Federal Register / Vol. 81, No. 71 / Wednesday, April 13, 2016 / Rules and Regulations 21709 

List of Subjects in 9 CFR Part 381 

Food grades and standards, Poultry 

and poultry products. 

For the reasons stated in the 

preamble, FSIS amends 9 CFR part 381, 

as follows: 

PART 381—POULTRY PRODUCTS 

INSPECTION REGULATIONS 

■ 1. The authority citation for part 381 

continues to read as follows: 

Authority: 7 U.S.C. 138f, 450; 21 U.S.C. 

451–470; 7 CFR 2.7, 2.18, 2.53. 

■ 2. Amend § 381.170 by revising 

paragraph (a)(1)(iii) to read as follows: 

§ 381.170 Standards for kinds and classes, 

and for cuts of raw poultry. 

(a) * * * 

(1) * * * 

(iii) Roaster or roasting chicken. A 

‘‘roaster’’ or ‘‘roasting chicken’’ is a 

young chicken (less than 12 weeks of 

age), of either sex, with a ready-to-cook 

carcass weight of 5.5 pounds or more, 

that is tender-meated with soft, pliable, 

smooth-textured skin and breastbone 

cartilage that is somewhat less flexible 

than that of a broiler or fryer. 

* * * * * 

Done at Washington, DC, on: April 8, 2016. 

Alfred V. Almanza, 

Acting Administrator. 

[FR Doc. 2016–08488 Filed 4–12–16; 8:45 am] 

BILLING CODE 3410–DM–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2015–4811; Directorate 

Identifier 2015–NM–104–AD; Amendment 

39–18481; AD 2016–08–05] 

RIN 2120–AA64 

Airworthiness Directives; Bombardier, 

Inc. Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for certain 

Bombardier, Inc. Model CL–600–2C10 

(Regional Jet Series 700, 701, & 702) 

airplanes, Model CL–600–2D15 

(Regional Jet Series 705) airplanes, 

Model CL–600–2D24 (Regional Jet 

Series 900) airplanes, and Model CL– 

600–2E25 (Regional Jet Series 1000) 

airplanes. This AD was prompted by the 

discovery of a number of incorrectly 

calibrated angle of attack (AOA) 

transducers installed in the stall 

protection system. This AD requires 

replacement of affected AOA 

transducers. We are issuing this AD to 

detect and replace incorrectly calibrated 

AOA transducers; incorrect calibration 

of the transducers could result in late 

activation of the stick pusher. 

DATES: This AD is effective May 18, 

2016. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in this AD 

as of May 18, 2016. 

ADDRESSES: For service information 

identified in this final rule, contact 

Bombardier, Inc., 400 Coˆte-Vertu Road 

West, Dorval, Que ́bec H4S 1Y9, Canada; 

telephone 514–855–5000; fax 514–855– 

7401; email thd.crj@

aero.bombardier.com; Internet http://

www.bombardier.com. You may view 

this referenced service information at 

the FAA, Transport Airplane 

Directorate, 1601 Lind Avenue SW., 

Renton, WA. For information on the 

availability of this material at the FAA, 

call 425–227–1221. It is also available 

on the Internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2015– 

4811. 

Examining the AD Docket 

You may examine the AD docket on 

the Internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2015– 

4811; or in person at the Docket 

Management Facility between 9 a.m. 

and 5 p.m., Monday through Friday, 

except Federal holidays. The AD docket 

contains this AD, the regulatory 

evaluation, any comments received, and 

other information. The street address for 

the Docket Office (telephone 800–647– 

5527) is Docket Management Facility, 

U.S. Department of Transportation, 

Docket Operations, M–30, West 

Building Ground Floor, Room W12–140, 

1200 New Jersey Avenue SE., 

Washington, DC 20590. 

FOR FURTHER INFORMATION CONTACT: 

Cesar Gomez, Aerospace Engineer, 

Airframe and Mechanical Systems 

Branch, ANE–171, FAA, New York 

Aircraft Certification Office (ACO), 1600 

Stewart Avenue, Suite 410, Westbury, 

NY 11590; telephone 516–228–7318; fax 

516–794–5531. 

