Airworthiness Directives; AvCraft Dornier Model 328-100 and -300 Airplanes, 35514-35516 [05-12001]
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35514
Federal Register / Vol. 70, No. 118 / Tuesday, June 21, 2005 / Rules and Regulations
11. The inflatable restraint system
installation must be protected from the
effects of fire such that no hazard to
occupants will result.
12. There must be a means to verify
the integrity of the inflatable restraint
activation system before each flight or it
must be demonstrated to reliably
operate between inspection intervals.
13. A life limit must be established for
appropriate system components.
14. Qualification testing of the
internal firing mechanism must be
performed at vibration levels
appropriate for a general aviation
airplane.
Issued in Kansas City, Missouri on June 8,
2005.
John Colomy,
Acting Manager, Small Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 05–12148 Filed 6–20–05; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2005–20869; Directorate
Identifier 2004–NM–09–AD; Amendment 39–
14139; AD 2005–13–03]
RIN 2120–AA64
Airworthiness Directives; AvCraft
Dornier Model 328–100 and –300
Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
The FAA is adopting a new
airworthiness directive (AD) for certain
SUMMARY:
AvCraft Dornier Model 328–100 and
–300 airplanes. This AD requires
operators to install colored
identification strips on the pulley
brackets, fairlead bracket assemblies,
operational assemblies, and flight
control cables. This AD is prompted by
a report that the flight control systems
do not have elements that are
distinctively identified. We are issuing
this AD to prevent the incorrect reassembly of the flight control system
during maintenance, which could result
in reduced controllability of the
airplane.
Transport Airplane Directorate, 1601
Lind Avenue, SW., Renton, Washington
98055–4056; telephone (425) 227–2125;
fax (425) 227–1149.
SUPPLEMENTARY INFORMATION: The FAA
proposed to amend 14 CFR part 39 with
an AD for certain AvCraft Dornier
Model 328–100 and –300 airplanes.
That action, published in the Federal
Register on April 6, 2005 (70 FR 17370),
proposed to require operators to install
colored identification strips on the
pulley brackets, fairlead bracket
assemblies, operational assemblies, and
flight control cables.
This AD becomes effective July
26, 2005.
The incorporation by reference of
certain publications listed in the AD is
approved by the Director of the Federal
Register as of July 26, 2005.
ADDRESSES: For service information
identified in this AD, contact AvCraft
Aerospace GmbH, P.O. Box 1103, D–
82230 Wessling, Germany.
Docket: 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–2005–20869; the directorate
identifier for this docket is 2004–NM–
09–AD.
FOR FURTHER INFORMATION CONTACT: Dan
Rodina, Aerospace Engineer,
International Branch, ANM–116, FAA,
Comments
DATES:
We provided the public the
opportunity to participate in the
development of this AD. No comments
have been submitted on the proposed
AD or on the determination of the cost
to the public.
Explanation of Change to Applicability
We have revised the applicability of
the proposed AD to identify model
designations as published in the most
recent type certificate data sheet for the
affected models.
Conclusion
We have carefully reviewed the
available data and determined that air
safety and the public interest require
adopting the AD with the change
described previously. We have
determined that these changes will
neither increase the economic burden
on any operator nor increase the scope
of the AD.
Costs of Compliance
The following table provides the
estimated costs for U.S. operators to
comply with this AD.
ESTIMATED COSTS
Average
labor rate
per hour
Work
hours
Action
Installation ................................................
16
The following table provides the
estimated costs for operators to comply
with this AD if they have airplanes that
Parts
$65
Cost per
airplane
$291
$1,331
Number of
U.S.registered
airplanes
112
Fleet cost
$149,072
are subject to the concurrent
requirements.
ESTIMATED COSTS—CONCURRENT REQUIREMENTS
Concurrent Dornier Service Bulletin
SB–328–27–290 .............................................
SB–328–27–291 .............................................
SB–328–27–292 .............................................
VerDate jul<14>2003
15:18 Jun 20, 2005
Jkt 205001
Average
labor rate
per hour
Work hours
PO 00000
5
5
5
Frm 00004
Fmt 4700
$65
65
65
Sfmt 4700
Parts
Operator Supplied ..........................................
Operator Supplied ..........................................
Operator Supplied ..........................................
E:\FR\FM\21JNR1.SGM
21JNR1
Cost per
airplane
$325
325
325
35515
Federal Register / Vol. 70, No. 118 / Tuesday, June 21, 2005 / Rules and Regulations
ESTIMATED COSTS—CONCURRENT REQUIREMENTS—Continued
Concurrent Dornier Service Bulletin
Average
labor rate
per hour
Work hours
SB–328J–27–035 ............................................
