Airworthiness Directives; Fokker Model F.28 Mark 0070 and 0100 Airplanes, 43033-43035 [E6-12092]
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Federal Register / Vol. 71, No. 146 / Monday, July 31, 2006 / Rules and Regulations
Issued in Renton, Washington, on July 20,
2006.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. E6–12139 Filed 7–28–06; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2006–24868; Directorate
Identifier 2006–NM–103–AD; Amendment
39–14698; AD 2006–15–17]
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.
rmajette on PROD1PC67 with RULES1
AGENCY:
SUMMARY: The FAA is adopting a new
airworthiness directive (AD) for all
Fokker Model F.28 Mark 0070 and 0100
airplanes. This AD requires
modification of the wiring distribution
of the alternating current bus transfer
power system and the right-hand and
left-hand windshield anti-icing system,
as necessary. This AD results from a
report of electrical sparks coming out of
the flight deck from a panel behind the
left seat. We are issuing this AD to
prevent failure of the sliding window
heating element(s), due to electrical
overload, which could result in smoke
and fire in the cockpit.
DATES: This AD becomes effective
September 5, 2006.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in the AD
as of September 5, 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,
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 98057–3356; telephone
(425) 227–1137; fax (425) 227–1149.
VerDate Aug<31>2005
14:56 Jul 28, 2006
Jkt 208001
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 all Fokker Model F.28 Mark
0070 and 0100 airplanes. That NPRM
was published in the Federal Register
on May 25, 2006 (71 FR 30072). That
NPRM proposed to require modification
of the wiring distribution of the
alternating current bus transfer power
system and the right-hand and left-hand
windshield anti-icing system, as
necessary.
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.
43033
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.
Costs of Compliance
Adoption of the Amendment
This AD will affect about 10 airplanes
of U.S. registry. The required actions
will take about 3 work hours per
airplane, at an average labor rate of $80
per work hour. Based on these figures,
the estimated cost of the AD for U.S.
operators is $2,400, or $240 per
airplane.
I
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
PO 00000
Frm 00003
Fmt 4700
Sfmt 4700
Accordingly, under the authority
delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as
follows:
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
2006–15–17 Fokker Services B.V.:
Amendment 39–14698. Docket No.
FAA–2006–24868; Directorate Identifier
2006–NM–103–AD.
Effective Date
(a) This AD becomes effective September 5,
2006.
E:\FR\FM\31JYR1.SGM
31JYR1
43034
Federal Register / Vol. 71, No. 146 / Monday, July 31, 2006 / Rules and Regulations
Affected ADs
(b) None.
electrical overload, which could result in
smoke and fire in the cockpit.
Applicability
(c) This AD applies to all Fokker Model
F.28 Mark 0070 and 0100 airplanes,
certificated in any category.
Compliance
Unsafe Condition
(d) This AD results from a report of
electrical sparks coming out of the flight deck
from a panel behind the left seat. We are
issuing this AD to prevent failure of the
sliding window heating element(s), due to
(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.
Modification of Wiring Distribution
(f) Within 36 months after the effective
date of this AD, modify the wiring
distribution of the alternating current bus
transfer power system and the right-hand and
left-hand windshield anti-icing system, by
accomplishing all of the actions specified in
the Accomplishment Instructions of Fokker
Service Bulletin SBF100–30–027, dated May
9, 2005, as applicable; including Fokker
Manual Change Notification—Maintenance
Documentation MCNM F100–098, dated May
9, 2005, and 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.)
TABLE 1.—DRAWINGS INCLUDED IN FOKKER SERVICE BULLETIN SBF100–30–027
Fokker drawing
W41043
W41043
W41249
W41249
W41249
W41249
W41249
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 § 39.19 on any airplane to
which the AMOC applies, notify the
appropriate principal inspector in the FAA
Flight Standards Certificate Holding District
Office.
007
008
006
007
008
009
010
Issue
H
H
F
F
F
G
G
.................................................................
.................................................................
.................................................................
.................................................................
.................................................................
.................................................................
.................................................................
Related Information
(h) Dutch airworthiness directive NL–
2005–009, dated June 30, 2005, also
addresses the subject of this AD.
