Airworthiness Directives; The Boeing Company Airplanes, 36471-36472 [C1-2015-14703]
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Federal Register / Vol. 80, No. 122 / Thursday, June 25, 2015 / Rules and Regulations
Lhorne on DSK7TPTVN1PROD with RULES
BD–500–1A11 series airplanes (hereafter
collectively referred to as ‘‘CSeries’’).
Bombardier later applied for, and was
granted, an extension of time for the
type certificate, which changed the
effective application date to December
31, 2011. The CSeries airplanes are
swept-wing monoplanes with an
aluminum alloy fuselage, sized for 5abreast seating. Passenger capacity is
110 for the Model BD–500–1A10 and
125 for the Model BD–500–1A11. The
airplanes are powered by two
underwing Pratt and Whitney PW1524G
ultra-high bypass, geared, turbofan
engines. Maximum takeoff weight is
131,000 pounds for the Model BD–500–
1A10 and 144,000 pounds for the Model
BD–500–1A11. The CSeries airplanes
will have a fly-by-wire EFCS.
Type Certification Basis
Under the provisions of Title 14, Code
of Federal Regulations (14 CFR) 21.17,
Bombardier Aerospace must show that
the CSeries airplane meets the
applicable provisions of part 25, as
amended by Amendments 25–1 through
25–129.
If the Administrator finds that the
applicable airworthiness regulations
(i.e., 14 CFR part 25) do not contain
adequate or appropriate safety standards
for the Bombardier CSeries airplanes
because of a novel or unusual design
feature, special conditions are
prescribed under the provisions of
§ 21.16.
Special conditions are initially
applicable to the model for which they
are issued. Should the type certificate
for that model be amended later to
include any other model that
incorporates the same or similar novel
or unusual design feature, these special
conditions would also apply to the other
model under § 21.101.
In addition to the applicable
airworthiness regulations and special
conditions, the Bombardier CSeries
airplane must comply with the fuel-vent
and exhaust-emission requirements of
14 CFR part 34, and the noisecertification requirements of 14 CFR
part 36. The FAA must issue a finding
of regulatory adequacy under § 611 of
Public Law 92–574, the ‘‘Noise Control
Act of 1972.’’
The FAA issues special conditions, as
defined in 14 CFR 11.19, in accordance
with § 11.38, and they become part of
the type-certification basis under
§ 21.17(a)(2).
Novel or Unusual Design Features
The Bombardier CSeries airplane will
incorporate the following novel or
unusual design feature: Fly-by-wire
EFCS that will limit pitch and roll
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functions to prevent the airplane from
attaining certain pitch attitudes and roll
angles greater than plus or minus 65
degrees, and positive spiral stability
introduced for roll angles greater than
30 degrees at speeds below VMO/MMO.
This system generates the actual surface
commands that provide for stability
augmentation and flight control for all
three airplane axes (longitudinal, lateral,
and directional).
Discussion
Part 25 does not specifically relate to
flight characteristics associated with
fixed attitude limits. Bombardier
proposes to implement on the CSeries
airplanes pitch and roll attitude-limiting
functions via the EFCS normal mode.
This will prevent the airplane from
attaining certain pitch attitudes and roll
angles greater than plus or minus 65
degrees. In addition, positive spiral
stability, introduced for roll angles
greater than 30 degrees at speeds below
VMO/MMO, and spiral stability
characteristics, must not require
excessive pilot strength to achieve bank
angles up to the bank-angle limit.
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.
Discussion of Comments
Notice of proposed special conditions
no. 25–15–02–SC for the Bombardier
Model BD–500–1A10 and BD–500–
1A11 series airplanes was published in
the Federal Register on February 27,
2015 (80 FR 10632). No substantive
comments were received, and the
special conditions are adopted as
proposed.
Applicability
As discussed above, these special
conditions are applicable to the
Bombardier CSeries airplane. Should
Bombardier Aerospace apply later for a
change to the type certificate to include
another model incorporating the same
or similar novel or unusual design
feature, these special conditions would
apply to that model as well.
Conclusion
This action affects only certain novel
or unusual design features on
Bombardier CSeries airplanes. It is not
a rule of general applicability.
List of Subjects in 14 CFR Part 25
Aircraft, Aviation safety, Reporting
and recordkeeping requirements.
The authority citation for these
special conditions is as follows:
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36471
Authority: 49 U.S.C. 106(g), 40113, 44701,
44702, 44704.
