Federal Register / Vol. 72, No. 98 / Tuesday, May 22, 2007 / Rules and Regulations 28589 

Other FAA AD Provisions 

(h) The following provisions also apply to 

this AD: 

(1) Alternative Methods of Compliance 

(AMOCs): The Manager, Standards Staff, 

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: Taylor Martin, Aerospace Engineer, 

FAA, Small Airplane Directorate, 901 Locust, 

Room 301, Kansas City, Missouri 64106; 

telephone: (816) 329–4138; 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) AMOCs approved for AD 2003–07–06 

are not approved for this AD. 

(3) 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 FAAapproved 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. 

(4) 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 

(i) Refer to MCAI Civil Aviation Authority 

AD No. G–2004–0029, dated December 20, 

2004; BAE Systems British Aerospace 

Jetstream Series 3100 & 3200 Service Bulletin 

32–JA030644, dated October 6, 2003; BAE 

Systems British Aerospace Jetstream 

Mandatory Service Bulletin 32–JA020741, 

Original Issue: November 2, 2002; APPH Ltd. 

Service Bulletin 32–76, Revision 1, dated 

August 2003; and APPH Ltd. Service Bulletin 

32–76, pages 1, 2, and 4 through 7, dated 

October 2002; and page 3, Erratum 1, dated 

November 2002, for related information. 

Material Incorporated by Reference 

(j) You must use APPH Ltd. Service 

Bulletin 32–76, Revision 1, dated August 

2003; as referenced in BAE Systems British 

Aerospace Jetstream Series 3100 & 3200 

Service Bulletin 32–JA030644, dated October 

6, 2003; and APPH Ltd. Service Bulletin 32–

76, pages 1, 2, and 4 through 7, dated October 

2002; and page 3, Erratum 1, dated November 

2002; as referenced in BAE Systems British 

Aerospace Jetstream Mandatory Service 

Bulletin 32–JA020741, Original Issue: 

November 2, 2002; to do the actions required 

by this AD, unless the AD specifies 

otherwise. 

(1) The Director of the Federal Register 

approved the incorporation by reference of 

APPH Ltd. Service Bulletin 32–76, Revision 

1, dated August 2003; as referenced in BAE 

Systems British Aerospace Jetstream Series 

3100 & 3200 Service Bulletin 32–JA030644, 

dated October 6, 2003, under 5 U.S.C. 552(a) 

and 1 CFR part 51. 

(2) On May 22, 2003 (68 FR 16195, April 

3, 2003), the Director of the Federal Register 

approved the incorporation by reference of 

APPH Ltd. Service Bulletin 32–76, pages 1, 

2, and 4 through 7, dated October 2002; and 

page 3, Erratum 1, dated November 2002, as 

referenced in BAE Systems British Aerospace 

Jetstream Mandatory Service Bulletin 32–

JA020741, Original Issue: November 2, 2002. 

(3) For service information identified in 

this AD, contact BAE Systems, Prestwick 

International Airport, Ayshire, KA9 2RW, 

Scotland; telephone: (01292) 675207; fax: 

(01292) 675704. 

(4) You may review copies at the FAA, 

Central Region, Office of the Regional 

Counsel, 901 Locust, Room 506, Kansas City, 

Missouri 64106; or 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/ 

cfr/ibr-locations.html. 

Issued in Kansas City, Missouri, on May 9, 

2007. 

Charles L. Smalley, 

Acting Manager, Small Airplane Directorate, 

Aircraft Certification Service. 

[FR Doc. 07–2522 Filed 5–21–07; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2006–26112; Directorate 

Identifier 2006–NE–35–AD; Amendment 39–

14837; AD 2006–24–08] 

RIN 2120–AA64 

Airworthiness Directives; Pratt & 

Whitney Canada (P&WC) PW535A 

Turbofan Engines; Correction 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule; correction. 

SUMMARY: The FAA is correcting 

airworthiness directive (AD) 2006–24–

08. That AD applies to Pratt & Whitney 

Canada (P&WC) PW535A turbofan 

engines. We published that AD in the 

Federal Register on December 4, 2006 

(71 FR 70284). The fuel manifold part 

number (P/N) 3025267–01 listed in 

paragraph (c) is incorrect. This 

document corrects that P/N. In all other 

respects, the original document remains 

the same. 

EFFECTIVE DATE: Effective May 22, 2007. 

FOR FURTHER INFORMATION CONTACT: Ian 

Dargin, Aerospace Engineer, Engine 

Certification Office, FAA, Engine & 

Propeller Directorate, 12 New 

EnglandExecutive Park, Burlington, MA, 

01803; telephone (781) 238–7178; fax 

(781) 238–7199. 

SUPPLEMENTARY INFORMATION: On 

December 4, 2006 (71 FR 70284), we 

published a final rule AD, FR Doc, E6–

20204, in the Federal Register. That AD 

applies to P&WC PW535A turbofan 

engines. We need to make the following 

correction: 

§ 39.13 [Corrected] 

On page 70286, in the second column, 

in paragraph (c), in the fourth line, 

‘‘3025267–01’’ is corrected to read 

‘‘3052627–01’’. 

Issued in Burlington, Massachusetts, on 

May 14, 2007. 

Peter A. White, 

Acting Manager, Engine and Propeller 

Directorate, Aircraft Certification Service. 

[FR Doc. E7–9719 Filed 5–21–07; 8:45 am] 

BILLING CODE 4910–13–P 

DEPARTMENT OF TRANSPORTATION 

Federal Aviation Administration 

14 CFR Part 39 

[Docket No. FAA–2005–22430; Directorate 

Identifier 2005–NE–34–AD; Amendment 39–

15063; AD 2007–11–06] 

RIN 2120–AA64 

Airworthiness Directives; Turbomeca 

Arrius 2F Turboshaft Engines 

AGENCY: Federal Aviation 

Administration (FAA), Department of 

Transportation (DOT). 

ACTION: Final rule. 

SUMMARY: The FAA is superseding an 

existing airworthiness directive (AD) for 

Turbomeca Arrius 2F turboshaft 

engines. That AD currently requires 

removing from service certain serial 

number (SN) fuel control units (FCUs) 

or replacing the constant delta pressure 

(delta P) diaphragm in those FCUs. This 

AD requires replacing all FCUs not 

incorporating modification Tf 55 with 

FCUs that incorporate modification Tf 

55. This AD results from the European 

Aviation Safety Agency (EASA) and 

Turbomeca expanding the applicability 

to the full population of FCUs installed 

on Arrius 2F turboshaft engines. FCUs 

not incorporating modification Tf 55 are 

susceptible to having an improperly 

assembled constant delta P diaphragm. 

We are issuing this AD to prevent an 

uncommanded engine in-flight 

shutdown on a single-engine helicopter, 

resulting in a forced autorotation 

landing or an accident. 

DATES: This AD becomes effective June 

26, 2007. 

ADDRESSES: You can get the service 

information identified in this AD from 


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