Special Conditions: Bombardier Aerospace, Model BD-500-1A10 and BD-500-1A11 Airplanes; Sidestick Controllers, 11089-11090 [2013-03590]

Download as PDF 11089 Rules and Regulations Federal Register Vol. 78, No. 32 Friday, February 15, 2013 This section of the FEDERAL REGISTER contains regulatory documents having general applicability and legal effect, most of which are keyed to and codified in the Code of Federal Regulations, which is published under 50 titles pursuant to 44 U.S.C. 1510. The Code of Federal Regulations is sold by the Superintendent of Documents. Prices of new books are listed in the first FEDERAL REGISTER issue of each week. DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 25 [Docket No. FAA–2012–1236; Special Conditions No. 25–477–SC] Special Conditions: Bombardier Aerospace, Model BD–500–1A10 and BD–500–1A11 Airplanes; Sidestick Controllers Federal Aviation Administration (FAA), DOT. ACTION: Final special conditions. AGENCY: These special conditions are issued for the Bombardier Aerospace Model BD–500–1A10 and BD–500– 1A11 airplanes. These airplanes 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 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: March 18, 2013. 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 425–227–1232. SUPPLEMENTARY INFORMATION: wreier-aviles on DSK5TPTVN1PROD with RULES SUMMARY: Background On December 10, 2009, Bombardier Aerospace applied for a type certificate for their new Model BD–500–1A10 and BD–500–1A11 airplanes. The Model BD–500–1A10 and BD–500–1A11 airplanes are swept-wing monoplanes VerDate Mar<15>2010 15:00 Feb 14, 2013 Jkt 229001 with pressurized cabins, and they share an identical supplier base and significant common design elements. The fuselages are aluminum alloy material, blended double-bubble fuselages, sized for nominal five-abreast seating. Each airplane’s powerplant includes two under-wing Pratt and Whitney PW1524G ultra-high bypass, geared turbofan engines. The flight controls are fly-by-wire flight with two passive/uncoupled sidesticks. Avionics include five landscape primary cockpit displays. The dimension of the aircraft encompasses a wingspan of 115 feet; height of 37.75 feet; and length of 114.75 feet for the Model BD–500–1A10 and length of 127 feet for the Model BD– 500–1A11. 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. Maximum takeoff thrust is 21,000 pounds for the Model BD– 500–1A10 and 23,300 pounds for the Model BD–500–1A11. The range is 5,463 kilometres for both model airplanes. The maximum operating altitude is 41,000 feet for both model airplanes. Bombardier Model BD–500–1A10 and BD–500–1A11 airplanes will be equipped with a sidestick controller instead of a conventional control column and wheel. This kind of controller is designed for only one-hand operation. The requirement of Title 14, Code of Federal Regulations (14 CFR) 25.397(c), which defines limit pilot forces and torques for conventional wheel or stick controls, is not adequate for a sidestick controller. A special condition is necessary to specify the appropriate loading conditions for this kind of controller. Type Certification Basis Under the provisions of 14 CFR 21.17, Bombardier Aerospace must show that the Model BD–500–1A10 and BD–500– 1A11 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 Bombardier Aerospace Model BD–500–1A10 and BD–500–1A11 PO 00000 Frm 00001 Fmt 4700 Sfmt 4700 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 Bombardier Aerospace Model BD–500–1A10 and BD–500– 1A11 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 Bombardier Aerospace Model BD–500–1A10 and BD–500–1A11 airplanes will incorporate the following novel or unusual design feature: A sidestick controller instead of a conventional control column and wheel. This kind of controller is designed for one-hand operation. Discussion The Bombardier Aerospace Model BD–500–1A10 and BD–500–1A11 airplanes are 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 adequate for a sidestick controller, because pilot forces are applied to sidestick controllers with only the wrist, not arms. A special condition is necessary to specify the appropriate loading conditions for a sidestick controller. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to E:\FR\FM\15FER1.SGM 15FER1 11090 Federal Register / Vol. 78, No. 32 / Friday, February 15, 2013 / Rules and Regulations that established by the existing airworthiness standards. the internal components of the electrical sensor assemblies, to avoid damage as a result of an in-flight jam. Discussion of Comments Notice of proposed special conditions No. 25–12–14–SC for the Bombardier Aerospace Model BD–500–1A10 and BD–500–1A11 airplanes was published in the Federal Register on November 20, 2012 (77 FR 69568). No comments were received, and the special conditions are adopted as proposed. Applicability Pitch Roll Nose up 125 lbf Nose down 125 lbf Nose Left 50 lbf Nose Right 50 lbf Issued in Renton, Washington, on February 12, 2013. