Airworthiness Directives; Piaggio Aero Industries S.p.A. Model P 180 Airplanes, 6601-6602 [E8-2040]

Download as PDF Federal Register / Vol. 73, No. 24 / Tuesday, February 5, 2008 / Rules and Regulations Alternative Methods of Compliance (AMOCs) (f) The Manager, Chicago Aircraft Certification Office (ACO), FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Send information to ATTN: Wess Rouse, Aerospace Engineer, 2300 East Devon Avenue, Room 107, Des Plaines, Illinois 60018; telephone: (847) 294–8113; fax: (847) 294–7834. Before using any approved AMOC on any airplane to which the AMOC applies, notify your appropriate principal inspector (PI) in the FAA Flight Standards District Office (FSDO), or lacking a PI, your local FSDO. Material Incorporated by Reference (g) You must use Cirrus Service Bulletin No. SB 2X–27–14 R3, Revised: October 10, 2007, to do the actions required by this AD, unless the AD specifies otherwise. (1) The Director of the Federal Register approved the incorporation by reference of this service information under 5 U.S.C. 552(a) and 1 CFR part 51. (2) For service information identified in this AD, contact Cirrus Design Corporation, 4515 Taylor Circle, Duluth, Minnesota 55811; telephone: (218) 727–2737; internet address: www.cirrusdesign.com. (3) You may review copies at the FAA, Central Region, Office of the Regional Counsel, 901 Locust, Kansas City, Missouri 64106; or at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202–741–6030, or go to: https://www.archives.gov/federal_register/ code_of_federal_regulations/ ibr_locations.html. Issued in Kansas City, Missouri, on January 29, 2008. John Colomy, Acting Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. E8–2044 Filed 2–4–08; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2007–0294 Directorate Identifier 2007–CE–087–AD; Amendment 39–15365; AD 2008–03–14] RIN 2120–AA64 Airworthiness Directives; Piaggio Aero Industries S.p.A. Model P 180 Airplanes Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule. rmajette on PROD1PC64 with RULES AGENCY: SUMMARY: We are adopting a new airworthiness directive (AD) for the products listed above. This AD results VerDate Aug<31>2005 15:28 Feb 04, 2008 Jkt 214001 from mandatory continuing airworthiness information (MCAI) issued by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as: Due to pressurization loads, the fuselage frame of the emergency exit door could suffer from fatigue and develop cracks in its corners. The superseded Italian Airworthiness Directive (AD) 1995–059 was issued to require modification of the emergency door frame in accordance with Piaggio (at the time I.A.M. Rinaldo Piaggio S.p.A.) Service Bulletin 80–0057 original issue. Parts necessary to carry out the modification were a new door pan assembly and a doubler; Since these parts are no longer available, Piaggio Aero Industries S.p.A. (PAI) designed new suitable part numbers introduced by Revision 1 of Service Bulletin 80–0057. The present AD mandates modification of the fuselage emergency door frame in accordance with Revision 1 of Service Bulletin 80–0057 from PAI. We are issuing this AD to require actions to correct the unsafe condition on these products. DATES: This AD becomes effective March 11, 2008. ADDRESSES: You may examine the AD docket on the Internet at https:// www.regulations.gov or in person at Document Management Facility, U.S. Department of Transportation, Docket Operations, M–30, West Building, Ground Floor, Room W12–140, 1200 New Jersey Avenue, SE., Washington, DC 20590. FOR FURTHER INFORMATION CONTACT: Sarjapur Nagarajan, Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329– 4145; fax: (816) 329–4090. SUPPLEMENTARY INFORMATION: Discussion We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to include an AD that would apply to the specified products. That NPRM was published in the Federal Register on December 14, 2007 (72 FR 71089). That NPRM proposed to correct an unsafe condition for the specified products. The MCAI states: Due to pressurization loads, the fuselage frame of the emergency exit door could suffer from fatigue and develop cracks in its corners. The superseded Italian Airworthiness Directive (AD) 1995–059 was issued to require modification of the emergency door frame in accordance with Piaggio (at the time I.A.M. Rinaldo Piaggio S.p.A.) Service Bulletin 80–0057 original issue. Parts necessary to carry out the modification were a new door pan assembly and a doubler; Since these parts are no longer PO 00000 Frm 00025 Fmt 4700 Sfmt 4700 6601 available, Piaggio Aero Industries S.p.A. (PAI) designed new suitable part numbers introduced by Revision 1 of Service Bulletin 80–0057. The present AD mandates modification of the fuselage emergency door frame in accordance with Revision 1 of Service Bulletin 80–0057 from PAI. We are issuing this AD to require actions to correct the unsafe condition on these products. Comments We gave the public the opportunity to participate in developing this AD. We received no comments on the NPRM or on the determination of the cost to the public. Conclusion We reviewed the available data and determined that air safety and the public interest require adopting the AD as proposed. Differences Between This AD and the MCAI or Service Information We have reviewed the MCAI and related service information and, in general, agree with their substance. But we might have found it necessary to use different words from those in the MCAI to ensure the AD is clear for U.S. operators and is enforceable. In making these changes, we do not intend to differ substantively from the information provided in the MCAI and related service information. We might also have required different actions in this AD from those in the MCAI in order to follow FAA policies. Any such differences are highlighted in a NOTE within the AD. Costs of Compliance We estimate that this AD will affect 31 products of U.S. registry. We also estimate that it will take about 70 workhours per product to comply with basic requirements of this AD. The average labor rate is $80 per work-hour. Required parts will cost about $14,105 per product. Based on these figures, we estimate the cost of this AD to the U.S. operators to be $610,855 or $19,705 per product. 