Federal Register / Vol. 81, No. 181 / Monday, September 19, 2016 / Rules and Regulations 64057 

(m) Life Limit for P/N C2CF619A 

As of October 24, 2016 (the effective date 

of this AD), elevator control rod assemblies, 

P/N C2CF619A, are life-limited to 15 years 

and must be replaced with P/N C2CF619A– 

11, which is not a life-limited part, at the 

following compliance time: 

(1) If, as of October 24, 2016 (the effective 

date of this AD), the age of the installed P/ 

N C2CF619A is known, it must be replaced 

before exceeding the life limit or within the 

next 12 months after October 24, 2016 (the 

effective date of this AD), whichever occurs 

later. 

(2) If, as of October 24, 2016 (the effective 

date of this AD), the age of the installed P/ 

N C2CF619A is not known, it must be 

replaced within the next 12 months after 

October 24, 2016 (the effective date of this 

AD). 

(n) Credit for Actions Accomplished in 

Accordance With Previous Service 

Information 

Credit will be given for the inspections 

required in paragraphs (g)(1) through (3) of 

this AD if they were done before October 24, 

2016 (the effective date of this AD) following 

Viking Air Limited DHC–2 Beaver Service 

Bulletin Number: V2/0005, Revision ‘NC’, 

dated March 26, 2012; Viking Air Limited 

DHC–2 Beaver Service Bulletin Number: V2/ 

0005, Revision ‘A’, dated November 7, 2014; 

or Viking Air Limited DHC–2 Beaver Service 

Bulletin Number: V2/0005, Revision ‘B’, 

dated March 4, 2015. 

(o) 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), FAA, has the 

authority to approve AMOCs for this AD, if 

requested using the procedures found in 14 

CFR 39.19. Send information to ATTN: Aziz 

Ahmed, Aerospace Engineer, FAA, New York 

ACO, 1600 Stewart Avenue, Suite 410, 

Westbury, New York 11590; telephone: (516) 

228–7329; fax: (516) 794–5531; email: 

aziz.ahmed@faa.gov. Before using any 

approved AMOC on any airplane to which 

the AMOC applies, notify your appropriate 

principal inspector (PI) in the FAA Flight 

Standards District Office (FSDO), or lacking 

a PI, your local FSDO. 

(2) Airworthy Product: For any requirement 

in this AD to obtain corrective actions from 

a manufacturer or other source, use these 

actions if they are FAA-approved. Corrective 

actions are considered FAA-approved if they 

are approved by the State of Design Authority 

(or their delegated agent). You are required 

to assure the product is airworthy before it 

is returned to service. 

(3) Reporting Requirements: For any 

reporting requirement in this AD, a federal 

agency may not conduct or sponsor, and a 

person is not required to respond to, nor 

shall a person be subject to a penalty for 

failure to comply with a collection of 

information subject to the requirements of 

the Paperwork Reduction Act unless that 

collection of information displays a current 

valid OMB Control Number. The OMB 

Control Number for this information 

collection is 2120–0056. Public reporting for 

this collection of information is estimated to 

be approximately 5 minutes per response, 

including the time for reviewing instructions, 

completing and reviewing the collection of 

information. All responses to this collection 

of information are mandatory. Comments 

concerning the accuracy of this burden and 

suggestions for reducing the burden should 

be directed to the FAA at: 800 Independence 

Ave. SW., Washington, DC 20591, Attn: 

Information Collection Clearance Officer, 

AES–200. 

(p) Related Information 

Refer to MCAI Transport Canada AD No. 

CF–2015–21, dated July 30, 2015; and Viking 

Air Limited DHC–2 Beaver Service Bulletin 

Number: V2/0005, Revision ‘NC’, dated 

March 26, 2012; Viking Air Limited DHC–2 

Beaver Service Bulletin Number: V2/0005, 

Revision ‘A’, dated November 7, 2014; or 

Viking Air Limited DHC–2 Beaver Service 

Bulletin Number: V2/0005, Revision ‘B’, 

dated March 4, 2015, for related information. 

