Airworthiness Directives; Fokker Model F.28 Mark 0070 and 0100 Airplanes, 6343-6345 [06-988]
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<![CDATA[
Federal Register / Vol. 71, No. 26 / Wednesday, February 8, 2006 / Rules and Regulations
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, Safety.
Adoption of the Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as
follows:
rmajette on PROD1PC67 with RULES1
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.
VerDate Aug<31>2005
15:23 Feb 07, 2006
Jkt 208001
§ 39.13
[Amended]
2. The Federal Aviation
Administration (FAA) amends § 39.13
by adding the following new
airworthiness directive (AD):
I
2006–03–16 Hamburger Flugzeugbau
GmbH: Amendment 39–14480. Docket
No. FAA–2005–22401; Directorate
Identifier 2004–NM–93–AD.
6343
Material Incorporated by Reference
(j) None.
Issued in Renton, Washington, on January
31, 2006.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 06–1147 Filed 2–7–06; 8:45 am]
BILLING CODE 4910–13–P
Effective Date
(a) This AD becomes effective March 15,
2006.
DEPARTMENT OF TRANSPORTATION
Affected ADs
Federal Aviation Administration
(b) None.
14 CFR Part 39
Applicability
(c) This AD applies to all Hamburger
Flugzeugbau GmbH Model HFB 320 HANSA
airplanes, certificated in any category.
[Docket No. FAA–2005–22748; Directorate
Identifier 2005–NM–127–AD; Amendment
39–14471; AD 2006–03–07]
Unsafe Condition
RIN 2120–AA64
(d) This AD results from a report that all
airplanes in operation might have met or
exceeded the designed life limit for the
primary structure. We are issuing this AD to
prevent continued operation of an airplane
beyond its designed life limit for the primary
structure, which could result in reduced
structural integrity 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.
Airworthiness Limitations Revision
(f) Within 30 days after the effective date
of this AD: Revise the Limitations section of
the HFB 320 Hansa Airplane Flight Manual
(AFM) to state the following (or insert a copy
of this AD into the Limitations section):
‘‘Do not operate the airplane beyond 15,000
total flight cycles, or 15,000 total flight hours,
whichever occurs first.’’
(g) This limitation may be removed from
the HFB 320 Hansa AFM after the Manager,
International Branch, ANM–116, FAA,
approves analysis that would substantiate
continued safe operation beyond the
designed life limit of 15,000 total flight
cycles, or within 15,000 total flight hours on
the airplane, whichever occurs first.
Alternative Methods of Compliance
(AMOCs)
(h)(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
(i) German airworthiness directive 2002–
158, effective October 3, 2002, also addresses
the subject of this AD.
PO 00000
Frm 00007
Fmt 4700
Sfmt 4700
Airworthiness Directives; Fokker
Model F.28 Mark 0070 and 0100
Airplanes
Federal Aviation
Administration, 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 modifying
the passenger door and installing new
placards. This AD results from reports
of the airstairs-type passenger door
opening during flight. We are issuing
this AD to prevent rapid decompression
of the airplane, or ejection of a
passenger or crew member out the door
during flight.
DATES: This AD becomes effective
March 15, 2006.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in the AD
as of March 15, 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., P.O.
Box 231, 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:
E:\FR\FM\08FER1.SGM
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6344
Federal Register / Vol. 71, No. 26 / Wednesday, February 8, 2006 / Rules and Regulations
Examining the Docket
Discussion
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.
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 October 21, 2005 (70 FR
61239). That NPRM proposed to require
modifying the passenger door and
installing new placards.
Comments
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 as proposed.
Costs of Compliance
The following table provides the
estimated costs for U.S. operators to
comply with this AD.
We provided the public the
opportunity to participate in the
ESTIMATED COSTS
Work
hours
Action
Modify door and install placards ..............................
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.
rmajette on PROD1PC67 with RULES1
Regulatory Findings
19:51 Feb 07, 2006
17–18
$65
Parts
Cost per airplane
$2,645
Jkt 208001
Number
of U.S.registered
airplanes
$3,750–3,815
2
Fleet cost
$7,500–7,630
(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.
Affected ADs
List of Subjects in 14 CFR Part 39
(d) This AD results from reports of the
airstairs-type passenger door opening during
flight. We are issuing this AD to prevent
rapid decompression of the airplane, or
ejection of a passenger or crew member out
the door during flight.
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:
I
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
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
2006–03–07 Fokker Services B.V.:
Amendment 39–14471. Docket No.
FAA–2005–22748; Directorate Identifier
2005–NM–127–AD.
Effective Date
(a) This AD becomes effective March 15,
2006.
PO 00000
Frm 00008
Fmt 4700
Sfmt 4700
(b) None.
Applicability
(c) This AD applies to Fokker Model F.28
Mark 0070 and 0100 airplanes, certificated in
any category, as identified in Fokker Service
Bulletin SBF100–52–069, Revision 3, dated
December 18, 2002.
