14640 Federal Register / Vol. 78, No. 45 / Thursday, March 7, 2013 / Rules and Regulations 

List of Subjects in 9 CFR Part 424 

Food additives, Food packaging, Meat 

inspection, Poultry and poultry 

products. 

For the reasons set forth in the 

preamble, FSIS is amending 9 CFR part 

424 as follows: 

PART 424—PREPARATION AND 

PROCESSING OPERATIONS 

■ 1. The authority citation for part 424 

continues to read as follows: 

Authority: 7 U.S.C. 450, 1901–1906; 21 

U.S.C. 451–470, 601–695; 7 CFR 2.18, 2.53. 

■ 2. In § 424.23, revise paragraph (a)(3) 

to read as follows: 

§ 424.23 Prohibited uses. 

(a) * * * 

(3) Sorbic acid, calcium sorbate, 

sodium sorbate, and other salts of sorbic 

acid shall not be used in cooked 

sausages or any other meat; sulfurous 

acid and salts of sulfurous acid shall not 

be used in or on any meat; and niacin 

or nicotinamide shall not be used in or 

on fresh meat product; except that 

potassium sorbate, propylparaben 

(propyl p-hydroxybenzoate), and 

calcium propionate, may be used in or 

on any product, only as provided in 9 

CFR Chapter III. 

* * * * * 

Done at Washington, DC on: February 28, 

2013. 

Alfred V. Almanza, 

Administrator. 

[FR Doc. 2013–05341 Filed 3–6–13; 8:45 am] 

BILLING CODE 3410–DM–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2012–0720; Directorate 

Identifier 2012–NM–059–AD; Amendment 

39–17360; AD 2013–04–03] 

RIN 2120–AA64 

Airworthiness Directives; Cessna 

Aircraft Company Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for certain 

Cessna Aircraft Company Model 750 

airplanes. This AD was prompted by 

reports of loss of displayed airspeed. 

This AD requires inspecting certain 

logic modules to determine if certain 

cabin altitude/pitot static heater module 

assemblies are installed and replacing 

those assemblies with a new assembly; 

and revising the Non-Normal 

Procedures Section of the airplane flight 

manual (AFM) to include procedures for 

resetting the pitot switch in the event of 

pitot heater failure and for total loss of 

airspeed indication. We are issuing this 

AD to prevent the loss of all displayed 

airspeed, which could result in reduced 

ability to control the airplane. 

DATES: This AD is effective April 11, 

2013. 

The Director of the Federal Register 

approved the incorporation by reference 

of certain publication listed in the AD 

as of April 11, 2013. 

ADDRESSES: For service information 

identified in this AD, contact Cessna 

Aircraft Co., P.O. Box 7706, Wichita, 

Kansas 67277; telephone 316–517–6215; 

fax 316–517–5802; email 

citationpubs@cessna.textron.com; 

Internet https:// 

www.cessnasupport.com/newlogin.html. 

You may review copies of the 

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. 

Examining the AD Docket 

You may examine the AD docket on 

the Internet at http:// 

www.regulations.gov; 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 address for the 

Docket Office (phone: 800–647–5527) is 

Document 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: 

Christine Abraham, Aerospace Engineer, 

Electrical Systems and Avionics Branch, 

ACE–119W, FAA, Wichita Aircraft 

Certification Office (ACO), 1801 Airport 

Road, Room 100, Mid-Continent 

Airport, Wichita, Kansas 67209; phone: 

316–946–4165; fax: 316–946–4107; 

email: Christine.Abraham@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Discussion 

We issued a notice of proposed 

rulemaking (NPRM) to amend 14 CFR 

part 39 to include an AD that would 

apply to the specified products. That 

NPRM published in the Federal 

Register on July 17, 2012 (77 FR 41937). 

