[Federal Register Volume 77, Number 224 (Tuesday, November 20, 2012)]
[Proposed Rules]
[Pages 69571-69572]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2012-28113]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 25
[Docket No. FAA-2012-1216; Notice No. 25-12-13-SC]
Special Conditions: Embraer S.A., Model EMB-550 Airplane, Limit
Pilot Forces for Sidestick Control
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed special conditions.
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SUMMARY: This action proposes special conditions for the Embraer S.A.
Model EMB-550 airplane. This airplane will have a novel or unusual
design feature, specifically sidestick controllers designed to be
operated with only one hand. The applicable airworthiness regulations
do not contain adequate or appropriate safety standards for this design
feature. These proposed 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: Send your comments on or before January 4, 2013.
ADDRESSES: Send comments identified by docket number [FAA-2012-1216]
using any of the following methods:
Federal eRegulations Portal: Go to http://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 8 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 http://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 http://DocketsInfo. dot.gov/.
Docket: Background documents or comments received may be read at
http://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: Todd Martin, FAA, Airframe and Cabin
Safety Branch, ANM-115, Transport Airplane Directorate, Aircraft
Certification Service, 1601 Lind Avenue SW., Renton, Washington 98057-
3356; telephone 425-227-1178; facsimile 425-227-1149.
SUPPLEMENTARY INFORMATION:
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 on or before the closing
date for comments. We may change these special conditions based on the
comments we receive.
Background
On May 14, 2009, Embraer S.A. applied for a type certificate for
their new Model EMB-550 airplane. The Model EMB-550 airplane is the
first of a new family of jet airplanes designed for corporate flight,
fractional, charter, and private owner operations. The aircraft has a
conventional configuration with low wing and T-tail empennage. The
primary structure is metal with composite empennage and control
surfaces. The Model EMB-550 airplane is designed for 8 passengers, with
a maximum of 12 passengers. It is equipped with two Honeywell HTF7500-E
medium bypass ratio turbofan engines mounted on aft fuselage pylons.
Each engine produces approximately 6,540 pounds of thrust for normal
takeoff. The primary flight controls consist of hydraulically powered
fly-by-wire elevators, ailerons, and rudder, controlled by the pilot or
copilot sidestick.
Current regulations reference pilot effort loads for the cockpit
pitch and roll controls that are based on a two-handed effort. The
cockpit roll and pitch controls for the Model EMB-550 airplane are
designed for one-handed operation.
Type Certification Basis
Under the provisions of Title 14, Code of Federal Regulations (14
CFR) 21.17, Embraer S.A. must show that the Model EMB-550 airplane
meets the applicable provisions of part 25, as amended by Amendments
25-1 through 25-127 thereto.
If the Administrator finds that the applicable airworthiness
regulations 14 CFR part 25 do not contain adequate or appropriate
safety standards for the Model EMB-550 airplane 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.
[[Page 69572]]
In addition to the applicable airworthiness regulations and special
conditions, the Model EMB-550 airplane 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 section 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 Model EMB-550 airplane will incorporate the following novel or
unusual design features: The Embraer S.A. Model EMB-550 airplane is
equipped with a sidestick controller instead of a conventional wheel or
control stick. This kind of controller is designed to be operated using
only one hand. The requirement of 14 CFR 25.397(c), which defines limit
pilot forces and torques for conventional wheel or stick controls, is
not appropriate for a sidestick controller. Therefore, a special
condition is necessary to specify the appropriate loading conditions
for this kind of controller.
Discussion
The Embraer S.A. Model EMB-550 airplane is equipped with a
sidestick controller instead of a conventional wheel or control stick.
This kind of controller is designed to be operated using only one hand.
The requirement of 14 CFR 25.397(c), which defines limit pilot forces
and torques for conventional wheel or stick controls, is not
appropriate for a sidestick controller, because pilot forces are
applied to sidestick controllers with only the wrist, not arms. These
proposed 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.
Applicability
As discussed above, these special conditions are applicable to the
Model EMB-550 airplane. Should Embraer S.A. 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 one model 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 Proposed Special Conditions
Accordingly, the FAA proposes the following special conditions as
part of the type certification basis for Embraer S.A. Model EMB-550
airplanes.
1. Limit Pilot Forces for Sidestick Control.
In lieu of the pilot forces specified in Sec. 25.397(c):
(a) The limit pilot forces are:
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Pitch Roll
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Nose up 200 pounds force (lbf)............ Nose left 100 lbf.
Nose down 200 lbf......................... Nose right 100 lbf.
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(b) For all other components of the sidestick control assembly,
excluding the internal components of the electrical sensor assemblies,
to avoid damage as a result of an in-flight jam.
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Pitch Roll
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Nose up 125 lbf........................... Nose left 50 lbf.
Nose down 125 lbf......................... Nose right 50 lbf.
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Issued in Renton, Washington, on November 14, 2012.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2012-28113 Filed 11-19-12; 8:45 am]
BILLING CODE 4910-13-P