SUPPLEMENTARY INFORMATION: 

Discussion 

We issued a notice of proposed 

rulemaking (NPRM) to amend 14 CFR 

part 39 by adding an AD that would 

apply to certain Bombardier, Inc. Model 

CL–600–2C10 (Regional Jet Series 700, 

701, & 702) airplanes, Model CL–600– 

2D15 (Regional Jet Series 705) airplanes, 

Model CL–600–2D24 (Regional Jet 

Series 900) airplanes, and Model CL– 

600–2E25 (Regional Jet Series 1000) 

airplanes. The NPRM published in the 

Federal Register on November 12, 2015 

(80 FR 69896) (‘‘the NPRM’’). 

Transport Canada Civil Aviation 

(TCCA), which is the aviation authority 

Canada, has issued Canadian 

Airworthiness Directive CF–2015–18, 

dated July 16, 2015 (referred to after this 

as the Mandatory Continuing 

Airworthiness Information, or ‘‘the 

MCAI’’), to correct an unsafe condition 

for certain Bombardier, Inc. Model CL– 

600–2C10 (Regional Jet Series 700, 701, 

& 702) airplanes, Model CL–600–2D15 

(Regional Jet Series 705) airplanes, 

Model CL–600–2D24 (Regional Jet 

Series 900) airplanes, and Model CL– 

600–2E25 (Regional Jet Series 1000) 

airplanes. The MCAI states: 

It was discovered that a number of AOA 

transducers installed on Bombardier CL– 

600–2C10, CL–600–2D15, CL–600–2D24, and 

CL–600–2E25 aeroplanes were incorrectly 

calibrated due to a quality control problem at 

both the production and repair facilities. 

Incorrect calibration of the AOA transducer 

could result in a late activation of the stick 

pusher. 

This [Canadian] AD mandates the 

replacement of the incorrectly calibrated 

AOA transducer. 

You may examine the MCAI in the 

AD docket on the Internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2015– 

4811. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. We 

considered the one comment received. 

The commenter supported the NPRM. 

Conclusion 

We reviewed the relevant data, 

considered the comments received, and 

determined that air safety and the 

public interest require adopting this AD 

as proposed except for minor editorial 

changes. We have determined that these 

minor changes: 

• Are consistent with the intent that 

was proposed in the NPRM for 

correcting the unsafe condition; and 

• Do not add any additional burden 

upon the public than was already 

proposed in the NPRM. 

Related Service Information Under 1 

CFR Part 51 

We reviewed Bombardier Service 

Bulletin 670BA–27–069, dated March 

30, 2015. This service information 


jstallworth on DSK7TPTVN1PROD with RULES
21710 Federal Register / Vol. 81, No. 71 / Wednesday, April 13, 2016 / Rules and Regulations 

describes procedures for replacement of 

transducers with correctly calibrated 

AOA transducers. This service 

information is reasonably available 

because the interested parties have 

access to it through their normal course 

of business or by the means identified 

in the ADDRESSES section. 

Costs of Compliance 

We estimate that this AD affects 400 

airplanes of U.S. registry. 

We also estimate that it would take 

about 4 work-hours per product to 

comply with the basic requirements of 

this AD. The average labor rate is $85 

per work-hour. Required parts would 

cost about $10,000 per product. Based 

on these figures, we estimate the cost of 

this AD on U.S. operators to be 

$4,136,000, or $10,340 per product. 

Authority for This Rulemaking 

Title 49 of the United States Code 

specifies the FAA’s authority to issue 

rules on aviation safety. 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. 

We are issuing this rulemaking under 

the authority described in ‘‘Subtitle VII, 

Part A, Subpart III, Section 44701: 

General requirements.’’ Under that 

section, Congress charges the FAA with 

promoting safe flight of civil aircraft in 

air commerce by prescribing regulations 

for practices, methods, and procedures 

the Administrator finds necessary for 

safety in air commerce. This regulation 

is within the scope of that authority 

because it addresses an unsafe condition 

that is likely to exist or develop on 

products identified in this rulemaking 

action. 

