11090 Federal Register / Vol. 78, No. 32 / Friday, February 15, 2013 / Rules and Regulations 

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 

§ 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 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Parts 117, 119, and 121 

[Docket No. FAA–2009–1093; Amdt. Nos. 

117–1, 119–16, 121–357] 

RIN 2120–AJ58 

Flightcrew Member Duty and Rest 

Requirements; Technical Correction 

AGENCY: Federal Aviation 

Administration, DOT. 

ACTION: Final rule; technical correction. 

SUMMARY: 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. 

SUPPLEMENTARY INFORMATION: 

Background 

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. 

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] 

BILLING CODE 4910–13–P 

DEPARTMENT OF COMMERCE 

International Trade Administration 

19 CFR Part 360 

[Docket No.: 121016549–2549–01] 

RIN 0625–AA93 

Steel Import Monitoring and Analysis 

System 

AGENCY: Import Administration, 

International Trade Administration, 

Department of Commerce. 

ACTION: Final rule. 

SUMMARY: 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. 


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