Airworthiness Directives; Boeing Model 737-300, -400, and -500 Series Airplanes Modified in Accordance With Supplemental Type Certificate (STC) ST00127BO, 21924 [05-8402]
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21924
Federal Register / Vol. 70, No. 81 / Thursday, April 28, 2005 / Rules and Regulations
period of 3 years. This waiver expires
July 31, 2010.
David R. Shipman,
Acting Administrator, Grain Inspection,
Packers and Stockyards Administration.
[FR Doc. 05–8519 Filed 4–27–05; 8:45 am]
BILLING CODE 3410–EN–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2004–19891; Directorate
Identifier 2004–NM–136–AD; Amendment
39–14006; AD 2005–05–17]
RIN 2120–AA64
Airworthiness Directives; Boeing
Model 737–300, –400, and –500 Series
Airplanes Modified in Accordance With
Supplemental Type Certificate (STC)
ST00127BO
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
March 14, 2005 (70 FR 12401). The error
resulted in specifying a non-existing
part number. This AD applies to Boeing
Model 737–300, –400, and –500 series
airplanes modified in accordance with
STC ST00127BO. This AD requires
installation of bonding straps to the safe
side harnesses of the digital transient
suppression device of the fuel quantity
indicating system.
DATES: Effective April 18, 2005.
ADDRESSES: The AD docket contains the
proposed AD, comments, and any final
disposition. You can 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–2004–19891; the directorate
identifier for this docket is 2004–NM–
136–AD.
FOR FURTHER INFORMATION CONTACT:
Richard Spencer, Aerospace Engineer,
Boston Aircraft Certification Office,
ANE–150, FAA, Engine and Propeller
Directorate, 12 New England Executive
VerDate jul<14>2003
17:28 Apr 27, 2005
Jkt 205001
Park, Burlington, Massachusetts 01803;
telephone (781) 238–7184; fax (781)
238–7170.
DEPARTMENT OF TRANSPORTATION
On March
2, 2005, the FAA issued AD 2005–05–
17, amendment 39–14006 (70 FR 12401,
March 14, 2005), for Boeing Model 737–
300, –400, and –500 series airplanes
modified in accordance with
Supplemental Type Certificate (STC)
ST00127BO. The AD requires
installation of bonding straps to the safe
side harnesses of the digital transient
suppression device of the fuel quantity
indicating system.
As published, paragraph (g) of the AD
specifies that, ‘‘As of the effective date
of this AD, no person may install a safe
side harness, Part Number 50357–01XX,
on any airplane, unless that safe side
harness has been modified in
accordance with Goodrich Service
Bulletin 737–300766–28–2, Revision 2,
dated July 28, 2004.’’ We have
determined that 50357–01XX is not an
existing part number, and that the
correct part number is 50367–01XX.
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
April 18, 2005.
14 CFR Part 39
SUPPLEMENTARY INFORMATION:
§ 39.13
[Corrected]
In the Federal Register of March 14,
2005, on page 12402, in the first
column, paragraph (g) of AD 2005–05–
17 is corrected to read as follows:
*
*
*
*
*
(g) As of the effective date of this AD,
no person may install a safe side
harness, Part Number 50367–01XX, on
any airplane, unless that safe side
harness has been modified in
accordance with Goodrich Service
Bulletin 737–300766–28–2, Revision 2,
dated July 28, 2004.
*
*
*
*
*
Issued in Renton, Washington, on April 19,
2005.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 05–8402 Filed 4–27–05; 8:45 am]
BILLING CODE 4910–13–P
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Frm 00004
Fmt 4700
Sfmt 4700
Federal Aviation Administration
[Docket No. 2001–NM–293–AD; Amendment
39–14072; AD 2005–09–04]
RIN 2120–AA64
Airworthiness Directives; McDonnell
Douglas Model DC–9–81 (MD–81), DC–
9–82 (MD–82), DC–9–83 (MD–83), DC–
9–87 (MD–87), and MD–88 Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
SUMMARY: This amendment supersedes
an existing airworthiness directive (AD),
applicable to certain McDonnell
Douglas Model DC–9–81 (MD–81), DC–
9–82 (MD–82), DC–9–83 (MD–83), DC–
9–87 (MD–87), MD–88, and MD–90–30
airplanes. The existing AD currently
requires repetitive inspections to detect
cracking of the main landing gear (MLG)
shock strut pistons, and replacement of
a cracked piston with a new or
serviceable part. This amendment
removes certain airplanes but requires
that the existing inspections, and
corrective actions if necessary, be
accomplished on additional MLG shock
strut pistons. This amendment also
requires replacing the MLG shock strut
pistons with new improved parts, which
would terminate the repetitive
inspections. The actions specified by
this AD are intended to prevent fatigue
cracking of the MLG pistons, which
could result in failure of the pistons and
consequent damage to the airplane
structure or injury to airplane
occupants. This action is intended to
address the identified unsafe condition.