Regulatory Findings 

We determined that this AD will not 

have federalism implications under 

Executive Order 13132. This AD will 

not have a substantial direct effect on 

the States, on the relationship between 

the national government and the States, 

or on the distribution of power and 

responsibilities among the various 

levels of government. 

For the reasons discussed above, I 

certify that this AD: 

1. Is not a ‘‘significant regulatory 

action’’ under Executive Order 12866; 

2. Is not a ‘‘significant rule’’ under the 

DOT Regulatory Policies and Procedures 

(44 FR 11034, February 26, 1979); 

3. Will not affect intrastate aviation in 

Alaska; and 

4. Will not have a significant 

economic impact, positive or negative, 

on a substantial number of small entities 

under the criteria of the Regulatory 

Flexibility Act. 

List of Subjects in 14 CFR Part 39 

Air transportation, Aircraft, Aviation 

safety, Incorporation by reference, 

Safety. 

Adoption of the Amendment 

Accordingly, under the authority 

delegated to me by the Administrator, 

the FAA amends 14 CFR part 39 as 

follows: 

PART 39—AIRWORTHINESS 

DIRECTIVES 

■ 1. The authority citation for part 39 

continues to read as follows: 

Authority: 49 U.S.C. 106(g), 40113, 44701. 

§ 39.13 [Amended] 

■ 2. The FAA amends § 39.13 by adding 

the following new airworthiness 

directive (AD): 

2016–08–05 Bombardier, Inc.: Amendment 

39–18481. Docket No. FAA–2015–4811; 

Directorate Identifier 2015–NM–104–AD. 

(a) Effective Date 

This AD is effective May 18, 2016. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to the Bombardier, Inc. 

airplanes, certificated in any category, 

identified in paragraphs (c)(1), (c)(2), and 

(c)(3) of this AD. 

(1) Model CL–600–2C10 (Regional Jet 

Series 700, 701, & 702) airplanes, serial 

numbers 10002 through 10999 inclusive. 

(2) Model CL–600–2D15 (Regional Jet 

Series 705) airplanes and Model CL–600– 

2D24 (Regional Jet Series 900) airplanes, 

serial numbers 15001 through 15990 

inclusive. 

(3) Model CL–600–2E25 (Regional Jet 

Series 1000) airplanes, serial numbers 19001 

through 19990 inclusive. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 27, Flight Controls. 

(e) Reason 

This AD was prompted by the discovery of 

a number of incorrectly calibrated angle of 

attack (AOA) transducers installed in the 

stall protection system. We are issuing this 

AD to detect and replace incorrectly 

calibrated AOA transducers; incorrect 

calibration of the transducers could result in 

late activation of the stick pusher. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Replacement 

Within 2,500 flight hours or 12 months, 

whichever occurs first after the effective date 

of this AD, replace the AOA transducers 

identified in paragraph 1.A., ‘‘Effectivity,’’ of 

Bombardier Service Bulletin 670BA–27–069, 

dated March 30, 2015, with correctly 

calibrated AOA transducers, in accordance 

with the Accomplishment Instructions of 

Bombardier Service Bulletin 670BA–27–069, 

dated March 30, 2015. 

(h) Parts Installation Prohibition 

As of the effective date of this AD, no 

person may install, on any airplane, an AOA 

transducer having a part number or serial 

number identified in paragraph 1.A., 

‘‘Effectivity,’’ of Bombardier Service Bulletin 

670BA–27–069, dated March 30, 2015. 

(i) Other FAA AD Provisions 

The following provisions also apply to this 

AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, New York Aircraft 

Certification Office (ACO), ANE–170, FAA, 

has the authority to approve AMOCs for this 

AD, if requested using the procedures found 

in 14 CFR 39.19. In accordance with 14 CFR 

39.19, send your request to your principal 

inspector or local Flight Standards District 

Office, as appropriate. If sending information 

directly to the ACO, send it to ATTN: 

Program Manager, Continuing Operational 

Safety, FAA, New York ACO, 1600 Stewart 

Avenue, Suite 410, Westbury, NY 11590; 

telephone 516–228–7300; fax 516–794–5531. 

Before using any approved AMOC, notify 

your appropriate principal inspector, or 

lacking a principal inspector, the manager of 

the local flight standards district office/

certificate holding district office. The AMOC 

approval letter must specifically reference 

this AD. 

