Airworthiness Directives; Fokker Model F.28 Mark 0070 and 0100 Airplanes, 14363-14365 [06-2674]
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Federal Register / Vol. 71, No. 55 / Wednesday, March 22, 2006 / Rules and Regulations
(f) Relevance to litigation—whether
the testimony and/or production of
records sought is relevant to the subject
litigation;
(g) Necessity—whether the testimony
and/or production of records, including
a release of such in camera, is
appropriate or necessary as determined
by either the procedural rules governing
the legal proceeding, or according to the
relevant laws concerning privilege;
(h) Availability from another source—
whether the information sought through
testimony or production of records is
available from another source;
(i) Violations of laws or regulations—
whether the testimony and/or
production of records would violate a
statute, regulation, executive order, or
other official directive;
(j) Classified information—whether
the testimony and/or production of
records would improperly reveal
information classified pursuant to
applicable statute or Executive Order;
and
(k) Compromise of rights and
interests—whether the testimony and/or
production of records would
compromise any of the following: law
enforcement interests, constitutional
rights, national security interests,
foreign policy interests, or the
confidentiality of commercial and/or
financial information.
cprice-sewell on PROD1PC70 with RULES
§ 404.31 Procedure for declining to testify
and/or produce records.
Ex-Im Bank personnel receiving a
demand to provide testimony and/or
produce records regarding information
acquired in the course of their
performance of official duties, or due to
their official status, and who have not
received written authorization from the
General Counsel to provide such
information, shall:
(a) Respectfully decline to answer or
appear for examination on the grounds
that such testimony is forbidden by this
subpart;
(b) Request the opportunity to consult
with the General Counsel;
(c) Explain that only upon
consultation may they be granted
approval to provide such testimony;
(d) Explain that providing such
testimony or records absent approval
may subject the individual to criminal
liability under 18 U.S.C. 641, as well as
other applicable laws, and other
disciplinary action; and
(e) Request a stay of the request or
demand pending a determination by the
General Counsel.
VerDate Aug<31>2005
15:10 Mar 21, 2006
Jkt 208001
§ 404.32 Procedure in the event a decision
concerning a demand is not made prior to
the time a response to the demand is
required.
If response to a demand is required
before a determination has been
rendered by the General Counsel, the
U.S. Attorney or such other attorney as
may be designated for the purpose will
appear with the Ex-Im Bank personnel
upon whom the demand has been made,
and will furnish the court or other
authority with a copy of the regulations
contained in this subpart and inform the
court or other authority that the demand
has been or is being, as the case may be,
referred for prompt consideration of the
General Counsel. The court or other
authority shall be requested respectfully
to stay the demand pending
determination by the General Counsel.
§ 404.33 Procedure in the event of an
adverse ruling.
If the court or other authority declines
to stay the effect of the demand in
response to a request made in
accordance with § 404.32 pending a
determination by the General Counsel,
or if the court or other authority rules
that the demand must be complied with
irrespective of the instructions from the
General Counsel not to produce the
material or disclose the information
sought, the Ex-Im Bank personnel upon
whom the demand has been made shall
respectfully decline to comply with the
demand (United States ex rel. Touhy v.
Ragen, 340 U.S. 462).
§ 404.34 Procedure for demands for
testimony or production of documents
regarding confidential information.
In addition to compliance with the
requirements of this subpart, demands
to provide testimony and/or produce
records that concern information
protected by the Privacy Act, 5 U.S.C.
552a, or any other authority mandating
confidentiality of certain classes of
records or information, must also satisfy
the requirements for disclosure imposed
by such authority before records may be
produced or testimony given.
§ 404.35 Procedures for requests for Ex-Im
Bank employees to provide expert or
opinion testimony.
No Ex-Im Bank personnel may, unless
specifically authorized by the General
Counsel, testify in any legal proceeding
as an expert or opinion witness as to
any matter related to his or her duties
or the functions of the Ex-Im Bank,
including the meaning of Ex-Im Bank
documents. Any demand for expert or
opinion testimony shall comply with
the policies and procedures outlined in
this subpart.