Material Incorporated by Reference
(i) You must use Fokker Service Bulletin
SBF100–30–027, dated May 9, 2005;
including Fokker Manual Change
Notification—Maintenance Documentation
MCNM F100–098, dated May 9, 2005; and
the Fokker drawings identified 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 approved the incorporation by
reference of this document in accordance
Date
May
May
May
May
May
May
May
9,
9,
9,
9,
9,
9,
9,
2005.
2005.
2005.
2005.
2005.
2005.
2005.
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.
TABLE 2.—ATTACHED DRAWINGS INCORPORATED BY REFERENCE
Fokker drawing
rmajette on PROD1PC67 with RULES1
W41043
W41043
W41249
W41249
W41249
W41249
W41249
Sheet
....................................................................................................
....................................................................................................
....................................................................................................
....................................................................................................
....................................................................................................
....................................................................................................
....................................................................................................
VerDate Aug<31>2005
14:56 Jul 28, 2006
Jkt 208001
PO 00000
Frm 00004
Fmt 4700
007
008
006
007
008
009
010
Sfmt 4700
Issue
H
H
F
F
F
G
G
.................................................................
.................................................................
.................................................................
.................................................................
.................................................................
.................................................................
.................................................................
E:\FR\FM\31JYR1.SGM
31JYR1
Date
May
May
May
May
May
May
May
9,
9,
9,
9,
9,
9,
9,
2005.
2005.
2005.
2005.
2005.
2005.
2005.
Federal Register / Vol. 71, No. 146 / Monday, July 31, 2006 / Rules and Regulations
Issued in Renton, Washington, on July 20,
2006.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. E6–12092 Filed 7–28–06; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2001–NM–387–AD; Amendment
39–14696; AD 2006–15–15]
RIN 2120–AA64
Airworthiness Directives; McDonnell
Douglas Model DC–9–81 (MD–81), DC–
9–82 (MD–82), DC–9–83 (MD–83), DC–
9–87 (MD–87), and MD–88 Airplanes
Federal Aviation
Administration, DOT.
ACTION: Final rule.
rmajette on PROD1PC67 with RULES1
AGENCY:
SUMMARY: This amendment adopts a
new airworthiness directive (AD),
applicable to certain McDonnell
Douglas airplane models, that requires a
one-time inspection for chafing or signs
of arcing of the wire bundle for the
auxiliary hydraulic pump, and other
specified and corrective actions, as
applicable. This AD also requires that,
for certain airplanes, installation of
additional protective sleeving on the
upper portion of the auxiliary hydraulic
pump wire assembly. This AD results
from reports of shorted wires and
evidence of arcing on the power cables
of the auxiliary hydraulic pump, as well
a fuel system reviews conducted by the
manufacturer. We are issuing this AD to
prevent shorted wires or arcing at the
auxiliary hydraulic pump, which could
result in loss of auxiliary hydraulic
power, or a fire in the wheel well of the
airplane. The actions specified by this
AD are also intended to reduce the
potential of an ignition source adjacent
to the fuel tanks, which, in combination
with flammable fuel vapors, could result
in a fuel tank explosion and consequent
loss of the airplane.
DATES: Effective September 5, 2006.
The incorporation by reference of a
certain publication listed in the
regulations is approved by the Director
of the Federal Register as of September
5, 2006.
ADDRESSES: The service information
referenced in this AD may be obtained
from Boeing Commercial Airplanes,
Long Beach Division, 3855 Lakewood
Boulevard, Long Beach, California
90846, Attention: Data and Service
VerDate Aug<31>2005
14:56 Jul 28, 2006
Jkt 208001
Management, Dept. C1–L5A (D800–
0024). This information may be
examined at the FAA, Transport
Airplane Directorate, 1601 Lind
Avenue, SW., Renton, Washington; or at
the FAA, Los Angeles Aircraft
Certification Office, 3960 Paramount
Boulevard, Lakewood, California.
FOR FURTHER INFORMATION CONTACT:
Elvin Wheeler, Aerospace Engineer,
Systems and Equipment Branch, ANM–
130L, FAA, Los Angeles Aircraft
Certification Office, 3960 Paramount
Boulevard, Lakewood, California
90712–4137; telephone (562) 627–5344;
fax (562) 627–5210.
