This section of the FEDERAL REGISTER

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

the Superintendent of Documents. Prices of

new books are listed in the first FEDERAL

REGISTER issue of each week.

Rules and Regulations Federal Register

1009 

Vol. 77, No. 5 

Monday, January 9, 2012 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2010–0710; Directorate 

Identifier 2010–NE–26–AD; Amendment 39– 

16892; AD 2010–19–06R1] 

RIN 2120–AA64 

Airworthiness Directives; Turbomeca 

Turboshaft Engines 

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 Turbomeca Arriel 1 series 

turboshaft engines. The AD number is 

incorrect in the preamble and in the 

Regulatory text. This document corrects 

those errors. In all other respects, the 

original document remains the same. 

DATES: This final rule revision is 

effective January 17, 2012. 

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: 

Frederick Zink, Aerospace Engineer, 

Engine Certification Office, FAA, 12 

New England Executive Park, 

Burlington, MA; phone: (781) 238–7779; 

fax: (781) 238–7199; email: 

frederick.zink@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Airworthiness Directive 2011–26–02, 

Amendment 39–16892 (76 FR 77378, 

December 13, 2011), currently requires 

removing from service certain gas 

generator second stage turbine discs, 

part number (P/N) 0 292 25 040 0, that 

are not marked with ‘‘CFR’’ before the 

discs exceed 4,000 cycles-in-service 

(CIS) since new. That AD also requires 

removing from service certain gas 

generator second stage turbine discs, 

P/N 0 292 25 040 0, that are marked 

with ‘‘CFR’’ before the discs exceed 

6,500 CIS since new. 

As published, the AD number 2011– 

26–02 in the preamble of the AD and 

under § 39.13 [Amended], is incorrect. 

No other part of the preamble or 

regulatory information has been 

changed; therefore, only the changed 

portion of the final rule is being 

published in the Federal Register. 

The effective date of this AD revision 

remains January 17, 2012. 

Correction of Non-Regulatory Text 

In the Federal Register of December 

13, 2011, AD 2011–26–02; Amendment 

39–16892 is corrected as follows: 

On page 77378, in the second column, 

on line 3 under 14 CFR Part 39, change 

AD 2011–26–02 to AD 2010–19–06R1. 

Correction of Regulatory Text 

§ 39.13 [Corrected] 

■ In the Federal Register of December 

13, 2011, on page 77379, in the second 

column, lines 6 and 7 under § 39.13 

[Amended] of AD 2011–26–02, are 

corrected to read as follows: 

* * * * * 

AD 2010–19–06R1 Turbomeca: 

Amendment 39–16892; Docket No. 

FAA–2010–0710; 

* * * * * 

Issued in Burlington, Massachusetts, on 

December 29, 2011. 

Peter A. White, 

Manager, Engine & Propeller Directorate, 

Aircraft Certification Service. 

[FR Doc. 2012–79 Filed 1–6–12; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2009–0162; Directorate 

Identifier 2004–NE–19–AD; Amendment 39– 

16803; AD 2011–18–21] 

RIN 2120–AA64 

Airworthiness Directives; Rolls-Royce 

plc (RR) RB211–524 Series Turbofan 

Engines 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: We are superseding an 

existing airworthiness directive (AD) for 

the products listed above. That AD 

currently requires initial and repetitive 

borescope inspections of the head 

section and meterpanel assembly of the 

combustion liner, and replacement if 

necessary. This new AD requires those 

same inspections, and replacement. 

This AD also expands the applicability 

to include part numbers (P/N) of 

additional combustion liners. This AD 

was prompted by an inquiry submitted 

by an operator, which resulted in RR 

performing a complete review of the 

affected front combustion liner part 

numbers. We are issuing this AD to 

prevent deterioration of the engine 

combustion liner, which can result in 

combustion liner breakup, case burnthrough, engine fire, and damage to the 

airplane. 