(2) Contacting the Manufacturer: For any 

requirement in this AD to obtain corrective 

actions from a manufacturer, the action must 

be accomplished using a method approved 

by the Manager, New York ACO, ANE–170, 

FAA; or Transport Canada Civil Aviation 

(TCCA); or Bombardier, Inc.’s TCCA Design 

Approval Organization (DAO). If approved by 

the DAO, the approval must include the 

DAO-authorized signature. 

(j) Related Information 

Refer to Mandatory Continuing 

Airworthiness Information (MCAI) Canadian 

Airworthiness Directive CF–2015–18, dated 

July 16, 2015, for related information. This 

MCAI may be found in the AD docket on the 

Internet at http://www.regulations.gov by 

searching for and locating Docket No. FAA– 

2015–4811. 

(k) Material Incorporated by Reference 

(1) The Director of the Federal Register 

approved the incorporation by reference 

(IBR) of the service information listed in this 

paragraph under 5 U.S.C. 552(a) and 1 CFR 

part 51. 

(2) You must use this service information 

as applicable to do the actions required by 

this AD, unless this AD specifies otherwise. 

(i) Bombardier Service Bulletin 670BA–27– 

069, dated March 30, 2015. 

(ii) Reserved. 

(3) For service information identified in 

this AD, contact Bombardier, Inc., 400 CoˆteVertu Road West, Dorval, Que ́bec H4S 1Y9, 


jstallworth on DSK7TPTVN1PROD with RULES
Federal Register / Vol. 81, No. 71 / Wednesday, April 13, 2016 / Rules and Regulations 21711 

Canada; telephone 514–855–5000; fax 514– 

855–7401; email thd.crj@

aero.bombardier.com; Internet http://

www.bombardier.com. 

(4) You may view this service information 

at the FAA, Transport Airplane Directorate, 

1601 Lind Avenue SW., Renton, WA. For 

information on the availability of this 

material at the FAA, call 425–227–1221. 

(5) You may view this service information 

that is incorporated by reference 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: http://

www.archives.gov/federal-register/cfr/ibrlocations.html. 

Issued in Renton, Washington, on March 

31, 2016. 

Victor Wicklund, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. 2016–08346 Filed 4–12–16; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2016–0068; Directorate 

Identifier 2015–CE–037–AD; Amendment 

39–18484; AD 2016–08–08] 

RIN 2120–AA64 

Airworthiness Directives; SOCATA 

Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule. 

SUMMARY: We are superseding 

airworthiness directive (AD) 92–06–10 

for SOCATA Models MS 880B, MS 885, 

MS 892A–150, MS 892E–150, MS 893A, 

MS 893E, MS 894A, MS 894E, Rallye 

100S, Rallye 150ST, Rallye 150T, Rallye 

235E, and Rallye 235C airplanes. This 

AD results from mandatory continuing 

airworthiness information (MCAI) 

issued by an aviation authority of 

another country to identify and correct 

an unsafe condition on an aviation 

product. The MCAI describes the unsafe 

condition as fatigue failure of the nose 

landing gear wheel axle. We are issuing 

this AD to require actions to address the 

unsafe condition on these products. 

DATES: This AD is effective May 18, 

2016. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in the AD 

as of May 18, 2016. 

ADDRESSES: You may examine the AD 

docket on the Internet at http://

www.regulations.gov by searching for 

and locating Docket No. FAA–2016– 

0068; or in person at the Docket 

Management Facility, U.S. Department 

of Transportation, Docket Operations, 

M–30, West Building Ground Floor, 

Room W12–140, 1200 New Jersey 

Avenue SE., Washington, DC 20590. 

For service information identified in 

this AD, contact SOCATA, Direction des 

services, 65921 Tarbes Cedex 9, France; 

phone: +33 (0) 5 62 41 73 00; fax: +33 

(0) 5 62 41 76 54; email: info@

socata.daher.com; Internet: http://

www.tbm.aero/. For the United States, 

contact SOCATA NORTH AMERICA, 

North Perry Airport, 601 NE 10 Street, 

Pompano Beach, Florida 33060; phone: 

(954) 366–3331; Internet: http://

www.socatanorthamerica.com/

default.htm. You may view this 

referenced service information at the 

FAA, Small Airplane Directorate, 901 

Locust, Kansas City, Missouri 64106. 