You may examine the MCAI on the Internet 

at https://www.regulations.gov/ 

document?D=FAA-2016-4229-0002. 

(q) 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) Viking DHC–2 Beaver Service Bulletin 

Number: V2/0005, Revision ‘‘C’’, dated July 

17, 2015. 

(ii) Item 20A., of Part 3, in Appendix 2 of 

Temporary Revision No.: 2–38, dated March 

4, 2015, into the VIKING PSM NO.: 1–2–2, 

AIRCRAFT: DHC–2 BEAVER, SERIES: ALL, 

PUBLICATION: MAINTENANCE MANUAL. 

(iii) Item 20A., in Part 4, of Temporary 

Revision No.: 2T–14, dated March 4, 2015, 

into VIKING PSM NO.: 1–2T–2, AIRCRAFT: 

DHC–2 TURBO BEAVER, SERIES: ALL, 

PUBLICATION: MAINTENANCE MANUAL. 

(3) For Viking Air Limited service 

information identified in this AD, contact 

Viking Air Limited Technical Support, 1959 

De Havilland Way, Sidney, British Columbia, 

Canada, V8L 5V5; Fax: 250–656–0673; 

telephone: (North America) (800) 663–8444; 

email: technical.support@vikingair.com; 

Internet: http://www.vikingair.com/support/ 

service-bulletins. 

(4) You may view this 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. In 

addition, you can access this service 

information on the Internet at http://

www.regulations.gov by searching for and 

locating Docket No. FAA–2016–4229. 

(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 Kansas City, Missouri, on 

September 8, 2016. 

Pat Mullen, 

Acting Manager, Small Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 2016–22183 Filed 9–16–16; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2016–5035; Directorate 

Identifier 2015–NM–042–AD; Amendment 

39–18650; AD 2016–19–01] 

RIN 2120–AA64 

Airworthiness Directives; Fokker 

Services B.V. Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule. 

SUMMARY: We are adopting a new 

airworthiness directive (AD) for all 

Fokker Services B.V. Model F28 Mark 

0070 and Mark 0100 airplanes. This AD 

was prompted by reports of cracking in 

a certain area of the pressure bulkhead 

webplate and skin connection angle. 

This AD requires a one-time inspection 

of the affected pressure bulkhead 

webplate and skin connection angle, 

and corrective actions if necessary. We 

are issuing this AD to detect and correct 

cracking of the pressure bulkhead 

webplate and skin connection angle that 

could lead to sudden inflight 

decompression of the airplane, resulting 

in injury to occupants. 

DATES: This AD is effective October 24, 

2016. 

The Director of the Federal Register 

approved the incorporation by reference 

of certain publications listed in this AD 

as of October 24, 2016. 

ADDRESSES: For service information 

identified in this final rule, contact 

Fokker Services B.V., Technical 

Services Dept., P.O. Box 1357, 2130 EL 

Hoofddorp, the Netherlands; telephone 

+31 (0)88–6280–350; fax +31 (0)88– 

6280–111; email technicalservices@

fokker.com; Internet http://

www.myfokkerfleet.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–2016– 

5035. 


rmajette on DSK2TPTVN1PROD with RULES
64058 Federal Register / Vol. 81, No. 181 / Monday, September 19, 2016 / Rules and Regulations 

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–2016– 

5035; 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: Tom 

Rodriguez, Aerospace Engineer, 

International Branch, ANM–116, 

Transport Airplane Directorate, FAA, 

1601 Lind Avenue SW., Renton, WA 

98057–3356; telephone 425–227–1137; 

fax 425–227–1139. 

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 all Fokker Services B.V. Model 

F28 Mark 0070 and Mark 0100 

airplanes. The NPRM published in the 

Federal Register on March 29, 2016 (81 

FR 17417) (‘‘the NPRM’’). The NPRM 

was prompted by reports of cracking in 

a certain area of the pressure bulkhead 

webplate and skin connection angle. 

