Airworthiness Directives; GROB-WERKE Model G120A Airplanes, 49184-49185 [05-16440]
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49184
Federal Register / Vol. 70, No. 162 / Tuesday, August 23, 2005 / Rules and Regulations
Issued in Burlington, Massachusetts, on
August 12, 2005.
Peter A. White,
Acting Manager, Engine and Propeller
Directorate, Aircraft Certification Service.
[FR Doc. 05–16453 Filed 8–22–05; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2005–19473; Directorate
Identifier 2004–CE–35–AD; Amendment 39–
14146; AD 2005–13–09]
RIN 2120–AA64
Airworthiness Directives; GROB–
WERKE Model G120A Airplanes
Federal Aviation
Administration, DOT.
ACTION: Final rule; correction.
AGENCY:
This document incorporates
corrections to add service information to
Airworthiness Directive (AD) 2005–13–
09, which was published in the Federal
Register on June 22, 2005 (70 FR 35993).
AD 2005–13–09 applies to certain
GROB–WERKE Model G120A airplanes.
This action adds GROB–WERKE Service
Bulletin No. MSB1121–052/2, dated
February 14, 2005, to paragraphs (e)(1),
(e)(2), and (h) of AD 2005–13–09. This
service information was included in the
notice of proposed rulemaking (NPRM)
for this AD, but we inadvertently
omitted it in the final rule request for
comments. We are re-issuing the AD in
its entirety to help eliminate any
confusion that this AD may have
created.
SUMMARY:
The effective date of this AD
remains July 26, 2005. As of July 26,
2005, the Director of the Federal
Register approved the incorporation by
reference of certain publications listed
in the regulation.
DATES:
To get the service
information identified in this AD,
contact GROB–WERKE, Burkart Grob
e.K., Unternehmenbereich Luft-und
Raumfahrt, Lettenbachstrasse 9, 86874
Tussenhausen-Mattsies, Germany;
telephone: 011 49 8268 998 105;
facsimile: 011 49 8268 998 200. To
review this service information, go to
the National Archives and Records
Administration (NARA). For
information on the availability of this
material at NARA, go to: https://
www.archives.gov/federal_register/
code_of_federal_regulations/
ibr_locations.html or call (202) 741–
6030.
To view the AD docket, go to the
Docket Management Facility; U.S.
Department of Transportation, 400
Seventh Street, SW., Nassif Building,
Room PL–401, Washington, DC 20590–
001 or on the Internet at https://
dms.dot.gov. The docket number is
FAA–2004–19473.
FOR FURTHER INFORMATION CONTACT: Karl
Schletzbaum, Aerospace Engineer,
ACE–112, Small Airplane Directorate,
901 Locust, Room 301, Kansas City,
Missouri 64106; telephone: 816–329–
4146; facsimile: 816–329–4090.
SUPPLEMENTARY INFORMATION:
ADDRESSES:
Discussion
On June 14, 2005, FAA issued AD
2005–13–09, Amendment 39–14146 (70
FR 35993, June 22, 2005), which applies
to certain GROB–WERKE Model G120A
airplanes. That AD requires you to
replace the main landing gear (MLG) uplock hook assembly.
Need for This Action
GROB–WERKE Service Bulletin No.
MSB1121–052/2, dated February 14,
2005, was included in the NPRM, but
we inadvertently omitted it from AD
2005–13–09. We are adding it
paragraphs (e)(1), (e)(2), and (h) of this
AD.
We are clarifying and re-issuing the
AD in its entirety to help eliminate any
confusion that this AD may have
created.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
Adoption of the Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the Federal Aviation Administration
amends part 39 of the Federal Aviation
Regulations (14 CFR part 39) as follows:
I
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
I
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. FAA amends § 39.13 by adding a
new AD to read as follows:
I
2005–13–09 GROB–WERKE: Amendment
39–14146; Docket No. FAA–2005–19473;
Directorate Identifier 2004-CE–35-AD.
When Does This AD Become Effective?
(a) The effective date of this AD (2005–13–
09) remains July 26, 2005.
What Other ADs Are Affected by This
Action?
(b) None.
What Airplanes Are Affected by This AD?
(c) This AD affects the following airplane
models and serial numbers that are
certificated in any category: Model G120A,
all serial numbers beginning with 85001.