SB–328J–27–036 ............................................
SB–328J–27–037 ............................................
5
5
5
Cost per
airplane
Parts
65
65
65
$462 ...............................................................
578 .................................................................
Operator Supplied ..........................................
787
903
$325
Authority for This Rulemaking
Title 49 of the United States Code
specifies the FAA’s authority to issue
rules on aviation safety. Subtitle I,
Section 106, describes the authority of
the FAA Administrator. Subtitle VII,
Aviation Programs, describes in more
detail the scope of the Agency’s
authority.
We are issuing this rulemaking under
the authority described in Subtitle VII,
Part A, Subpart III, Section 44701,
‘‘General requirements.’’ Under that
section, Congress charges the FAA with
promoting safe flight of civil aircraft in
air commerce by prescribing regulations
for practices, methods, and procedures
the Administrator finds necessary for
safety in air commerce. This regulation
is within the scope of that authority
because it addresses an unsafe condition
that is likely to exist or develop on
products identified in this rulemaking
action.
(3) Will not have a significant
economic impact, positive or negative,
on a substantial number of small entities
under the criteria of the Regulatory
Flexibility Act.
We prepared a regulatory evaluation
of the estimated costs to comply with
this AD. See the ADDRESSES section for
a location to examine the regulatory
evaluation.
Affected ADs
List of Subjects in 14 CFR Part 39
Unsafe Condition
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
(d) This AD was prompted by a report that
the flight control systems do not have
elements that are distinctively identified. We
are issuing this AD to prevent the incorrect
re-assembly of the flight control system
during maintenance, which could result in
reduced controllability of the airplane.
Regulatory Findings
We have determined that this AD will
not have federalism implications under
Executive Order 13132. This AD will
not have a substantial direct effect on
the States, on the relationship between
the national government and the States,
or on the distribution of power and
responsibilities among the various
levels of government.
For the reasons discussed above, I
certify that this AD:
(1) Is not a ‘‘significant regulatory
action’’ under Executive Order 12866;
(2) Is not a ‘‘significant rule’’ under
DOT Regulatory Policies and Procedures
(44 FR 11034, February 26, 1979); and
I
Adoption of the Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as
follows:
(b) None.
Applicability
(c) This AD applies to AvCraft Dornier
Model 328–100 and –300 series airplanes,
certificated in any category; as identified in
Dornier Service Bulletin SB–328J–27–176,
Revision 1, dated April 15, 2003; and Dornier
Service Bulletin SB–328–27–436, Revision 1,
dated April 15, 2003; as applicable.
Compliance
PART 39—AIRWORTHINESS
DIRECTIVES
(e) You are responsible for having the
actions required by this AD performed within
the compliance times specified, unless the
actions have already been done.
1. The authority citation for part 39
continues to read as follows:
Installation
I
2005–13–03 AvCraft Aerospace Gmbh
(Formerly Fairchild Dornier GmbH):
Amendment 39–14139. Docket No.
FAA–2005–20869; Directorate Identifier
2004–NM–09–AD.
(f) Within 24 months after the effective
date of this AD, install colored identification
strips on the pulley brackets, fairlead bracket
assemblies, operational assemblies, and flight
control cables, in accordance with the
Accomplishment Instructions of Dornier
Service Bulletin SB–328J–27–176, Revision
1, dated April 15, 2003; or Dornier Service
Bulletin SB–328–27–436, Revision 1, dated
April 15, 2003; as applicable.
Prior or Concurrent Requirements
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive (AD):
Effective Date
(a) This AD becomes effective July 26,
2005.
(g) Prior to or concurrently with the
accomplishment of the actions in paragraph
(f) of this AD, accomplish the actions in the
applicable service bulletins listed in Table 1
of this AD.
TABLE 1.—PRIOR OR CONCURRENT REQUIREMENTS
Model
Dornier Service
Bulletin
Revision
Date
328–100 airplanes ......................................
SB–328–27–290
1 ..................
SB–328–27–291
1 ..................
SB–328–27–292
1 ..................
SB–328J–27–035
SB–328J–27–036
SB–328J–27–037
Original ........
Original ........
Original ........
December 8,
2000.
December 8,
2000.
December 8,
2000.
April 25, 2000 .....
April 25, 2000 .....
April 25, 2000 .....
328–300 airplanes ......................................
VerDate jul<14>2003
15:18 Jun 20, 2005
Jkt 205001
PO 00000
Frm 00005
Fmt 4700
Sfmt 4700
E:\FR\FM\21JNR1.SGM
Action
Relocate the auto-pilot rudder servo.
