Airworthiness Directives; Various Aircraft Equipped With Rotax Aircraft Engines 912 A Series Engines, 50865-50867 [2010-19840]

Download as PDF Federal Register / Vol. 75, No. 159 / Wednesday, August 18, 2010 / Rules and Regulations erowe on DSK5CLS3C1PROD with RULES pins for proper position by following the Compliance Instructions, Parts I and II, paragraphs 2. through 4.1 for the pilot control box and paragraphs 5. through 7.1 for the copilot control box, in Agusta Alert Bollettino Tecnico No. 119–39, dated July 2, 2010. (b) If the locking pin is recessed or extended in excess of 2.0 millimeters from the face of the pin bore, or missing, before further flight, replace the control box with an airworthy control box that has been inspected in accordance with paragraph (a) of this AD. Replacing the control box does not constitute terminating action for the inspection requirements of this AD. (c) To request a different method of compliance or a different compliance time for this AD, follow the procedures in 14 CFR 39.19. Contact the Manager, Safety Management Group, FAA, ATTN: Rao Edupuganti, Aviation Safety Engineer, Rotorcraft Directorate, Regulations and Policy Group, 2601 Meacham Blvd., Fort Worth, Texas 76137, telephone (817) 222–4389, fax (817) 222–5961, for information about previously approved alternative methods of compliance. (d) The Joint Aircraft System/Component (JASC) Code is 6700: Rotors Flight Control. (e) The inspections shall be done in accordance with the specified portions of Agusta Alert Bollettino Tecnico No. 119–39, dated July 2, 2010. The Director of the Federal Register approved this incorporation by reference in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Copies may be obtained from Agusta, Via Giovanni Agusta, 520 21017 Cascina Costa di Samarate (VA), Italy, telephone 39 0331–229111, fax 39 0331–229605/222595, or at https:// customersupport.agusta.com/ technical_advice.php. Copies may be inspected at the FAA, Office of the Regional Counsel, Southwest Region, 2601 Meacham Blvd., Room 663, Fort Worth, Texas 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. (f) This amendment becomes effective on September 2, 2010, to all persons except those persons to whom it was made immediately effective by Emergency AD 2010–15–51, issued July 16, 2010, which contained the requirements of this amendment. Note: The subject of this AD is addressed in European Aviation Safety Agency AD 2010–0142–E, dated July 5, 2010. Issued in Fort Worth, Texas, on August 4, 2010. Scott A. Horn, Acting Manager, Rotorcraft Directorate, Aircraft Certification Service. [FR Doc. 2010–19816 Filed 8–17–10; 8:45 am] BILLING CODE 4910–13–P VerDate Mar<15>2010 15:12 Aug 17, 2010 Jkt 220001 DEPARTMENT OF TRANSPORTATION SUPPLEMENTARY INFORMATION: Federal Aviation Administration 50865 Discussion 14 CFR Part 39 [Docket No. FAA–2010–0329 Directorate Identifier 2010–CE–016–AD; Amendment 39–16400; AD 2010–17–08] RIN 2120–AA64 Airworthiness Directives; Various Aircraft Equipped With Rotax Aircraft Engines 912 A Series Engines Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule. AGENCY: 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: SUMMARY: Due to high fuel pressure, caused by exceeding pressure in front of the mechanical fuel pump (e.g. due to an electrical fuel pump), in limited cases a deviation in the fuel supply could occur. This can result in exceeding of the fuel pressure and might cause engine malfunction and/or massive fuel leakage. We are issuing this AD to prevent the pump from causing excessive fuel pressure, which could result in engine malfunction or a massive fuel leak. These conditions could cause loss of control of the airplane or a fire. We are issuing this AD to require actions to correct the unsafe condition on these products. DATES: This AD becomes effective September 22, 2010. On September 22, 2010, the Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD. 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; e-mail: sarjapur.nagarajan@faa.gov. PO 00000 Frm 00021 Fmt 4700 Sfmt 4700 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 June 8, 2010 (75 FR 32315). That NPRM proposed to correct an unsafe condition for the specified products. The MCAI states: Due to high fuel pressure, caused by exceeding pressure in front of the mechanical fuel pump (e.g. due to an electrical fuel pump), in limited cases a deviation in the fuel supply could occur. This can result in exceeding of the fuel pressure and might cause engine malfunction and/or massive fuel leakage. Non-compliance with these instructions could result in engine damages, personal injuries or death. The MCAI requires replacing the affected fuel pumps with a different part number fuel pump. The MCAI applies to all versions of Bombardier-Rotax GmbH 912 A, 912 F, and 912 S series engines. Versions of the 912 F series and 912 S series engines are type certificated in the United States. However, the Model 912 A series engine installed in various aircraft does not have an engine type certificate; instead, the engine is part of the aircraft type design. 