38572 Federal Register / Vol. 81, No. 114 / Tuesday, June 14, 2016 / Rules and Regulations 
Civil Penalties Inflation Adjustment Act Improvements Act of 2015, (28 U.S.C. 
2461 note) as follows: 
U.S. code citation Civil penalty description Adjusted 
maximum civil 
penalty amount 
12 U.S.C. 5565(c)(2)(A) ........................................................... Tier 1 penalty ............................... ........................................... $5,437 
12 U.S.C. 5565(c)(2)(B) ........................................................... Tier 2 penalty ............................... ........................................... 27,186 
12 U.S.C. 5565(c)(2)(C) .......................................................... Tier 3 penalty ................................ .......................................... 1,087,450 
15 U.S.C. 1717a(a)(2) ............................................................. Per violation ................................ ............................................. 1,894 
15 U.S.C. 1717a(a)(2) ............................................................. Annual cap ................................... ........................................... 1,893,610 
12 U.S.C. 2609(d)(1) ............................................................... Per failure ................................. ............................................... 89 
12 U.S.C. 2609(d)(1) ............................................................... Annual cap .................................. ............................................ 178,156 
12 U.S.C. 2609(d)(2)(A) .......................................................... Per failure, where intentional ................ .................................. 178 
12 U.S.C. 5113(d)(2) ............................................................... Per violation ............................... .............................................. 27,455 
15 U.S.C. 1639e(k)(1) ............................................................. First violation .............................. ............................................. 10,875 
15 U.S.C. 1639e(k)(2) ............................................................. Subsequent violations ........................ ..................................... 21,749 
(b) The adjustments in paragraph (a) 
of this section shall apply to civil 
penalties assessed after July 14, 2016, regardless of when the violation for which the penalty is assessed occurred. 
Dated: June 7, 2016. 
Richard Cordray, 
Director, Bureau of Consumer Financial 
Protection. 
[FR Doc. 2016–14031 Filed 6–13–16; 8:45 am] 
BILLING CODE 4810–AM–P 
DEPARTMENT OF TRANSPORTATION 
Federal Aviation Administration 
14 CFR Parts 1, 11, 121, 125, and 135 Office of the Secretary 14 CFR Part 382 
[Docket No.: FAA–2014–0554; Amdt. Nos. 
1–69; 11–60; 121–374, 125–65, 135–133] 
RIN 2120–AK32 
Acceptance Criteria for Portable 
Oxygen Concentrators Used On Board Aircraft; Correction 
AGENCY : Federal Aviation 
Administration (FAA) and the Office of the Secretary (OST), Department of Transportation (DOT). 
ACTION : Final rule; correction. 
SUMMARY : This final rule replaces the 
existing process by which the Federal Aviation Administration (Agency or FAA) approves portable oxygen concentrators (POC) for use on board aircraft in air carrier operations, commercial operations, and certain other operations using large aircraft. The FAA currently assesses each POC make and model on a case-by-case basis and if the FAA determines that a particular POC is safe for use on board an aircraft, the FAA conducts rulemaking to identify the specific POC model in an FAA regulation. This final rule replaces the current process and allows passengers to use a POC on board an aircraft if the POC satisfies certain acceptance criteria and bears a label indicating conformance with the acceptance criteria. The labeling requirement only affects POCs intended for use on board aircraft that were not previously approved for use on aircraft by the FAA. Additionally, this rulemaking will eliminate redundant operational requirements and paperwork requirements related to the physician’s statement. As a result, this rulemaking will reduce burdens for POC manufacturers, passengers who use POCs while traveling, and affected aircraft operators. This final rule also makes conforming amendments to the Department of Transportation’s (Department or DOT) rule implementing the Air Carrier Access Act (ACAA) to require carriers to accept all POC models that meet FAA acceptance criteria as detailed in this rule. 
DATES : This correction will become 
effective on June 23, 2016. 