Unsafe Condition
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
I
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
VerDate Aug<31>2005
Average
labor rate
per hour
(f) Within 30 months after the effective
date of this AD, modify the passenger door
and install new placards, in accordance with
the Accomplishment Instructions of Fokker
Service Bulletin SBF100–52–069, Revision 3,
dated December 18, 2002; including Fokker
Manual Change Notification—Operational
Documentation MCNO–F100–031, dated
December 3, 2001; and Fokker Manual
Change Notification—Maintenance
Documentation MCNM–F100–064, Revision
2, dated December 18, 2002; and including
the drawings listed in Table 1 of this AD. (To
conform to certain Office of the Federal
Register requirements for incorporating these
materials by reference, the table identifies the
date of the service bulletin for undated
drawings.)
E:\FR\FM\08FER1.SGM
08FER1
6345
Federal Register / Vol. 71, No. 26 / Wednesday, February 8, 2006 / Rules and Regulations
TABLE 1.—DRAWINGS INCLUDED IN SERVICE BULLETIN SBF100–52–069
Fokker drawing
W41074
W41418
W41418
W41418
W41418
W41418
W42310
W42310
W42310
W59243
W59261
W59261
Sheet
....................................................................................................................................
....................................................................................................................................
....................................................................................................................................
....................................................................................................................................
....................................................................................................................................
....................................................................................................................................
....................................................................................................................................
....................................................................................................................................
....................................................................................................................................
....................................................................................................................................
....................................................................................................................................
....................................................................................................................................
Alternative Methods of Compliance
(AMOCs)
(g)(1) 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.
(2) Before using any AMOC approved in
accordance with 14 CFR 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
(h) Dutch airworthiness directive 2002–
057, dated April 29, 2002, also addresses the
subject of this AD.
Material Incorporated by Reference
(i) You must use Fokker Service Bulletin
SBF100–52–069, Revision 3, dated December
18, 2002; including Fokker Manual Change
Notification—Operational Documentation
MCNO–F100–031, dated December 3, 2001;
and including Fokker Manual Change
Notification—Maintenance Documentation
MCNM–F100–064, Revision 2, dated
December 18, 2002; and including the
drawings listed in Table 2 of this AD, to do
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., P.O.
Issue
065
003
005
006
007
008
001
002
003
024
017
025
Date
DB
L
E
E
E
M
D
B
F
AU
W
S
December 18, 2002.
December 18, 2002.
December 18, 2002.
December 18, 2002.
December 18, 2002.
December 18, 2002.
August 14, 2000.
August 14, 2000.
June 11, 2001.
June 12, 2001.
August 9, 2002.
July 3, 2001.
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.
TABLE 2.—DRAWINGS INCLUDED IN SERVICE BULLETIN SBF100–52–069
Fokker drawing
W41074
W41418
W41418
W41418
W41418
W41418
W42310
W42310
W42310
W59243
W59261
W59261
....................................................................................................................................
....................................................................................................................................
....................................................................................................................................
....................................................................................................................................
....................................................................................................................................
....................................................................................................................................
....................................................................................................................................
....................................................................................................................................
....................................................................................................................................
....................................................................................................................................
....................................................................................................................................
....................................................................................................................................
Issued in Renton, Washington, on January
26, 2006.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 06–988 Filed 2–7–06; 8:45 am]
BILLING CODE 4910–13–P
rmajette on PROD1PC67 with RULES1
Sheet
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 97
[Docket No. 30478; Amdt. No. 3152]
Standard Instrument Approach
Procedures, Weather Takeoff
Minimums; Miscellaneous
Amendments
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
SUMMARY: This amendment establishes,
amends, suspends, or revokes Standard
VerDate Aug<31>2005
15:23 Feb 07, 2006
Jkt 208001
PO 00000
Frm 00009
Fmt 4700
Sfmt 4700
Issue
065
003
005
006
007
008
001
002
003
024
017
025
Date
DB
L
E
E
E
M
D
B
F
AU
W
S
December 18, 2002.
December 18, 2002.
December 18, 2002.
December 18, 2002.
December 18, 2002.
December 18, 2002.
August 14, 2000.
August 14, 2000.
June 11, 2001.
June 12, 2001.
August 9, 2002.
July 3, 2001.
Instrument Approach Procedures
(SIAPs) and/or Weather Takeoff
Minimums for operations at certain
airports. These regulatory actions are
needed because of the adoption of new
or revised criteria, or because of changes
occurring in the National Airspace
System, such as the commissioning of
new navigational facilities, addition of
new obstacles, or changes in air traffic
requirements. These changes are
designed to provide safe and efficient
use of the navigable airspace and to
promote safe flight operations under
instrument flight rules at the affected
airports.
E:\FR\FM\08FER1.SGM
08FER1
]]>Agencies
[Federal Register Volume 71, Number 26 (Wednesday, February 8, 2006)]
[Rules and Regulations]
[Pages 6343-6345]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 06-988]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2005-22748; Directorate Identifier 2005-NM-127-AD;
Amendment 39-14471; AD 2006-03-07]
RIN 2120-AA64
Airworthiness Directives; Fokker Model F.28 Mark 0070 and 0100
Airplanes
AGENCY: Federal Aviation Administration, 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 modifying the passenger door and installing new placards. This
AD results from reports of the airstairs-type passenger door opening
during flight. We are issuing this AD to prevent rapid decompression of
the airplane, or ejection of a passenger or crew member out the door
during flight.