Relocate the auto-pilot aileron servo.
Relocate the auto pilot elevator servo.
Relocate the auto-pilot rudder servo.
Relocate the auto-pilot elevator servo.
Relocate the auto-2000 pilot aileron servo.
21JNR1
35516
Federal Register / Vol. 70, No. 118 / Tuesday, June 21, 2005 / Rules and Regulations
Alternative Methods of Compliance
(AMOCs)
effective November 11, 2003; also address the
subject of this AD.
(h) 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.
Material Incorporated by Reference
Related Information
(i) German airworthiness directive 2003–
376, effective November 11, 2003; and
German airworthiness directive 2003–377,
(j) You must use the applicable service
bulletins in Table 2 of this AD 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 AvCraft
Aerospace GmbH, P.O. Box 1103, D–82230
Wessling, Germany. 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.
TABLE 2.—MATERIAL INCORPORATED BY REFERENCE
Dornier service bulletin
Revision level
SB–328–27–290 ......................................................................
1 ...............................................................................................
SB–328–27–291 ......................................................................
1 ...............................................................................................
SB–328–27–292 ......................................................................
1 ...............................................................................................
SB–328–27–436 ......................................................................
SB–328J–27–035 .....................................................................
SB–328J–27–036 .....................................................................
SB–328J–27–037 .....................................................................
SB–328J–27–176 .....................................................................
1 ...............................................................................................
Original .....................................................................................
Original .....................................................................................
Original .....................................................................................
1 ...............................................................................................
Issued in Renton, Washington, on June 10,
2005.
Michael J. Kaszycki,
Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. 05–12001 Filed 6–20–05; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2005–20866; Directorate
Identifier 2004–NM–258–AD; Amendment
39–14140; AD 2005–13–04]
RIN 2120–AA64
Airworthiness Directives; Avcraft
Dornier Model 328–100 and –300
Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
SUMMARY: The FAA is adopting a new
airworthiness directive (AD) for certain
Avcraft Dornier Model 328–100 and
–300 airplanes. This AD requires a
pressure test and detailed inspection of
each fuselage drain line to determine if
there is a blockage, and related
investigative/corrective actions if
necessary. This AD is prompted by a
report of leakage at one of the drain
lines in the fuselage. We are issuing this
AD to prevent blockage within the drain
VerDate jul<14>2003
15:18 Jun 20, 2005
Jkt 205001
lines, causing fluids to collect. These
fluids may freeze and expand, damaging
the drain lines, and allowing fuel to leak
into the cabin and fuel vapors to come
into contact with ignition sources,
which could result in consequent fire in
the cabin.
DATES: This AD becomes effective July
26, 2005.
The incorporation by reference of
certain publications listed in the AD is
approved by the Director of the Federal
Register as of July 26, 2005.
ADDRESSES: For service information
identified in this AD, contact AvCraft
Aerospace GmbH, P.O. Box 1103, D–
82230 Wessling, Germany.
Docket: 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–2005–20866; the directorate
identifier for this docket is 2004–NM–
258–AD.
FOR FURTHER INFORMATION CONTACT: Dan
Rodina, Aerospace Engineer,
International Branch, ANM–116, FAA,
Transport Airplane Directorate, 1601
Lind Avenue, SW., Renton, Washington
PO 00000
Frm 00006
Fmt 4700
Sfmt 4700
Date
December 8,
2000.
December 8,
2000.
December 8,
2000.
April 15, 2003.
April 25, 2000.
April 25, 2000.
April 25, 2000.
April 15, 2003.
98055–4056; telephone (425) 227–2125;
fax (425) 227–1149.
SUPPLEMENTARY INFORMATION: The FAA
proposed to amend 14 CFR part 39 with
an AD for certain Avcraft Dornier Model
328–100 and –300 series airplanes. That
action, published in the Federal
Register on April 6, 2005 (70 FR 17357),
proposed to require a pressure test and
detailed inspection of each fuselage
drain line to determine if there is a
blockage, and related investigative/
corrective actions if necessary.
Comments
We provided the public the
opportunity to participate in the
development of this AD. No comments
have been submitted on the proposed
AD or on the determination of the cost
to the public.
Explanation of Change to Applicability
We have revised the applicability of
the proposed AD to identify model
designations as published in the most
recent type certificate data sheet for the
affected models. In addition, we noticed
that we had inadvertently reversed the
qualifiers of the airplane models
specified in the applicability of the
proposed AD. The applicability for this
AD has been corrected for this AD and
now reads, ‘‘This AD applies to Avcraft
Dornier Model 328–100 series airplanes
having serial numbers 3005 through
3119 inclusive, and Avcraft Dornier
Model 328–300 series airplanes without
option 033F003 ‘‘Extended Range’’
installed; certificated in any category.’’