SUPPLEMENTARY INFORMATION: A
proposal to amend part 39 of the Federal
Aviation Regulations (14 CFR part 39) to
include an airworthiness directive (AD)
that is applicable to certain McDonnell
Douglas Model DC–9–81 (MD–81), DC–
9–82 (MD–82), DC–9–83 (MD–83), DC–
9–87 (MD–87), and MD–88 airplanes,
was published as a second
supplemental notice of proposed
rulemaking (NPRM) in the Federal
Register on March 14, 2006 (71 FR
13050). That action proposed to require
a one-time inspection for chafing or
signs of arcing of the wire bundle for the
auxiliary hydraulic pump, and other
specified and corrective actions, as
applicable. That action also proposed to
require, for certain airplanes,
installation of additional protective
sleeving on the upper portion of the
auxiliary hydraulic pump wire
assembly.
Comments
We provided the public the
opportunity to participate in the
development of this AD. No comments
have been received on the second
supplemental NPRM or on the
determination of the cost to the public.
Explanation of Changes to the Second
Supplemental NPRM
In paragraph (a) of the second
supplemental NPRM we inadvertently
referred to Configurations 1 through 3
when we should have referred to
Configurations 1 through 4. It was our
intent that the requirements of
paragraph (a) apply to Configurations 1
through 4 airplanes, as described in the
referenced Boeing Alert Service Bulletin
MD80–29A070, Revision 1, dated July
28, 2005. As described in the preamble
of the second supplemental NPRM, we
added paragraph (c) to this AD to give
credit for actions done before the
effective date of this AD in accordance
with the original issue of Boeing Alert
Service Bulletin MD80–29A070, dated
August 3, 2004, except that the
PO 00000
Frm 00005
Fmt 4700
Sfmt 4700
43035
additional requirements of paragraph (b)
of this AD must be done on airplanes in
Configuration 4, as defined in Boeing
Alert Service Bulletin MD80–29A070,
Revision 1. Therefore, we have revised
paragraph (a) of this AD accordingly.
We also have clarified the Cost Impact
section of this AD in regard to the
airplane configurations.
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 this change will neither
increase the economic burden on any
operator nor increase the scope of the
AD.
Cost Impact
There are approximately 1,063
airplanes of the affected design in the
worldwide fleet. We estimate that 732
airplanes of U.S. registry (i.e., airplane
Configurations 1 through 4; we do not
know how many airplanes are in
Configuration 4) will be affected by this
AD, that it will take up to 12 work hours
per airplane to accomplish the required
inspection and other specified actions,
and that the average labor rate is $65 per
work hour. Required parts will cost up
to $524 per airplane. Based on these
figures, the cost impact of this AD on
U.S. operators is estimated to be up to
$954,528, or up to $1,304 per airplane.
For airplanes in Configuration 4, as
defined in Boeing Alert Service Bulletin
MD80–29A070, Revision 1, it will take
approximately 2 work hours to
accomplish the required additional
wiring protection, at an average labor
rate of $65 per work hour. Required
parts will cost approximately $40 per
airplane. Based on these figures, the cost
impact of this action on an affected
airplane is estimated to be $170 per
airplane.
The cost impact figures discussed
above are based on assumptions that no
operator has yet accomplished any of
the proposed requirements of this AD
action, and that no operator would
accomplish those actions in the future if
this AD were not adopted. The cost
impact figures discussed in AD
rulemaking actions represent only the
time necessary to perform the specific
actions actually required by the AD.
These figures typically do not include
incidental costs, such as the time
required to gain access and close up,
planning time, or time necessitated by
other administrative actions.
E:\FR\FM\31JYR1.SGM
31JYR1
]]>Agencies
[Federal Register Volume 71, Number 146 (Monday, July 31, 2006)]
[Rules and Regulations]
[Pages 43033-43035]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E6-12092]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2006-24868; Directorate Identifier 2006-NM-103-AD;
Amendment 39-14698; AD 2006-15-17]
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 all
Fokker Model F.28 Mark 0070 and 0100 airplanes. This AD requires
modification of the wiring distribution of the alternating current bus
transfer power system and the right-hand and left-hand windshield anti-
icing system, as necessary. This AD results from a report of electrical
sparks coming out of the flight deck from a panel behind the left seat.
