Federal Register / Vol. 75, No. 142 / Monday, July 26, 2010 / Rules and Regulations 43397 

Actions and Compliance 

(f) Unless already done, do the following 

actions: 

(1) Before further flight as of April 6, 2010 

(the effective date of AD 2010–08–01), 

inspect the elevator inner hinges on the 

stabilizer following paragraphs A.1., A.2., 

and A.4. of Aircraft Industries, a.s. 

Mandatory Bulletin MB No.: L23/052a, dated 

March 2, 2010. 

(2) Repetitively thereafter at intervals not 

to exceed every 1,000 hours time-in-service, 

inspect the elevator inner hinges on the 

stabilizer following paragraphs A.1., A.2., 

and A.4. of Aircraft Industries, a.s. 

Mandatory Bulletin MB No.: L23/052a, dated 

March 2, 2010. 

(3) If, as a result of the inspection required 

by paragraph (f)(1) or (f)(2) of this AD, you 

find any elevator inner hinge on the elevator 

is cracked or damaged, before further flight, 

replace it following paragraphs A.3. and A.4. 

of Aircraft Industries, a.s. Mandatory Bulletin 

MB No.: L23/052a, dated March 2, 2010. 

FAA AD Differences 

Note: This AD differs from the MCAI and/ 

or service information as follows: No 

differences. 

Other FAA AD Provisions 

(g) The following provisions also apply to 

this AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, Standards Office, 

FAA, has the authority to approve AMOCs 

for this AD, if requested using the procedures 

found in 14 CFR 39.19. Send information to 

ATTN: Greg Davison, Aerospace Engineer, 

FAA, Small Airplane Directorate, 901 Locust, 

Room 301, Kansas City, Missouri 64106; 

telephone: (816) 329–4130; fax: (816) 329– 

4090. Before using any approved AMOC on 

any airplane to which the AMOC applies, 

notify your appropriate principal inspector 

(PI) in the FAA Flight Standards District 

Office (FSDO), or lacking a PI, your local 

FSDO. 

(2) Airworthy Product: For any requirement 

in this AD to obtain corrective actions from 

a manufacturer or other source, use these 

actions if they are FAA-approved. Corrective 

actions are considered FAA-approved if they 

are approved by the State of Design Authority 

(or their delegated agent). You are required 

to assure the product is airworthy before it 

is returned to service. 

(3) Reporting Requirements: For any 

reporting requirement in this AD, under the 

provisions of the Paperwork Reduction Act 

(44 U.S.C. 3501 et seq.), the Office of 

Management and Budget (OMB) has 

approved the information collection 

requirements and has assigned OMB Control 

Number 2120–0056. 

Related Information 

(h) Refer to MCAI EASA Emergency AD 

No.: 2010–0037–E, dated March 8, 2010; and 

Aircraft Industries, a.s. Mandatory Bulletin 

MB No.: L23/052a, dated March 2, 2010, for 

related information. 

Material Incorporated by Reference 

(h) You must use Aircraft Industries, a.s. 

Mandatory Bulletin MB No.: L23/052a, dated 

March 2, 2010, to do the actions required by 

this AD, unless the AD specifies otherwise. 

(1) On April 26, 2010 (75 FR 17295, April 

6, 2010), the Director of the Federal Register 

previously approved the incorporation by 

reference of Aircraft Industries, a.s. 

Mandatory Bulletin MB No.: L23/052a, dated 

March 2, 2010. 

(2) For service information identified in 

this AD, contact Aircraft Industries, a.s.– 

Naza ́honech1177, 686 04 Kunovice, Czech 

Republic; telephone: +420 572 817 660; fax: 

+420 572 816 112; e-mail: ots@let.cz; 

Internet: http://www.let.cz. 

(3) You may review copies of the service 

information incorporated by reference for 

this AD at the FAA, Central Region, Office of 

the Regional Counsel, 901 Locust, Kansas 

City, Missouri 64106. For information on the 

availability of this material at the Central 

Region, call (816) 329–3768. 

(4) You may also review copies of the 

service information incorporated by reference 

for this AD at the National Archives and 

Records Administration (NARA). For 

information on the availability of this 

material at NARA, call (202) 741–6030, or go 

to: http://www.archives.gov/federal_register/

code_of_federal_regulations/ibr_

locations.html. 

Issued in Kansas City, Missouri, on July 15, 

2010. 

Kim Smith, 

Manager, Small Airplane Directorate, Aircraft 

Certification Service. 

