTMENT OF TRANSPORTATION Note: Flight Structures, Inc., must Building Ground Floor, Washington,
demonstrate that the installation of seats via DC, 20590–0001.
plinths or pallets meets all applicable
Federal Aviation Administration • Hand Delivery or Courier: Take
requirements. Compliance with the guidance
contained in FAA Policy Memorandum PS– comments to Docket Operations in
14 CFR Part 25 Room W12–140 of the West Building
ANM–100–2000–00123, dated February 2,
[Docket No. FAA–2015–3367; Special 2000, titled ‘‘Guidance for Demonstrating Ground Floor at 1200 New Jersey
Conditions No. 25–596–SC] Compliance with Seat Dynamic Testing for Avenue SE., Washington, DC, between 9
Plinths and Pallets,’’ is acceptable to the a.m. and 5 p.m., Monday through
Special Conditions: Flight Structures, FAA. Friday, except federal holidays.
Inc., Boeing Model 777–200 Dynamic
Issued in Renton, Washington, on
• Fax: Fax comments to Docket
Test Requirements for Single- November 11, 2015. Operations at 202–493–2251.
Occupant, Oblique (Side-Facing) Seats Privacy: The FAA will post all
Michael Kaszycki,
With Airbag Devices comments it receives, without change,
Acting Manager, Transport Airplane
AGENCY: Federal Aviation Directorate, Aircraft Certification Service. to http://www.regulations.gov, including
Administration (FAA), DOT. [FR Doc. 2015–29624 Filed 11–19–15; 8:45 am]
any personal information the
commenter provides. Using the search
ACTION: Final special conditions; request BILLING CODE 4910–13–P
function of the docket Web site, anyone
for comments; correction. can find and read the electronic form of
SUMMARY: This document corrects an DEPARTMENT OF TRANSPORTATION all comments received into any FAA
error that appeared in Docket No. FAA– docket, including the name of the
2015–3367, Special Conditions No. 25– Federal Aviation Administration individual sending the comment (or
596–SC, which was published in the signing the comment for an association,
Federal Register on September 30, 2015 14 CFR Parts 33 and 35 business, labor union, etc.). DOT’s
(80 FR 58597). The error is in a complete Privacy Act Statement can be
reference to Boeing in a note preceding [Docket No. FAA–2015–4220; Special found in the Federal Register published
a section titled, Inflatable Lap Belt Conditions No. 33–017–SC] on April 11, 2000 (65 FR 19477–19478),
Special Conditions. It is being corrected as well as at http://DocketsInfo.dot.gov.
herein. Special Conditions: CFM International, Docket: Background documents or
LEAP–1B Engine Models; comments received may be read at
DATES: The effective date of this Incorporation of Woven Composite
correction is November 20, 2015. http://www.regulations.gov at any time.
Fan Blades Follow the online instructions for
FOR FURTHER INFORMATION CONTACT: John
AGENCY: Federal Aviation accessing the docket or go to the Docket
Shelden, FAA, Airframe and Cabin
Administration (FAA), DOT. Operations in Room W12–140 of the
Safety Branch, ANM–115, Transport
West Building Ground Floor at 1200
Airplane Directorate, Aircraft ACTION: Final special conditions; request
New Jersey Avenue SE., Washington,
Certification Service, 1601 Lind Avenue for comments.
DC, between 9 a.m. and 5 p.m., Monday
SW., Renton, Washington 98057–3356;
SUMMARY: These special conditions are through Friday, except Federal holidays.
telephone 425–227–2785; facsimile
425–227–1149. issued for the CFM International (CFM), FOR FURTHER INFORMATION CONTACT:
LEAP–1B engine models. This engine Alan Strom, Federal Aviation
SUPPLEMENTARY INFORMATION: The
model will have a novel or unusual Administration Engine and Propeller
document designated as ‘‘Docket No.
design feature associated with the Directorate, Aircraft Certification
FAA–2015–3367, Special Conditions
engine: woven composite fan blades. Service, ANE–112, 12 New England
No. 25–596–SC’’ was published in the
The applicable airworthiness Executive Park, Burlington,
Federal Register on September 30, 2015
regulations do not contain adequate or Massachusetts, 01803–5213; telephone
(80 FR 58597). The document issued
appropriate safety standards for this (781) 238–7143; fax (781) 238–7199;
special conditions pertaining to
design feature. These special conditions email alan.strom@faa.gov.
dynamic test requirements for single-
contain the additional safety standards SUPPLEMENTARY INFORMATION:
occupant, oblique (side-facing) seats
that the Administrator considers
with airbag devices on Boeing Model Comment History
necessary to establish a level of safety
777–200 airplanes.
equivalent to that established by the
As published, the document The FAA has determined, in
existing airworthiness standards.
contained one error in a note that refers accordance with 5 U.S.C. 553(b)(3)(B)
to Boeing rather than Flight Structures, DATES: The effective date of these and 553(d)(3), that notice and
Inc. special conditions is December 21, opportunity for prior public comment
Because no other part of the 2015. heron are unnecessary because the
regulatory information has been We must receive your comments by substance of these special conditions
changed, the Special Conditions are not December 7, 2015. was subject to the public comment
being re-published. ADDRESSES: Send comments identified process in a prior instance, with no
by docket number FAA–2015–4220 substantive comments received. The
Correction using any of the following methods: FAA therefore finds that good cause
In the Final Special Conditions, • Federal eRegulations Portal: Go to exists for making these special
Request for Comments document [FR http://www.regulations.gov and follow conditions effective upon issuance.
tkelley on DSK3SPTVN1PROD with RULES
Doc. 2015–24727 filed 9–29–15; 8:45 the online instructions for sending your
a.m.] published on September 30, 2015 comments electronically. Special condition No. Company/Airplane
(80 FR 58597), make the following • Mail: Send comments to Docket model
correction: Operations, M–30, U.S. Department of
33–14–02–SC ........... CFM/LEAP–1A
On page 58599, column 3, the Transportation (DOT), 1200 New Jersey CFM/LEAP–1C
paragraph marked ‘‘Note:’’ should read: Avenue SE., Room W12–140, West
VerDate Sep<11>2014 17:28 Nov 19, 2015 Jkt 238001 PO 00000 Frm 00007 Fmt 4700 Sfmt 4700 E:\FR\FM\20NOR1.SGM 20NOR1](https://thefederalregister.org/doc/80_FR_72785/page/1.svg)
Document Created: 2015-12-14 13:58:32
Document Modified: 2015-12-14 13:58:32
| Category | Regulatory Information | |
| Collection | Federal Register | |
| sudoc Class | AE 2.7: GS 4.107: AE 2.106: | |
| Publisher | Office of the Federal Register, National Archives and Records Administration | |
| Section | Rules and Regulations | |
| Action | Final special conditions; request for comments; correction. | |
| Dates | The effective date of this correction is November 20, 2015. | |
| 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. | |
| FR Citation | 80 FR 72561 |
2025 Federal Register | Disclaimer | Privacy Policy
USC | CFR | eCFR