Airworthiness Directives; Fokker Model F.28 Mark 0070 and 0100 Airplanes, 6343-6345 [06-988]

Download as PDF 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 http:// 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 08FER1 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 http://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 http:// 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 http://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 http://
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 http://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 
http://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 http://
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