DATES: This AD is effective February 13, 

2012. 

The Director of the Federal Register 

approved the incorporation by reference 

of certain publications listed in this AD 

as of February 9, 2005 (70 FR 680, 

January 5, 2005). 

ADDRESSES: For service information 

identified in this AD, contact RollsRoyce plc, P.O. Box 31, Derby, DE24 

8BJ, United Kingdom; phone: 011–44– 

1332–242424; fax: 011–44–1332– 

249936, for the service information 

identified in this proposed AD. You 

may review copies of the referenced 

service information at the FAA, Engine 

& Propeller Directorate, 12 New England 

Executive Park, Burlington, MA. For 

information on the availability of this 

material at the FAA, call (781) 238– 

7125. 


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1010 Federal Register / Vol. 77, No. 5 / Monday, January 9, 2012 / Rules and Regulations 

Examining the AD Docket 

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: 

Alan Strom, Aerospace Engineer, Engine 

Certification Office, FAA, 12 New 

England Executive Park, Burlington, MA 

01803; phone: (781) 238–7143; fax: (781) 

238–7199; email: alan.strom@faa.gov. 

SUPPLEMENTARY INFORMATION: 

Discussion 

We issued a supplemental notice of 

proposed rulemaking (SNPRM) to 

amend 14 CFR part 39 to supersede 

airworthiness directive (AD) 2004–26– 

05, amendment 39–13917 (70 FR 680, 

January 5, 2005). That AD applies to the 

specified products. The SNPRM 

published in the Federal Register on 

October 18, 2010 (75 FR 63727). The 

SNPRM proposed to require: 

• Initial and repetitive borescope 

inspections of the combustion liner 

head section and meterpanel assembly 

of the combustion liner and, if 

necessary, replacement. 

• Reduction of the inspection 

intervals of certain RB211–524 engine 

models that have not been repaired to 

RR Field Repair Scheme FRS5367/B, 

and 

• A mandatory terminating action to 

the repetitive inspections to be 

completed no later than December 31, 

2012. 

Comments 

We gave the public the opportunity to 

participate in developing this AD. We 

have considered the comment received. 

The Boeing Company supports the 

SNPRM published in the Federal 

Register on October 18, 2010 (75 FR 

63727). 

We simplified wording for clarity in 

the regulatory section. We did not 

change the requirements of this AD. 

Conclusion 

We reviewed the relevant data, 

considered the comments received, and 

determined that air safety and the 

public interest require adopting the AD 

as proposed. 

Costs of Compliance 

We estimate that this AD will affect 

18 engines installed on airplanes of U.S. 

registry. We also estimate that it will 

take about 32 work-hours per engine to 

perform the required actions, and that 

the average labor rate is $85 per workhour. Required parts will cost about 

$231,000. Based on these figures, we 

estimate the total cost of the AD to U.S. 

operators to be $4,206,960. 

Authority for This Rulemaking 

Title 49 of the United States Code 

specifies the FAA’s authority to issue 

rules on aviation safety. Subtitle I, 

Section 106, describes the authority of 

the FAA Administrator. Subtitle VII, 

Aviation Programs, describes in more 

detail the scope of the Agency’s 

authority. 

We are issuing this rulemaking under 

the authority described in subtitle VII, 

part A, subpart III, section 44701, 

‘‘General requirements.’’ Under that 

section, Congress charges the FAA with 

promoting safe flight of civil aircraft in 

air commerce by prescribing regulations 

for practices, methods, and procedures 

the Administrator finds necessary for 

safety in air commerce. This regulation 

is within the scope of that authority 

because it addresses an unsafe condition 

that is likely to exist or develop on 

products identified in this rulemaking 

action. 

Regulatory Findings 

We have determined that this AD will 

not have federalism implications under 

Executive Order 13132. This AD will 

not have a substantial direct effect on 

the States, on the relationship between 

the national government and the States, 

or on the distribution of power and 

responsibilities among the various 

levels of government. 

