Fuel Tank Vent Fire Protection; Correction, 48693-48694 [2016-17590]
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Federal Register / Vol. 81, No. 143 / Tuesday, July 26, 2016 / Rules and Regulations
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conduct contained in § 2635.101(b).
DEPARTMENT OF TRANSPORTATION
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time that he files the notification statement
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employee has complied with the notification
requirement of section 17 of the STOCK Act.
14 CFR Parts 25, 121, and 129
Federal Aviation Administration
rmajette on DSK2TPTVN1PROD with RULES
(d) Agreement of future employment
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among other things, an arrangement to
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termination of Government service.
[FR Doc. 2016–17553 Filed 7–25–16; 8:45 am]
BILLING CODE 6345–03–P
VerDate Sep<11>2014
13:45 Jul 25, 2016
[Docket No.: FAA–2014–0500; Amdt. Nos.
25–143, 121–375, and 129–52]
RIN 2120–AK30
Fuel Tank Vent Fire Protection;
Correction
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule; correction.
AGENCY:
The FAA is correcting a final
rule published in the Federal Register
on June 24, 2016 (81 FR 41200). In that
final rule, the FAA amended certain
airworthiness regulations for transport
category airplanes to require fuel tank
designs that prevent a fuel tank
explosion caused by the propagation of
flames, from external fires, through the
fuel tank vents. The final rule requires
a delay of two minutes and thirty
seconds between exposure of external
fuel tank vents to ignition sources and
explosions caused by propagation of
flames into the fuel tank, thus
increasing the time available for
passenger evacuation and emergency
response. The amendments apply to
applications for new type certificates
and certain applications for amended or
supplemental type certificates. The
amendments also require certain
airplanes produced in the future and
operated by air carriers to meet the new
standards.
However, in that document, the
amendment numbers for the final rules
were incorrect, and an airplane model
number in a footnote was incorrect. This
document now posts the correct
amendment numbers and airplane
model number in the footnote.
DATES: This correction is effective on
July 26, 2016.
FOR FURTHER INFORMATION CONTACT: For
technical questions concerning this
action, contact Mike Dostert, Propulsion
and Mechanical Systems Branch, ANM–
112, Transport Airplane Directorate,
Aircraft Certification Service, Federal
Aviation Administration, 1601 Lind
Ave. SW., Renton, WA 98057–3356;
telephone (425) 227–2132; facsimile
(425) 227 1149; email Mike.Dostert@
faa.gov.
SUPPLEMENTARY INFORMATION:
SUMMARY:
Background
On June 24, 2016, the FAA published
a final rule titled, ‘‘Fuel Tank Vent Fire
Protection’’ in the Federal Register (81
FR 41200).
Jkt 238001
PO 00000
Frm 00007
Fmt 4700
Sfmt 4700
48693
The intent of that rule is to prevent
fuel tank explosions caused by ignition
from external ignition sources of fuel
vapor either contained in vapor spaces 1
or exiting from vapor spaces through the
fuel tank vent outlets. Potential external
ignition sources include, but are not
limited to, ground handling equipment,
fuel fires that result from refueling
spills, or ground fires that follow a
survivable crash landing in which the
fuel tank and the vent system remain
intact. Means to prevent or delay the
propagation of flame 2 from external
sources into the fuel tank through the
fuel tank vent system 3 would also
prevent or delay fuel tank explosions
following certain accidents. These
means include flame arrestors or fuel
tank inerting. This prevention or delay
would provide additional time for the
safe evacuation of passengers from the
airplane and for emergency personnel to
provide assistance.
The rule applies to applications for
new type certificates and applications
for amended or supplemental type
certificates on significant product-level
change projects in which title 14, Code
of Federal Regulations (14 CFR) 25.975,
‘‘Fuel tank vents and carburetor vapor
vents,’’ is applicable to a changed area.
Additionally, a new operating
requirement in both 14 CFR part 121,
‘‘Operating Requirements: Domestic,
Flag, and Supplemental Operations,’’
and 14 CFR part 129, ‘‘Operations:
Foreign Air Carriers and Foreign
Operators of U.S.-Registered Aircraft
Engaged in Common Carriage,’’ applies
to airplanes that are issued an original
airworthiness certificate after a specified
date.