We are issuing this AD to prevent failure of the sliding window heating
element(s), due to electrical overload, which could result in smoke and
fire in the cockpit.
DATES: This AD becomes effective September 5, 2006.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in the AD as of September 5,
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, 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 98057-3356; 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 all Fokker Model F.28
Mark 0070 and 0100 airplanes. That NPRM was published in the Federal
Register on May 25, 2006 (71 FR 30072). That NPRM proposed to require
modification of the wiring distribution of the alternating current bus
transfer power system and the right-hand and left-hand windshield anti-
icing system, as necessary.
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
This AD will affect about 10 airplanes of U.S. registry. The
required actions will take about 3 work hours per airplane, at an
average labor rate of $80 per work hour. Based on these figures, the
estimated cost of the AD for U.S. operators is $2,400, or $240 per
airplane.
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):
2006-15-17 Fokker Services B.V.: Amendment 39-14698. Docket No. FAA-
2006-24868; Directorate Identifier 2006-NM-103-AD.
Effective Date
(a) This AD becomes effective September 5, 2006.
[[Page 43034]]
Affected ADs
(b) None.
Applicability
(c) This AD applies to all Fokker Model F.28 Mark 0070 and 0100
airplanes, certificated in any category.
Unsafe Condition
(d) This AD results from a report of electrical sparks coming
out of the flight deck from a panel behind the left seat. We are
issuing this AD to prevent failure of the sliding window heating
element(s), due to electrical overload, which could result in smoke
and fire in the cockpit.
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.
Modification of Wiring Distribution
(f) Within 36 months after the effective date of this AD, modify
the wiring distribution of the alternating current bus transfer
power system and the right-hand and left-hand windshield anti-icing
system, by accomplishing all of the actions specified in the
Accomplishment Instructions of Fokker Service Bulletin SBF100-30-
027, dated May 9, 2005, as applicable; including Fokker Manual
Change Notification--Maintenance Documentation MCNM F100-098, dated
May 9, 2005, and 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.)
Table 1.--Drawings Included in Fokker Service Bulletin SBF100-30-027
----------------------------------------------------------------------------------------------------------------
Fokker drawing Sheet Issue Date
----------------------------------------------------------------------------------------------------------------
W41043................................... 007 H.......................... May 9, 2005.
W41043................................... 008 H.......................... May 9, 2005.
W41249................................... 006 F.......................... May 9, 2005.
W41249................................... 007 F.......................... May 9, 2005.
W41249................................... 008 F.......................... May 9, 2005.
W41249................................... 009 G.......................... May 9, 2005.
W41249................................... 010 G.......................... May 9, 2005.
----------------------------------------------------------------------------------------------------------------
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 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
(h) Dutch airworthiness directive NL-2005-009, dated June 30,
2005, also addresses the subject of this AD.
Material Incorporated by Reference
(i) You must use Fokker Service Bulletin SBF100-30-027, dated
May 9, 2005; including Fokker Manual Change Notification--
Maintenance Documentation MCNM F100-098, dated May 9, 2005; and the
Fokker drawings identified 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 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.
Table 2.--Attached Drawings Incorporated by Reference
----------------------------------------------------------------------------------------------------------------
Fokker drawing Sheet Issue Date
----------------------------------------------------------------------------------------------------------------
W41043................................... 007 H.......................... May 9, 2005.
W41043................................... 008 H.......................... May 9, 2005.
W41249................................... 006 F.......................... May 9, 2005.
W41249................................... 007 F.......................... May 9, 2005.
W41249................................... 008 F.......................... May 9, 2005.
W41249................................... 009 G.......................... May 9, 2005.
W41249................................... 010 G.......................... May 9, 2005.
----------------------------------------------------------------------------------------------------------------
[[Page 43035]]
Issued in Renton, Washington, on July 20, 2006.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E6-12092 Filed 7-28-06; 8:45 am]
BILLING CODE 4910-13-P