For the reasons discussed above, I 

certify that this AD: 

(1) Is not a ‘‘significant regulatory 

action’’ under Executive Order 12866, 

(2) Is not a ‘‘significant rule’’ under 

DOT Regulatory Policies and Procedures 

(44 FR 11034, February 26, 1979), 

(3) Will not affect intrastate aviation 

in Alaska, and 

(4) Will not have a significant 

economic impact, positive or negative, 

on a substantial number of small entities 

under the criteria of the Regulatory 

Flexibility Act. 

List of Subjects in 14 CFR Part 39 

Air transportation, Aircraft, Aviation 

safety, Incorporation by reference, 

Safety. 

Adoption of the Amendment 

Accordingly, under the authority 

delegated to me by the Administrator, 

the FAA amends 14 CFR part 39 as 

follows: 

PART 39—AIRWORTHINESS 

DIRECTIVES 

■ 1. The authority citation for part 39 

continues to read as follows: 

Authority: 49 U.S.C. 106(g), 40113, 44701. 

§ 39.13 [Amended] 

■ 2. The FAA amends § 39.13 by 

removing airworthiness directive (AD) 

2004–26–05, Amendment 39–13917 (70 

FR 680, January 5, 2005), and adding the 

following new AD: 

2011–18–21 Rolls-Royce plc: Amendment 

39–16803; Docket No. FAA–2009–0162; 

Directorate Identifier 2004–NE–19–AD. 

(a) Effective Date 

This airworthiness directive (AD) is 

effective February 13, 2012. 

(b) Affected ADs 

This AD supersedes AD 2004–26–05, 

Amendment 39–13917 (70 FR 680, January 5, 

2005). 

(c) Applicability 

This AD applies to Rolls-Royce plc (RR) 

engine models RB211–524B–02, –524B3–02 

engines and RB211–524B2, –524B4, –524C2, 

and –524D4 series engines with a front 

combustion liner assembly that incorporates 

RR Service Bulletin (SB) No. RB.211–72– 

7221 or RR SB No. RB.211–72–7998, but 

doesn’t incorporate RR SB No. RB.211–72– 

9670 or RR SB No. RB.211–72–9764, and 

engine models RB211–524G and –524H 

series engines with a front combustion liner 

assembly that doesn’t incorporate RR SB No. 

RB.211–72–9764. 

(d) Unsafe Condition 

This AD results from an inquiry submitted 

by an operator which resulted in RR 

performing a complete review of the affected 

front combustion liner part numbers. We are 

issuing this AD to prevent deterioration of 

the engine combustion liner, which can 

result in combustion liner breakup, case 

burn-through, engine fire, and damage to the 

airplane. 

(e) Compliance 

You are responsible for having the actions 

required by this AD performed within the 

compliance times specified unless the 

actions have already been done. 

(f) Credit for Previous Inspections 

Engine inspections previously done using 

RR SB No. RB.211–72–B482, Revision 8, 

meet the requirements of this AD for the 

initial and repetitive inspections specified in 

paragraph (g) and Table 1 of this AD; and 

paragraph (h) and Table 2 of this AD. 


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Federal Register / Vol. 77, No. 5 / Monday, January 9, 2012 / Rules and Regulations 1011 

(g) Inspections of Combustion Liner Head 

Sections—Not Previously Repaired 

Borescope-inspect combustion liner head 

sections that have not been previously 

repaired. Use paragraphs 3.A.(1) through 

3.A.(5) of the Accomplishment Instructions 

of RR Alert Service Bulletin (ASB) No. 

RB.211–72–AB482, Revision 9, dated July 28, 

2003, and the compliance thresholds in Table 

1 of this AD to do the inspections. 

TABLE 1—COMBUSTION LINER HEAD SECTION—NOT PREVIOUSLY REPAIRED

Engine series Initial inspection Repetitive inspection Parts exceeding initial inspection 

cycles 

RB211–524C2, –524D4, –524G, 

and –524H.