What Is the Unsafe Condition Presented in
This AD?
(d) This AD results from a report that the
main landing gear (MLG) may not extend
because of contamination or misalignment of
the assembly. The actions specified in this
AD are intended to prevent the MLG from
becoming jammed and not extending, which
could result in loss of control of the airplane
during landing.
(e) To address this problem, you must do
the following:
Actions
Compliance
Procedures
(1) Remove MLG up-lock hook assembly and replace with the new MLG up-lock hook assembly.
Within 100 hours time-in-service after
July 26, 2005 (the effective date of
this AD), unless already done.
(2) For all serial numbers: Do not install any elevator and aileron hinge pins that are not part
number SY991A hinge pins.
After July 26, 2005 (the effective date
of this AD).
Follow GROB–WERKE Service Bulletin No.
MSB1121–052/2, dated February 14, 2005; and
GROB–WERKE Service Bulletin No.MSB1121–
060, dated March 7, 2005.
Follow GROB–WERKE Service Bulletin No.
MSB1121–052/2, datedFebruary 14, 2005; and
GROB–WERKE Service Bulletin No. MSB1121–
060, dated March 7, 2005.
May I Request an Alternative Method of
Compliance?
(f) You may request a different method of
compliance or a different compliance time
VerDate jul<14>2003
16:13 Aug 22, 2005
Jkt 205001
for this AD by following the procedures in 14
CFR 39.19. Unless FAA authorizes otherwise,
send your request to your principal
inspector. The principal inspector may add
PO 00000
Frm 00032
Fmt 4700
Sfmt 4700
comments and will send your request to the
Manager, Small Airplane Directorate, FAA.
For information on any already approved
alternative methods of compliance, contact
E:\FR\FM\23AUR1.SGM
23AUR1
Federal Register / Vol. 70, No. 162 / Tuesday, August 23, 2005 / Rules and Regulations
Karl Schletzbaum, Aerospace Engineer, ACE–
112, Small Airplane Directorate, 901 Locust,
Room 301, Kansas City, Missouri 64106;
telephone: 816–329–4146; facsimile: 816–
329–4090.
Is There Other Information That Relates to
This Subject?
(g) Luftfahrt-Bundesamt Airworthiness
Directive D–2004–299R2, dated March 15,
2005; GROB–WERKE Service Bulletin No.
MSB1121–052/2, dated February 14, 2005;
and GROB–WERKE Service Bulletin No.
MSB1121–060, dated March 7, 2005; also
address the subject of this AD.
Does This AD Incorporate Any Material by
Reference?
(h) You must do the actions required by
this AD following the instructions in GROB–
WERKE Service Bulletin No. MSB1121–052/
2, dated February 14, 2005; and GROB–
WERKE Service Bulletin No. MSB1121–060,
dated March 7, 2005. The Director of the
Federal Register approved the incorporation
by reference of these service bulletins in
accordance with 5 U.S.C. 552(a) and 1 CFR
part 51. To get a copy of this service
information, contact GROB–WERKE, Burkart
Grob e.K., Unternehmenbereich Luft-und
Raumfahrt, Lettenbachstrasse 9, 86874
Tussenhausen-Mattsies, Germany; telephone:
011 49 8268 998 105; facsimile: 011 49 8268
998 200. To review copies of this service
information, go to the National Archives and
Records Administration (NARA). For
information on the availability of this
material at NARA, go to: https://
www.archives.gov/federal_register/
code_of_federal_regulations/
ibr_locations.html or call (202) 741–6030. To
view the AD docket, go to the Docket
Management Facility; U.S. Department of
Transportation, 400 Seventh Street, SW.,
Nassif Building, Room PL–401, Washington,
DC 20590–001 or on the Internet at https://
dms.dot.gov. The docket number is FAA–
2004–19616.
Issued in Kansas City, Missouri, on August
15, 2005.
Terry L. Chasteen,
Acting Manager, Small Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 05–16440 Filed 8–22–05; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
ACTION:
Final rule; correction.
SUMMARY: This action corrects errors in
the legal descriptions of Area
Navigation Instrument Flight Rules
Terminal Transition Routes (RITTR)
listed in a final rule published in the
Federal Register on June 15, 2005 (70
FR 34649), Airspace Docket No. 04–
ASO–15.