However, the rule published with
incorrect amendment numbers, ‘‘25–
142, 21–376, and 129–53.’’ Amendment
number 25–142 is the same amendment
number as the rule titled
‘‘Harmonization of Airworthiness
Standards—Fire Extinguishers and Class
B and F Cargo Compartments,’’ which
published in the Federal Register on
February 16, 2016 (81 FR 7698).
Amendment numbers 21–376 and 129–
53 are incorrect designations. The
correct amendment numbers for this
rule are ‘‘25–143, 121–375, and 129–
52.’’
1 A vapor space is any portion of the airplane fuel
tanks and the fuel tank vent system that, if such
tanks and system held any fuel, could contain fuel
vapor.
2 Flame propagation is the spread of a flame in
a combustible environment outward from the point
at which the combustion started.
3 A fuel tank vent system is a system that
ventilates fuel vapor from the airplane fuel tanks to
the atmosphere. A fuel tank vent system ensures
that the air and fuel pressure within the fuel tank
stay within structural limits required by § 25.975(a).
E:\FR\FM\26JYR1.SGM
26JYR1
48694
Federal Register / Vol. 81, No. 143 / Tuesday, July 26, 2016 / Rules and Regulations
In the same publication on page
41203 in footnote number 14, the
Lockheed airplane model number
referenced is ‘‘328.’’ The correct number
should be ‘‘382.’’
Correction
In FR Doc. 2016–14454, beginning on
page 41200 in the Federal Register of
June 24, 2016, make the following
corrections:
Correction
1. On page 41200, in the second
column, correct the 4th header
paragraph to read as follows:
‘‘[Docket No.: FAA–2014–0500; Amdt.
Nos. 25–143, 121–375, and 129–52].’’
2. On page 41203, in the second
column, correct the text of footnote
number 14 to read as follows:
‘‘The previously approved Lockheed
382 and Embraer flame arrestors would
not have met the 2 minute and 30
second requirement.’’
Issued under authority provided by 49
U.S.C. 106(f) and 44701(a) in Washington,
DC, on July 19, 2016.
Lirio Liu,
Director, Office of Rulemaking.
[FR Doc. 2016–17590 Filed 7–25–16; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Parts 91, 121, 125, 129, and 135
[Docket No. FAA–2011–1082]
Provision of Navigation Services for
the Next Generation Air Transportation
System (NextGen) Transition to
Performance-Based Navigation (PBN)
(Plan for Establishing a VOR Minimum
Operational Network)
Federal Aviation
Administration (FAA), DOT.
ACTION: Final policy statement.
AGENCY:
This action sets forth the Very
High Frequency (VHF) Omnidirectional
Range (VOR) Minimum Operational
Network (MON) policy as proposed in
the Proposed Provision of Navigation
Services for the Next Generation Air
Transportation System (NextGen)
Transition to Performance-Based
Navigation (PBN) notice of proposed
policy published on December 15, 2011
(76 FR 77939). This document provides
the discontinuance selection criteria
and candidate list of VOR Navigational
Aids (NAVAIDs) targeted for
discontinuance as part of the VOR MON
Implementation Program and United
States (U.S.) National Airspace System
rmajette on DSK2TPTVN1PROD with RULES
SUMMARY:
VerDate Sep<11>2014
13:45 Jul 25, 2016
Jkt 238001
(NAS) Efficient Streamline Services
Initiative. Additionally, this policy
addresses the regulatory processes the
FAA plans to follow to discontinue
VORs.
DATES: Effective July 26, 2016.
FOR FURTHER INFORMATION CONTACT: Ms.
Leonixa Salcedo, VOR MON Program
Manager, AJM–324, Navigation
Programs, Federal Aviation
Administration, 800 Independence
Avenue SW., Washington, DC 20591;
email: vormon@faa.gov; telephone: (844)
4VORMON (844–486–7666).
SUPPLEMENTARY INFORMATION:
Background
On December 15, 2011 the FAA
published in the Federal Register a
notice of proposed policy and request
for comments (76 FR 77939) on the
FAA’s proposed strategy for gradually
reducing the current VOR network to a
Minimum Operational Network (MON)
as the NAS transitions to performancebased navigation (PBN) as part of the
Next Generation Air Transportation
System (NextGen). The FAA announced
that, as part of a NAS Efficient
Streamlined Services Initiative, the
number of conventional NAVAIDs
would be reduced while more efficient
Area Navigation (RNAV) routes and
procedures are implemented throughout
the NAS. The FAA noted its intention
to convene a working group to assist in
developing a candidate list of VORs for
discontinuance using relevant
operational, safety, cost, and economic
criteria. Interested parties were invited
to participate in the review of this
policy and planning effort by submitting
written comments on the proposal.