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. E:\FR\FM\18AUR1.SGM 18AUR1 50866 Federal Register / Vol. 75, No. 159 / Wednesday, August 18, 2010 / Rules and Regulations Costs of Compliance We estimate that this AD will affect 60 products of U.S. registry. We also estimate that it will take about .5 workhour per product to comply with the basic requirements of this AD. The average labor rate is $85 per work-hour. Required parts will cost about $650 per product. Based on these figures, we estimate the cost of this AD to the U.S. operators to be $41,550 or $692.50 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 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: ■ 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 2. The FAA amends § 39.13 by adding the following new AD: ■ 2010–17–08 Various Aircraft: Amendment 39–16400; Docket No. FAA–2010–0329; Directorate Identifier 2010–CE–016–AD. Effective Date (a) This airworthiness directive (AD) becomes effective September 22, 2010. Affected ADs (b) None. Applicability (c) This AD applies to all serial numbers of the following aircraft, equipped with a Rotax Aircraft Engines 912 A series engine with fuel pumps, part numbers (P/Ns) 892230, 892232, 892540 (standard version) or P/Ns 892235, 892236, 892545 (version including flexible fuel line) installed, and certificated in any category: Type certificate holder Aircraft model Aeromot-Industria Mecanico Metalurgica Ltda ........ Diamond Aircraft Industries ..................................... Diamond Aircraft Industries ..................................... GmbH ....................................................................... Diamond Aircraft Industries Inc ............................... HOAC-Austria .......................................................... Iniziative Industriali Italiane S.p.A ............................ SCHEIBE-Flugzeugbau GmbH ................................ AMT–200 ............................................................... HK 36 R ‘‘SUPER DIMONA’’ ................................ HK 36 TS ............................................................... HK 36 TC .............................................................. DA20–A1 ............................................................... DV 20 KATANA ..................................................... Sky Arrow 650 TC ................................................. SF 25C .................................................................. Subject (d) Air Transport Association of America (ATA) Code 73: Engine Fuel and Control. Reason erowe on DSK5CLS3C1PROD with RULES [Amended] (e) The mandatory continuing airworthiness information (MCAI) states: Due to high fuel pressure, caused by exceeding pressure in front of the mechanical fuel pump (e.g., due to an electrical fuel pump), in limited cases a deviation in the fuel supply could occur. This can result in exceeding of the fuel pressure and might cause engine malfunction and/or massive fuel leakage. VerDate Mar<15>2010 15:12 Aug 17, 2010 Jkt 220001 Engine model 912 912 912 912 912 912 912 912 A2. A. A3. A3. A3. A3. A2. A2 or 912 A3. Non-compliance with these instructions could result in engine damages, personal injuries or death. We are issuing this AD to prevent the pump from causing excessive fuel pressure, which could result in engine malfunction or a massive fuel leak. These conditions could cause loss of control of the airplane or a fire. The MCAI requires replacing the affected fuel pumps with a different part number fuel pump. effective date of this AD), replace fuel pump P/N 892230, 892232, 892540, 892235, 892236, or 892545 with an FAA-approved fuel pump that does not have one of the P/Ns referenced above following Rotax Aircraft Engines Mandatory Service Bulletin SB–912–053, dated April 13, 2007. (2) As of September 22, 2010 (the effective date of this AD) do not install fuel pump P/ N 892230, 892232, 892540, 892235, 892236, or 892545, on any airplane. Actions and Compliance FAA AD Differences (f) Unless already done, do the following actions: (1) Within the next 25 hours time-inservice after September 22, 2010 (the Note: This AD differs from the MCAI and/ or service information as follows: The MCAI requires replacing an affected fuel pump with fuel pump P/N 892542 or 892546. This AD PO 00000 Frm 00022 Fmt 4700 Sfmt 4700 E:\FR\FM\18AUR1.SGM 18AUR1 Federal Register / Vol. 75, No. 159 / Wednesday, August 18, 2010 / Rules and Regulations requires replacement of an affected fuel pump with an FAA-approved fuel pump that does not have one of the P/Ns referenced in paragraph (f)(1) of this AD. 