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§ 404.36
14363
No private right of action.
Nothing in this subpart shall be
construed as creating any right,
substantive or procedural, enforceable at
law or equity by a party against Ex-Im
Bank or the United States.
Dated: March 15, 2006.
Howard A. Schweitzer,
General Counsel (Acting), Export-Import
Bank of the United States.
[FR Doc. 06–2749 Filed 3–21–06; 8:45 am]
BILLING CODE 6690–01–M
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2005–23476; Directorate
Identifier 2005–NM–204–AD; Amendment
39–14516; AD 2006–06–07]
RIN 2120–AA64
Airworthiness Directives; Fokker
Model F.28 Mark 0070 and 0100
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
Fokker Model F.28 Mark 0070 and 0100
airplanes. This AD requires inspecting
the main landing gear (MLG) main
fitting for cracks, and repair if
necessary. This AD also requires
installing a placard and revising the
airplane flight manual to include
procedures to prohibit the application of
brakes during backward movement of
the airplane. This AD results from a
report that an MLG main fitting failed
on an airplane that was braking while
moving backward. We are issuing this
AD to detect and correct cracks in the
MLG main fitting, which could result in
reduced structural integrity of the MLG
main fitting.
DATES: This AD becomes effective April
26, 2006.
The Director of the Federal Register
approved the incorporation by reference
of certain publications listed in the AD
as of April 26, 2006.
ADDRESSES: You may examine the AD
docket on the Internet at https://
dms.dot.gov or in person at the Docket
Management Facility, U.S. Department
of Transportation, 400 Seventh Street
SW., Nassif Building, room PL–401,
Washington, DC.
Contact Fokker Services B.V.,
Technical Services Dept, P.O. Box 231,
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Federal Register / Vol. 71, No. 55 / Wednesday, March 22, 2006 / Rules and Regulations
Discussion
2150 AE Nieuw-Vennep, the
Netherlands, for service information
identified in this AD.
Tom
Rodriguez, Aerospace Engineer,
International Branch, ANM–116,
Transport Airplane Directorate, FAA,
1601 Lind Avenue, SW., Renton,
Washington 98055–4056; telephone
(425) 227–1137; fax (425) 227–1149.
FOR FURTHER INFORMATION CONTACT:
SUPPLEMENTARY INFORMATION:
Examining the Docket
You may examine the airworthiness
directive (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 street address stated in the
ADDRESSES section.
Explanation of Changes to the NPRM
The FAA issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 to include an AD that would
apply to certain Fokker Model F.28
Mark 0070 and 0100 airplanes. That
NPRM was published in the Federal
Register on January 4, 2006 (71 FR 293).
That NPRM proposed to require
inspecting the main landing gear (MLG)
main fitting for cracks, and repair if
necessary. That NPRM proposed also to
require installing a placard and revising
the airplane flight manual (AFM) to
include procedures to prohibit the
application of brakes during backward
movement of the airplane.
We have added the model number in
paragraph (f). We have also corrected a
typographical error in paragraph (g) of
the AD. We have also corrected the
service bulletin name in paragraphs (i)
and (j) of the AD, and corrected the
service bulletin reference in paragraphs
(h), (i) and (j) of the AD.
Comments
We provided the public the
opportunity to participate in the
development of this AD. We received no
comments on the NPRM or on the
determination of the cost to the public.
Conclusion
We have carefully reviewed the
available data, and determined that air
safety and the public interest require
adopting the AD with the changes
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
Action
Inspection .................................................
AFM Revision and Placard Installation ....
2
1
cprice-sewell on PROD1PC70 with RULES
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
VerDate Aug<31>2005
15:10 Mar 21, 2006
Average labor
rate per hour
Work hours
Jkt 208001
$65
65
Number of
U.S.-registered
airplanes
Cost per
airplane
Parts
$0
0
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 and placed it in the AD docket.