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. As discussed above, these special conditions are applicable to the Bombardier Aerospace Model BD–500– 1A10 and BD–500–1A11 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. [FR Doc. 2013–03590 Filed 2–14–13; 8:45 am] Conclusion [Docket No. FAA–2009–1093; Amdt. Nos. 117–1, 119–16, 121–357] This action affects only certain novel or unusual design features on Bombardier Aerospace Model BD–500– 1A10 and BD–500–1A11 airplanes. It is not a rule of general applicability. The authority citation for these special conditions is as follows: 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 certification basis for Model BD–500– 1A10 and BD–500–1A11 airplanes by Bombardier Aerospace: Limit Pilot Forces for Sidestick Control wreier-aviles on DSK5TPTVN1PROD with RULES In lieu of the pilot forces specified in § 25.397(c), for the Bombardier Model BD–500–1A10 and BD–500–1A11 airplanes equipped with sidestick controls designed for forces to be applied by one wrist and not arms, the limit pilot forces are as follows: 1. For all components between and including the handle and its control stops. VerDate Mar<15>2010 Roll Nose Left 100 Lbf Nose Right 100 Lbf 16:26 Feb 14, 2013 Jkt 229001 14 CFR Parts 117, 119, and 121 Flightcrew Member Duty and Rest Requirements; Technical Correction Issued in Washington, DC, on February 11, 2013. Mark W. Bury, Acting Assistant Chief Counsel for International Law, Legislation, and Regulations. [FR Doc. 2013–03559 Filed 2–14–13; 8:45 am] RIN 2120–AJ58 The FAA is correcting the effective date of a final rule correction for flightcrew member duty and rest requirements published on February 6, 2013, that required technical corrections in the codified text of the final flightcrew member duty and rest rule. The correct effective date of the rule should read January 4, 2014. DATES: Effective date: The effective date of a final rule correction published in the Federal Register of February 6, 2013 (78 FR 8361), is corrected from January 14, 2014, to January 4, 2014. FOR FURTHER INFORMATION CONTACT: For technical questions concerning this action, contact Dale E. Roberts, AFS– 200, Flight Standards Service, Air Transportation Division Federal Aviation Administration, 800 Independence Avenue SW., Washington, DC 20591; telephone (202) 267–5749; email dale.e.roberts@faa.gov. For legal questions concerning this action, contact Robert Frenzel, AGC– 220, Office of Chief Counsel, Regulations Division, Federal Aviation Administration, 800 Independence Avenue SW., Washington, DC 20591; telephone (202) 267–3073; email: robert.frenzel@faa.gov. BILLING CODE 4910–13–P SUMMARY: Authority: 49 U.S.C. 106(g), 40113, 44701, 44702, 44704. 2. For all other components of the sidestick control assembly, excluding Federal Aviation Administration AGENCY: Aircraft, Aviation safety, Reporting and recordkeeping requirements. Nose up 200 pounds force (Lbf) Nose down 200 Lbf DEPARTMENT OF TRANSPORTATION On January 4, 2012, the FAA published a final rule entitled ‘‘Flightcrew Member Duty and Rest Requirements’’ (77 FR 330). In that rule, the FAA created a new part, part 117, which replaced the then-existing flight, duty, and rest regulations for part 121 passenger operations. As part of this rulemaking, the FAA also applied the new part 117 to certain part 91 operations, and it permitted all-cargo operations operating under part 121 to voluntarily opt into the part 117 flight, duty, and rest regulations. Subsequent to publication, the FAA discovered several issues requiring a technical correction in the regulatory text of the rule and published a final rule, technical correction on February 6, 2013 (78 FR 8361). The FAA realized that the effective date in this rule was inadvertently changed from January 4, 2014, to January 14, 2014. This technical correction changes the effective date to January 4, 2014. Federal Aviation Administration, DOT. ACTION: Final rule; technical correction. List of Subjects in 14 CFR Part 25 Pitch BILLING CODE 4910–13–P Background SUPPLEMENTARY INFORMATION: PO 00000 Frm 00002 Fmt 4700 Sfmt 4700 DEPARTMENT OF COMMERCE International Trade Administration 19 CFR Part 360 [Docket No.: 121016549–2549–01] RIN 0625–AA93 Steel Import Monitoring and Analysis System Import Administration, International Trade Administration, Department of Commerce. ACTION: Final rule. AGENCY: The Department of Commerce (the Department) publishes this action to make final a rule to extend the Steel Import Monitoring and Analysis (SIMA) system until March 21, 2017. The purpose of the SIMA system is to provide the public statistical data on steel imports entering the United States seven weeks earlier than it would otherwise be available to the public. Aggregate data collected from the licenses are made available to the public on a weekly basis following review by the Department. SUMMARY: E:\FR\FM\15FER1.SGM 15FER1