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; e-mail: sarjapur.nagarajan@faa.gov. 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. erowe on DSK5CLS3C1PROD with RULES Related Information (h) Refer to MCAI EASA AD No.: 2007– 0060R1–E, dated April 20, 2007; and Rotax Aircraft Engines Service Bulletin SB–912– 053, dated April 13, 2007, for related information. Material Incorporated by Reference (i) You must use Rotax Aircraft Engines Mandatory Service Bulletin SB–912–053, dated April 13, 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 BRP-Powertrain GMBH & Co KG, Welser Strasse 32, A–4623 Gunskirchen, Austria; phone: (+43) (0) 7246 601–0; fax: (+43) (0) 7246 6370; Internet: https:// www.rotax.com. (3) You may review copies of the service information incorporated by reference for this AD at the FAA, Central Region, Office of the Regional Counsel, 901 Locust, Kansas City, Missouri 64106. For information on the availability of this material at the Central Region, call (816) 329–3768. (4) You may also review copies of the service information incorporated by reference for this AD at the National Archives and Records Administration (NARA). For VerDate Mar<15>2010 15:12 Aug 17, 2010 Jkt 220001 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 August 5, 2010. Brian A. Yanez, Acting Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. 2010–19840 Filed 8–17–10; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2010–0278; Directorate Identifier 2009–NM–255–AD; Amendment 39–16399; AD 2010–17–07] RIN 2120–AA64 Airworthiness Directives; Airbus Model A330–223, –321, –322, and –323 Airplanes Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule. AGENCY: We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) originated 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: SUMMARY: During accomplishment of Damage Tolerant—Airworthiness Limitation Item task 712106–01–01 from A330 ALS Part 2, an A330 operator found a Fluorescent Penetrant Inspection (FPI) indication in the head of the shank filet radius in one of the Pratt & Whitney (PW) forward (FWD) engine mount pylon bolts. * * * * * Dual-bolt fractures could lead to inability for mount assembly to sustain loads which may lead to an engine mount failure and consequently to engine separation from the aeroplane during flight, which would constitute an unsafe condition. * * * * * We are issuing this AD to require actions to correct the unsafe condition on these products. DATES: This AD becomes effective September 22, 2010. The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of September 22, 2010. ADDRESSES: You may examine the AD docket on the Internet at https:// PO 00000 Frm 00023 Fmt 4700 Sfmt 4700 50867 www.regulations.gov or in person at the U.S. Department of Transportation, Docket Operations, M–30, West Building Ground Floor, Room W12–140, 1200 New Jersey Avenue, SE., Washington, DC. FOR FURTHER INFORMATION CONTACT: Vladimir Ulyanov, Aerospace Engineer, International Branch, ANM–116, Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton, Washington 98057–3356; telephone (425) 227–1138; fax (425) 227–1149. 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 April 2, 2010 (75 FR 16696). That NPRM proposed to correct an unsafe condition for the specified products. The MCAI states: During accomplishment of Damage Tolerant—Airworthiness Limitation Item task 712106–01–01 from A330 ALS Part 2, an A330 operator found a Fluorescent Penetrant Inspection (FPI) indication in the head of the shank filet radius in one of the Pratt & Whitney (PW) forward (FWD) engine mount pylon bolts. Investigation has confirmed that this FPI indication was due to a quality manufacturing process issue which led to a bolt non-conformance and is also applicable to aftward (AFT) mount pylon bolts. Dual-bolt fractures could lead to inability for mount assembly to sustain loads which may lead to an engine mount failure and consequently to engine separation from the aeroplane during flight, which would constitute an unsafe condition. This AD requires a one time detailed visual inspection of the FWD and AFT mount pylon bolts on all A330 aeroplanes fitted with PW engines (8 bolts per engine) and replacement of any affected bolt. You may obtain further information by examining the MCAI in the AD docket. Comments We gave the public the opportunity to participate in developing this AD. We considered the comments received. Requests To Refer to the Latest Pratt & Whitney Service Information Delta Airlines and Pratt & Whitney— Cheshire Engine Center request that we revise the NPRM to refer to Pratt & Whitney Service Bulletin PW4G–100– 71–35, Revision 1, dated December 4, 2009, for determining suspect bolts, rather than Pratt & Whitney Service Bulletin PW4G–100–71–35, dated March 14, 2008, which was referenced in the NPRM as the appropriate source for determining suspect bolts. The E:\FR\FM\18AUR1.SGM 18AUR1