EFFECTIVE DATE: 0901 UTC, September 1,
2005.
FOR FURTHER INFORMATION CONTACT: Paul
Gallant, Airspace and Rules, Office of
System Operations Airspace and AIM,
Federal Aviation Administration, 800
Independence Avenue, SW.,
Washington, DC 20591; telephone: (202)
267–8783.
SUPPLEMENTARY INFORMATION:
History
On June 15, 2005, a final rule for
Airspace Docket No. 04–ASO–15 was
published in the Federal Register (70
FR 34649). This rule established four
RITTR routes (T–200, T–201, T–202,
and T–203) in the Charlotte, NC,
terminal area. In all four routes, points
that were listed in the route descriptions
as ‘‘waypoint’’ (WP) are actually
existing published navigation ‘‘fixes.’’
Therefore, the descriptions are corrected
by removing ‘‘WP’’ and substituting
‘‘Fix.’’ In addition, the descriptions for
two of the routes contained an error in
the geographic coordinates listed for one
fix in each route. In route T–202, the
latitude coordinate for the GANTS fix
was published as 35°27′12″ N., while
the correct point is 35°27′11″ N. In route
T–203, the longitude coordinate for the
LOCKS fix was published as 81°17′37″
W. The correct point is 81°17′33″ W.
This action corrects those errors.
Accordingly, pursuant to the authority
delegated to me, the legal descriptions
for T–200, T–201, T–202 and T–203 as
published in the Federal Register on
June 15, 2005 (70 FR 34649), and
incorporated by reference in 14 CFR
71.1, are corrected as follows:
I
§ 71.1
[Docket No. FAA–2005–20246; Airspace
Docket No. 04–ASO–15]
*
[Amended]
*
*
*
*
Establishment of Area Navigation
Instrument Flight Rules Terminal
Transition Routes (RITTR); Charlotte,
NC
Federal Aviation
Administration (FAA), DOT.
T–200 Foothills, GA to Florence, SC
[Corrected]
Foothills, GA (ODF), VORTAC, (lat.
34°41′45″ N., long. 83°17′52″ W.)
RICHE, Fix, (lat. 34°41′54″ N., long. 80°59′23″
W.)
Florence, SC (FLO), VORTAC, (lat. 34°13′59″
N., long. 79°39′26″ W.)
*
RIN 2120–AA66
AGENCY:
VerDate jul<14>2003
16:13 Aug 22, 2005
Jkt 205001
PO 00000
*
Frm 00033
*
*
Fmt 4700
*
Sfmt 4700
T–201 Columbia, SC to JOTTA [Corrected]
Columbia, SC (CAE), VORTAC, (lat.
33°51′26″ N., long. 81°03′14″ W.)
HUSTN, Fix, (lat. 34°53′20″ N., long.
80°34′20″ W.)
LOCAS, Fix, (lat. 35°12′05″ N., long.
80°26′45″ W.)
JOTTA, Fix, (lat. 36°00′53″ N., long.
80°50′58″ W.)
*
*
*
*
*
T–202 RICHE to GANTS [Corrected]
RICHE, Fix, (lat. 34°41′54″ N., long. 80°59′23″
W.)
HUSTN, Fix, (lat. 34°53′20″ N., long.
80°34′20″ W.)
GANTS, Fix, (lat. 35°27′11″ N., long.
80°06′16″ W.)
*
*
*
*
*
T–203 Columbia, SC to Pulaski, VA
[Corrected]
Columbia, SC (CAE), VORTAC, (lat.
33°51′26″ N., long. 81°03′14″ W.)
LOCKS, Fix, (lat. 34°55′40″ N., long.
81°17′33″ W.)
Barretts Mountain, NC (BZM), VOR/DME,
(lat. 35°52′08″ N., long. 81°14′26″ W.)
Pulaski, VA (PSK), VORTAC, (lat. 37°05′16″
N., long. 80°42′46″ W.)
*
*
*
*
*
Issued in Washington, DC, on August 18,
2005.
Edith V. Parish,
Acting Manager, Airspace and Rules.
