Airworthiness Directives; Boeing Model 747 Airplanes, 53923 [E7-18472]
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Federal Register / Vol. 72, No. 183 / Friday, September 21, 2007 / Rules and Regulations
Customer Liaison Manager, CH 6371 STANS,
Switzerland; telephone: + 41 (0)41 619 6580;
fax: + 41 (0)41 619 6576; e-mail:
fodermatt@pilatus aircaft.com.
(3) 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
September 13, 2007.
Kim Smith,
Manager, Small Airplane Directorate, Aircraft
Certification Service.
[FR Doc. E7–18476 Filed 9–20–07; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2006–26441; Directorate
Identifier 2006–NM–204–AD; Amendment
39–15139; AD 2007–15–10]
RIN 2120–AA64
Airworthiness Directives; Boeing
Model 747 Airplanes
The FAA is correcting a
typographical error in an existing
airworthiness directive (AD) that was
published in the Federal Register on
July 30, 2007 (72 FR 41438). The error
resulted in certain compliance times
being mislabeled as units of flight cycles
instead of flight hours. This AD applies
to all Boeing Model 747 airplanes. This
AD requires an inspection of the No. 2
and No. 3 windows on the left and right
sides of the airplane to determine their
part numbers, and related investigative
and corrective actions if necessary.
DATES: Effective September 21, 2007.
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
Operations office between 9 a.m. and 5
p.m., Monday through Friday, except
Federal holidays. The Docket
Operations office (telephone (800) 647–
5527) is located on the ground level of
the West Building at the DOT street
address stated in the ADDRESSES section.
This docket number is FAA–2006–
26441; the directorate identifier for this
docket is 2006–NM–204–AD.
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15:32 Sep 20, 2007
Jkt 211001
Steve Fox, Aerospace Engineer,
Airframe Branch, ANM–120S, FAA,
Seattle Aircraft Certification Office,
1601 Lind Avenue, SW., Renton,
Washington 98057–3356; telephone
(425) 917–6425; fax (425) 917–6590.
On July
18, 2007, the FAA issued AD 2007–15–
10, amendment 39–15139 (72 FR 41438,
July 30, 2007), for all Boeing Model
747–100, 747–100B, 747–100B SUD,
747–200B, 747–200C, 747–200F, 747–
300, 747–400, 747–400D, 747–400F,
747SR, and 747SP series airplanes. The
AD requires an inspection of the No. 2
and No. 3 windows on the left and right
sides of the airplane to determine their
part numbers, and related investigative
and corrective actions if necessary.
As published, the compliance times
in paragraph (g) of AD 2007–15–10 were
mislabeled as units of flight cycles
instead of flight hours.
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 4, 2007.
SUPPLEMENTARY INFORMATION:
§ 39.13
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; correction.
AGENCY:
SUMMARY:
FOR FURTHER INFORMATION CONTACT:
[Corrected]
I In the Federal Register of July 30,
2007, on page 41441, in the 2nd
column, paragraph (g) of AD 2007–15–
10 is corrected to read as follows:
*
*
*
*
*
(g) Where Tables 1, 2, and 3 of
paragraph 1.E. of Boeing Alert Service
Bulletin 747–56A2012, dated August 24,
2006, specify counting the compliance
time from ‘‘* * * after the date on this
service bulletin,’’ this AD requires
counting the compliance time from the
effective date of this AD. After replacing
a discrepant window with a new
window, do the initial detailed
inspection of the new window at the
applicable compliance time: (1) within
5,500 flight hours after installing part
number (P/N) 65B27042–( ) or
65B27043–( ), or (2) within 22,000 flight
hours after installing P/N 65B27046–( )
or 65B27047–( ).
*
*
*
*
*
Issued in Renton, Washington, on
September 10, 2007.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. E7–18472 Filed 9–20–07; 8:45 am]
BILLING CODE 4910–13–P
PO 00000
Frm 00011
Fmt 4700
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53923
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2007–27787 Directorate
Identifier 2007–CE–032–AD; Amendment
39–15209; AD 2007–19–18]
RIN 2120–AA64
Airworthiness Directives; DG
Flugzeugbau GmbH Model DG–1000T
Gliders
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
SUMMARY: We are adopting a new
airworthiness directive (AD) for the
products listed above. This AD results
from mandatory continuing
airworthiness information (MCAI)
issued by an aviation authority of
another country to identify and correct
an unsafe condition on an aviation
product. The MCAI describes the unsafe
condition as:
The digital engine indicating system (DEI–
NT) and associated control unit must get
their latest software update. It has been found
out in operation, that some combinations of
system states while pressing switches can
cause electrical damages to the system. A
new software update is mandated to correct
this deficiency and to incorporate additional
safety functions to the system.
