Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-135 Airplanes, and Model EMB-145, -145ER, -145MR, -145LR, -145XR, -145MP, and -145EP Airplanes, 41948 [05-14169]
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Federal Register / Vol. 70, No. 139 / Thursday, July 21, 2005 / Rules and Regulations
circuit as of the effective date of this AD:
Within 3 days or 20 flight hours after
performing any maintenance that would
normally require bleeding of the blue
hydraulic circuit (as instructed by the related
AMM procedure), bleed the blue hydraulic
circuit by accomplishing all the actions
specified in Airbus AOT A320–29A1112,
Revision 01, dated April 8, 2004.
DEPARTMENT OF TRANSPORTATION
Replacement of AGCM and Reducer
RIN 2120–AA64
(h) Within 35 months after the effective
date of this AD, replace the AGCM with a
modified and reidentified AGCM; and
replace the reducer with a new reducer if
applicable; in accordance with the
Accomplishment Instructions of Airbus
Service Bulletin A320–29–1111, dated June
29, 2004. Replacing the AGCM, and the
reducer if applicable, ends the actions
required by paragraphs (f) and (g) of this AD.
Note 1: Airbus Service Bulletin A320–29–
1111 refers to Hamilton Sundstrand Service
Bulletin ERPS13GCM–29–5, dated June 29,
2004, as an additional source of service
information for modifying and reidentifying
the AGCM.
Alternative Methods of Compliance
(AMOCs)
(i) The Manager, International Branch,
ANM–116, Transport Airplane Directorate,
FAA, has the authority to approve AMOCs
for this AD, if requested in accordance with
the procedures found in 14 CFR 39.19.
Related Information
(j) French airworthiness directive F–2004–
150, dated September 1, 2004, also addresses
the subject of this AD.
Material Incorporated by Reference
(k) You must use All Operators Telex
(Airbus) A320–29A1112, Revision 01, dated
April 8, 2004; and Airbus Service Bulletin
A320–29–1111, dated June 29, 2004; as
applicable, to perform the actions that are
required by this AD, unless the AD specifies
otherwise. The Director of the Federal
Register approves the incorporation by
reference of these documents in accordance
with 5 U.S.C. 552(a) and 1 CFR part 51. To
get copies of the service information, contact
Airbus, 1 Rond Point Maurice Bellonte,
31707 Blagnac Cedex, France. To view the
AD docket, go to the Docket Management
Facility, U.S. Department of Transportation,
400 Seventh Street SW., room PL–401, Nassif
Building, Washington, DC. To review copies
of the service information, go to the National
Archives and Records Administration
(NARA). For information on the availability
of this material at the NARA, call (202) 741–
6030, or go to https://www.archives.gov/
federal_register/code_of_federal_regulations/
ibr_locations.html.
Issued in Renton, Washington, on July 8,
2005.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 05–14087 Filed 7–20–05; 8:45 am]
BILLING CODE 4910–13–P
VerDate jul<14>2003
17:10 Jul 20, 2005
Jkt 205001
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2005–21598; Directorate
Identifier 2005–NM–121–AD; Amendment
39–14159; AD 2005–13–22]
Airworthiness Directives; Empresa
Brasileira de Aeronautica S.A.
(EMBRAER) Model EMB–135
Airplanes, and Model EMB–145,
–145ER, –145MR, –145LR, –145XR,
–145MP, and –145EP 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
June 22, 2005 (70 FR 36011). The error
resulted in an incomplete listing of the
affected airplanes. This AD applies to
all EMBRAER Model EMB–135
airplanes, and all Model EMB–145,
–145ER, –145MR, –145LR, –145XR,
–145MP, and –145EP airplanes. This AD
requires repetitive inspections of the
electrical connectors of the electric fuel
pumps to detect discrepancies,
application of anti-corrosion spray,
replacement of all fuel pumps with
improved fuel pumps, repetitive
inspections after all six fuel pumps are
replaced, and applicable corrective
actions.
Effective July 7, 2005.
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–2005–21598; the directorate
identifier for this docket is 2005–NM–
121–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.
