### 12991 Federal Register / Vol. 77, No. 43 / Monday, March 5, 2012 / Rules and Regulations

Issued in Renton, Washington, on February 14, 2012. Kalene C. Yanamura, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service.
[FR Doc. 2012–4498 Filed 3–2–12; 8:45 am]

**BILLING CODE 4910–13–P**

**DEPARTMENT OF TRANSPORTATION**

**Federal Aviation Administration**

**14 CFR Part 39**

**[Docket No. FAA–2011–1420; Directorate Identifier 2011–CE–035–AD; Amendment**  **39–16905; AD 2011–27–04]**

**RIN 2120–AA64**

**Airworthiness Directives; Hawker Beechcraft Corporation Airplanes**  **Equipped With a Certain Supplemental Type Certificate (STC)** 

**AGENCY :**  Federal Aviation Administration (FAA), DOT.

**ACTION :**  Final rule; correction.

**SUMMARY :**  The FAA is correcting an airworthiness directive (AD) that published in the Federal Register. That AD applies to all Hawker Beechcraft Corporation Models 95–C55, D55, E55, 58, and 58A airplanes equipped with a certain STC. The description of the affected STCs in the first sentence of the

**SUPPLEMENTARY INFORMATION** , Discussion section, is incorrect. This document corrects that error. In all other respects, the original document remains the

same.

**DATES :**  This final rule is effective March 5, 2012. The effective date for AD 2011– 27–04 (76 FR 81790, December 29, 2011) remains December 29, 2011.

**ADDRESSES :**  You may examine the AD docket on the Internet at http:// www.regulations.gov; 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 address for the Docket Office (phone: 800–647–5527) is Document 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 :**  Eric B. Potter, Aerospace Engineer, Atlanta Aircraft Certification Office, FAA, 1701 Columbia Avenue, College Park, Georgia 30337; phone: (404) 474–5583; fax: (404) 474–5606; email: eric.potter@faa.gov. **SUPPLEMENTARY INFORMATION :**  Airworthiness Directive 2011–27–04, amendment 39–16905 (76 FR 81790, December 29, 2011), currently requires assuring the airspeed indicator(s) and/or airspeed limitations placard(s) have the correct minimum control speed (VMC) markings for all Hawker Beechcraft Corporation Models 95–C55, D55, E55, 58, and 58A airplanes equipped with a certain STC.

As published, the description of the affected STCs in the first sentence of the

**SUPPLEMENTARY INFORMATION** , Discussion section, is incorrect.

No other part of the preamble or regulatory information has been changed; therefore, only the changed portion of the preamble to the final rule is being published in the Federal Register

.

The effective date of this AD remains December 29, 2011. Correction of Non-Regulatory Text

In the Federal Register of December 29, 2011, AD 2011–27–04; Amendment 39–16905 is corrected as follows:

On page 81790, in the third column, on line 2 under the heading

**SUPPLEMENTARY INFORMATION**
, Discussion, correct ‘‘, we found that STC SA1762SO (installation of vortex generators) and STC SA4016NM (Foxstar Baron modification of winglets and different engines and propellers) were installed.’’ to read ‘‘, we found that STC SA1762SO (Foxstar Baron modification of winglets and different engines and propellers) and STC SA4016NM (installation of vortex generators) were installed.’’

Issued in Kansas City, Missouri, on February 23, 2012. John Colomy, Acting Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 2012–5290 Filed 3–2–12; 8:45 am]

**BILLING CODE 4910–13–P**

**DEPARTMENT OF TRANSPORTATION**

**Federal Aviation Administration**

**14 CFR Part 39**

**[Docket No. FAA–2011–0588; Directorate Identifier 2010–SW–074–AD; Amendment**  **39–16717; AD 2011–12–10]**

**RIN 2120–AA64**

**Airworthiness Directives; Robinson Helicopter Company Helicopters** 

**AGENCY :**  Federal Aviation Administration (FAA), DOT.

**ACTION :**  Final rule; correction. **SUMMARY :**  The FAA is correcting an airworthiness directive (AD) that was published in the Federal Register. That AD applies to Robinson Helicopter Company (Robinson) Model R22, R22 Alpha, R22 Beta, R22 Mariner, R44, and R44 II helicopters. The paragraph reference in paragraph (b) of the Compliance section is incorrect. Paragraph (b) references paragraph (d), when it should reference paragraph (c). This document corrects that error. Additionally, the word ‘‘inspection’’ has been added in paragraph (b) for clarification. In all other respects, the original document remains the same.

**DATES :**  The effective date of this final rule is March 5, 2012. The effective date for AD 2011–12–10 remains July 5,
2011.

Examining the AD Docket: You may examine the AD docket on the Internet
at http://www.regulations.gov; or in person at the Docket Operations Office between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this AD, any incorporated-by-reference service information, the economic evaluation, any comments received, and other information. The street address for the Docket Operations Office (phone: 800– 647–5527) is U.S. Department of Transportation, Docket Operations Office, M–30, West Building Ground Floor, Room W12–140, 1200 New Jersey Avenue SE., Washington, DC 20590.

**FOR FURTHER INFORMATION CONTACT :**  Eric D. Schrieber, Aerospace Engineer, Los Angeles Aircraft Certification Office, Transport Airplane Directorate, FAA, 3960 Paramount Blvd., Lakewood, CA 90712; telephone (562) 627–5348; email eric.schrieber@faa.gov (regarding Model R22 helicopters); or Fred Guerin, Aerospace Engineer, Los Angeles Aircraft Certification Office, Transport Airplane Directorate, FAA, 3960 Paramount Blvd., Lakewood, CA 90712; telephone (562) 627–5232; email fred.guerin@faa.gov (regarding Model R44 helicopters).

**SUPPLEMENTARY INFORMATION :**  Airworthiness Directive 2011–12–10, Amendment 39–16717 (76 FR 35330, June 17, 2011), currently includes the following paragraph (b) in the compliance section:

‘‘(b) If you find any bare metal in the area of the skin-to-spar bond line, before further flight, inspect the blade by following the requirements of paragraph (d) of this AD.’’

As published, the reference to paragraph (d) is incorrect. The correct reference is to paragraph (c). Paragraph (c) contains the inspection requirements, and the incorrect