The NPRM proposed to require a onetime inspection of the affected pressure 

bulkhead webplate and skin connection 

angle, and corrective actions if 

necessary. We are issuing this AD to 

detect and correct cracking of the 

pressure bulkhead webplate and skin 

connection angle that could lead to 

sudden inflight decompression of the 

airplane, resulting in injury to 

occupants. 

The European Aviation Safety Agency 

(EASA), which is the Technical Agent 

for the Member States of the European 

Union, has issued EASA Airworthiness 

Directive 2015–0024, dated February 19, 

2015 (referred to after this as the 

Mandatory Continuing Airworthiness 

Information, or ‘‘the MCAI’’), to correct 

an unsafe condition for all Fokker 

Services B.V. Model F28 Mark 0070 and 

Mark 0100 airplanes. The MCAI states: 

Service experience with the Fokker 100 

type design has shown that cracking can 

occur in the pressure bulkhead webplate and 

skin connection angle on the right hand (RH) 

side at station 14911 (station 12447 for F28 

Mark 0070) at stringer 67 of fuselage section 

2, before reaching the existing threshold for 

inspection per ALS [Airworthiness 

Limitations Section] task 533016–00–03 (F28 

Mark 0100) or task 533016–01–03 (F28 Mark 

0070). Any cracks in this area are not visible 

from the outside (covered by fairing) until 

they reach a critical length. 

This condition, if not detected and 

corrected, could lead to sudden in-flight 

decompression of the aeroplane, possibly 

resulting in injury to occupants. 

To address this potential unsafe condition, 

Fokker Services published Service Bulletin 

(SB) SBF100–53–128, which provides 

inspection instructions to detect any crack in 

the affected area. 

For the reasons described above, this 

[EASA] AD requires a one-time inspection of 

the affected pressure bulkhead webplate and 

skin connection angle, and, depending on 

findings, accomplishment of applicable 

corrective action(s). 

This [EASA] AD is considered to be an 

interim action and further AD action may 

follow, possibly to lower the current ALS 

task threshold, if justified by the inspection 

results. 

Corrective actions include repair of 

cracking in the skin connection angle 

and pressure bulkhead webplate, as 

applicable. 

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–2016– 

5035. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. We 

received no comments on the NPRM 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 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 Fokker Service Bulletin 

SBF100–53–128, dated November 12, 

2014; and Fokker Service Bulletin 

SBF100–53–129, dated February 16, 

2015. The service information describes 

procedures for inspection of the affected 

pressure bulkhead webplate and skin 

connection angle, and corrective actions 

if necessary. 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 8 

airplanes of U.S. registry. 

We also estimate that it will take 

about 1 work-hour per product to 

comply with the basic requirements of 

this AD, and 1 work-hour per product 

for reporting. The average labor rate is 

$85 per work-hour. Required parts will 

cost about $0 per product. Based on 

these figures, we estimate the cost of 

this AD on U.S. operators to be $1,360, 

or $170 per product. 

In addition, we estimate that any 

necessary follow-on actions will take 

about 46 work-hours and require parts 

costing $2,000, for a cost of $5,910 per 

product. We have no way of 

determining the number of aircraft that 

might need these actions. 

Paperwork Reduction Act 

A federal agency may not conduct or 

sponsor, and a person is not required to 

respond to, nor shall a person be subject 

to penalty for failure to comply with a 

collection of information subject to the 

requirements of the Paperwork 

Reduction Act unless that collection of 

information displays a current valid 

OMB control number. The control 

number for the collection of information 

required by this AD is 2120–0056. The 

paperwork cost associated with this AD 

has been detailed in the Costs of 

Compliance section of this document 

and includes time for reviewing 

instructions, as well as completing and 

reviewing the collection of information. 