The Special Conditions
Accordingly, pursuant to the
authority delegated to me by the
Administrator, the following special
conditions are issued as part of the typecertification basis for the Bombardier
CSeries airplanes.
In addition to § 25.143, the following
requirements apply to the EFCS pitchand roll-limiting functions:
1. The pitch-limiting function must
not impede normal maneuvering for
pitch angles up to the maximum
required for normal maneuvering,
including a normal, all-enginesoperating takeoff, plus a suitable margin
to allow for satisfactory speed control.
2. The pitch- and roll-limiting
functions must not restrict or prevent
attaining pitch attitudes necessary for
emergency maneuvering, or roll angles
up to 65 degrees. Spiral stability, which
is introduced above 30 degrees roll
angle, must not require excessive pilot
strength to achieve these roll angles.
Other protections, which further limit
the roll capability under certain extreme
angle-of-attack, attitude, or high-speed
conditions, are acceptable, as long as
they allow at least 45 degrees of roll
capability.
3. A lower limit of roll is acceptable
beyond the overspeed warning if it is
possible to recover the airplane to the
normal flight envelope without undue
difficulty or delay.
Issued in Renton, Washington, on June 17,
2015.
Jeffrey E. Duven,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 2015–15545 Filed 6–24–15; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2014–0426; Directorate
Identifier 2013–NM–231–AD; Amendment
39–18186; AD 2015–12–11]
RIN 2120–AA64
Airworthiness Directives; The Boeing
Company Airplanes
Correction
In rule document 2015–14703
beginning on page 34827 in the issue of
Thursday, June 18, 2015 make the
following correction:
1. On page 34827, in the second
column, in the SUMMARY section, in
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25JNR1
36472
Federal Register / Vol. 80, No. 122 / Thursday, June 25, 2015 / Rules and Regulations
the third line, ‘‘The Boeing Company
Model and 777 airplanes’’ should read
‘‘The Boeing Company Model 767 and
777 airplanes.’’
[FR Doc. C1–2015–14703 Filed 6–24–15; 8:45 am]
BILLING CODE 1505–01–D
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 71
[Docket No. FAA–2014–0723; Airspace
Docket No. 14–AGL–13]
Establishment of Class E Airspace;
Highmore, SD
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
This action establishes Class
E airspace at Highmore, SD. Controlled
airspace is necessary to accommodate
new Standard Instrument Approach
Procedures (SIAPs) at Highmore
Municipal Airport. The FAA is taking
this action to enhance the safety and
management of Instrument Flight Rules
(IFR) operations for SIAPs at the airport.
Additionally, a minor adjustment is
made to the geographic coordinates for
Highmore Municipal Airport.
DATES: Effective 0901 UTC, August 20,
2015. The Director of the Federal
Register approves this incorporation by
reference action under title 1, Code of
Federal Regulations, part 51, subject to
the annual revision of FAA Order
7400.9 and publication of conforming
amendments.
SUMMARY:
FAA Order 7400.9Y,
Airspace Designations and Reporting
Points, and subsequent amendments can
be viewed on line at https://
www.faa.gov/airtraffic/publications/.
The Order is also available for
inspection at the National Archives and
Records Administration (NARA). For
information on the availability of this
material at NARA, call 202–741–6030,
or go to https://www.archives.gov/
federal_register/code_of_federalregulations/ibr_locations.html.
FAA Order 7400.9, Airspace
Designations and Reporting Points, is
published yearly and effective on
September 15. For further information,
you can contact the Airspace Policy and
ATC Regulations Group, Federal
Aviation Administration, 800
Independence Avenue SW.,
Washington, DC 29591; telephone: 202–
267–8783.
FOR FURTHER INFORMATION CONTACT:
Rebecca Shelby, Central Service Center,
Lhorne on DSK7TPTVN1PROD with RULES
ADDRESSES:
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Operations Support Group, Federal
Aviation Administration, Southwest
Region, 2601 Meacham Blvd., Fort
Worth, TX 76137; telephone: 817–321–
7740.
SUPPLEMENTARY INFORMATION:
Authority for This Rulemaking
The FAA’s authority to issue rules
regarding aviation safety is found in
Title 49 of the United States Code.
Subtitle I, Section 106 describes the
authority of the FAA Administrator.
Subtitle VII, Aviation Programs,
describes in more detail the scope of the
agency’s authority. This rulemaking is
promulgated under the authority
described in Subtitle VII, Part, A,
Subpart I, Section 40103. Under that
section, the FAA is charged with
prescribing regulations to assign the use
of airspace necessary to ensure the
safety of aircraft and the efficient use of
airspace. This regulation is within the
scope of that authority as it amends
Class E airspace at Highmore Municipal
Airport, Highmore, SD.