[FR Doc. 05–16747 Filed 8–22–05; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 71
[Docket No. FAA–2005–22069; Airspace
Docket No. 05–AEA–15]
Amendment of Class D Airspace;
Worcester, MA
Correction to Final Rule
PART 71—[Amended]
14 CFR Part 71
49185
Federal Aviation
Administration (FAA), DOT.
ACTION: Direct final rule; request for
comments.
AGENCY:
SUMMARY: This amendment realigns the
boundary of the Class D airspace area at
Worcester Regional Airport, MA. This
action will incorporate a shelf and
cutout of the Worcester Class D airspace
area to accommodate the airport traffic
pattern for Spencer Airport (60M).
DATES: Effective 0901 UTC, October 27,
2005.
Comments for inclusion in the Rules
Docket must be received on or before
September 22, 2005.
ADDRESSES: Send comments on the rule
to the Docket Management System, U.S.
Department of Transportation, Room
E:\FR\FM\23AUR1.SGM
23AUR1
Agencies
[Federal Register Volume 70, Number 162 (Tuesday, August 23, 2005)]
[Rules and Regulations]
[Pages 49184-49185]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 05-16440]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2005-19473; Directorate Identifier 2004-CE-35-AD;
Amendment 39-14146; AD 2005-13-09]
RIN 2120-AA64
Airworthiness Directives; GROB-WERKE Model G120A Airplanes
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule; correction.
-----------------------------------------------------------------------
SUMMARY: This document incorporates corrections to add service
information to Airworthiness Directive (AD) 2005-13-09, which was
published in the Federal Register on June 22, 2005 (70 FR 35993). AD
2005-13-09 applies to certain GROB-WERKE Model G120A airplanes. This
action adds GROB-WERKE Service Bulletin No. MSB1121-052/2, dated
February 14, 2005, to paragraphs (e)(1), (e)(2), and (h) of AD 2005-13-
09. This service information was included in the notice of proposed
rulemaking (NPRM) for this AD, but we inadvertently omitted it in the
final rule request for comments. We are re-issuing the AD in its
entirety to help eliminate any confusion that this AD may have created.
DATES: The effective date of this AD remains July 26, 2005. As of July
26, 2005, the Director of the Federal Register approved the
incorporation by reference of certain publications listed in the
regulation.
ADDRESSES: To get the service information identified in this AD,
contact GROB-WERKE, Burkart Grob e.K., Unternehmenbereich Luft-und
Raumfahrt, Lettenbachstrasse 9, 86874 Tussenhausen-Mattsies, Germany;
telephone: 011 49 8268 998 105; facsimile: 011 49 8268 998 200. To
review this service information, go to the National Archives and
Records Administration (NARA). For information on the availability of
this material at NARA, go to: https://www.archives.gov/federal_
register/code_of_federal_regulations/ibr_locations.html or call
(202) 741-6030.
To view the AD docket, go to the Docket Management Facility; U.S.
Department of Transportation, 400 Seventh Street, SW., Nassif Building,
Room PL-401, Washington, DC 20590-001 or on the Internet at https://
dms.dot.gov. The docket number is FAA-2004-19473.
FOR FURTHER INFORMATION CONTACT: Karl Schletzbaum, Aerospace Engineer,
ACE-112, Small Airplane Directorate, 901 Locust, Room 301, Kansas City,
Missouri 64106; telephone: 816-329-4146; facsimile: 816-329-4090.
SUPPLEMENTARY INFORMATION:
Discussion
On June 14, 2005, FAA issued AD 2005-13-09, Amendment 39-14146 (70
FR 35993, June 22, 2005), which applies to certain GROB-WERKE Model
G120A airplanes. That AD requires you to replace the main landing gear
(MLG) up-lock hook assembly.
Need for This Action
GROB-WERKE Service Bulletin No. MSB1121-052/2, dated February 14,
2005, was included in the NPRM, but we inadvertently omitted it from AD
2005-13-09. We are adding it paragraphs (e)(1), (e)(2), and (h) of this
AD.
We are clarifying and re-issuing the AD in its entirety to help
eliminate any confusion that this AD may have created.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Amendment
0
Accordingly, under the authority delegated to me by the Administrator,
the Federal Aviation Administration amends part 39 of the Federal
Aviation Regulations (14 CFR part 39) as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
0
2. FAA amends Sec. 39.13 by adding a new AD to read as follows:
2005-13-09 GROB-WERKE: Amendment 39-14146; Docket No. FAA-2005-
19473; Directorate Identifier 2004-CE-35-AD.