We are issuing this AD to require
actions to correct the unsafe condition
on these products.
DATES: This AD becomes effective
October 26, 2007.
On October 26, 2007, the Director of
the Federal Register approved the
incorporation by reference of certain
publications listed in this AD.
ADDRESSES: You may examine the AD
docket on the Internet at https://
dms.dot.gov or in person at Document
Management Facility, U.S. Department
of Transportation, Docket Operations,
M–30, West Building Ground Floor,
Room W12–140, 1200 New Jersey
Avenue, SE., Washington, DC 20590.
FOR FURTHER INFORMATION CONTACT: Greg
Davison, Glider Program Manager, FAA,
Small Airplane Directorate, 901 Locust,
Room 301, Kansas City, Missouri 64106;
telephone: (816) 329–4130; fax: (816)
329–4090.
SUPPLEMENTARY INFORMATION:
Discussion
We issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 to include an AD that would
apply to the specified products. That
E:\FR\FM\21SER1.SGM
21SER1
]]>Agencies
[Federal Register Volume 72, Number 183 (Friday, September 21, 2007)]
[Rules and Regulations]
[Page 53923]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E7-18472]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2006-26441; Directorate Identifier 2006-NM-204-AD;
Amendment 39-15139; AD 2007-15-10]
RIN 2120-AA64
Airworthiness Directives; Boeing Model 747 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 July 30, 2007 (72 FR 41438). The error resulted in certain
compliance times being mislabeled as units of flight cycles instead of
flight hours. This AD applies to all Boeing Model 747 airplanes. This
AD requires an inspection of the No. 2 and No. 3 windows on the left
and right sides of the airplane to determine their part numbers, and
related investigative and corrective actions if necessary.
DATES: Effective September 21, 2007.
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 Operations office
between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The Docket Operations office (telephone (800) 647-5527) is
located on the ground level of the West Building at the DOT street
address stated in the ADDRESSES section. This docket number is FAA-
2006-26441; the directorate identifier for this docket is 2006-NM-204-
AD.
FOR FURTHER INFORMATION CONTACT: Steve Fox, Aerospace Engineer,
Airframe Branch, ANM-120S, FAA, Seattle Aircraft Certification Office,
1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone (425)
917-6425; fax (425) 917-6590.
SUPPLEMENTARY INFORMATION: On July 18, 2007, the FAA issued AD 2007-15-
10, amendment 39-15139 (72 FR 41438, July 30, 2007), for all Boeing
Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-200F,
747-300, 747-400, 747-400D, 747-400F, 747SR, and 747SP series
airplanes. The AD requires an inspection of the No. 2 and No. 3 windows
on the left and right sides of the airplane to determine their part
numbers, and related investigative and corrective actions if necessary.
As published, the compliance times in paragraph (g) of AD 2007-15-
10 were mislabeled as units of flight cycles instead of flight hours.
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 4, 2007.
Sec. 39.13 [Corrected]
0
In the Federal Register of July 30, 2007, on page 41441, in the 2nd
column, paragraph (g) of AD 2007-15-10 is corrected to read as follows:
* * * * *
(g) Where Tables 1, 2, and 3 of paragraph 1.E. of Boeing Alert
Service Bulletin 747-56A2012, dated August 24, 2006, specify counting
the compliance time from ``* * * after the date on this service
bulletin,'' this AD requires counting the compliance time from the
effective date of this AD. After replacing a discrepant window with a
new window, do the initial detailed inspection of the new window at the
applicable compliance time: (1) within 5,500 flight hours after
installing part number (P/N) 65B27042-( ) or 65B27043-( ), or (2)
within 22,000 flight hours after installing P/N 65B27046-( ) or
65B27047-( ).
* * * * *
Issued in Renton, Washington, on September 10, 2007.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E7-18472 Filed 9-20-07; 8:45 am]
BILLING CODE 4910-13-P