E:\FR\FM\21JNR1.SGM
21JNR1
]]>Agencies
[Federal Register Volume 70, Number 118 (Tuesday, June 21, 2005)]
[Rules and Regulations]
[Pages 35514-35516]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 05-12001]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2005-20869; Directorate Identifier 2004-NM-09-AD;
Amendment 39-14139; AD 2005-13-03]
RIN 2120-AA64
Airworthiness Directives; AvCraft Dornier Model 328-100 and -300
Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain AvCraft Dornier Model 328-100 and -300 airplanes. This AD
requires operators to install colored identification strips on the
pulley brackets, fairlead bracket assemblies, operational assemblies,
and flight control cables. This AD is prompted by a report that the
flight control systems do not have elements that are distinctively
identified. We are issuing this AD to prevent the incorrect re-assembly
of the flight control system during maintenance, which could result in
reduced controllability of the airplane.
DATES: This AD becomes effective July 26, 2005.
The incorporation by reference of certain publications listed in
the AD is approved by the Director of the Federal Register as of July
26, 2005.
ADDRESSES: For service information identified in this AD, contact
AvCraft Aerospace GmbH, P.O. Box 1103, D-82230 Wessling, Germany.
Docket: 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-2005-20869; the directorate
identifier for this docket is 2004-NM-09-AD.
FOR FURTHER INFORMATION CONTACT: Dan Rodina, Aerospace Engineer,
International Branch, ANM-116, FAA, Transport Airplane Directorate,
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425)
227-2125; fax (425) 227-1149.
SUPPLEMENTARY INFORMATION: The FAA proposed to amend 14 CFR part 39
with an AD for certain AvCraft Dornier Model 328-100 and -300
airplanes. That action, published in the Federal Register on April 6,
2005 (70 FR 17370), proposed to require operators to install colored
identification strips on the pulley brackets, fairlead bracket
assemblies, operational assemblies, and flight control cables.
Comments
We provided the public the opportunity to participate in the
development of this AD. No comments have been submitted on the proposed
AD or on the determination of the cost to the public.
Explanation of Change to Applicability
We have revised the applicability of the proposed AD to identify
model designations as published in the most recent type certificate
data sheet for the affected models.
Conclusion
We have carefully reviewed the available data and determined that
air safety and the public interest require adopting the AD with the
change described previously. We have determined that these changes will
neither increase the economic burden on any operator nor increase the
scope of the AD.
Costs of Compliance
The following table provides the estimated costs for U.S. operators
to comply with this AD.
Estimated Costs
--------------------------------------------------------------------------------------------------------------------------------------------------------
Number of U.S.-
Action Work hours Average labor Parts Cost per registered Fleet cost
rate per hour airplane airplanes
--------------------------------------------------------------------------------------------------------------------------------------------------------
Installation............................................ 16 $65 $291 $1,331 112 $149,072
--------------------------------------------------------------------------------------------------------------------------------------------------------
The following table provides the estimated costs for operators to
comply with this AD if they have airplanes that are subject to the
concurrent requirements.
Estimated Costs--Concurrent Requirements
----------------------------------------------------------------------------------------------------------------
Average labor Cost per
Concurrent Dornier Service Bulletin Work hours rate per hour Parts airplane
----------------------------------------------------------------------------------------------------------------
SB-328-27-290......................... 5 $65 Operator Supplied....... $325
SB-328-27-291......................... 5 65 Operator Supplied....... 325
SB-328-27-292......................... 5 65 Operator Supplied....... 325
[[Page 35515]]
SB-328J-27-035........................ 5 65 $462.................... 787
SB-328J-27-036........................ 5 65 578..................... 903
SB-328J-27-037........................ 5 65 Operator Supplied....... $325
----------------------------------------------------------------------------------------------------------------
Authority for This Rulemaking
Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, Section 106, describes the
authority of the FAA Administrator. Subtitle VII, Aviation Programs,
describes in more detail the scope of the Agency's authority.
We are issuing this rulemaking under the authority described in
Subtitle VII, Part A, Subpart III, Section 44701, ``General
requirements.'' Under that section, Congress charges the FAA with
promoting safe flight of civil aircraft in air commerce by prescribing
regulations for practices, methods, and procedures the Administrator
finds necessary for safety in air commerce. This regulation is within
the scope of that authority because it addresses an unsafe condition
that is likely to exist or develop on products identified in this
rulemaking action.