The FAA reviewed all 330 comments
received and on August 21, 2012,
published in the Federal Register the
disposition of the comments on the
notice of proposed policy (77 FR 50420).
In considering and disposing of the
comments, the FAA noted that it would
develop an initial VOR MON Plan
which would be made publicly
available. The FAA renewed its
intention to convene a working group
that would assist in developing
objective criteria which would be
applied consistently nationally and
regionally to help identify those VOR
facilities that would remain operational.
Criteria for Assessing VOR
Discontinuance
After the FAA published the
disposition of comments, stakeholders,
industry, and military services provided
further inputs to the FAA for
consideration in developing the criteria
used to select VORs that would need to
PO 00000
Frm 00008
Fmt 4700
Sfmt 4700
be retained as a part of the MON. The
FAA also sought recommendations from
aviation industry stakeholders through
the RTCA Tactical Operations
Committee (TOC). With this collective
input, the FAA developed the criteria to
determine which VORs would be
candidates for retention. VORs not
meeting these criteria were considered
as discontinuance candidates.
The following criteria were used by
the FAA to determine which VORs
would be retained as a part of the MON:
— Retain VORs to perform Instrument
Landing System (ILS), Localizer
(LOC), or VOR approaches supporting
MON airports at suitable destinations
within 100 NM of any location within
the CONUS. Selected approaches
would not require Automatic
Direction Finder (ADF), Distance
Measuring Equipment (DME), Radar,
or GPS.
— Retain VORs to support international
oceanic arrival routes.
— Retain VORs to provide coverage at
and above 5,000 ft AGL.
— Retain most VORs in the Western
U.S. Mountainous Area (WUSMA),
specifically those anchoring Victor
airways through high elevation
terrain.
— Retain VORs required for military
use.
— VORs outside of the CONUS were not
considered for discontinuance under
the VOR MON Implementation
Program.
The following considerations were
used to supplement the VOR MON
criteria above:
— Only FAA owned/operated VORs
were considered for discontinuance.
— Co-located DME and Tactical Air
Navigation (TACAN) systems will
generally be retained when the VOR
service is terminated.
— Co-located communication services
relocated or reconfigured to continue
transmitting their services.
Working Group
Using the established criteria, the
FAA convened an internal working
group to develop a candidate list of
VORs using the VOR MON criteria
relevant to operational, safety, cost, and
economic considerations. The group
developed the VOR MON service by
first selecting MON airports that met the
criteria listed above. Airports with ILS
approaches that met the criteria were
selected in preference to VOR
approaches. If two airports in close
proximity had suitable approaches, then
the airport whose ILS or VOR approach
required the FAA to retain the fewest
number of VORs (i.e., to identify initial,
E:\FR\FM\26JYR1.SGM
26JYR1
Agencies
[Federal Register Volume 81, Number 143 (Tuesday, July 26, 2016)]
[Rules and Regulations]
[Pages 48693-48694]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2016-17590]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Parts 25, 121, and 129
[Docket No.: FAA-2014-0500; Amdt. Nos. 25-143, 121-375, and 129-52]
RIN 2120-AK30
Fuel Tank Vent Fire Protection; Correction
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; correction.
-----------------------------------------------------------------------
SUMMARY: The FAA is correcting a final rule published in the Federal
Register on June 24, 2016 (81 FR 41200). In that final rule, the FAA
amended certain airworthiness regulations for transport category
airplanes to require fuel tank designs that prevent a fuel tank
explosion caused by the propagation of flames, from external fires,
through the fuel tank vents. The final rule requires a delay of two
minutes and thirty seconds between exposure of external fuel tank vents
to ignition sources and explosions caused by propagation of flames into
the fuel tank, thus increasing the time available for passenger
evacuation and emergency response. The amendments apply to applications
for new type certificates and certain applications for amended or
supplemental type certificates. The amendments also require certain
airplanes produced in the future and operated by air carriers to meet
the new standards.
