Special Conditions: Bombardier Aerospace, Models BD-500-1A10 and BD-500-1A11 Series Airplanes; Flight Envelope Protection: High-Speed Limiting, 32639-32640 [2014-13243]
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Federal Register / Vol. 79, No. 109 / Friday, June 6, 2014 / Rules and Regulations
Issued in Renton, Washington, April 22,
2014.
Jeffrey E. Duven,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 2014–13242 Filed 6–5–14; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 25
[Docket No. FAA–2013–1038; Special
Conditions No. 25–549–SC]
Special Conditions: Bombardier
Aerospace, Models BD–500–1A10 and
BD–500–1A11 Series Airplanes; Flight
Envelope Protection: High-Speed
Limiting
Federal Aviation
Administration (FAA), DOT.
ACTION: Final Special Conditions.
AGENCY:
These special conditions are
issued for the Bombardier Aerospace
Models BD–500–1A10 and BD–500–
1A11 series airplanes. These airplanes
will have a novel or unusual design
feature associated with an electronic
flight control system that contains flyby-wire control laws, including
envelope protections, for the overspeed
protection and roll-limiting function.
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: Effective Date: July 7, 2014.
FOR FURTHER INFORMATION CONTACT: Joe
Jacobsen, FAA, Airplane and Flight
Crew Interface Branch, ANM–111,
Transport Airplane Directorate, Aircraft
Certification Service, 1601 Lind Avenue
SW., Renton, Washington 98057–3356;
telephone 425–227–2011; facsimile
425–227–1149.
SUPPLEMENTARY INFORMATION:
mstockstill on DSK4VPTVN1PROD with RULES
SUMMARY:
Background
On December 10, 2009, Bombardier
Aerospace applied for a type certificate
for their new Models BD–500–1A10 and
BD–500–1A11 series airplanes (hereafter
collectively referred to as ‘‘CSeries’’).
The CSeries airplanes are swept-wing
monoplanes with an aluminum alloy
fuselage sized for 5-abreast seating.
Passenger capacity is designated as 110
for the Model BD–500–1A10 and 125 for
the Model BD–500–1A11. Maximum
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takeoff weight is 131,000 pounds for the
Model BD–500–1A10 and 144,000
pounds for the Model BD–500–1A11.
The longitudinal control law design of
the Bombardier CSeries airplanes
incorporates an overspeed protection
system in the normal mode. This mode
prevents the pilot from inadvertently or
intentionally exceeding a speed
approximately equivalent to the
maximum speed for stability
characteristics (VFC) or attaining
demonstrated flight diving speed (VDF).
Current Title 14, Code of Federal
Regulations (14 CFR) part 25 standards
did not envision a high-speed limiter
that might preclude or modify flying
qualities assessments in the overspeed
region.
Type Certification Basis
Under the provisions of 14 CFR 21.17,
Bombardier Aerospace must show that
the CSeries airplanes meet the
applicable provisions of part 25 as
amended by Amendments 25–1 through
25–129 thereto.
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 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, the special
conditions would also apply to the other
model under § 21.101.
In addition to the applicable
airworthiness regulations and special
conditions, the CSeries airplanes must
comply with the fuel vent and exhaust
emission requirements of 14 CFR part
34 and the noise certification
requirements of 14 CFR part 36, and 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 CSeries airplanes will incorporate
the following novel or unusual design
features: An electronic flight control
system that contains fly-by-wire control
laws, including envelope protections,
for the overspeed protection and rolllimiting function. Current part 25
requirements do not contain appropriate
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Fmt 4700
Sfmt 4700
32639
standards for high-speed protection
systems.
Discussion
The overspeed protection
functionality includes multifunction
spoilers (MFS) that will automatically
deploy as speed brakes once the
airspeed exceeds a small tolerance
above maximum operating limit speed
(Vmo/Mmo); the MFS will retract
automatically when speed is
subsequently reduced. Special
conditions are necessary in addition to
the requirements of § 25.143 for the
operation of the high-speed protection.
The general intent is that the overspeed
protection does not impede normal
maneuvering and speed control, and
that the overspeed protection does not
restrict or prevent emergency
maneuvering.
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. 25–13–38–SC for the Bombardier
CSeries airplanes was published in the
Federal Register on December 11, 2013
(78 FR 75284). We received one
comment in favor of the proposed
special conditions as written.
Applicability
As discussed above, these special
conditions are applicable to the Models
BD–500–1A10 and BD–500–1A11 series
airplanes. Should Bombardier
Aerospace apply at a later date for a
change to the type certificate to include
another model incorporating the same
novel or unusual design feature, the
special conditions would apply to that
model as well.