Agencies

[Federal Register Volume 75, Number 159 (Wednesday, August 18, 2010)]
[Rules and Regulations]
[Pages 50865-50867]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2010-19840]


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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2010-0329 Directorate Identifier 2010-CE-016-AD; 
Amendment 39-16400; AD 2010-17-08]
RIN 2120-AA64


Airworthiness Directives; Various Aircraft Equipped With Rotax 
Aircraft Engines 912 A Series Engines

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 high fuel pressure, caused by exceeding pressure in front 
of the mechanical fuel pump (e.g. due to an electrical fuel pump), 
in limited cases a deviation in the fuel supply could occur. This 
can result in exceeding of the fuel pressure and might cause engine 
malfunction and/or massive fuel leakage.

We are issuing this AD to prevent the pump from causing excessive fuel 
pressure, which could result in engine malfunction or a massive fuel 
leak. These conditions could cause loss of control of the airplane or a 
fire. We are issuing this AD to require actions to correct the unsafe 
condition on these products.

DATES: This AD becomes effective September 22, 2010.
    On September 22, 2010, the Director of the Federal Register 
approved the incorporation by reference of certain publications listed 
in this AD.

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; 
e-mail: sarjapur.nagarajan@faa.gov.

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 June 8, 2010 (75 FR 
32315). That NPRM proposed to correct an unsafe condition for the 
specified products. The MCAI states:

    Due to high fuel pressure, caused by exceeding pressure in front 
of the mechanical fuel pump (e.g. due to an electrical fuel pump), 
in limited cases a deviation in the fuel supply could occur. This 
can result in exceeding of the fuel pressure and might cause engine 
malfunction and/or massive fuel leakage.
    Non-compliance with these instructions could result in engine 
damages, personal injuries or death.

The MCAI requires replacing the affected fuel pumps with a different 
part number fuel pump.
    The MCAI applies to all versions of Bombardier-Rotax GmbH 912 A, 
912 F, and 912 S series engines. Versions of the 912 F series and 912 S 
series engines are type certificated in the United States. However, the 
Model 912 A series engine installed in various aircraft does not have 
an engine type certificate; instead, the engine is part of the aircraft 
type design.

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.

[[Page 50866]]

Costs of Compliance

    We estimate that this AD will affect 60 products of U.S. registry. 
We also estimate that it will take about .5 work-hour per product to 
comply with the basic requirements of this AD. The average labor rate 
is $85 per work-hour. Required parts will cost about $650 per product.
    Based on these figures, we estimate the cost of this AD to the U.S. 
operators to be $41,550 or $692.50 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 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:

2010-17-08 Various Aircraft: Amendment 39-16400; Docket No. FAA-
2010-0329; Directorate Identifier 2010-CE-016-AD.

