Amendment to the Privacy of Consumer Financial Information Rule Under the Gramm-Leach-Bliley Act, 38410 [C1-2015-14328]

Download as PDF 38410 Federal Register / Vol. 80, No. 128 / Monday, July 6, 2015 / Proposed Rules (a) Comments Due Date We must receive comments by August 20, 2015. (b) Affected ADs None. (c) Applicability This AD applies to all The Boeing Company Model 767–200, –300, –300F, and –400ER series airplanes, certificated in any category. (d) Subject Air Transport Association (ATA) of America Code 53, Fuselage. (e) Unsafe Condition This AD was prompted by reports of cracking at the station (STA 786) ring chord at the tension bolt hole common to the wing front spar lower chord and the internal bathtub fittings. We are issuing this AD to detect and correct fatigue cracking of the hidden fuselage skin and cracking, corrosion, and other damage to the splice fittings and adjacent visible fuselage skin and structure that could lead to loss of a primary load path between the fuselage and the wing box, and consequent reduced structural integrity of the airplane. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Inspection Lhorne on DSK7TPTVN1PROD with PROPOSALS At the applicable time specified in paragraph 1.E., ‘‘Compliance,’’ of Boeing Alert Service Bulletin 767–53A0263, dated January 12, 2015, except as required by paragraph (h) of this AD, do external ultrasonic and detailed inspections to detect cracking, corrosion, or other damage at the splice fitting location, in accordance with the Accomplishment Instructions of Boeing Alert Service Bulletin 767–53A0263, dated January 12, 2015. (1) If cracking, corrosion, or other damage is not found, repeat the inspections at intervals not to exceed 6,000 flight cycles or 18,000 flight hours, whichever occurs first. Accomplishing a repair as specified in paragraph (g)(2) of this AD terminates the repetitive inspections in the repaired area only. (2) If any cracking, corrosion, or other damage is found, before further flight, repair using a method approved in accordance with the procedures specified in paragraph (i) of this AD. The repetitive inspections of paragraph (g)(1) are terminated in the repaired area only. (h) Exceptions to Service Information Specifications Where Boeing Alert Service Bulletin 767– 53A0263, dated January 12, 2015, specifies a compliance time ‘‘after the original issue date of this Service Bulletin,’’ this AD requires compliance within the specified compliance time after the effective date of this AD. VerDate Sep<11>2014 14:36 Jul 02, 2015 Jkt 235001 (i) Alternative Methods of Compliance (AMOCs) (1) The Manager, Seattle 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 paragraph (j)(1) of this AD. Information may be emailed to: 9-ANM-Seattle-ACO-AMOCRequests@faa.gov. (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. (3) An AMOC that provides an acceptable level of safety may be used for any repair required by this AD if it is approved by the Boeing Commercial Airplanes Organization Designation Authorization (ODA) that has been authorized by the Manager, Seattle ACO, to make those findings. For a repair method to be approved, the repair must meet the certification basis of the airplane, and the approval must specifically refer to this AD. (4) For service information that contains steps that are labeled as Required for Compliance (RC), the provisions of paragraphs (i)(4)(i) and (i)(4)(ii) apply. (i) The steps labeled as RC, including substeps under an RC step and any figures identified in an RC step, must be done to comply with the AD. An AMOC is required for any deviations to RC steps, including substeps and identified figures. (ii) Steps not labeled as RC may be deviated from using accepted methods in accordance with the operator’s maintenance or inspection program without obtaining approval of an AMOC, provided the RC steps, including substeps and identified figures, can still be done as specified, and the airplane can be put back in an airworthy condition. (j) Related Information (1) For more information about this AD, contact Wayne Lockett, Aerospace Engineer, Airframe Branch, ANM–120S, FAA, Seattle Aircraft Certification Office (ACO), 1601 Lind Avenue SW., Renton, WA 98057–3356; phone: 425–917–6447; fax: 425–917–6590; email: wayne.lockett@faa.gov. (2) For service information identified in this AD, contact Boeing Commercial Airplanes, Attention: Data & Services Management, P.O. Box 3707, MC 2H–65, Seattle, WA 98124–2207; telephone 206– 544–5000, extension 1; fax 206–766–5680; Internet https://www.myboeingfleet.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. PO 00000 Frm 00005 Fmt 4702 Sfmt 4702 Issued in Renton, Washington, on June 24, 2015. Dionne Palermo, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2015–16296 Filed 7–2–15; 8:45 am] BILLING CODE 4910–13–P FEDERAL TRADE COMMISSION 16 CFR Part 313 RIN 3084–AB42 Amendment to the Privacy of Consumer Financial Information Rule Under the Gramm-Leach-Bliley Act Correction In proposed rule document 2015– 14328 beginning on page 36267 in the issue of Wednesday, June 24, 2015, make the following correction: On page 36268, in the first column, in the second full paragraph, in the second line, ‘‘August 17, 2015’’ should read ‘‘August 31, 2015’’. [FR Doc. C1 2015–14328 Filed 7–2–15; 8:45 am] BILLING CODE 1505–01–D DEPARTMENT OF HOUSING AND URBAN DEVELOPMENT 24 CFR Part 203 [Docket No. FR–5742–P–01] RIN 2502–AJ23 Federal Housing Administration (FHA): Single Family Mortgage Insurance Maximum Time Period for Filing Insurance Claims, Curtailment of Interest and Disallowance of Operating Expenses Incurred Beyond Certain Established Timeframes Office of the Assistant Secretary for Housing—Federal Housing Commissioner, HUD. ACTION: Proposed rule. AGENCY: This proposed rule would establish the maximum time period within which an FHA-approved mortgagee must file a claim with FHA for insurance benefits. HUD’s current regulations are silent with respect to a deadline by which a claim for insurance benefits must be filed with FHA. Due to the downturn in the housing market, which resulted in a significant increase in mortgage defaults, some mortgagees have refrained from promptly filing claims for insurance benefits and instead have opted to wait and file multiple claims with FHA at a single point in time. The uncertainty regarding a deadline by which a claim must be SUMMARY: E:\FR\FM\06JYP1.SGM 06JYP1

Agencies

[Federal Register Volume 80, Number 128 (Monday, July 6, 2015)]
[Proposed Rules]
[Page 38410]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: C1-2015-14328]


-----------------------------------------------------------------------

FEDERAL TRADE COMMISSION

16 CFR Part 313

RIN 3084-AB42


Amendment to the Privacy of Consumer Financial Information Rule 
Under the Gramm-Leach-Bliley Act

Correction

    In proposed rule document 2015-14328 beginning on page 36267 in the 
issue of Wednesday, June 24, 2015, make the following correction:
    On page 36268, in the first column, in the second full paragraph, 
in the second line, ``August 17, 2015'' should read ``August 31, 
2015''.

[FR Doc. C1-2015-14328 Filed 7-2-15; 8:45 am]
 BILLING CODE 1505-01-D