Airworthiness Directives; Pratt & Whitney Canada (P&WC) PW535A Turbofan Engines; Correction, 28589 [E7-9719]
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Federal Register / Vol. 72, No. 98 / Tuesday, May 22, 2007 / Rules and Regulations
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.
cprice-sewell on PRODPC61 with RULES
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.
VerDate Aug<31>2005
15:01 May 21, 2007
Jkt 211001
(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: https://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
[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
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; correction.
AGENCY:
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.
Frm 00003
Fmt 4700
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:
SUPPLEMENTARY INFORMATION:
§ 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
14 CFR Part 39
PO 00000
28589
Sfmt 4700
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
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
E:\FR\FM\22MYR1.SGM
22MYR1
]]>Agencies
[Federal Register Volume 72, Number 98 (Tuesday, May 22, 2007)]
[Rules and Regulations]
[Page 28589]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E7-9719]
-----------------------------------------------------------------------
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:
Sec. 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