For information on the availability of 

this material at the FAA, call (816) 329– 

4148. It is also available on the Internet 

at http://www.regulations.gov by 

searching for Docket No. FAA–2016– 

0068. 

FOR FURTHER INFORMATION CONTACT: 

Albert Mercado, Aerospace Engineer, 

901 Locust, Room 301, Kansas City, 

Missouri 64106; telephone: (816) 329– 

4119; fax: (816) 329–4090; email: 

albert.mercado@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Discussion 

We issued a notice of proposed 

rulemaking (NPRM) to amend 14 CFR 

part 39 by adding an AD that would 

apply to SOCATA Models MS 880B, MS 

885, MS 894A, MS 893A, MS 892A–150, 

MS 892E–150, MS 893E, MS 894E, 

Rallye 100S, Rallye 150T, Rallye 150ST, 

Rallye 235E, and Rallye 235C airplanes. 

That NPRM was published in the 

Federal Register on January 15, 2016 

(81 FR 2134), and proposed to 

supersede AD 92–06–10, Amendment 

39–8190 (57 FR 8063; March 6, 1992) 

(‘‘92–06–10’’). 

The NPRM proposed to correct an 

unsafe condition for the specified 

products and was based on mandatory 

continuing airworthiness information 

(MCAI) originated by an aviation 

authority of another country. The MCAI 

states that: 

A nose landing gear (NLG) wheel axle 

rupture occurred in service. The results of 

the technical investigation revealed that this 

failure was due to premature wear. 

This condition, if not detected and 

corrected, could lead to cracks in the axle 

and detachment of axle and wheel, possibly 

resulting in failure of the NLG with 

consequent damage to the aeroplane and 

injury to occupants. 

To address this potential unsafe condition, 

DGAC France issued AD 91–163(A) (later 

revised twice) to require repetitive detailed 

inspections (DET) of the NLG wheel axle and 

replacement of the NLG wheel axle 

attachment screws in accordance with the 

instructions of SOCATA Service Bulletin 

(SB) 150–32. 

Since DGAC France AD 91–163(A)R2 was 

issued, new findings led to an adjustment of 

the inspection interval. Consequently, 

SOCATA issued SB 150–32, now at Revision 

3. 

The MCAI can be found in the AD 

docket on the Internet at: http://

www.regulations.gov/

#!documentDetail;D=FAA-2016-0068- 

0002. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. We 

received no comments on the NPRM (81 

FR 2134, January 15, 2016) or on the 

determination of the cost to the public. 

Conclusion 

We reviewed the relevant data and 

determined that air safety and the 

public interest require adopting the AD 

as proposed except for minor editorial 

changes. We have determined that these 

minor changes: 

• Are consistent with the intent that 

was proposed in the NPRM (81 FR 2134, 

January 15, 2016) for correcting the 

unsafe condition; and 

• Do not add any additional burden 

upon the public than was already 

proposed in the NPRM (81 FR 2134, 

January 15, 2016). 

Related Service Information Under 1 

CFR Part 51 

We reviewed Daher-Socata Mandatory 

Service Bulletin SB 150–32, Revision 3, 

dated September 2015. The service 

bulletin describes procedures for 

inspection of the nose gear wheel axle. 

This service information is reasonably 

available because the interested parties 

have access to it through their normal 

course of business or by the means 

identified in the ADDRESSES section of 

the AD. 

Costs of Compliance 

We estimate that this AD will affect 

77 products of U.S. registry. We also 

estimate that it would take about 10 

work-hours per product to comply with 

the basic requirements of this AD. The 

average labor rate is $85 per work-hour. 

Required parts would cost about $500 

per product. 

Based on these figures, we estimate 

the cost of the AD on U.S. operators to 

be $103,950, or $1,350 per product. 

In addition, we estimate that any 

necessary follow-on actions would take 


jstallworth on DSK7TPTVN1PROD with RULES