Regulatory Findings
We have determined that this AD will not have federalism
implications under Executive Order 13132. This AD will not have a
substantial direct effect on the States, on the relationship between
the national government and the States, or on the distribution of power
and responsibilities among the various levels of government.
For the reasons discussed above, I certify that this AD:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866;
(2) Is not a ``significant rule'' under DOT Regulatory Policies and
Procedures (44 FR 11034, February 26, 1979); and
(3) Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
We prepared a regulatory evaluation of the estimated costs to
comply with this AD. See the ADDRESSES section for a location to
examine the regulatory evaluation.
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 FAA amends 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. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive (AD):
2005-13-03 AvCraft Aerospace Gmbh (Formerly Fairchild Dornier GmbH):
Amendment 39-14139. Docket No. FAA-2005-20869; Directorate
Identifier 2004-NM-09-AD.
Effective Date
(a) This AD becomes effective July 26, 2005.
Affected ADs
(b) None.
Applicability
(c) This AD applies to AvCraft Dornier Model 328-100 and -300
series airplanes, certificated in any category; as identified in
Dornier Service Bulletin SB-328J-27-176, Revision 1, dated April 15,
2003; and Dornier Service Bulletin SB-328-27-436, Revision 1, dated
April 15, 2003; as applicable.
Unsafe Condition
(d) This AD was prompted by a report that the flight control
systems do not have elements that are distinctively identified. We
are issuing this AD to prevent the incorrect re-assembly of the
flight control system during maintenance, which could result in
reduced controllability of the airplane.
Compliance
(e) You are responsible for having the actions required by this
AD performed within the compliance times specified, unless the
actions have already been done.
Installation
(f) Within 24 months after the effective date of this AD,
install colored identification strips on the pulley brackets,
fairlead bracket assemblies, operational assemblies, and flight
control cables, in accordance with the Accomplishment Instructions
of Dornier Service Bulletin SB-328J-27-176, Revision 1, dated April
15, 2003; or Dornier Service Bulletin SB-328-27-436, Revision 1,
dated April 15, 2003; as applicable.
Prior or Concurrent Requirements
(g) Prior to or concurrently with the accomplishment of the
actions in paragraph (f) of this AD, accomplish the actions in the
applicable service bulletins listed in Table 1 of this AD.
Table 1.--Prior or Concurrent Requirements
----------------------------------------------------------------------------------------------------------------
Dornier Service
Model Bulletin Revision Date Action
----------------------------------------------------------------------------------------------------------------
328-100 airplanes............ SB-328-27-290......... 1................ December 8, 2000..... Relocate the
auto-pilot
rudder servo.
SB-328-27-291......... 1................ December 8, 2000..... Relocate the
auto-pilot
aileron servo.
SB-328-27-292......... 1................ December 8, 2000..... Relocate the
auto pilot
elevator
servo.
328-300 airplanes............ SB-328J-27-035........ Original......... April 25, 2000....... Relocate the
auto-pilot
rudder servo.
SB-328J-27-036........ Original......... April 25, 2000....... Relocate the
auto-pilot
elevator
servo.
SB-328J-27-037........ Original......... April 25, 2000....... Relocate the
auto-2000
pilot aileron
servo.
----------------------------------------------------------------------------------------------------------------
[[Page 35516]]
Alternative Methods of Compliance (AMOCs)
(h) 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
(i) German airworthiness directive 2003-376, effective November
11, 2003; and German airworthiness directive 2003-377, effective
November 11, 2003; also address the subject of this AD.
Material Incorporated by Reference
(j) You must use the applicable service bulletins in Table 2 of
this AD 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 AvCraft Aerospace GmbH, P.O. Box
1103, D-82230 Wessling, Germany. 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.
Table 2.--Material Incorporated by Reference
------------------------------------------------------------------------
Dornier service bulletin Revision level Date
------------------------------------------------------------------------
SB-328-27-290................. 1............... December 8, 2000.
SB-328-27-291................. 1............... December 8, 2000.
SB-328-27-292................. 1............... December 8, 2000.
SB-328-27-436................. 1............... April 15, 2003.
SB-328J-27-035................ Original........ April 25, 2000.
SB-328J-27-036................ Original........ April 25, 2000.
SB-328J-27-037................ Original........ April 25, 2000.
SB-328J-27-176................ 1............... April 15, 2003.
------------------------------------------------------------------------
Issued in Renton, Washington, on June 10, 2005.
Michael J. Kaszycki,
Acting Manager, Transport Airplane Directorate,Aircraft Certification
Service.
[FR Doc. 05-12001 Filed 6-20-05; 8:45 am]
BILLING CODE 4910-13-P