History
On April 24, 2015, the FAA published
in the Federal Register a notice of
proposed rulemaking (NPRM) to
establish Class E airspace extending
upward from 700 feet above the surface
at Highmore Municipal Airport,
Highmore, SD, (80 FR 22947). Interested
parties were invited to participate in
this rulemaking effort by submitting
written comments on the proposal to the
FAA. No comments were received.
Class E airspace designations are
published in Paragraphs 6005, of FAA
Order 7400.9Y, dated August 6, 2014,
and effective September 15, 2014, which
is incorporated by reference in 14 CFR
71.1. The Class E airspace designations
listed in this document will be
published subsequently in the Order.
Availability and Summary of
Documents for Incorporation by
Reference
This document amends FAA Order
7400.9Y, airspace Designations and
Reporting Points, dated August 6, 2014,
and effective September 15, 2014. FAA
Order 7400.9Y is publicly available as
listed in the ADDRESSES section of this
final rule. FAA Order 7400.9Y lists
Class A, B, C, D, and E airspace areas,
air traffic service routes, and reporting
points.
The Rule
This action amends Title 14, Code of
Federal Regulations (14 CFR), Part 71 by
establishing Class E airspace extending
upward from 700 feet above the surface
within a 6.5-mile radius of Highmore
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Municipal Airport, Highmore, SD, to
accommodate new Standard Instrument
Approach Procedures for IFR operations
at the airport. Additionally, geographic
coordinates for Highmore Municipal
airport, are changed from (lat. 44°32′40″
N., long. 99°27′04″ W.) to (lat. 44°32′27″
N., long. 99°27′04″ W.). This minor
adjustment reflects the current
information in the FAA’s aeronautical
database.
Regulatory Notices and Analyses
The FAA has determined that this
regulation only involves an established
body of technical regulations for which
frequent and routine amendments are
necessary to keep them operationally
current. Therefore, this regulation: (1) Is
not a ‘‘significant regulatory action’’
under Executive Order 12866; (2) is not
a ‘‘significant rule’’ under DOT
Regulatory Policies and Procedures (44
FR 11034; February 26, 1979); and (3)
does not warrant preparation of a
regulatory evaluation as the anticipated
impact is so minimal. Since this is a
routine matter that only affects air traffic
procedures and air navigation, it is
certified that this rule, when
promulgated, does not have a significant
economic impact on a substantial
number of small entities under the
criteria of the Regulatory Flexibility Act.
Environmental Review
The FAA has determined that this
action qualifies for categorical exclusion
under the National Environmental
Policy Act in accordance with FAA
Order 1050.1E. ‘‘Environmental
Impacts: Policies and Procedures,’’
paragraph 311a. This airspace action is
not expected to cause any potentially
significant environmental impacts, and
no extraordinary circumstances exist
that warrant preparation of an
environmental assessment.
List of Subjects in 14 CFR Part 71
Airspace, Incorporation by reference,
Navigation (air)
Adoption of the Amendment
In consideration of the foregoing, the
Federal Aviation Administration
amends 14 CFR part 71 as follows:
PART 71—DESIGNATION OF CLASS A,
B, C, D, AND E AIRSPACE AREAS; AIR
TRAFFIC SERVICE ROUTES; AND
REPORTING POINTS
1. The authority citation for part 71
continues to read as follows:
■
Authority: 49 U.S.C. 106(f), 106(g); 40103,
40113, 40120; E.O. 10854, 24 FR 9565, 3 CFR,
1959–1963 Comp., p. 389.
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25JNR1
Agencies
[Federal Register Volume 80, Number 122 (Thursday, June 25, 2015)]
[Rules and Regulations]
[Pages 36471-36472]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: C1-2015-14703]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2014-0426; Directorate Identifier 2013-NM-231-AD;
Amendment 39-18186; AD 2015-12-11]
RIN 2120-AA64
Airworthiness Directives; The Boeing Company Airplanes
Correction
In rule document 2015-14703 beginning on page 34827 in the issue of
Thursday, June 18, 2015 make the following correction:
1. On page 34827, in the second column, in the SUMMARY section, in
[[Page 36472]]
the third line, ``The Boeing Company Model and 777 airplanes'' should
read ``The Boeing Company Model 767 and 777 airplanes.''
[FR Doc. C1-2015-14703 Filed 6-24-15; 8:45 am]
BILLING CODE 1505-01-D