Within 1,400 to 1,600 cyclessince-new (CSN).Within 200 cycles-since-last inspection (CSLI).Within 100 cycles-in-service (CIS) 

after the effective date of this 

AD. 

RB211–524B–02, –524B2, 

–524B3–02, and –524B4.

Within 3,000 to 3,200 CSN .......... Within 200 CSLI ........................... Within 200 CIS after the effective 

date of this AD. 

(h) Inspections of Combustion Liner Head 

Sections—Previously Repaired Using RR 

Field Repair Scheme FRS5367/B 

Borescope-inspect combustion liner head 

sections previously repaired using RR Field 

Repair Scheme FRS5367/B. Use paragraphs 

3.A.(1) through 3.A.(5) of the 

Accomplishment Instructions of RR ASB No. 

RB.211–72–AB482, Revision 9, dated July 28, 

2003, and the compliance thresholds in Table 

2 of this AD to do the inspections. 

TABLE 2—COMBUSTION LINER HEAD SECTION—PREVIOUSLY REPAIRED USING RR FIELD REPAIR SCHEME FRS5367/B 

Engine series Initial inspection Repetitive inspection Parts exceeding initial inspection 

cycles 

RB211–524C2, –524D4, –524G, 

and –524H.

Within 1,800 to 2,200 cyclessince-last repair (CSLR).Within 400 CSLI ........................... Within 200 CIS after the effective 

date of this AD. 

RB211–524B–02, –524B2, 

–524B3–02, and –524B4.

Within 3,000 to 3,200 CSLR ........ Within 400 CSLI ........................... Within 200 CIS after the effective 

date of this AD. 

(i) Inspections of Combustion Liner Head 

Sections That Have Been Repaired But Did 

Not Use RR Field Repair Scheme 

FRS5367/B 

Borescope-inspect combustion liner head 

sections that have been repaired using a 

method other than RR Field Repair Scheme 

FRS5367/B. Use paragraphs 3.A.(1) through 

3.A.(5) of the Accomplishment Instructions 

of RR ASB No. RB.211–72–AB482, Revision 

9, dated July 28, 2003, and the compliance 

thresholds in Table 3 of this AD to do the 

inspections. 

TABLE 3—COMBUSTION LINER HEAD SECTION—REPAIRED, BUT DID NOT USE RR FIELD REPAIR SCHEME FRS5367/B 

Engine series Initial inspection Repetitive inspection Parts exceeding initial inspection 

cycles 

RB211–524C2, –524D4, –524G, 

and –524H.

Within 500 to 700 CSLR .............. Within 200 CSLI ........................... Within 100 CIS after the effective 

date of this AD. 

RB211–524B–02, –524B2, 

–524B3–02, and -524B4.

Within 2,000 to 2,200 CSLR ........ Within 200 CSLI ........................... Within 200 CIS after the effective 

date of this AD. 

(1) For an installed front combustion liner 

that is subject to RR ASB No. RB.211–72– 

AB482, Revision 9, dated July 28, 2003, if the 

nicrobraze repair RR Field Repair Scheme 

FRS5367 has been applied to all 18 struts, 

then that repair is equivalent to compliance 

with RR Field Repair Scheme FRS5367/B. 

(2) Head sections repaired by replacement 

of all 18 struts using RR Field Repair Scheme 

FRS6548 are considered as equivalent to 

fitting a new head section for inspection 

purposes. 

(j) Inspections of Meterpanel Assemblies— 

Not Repaired 

Borescope-inspect meterpanel assemblies 

that incorporate SB No. RB.211–72–7998, 

that have not been previously repaired. Use 

paragraphs 3.B.(1) through 3.B.(7) of the 

Accomplishment Instructions of RR ASB No. 

