Special Conditions: Flight Structures, Inc., Boeing Model 777-200 Dynamic Test Requirements for Single-Occupant, Oblique (Side-Facing) Seats With Airbag Devices, 72561 [2015-29624]
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Federal Register / Vol. 80, No. 224 / Friday, November 20, 2015 / Rules and Regulations
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 SingleOccupant, Oblique (Side-Facing) Seats
With Airbag Devices
Federal Aviation
Administration (FAA), DOT.
ACTION: Final special conditions; request
for comments; correction.
AGENCY:
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 singleoccupant, 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.
SUMMARY:
tkelley on DSK3SPTVN1PROD with RULES
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:
VerDate Sep<11>2014
17:28 Nov 19, 2015
Jkt 238001
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
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Parts 33 and 35
[Docket No. FAA–2015–4220; Special
Conditions No. 33–017–SC]
Special Conditions: CFM International,
LEAP–1B Engine Models;
Incorporation of Woven Composite
Fan Blades
Federal Aviation
Administration (FAA), DOT.
ACTION: Final special conditions; request
for comments.
AGENCY:
These special conditions are
issued for the CFM International (CFM),
LEAP–1B engine models. This engine
model will have a novel or unusual
design feature associated with the
engine: woven composite fan blades.
The applicable airworthiness
regulations do not contain adequate or
appropriate safety standards for this
design feature. These special conditions
contain the additional safety standards
that the Administrator considers
necessary to establish a level of safety
equivalent to that established by the
existing airworthiness standards.
DATES: The effective date of these
special conditions is December 21,
2015.
We must receive your comments by
December 7, 2015.
ADDRESSES: Send comments identified
by docket number FAA–2015–4220
using any of the following methods:
• Federal eRegulations Portal: Go to
https://www.regulations.gov and follow
the online instructions for sending your
comments electronically.
• Mail: Send comments to Docket
Operations, M–30, U.S. Department of
Transportation (DOT), 1200 New Jersey
Avenue SE., Room W12–140, West
SUMMARY:
PO 00000
Frm 00007
Fmt 4700
Sfmt 4700
72561
Building Ground Floor, Washington,
DC, 20590–0001.
• Hand Delivery or Courier: Take
comments to Docket Operations in
Room W12–140 of the West Building
Ground Floor at 1200 New Jersey
Avenue SE., Washington, DC, between 9
a.m. and 5 p.m., Monday through
Friday, except federal holidays.
• Fax: Fax comments to Docket
Operations at 202–493–2251.
Privacy: The FAA will post all
comments it receives, without change,
to https://www.regulations.gov, including
any personal information the
commenter provides. Using the search
function of the docket Web site, anyone
can find and read the electronic form of
all comments received into any FAA
docket, including the name of the
individual sending the comment (or
signing the comment for an association,
business, labor union, etc.). DOT’s
complete Privacy Act Statement can be
found in the Federal Register published
on April 11, 2000 (65 FR 19477–19478),
as well as at https://DocketsInfo.dot.gov.
Docket: Background documents or
comments received may be read at
https://www.regulations.gov at any time.
Follow the online instructions for
accessing the docket or go to the Docket
Operations in Room W12–140 of the
West Building Ground Floor at 1200
New Jersey Avenue SE., Washington,
DC, between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
FOR FURTHER INFORMATION CONTACT:
Alan Strom, Federal Aviation
Administration Engine and Propeller
Directorate, Aircraft Certification
Service, ANE–112, 12 New England
Executive Park, Burlington,
Massachusetts, 01803–5213; telephone
(781) 238–7143; fax (781) 238–7199;
email alan.strom@faa.gov.
SUPPLEMENTARY INFORMATION:
Comment History
The FAA has determined, in
accordance with 5 U.S.C. 553(b)(3)(B)
and 553(d)(3), that notice and
opportunity for prior public comment
heron are unnecessary because the
substance of these special conditions
was subject to the public comment
process in a prior instance, with no
substantive comments received. The
FAA therefore finds that good cause
exists for making these special
conditions effective upon issuance.
Special condition No.
33–14–02–SC ...........
E:\FR\FM\20NOR1.SGM
20NOR1
Company/Airplane
model
CFM/LEAP–1A
CFM/LEAP–1C
]]>Agencies
[Federal Register Volume 80, Number 224 (Friday, November 20, 2015)]
[Rules and Regulations]
[Page 72561]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2015-29624]
[[Page 72561]]
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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