Therefore, all reporting associated with 

this AD is mandatory. Comments 

concerning the accuracy of this burden 

and suggestions for reducing the burden 

should be directed to the FAA at 800 

Independence Ave. SW., Washington, 

DC 20591, ATTN: Information 

Collection Clearance Officer, AES–200. 

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 


rmajette on DSK2TPTVN1PROD with RULES
Federal Register / Vol. 81, No. 181 / Monday, September 19, 2016 / Rules and Regulations 64059 

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): 

2016–19–01 Fokker Services B.V.: 

Amendment 39–18650. Docket No. 

FAA–2016–5035; Directorate Identifier 

2015–NM–042–AD. 

(a) Effective Date 

This AD is effective October 24, 2016. 

(b) Affected ADs 

None. 

(c) Applicability 

This AD applies to Fokker Services B.V. 

Model F28 Mark 0070 and F28 Mark 0100 

airplanes, certificated in any category, all 

serial numbers. 

(d) Subject 

Air Transport Association (ATA) of 

America Code 53, Fuselage. 

(e) Reason 

This AD was prompted by reports of 

cracking in the pressure bulkhead webplate 

and skin connection angle. We are issuing 

this AD to detect and correct cracking of the 

pressure bulkhead webplate and skin 

connection angle that could lead to sudden 

inflight decompression of the airplane, 

resulting in injury to occupants. 

(f) Compliance 

Comply with this AD within the 

compliance times specified, unless already 

done. 

(g) Inspection 

At the time specified in paragraph (h) of 

this AD: Do a detailed inspection of the 

pressure bulkhead webplate and skin 

connection angle on the right-hand side at 

station 14911 (for Model F28 Mark 0100 

airplanes) or station 12447 (for Model F28 

Mark 0070 airplanes) at stringer 67 of 

fuselage section 2, as applicable, in 

accordance with the Accomplishment 

Instructions of Fokker Service Bulletin 

SBF100–53–128, dated November 12, 2014. 

This AD does not require action for airplanes 

which, as of the effective date of this AD, 

have accumulated less than 30,000 flight 

cycles. 

(1) If any crack is found in the skin 

connection angle, before further flight, repair 

the skin connection angle, in accordance 

with the Accomplishment Instructions of 

Fokker Service Bulletin SBF100–53–129, 

dated February 16, 2015. 

(2) If any crack is found in the pressure 

bulkhead webplate, before further flight, 

repair the pressure bulkhead webplate, in 

accordance with the Accomplishment 

Instructions of Fokker Service Bulletin 

SBF100–53–129, dated February 16, 2015. 

(h) Compliance Times 

At the applicable time specified in 

paragraph (h)(1) or (h)(2) of this AD, do the 

actions required by paragraph (g) of this AD. 

(1) For airplanes that have accumulated 

less than 40,000 total flight cycles as of the 

effective date of this AD, do the actions in 

paragraph (g) of this AD within 2,000 flight 

cycles after the effective date of this AD. 

(2) For airplanes that have accumulated 

40,000 or more total flight cycles as of the 

effective date of this AD, do the actions in 

paragraph (g) of this AD within 750 flight 

cycles after the effective date of this AD. 

(i) Reporting 

Submit a report of the findings (both 

positive and negative) of the inspection 

required by paragraph (g) of this AD to 

Fokker Services B.V. Engineering, Quality 

Department P.O. Box 1357, 2130 EL 

Hoofddorp, the Netherlands; telephone +31 

(0)88–6280–350; fax +31 (0)88–6280–111; 

email technicalservices@fokker.com; Internet 

http://www.myfokkerfleet.com, in accordance 

with the Accomplishment Instructions of 

Fokker Service Bulletin SBF100–53–128, 

dated November 12, 2014, at the applicable 

time specified in paragraph (i)(1) or (i)(2) of 

this AD. The report must include the 

inspection results; the airplane serial 

number; the total number of flight cycles and 

flight hours on the airplane; a sketch or photo 

to show the location of the crack(s) and 

damaged part(s), if applicable; and the length 

of each crack, if applicable. 