See the ADDRESSES section for a location
to examine the regulatory evaluation.
List of Subjects in 14 CFR Part 39
$130
65
11
11
Fleet cost
$1,430
715
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. The Federal Aviation
Administration (FAA) amends § 39.13
by adding the following new
airworthiness directive (AD):
I
2006–06–07 Fokker Services B.V.:
Amendment 39–14516. Docket No.
FAA–2005–23476; Directorate Identifier
2005–NM–204–AD.
Effective Date
(a) This AD becomes effective April 26,
2006.
Affected ADs
(b) None.
Adoption of the Amendment
Applicability
(c) This AD applies to Fokker Model F.28
Mark 0070 and 0100 airplanes, certificated in
any category; equipped with Messier-Dowty
main landing gears (MLGs).
Accordingly, under the authority
delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as
follows:
Unsafe Condition
(d) This AD results from a report that an
MLG main fitting failed on an airplane that
was braking while moving backward. We are
issuing this AD to detect and correct cracks
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
I
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Federal Register / Vol. 71, No. 55 / Wednesday, March 22, 2006 / Rules and Regulations
in the MLG main fitting, which could result
in reduced structural integrity of the MLG
main fitting.
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.
Airplane Flight Manual (AFM) Revision and
Placard Installation
(f) Within 14 days after the effective date
of this AD, amend the Limitations section of
the Fokker F.28 AFM to prohibit application
of brakes during backward movement of the
airplane. This may be done by inserting a
copy of this AD in the AFM.
Note 1: When a statement to prohibit
application of brakes during backward
movement of the airplane has been included
in the general revisions of the AFM, the
general revisions may be inserted into the
AFM, and the copy of this AD may be
removed from the AFM.
(g) Within 14 days after the effective date
of this AD, affix a placard on the pedestal,
next to the parking brake handle, having the
following wording: ‘‘APPLICATION OF
BRAKES DURING BACKWARD MOVEMENT
IS PROHIBITED.’’
cprice-sewell on PROD1PC70 with RULES
Inspection and Corrective Action
(h) At the applicable time specified in
paragraph (h)(1) or (h)(2) of this AD: Do an
eddy current inspection of the MLG main
fittings and repair before further flight as
applicable, in accordance with the
Accomplishment Instructions of MessierDowty Service Bulletin F100–32–106,
including Appendices A through C and
excluding Appendix D, dated February 18,
2005, except as provided by paragraphs (i)
and (j) of this AD.
(1) For airplanes on which an inspection
has not been done in accordance with
Messier-Dowty Service Bulletin F100–32–
104, Revision 2, dated October 30, 2003:
Within 3 months after the effective date of
this AD.
(2) For airplanes on which an inspection
has been done in accordance with MessierDowty Service Bulletin F100–32–104,
Revision 2, dated October 30, 2003: Within
2,000 flight cycles since the last inspection
done in accordance with the service bulletin
or within 3 months after the effective date of
this AD, whichever occurs later.
Exceptions to the Service Bulletin
(i) Where Messier-Dowty Service Bulletin
F100–32–106, including Appendices A
through C and excluding Appendix D, dated
February 18, 2005, specifies contacting the
manufacturer for repair: Before further flight,
repair using a method approved by either the
Manager, International Branch, ANM–116,
Transport Airplane Directorate, FAA; or the
Civil Aviation Authority—The Netherlands
(CAA–NL) (or its delegated agent).
(j) Although Messier-Dowty Service
Bulletin F100–32–106, including Appendices
A through C and excluding Appendix D,
dated February 18, 2005, specifies to submit
certain information to the manufacturer, this
AD does not include that requirement.
