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1) Federal Register / Vol. 80, No. 217 / Tuesday, November 10, 2015 / Rules and Regulations within 10 days of completion of the APHIS/ CDC Form 2. * * * * * [FR Doc. 2015–28575 Filed 11–9–15; 8:45 am] BILLING CODE 6450–01–P BUREAU OF CONSUMER FINANCIAL PROTECTION 12 CFR Part 1003 [Docket No. CFPB–2014–0019] RIN 3170–AA10 Home Mortgage Disclosure (Regulation C) Correction In rule document 2015–26607 beginning on page 66128 in the issue of Wednesday, October 28, 2015, make the following corrections: 1. On page 66256, in the second column, in the nineteenth line, ‘‘I. Effective Date’’ should read ‘‘VI. Effective Date.’’ 2. On page 66296, in the third column, in the fourteenth and fifteenth lines, ‘‘III. Final Regulatory Flexibility Act Analysis’’ should read ‘‘VIII. Final Regulatory Flexibility Act Analysis’’. 3. On page 66305, in the first column, in the 23rd line, ‘‘IV. Paperwork Reduction Act’’ should read ‘‘IX. Paperwork Reduction Act’’. [FR Doc. C1–2015–26607 Filed 11–9–15; 8:45 am] BILLING CODE 1505–01–D DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 25 [Docket No. FAA–2015–4086; Special Conditions No. 25–605–SC] Special Conditions: Boeing Model 787– 9 Airplane; Structure-Mounted Airbags Federal Aviation Administration (FAA), DOT. ACTION: Final special conditions; request for comments. AGENCY: These special conditions are issued for the Boeing Model 787–9 airplane. This airplane will have a novel or unusual design feature when compared to the state of technology envisioned in the airworthiness standards for transport-category airplanes. This design feature is airbags mounted to structure to prevent serious injury. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this rmajette on DSK2TPTVN1PROD with RULES SUMMARY: VerDate Sep<11>2014 17:21 Nov 09, 2015 Jkt 238001 design feature. These special conditions contain the additional safety standards that the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards. DATES: This action is effective on Boeing on November 10, 2015. We must receive your comments by December 28, 2015 using any of the following methods: • Federal eRegulations Portal: Go to http://www.regulations.gov/and follow the online instructions for sending your comments electronically. • Mail: Send comments to Docket Operations, M–30, U.S. Department of Transportation (DOT), 1200 New Jersey Avenue SE., Room W12–140, West Building Ground Floor, Washington, DC, 20590–0001. • Hand Delivery or Courier: Take comments to Docket Operations in Room W12–140 of the West Building Ground Floor at 1200 New Jersey Avenue SE., Washington, DC, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. • Fax: Fax comments to Docket Operations at 202–493–2251. Privacy: The FAA will post all comments it receives, without change, to http://www.regulations.gov/, including any personal information the commenter provides. Using the search function of the docket Web site, anyone can find and read the electronic form of all comments received into any FAA docket, including the name of the individual sending the comment (or signing the comment for an association, business, labor union, etc.). DOT’s complete Privacy Act Statement can be found in the Federal Register published on April 11, 2000 (65 FR 19477–19478), as well as at http:// DocketsInfo.dot.gov/. Docket: Background documents or comments received may be read at http://www.regulations.gov/ at any time. Follow the online instructions for accessing the docket or go to Docket Operations in Room W12–140 of the West Building Ground Floor at 1200 New Jersey Avenue SE., Washington, DC, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. FOR FURTHER INFORMATION CONTACT: Jeff Gardlin, FAA, Airframe and Cabin Safety Branch, ANM–115, Transport Airplane Directorate, Aircraft Certification Service, 1601 Lind Avenue SW., Renton, Washington 98057–3356; telephone 425–227–2136; facsimile 425–227–1232. SUPPLEMENTARY INFORMATION: The FAA has determined that notice of, and opportunity for prior public comment on, these special conditions is PO 00000 Frm 00005 Fmt 4700 Sfmt 4700 69567 impracticable because these procedures would significantly delay issuance of the design approval and thus delivery of the affected airplane. In addition, the substance of these special conditions has been subject to the public comment process in prior instances with no substantive comments received. The FAA therefore finds that good cause exists for making these special conditions effective upon publication in the Federal Register. Comments Invited We invite interested people to take part in this rulemaking by sending written comments, data, or views. The most helpful comments reference a specific portion of the special conditions, explain the reason for any recommended change, and include supporting data. We will consider all comments we receive by the closing date for comments. We may change these special conditions based on the comments we receive. Background On July 5, 2009, The Boeing Company applied for a change to type certificate no. T00021SE for structure-mounted airbags in the Model 787–9 airplane. The Model 787–9 airplane, which is a derivative of the Model 787 series currently approved under type certificate no. T00021SE, has a maximum passenger capacity of 420 passengers and a maximum takeoff weight of 557,000 lbs. Type Certification Basis Under the provisions of Title 14, Code of Federal Regulations (14 CFR) 21.101, The Boeing Company must show that the 787–9, as changed, continues to meet the applicable provisions of the regulations reference listed in type certificate no. T00021SE or the applicable regulations in effect on the date of application for the change, except for earlier amendments as agreed upon by the FAA. The certification basis includes certain special conditions, exemptions, or later amended sections of the applicable part that are not relevant to these special conditions. If the Administrator finds that the applicable airworthiness regulations (i.e., 14 CFR part 25) do not contain adequate or appropriate safety standards for the Model 787–9 airplane because of a novel or unusual design feature, special conditions are prescribed under the provisions of § 21.16. Special conditions are initially applicable to the model for which they are issued. Should the type certificate E:\FR\FM\10NOR1.SGM 10NOR1