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 E:\FR\FM\05FER1.SGM 05FER1 6602 Federal Register / Vol. 73, No. 24 / Tuesday, February 5, 2008 / Rules and Regulations 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 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 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. Examining the AD Docket You may examine the AD docket on the Internet at https:// www.regulations.gov; or in person at the Docket Management Facility between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains the NPRM, the regulatory evaluation, any comments received, and other information. The street address for the Docket Office (telephone (800) 647–5527) is in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. Adoption of the Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: rmajette on PROD1PC64 with RULES I PART 39—AIRWORTHINESS DIRECTIVES 1. The authority citation for part 39 continues to read as follows: I VerDate Aug<31>2005 15:28 Feb 04, 2008 Jkt 214001 Authority: 49 U.S.C. 106(g), 40113, 44701. § 39.13 [Amended] 2. The FAA amends § 39.13 by adding the following new AD: I 2008–03–14 Piaggio Aero Industries S.p.A.: Amendment 39–15365; Docket No. FAA–2007–0294; Directorate Identifier 2007–CE–087–AD. Effective Date (a) This airworthiness directive (AD) becomes effective March 11, 2008. Affected ADs (b) None. Applicability (c) This AD applies to PIAGGIO P–180 airplanes, manufacturer serial numbers (MSN) 1001, 1002, 1004, and MSN 1006 through 1033, that: (1) are certificated in any category; and (2) have not been modified in accordance with Piaggio Aero Industries Service Bulletin No. 80–0057, dated February 7, 1995. Subject (d) Air Transport Association of America (ATA) Code 53: Fuselage. Reason (e) The mandatory continuing airworthiness information (MCAI) states: Due to pressurization loads, the fuselage frame of the emergency exit door could suffer from fatigue and develop cracks in its corners. The superseded Italian Airworthiness Directive (AD) 1995–059 was issued to require modification of the emergency door frame in accordance with Piaggio (at the time I.A.M. Rinaldo Piaggio S.p.A.) Service Bulletin 80–0057 original issue. Parts necessary to carry out the modification were a new door pan assembly and a doubler; Since these parts are no longer available, Piaggio Aero Industries S.p.A. (PAI) designed new suitable part numbers introduced by Revision 1 of Service Bulletin 80–0057. The present AD mandates modification of the fuselage emergency door frame in accordance with Revision 1 of Service Bulletin 80–0057 from PAI. The MCAI requires the modification of the fuselage frame of the emergency door, using the newly designed door pan assembly and doubler, following Piaggio Aero Industries S.p.A. SB 80–0057, Revision 1, dated May 31, 2007. Actions and Compliance (f) Unless already done, replace the emergency exit door pan assembly part number (P/N) 80–111152–401 with a new door pan assembly P/N 80–111152–405, and a new doubler reinforcement P/N 80– 111604–001, following Piaggio Aero Industries S.p.A. Mandatory Service Bulletin N.: 80–0057, Revision 1, dated May 31, 2007, at whichever of the following occurs later: (1) When the airplane reaches 4,500 hours total time-in-service (TIS); or (2) Within 6 months after March 11, 2008 (the effective date of this AD) or 500 hours TIS after March 11, 2008 (the effective date of this AD), whichever of these occurs first. PO 00000 Frm 00026 Fmt 4700 Sfmt 4700 FAA AD Differences Note: This AD differs from the MCAI and/ or service information as follows: No differences. Other FAA AD Provisions (g) The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, Standards Office, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Send information to ATTN: Sarjapur Nagarajan, Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329–4145; fax: (816) 329–4090. Before using any approved AMOC on any airplane to which the AMOC applies, notify your appropriate principal inspector (PI) in the FAA Flight Standards District Office (FSDO), or lacking a PI, your local FSDO. (2) Airworthy Product: For any requirement in this AD to obtain corrective actions from a manufacturer or other source, use these actions if they are FAA-approved. Corrective actions are considered FAA-approved if they are approved by the State of Design Authority (or their delegated agent). You are required to assure the product is airworthy before it is returned to service. (3) Reporting Requirements: For any reporting requirement in this AD, under the provisions of the Paperwork Reduction Act (44 U.S.C. 3501 et seq.), the Office of Management and Budget (OMB) has approved the information collection requirements and has assigned OMB Control Number 2120–0056. Material Incorporated by Reference (h) You must use Piaggio Aero Industries S.p.A. Mandatory Service Bulletin N.: 80– 0057, Revision 1, dated May 31, 2007 to do the actions required by this AD, unless the AD specifies otherwise. (1) The Director of the Federal Register approved the incorporation by reference of this service information under 5 U.S.C. 552(a) and 1 CFR part 51. (2) For service information identified in this AD, contact Piaggio Aero Industries S.p.a., Via Cibrario, 4—16154 Genoa, Italy; telephone +39 010 06481 741; fax: +39 010 6481 309; e-mail: MMicheli@piaggioaero.it. (3) You may review copies at the FAA, Central Region, Office of the Regional Counsel, 901 Locust, Room 506, Kansas City, Missouri 64106; or at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202–741–6030, or go to: https://www.archives.gov/federal-register/ cfr/ibr-locations.html. Issued in Kansas City, Missouri, on January 29, 2008. John Colomy, Acting Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. E8–2040 Filed 2–4–08; 8:45 am] BILLING CODE 4910–13–P E:\FR\FM\05FER1.SGM 05FER1