VerDate Aug<31>2005
15:10 Mar 21, 2006
Jkt 208001
Parts Installation
DEPARTMENT OF TRANSPORTATION
(k) As of the effective date of this AD, no
person may install, on any airplane, a
Messier-Dowty MLG, unless it has been
inspected/repaired according to paragraph
(h) of this AD.
Alternative Methods of Compliance
(AMOCs)
(l)(1) The Manager, International Branch,
ANM–116, has the authority to approve
AMOCs for this AD, if requested in
accordance with the procedures found in 14
CFR 39.19.
(2) Before using any AMOC approved in
accordance with § 39.19 on any airplane to
which the AMOC applies, notify the
appropriate principal inspector in the FAA
Flight Standards Certificate Holding District
Office.
Related Information
(m) Dutch airworthiness directives 2002–
115/2, dated October 8, 2004; and NL–2005–
002, dated April 14, 2005, also address the
subject of this AD.
Material Incorporated by Reference
(n) You must use Messier-Dowty Service
Bulletin F100–32–106, including Appendices
A through C and excluding Appendix D,
dated February 18, 2005; to perform the
actions that are required by this AD, unless
the AD specifies otherwise. The Director of
the Federal Register approved the
incorporation by reference of this document
in accordance with 5 U.S.C. 552(a) and 1 CFR
part 51. Contact Fokker Services B.V.,
Technical Services Dept, P.O. Box 231, 2150
AE Nieuw-Vennep, the Netherlands, for a
copy of this service information. You may
review copies at the Docket Management
Facility, U.S. Department of Transportation,
400 Seventh Street, SW., room PL–401,
Nassif Building, Washington, DC; on the
Internet at https://dms.dot.gov; or at 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 March
10, 2006.
Kalene C. Yanamura,
Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. 06–2674 Filed 3–21–06; 8:45 am]
BILLING CODE 4910–13–P
PO 00000
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Fmt 4700
14365
Sfmt 4700
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2005–23475; Directorate
Identifier 2005–NM–117–AD; Amendment
39–14518; AD 2006–06–09]
RIN 2120–AA64
Airworthiness Directives; Empresa
Brasileira de Aeronautica S.A.
(EMBRAER) Model ERJ 170 Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
SUMMARY: The FAA is adopting a new
airworthiness directive (AD) for all
EMBRAER Model ERJ 170 airplanes.
This AD requires revising the
Airworthiness Limitations section (ALS)
of the airplane maintenance manual
(AMM) to include new, specific
maintenance tasks related to the
incorporation of a new horizontal
stabilizer actuator. This AD also
requires revising the ALS of the AMM
to include revised repetitive inspection
intervals for certain tasks in the
maintenance plan related to the aileron
and flap/slat flight controls system. This
AD results from safety assessments of
the aileron and flap/slat flight controls
system, conducted after the type
certification of the airplane, which
showed that some dormant faults did
not comply with the safety assessment
criteria. We are issuing this AD to
prevent failure of the aileron and flap/
slat controls system, which could result
in reduced controllability of the
airplane.
DATES: This AD becomes effective April
26, 2006.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in the AD
as of April 26, 2006.
ADDRESSES: You may examine the AD
docket on the Internet at https://
dms.dot.gov or in person at the Docket
Management Facility, U.S. Department
of Transportation, 400 Seventh Street,
SW., Nassif Building, room PL–401,
Washington, DC.
Contact Empresa Brasileira de
Aeronautica S.A. (EMBRAER), P.O. Box
343—CEP 12.225, Sao Jose dos
Campos—SP, Brazil, for service
information identified in this AD.