Conclusion
This action affects only certain novel
or unusual design features on two
model series of 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:
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 type
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06JNR1
32640
Federal Register / Vol. 79, No. 109 / Friday, June 6, 2014 / Rules and Regulations
certification basis for the Bombardier
Aerospace Models BD–500–1A10 and
BD–500–1A11 series airplanes.
Flight Envelope Protection—HighSpeed Limiting
1. In addition to § 25.143, the
following requirements apply:
Operation of the high-speed limiter
during all routine and descent
procedure flight must not impede
normal attainment of speeds up to
overspeed warning.
■
Issued in Renton, Washington, on April 22,
2014.
Jeffrey E. Duven,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 2014–13243 Filed 6–5–14; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 25
[Docket No. FAA–2014–0301; Special
Conditions No. 25–550–SC]
Special Conditions: The Boeing
Company, Models 737–700, –700C,
–800, –900ER, –7, –8, and –9 Series
Airplanes; Airplane Electronic Systems
Security Protection From Unauthorized
External Access
Federal Aviation
Administration (FAA), DOT.
ACTION: Final Special Condition;
Request for Comments.
AGENCY:
These special conditions are
issued for the Boeing Company Models
737–700, –700C, –800, –900ER, –7, –8,
and –9 series airplanes. These airplanes
will have novel or unusual design
features associated with the architecture
and connectivity capabilities of the
airplanes’ computer systems and
networks, which may allow access to or
by external computer systems and
networks and may result in security
vulnerabilities to the airplanes’ systems.
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 June 6, 2014. We
must receive your comments by July 21,
2014.
mstockstill on DSK4VPTVN1PROD with RULES
SUMMARY:
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16:43 Jun 05, 2014
Jkt 232001
Send comments identified
by docket number FAA–2014–0301
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
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:
Varun Khanna, FAA, Airplane and
Flight Crew Interface Branch, ANM–
111, Transport Airplane Directorate,
Aircraft Certification Service, 1601 Lind
Avenue SW., Renton, Washington
98057–3356; telephone 425–227–1298;
facsimile 425–227–1149.
SUPPLEMENTARY INFORMATION: The FAA
has determined that notice of, and
opportunity for prior public comment
on, these special conditions is
impracticable because these procedures
would significantly delay issuance of
the design approval and thus delivery of
the affected aircraft. In addition, the
substance of these special conditions
has been subject to the public comment
process in several prior instances with
ADDRESSES:
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Fmt 4700
Sfmt 4700
no substantive comments received. The
FAA therefore finds that good cause
exists for making these special
conditions effective upon publication in
the Federal Register.
Comments Invited
We invite interested people to take
part in this rulemaking by sending
written comments, data, or views. The
most helpful comments reference a
specific portion of the special
conditions, explain the reason for any
recommended change, and include
supporting data.
We will consider all comments we
receive by the closing date for
comments. We may change these special
conditions based on the comments we
receive.
Background
On January 27, 2012, the Boeing
Company applied for an amendment to
Type Certificate No. A16WE to include
new minor models, 737–7, –8, and –9.
The Models 737–7, –8, and –9, which
are derivatives of the 737–700, –800,
–900ER currently approved under Type
Certificate No. A16WE, are passenger
series airplanes designed to
substantially reduce fuel burn and
community noise. In addition, the
design will include a new CFM LEAP–
1B engine with a 68.4-inch diameter fan,
8-inch longer nose gear to accommodate
the larger engine, a relofted tailcone
(which requires the elevator to be
trimmed and the elevator tab to be
relocated outboard to accommodate the
new contours), new horizontal stabilizer
strakelets, a retractable auxiliary power
unit inlet door, fly-by-wire spoilers,
strengthened flight deck bulkhead, and
a new winglet design.
Type Certification Basis
Under the provisions of Title 14, Code
of Federal Regulations (14 CFR) 21.101,
The Boeing Company must show that
the Models 737–700, –700C, –800,
–900ER, –7, –8, and –9 series airplanes
meet the applicable provisions of the
regulations incorporated by reference in
Type Certificate No. A16WE or the
applicable regulations in effect on the
date of application for the change to the
type certificate. The regulations
incorporated by reference in the type
certificate are commonly referred to as
the ‘‘original type certification basis.’’ In
addition, the certification basis includes
certain special conditions, exemptions,
or later amended sections of the
applicable part that are not relevant to
these special conditions.
If the Administrator finds that the
applicable airworthiness regulations
(i.e., 14 CFR part 25) do not contain
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06JNR1
Agencies
[Federal Register Volume 79, Number 109 (Friday, June 6, 2014)]
[Rules and Regulations]
[Pages 32639-32640]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2014-13243]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 25
[Docket No. FAA-2013-1038; Special Conditions No. 25-549-SC]
Special Conditions: Bombardier Aerospace, Models BD-500-1A10 and
BD-500-1A11 Series Airplanes; Flight Envelope Protection: High-Speed
Limiting
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final Special Conditions.