Effective Date

    (a) This airworthiness directive (AD) becomes effective 
September 22, 2010.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to all serial numbers of the following 
aircraft, equipped with a Rotax Aircraft Engines 912 A series engine 
with fuel pumps, part numbers (P/Ns) 892230, 892232, 892540 
(standard version) or P/Ns 892235, 892236, 892545 (version including 
flexible fuel line) installed, and certificated in any category:

------------------------------------------------------------------------
    Type certificate holder         Aircraft model        Engine model
------------------------------------------------------------------------
Aeromot-Industria Mecanico      AMT-200..............  912 A2.
 Metalurgica Ltda.
Diamond Aircraft Industries...  HK 36 R ``SUPER        912 A.
                                 DIMONA''.
Diamond Aircraft Industries...  HK 36 TS.............  912 A3.
GmbH..........................  HK 36 TC.............  912 A3.
Diamond Aircraft Industries     DA20-A1..............  912 A3.
 Inc.
HOAC-Austria..................  DV 20 KATANA.........  912 A3.
Iniziative Industriali          Sky Arrow 650 TC.....  912 A2.
 Italiane S.p.A.
SCHEIBE-Flugzeugbau GmbH......  SF 25C...............  912 A2 or 912 A3.
------------------------------------------------------------------------

Subject

    (d) Air Transport Association of America (ATA) Code 73: Engine 
Fuel and Control.

Reason

    (e) The mandatory continuing airworthiness information (MCAI) 
states:
    Due to high fuel pressure, caused by exceeding pressure in front 
of the mechanical fuel pump (e.g., due to an electrical fuel pump), 
in limited cases a deviation in the fuel supply could occur. This 
can result in exceeding of the fuel pressure and might cause engine 
malfunction and/or massive fuel leakage.
    Non-compliance with these instructions could result in engine 
damages, personal injuries or death.
    We are issuing this AD to prevent the pump from causing 
excessive fuel pressure, which could result in engine malfunction or 
a massive fuel leak. These conditions could cause loss of control of 
the airplane or a fire. The MCAI requires replacing the affected 
fuel pumps with a different part number fuel pump.

Actions and Compliance

    (f) Unless already done, do the following actions:
    (1) Within the next 25 hours time-in-service after September 22, 
2010 (the effective date of this AD), replace fuel pump P/N 892230, 
892232, 892540, 892235, 892236, or 892545 with an FAA-approved fuel 
pump that does not have one of the P/Ns referenced above following 
Rotax Aircraft Engines Mandatory Service Bulletin SB-912-053, dated 
April 13, 2007.
    (2) As of September 22, 2010 (the effective date of this AD) do 
not install fuel pump P/N 892230, 892232, 892540, 892235, 892236, or 
892545, on any airplane.

FAA AD Differences

    Note: This AD differs from the MCAI and/or service information 
as follows: The MCAI requires replacing an affected fuel pump with 
fuel pump P/N 892542 or 892546. This AD

[[Page 50867]]

requires replacement of an affected fuel pump with an FAA-approved 
fuel pump that does not have one of the P/Ns referenced in paragraph 
(f)(1) of this AD.

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; e-
mail: sarjapur.nagarajan@faa.gov. 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.

Related Information

    (h) Refer to MCAI EASA AD No.: 2007-0060R1-E, dated April 20, 
2007; and Rotax Aircraft Engines Service Bulletin SB-912-053, dated 
April 13, 2007, for related information.

Material Incorporated by Reference

    (i) You must use Rotax Aircraft Engines Mandatory Service 
Bulletin SB-912-053, dated April 13, 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 BRP-
Powertrain GMBH & Co KG, Welser Strasse 32, A-4623 Gunskirchen, 
Austria; phone: (+43) (0) 7246 601-0; fax: (+43) (0) 7246 6370; 
Internet: https://www.rotax.com.
    (3) You may review copies of the service information 
incorporated by reference for this AD at the FAA, Central Region, 
Office of the Regional Counsel, 901 Locust, Kansas City, Missouri 
64106. For information on the availability of this material at the 
Central Region, call (816) 329-3768.
    (4) You may also review copies of the service information 
incorporated by reference for this AD 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 August 5, 2010.
Brian A. Yanez,
Acting Manager, Small Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2010-19840 Filed 8-17-10; 8:45 am]
BILLING CODE 4910-13-P
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