[FR Doc. 2010–18022 Filed 7–23–10; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2010–0122; Directorate 

Identifier 2009–CE–067–AD; Amendment 

39–16338; AD 2010–13–07] 

RIN 2120–AA64 

Airworthiness Directives; Piper 

Aircraft, Inc. Models PA–32R–301T and 

PA–46–350P Airplanes 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule; correction. 

SUMMARY: This document makes a 

correction to AD 2010–13–07, which 

was published in the Federal Register 

on June 23, 2010 (75 FR 35619), and 

applies to certain Piper Aircraft, Inc. 

Models PA–32R–301T and PA–46–350P 

airplanes. AD 2010–13–07 requires you 

to replace V-band exhaust couplings, 

part number (P/N) Lycoming 40D21162– 

340M or Eaton/Aeroquip 55677–340M 

with an improved design Eaton/ 

Aeroquip P/N NH1009399–10 or 

Lycoming P/N 40D23255–340M. In the 

Summary and Discussion sections of the 

published AD, we incorrectly stated that 

the AD requires replacing any spotwelded, V-band exhaust coupling with 

a riveted, V-band exhaust coupling 

instead of stating the specific P/N to be 

replaced. Also, in the Cost of 

Compliance section, we incorrectly 

stated that Model PA–32R–301T 

airplanes, instead of Model PA–46–350P 

airplanes, are equipped with two of the 

affected V-band clamps. We are issuing 

this document to help eliminate any 

confusion that this AD may have 

created. 

DATES: The effective date of this 

correction is July 26, 2010. The effective 

date of this AD (2010–13–07) remains 

July 28, 2010. 

FOR FURTHER INFORMATION CONTACT: 

Darby Mirocha, Aerospace Engineer, 

FAA, Atlanta Aircraft Certification 

Office (ACO), 1701 Columbia Avenue, 

College Park, Georgia 30337; telephone: 

(404) 474–5573; fax: (404) 474–5606; email: darby.mirocha@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Discussion 

On June 14, 2010, the FAA issued AD 

2010–13–07, Amendment 39–16338 (75 

FR 35619, June 23, 2010), which applies 

to certain Piper Aircraft, Inc. Models 

PA–32R–301T and PA–46–350P 

airplanes. AD 2010–13–07 requires you 

to replace V-band exhaust couplings, P/ 

N Lycoming 40D21162–340M or Eaton/ 

Aeroquip 55677–340M with an 

improved design Eaton/Aeroquip P/N 

NH1009399–10 or Lycoming P/N 

40D23255–340M. 

In the published AD, we incorrectly 

stated in the the Summary and 

Discussion sections that the AD requires 

replacing any spot-welded, V-band 

exhaust coupling with a riveted, V-band 

exhaust coupling instead of stating the 

specific P/N to be replaced. Also, in the 

Cost of Compliance section, we 

incorrectly stated which of the affected 

model airplanes are equipped with two 

of the affected V-band clamps. 

Need for the Correction 

This correction is needed to help 

eliminate any confusion that this AD 

may have created. 

Correction of Publication 

Accordingly, the publication of June 

23, 2010 (75 FR 35619), of Amendment 

39–16338; AD 2010–13–07, which was 

the subject of FR Doc. 2010–14991, is 

corrected as follows: 

On page 35619, under the heading 

‘‘Summary,’’ in line 5, change the word 

‘‘any’’ to ‘‘specific.’’ 

On page 35620, under the heading 

‘‘Discussion,’’ in line 11, change the 

word ‘‘any’’ to ‘‘specific.’’ 


wwoods2 on DSK1DXX6B1PROD with RULES_PART 1
43398 Federal Register / Vol. 75, No. 142 / Monday, July 26, 2010 / Rules and Regulations 

On page 35620, under the heading 

‘‘Comments,’’ under the subheading 

‘‘Comment Issue No. 2: Correct the Cost 

of Compliance,’’ in paragraph 3, change 

the second sentence to ‘‘After further 

research, we determined that Model 

PA–46–350P (Mirage) has two of the 

affected V-Band clamps installed, and 

Model PA–32R–301T (Saratoga II TC) 

has one.’’ 

On page 35620, under the heading 

‘‘Costs of Compliance,’’ change the entire 

section to read as follows: 

‘‘We estimate that this AD affects 596 

airplanes in the U.S. registry provided 

they have the affected V-band exhaust 

coupling installed. 