However, in that document, the amendment numbers for the final
rules were incorrect, and an airplane model number in a footnote was
incorrect. This document now posts the correct amendment numbers and
airplane model number in the footnote.
DATES: This correction is effective on July 26, 2016.
FOR FURTHER INFORMATION CONTACT: For technical questions concerning
this action, contact Mike Dostert, Propulsion and Mechanical Systems
Branch, ANM-112, Transport Airplane Directorate, Aircraft Certification
Service, Federal Aviation Administration, 1601 Lind Ave. SW., Renton,
WA 98057-3356; telephone (425) 227-2132; facsimile (425) 227 1149;
email Mike.Dostert@faa.gov.
SUPPLEMENTARY INFORMATION:
Background
On June 24, 2016, the FAA published a final rule titled, ``Fuel
Tank Vent Fire Protection'' in the Federal Register (81 FR 41200).
The intent of that rule is to prevent fuel tank explosions caused
by ignition from external ignition sources of fuel vapor either
contained in vapor spaces \1\ or exiting from vapor spaces through the
fuel tank vent outlets. Potential external ignition sources include,
but are not limited to, ground handling equipment, fuel fires that
result from refueling spills, or ground fires that follow a survivable
crash landing in which the fuel tank and the vent system remain intact.
Means to prevent or delay the propagation of flame \2\ from external
sources into the fuel tank through the fuel tank vent system \3\ would
also prevent or delay fuel tank explosions following certain accidents.
These means include flame arrestors or fuel tank inerting. This
prevention or delay would provide additional time for the safe
evacuation of passengers from the airplane and for emergency personnel
to provide assistance.
---------------------------------------------------------------------------
\1\ A vapor space is any portion of the airplane fuel tanks and
the fuel tank vent system that, if such tanks and system held any
fuel, could contain fuel vapor.
\2\ Flame propagation is the spread of a flame in a combustible
environment outward from the point at which the combustion started.
\3\ A fuel tank vent system is a system that ventilates fuel
vapor from the airplane fuel tanks to the atmosphere. A fuel tank
vent system ensures that the air and fuel pressure within the fuel
tank stay within structural limits required by Sec. 25.975(a).
---------------------------------------------------------------------------
The rule applies to applications for new type certificates and
applications for amended or supplemental type certificates on
significant product-level change projects in which title 14, Code of
Federal Regulations (14 CFR) 25.975, ``Fuel tank vents and carburetor
vapor vents,'' is applicable to a changed area. Additionally, a new
operating requirement in both 14 CFR part 121, ``Operating
Requirements: Domestic, Flag, and Supplemental Operations,'' and 14 CFR
part 129, ``Operations: Foreign Air Carriers and Foreign Operators of
U.S.-Registered Aircraft Engaged in Common Carriage,'' applies to
airplanes that are issued an original airworthiness certificate after a
specified date.
However, the rule published with incorrect amendment numbers, ``25-
142, 21-376, and 129-53.'' Amendment number 25-142 is the same
amendment number as the rule titled ``Harmonization of Airworthiness
Standards--Fire Extinguishers and Class B and F Cargo Compartments,''
which published in the Federal Register on February 16, 2016 (81 FR
7698). Amendment numbers 21-376 and 129-53 are incorrect designations.
The correct amendment numbers for this rule are ``25-143, 121-375, and
129-52.''
[[Page 48694]]
In the same publication on page 41203 in footnote number 14, the
Lockheed airplane model number referenced is ``328.'' The correct
number should be ``382.''
Correction
In FR Doc. 2016-14454, beginning on page 41200 in the Federal
Register of June 24, 2016, make the following corrections:
Correction
1. On page 41200, in the second column, correct the 4th header
paragraph to read as follows:
``[Docket No.: FAA-2014-0500; Amdt. Nos. 25-143, 121-375, and 129-
52].''
2. On page 41203, in the second column, correct the text of
footnote number 14 to read as follows:
``The previously approved Lockheed 382 and Embraer flame arrestors
would not have met the 2 minute and 30 second requirement.''
Issued under authority provided by 49 U.S.C. 106(f) and 44701(a)
in Washington, DC, on July 19, 2016.
Lirio Liu,
Director, Office of Rulemaking.
[FR Doc. 2016-17590 Filed 7-25-16; 8:45 am]
BILLING CODE 4910-13-P