Agencies

[Federal Register Volume 73, Number 24 (Tuesday, February 5, 2008)]
[Rules and Regulations]
[Pages 6601-6602]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E8-2040]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2007-0294 Directorate Identifier 2007-CE-087-AD; 
Amendment 39-15365; AD 2008-03-14]
RIN 2120-AA64


Airworthiness Directives; Piaggio Aero Industries S.p.A. Model P 
180 Airplanes

AGENCY: Federal Aviation Administration (FAA), Department of 
Transportation (DOT).

ACTION: Final rule.

-----------------------------------------------------------------------

SUMMARY: We are adopting a new airworthiness directive (AD) for the 
products listed above. This AD results from mandatory continuing 
airworthiness information (MCAI) issued by an aviation authority of 
another country to identify and correct an unsafe condition on an 
aviation product. The MCAI describes the unsafe condition as:

    Due to pressurization loads, the fuselage frame of the emergency 
exit door could suffer from fatigue and develop cracks in its 
corners. The superseded Italian Airworthiness Directive (AD) 1995-
059 was issued to require modification of the emergency door frame 
in accordance with Piaggio (at the time I.A.M. Rinaldo Piaggio 
S.p.A.) Service Bulletin 80-0057 original issue. Parts necessary to 
carry out the modification were a new door pan assembly and a 
doubler; Since these parts are no longer available, Piaggio Aero 
Industries S.p.A. (PAI) designed new suitable part numbers 
introduced by Revision 1 of Service Bulletin 80-0057. The present AD 
mandates modification of the fuselage emergency door frame in 
accordance with Revision 1 of Service Bulletin 80-0057 from PAI.

We are issuing this AD to require actions to correct the unsafe 
condition on these products.