That NPRM proposed to require 

inspecting certain logic modules to 

determine if certain cabin altitude/pitot 

static heater module assemblies are 

installed and replacing those assemblies 

with a new assembly; and revising the 

Non-Normal Procedures Section of the 

AFM to include procedures for resetting 

the pitot switch in the event of pitot 

heater failure and for total loss of 

airspeed indication. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. The 

following presents the comments 

received on the proposal (77 FR 41937, 

July 17, 2012) and the FAA’s response 

to each comment. 

Request To Change Compliance Time 

Cessna Aircraft Company (Cessna) 

requested that the NPRM (77 FR 41937, 

July 17, 2012) use the compliance time 

described in Cessna Service Letter 

SL750–30–08, Revision 1, dated July 11, 

2011, of within two years or 1,200 flight 

hours after July 11, 2011 (The issue date 

of Cessna Service Letter SL750–30–08, 

Revision 1), whichever occurs first. 

Cessna noted that the proposed NPRM 

compliance time is within 600 flight 

hours or one year after the effective date 

of the AD, whichever occurs first. 

Cessna stated that the NPRM 

compliance time will extend the 

compliance time beyond what is 

suggested by Cessna Service Letter 

SL750–30–08, Revision 1, dated July 11, 

2011. 

We disagree with the request to 

change the compliance time. We 

coordinated with Cessna regarding the 

compliance time difference prior to 

issuing the NPRM (77 FR 41937, July 17, 

2012). We have determined that a 

compliance time of within 600 flight 

hours or one year after the effective date 

of the AD (whichever occurs first) is an 

appropriate compliance time to 

adequately address the identified unsafe 

condition. If additional data are 

presented to justify a shorter 

compliance time, we might consider 

further rulemaking. We have not 

changed the AD in this regard. 

Request To Change Logic Module 

Designators 

Cessna requested that we change the 

reference designators to the logic 

modules in paragraph (g) of the NPRM 

(77 FR 41937, July 17, 2012). Cessna 

stated that NC006 and NC007 are the 

correct reference designators for the 

logic modules. 

We agree to change the references 

because we have determined that the 

commenter’s stated references are 


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Federal Register / Vol. 78, No. 45 / Thursday, March 7, 2013 / Rules and Regulations 14641 

correct. We have changed paragraph (g) 

of this AD to refer to the logic modules 

as NC006 and NC007. 

Conclusion 

We reviewed the relevant data, 

considered the comments received, and 

determined that air safety and the 

public interest require adopting the AD 

with the change described previously 

and minor editorial changes. We have 

determined that these minor changes: 

• Are consistent with the intent that 

was proposed in the NPRM (77 FR 

41937, July 17, 2012) for correcting the 

unsafe condition; and 

• Do not add any additional burden 

upon the public than was already 

proposed in the NPRM (77 FR 41937, 

July 17, 2012). 

We also determined that these 

changes will not increase the economic 

burden on any operator or increase the 

scope of the AD. 

Costs of Compliance 

We estimate that this AD affects 210 

airplanes of U.S. registry. 

We estimate the following costs to 

comply with this AD: 

ESTIMATED COSTS

Action Labor cost Parts cost Cost per 

product 

Cost on U.S. 

operators 

Inspection ................................ 2 work-hours × $85 per hour = $170 ..................................... $0 $170 $35,700 

Revision .................................. 1 work-hour × $85 per hour = $85 ......................................... 0 85 17,850 

We estimate the following costs to do 

any necessary replacements that would 

be required based on the results of the 

inspection. We have no way of 

determining the number of aircraft that 

might need these replacements: 

ON-CONDITION COSTS

Action Labor cost Parts cost Cost per 

product 

Replacement .................................... 1 work-hour × $85 per hour = $85 ............................................................ $4,058 $4,143 

According to the manufacturer, some 

of the costs of this AD may be covered 

under warranty, thereby reducing the 

cost impact on affected individuals. We 

do not control warranty coverage for 

affected individuals. As a result, we 

have included all costs in our cost 

estimate. 

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 

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 

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): 

2013–04–03 Cessna Aircraft Company: 

Amendment 39–17360; Docket No. 