When Does This AD Become Effective?
(a) The effective date of this AD (2005-13-09) remains July 26,
2005.
What Other ADs Are Affected by This Action?
(b) None.
What Airplanes Are Affected by This AD?
(c) This AD affects the following airplane models and serial
numbers that are certificated in any category: Model G120A, all
serial numbers beginning with 85001.
What Is the Unsafe Condition Presented in This AD?
(d) This AD results from a report that the main landing gear
(MLG) may not extend because of contamination or misalignment of the
assembly. The actions specified in this AD are intended to prevent
the MLG from becoming jammed and not extending, which could result
in loss of control of the airplane during landing.
(e) To address this problem, you must do the following:
----------------------------------------------------------------------------------------------------------------
Actions Compliance Procedures
----------------------------------------------------------------------------------------------------------------
(1) Remove MLG up-lock hook assembly and Within 100 hours time-in- Follow GROB-WERKE Service Bulletin
replace with the new MLG up-lock hook service after July 26, 2005 No. MSB1121-052/2, dated February
assembly. (the effective date of this 14, 2005; and GROB-WERKE Service
AD), unless already done. Bulletin No.MSB1121-060, dated
March 7, 2005.
(2) For all serial numbers: Do not After July 26, 2005 (the Follow GROB-WERKE Service Bulletin
install any elevator and aileron hinge effective date of this AD). No. MSB1121-052/2, datedFebruary
pins that are not part number SY991A 14, 2005; and GROB-WERKE Service
hinge pins. Bulletin No. MSB1121-060, dated
March 7, 2005.
----------------------------------------------------------------------------------------------------------------
May I Request an Alternative Method of Compliance?
(f) You may request a different method of compliance or a
different compliance time for this AD by following the procedures in
14 CFR 39.19. Unless FAA authorizes otherwise, send your request to
your principal inspector. The principal inspector may add comments
and will send your request to the Manager, Small Airplane
Directorate, FAA. For information on any already approved
alternative methods of compliance, contact
[[Page 49185]]
Karl Schletzbaum, Aerospace Engineer, ACE-112, Small Airplane
Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106;
telephone: 816-329-4146; facsimile: 816-329-4090.
Is There Other Information That Relates to This Subject?
(g) Luftfahrt-Bundesamt Airworthiness Directive D-2004-299R2,
dated March 15, 2005; GROB-WERKE Service Bulletin No. MSB1121-052/2,
dated February 14, 2005; and GROB-WERKE Service Bulletin No.
MSB1121-060, dated March 7, 2005; also address the subject of this
AD.
Does This AD Incorporate Any Material by Reference?
(h) You must do the actions required by this AD following the
instructions in GROB-WERKE Service Bulletin No. MSB1121-052/2, dated
February 14, 2005; and GROB-WERKE Service Bulletin No. MSB1121-060,
dated March 7, 2005. The Director of the Federal Register approved
the incorporation by reference of these service bulletins in
accordance with 5 U.S.C. 552(a) and 1 CFR part 51. To get a copy of
this service information, contact GROB-WERKE, Burkart Grob e.K.,
Unternehmenbereich Luft-und Raumfahrt, Lettenbachstrasse 9, 86874
Tussenhausen-Mattsies, Germany; telephone: 011 49 8268 998 105;
facsimile: 011 49 8268 998 200. To review copies of this service
information, go to the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, go to: https://www.archives.gov/federal_register/code_of_
federal_regulations/ibr_locations.html or call (202) 741-6030. To
view the AD docket, go to the Docket Management Facility; U.S.
Department of Transportation, 400 Seventh Street, SW., Nassif
Building, Room PL-401, Washington, DC 20590-001 or on the Internet
at https://dms.dot.gov. The docket number is FAA-2004-19616.
Issued in Kansas City, Missouri, on August 15, 2005.
Terry L. Chasteen,
Acting Manager, Small Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 05-16440 Filed 8-22-05; 8:45 am]
BILLING CODE 4910-13-P