We estimate the following costs to do 

the replacement for Model PA–32R– 

301T airplanes. These airplanes have 

one V-band clamp installed: 

Labor cost Parts cost 

Total cost 

per Model 

PA–32R– 

301T 

airplane 

2 work-hours × $85 per hour = $170 .............................................................................................................................. $714 $884 

We estimate the following costs to do 

the replacement for Model PA–46–350P 

airplanes. These airplanes have two Vband clamps installed: 

Labor cost Parts cost 

Total cost 

per Model 

PA–46– 

350P 

airplane 

2 work-hours per V-band clamp. 2 clamps per airplane: 4 work-hours × $85 per hour 

= $340.

$714 per V-band clamp. $714 × 2 = 

$1,428.

$1,768 

The effective date of this AD (2010– 

13–07) remains July 28, 2010. 

Issued in Kansas City, Missouri, on July 15, 

2010. 

Kim Smith, 

Manager, Small Airplane Directorate, Aircraft 

Certification Service. 

[FR Doc. 2010–18023 Filed 7–23–10; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 73 

[Docket No. FAA–2008–1261; Airspace 

Docket No. 06–ASO–18] 

Amendment and Establishment of 

Restricted Areas and Other Special 

Use Airspace, Avon Park Air Force 

Range, FL 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule, correction. 

SUMMARY: This action makes minor 

corrections to the geographic 

coordinates of restricted areas R–2901B, 

R–2910J, R–2901K, R–2901L and R– 

2901N, Avon Park, FL, in a final rule 

published in the Federal Register on 

Monday, May 24, 2010. The National 

Aeronautical Navigation Services Office 

requested these adjustments be made to 

better align the restricted areas. 

DATES: Effective date 0901 UTC, July 29, 

2010. The Director of the Federal 

Register approves this incorporation by 

reference action under 1 CFR part 51, 

subject to the annual revision of FAA 

Order 7400.9 and publication of 

conforming amendments. 

FOR FURTHER INFORMATION CONTACT: Paul 

Gallant, Airspace and Rules Group, 

Office of System Operations Airspace 

and AIM, Federal Aviation 

Administration, 800 Independence 

Avenue, SW., Washington, DC 20591; 

telephone: (202) 267–8783. 

SUPPLEMENTARY INFORMATION: 

History 

On May 24, 2010, a final rule was 

published in the Federal Register (75 

FR 28752), Airspace Docket No. 06– 

ASO–18, to modify the special use 

airspace at the Avon Park Air Force 

Range in Florida. As a result of further 

review of the latitude/longitude 

coordinates for the Avon Park Air Force 

Range restricted areas, the Aeronautical 

Navigation Services Office (formerly the 

National Aeronautical Charting Office) 

determined that a minor refinement was 

needed for two points in several 

restricted area descriptions. The 

correction adjusts the longitude 

coordinate by six seconds for one point 

and by two seconds for the second 

point. Specifically, the longitude point 

in lat. 27°32′31′′ N., long. 81°07′ 29′′ W., 

is corrected to read ‘‘long. 81°07′23′′ W.′′, 

and; the longitude point in lat. 

27°29′31′′ N., long. 81°05′29′′ W., is 

corrected to read ‘‘long. 81°05′27′′ W’’ 

List of Subjects in 14 CFR Part 73 

Airspace, Prohibited Areas, Restricted 

Areas. 

Correction to Final Rule 

■ Accordingly, pursuant to the authority 

delegated to me, the legal descriptions 

of R–2901B, R–2901J, R–2901K, R– 

2901L, and R–2901N, as published in 

the Federal Register on May 24, 2010 

(75 FR 28752), Airspace Docket 06– 

ASO–18, and incorporated by reference 

in 14 CFR part 73, is corrected as 

follows: 

§ 73.29 [Amended] 

On page 28755, column 2, correct two 

coordinates for restricted areas R–2901B 

and R–2910J; and on page 28756, 

columns 1 and 2, correct two 

coordinates for restricted areas 

R–2901K, R–2901L and R–2901N, Avon 

Park, FL, to read as follows: 

* * * * * 

R–2901B Avon Park, FL [Corrected] 

By removing lat. 27°32′31′′ N., long. 

81°07′29′′ W., and substituting lat. 27°32′21′′ 

N., long. 81°07′23′′ W.; and by removing lat. 

27°29′31′′ N., long. 81°05′29′′ W., and 

substituting lat. 27°29′31′′ N., long. 81°05′27′′ 

W. 

R–2901J Avon Park, FL [Corrected] 

By removing lat. 27°32′31′′ N., long. 

81°07′29′′ W., and substituting lat. 27°32′21′′ 

N., long. 81°07′23′′ W.; and by removing lat. 

27°29′31′′ N., long. 81°05′29′′ W., and 


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