RB.211–72–AB482, Revision 9, dated July 28, 

2003, and the compliance thresholds in Table 

4 of this AD to do the inspections. 

TABLE 4—METERPANEL ASSEMBLY—NOT REPAIRED

Engine series Initial inspection Repetitive inspection Parts exceeding initial inspection 

cycles 

RB211–524D4, –524G, and –524H Within 1,000 to 1,200 CSN .......... Within 400 CSLI ........................... Within 50 CIS after the effective 

date of this AD. 

RB211–524D4, –524G, and –524H 

that have not used RB211–524H 

ratings at any time.

Within 1,800 to 2,000 CSN .......... Within 400 CSLI ........................... Within 50 CIS after the effective 

date of this AD. 


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1012 Federal Register / Vol. 77, No. 5 / Monday, January 9, 2012 / Rules and Regulations 

(k) Inspections of Meterpanel Assemblies— 

Repaired 

Borescope-inspect meterpanel assemblies 

that incorporate SB No. RB.211–72–7998, 

that have been previously repaired. Use 

paragraphs 3.B.(1) through 3.B.(7) of the 

Accomplishment Instructions of RR ASB No. 

RB.211–72–AB482, Revision 9, dated July 28, 

2003, and the compliance thresholds in Table 

5 of this AD to do the inspections. 

TABLE 5—METERPANEL ASSEMBLY—REPAIRED

Engine series Initial inspection Repetitive inspection Parts exceeding initial inspection 

cycles 

RB211–524D4, –524G, and 

–524H..

Within 500 to 700 CSLR .............. Within 400 CSLI ........................... Within 50 CIS after the effective 

date of this AD. 

(l) Reject Parts 

Remove from service, parts that exceed the 

acceptance criteria. 

(m) Mandatory Terminating Action 

Replace any front combustion liner 

assembly that has a P/N listed in paragraph 

(c) of this AD at the next shop visit. 

(1) For RB211–524B–02, –524B3–02, 

–524B4, –524C2 and –524B2, –524B4, 

–524C2, and –524D4 series engines, replacing 

the front combustion liner assembly with a 

front combustion liner assembly that 

incorporates the modifications in RR SB No. 

RB.211–72–9670, Original Issue, dated 

August 27, 1993; or RR SB No. RB.211–72– 

9764, Revision 3, dated January 16, 1998, 

constitutes terminating action to the 

repetitive inspections in paragraphs (g), (h), 

(i), (j), and (k) of this AD. 

(2) For RB211–524G and –524H engines, 

replacing the front combustion liner 

assembly with a front combustion liner 

assembly that incorporates the modifications 

in RR SB No. RB.211–72–9764, Revision 3, 

dated January 16, 1998, constitutes 

terminating action to the repetitive 

inspections in paragraphs (f), (g), (h), (i), and 

(j) of this AD. 

(n) Definition of Shop Visit 

For the purpose of this AD, a shop visit is 

any time that the 04 module is removed for 

refurbishment or overhaul. 

(o) Related Information 

Contact Alan Strom, Aerospace Engineer, 

Engine Certification Office, FAA, 12 New 

England Executive Park, Burlington, MA 

01803; phone: (781) 238–7143; fax: (781) 

238–7199; email: alan.strom@faa.gov, for 

more information about this AD. 

(p) Material Incorporated by Reference 

You must use the following service 

information to do the actions required by this 

AD, unless the AD specifies otherwise. The 

Director of the Federal Register approved the 

incorporation by reference (IBR) of the 

following service information under 5 U.S.C. 

552(a) and 1 CFR part 51 on the date 

specified: 

(1) Rolls-Royce plc Alert Service Bulletin 

No. RB.211–72–AB482, Revision 9, July 28, 

2003, approved for IBR February 9, 2005 (70 

FR 680, January 5, 2005). 

(2) Rolls-Royce plc Service Bulletin No. 