FOR FURTHER INFORMATION CONTACT:
Todd Thompson, Aerospace Engineer,
International Branch, ANM–116,
Transport Airplane Directorate, FAA,
1601 Lind Avenue, SW., Renton,
E:\FR\FM\22MRR1.SGM
22MRR1
]]>Agencies
[Federal Register Volume 71, Number 55 (Wednesday, March 22, 2006)]
[Rules and Regulations]
[Pages 14363-14365]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 06-2674]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2005-23476; Directorate Identifier 2005-NM-204-AD;
Amendment 39-14516; AD 2006-06-07]
RIN 2120-AA64
Airworthiness Directives; Fokker Model F.28 Mark 0070 and 0100
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 Fokker Model F.28 Mark 0070 and 0100 airplanes. This AD
requires inspecting the main landing gear (MLG) main fitting for
cracks, and repair if necessary. This AD also requires installing a
placard and revising the airplane flight manual to include procedures
to prohibit the application of brakes during backward movement of the
airplane. This AD results from a report that an MLG main fitting failed
on an airplane that was braking while moving backward. We are issuing
this AD to detect and correct cracks in the MLG main fitting, which
could result in reduced structural integrity of the MLG main fitting.
DATES: This AD becomes effective April 26, 2006.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in the AD as of April 26,
2006.
ADDRESSES: You may examine the AD docket on the Internet at https://
dms.dot.gov or in person at the Docket Management Facility, U.S.
Department of Transportation, 400 Seventh Street SW., Nassif Building,
room PL-401, Washington, DC.
Contact Fokker Services B.V., Technical Services Dept, P.O. Box
231,
[[Page 14364]]
2150 AE Nieuw-Vennep, the Netherlands, for service information
identified in this AD.
FOR FURTHER INFORMATION CONTACT: Tom Rodriguez, Aerospace Engineer,
International Branch, ANM-116, Transport Airplane Directorate, FAA,
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425)
227-1137; fax (425) 227-1149.
SUPPLEMENTARY INFORMATION:
Examining the Docket
You may examine the airworthiness directive (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 street address stated in the ADDRESSES section.
Discussion
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 to include an AD that would apply to certain Fokker Model
F.28 Mark 0070 and 0100 airplanes. That NPRM was published in the
Federal Register on January 4, 2006 (71 FR 293). That NPRM proposed to
require inspecting the main landing gear (MLG) main fitting for cracks,
and repair if necessary. That NPRM proposed also to require installing
a placard and revising the airplane flight manual (AFM) to include
procedures to prohibit the application of brakes during backward
movement of the airplane.
Comments
We provided the public the opportunity to participate in the
development of this AD. We received no comments on the NPRM or on the
determination of the cost to the public.
Explanation of Changes to the NPRM
We have added the model number in paragraph (f). We have also
corrected a typographical error in paragraph (g) of the AD. We have
also corrected the service bulletin name in paragraphs (i) and (j) of
the AD, and corrected the service bulletin reference in paragraphs (h),
(i) and (j) of the AD.
Conclusion
We have carefully reviewed the available data, and determined that
air safety and the public interest require adopting the AD with the
changes 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
--------------------------------------------------------------------------------------------------------------------------------------------------------
Inspection.............................................. 2 $65 $0 $130 11 $1,430
AFM Revision and Placard Installation................... 1 65 0 65 11 715
--------------------------------------------------------------------------------------------------------------------------------------------------------
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 and placed it in the AD docket. 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
0
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 Federal Aviation Administration (FAA) amends Sec. 39.13 by
adding the following new airworthiness directive (AD):
2006-06-07 Fokker Services B.V.: Amendment 39-14516. Docket No. FAA-
2005-23476; Directorate Identifier 2005-NM-204-AD.
Effective Date
(a) This AD becomes effective April 26, 2006.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Fokker Model F.28 Mark 0070 and 0100
airplanes, certificated in any category; equipped with Messier-Dowty
main landing gears (MLGs).
Unsafe Condition
(d) This AD results from a report that an MLG main fitting
failed on an airplane that was braking while moving backward. We are
issuing this AD to detect and correct cracks
[[Page 14365]]
in the MLG main fitting, which could result in reduced structural
integrity of the MLG main fitting.
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.