DATES: This AD becomes effective March 15, 2006.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in the AD as of March 15,
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., P.O. Box 231, 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:
[[Page 6344]]
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 October 21, 2005 (70 FR 61239). That NPRM proposed
to require modifying the passenger door and installing new placards.
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 as proposed.
Costs of Compliance
The following table provides the estimated costs for U.S. operators
to comply with this AD.
Estimated Costs
--------------------------------------------------------------------------------------------------------------------------------------------------------
Average Number of
Work labor U.S.-
Action hours rate per Parts Cost per airplane registered Fleet cost
hour airplanes
--------------------------------------------------------------------------------------------------------------------------------------------------------
Modify door and install placards................................... 17-18 $65 $2,645 $3,750-3,815 2 $7,500-7,630
--------------------------------------------------------------------------------------------------------------------------------------------------------
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):
2006-03-07 Fokker Services B.V.: Amendment 39-14471. Docket No. FAA-
2005-22748; Directorate Identifier 2005-NM-127-AD.
Effective Date
(a) This AD becomes effective March 15, 2006.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Fokker Model F.28 Mark 0070 and 0100
airplanes, certificated in any category, as identified in Fokker
Service Bulletin SBF100-52-069, Revision 3, dated December 18, 2002.
Unsafe Condition
(d) This AD results from reports of the airstairs-type passenger
door opening during flight. We are issuing this AD to prevent rapid
decompression of the airplane, or ejection of a passenger or crew
member out the door during flight.
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 30 months after the effective date of this AD, modify
the passenger door and install new placards, in accordance with the
Accomplishment Instructions of Fokker Service Bulletin SBF100-52-
069, Revision 3, dated December 18, 2002; including Fokker Manual
Change Notification--Operational Documentation MCNO-F100-031, dated
December 3, 2001; and Fokker Manual Change Notification--Maintenance
Documentation MCNM-F100-064, Revision 2, dated December 18, 2002;
and including the drawings listed in Table 1 of this AD. (To conform
to certain Office of the Federal Register requirements for
incorporating these materials by reference, the table identifies the
date of the service bulletin for undated drawings.)
[[Page 6345]]
Table 1.--Drawings Included in Service Bulletin SBF100-52-069
----------------------------------------------------------------------------------------------------------------
Fokker drawing Sheet Issue Date
----------------------------------------------------------------------------------------------------------------
W41074..................................... 065 DB December 18, 2002.
W41418..................................... 003 L December 18, 2002.
W41418..................................... 005 E December 18, 2002.
W41418..................................... 006 E December 18, 2002.
W41418..................................... 007 E December 18, 2002.
W41418..................................... 008 M December 18, 2002.
W42310..................................... 001 D August 14, 2000.
W42310..................................... 002 B August 14, 2000.
W42310..................................... 003 F June 11, 2001.
W59243..................................... 024 AU June 12, 2001.
W59261..................................... 017 W August 9, 2002.
W59261..................................... 025 S July 3, 2001.
----------------------------------------------------------------------------------------------------------------
Alternative Methods of Compliance (AMOCs)
(g)(1) 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.
(2) Before using any AMOC approved in accordance with 14 CFR
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
(h) Dutch airworthiness directive 2002-057, dated April 29,
2002, also addresses the subject of this AD.
Material Incorporated by Reference
(i) You must use Fokker Service Bulletin SBF100-52-069, Revision
3, dated December 18, 2002; including Fokker Manual Change
Notification--Operational Documentation MCNO-F100-031, dated
December 3, 2001; and including Fokker Manual Change Notification--
Maintenance Documentation MCNM-F100-064, Revision 2, dated December
18, 2002; and including the drawings listed in Table 2 of this AD,
to do 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., 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.
Table 2.--Drawings Included in Service Bulletin SBF100-52-069
----------------------------------------------------------------------------------------------------------------
Fokker drawing Sheet Issue Date
----------------------------------------------------------------------------------------------------------------
W41074..................................... 065 DB December 18, 2002.
W41418..................................... 003 L December 18, 2002.
W41418..................................... 005 E December 18, 2002.
W41418..................................... 006 E December 18, 2002.
W41418..................................... 007 E December 18, 2002.
W41418..................................... 008 M December 18, 2002.
W42310..................................... 001 D August 14, 2000.
W42310..................................... 002 B August 14, 2000.
W42310..................................... 003 F June 11, 2001.
W59243..................................... 024 AU June 12, 2001.
W59261..................................... 017 W August 9, 2002.
W59261..................................... 025 S July 3, 2001.
----------------------------------------------------------------------------------------------------------------
Issued in Renton, Washington, on January 26, 2006.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 06-988 Filed 2-7-06; 8:45 am]
BILLING CODE 4910-13-P
