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

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 


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