Airplane Flight Manual (AFM) Revision and Placard Installation
(f) Within 14 days after the effective date of this AD, amend
the Limitations section of the Fokker F.28 AFM to prohibit
application of brakes during backward movement of the airplane. This
may be done by inserting a copy of this AD in the AFM.
Note 1: When a statement to prohibit application of brakes
during backward movement of the airplane has been included in the
general revisions of the AFM, the general revisions may be inserted
into the AFM, and the copy of this AD may be removed from the AFM.
(g) Within 14 days after the effective date of this AD, affix a
placard on the pedestal, next to the parking brake handle, having
the following wording: ``APPLICATION OF BRAKES DURING BACKWARD
MOVEMENT IS PROHIBITED.''
Inspection and Corrective Action
(h) At the applicable time specified in paragraph (h)(1) or
(h)(2) of this AD: Do an eddy current inspection of the MLG main
fittings and repair before further flight as applicable, in
accordance with the Accomplishment Instructions of Messier-Dowty
Service Bulletin F100-32-106, including Appendices A through C and
excluding Appendix D, dated February 18, 2005, except as provided by
paragraphs (i) and (j) of this AD.
(1) For airplanes on which an inspection has not been done in
accordance with Messier-Dowty Service Bulletin F100-32-104, Revision
2, dated October 30, 2003: Within 3 months after the effective date
of this AD.
(2) For airplanes on which an inspection has been done in
accordance with Messier-Dowty Service Bulletin F100-32-104, Revision
2, dated October 30, 2003: Within 2,000 flight cycles since the last
inspection done in accordance with the service bulletin or within 3
months after the effective date of this AD, whichever occurs later.
Exceptions to the Service Bulletin
(i) Where Messier-Dowty Service Bulletin F100-32-106, including
Appendices A through C and excluding Appendix D, dated February 18,
2005, specifies contacting the manufacturer for repair: Before
further flight, repair using a method approved by either the
Manager, International Branch, ANM-116, Transport Airplane
Directorate, FAA; or the Civil Aviation Authority--The Netherlands
(CAA-NL) (or its delegated agent).
(j) Although Messier-Dowty Service Bulletin F100-32-106,
including Appendices A through C and excluding Appendix D, dated
February 18, 2005, specifies to submit certain information to the
manufacturer, this AD does not include that requirement.
Parts Installation
(k) As of the effective date of this AD, no person may install,
on any airplane, a Messier-Dowty MLG, unless it has been inspected/
repaired according to paragraph (h) of this AD.
Alternative Methods of Compliance (AMOCs)
(l)(1) The Manager, International Branch, ANM-116, has the
authority to approve AMOCs for this AD, if requested in accordance
with the procedures found in 14 CFR 39.19.
(2) Before using any AMOC approved in accordance with Sec.
39.19 on any airplane to which the AMOC applies, notify the
appropriate principal inspector in the FAA Flight Standards
Certificate Holding District Office.
Related Information
(m) Dutch airworthiness directives 2002-115/2, dated October 8,
2004; and NL-2005-002, dated April 14, 2005, also address the
subject of this AD.
Material Incorporated by Reference
(n) You must use Messier-Dowty Service Bulletin F100-32-106,
including Appendices A through C and excluding Appendix D, dated
February 18, 2005; to perform the actions that are required by this
AD, unless the AD specifies otherwise. The Director of the Federal
Register approved the incorporation by reference of this document in
accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Contact Fokker
Services B.V., Technical Services Dept, P.O. Box 231, 2150 AE Nieuw-
Vennep, the Netherlands, for a copy of this service information. You
may review copies at the Docket Management Facility, U.S. Department
of Transportation, 400 Seventh Street, SW., room PL-401, Nassif
Building, Washington, DC; on the Internet at https://dms.dot.gov; or
at 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 March 10, 2006.
Kalene C. Yanamura,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 06-2674 Filed 3-21-06; 8:45 am]
BILLING CODE 4910-13-P