FOR FURTHER INFORMATION CONTACT : For 
technical questions concerning this action, contact DK Deaderick, 121 Air Carrier Operations Branch, Air Transportation Division, Flight Standards Service, Federal Aviation Administration, AFS–220, 800 Independence Avenue SW., Washington, DC 20591; telephone (202) 267–7480; email dk.deaderick@faa.gov. For questions regarding the Department’s disability regulation (14 CFR part 382), contact Clereece Kroha, Senior Attorney, Office of Aviation Enforcement and Proceedings, Department of Transportation, 1200 New Jersey Avenue SE., Washington, DC 20590; telephone (202) 366–9041; email clereece.kroha@dot.gov. 
SUPPLEMENTARY INFORMATION : Background 
On May 24, 2016, the FAA published 
a final rule entitled, ‘‘Acceptance Criteria for Portable Oxygen Concentrators Used On Board Aircraft’’ (81 FR 33098). 
This final rule affects the use of POCs 
on board aircraft in operations conducted under title 14 of the Code of Federal Regulations (14 CFR) parts 121, 125, and 135, by replacing the existing FAA case-by-case approval process for each make and model of POC in Special Federal Aviation Regulation (SFAR) No. 106, with FAA acceptance criteria. Under SFAR No. 106, each time the FAA approves a specific model of POC for use on board aircraft, the agency updates the list of approved POCs in the SFAR. 
This final rule removes SFAR No. 106 
and replaces it with POC acceptance criteria and specific labeling requirements to identify POCs that conform to the acceptance criteria. POCs that conform to the final rule acceptance criteria will be allowed on board aircraft without additional FAA review and rulemaking. 
As with existing requirements for 
FAA approval of POCs that may be used on aircraft, the final rule acceptance criteria and labeling requirement only apply to POCs intended for use on board aircraft. Table 1 provides a comparison of the final rule acceptance criteria and labeling requirement with related SFAR No. 106. 
However, the final rule was published 
with an incorrect amendment number, ‘‘11–59,’’ which is the same amendment number as the rule entitled ‘‘Administrative Practices and Procedures, Reporting and Recordkeeping Requirements ’’ (81 FR 13969), published on March 16, 2016. The correct amendment number for this rule should be ‘‘11–60.’’ 
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Correction 
In FR Doc. 2016–11908 beginning on 
page 33098 in the Federal Register of 
May 24, 2016, make the following correction: 
Correction 
1. On page 33098, in the first column, 
in the document heading, revise 
‘‘[Docket No.: FAA–2014–0554; Amdt. Nos. 1–69, 11–59, 121–374, 125–65, and 135–133]’’ to read ‘‘[Docket No.: FAA– 2014–0554; Amdt. Nos. 1–69, 11–60, 121–374, 125–65, and 135–133]’’. 
Issued under authority provided by 49 
U.S.C. 106(f) in Washington, DC, on June 1, 
2016. 
Dale A. Bouffiou, Acting Director, Office of Rulemaking. 
[FR Doc. 2016–13955 Filed 6–13–16; 8:45 am] 
BILLING CODE 4910–13–P 
DEPARTMENT OF TRANSPORTATION 
Federal Aviation Administration 
14 CFR Part 39 
[Docket No. FAA–2016–6899; Directorate 
Identifier 2016–NM–066–AD; Amendment 39–18558; AD 2016–12–09] 
RIN 2120–AA64 
Airworthiness Directives; Airbus 
Airplanes 
AGENCY : Federal Aviation 
Administration (FAA), Department of Transportation (DOT). 
ACTION : Final rule; request for 
comments. 
SUMMARY : We are superseding 
Airworthiness Directive (AD) 2016–09– 11 for certain Airbus Model A330–200, –200 Freighter, and –300 series airplanes; and Model A340–200 and –300 series airplanes. AD 2016–09–11 required removing fasteners, doing a rototest inspection of fastener holes, installing new fasteners, oversizing the holes and doing rototest inspections for cracks if necessary, and repairing any cracking that is found. This new AD requires the same actions as AD 2016– 09–11, but includes Model A330–300 series airplanes in paragraph (g)(2) of this AD. This AD was prompted by the discovery of missing affected airplanes in paragraph (g)(2) of AD 2016–09–11 that resulted from converting a table in the proposed AD to text in AD 2016–09– 11. We are issuing this AD to detect and correct cracking on certain holes of certain frames of the center wing box (CWB), which could affect the structural integrity of the airplane. DATES : This AD is effective June 29, 
2016. 