Agencies

[Federal Register Volume 78, Number 32 (Friday, February 15, 2013)]
[Rules and Regulations]
[Pages 11089-11090]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2013-03590]



========================================================================
Rules and Regulations
                                                Federal Register
________________________________________________________________________

This section of the FEDERAL REGISTER contains regulatory documents 
having general applicability and legal effect, most of which are keyed 
to and codified in the Code of Federal Regulations, which is published 
under 50 titles pursuant to 44 U.S.C. 1510.

The Code of Federal Regulations is sold by the Superintendent of Documents. 
Prices of new books are listed in the first FEDERAL REGISTER issue of each 
week.

========================================================================


Federal Register / Vol. 78, No. 32 / Friday, February 15, 2013 / 
Rules and Regulations

[[Page 11089]]



DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 25

[Docket No. FAA-2012-1236; Special Conditions No. 25-477-SC]


Special Conditions: Bombardier Aerospace, Model BD-500-1A10 and 
BD-500-1A11 Airplanes; Sidestick Controllers

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final special conditions.

-----------------------------------------------------------------------

SUMMARY: These special conditions are issued for the Bombardier 
Aerospace Model BD-500-1A10 and BD-500-1A11 airplanes. These airplanes 
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 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: March 18, 2013.

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 425-227-1232.

SUPPLEMENTARY INFORMATION:

Background

    On December 10, 2009, Bombardier Aerospace applied for a type 
certificate for their new Model BD-500-1A10 and BD-500-1A11 airplanes. 
The Model BD-500-1A10 and BD-500-1A11 airplanes are swept-wing 
monoplanes with pressurized cabins, and they share an identical 
supplier base and significant common design elements. The fuselages are 
aluminum alloy material, blended double-bubble fuselages, sized for 
nominal five-abreast seating. Each airplane's powerplant includes two 
under-wing Pratt and Whitney PW1524G ultra-high bypass, geared turbofan 
engines. The flight controls are fly-by-wire flight with two passive/
uncoupled sidesticks. Avionics include five landscape primary cockpit 
displays. The dimension of the aircraft encompasses a wingspan of 115 
feet; height of 37.75 feet; and length of 114.75 feet for the Model BD-
500-1A10 and length of 127 feet for the Model BD-500-1A11. 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. Maximum 
takeoff thrust is 21,000 pounds for the Model BD-500-1A10 and 23,300 
pounds for the Model BD-500-1A11. The range is 5,463 kilometres for 
both model airplanes. The maximum operating altitude is 41,000 feet for 
both model airplanes.
    Bombardier Model BD-500-1A10 and BD-500-1A11 airplanes will be 
equipped with a sidestick controller instead of a conventional control 
column and wheel. This kind of controller is designed for only one-hand 
operation.
    The requirement of Title 14, Code of Federal Regulations (14 CFR) 
25.397(c), which defines limit pilot forces and torques for 
conventional wheel or stick controls, is not adequate for a sidestick 
controller. A special condition is necessary to specify the appropriate 
loading conditions for this kind of controller.

Type Certification Basis

    Under the provisions of 14 CFR 21.17, Bombardier Aerospace must 
show that the Model BD-500-1A10 and BD-500-1A11 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 Bombardier Aerospace Model BD-500-
1A10 and BD-500-1A11 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 Bombardier Aerospace Model BD-500-1A10 and BD-500-1A11 
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 Bombardier Aerospace Model BD-500-1A10 and BD-500-1A11 
airplanes will incorporate the following novel or unusual design 
feature: A sidestick controller instead of a conventional control 
column and wheel. This kind of controller is designed for one-hand 
operation.

Discussion

    The Bombardier Aerospace Model BD-500-1A10 and BD-500-1A11 
airplanes are 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 adequate for a sidestick 
controller, because pilot forces are applied to sidestick controllers 
with only the wrist, not arms. A special condition is necessary to 
specify the appropriate loading conditions for a sidestick controller. 
These special conditions contain the additional safety standards that 
the Administrator considers necessary to establish a level of safety 
equivalent to

[[Page 11090]]

that established by the existing airworthiness standards.

Discussion of Comments

    Notice of proposed special conditions No. 25-12-14-SC for the 
Bombardier Aerospace Model BD-500-1A10 and BD-500-1A11 airplanes was 
published in the Federal Register on November 20, 2012 (77 FR 69568). 
No comments were received, and the special conditions are adopted as 
proposed.

Applicability

    As discussed above, these special conditions are applicable to the 
Bombardier Aerospace Model BD-500-1A10 and BD-500-1A11 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 Bombardier Aerospace Model BD-500-1A10 and BD-500-1A11 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 certification basis for Model BD-500-1A10 and BD-500-1A11 
airplanes by Bombardier Aerospace:

Limit Pilot Forces for Sidestick Control

    In lieu of the pilot forces specified in Sec.  25.397(c), for the 
Bombardier Model BD-500-1A10 and BD-500-1A11 airplanes equipped with 
sidestick controls designed for forces to be applied by one wrist and 
not arms, the limit pilot forces are as follows:
    1. For all components between and including the handle and its 
control stops.

------------------------------------------------------------------------
                   Pitch                                Roll
------------------------------------------------------------------------
Nose up 200 pounds force (Lbf)              Nose Left 100 Lbf
Nose down 200 Lbf                           Nose Right 100 Lbf
------------------------------------------------------------------------

    2. 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.

------------------------------------------------------------------------
                   Pitch                                Roll
------------------------------------------------------------------------
Nose up 125 lbf                             Nose Left 50 lbf
Nose down 125 lbf                           Nose Right 50 lbf
------------------------------------------------------------------------


    Issued in Renton, Washington, on February 12, 2013.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2013-03590 Filed 2-14-13; 8:45 am]
BILLING CODE 4910-13-P

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