FAA–2012–0720; Directorate Identifier 

2012–NM–059–AD. 

(a) Effective Date 

This AD is effective April 11, 2013. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to The Cessna Aircraft 

Company Model 750 airplanes, certificated in 

any category, serial numbers 0001 through 

0245 inclusive. 

(d) Subject 

Joint Aircraft System Component (JASC)/ 

Air Transport Association (ATA) of America 

Code 3030, Pitot/Static Anti-Ice System. 

(e) Unsafe Condition 

This AD was prompted by reports of loss 

of displayed airspeed. We are issuing this AD 

to prevent the loss of all displayed airspeed, 

which could result in reduced ability to 

control the airplane. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Inspection and Replacement 

Within 600 flight hours or one year after 

the effective date of this AD, whichever 

occurs first: Do an inspection of logic 


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14642 Federal Register / Vol. 78, No. 45 / Thursday, March 7, 2013 / Rules and Regulations 

modules NC006 and NC007 to determine if 

any cabin altitude/pitot static heater module 

assemblies having part number (P/N) 

6718477–9, P/N 6718477–10, or P/N 

9914731–1 are installed, in accordance with 

the Accomplishment Instructions of Cessna 

Service Letter SL750–30–08, Revision 1, 

dated July 11, 2011. If any altitude/pitot 

static heater module assembly having P/N 

6718477–9, P/N 6718477–10, or P/N 

9914731–1 is installed: Before further flight, 

replace that assembly with a new assembly 

having P/N 6718477–11, in accordance with 

the Accomplishment Instructions of Cessna 

Service Letter SL750–30–08, Revision 1, 

dated July 11, 2011. 

(h) Airplane Flight Manual (AFM) Revision 

Concurrently with the actions required by 

paragraph (g) of this AD: Revise the NonNormal Procedures Section of the Cessna 750 

AFM to include the information in the flight 

manual changes identified in paragraphs 

(h)(1), (h)(2), (h)(3), (h)(4), (h)(5), and (h)(6) 

of this AD. This may be done by inserting 

copies of these flight manual changes into the 

Cessna 750 AFM. When these flight manual 

changes have been included in general 

revisions of the AFM, the general revisions 

may be inserted in the AFM, provided the 

relevant information in the general revision 

is identical to that in these flight manual 

changes, and then these temporary flight 

manual changes may be removed. 

(1) Cessna Temporary FAA Approved 

Airplane Flight Manual Change 75FM TC– 

R11–23, approved June 26, 2012. 

(2) Cessna Temporary FAA Approved 

Airplane Flight Manual Change 75FM TC– 

R11–24, approved June 26, 2012. 

(3) Cessna Temporary FAA Approved 

Airplane Flight Manual Change 75FM TC– 

R11–25, approved June 26, 2012. 

(4) Cessna Temporary FAA Approved 

Airplane Flight Manual Change 75FM TC– 

R11–26, approved June 26, 2012. 

(5) Cessna Temporary FAA Approved 

Airplane Flight Manual Change 75FMA TC– 

R02–03, approved April 10, 2012. 

(6) Cessna Temporary FAA Approved 

Airplane Flight Manual Change 75FMA TC– 

R02–07, approved June 26, 2012. 

(i) Parts Installation Prohibition 

As of the effective date of this AD, no 

person may install an altitude/pitot static 

heater module assembly having P/N 

6718477–9, P/N 6718477–10, or P/N 

9914731–1, on any airplane. 

(j) Special Flight Permit 

Special flight permits may be issued in 

accordance with sections 21.197 and 21.199 

of the Federal Aviation Regulations (14 CFR 

21.197 and 21.199) to operate the airplane to 

a location where the airplane can be 

modified (if the operator elects to do so), 

provided the actions required by paragraph 

(h) of this AD have been accomplished. 