(1) If the inspection was done on or after 

the effective date of this AD: Submit the 

report within 30 days after the inspection. 

(2) If the inspection was done before the 

effective date of this AD: Submit the report 

within 30 days after the effective date of this 

AD. 

(j) Other FAA AD Provisions 

The following provisions also apply to this 

AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, International 

Branch, ANM–116, Transport Airplane 

Directorate, 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 International Branch, send it to ATTN: 

Tom Rodriguez, Aerospace Engineer, 

International Branch, ANM–116, Transport 

Airplane Directorate, FAA, 1601 Lind 

Avenue SW., Renton, WA 98057–3356; 

telephone 425–227–1137; fax 425–227–1149. 

Information may be emailed to: 9-ANM-116- 

AMOC-REQUESTS@faa.gov. 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. 

(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, International Branch, ANM– 

116, Transport Airplane Directorate, FAA; or 

the European Aviation Safety Agency 

(EASA); or Fokker B.V. Service’s EASA 

Design Organization Approval (DOA). If 

approved by the DOA, the approval must 

include the DOA-authorized signature. 

(3) Reporting Requirements: A federal 

agency may not conduct or sponsor, and a 

person is not required to respond to, nor 

shall a person be subject to a penalty for 

failure to comply with a collection of 

information subject to the requirements of 

the Paperwork Reduction Act unless that 

collection of information displays a current 

valid OMB Control Number. The OMB 

Control Number for this information 

collection is 2120–0056. Public reporting for 

this collection of information is estimated to 

be approximately 5 minutes per response, 

including the time for reviewing instructions, 

completing and reviewing the collection of 

information. All responses to this collection 

of information are mandatory. Comments 

concerning the accuracy of this burden and 

suggestions for reducing the burden should 

be directed to the FAA at: 800 Independence 

Ave. SW., Washington, DC 20591, Attn: 

Information Collection Clearance Officer, 

AES–200. 


rmajette on DSK2TPTVN1PROD with RULES
64060 Federal Register / Vol. 81, No. 181 / Monday, September 19, 2016 / Rules and Regulations 

(k) Related Information 

Refer to Mandatory Continuing 

Airworthiness Information (MCAI) EASA 

Airworthiness Directive 2015–0024, dated 

February 19, 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–2016–5035. 

(l) 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) Fokker Service Bulletin SBF100–53– 

128, dated November 12, 2014. 

(ii) Fokker Service Bulletin SBF100–53– 

129, dated February 16, 2015. 

(3) For service information identified in 

this AD, contact Fokker Services B.V., 

Technical Services Dept., P.O. Box 1357, 

2130 EL Hoofddorp, the Netherlands; 

telephone +31 (0)88–6280–350; fax +31 

(0)88–6280–111; email technicalservices@

fokker.com; Internet http://

www.myfokkerfleet.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 

September 6, 2016. 

Michael Kaszycki, 

Acting Manager, Transport Airplane 

Directorate, Aircraft Certification Service. 

[FR Doc. 2016–22186 Filed 9–16–16; 8:45 am] 

BILLING CODE 4910–13–P 

SOCIAL SECURITY ADMINISTRATION 

20 CFR Parts 404 and 416 

[Docket No. SSA–2006–0149] 

RIN 0960–AF58 

Revised Medical Criteria for Evaluating 

Respiratory System Disorders 

Correction 

In rule document 2016–13275, 

appearing on pages 37138–37153, in the 

issue of Thursday, June 9, 2016, make 

the following correction: 

PART 404—FEDERAL OLD AGE, 

SURVIVORS AND DISABILITY 

INSURANCE (1950) [CORRECTED] 

■ On page 37147, in the Table titled 

‘‘TABLE II—FVC CRITERIA FOR 

3.02B’’, the column headings are 

corrected to read as set forth below: 

