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contains regulatory documents having general

applicability and legal effect, most of which

are keyed to and codified in the Code of

Federal Regulations, which is published under

50 titles pursuant to 44 U.S.C. 1510.

The Code of Federal Regulations is sold by

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Rules and Regulations Federal Register

42949 

Vol. 77, No. 141 

Monday, July 23, 2012 

EXPORT-IMPORT BANK OF THE 

UNITED STATES 

12 CFR Part 404 

[EXIM–OIG–2012–0010] 

RIN 3048–AA02 

Privacy Act of 1974: Implementation of 

Exemptions; Export-Import Bank of the 

United States Office of Inspector 

General—EIB–35—Office of Inspector 

General Investigative Records; 

Correction 

AGENCY: Office of the Inspector General, 

Export-Import Bank of the United 

States. 

ACTION: Final rule; correction. 

SUMMARY: The Export-Import Bank of 

the United States (hereafter known as 

‘‘Ex-Im Bank’’) published in the Federal 

Register of July 17, 2012, a final rule to 

exempt portions of a system of records 

from one or more provisions of the 

Privacy Act. This document corrects an 

inaccurate amendatory instruction. 

DATES: Effective August 16, 2012. 

FOR FURTHER INFORMATION CONTACT: 

Osvaldo Gratacos, Ex-Im Bank, Office of 

Inspector General, 811 Vermont Avenue 

NW., Rm. 976, Washington, DC 20571 or 

by telephone (202) 565–3908 or 

facsimile (202) 565–3988. 

SUPPLEMENTARY INFORMATION: The Ex-Im 

Bank published a document on July 17, 

2012 (77 FR 41885–41886) exempting 

portions of a system of records entitled 

‘‘EIB–35—Office of Inspector General 

Investigative Records’’ from one or more 

provisions of the Privacy Act. The 

document incorrectly added § 404.24 to 

subpart B of 12 CFR part 404. Section 

404.24 currently exists in subpart C. The 

instruction should have revised 404.24, 

not added it. 

Accordingly, in rule FR Doc. 2012– 

17382 published on July 17, 2012 (77 FR 

41885–41886), make the following 

correction. 

1. On page 41886, in the first column, 

amendatory instruction 2 is corrected to 

read as follows: 

‘‘2. Section 404.24 is revised to read 

as follows:’’ 

Dated: July 17, 2012. 

Sharon A. Whitt, 

Agency Clearance Officer. 

[FR Doc. 2012–17896 Filed 7–20–12; 8:45 am] 

BILLING CODE 6690–01–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 23 

[Docket No. FAA–2012–0485; Special 

Conditions No. 23–258–SC] 

Special Conditions: Tamarack 

Aerospace Group, Cirrus Model SR22; 

Active Technology Load Alleviation 

System (ATLAS) 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final special conditions. 

SUMMARY: These special conditions are 

issued for the Tamarack Aerospace 

Group’s modification to the Cirrus SR22 

airplane. This airplane as modified by 

Tamarack will have a novel or unusual 

design feature(s) associated with 

Tamarack Aerospace Group’s 

modification. The design change will 

install winglets and an Active 

Technology Load Alleviation system 

(ATLAS). The addition of the ATLAS 

mitigates the negative effects of the 

winglets by effectively aerodynamically 

turning off the winglet under limit gust 

and maneuver loads. This is 

accomplished by measuring the aircraft 

loading and moving a small aileron-like 

device called a Tamarack Active Control 

Surface (TACS). The TACS movement 

reduces lift at the tip of the wing, 

resulting in the wing center of pressure 

moving inboard, thus reducing bending 

stresses along the wing span. The 

applicable airworthiness regulations do 

not contain adequate or appropriate 

safety standards for this 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: Effective Date: July 13, 2013. 

FOR FURTHER INFORMATION CONTACT: For 

sections 23.301 through 23.629 

(structural requirements), contact Mr. 

Mike Reyer, telephone (816) 329–4131. 

For sections 23.672 through 23.701 

(control system requirements), contact 

Mr. Ross Schaller, telephone (816) 329– 

4162. The address and facsimile for both 

Mr. Reyer and Mr. Schaller is: Small 

Airplane Directorate, Aircraft 

Certification Service, 901 Locust, 

Kansas City, Missouri 64106; facsimile 

(816) 329–4090. 

SUPPLEMENTARY INFORMATION: 

Background 

On February 15, 2011, Tamarack 

Aerospace Group applied for a 

supplemental type certificate for 

installation of winglets and an Active 

Technology Load Alleviation System 

(ATLAS) on the Cirrus Model SR22 

(serial numbers 0002–2333, 2335–2419, 

and 2421–2437). The Cirrus Model SR22 

is a certified, single reciprocating 

engine, four-passenger, composite 

airplane. 

The installation of winglets, as 

proposed by Tamarack, increases 

aerodynamic efficiency. However, the 

winglets by themselves also increase 

wing static loads and the wing fatigue 

stress ratio, which under limit gust and 

maneuver loads factors may exceed the 

certificated wing design limits. The 

addition of ATLAS mitigates the 

negative effects of the winglets by 

effectively aerodynamically turning off 

the winglet at elevated gust and 

maneuver loads factors. 

The ATLAS functions as a load-relief 

system. This is accomplished by 

measuring aircraft loading via an 

accelerometer, and by moving a small 

aileron-like device called a Tamarack 

Active Control Surface (TACS) that 

reduces lift at the tip of the wing. 

Because the ATLAS compensates for the 

increased wing root bending at elevated 

load factors, the overall effect of this 

modification is that the winglet can be 

added to the Cirrus wing without the 

traditionally required reinforcement of 

the existing structure. This is the first 

application of an active loads alleviation 

system on a part 23 aircraft and the 

applicable airworthiness regulations do 

not contain adequate or appropriate 

safety standards for this design feature. 

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