RB.211–72–9670, Original Issue, August 27, 

1993, approved for IBR February 9, 2005 (70 

FR 680, January 5, 2005). 

(3) Rolls-Royce plc Service Bulletin No. 

RB.211–72–9764, Revision 3, January 16, 

1998, approved for IBR February 9, 2005 (70 

FR 680, January 5, 2005). 

(4) For service information identified in 

this AD, contact Rolls-Royce plc, P.O. Box 

31, Derby, DE24 8BJ, United Kingdom; 

phone: 011–44–1332–242424; fax: 011–44– 

1332–249936. 

(5) You may review copies of the service 

information at the FAA, Engine & Propeller 

Directorate, 12 New England Executive Park, 

Burlington, MA. For information on the 

availability of this material at the FAA, call 

(781) 238–7125. 

(6) You may also review copies of the 

service information that is incorporated by 

reference at the National Archives and 

Records Administration (NARA). For 

information on the availability of this 

material at an NARA facility, call (202) 741– 

6030, or go to http://www.archives.gov/ 

federal_register/code_of_federal_regulations/ 

ibr_locations.html. 

Issued in Burlington, Massachusetts, on 

December 28, 2011. 

Peter A. White, 

Manager, Engine & Propeller Directorate, 

Aircraft Certification Service. 

[FR Doc. 2012–134 Filed 1–6–12; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 71 

[Docket No. FAA–2011–0540; Airspace 

Docket No. 11–ASO–20] 

Establishment of Class E Airspace; 

Inverness, FL 

AGENCY: Federal Aviation 

Administration (FAA), DOT. 

ACTION: Final rule. 

SUMMARY: This action establishes Class 

E Airspace at Inverness, FL, to 

accommodate the new Area Navigation 

(RNAV) Global Positioning System 

(GPS) Standard Instrument Approach 

Procedures serving Inverness Airport. 

This action enhances the safety and 

airspace management of Instrument 

Flight Rules (IFR) operations within the 

National Airspace System. This action 

also makes a minor adjustment to the 

geographic coordinates of the airport. 

DATES: Effective 0901 UTC, April 5, 

2012. The Director of the Federal 

Register approves this incorporation by 

reference action under title 1, Code of 

Federal Regulations, part 51, subject to 

the annual revision of FAA Order 

7400.9 and publication of conforming 

amendments. 

FOR FURTHER INFORMATION CONTACT: John 

Fornito, Operations Support Group, 

Eastern Service Center, Federal Aviation 

Administration, P.O. Box 20636, 

Atlanta, Georgia 30320; telephone (404) 

305–6364. 

SUPPLEMENTARY INFORMATION: 

History 

On October 28, 2011, the FAA 

published in the Federal Register a 

notice of proposed rulemaking to 

establish Class E airspace at Inverness, 

FL (76 FR 66871) Docket No. FAA– 

2011–0540. Interested parties were 

invited to participate in this rulemaking 

effort by submitting written comments 

on the proposal to the FAA. No 

comments were received. Subsequent to 

publication, the FAA found that the 

geographic coordinates for Inverness 

Airport needed to be adjusted. This 

action makes that adjustment. Class E 

airspace designations are published in 

paragraph 6005 of FAA Order 7400.9V 

dated August 9, 2011, and effective 

September 15, 2011, which is 

incorporated by reference in 14 CFR 

71.1. The Class E airspace designations 

listed in this document will be 

published subsequently in the Order. 

The Rule 

This amendment to Title 14, Code of 

Federal Regulations (14 CFR) part 71 

establishes the Class E airspace 

extending upward from 700 feet above 

the surface at Inverness, FL to provide 

the controlled airspace required to 

accommodate the new Area Navigation 

(RNAV) Global Positioning System 

(GPS) Standard Instrument Approach 

Procedures developed for Inverness 

Airport. This action is necessary for the 

safety and management of IFR 

operations at the airport. This action 

also adjusts the geographic coordinates 


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