DATES: This AD becomes effective March 11, 2008.

ADDRESSES: You may examine the AD docket on the Internet at https://
www.regulations.gov or in person at Document Management Facility, U.S. 
Department of Transportation, Docket Operations, M-30, West Building, 
Ground Floor, Room W12-140, 1200 New Jersey Avenue, SE., Washington, DC 
20590.

FOR FURTHER INFORMATION CONTACT: Sarjapur Nagarajan, Aerospace 
Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas 
City, Missouri 64106; telephone: (816) 329-4145; fax: (816) 329-4090.

SUPPLEMENTARY INFORMATION:

Discussion

    We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR 
part 39 to include an AD that would apply to the specified products. 
That NPRM was published in the Federal Register on December 14, 2007 
(72 FR 71089). That NPRM proposed to correct an unsafe condition for 
the specified products. The MCAI states:

    Due to pressurization loads, the fuselage frame of the emergency 
exit door could suffer from fatigue and develop cracks in its 
corners. The superseded Italian Airworthiness Directive (AD) 1995-
059 was issued to require modification of the emergency door frame 
in accordance with Piaggio (at the time I.A.M. Rinaldo Piaggio 
S.p.A.) Service Bulletin 80-0057 original issue. Parts necessary to 
carry out the modification were a new door pan assembly and a 
doubler; Since these parts are no longer available, Piaggio Aero 
Industries S.p.A. (PAI) designed new suitable part numbers 
introduced by Revision 1 of Service Bulletin 80-0057. The present AD 
mandates modification of the fuselage emergency door frame in 
accordance with Revision 1 of Service Bulletin 80-0057 from PAI.

We are issuing this AD to require actions to correct the unsafe 
condition on these products.

Comments

    We gave the public the opportunity to participate in developing 
this AD. We received no comments on the NPRM or on the determination of 
the cost to the public.

Conclusion

    We reviewed the available data and determined that air safety and 
the public interest require adopting the AD as proposed.

Differences Between This AD and the MCAI or Service Information

    We have reviewed the MCAI and related service information and, in 
general, agree with their substance. But we might have found it 
necessary to use different words from those in the MCAI to ensure the 
AD is clear for U.S. operators and is enforceable. In making these 
changes, we do not intend to differ substantively from the information 
provided in the MCAI and related service information.
    We might also have required different actions in this AD from those 
in the MCAI in order to follow FAA policies. Any such differences are 
highlighted in a NOTE within the AD.

Costs of Compliance

    We estimate that this AD will affect 31 products of U.S. registry. 
We also estimate that it will take about 70 work-hours per product to 
comply with basic requirements of this AD. The average labor rate is 
$80 per work-hour. Required parts will cost about $14,105 per product.
    Based on these figures, we estimate the cost of this AD to the U.S. 
operators to be $610,855 or $19,705 per product.

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

[[Page 6602]]

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 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 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.

Examining the AD Docket

    You may examine the AD docket on the Internet at https://
www.regulations.gov; or in person at the Docket Management Facility 
between 9 a.m. and 5 p.m., Monday through Friday, except Federal 
holidays. The AD docket contains the NPRM, the regulatory evaluation, 
any comments received, and other information. The street address for 
the Docket Office (telephone (800) 647-5527) is in the ADDRESSES 
section. Comments will be available in the AD docket shortly after 
receipt.

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 FAA amends Sec.  39.13 by adding the following new AD:

2008-03-14 Piaggio Aero Industries S.p.A.: Amendment 39-15365; 
Docket No. FAA-2007-0294; Directorate Identifier 2007-CE-087-AD.

Effective Date

    (a) This airworthiness directive (AD) becomes effective March 
11, 2008.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to PIAGGIO P-180 airplanes, manufacturer 
serial numbers (MSN) 1001, 1002, 1004, and MSN 1006 through 1033, 
that:
    (1) are certificated in any category; and
    (2) have not been modified in accordance with Piaggio Aero 
Industries Service Bulletin No. 80-0057, dated February 7, 1995.

Subject

    (d) Air Transport Association of America (ATA) Code 53: 
Fuselage.