Height without shoes 

(centimeters) 

< means less than 

Height without shoes 

(inches) 

< means less than 

Table II–A Table II–B 

Age 18 to attainment of age 20 Age 20 or older 

Females FVC 

less than or 

equal to 

(L, BTPS) 

Males FVC 

less than or 

equal to 

(L, BTPS) 

Females FVC 

less than or 

equal to 

(L, BTPS) 

Males FVC 

less than or 

equal to 

(L, BTPS) 

[FR Doc. C1–2016–13275 Filed 9–16–16; 8:45 am] 

BILLING CODE 1505–01–D 

DEPARTMENT OF HEALTH AND 

HUMAN SERVICES 

Food and Drug Administration 

21 CFR Parts 117 and 507 

[Docket Nos. FDA–2011–N–0920, FDA– 

2011–N–0922] 

Current Good Manufacturing Practice, 

Hazard Analysis, and Risk-Based 

Preventive Controls for Human Food 

and Current Good Manufacturing 

Practice, Hazard Analysis, and RiskBased Preventive Controls for Food for 

Animals; Definition of Qualified 

Auditor; Announcement of Effective 

Date 

AGENCY: Food and Drug Administration, 

HHS. 

ACTION: Final rule; announcement of 

effective date. 

SUMMARY: The Food and Drug 

Administration (FDA or we) is 

announcing the effective date for the 

definition of qualified auditor in the two 

final rules that appeared in the Federal 

Register of September 17, 2015. 

DATES: The effective date of paragraph 

(2) of the definition of qualified auditor 

in 21 CFR 117.3 and in 21 CFR 507.3, 

which published in the Federal Register 

of September 17, 2015 (80 FR 55908) 

and (80 FR 56170), is September 19, 

2016. 

FOR FURTHER INFORMATION CONTACT: For 

questions relating to Current Good 

Manufacturing Practice, Hazard 

Analysis and Risk-Based Preventive 

Controls for Human Food: Jenny Scott, 

Center for Food Safety and Applied 

Nutrition (HFS–300), Food and Drug 

Administration, 5001 Campus Dr., 

College Park, MD 20740, 240–402–2166. 

For questions relating to Current Good 

Manufacturing Practice, Hazard 

Analysis, and Risk-Based Preventive 

Controls for Food for Animals: Jeanette 

Murphy, Center for Veterinary Medicine 

(HFV–200), Food and Drug 

Administration, 7519 Standish Pl., 

Rockville, MD 20855, 240–402–6246. 

SUPPLEMENTARY INFORMATION: In the 

Federal Register of September 17, 2015 

(80 FR 55908), we published a final rule 

for ‘‘Current Good Manufacturing 

Practices, Hazard Analysis, and RiskBased Preventive Controls for Human 

Food’’ (preventive controls for human 

food rule). In § 117.3, we included the 

definition of a qualified auditor. In the 

definition, we provided examples of 

qualified auditors. Paragraph 2 of the 

definition reads ‘‘An audit agent of a 

certification body that is accredited in 

accordance with regulations in part 1, 

subpart M of this chapter.’’ At the time 

the final rule published, paragraph 2 

referred to a provision in a future final 

rule: ‘‘Accreditation of Third-Party 

Certification Bodies to Conduct Food 

Safety Audits to Issue Certifications’’ 

(third-party certification rule). In the 

preamble to the preventive controls for 

human food rule, we stated that we 

would publish a document in the 

Federal Register announcing the 

effective date of paragraph (2) once we 

finalized the third-party certification 

rule (80 FR 55908 at 55954). 

In the Federal Register of September 

17, 2015 (80 FR 56170), we published a 

final rule for ‘‘Current Good 

Manufacturing Practices, Hazard 

Analysis, and Risk-Based Preventive 

Controls for Food for Animals’’ 


rmajette on DSK2TPTVN1PROD with RULES