Airworthiness Directives; Aerospatiale Model ATR42-500 Airplanes, 57126 [05-19555]
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57126
Federal Register / Vol. 70, No. 189 / Friday, September 30, 2005 / Rules and Regulations
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2005–22406; Directorate
Identifier 2002–NM–242–AD; Amendment
39–14270; AD 2005–19–05]
RIN 2120–AA64
Airworthiness Directives; Aerospatiale
Model ATR42–500 Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; correction.
AGENCY:
SUMMARY: The FAA is correcting a
typographical error in an existing
airworthiness directive (AD) that was
published in the Federal Register on
September 14, 2005 (70 FR 54249). The
error resulted in an incorrect Docket No.
This AD applies to certain Aerospatiale
Model ATR42–500 airplanes. This AD
requires inspecting for correct
installation of the fastener that attaches
the ground braids on the elevator,
modifying the forward bonded assembly
of the elevator control rod, and
corrective action if necessary.
DATES: Effective September 29, 2005.
ADDRESSES: The AD docket contains the
proposed AD, comments, and any final
disposition. You may examine the AD
docket on the Internet at https://
dms.dot.gov, or in person at the Docket
Management Facility office between 9
a.m. and 5 p.m., Monday through
Friday, except Federal holidays. The
Docket Management Facility office
(telephone (800) 647–5227) is located on
the plaza level of the Nassif Building at
the U.S. Department of Transportation,
400 Seventh Street, SW., room PL–401,
Washington, DC. This docket number is
FAA–2005–22406; the directorate
identifier for this docket is 2002–NM–
242–AD.
FOR FURTHER INFORMATION CONTACT: Dan
Rodina, Aerospace Engineer,
International Branch, ANM–116,
Transport Airplane Directorate, FAA,
1601 Lind Avenue, SW., Renton,
Washington 98055–4056; telephone
(425) 227–2125; fax (425) 227–1149.
SUPPLEMENTARY INFORMATION: On
September 6, 2005, the FAA issued AD
2005–19–05, amendment 39–14270 (70
FR 54249, September 14, 2005), for
certain Aerospatiale Model ATR42–500
airplanes. This AD requires inspecting
for correct installation of the fastener
that attaches the ground braids on the
elevator, modifying the forward bonded
assembly of the elevator control rod,
and corrective action if necessary.
VerDate Aug<31>2005
15:28 Sep 29, 2005
Jkt 205001
As published, that AD specifies an
incorrect Docket No. (i.e., FAA–2005–
20406) throughout preamble and the
regulatory text of the AD. The correct
Docket No. is FAA–2005–22406.
No other part of the regulatory
information has been changed;
therefore, the final rule is not
republished in the Federal Register.
The effective date of this AD remains
September 29, 2005.
§ 39.13
[Corrected]
I In the Federal Register of September
14, 2005, on page 54250, in the third
column, paragraph 2. of PART 39—
AIRWORTHINESS DIRECTIVES of AD
2005–19–05 is corrected to read as
follows:
*
*
*
*
*
2005–19–05 Aerospatiale: Amendment 39–
14270. Docket No. FAA–2005–22406;
Directorate Identifier 2002–NM–242–AD.
*
*
*
*
*
Issued in Renton, Washington, on
September 26, 2005.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 05–19555 Filed 9–29–05; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2005–22404; Directorate
Identifier 2005–NM–018–AD; Amendment
39–14268; AD 2005–19–03]
RIN 2120–AA64
Airworthiness Directives; BAe
Systems (Operations) Limited Model
ATP Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; correction.
AGENCY:
SUMMARY: The FAA is correcting a
typographical error in an existing
airworthiness directive (AD) that was
published in the Federal Register on
September 13, 2005 (70 FR 53915). The
error resulted in an incorrect Docket No.
This AD applies to all BAe Systems
(Operations) Limited Model ATP
airplanes. This AD requires revising the
Airworthiness Limitations Section of
the Instructions for Continued
Airworthiness to incorporate life limits
for certain items and new inspections to
detect fatigue cracking in certain
structures and of certain significant
structural items, and to revise life limits
PO 00000
Frm 00006
Fmt 4700
Sfmt 4700
for certain equipment and various
components.
DATES: Effective September 28, 2005.
ADDRESSES: The AD docket contains the
proposed AD, comments, and any final
disposition. You may examine the AD
docket on the Internet at https://
dms.dot.gov, or in person at the Docket
Management Facility office between 9
a.m. and 5 p.m., Monday through
Friday, except Federal holidays. The
Docket Management Facility office
(telephone (800) 647–5227) is located on
the plaza level of the Nassif Building at
the U.S. Department of Transportation,
400 Seventh Street, SW., room PL–401,
Washington, DC. This docket number is
FAA–2005–22404; the directorate
identifier for this docket is 2005–NM–
018–AD.