(k) Alternative Methods of Compliance 

(AMOCs) 

(1) The Manager, Wichita Aircraft 

Certification Office (ACO), 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 manager of the ACO, send it to the 

attention of the person identified in the 

Related Information section of this AD. 

(2) 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. 

(l) Related Information 

For more information about this AD, 

contact Christine Abraham, Aerospace 

Engineer, Electrical Systems and Avionics 

Branch, ACE–119W, FAA, Wichita Aircraft 

Certification Office (ACO), 1801 Airport 

Road, Room 100, Mid-Continent Airport, 

Wichita, Kansas 67209; phone: 316–946– 

4165; fax: 316–946–4107; email: 

Christine.Abraham@faa.gov. 

(m) 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 the AD specifies otherwise. 

(i) Cessna Service Letter SL750–30–08, 

Revision 1, dated July 11, 2011. 

(ii) Cessna Temporary FAA Approved 

Airplane Flight Manual Change 75FM TC– 

R11–23, approved June 26, 2012. 

(iii) Cessna Temporary FAA Approved 

Airplane Flight Manual Change 75FM TC– 

R11–24, approved June 26, 2012. 

(iv) Cessna Temporary FAA Approved 

Airplane Flight Manual Change 75FM TC– 

R11–25, approved June 26, 2012. 

(v) Cessna Temporary FAA Approved 

Airplane Flight Manual Change 75FM TC– 

R11–26, approved June 26, 2012. 

(vi) Cessna Temporary FAA Approved 

Airplane Flight Manual Change 75FMA TC– 

R02–03, approved April 10, 2012. 

(vii) Cessna Temporary FAA Approved 

Airplane Flight Manual Change 75FMA TC– 

R02–07, approved June 26, 2012. 

(3) For Cessna service information 

identified in this AD, contact Cessna Aircraft 

Co., P.O. Box 7706, Wichita, Kansas 67277; 

telephone 316–517–6215; fax 316–517–5802; 

email citationpubs@cessna.textron.com; 

Internet https://www.cessnasupport.com/ 

newlogin.html. 

(4) You may review copies of the 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 February 

8, 2013. 

Ali Bahrami, 

Manager, 

Transport Airplane Directorate, Aircraft 

Certification Service. 

[FR Doc. 2013–04901 Filed 3–6–13; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2012–1157; Directorate 

Identifier 2012–NM–061–AD; Amendment 

39–17371; AD 2013–04–13] 

RIN 2120–AA64 

Airworthiness Directives; BAE 

SYSTEMS (OPERATIONS) LIMITED 

Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for all BAE 

SYSTEMS (OPERATIONS) LIMITED 

Model BAe 146 and Avro 146–RJ series 

airplanes. This AD was prompted by a 

report that certain ceramic terminal 

blocks, through which the wiring for the 

engine fire extinguishers, fire detection 

circuits, and engine and intake anti-ice 

system are routed, have been found to 

have moisture ingress, which can 

degrade the insulation resistance of the 

ceramic terminal blocks. This AD 

requires a one-time insulation resistance 

test of ceramic terminal blocks, and if 

necessary, replacement of the blocks. 

We are issuing this AD to prevent latent 

failure of the number 2 fire bottle, 

which, in the event of an engine fire, 

could result in failure of the fire bottle 

to discharge when activated and 

possibly preventing the flightcrew from 

extinguishing an engine fire. 

DATES: This AD becomes effective April 

11, 2013. 

The Director of the Federal Register 

approved the incorporation by reference 

of a certain publication listed in this AD 

as of April 11, 2013. 

ADDRESSES: You may examine the AD 

docket on the Internet at http:// 

www.regulations.gov or in person at the 

U.S. Department of Transportation, 

Docket Operations, M–30, West 

Building Ground Floor, Room W12–140, 

1200 New Jersey Avenue SE., 

Washington, DC. 

FOR FURTHER INFORMATION CONTACT: 

Todd Thompson, Aerospace Engineer, 


emcdonald on DSK67QTVN1PROD with RULES