The Director of the Federal Register 
approved the incorporation by reference 
of certain publications listed in this AD as of June 13, 2016 (81 FR 27986, May 9, 2016). 
We must receive comments on this 
AD by July 29, 2016. 
ADDRESSES : You may send comments, 
using the procedures found in 14 CFR 11.43 and 11.45, by any of the following methods: 
•Federal eRulemaking Portal: Go to 
http://www.regulations.gov. Follow the 
instructions for submitting comments. 
•Fax: 202–493–2251. 
•Mail: U.S. Department of 
Transportation, Docket Operations, M– 30, West Building Ground Floor, Room W12–140, 1200 New Jersey Avenue SE., Washington, DC 20590. 
•Hand Delivery: U.S. Department of 
Transportation, Docket Operations, M– 30, West Building Ground Floor, Room W12–140, 1200 New Jersey Avenue SE., Washington, DC, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. 
For service information identified in 
this final rule, contact Airbus SAS, Airworthiness Office—EAL, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France; telephone: +33 5 61 93 36 96; fax: +33 5 61 93 45 80; email: airworthiness.A330-A340@airbus.com; Internet: http://www.airbus.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– 6899. 
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– 6899; or in person at the Docket Management Facility between 9 a.m. and 5 p.m., proposed AD, the regulatory evaluation, any comments received, and other information. The street address for the Docket Operations office (telephone: 800–647–5527) is in the 
ADDRESSES  
section. Comments will be available in the AD docket shortly after receipt. 
FOR FURTHER INFORMATION CONTACT : 
Vladimir Ulyanov, Aerospace Engineer, International Branch, ANM–116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057–3356; telephone: 425–227–1138; fax: 425–227–1149. SUPPLEMENTARY INFORMATION : 
Discussion 
On April 21, 2016, we issued AD 
2016–09–11, Amendment 39–18509 (81 FR 27986, May 9, 2016) (‘‘AD 2016–09– 11’’), for certain Airbus Model A330– 200, –200 Freighter, and –300 series airplanes; and Model A340–200 and –300 series airplanes. AD 2016–09–11 was prompted by reports that cracks were found on an adjacent hole of certain frames of the CWB. AD 2016– 09–11 required removing fasteners, doing a rototest inspection of fastener holes, installing new fasteners, oversizing the holes and doing rototest inspections for cracks if necessary, and repairing any cracking that was found. We issued AD 2016–09–11 to detect and correct cracking on certain holes of certain frames of the CWB that could affect the structural integrity of the airplane. 
Since we issued AD 2016–09–11, we 
discovered missing affected airplanes in paragraph (g)(2) of AD 2016–09–11 that resulted from converting a table to text in that AD. We stated in the preamble of AD 2016–09–11 that we revised the format of paragraph (g) of that AD, at the request of the Office of the Federal Register, by converting the table to text. We also stated this change to the format does not affect the requirements of that paragraph. 
However, in converting the table to 
text, we inadvertently omitted Model A330–300 series airplanes from paragraph (g)(2) of AD 2016–09–11. We have changed paragraph (g)(2) of this AD to include Model A330–300 series airplanes. 
The European Aviation Safety Agency 
(EASA), which is the Technical Agent for the Member States of the European Union, has issued EASA Airworthiness Directive 2014–0149, dated June 13, 2014 (referred to after this as the Mandatory Continuing Airworthiness Information, or ‘‘the MCAI’’), to correct an unsafe condition for certain Airbus Model A330–200, –200 Freighter, and –300 series airplanes; and Model A340– 200 and –300 series airplanes. The MCAI states: 
During accomplishment of A330 
Airworthiness Limitation Item (ALI) task 57– 
11–04 on the rear fitting of the Frame (FR) 40 between stringers 38 and 39 on both [left- hand] LH/[right-hand] RH sides, cracks were found on an adjacent hole. After reaming at second oversize of the subject hole, the crack was still present. 
Other crack findings on this adjacent hole 
have been reported on A330 and A340–200/ 
–300 aeroplanes as a result of sampling 
inspections. 
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