FOR FURTHER INFORMATION CONTACT:
Todd Thompson, Aerospace Engineer,
International Branch, ANM–116, FAA,
Transport Airplane Directorate, 1601
Lind Avenue, SW., Renton, Washington
98055–4056; telephone (425) 227–1175;
fax (425) 227–1149.
SUPPLEMENTARY INFORMATION: On
September 6, 2005, the FAA issued AD
2005–19–03, amendment 39–14268 (70
FR 53915, September 13, 2005), for all
BAe Systems (Operations) Limited
Model ATP airplanes. The AD requires
revising the Airworthiness Limitations
Section of the Instructions for
Continued Airworthiness to incorporate
life limits for certain items and new
inspections to detect fatigue cracking in
certain structures and of certain
significant structural items, and to
revise life limits for certain equipment
and various components.
As published, that AD specifies an
incorrect Docket No. (i.e., FAA–2005–
20404) throughout preamble and the
regulatory text of the AD. The correct
Docket No. is FAA–2005–22404.
No other part of the regulatory
information has been changed;
therefore, the final rule is not
republished in the Federal Register.
The effective date of this AD remains
September 28, 2005.
§ 39.13
[Corrected]
I In the Federal Register of September
13, 2005, on page 53916, in the third
column, paragraph 2. of PART 39—
AIRWORTHINESS DIRECTIVES of AD
2005–19–03 is corrected to read as
follows:
*
*
*
*
*
2005–19–03 BAe Systems (Operations)
Limited (Formerly British Aerospace
Regional Aircraft): Amendment 39–
14268. Docket No. FAA–2005–22404;
Directorate Identifier 2005–NM–018–AD.
*
E:\FR\FM\30SER1.SGM
*
*
30SER1
*
*
]]>Agencies
[Federal Register Volume 70, Number 189 (Friday, September 30, 2005)]
[Rules and Regulations]
[Page 57126]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 05-19555]
[[Page 57126]]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2005-22406; Directorate Identifier 2002-NM-242-AD;
Amendment 39-14270; AD 2005-19-05]
RIN 2120-AA64
Airworthiness Directives; Aerospatiale Model ATR42-500 Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; correction.
-----------------------------------------------------------------------
SUMMARY: The FAA is correcting a typographical error in an existing
airworthiness directive (AD) that was published in the Federal Register
on September 14, 2005 (70 FR 54249). The error resulted in an incorrect
Docket No. This AD applies to certain Aerospatiale Model ATR42-500
airplanes. This AD requires inspecting for correct installation of the
fastener that attaches the ground braids on the elevator, modifying the
forward bonded assembly of the elevator control rod, and corrective
action if necessary.
DATES: Effective September 29, 2005.
ADDRESSES: The AD docket contains the proposed AD, comments, and any
final disposition. You may examine the AD docket on the Internet at
https://dms.dot.gov, or in person at the Docket Management Facility
office between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The Docket Management Facility office (telephone (800) 647-
5227) is located on the plaza level of the Nassif Building at the U.S.
Department of Transportation, 400 Seventh Street, SW., room PL-401,
Washington, DC. This docket number is FAA-2005-22406; the directorate
identifier for this docket is 2002-NM-242-AD.
FOR FURTHER INFORMATION CONTACT: Dan Rodina, Aerospace Engineer,
International Branch, ANM-116, Transport Airplane Directorate, FAA,
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425)
227-2125; fax (425) 227-1149.
SUPPLEMENTARY INFORMATION: On September 6, 2005, the FAA issued AD
2005-19-05, amendment 39-14270 (70 FR 54249, September 14, 2005), for
certain Aerospatiale Model ATR42-500 airplanes. This AD requires
inspecting for correct installation of the fastener that attaches the
ground braids on the elevator, modifying the forward bonded assembly of
the elevator control rod, and corrective action if necessary.
As published, that AD specifies an incorrect Docket No. (i.e., FAA-
2005-20406) throughout preamble and the regulatory text of the AD. The
correct Docket No. is FAA-2005-22406.
No other part of the regulatory information has been changed;
therefore, the final rule is not republished in the Federal Register.
The effective date of this AD remains September 29, 2005.
Sec. 39.13 [Corrected]
0
In the Federal Register of September 14, 2005, on page 54250, in the
third column, paragraph 2. of PART 39--AIRWORTHINESS DIRECTIVES of AD
2005-19-05 is corrected to read as follows:
* * * * *
2005-19-05 Aerospatiale: Amendment 39-14270. Docket No. FAA-2005-
22406; Directorate Identifier 2002-NM-242-AD.
* * * * *
Issued in Renton, Washington, on September 26, 2005.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 05-19555 Filed 9-29-05; 8:45 am]
BILLING CODE 4910-13-P