Reason

    (e) The mandatory continuing airworthiness information (MCAI) 
states:
    Due to pressurization loads, the fuselage frame of the emergency 
exit door could suffer from fatigue and develop cracks in its 
corners. The superseded Italian Airworthiness Directive (AD) 1995-
059 was issued to require modification of the emergency door frame 
in accordance with Piaggio (at the time I.A.M. Rinaldo Piaggio 
S.p.A.) Service Bulletin 80-0057 original issue. Parts necessary to 
carry out the modification were a new door pan assembly and a 
doubler; Since these parts are no longer available, Piaggio Aero 
Industries S.p.A. (PAI) designed new suitable part numbers 
introduced by Revision 1 of Service Bulletin 80-0057. The present AD 
mandates modification of the fuselage emergency door frame in 
accordance with Revision 1 of Service Bulletin 80-0057 from PAI.

The MCAI requires the modification of the fuselage frame of the 
emergency door, using the newly designed door pan assembly and 
doubler, following Piaggio Aero Industries S.p.A. SB 80-0057, 
Revision 1, dated May 31, 2007.

Actions and Compliance

    (f) Unless already done, replace the emergency exit door pan 
assembly part number (P/N) 80-111152-401 with a new door pan 
assembly P/N 80-111152-405, and a new doubler reinforcement P/N 80-
111604-001, following Piaggio Aero Industries S.p.A. Mandatory 
Service Bulletin N.: 80-0057, Revision 1, dated May 31, 2007, at 
whichever of the following occurs later:
    (1) When the airplane reaches 4,500 hours total time-in-service 
(TIS); or
    (2) Within 6 months after March 11, 2008 (the effective date of 
this AD) or 500 hours TIS after March 11, 2008 (the effective date 
of this AD), whichever of these occurs first.

FAA AD Differences

    Note: This AD differs from the MCAI and/or service information 
as follows: No differences.

Other FAA AD Provisions

    (g) The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager, 
Standards Office, FAA, has the authority to approve AMOCs for this 
AD, if requested using the procedures found in 14 CFR 39.19. Send 
information to ATTN: Sarjapur Nagarajan, Aerospace Engineer, FAA, 
Small Airplane Directorate, 901 Locust, Room 301, Kansas City, 
Missouri 64106; telephone: (816) 329-4145; fax: (816) 329-4090. 
Before using any approved AMOC on any airplane to which the AMOC 
applies, notify your appropriate principal inspector (PI) in the FAA 
Flight Standards District Office (FSDO), or lacking a PI, your local 
FSDO.
    (2) Airworthy Product: For any requirement in this AD to obtain 
corrective actions from a manufacturer or other source, use these 
actions if they are FAA-approved. Corrective actions are considered 
FAA-approved if they are approved by the State of Design Authority 
(or their delegated agent). You are required to assure the product 
is airworthy before it is returned to service.
    (3) Reporting Requirements: For any reporting requirement in 
this AD, under the provisions of the Paperwork Reduction Act (44 
U.S.C. 3501 et seq.), the Office of Management and Budget (OMB) has 
approved the information collection requirements and has assigned 
OMB Control Number 2120-0056.

Material Incorporated by Reference

    (h) You must use Piaggio Aero Industries S.p.A. Mandatory 
Service Bulletin N.: 80-0057, Revision 1, dated May 31, 2007 to do 
the actions required by this AD, unless the AD specifies otherwise.
    (1) The Director of the Federal Register approved the 
incorporation by reference of this service information under 5 
U.S.C. 552(a) and 1 CFR part 51.
    (2) For service information identified in this AD, contact 
Piaggio Aero Industries S.p.a., Via Cibrario, 4--16154 Genoa, Italy; 
telephone +39 010 06481 741; fax: +39 010 6481 309; e-mail: 
MMicheli@piaggioaero.it.
    (3) You may review copies at the FAA, Central Region, Office of 
the Regional Counsel, 901 Locust, Room 506, Kansas City, Missouri 
64106; or at the National Archives and Records Administration 
(NARA). For information on the availability of this material at 
NARA, call 202-741-6030, or go to: https://www.archives.gov/federal-
register/cfr/ibr-locations.html.

    Issued in Kansas City, Missouri, on January 29, 2008.
John Colomy,
Acting Manager, Small Airplane Directorate, Aircraft Certification 
Service.
 [FR Doc. E8-2040 Filed 2-4-08; 8:45 am]
BILLING CODE 4910-13-P