DATES:
ADDRESSES:
PO 00000
Frm 00012
Fmt 4700
Sfmt 4700
On June
15, 2005, the FAA issued AD 2005–13–
22, amendment 39–14159 (70 FR 36011,
June 22, 2005), for all EMBRAER Model
EMB–135 airplanes, and all Model
EMB–145, –145ER, –145MR, –145LR,
–145XR, –145MP, and –145EP
airplanes. The AD requires repetitive
inspections of the electrical connectors
of the electric fuel pumps to detect
discrepancies, application of anticorrosion spray, replacement of all fuel
pumps with improved fuel pumps,
repetitive inspections after all six fuel
pumps are replaced, and applicable
corrective actions.
As published, the AD includes an
incomplete applicability. Paragraph (c)
of the AD omits Models EMB–145XR,
–145MP, and –145EP airplanes,
although those three models were
included in all other references to the
applicability throughout the preamble
and regulatory language of the AD.
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
July 7, 2005.
SUPPLEMENTARY INFORMATION:
PART 39—[AMENDED]
§ 39.13
[Corrected]
I In the Federal Register of June 22,
2005, on page 36012, in the 3rd column,
paragraph (c) of AD 2005–13–22 is
corrected to read as follows:
*
*
*
*
*
(c) This AD applies to all EMBRAER
Model EMB–135BJ, –135ER, –135KE,
–135KL, and –135LR airplanes; and
Model EMB–145, –145ER, –145MR,
–145LR, –145XR, –145MP, and –145EP
airplanes.
*
*
*
*
*
Issued in Renton, Washington, on July 11,
2005.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 05–14169 Filed 7–20–05; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 71
[Docket No. FAA–2005–21103; Airspace
Docket No. 05–AEA–10]
Amendment of Class E Airspace;
Blairstown, NJ
Federal Aviation
Administration (FAA) DOT.
AGENCY:
E:\FR\FM\21JYR1.SGM
21JYR1
]]>Agencies
[Federal Register Volume 70, Number 139 (Thursday, July 21, 2005)]
[Rules and Regulations]
[Page 41948]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 05-14169]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2005-21598; Directorate Identifier 2005-NM-121-AD;
Amendment 39-14159; AD 2005-13-22]
RIN 2120-AA64
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A.
(EMBRAER) Model EMB-135 Airplanes, and Model EMB-145, -145ER, -145MR, -
145LR, -145XR, -145MP, and -145EP 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 June 22, 2005 (70 FR 36011). The error resulted in an incomplete
listing of the affected airplanes. This AD applies to all EMBRAER Model
EMB-135 airplanes, and all Model EMB-145, -145ER, -145MR, -145LR, -
145XR, -145MP, and -145EP airplanes. This AD requires repetitive
inspections of the electrical connectors of the electric fuel pumps to
detect discrepancies, application of anti-corrosion spray, replacement
of all fuel pumps with improved fuel pumps, repetitive inspections
after all six fuel pumps are replaced, and applicable corrective
actions.
DATES: Effective July 7, 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-2005-21598; the directorate
identifier for this docket is 2005-NM-121-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 June 15, 2005, the FAA issued AD 2005-13-
22, amendment 39-14159 (70 FR 36011, June 22, 2005), for all EMBRAER
Model EMB-135 airplanes, and all Model EMB-145, -145ER, -145MR, -145LR,
-145XR, -145MP, and -145EP airplanes. The AD requires repetitive
inspections of the electrical connectors of the electric fuel pumps to
detect discrepancies, application of anti-corrosion spray, replacement
of all fuel pumps with improved fuel pumps, repetitive inspections
after all six fuel pumps are replaced, and applicable corrective
actions.
As published, the AD includes an incomplete applicability.
Paragraph (c) of the AD omits Models EMB-145XR, -145MP, and -145EP
airplanes, although those three models were included in all other
references to the applicability throughout the preamble and regulatory
language of the AD.
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 July 7, 2005.
PART 39--[AMENDED]
Sec. 39.13 [Corrected]
0
In the Federal Register of June 22, 2005, on page 36012, in the 3rd
column, paragraph (c) of AD 2005-13-22 is corrected to read as follows:
* * * * *
(c) This AD applies to all EMBRAER Model EMB-135BJ, -135ER, -135KE,
-135KL, and -135LR airplanes; and Model EMB-145, -145ER, -145MR, -
145LR, -145XR, -145MP, and -145EP airplanes.
* * * * *
Issued in Renton, Washington, on July 11, 2005.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 05-14169 Filed 7-20-05; 8:45 am]
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DATE][RULES]