DATES: Effective June 2, 2005.
The incorporation by reference of
Boeing Alert Service Bulletin MD80–
32A308, Revision 04, dated June 12,
2001, as listed in the regulations, is
approved by the Director of the Federal
Register as of June 2, 2005.
The incorporation by reference of
Boeing Service Bulletin MD80–32–309,
Revision 01, dated April 25, 2001, as
listed in the regulations, was approved
previously by the Director of the Federal
Register as of June 20, 2002 (67 FR
34823, May 16, 2002).
The incorporation by reference of
McDonnell Douglas Alert Service
Bulletin MD80–32A308, dated March 5,
1998; and McDonnell Douglas Alert
Service Bulletin MD80–32A308,
Revision 01, dated May 12, 1998; as
listed in the regulations; was approved
E:\FR\FM\28APR1.SGM
28APR1
]]>Agencies
[Federal Register Volume 70, Number 81 (Thursday, April 28, 2005)]
[Rules and Regulations]
[Page 21924]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 05-8402]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2004-19891; Directorate Identifier 2004-NM-136-AD;
Amendment 39-14006; AD 2005-05-17]
RIN 2120-AA64
Airworthiness Directives; Boeing Model 737-300, -400, and -500
Series Airplanes Modified in Accordance With Supplemental Type
Certificate (STC) ST00127BO
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 March 14, 2005 (70 FR 12401). The error resulted in specifying a
non-existing part number. This AD applies to Boeing Model 737-300, -
400, and -500 series airplanes modified in accordance with STC
ST00127BO. This AD requires installation of bonding straps to the safe
side harnesses of the digital transient suppression device of the fuel
quantity indicating system.
DATES: Effective April 18, 2005.
ADDRESSES: The AD docket contains the proposed AD, comments, and any
final disposition. You can 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-2004-19891; the directorate
identifier for this docket is 2004-NM-136-AD.
FOR FURTHER INFORMATION CONTACT: Richard Spencer, Aerospace Engineer,
Boston Aircraft Certification Office, ANE-150, FAA, Engine and
Propeller Directorate, 12 New England Executive Park, Burlington,
Massachusetts 01803; telephone (781) 238-7184; fax (781) 238-7170.
SUPPLEMENTARY INFORMATION: On March 2, 2005, the FAA issued AD 2005-05-
17, amendment 39-14006 (70 FR 12401, March 14, 2005), for Boeing Model
737-300, -400, and -500 series airplanes modified in accordance with
Supplemental Type Certificate (STC) ST00127BO. The AD requires
installation of bonding straps to the safe side harnesses of the
digital transient suppression device of the fuel quantity indicating
system.
As published, paragraph (g) of the AD specifies that, ``As of the
effective date of this AD, no person may install a safe side harness,
Part Number 50357-01XX, on any airplane, unless that safe side harness
has been modified in accordance with Goodrich Service Bulletin 737-
300766-28-2, Revision 2, dated July 28, 2004.'' We have determined that
50357-01XX is not an existing part number, and that the correct part
number is 50367-01XX.
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 April 18, 2005.
Sec. 39.13 [Corrected]
In the Federal Register of March 14, 2005, on page 12402, in the
first column, paragraph (g) of AD 2005-05-17 is corrected to read as
follows:
* * * * *
(g) As of the effective date of this AD, no person may install a
safe side harness, Part Number 50367-01XX, on any airplane, unless that
safe side harness has been modified in accordance with Goodrich Service
Bulletin 737-300766-28-2, Revision 2, dated July 28, 2004.
* * * * *
Issued in Renton, Washington, on April 19, 2005.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 05-8402 Filed 4-27-05; 8:45 am]
BILLING CODE 4910-13-P