-----------------------------------------------------------------------
SUMMARY: These special conditions are issued for the Bombardier
Aerospace Models BD-500-1A10 and BD-500-1A11 series airplanes. These
airplanes will have a novel or unusual design feature associated with
an electronic flight control system that contains fly-by-wire control
laws, including envelope protections, for the overspeed protection and
roll-limiting function. 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: Effective Date: July 7, 2014.
FOR FURTHER INFORMATION CONTACT: Joe Jacobsen, FAA, Airplane and Flight
Crew Interface Branch, ANM-111, Transport Airplane Directorate,
Aircraft Certification Service, 1601 Lind Avenue SW., Renton,
Washington 98057-3356; telephone 425-227-2011; facsimile 425-227-1149.
SUPPLEMENTARY INFORMATION:
Background
On December 10, 2009, Bombardier Aerospace applied for a type
certificate for their new Models BD-500-1A10 and BD-500-1A11 series
airplanes (hereafter collectively referred to as ``CSeries''). The
CSeries airplanes are swept-wing monoplanes with an aluminum alloy
fuselage sized for 5-abreast seating. Passenger capacity is designated
as 110 for the Model BD-500-1A10 and 125 for the Model BD-500-1A11.
Maximum takeoff weight is 131,000 pounds for the Model BD-500-1A10 and
144,000 pounds for the Model BD-500-1A11.
The longitudinal control law design of the Bombardier CSeries
airplanes incorporates an overspeed protection system in the normal
mode. This mode prevents the pilot from inadvertently or intentionally
exceeding a speed approximately equivalent to the maximum speed for
stability characteristics (VFC) or attaining demonstrated
flight diving speed (VDF). Current Title 14, Code of Federal
Regulations (14 CFR) part 25 standards did not envision a high-speed
limiter that might preclude or modify flying qualities assessments in
the overspeed region.
Type Certification Basis
Under the provisions of 14 CFR 21.17, Bombardier Aerospace must
show that the CSeries airplanes meet the applicable provisions of part
25 as amended by Amendments 25-1 through 25-129 thereto.
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 CSeries airplanes because of a
novel or unusual design feature, special conditions are prescribed
under the provisions of Sec. 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, the special conditions would also
apply to the other model under Sec. 21.101.
In addition to the applicable airworthiness regulations and special
conditions, the CSeries airplanes must comply with the fuel vent and
exhaust emission requirements of 14 CFR part 34 and the noise
certification requirements of 14 CFR part 36, and the FAA must issue a
finding of regulatory adequacy under Sec. 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 Sec. 11.38, and they become part of the type-
certification basis under Sec. 21.17(a)(2).
Novel or Unusual Design Features
The CSeries airplanes will incorporate the following novel or
unusual design features: An electronic flight control system that
contains fly-by-wire control laws, including envelope protections, for
the overspeed protection and roll-limiting function. Current part 25
requirements do not contain appropriate standards for high-speed
protection systems.
Discussion
The overspeed protection functionality includes multifunction
spoilers (MFS) that will automatically deploy as speed brakes once the
airspeed exceeds a small tolerance above maximum operating limit speed
(Vmo/Mmo); the MFS will retract automatically
when speed is subsequently reduced. Special conditions are necessary in
addition to the requirements of Sec. 25.143 for the operation of the
high-speed protection. The general intent is that the overspeed
protection does not impede normal maneuvering and speed control, and
that the overspeed protection does not restrict or prevent emergency
maneuvering.
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. 25-13-38-SC for the
Bombardier CSeries airplanes was published in the Federal Register on
December 11, 2013 (78 FR 75284). We received one comment in favor of
the proposed special conditions as written.
Applicability
As discussed above, these special conditions are applicable to the
Models BD-500-1A10 and BD-500-1A11 series airplanes. Should Bombardier
Aerospace apply at a later date for a change to the type certificate to
include another model incorporating the same novel or unusual design
feature, the special conditions would apply to that model as well.
Conclusion
This action affects only certain novel or unusual design features
on two model series of 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:
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 type
[[Page 32640]]
certification basis for the Bombardier Aerospace Models BD-500-1A10 and
BD-500-1A11 series airplanes.
Flight Envelope Protection--High-Speed Limiting
0
1. In addition to Sec. 25.143, the following requirements apply:
Operation of the high-speed limiter during all routine and descent
procedure flight must not impede normal attainment of speeds up to
overspeed warning.
Issued in Renton, Washington, on April 22, 2014.
Jeffrey E. Duven,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2014-13243 Filed 6-5-14; 8:45 am]
BILLING CODE 4910-13-P