Airworthiness Directives; PILATUS AIRCRAFT LTD. Airplanes, 17865-17866 [2013-06169]

Download as PDF 17865 Rules and Regulations Federal Register Vol. 78, No. 57 Monday, March 25, 2013 This section of the FEDERAL REGISTER contains regulatory documents having general applicability and legal effect, most of which are keyed to and codified in the Code of Federal Regulations, which is published under 50 titles pursuant to 44 U.S.C. 1510. The Code of Federal Regulations is sold by the Superintendent of Documents. Prices of new books are listed in the first FEDERAL REGISTER issue of each week. DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2008–0070; Directorate Identifier 2007–CE–098–AD; Amendment 39–17398; AD 2008–07–11 R1] RIN 2120–AA64 Airworthiness Directives; PILATUS AIRCRAFT LTD. Airplanes Federal Aviation Administration (FAA), DOT. ACTION: Final rule; rescission; request for comments AGENCY: We are rescinding an airworthiness directive (AD) for all PILATUS AIRCRAFT LTD. Models PC– 12, PC–12/45, and PC–12/47 airplanes. This AD results from mandatory continuing airworthiness information (MCAI) issued by the aviation authority of another country to identify and correct an unsafe condition on an aviation product. We issued that AD to mandate new life limits for the pitch trim actuator and pitch trim actuator attachment parts. If these new limitations were not mandated, the pitch trim actuator and the pitch trim actuator components could fail. This failure could lead to an unsafe flying configuration. Since we issued that AD, we have determined that the unsafe condition addressed in that AD is now addressed in another AD. DATES: This AD is effective March 25, 2013. We must receive comments on this AD by May 9, 2013. ADDRESSES: You may send comments by any of the following methods: • Federal eRulemaking Portal: Go to https://www.regulations.gov. Follow the instructions for submitting comments. • Fax: (202) 493–2251. • Mail: U.S. Department of Transportation, Docket Operations, M– srobinson on DSK4SPTVN1PROD with NOTICES SUMMARY: VerDate Mar<15>2010 16:01 Mar 22, 2013 Jkt 229001 30, West Building Ground Floor, Room W12–140, 1200 New Jersey Avenue SE., Washington, DC 20590. • Hand Delivery: U.S. Department of Transportation, Docket Operations, M– 30, West Building Ground Floor, Room W12–140, 1200 New Jersey Avenue SE., Washington, DC 20590, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. 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 this AD, 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. FOR FURTHER INFORMATION CONTACT: Doug Rudolph, Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329– 4059; fax: (816) 329–4090; email: doug.rudolph@faa.gov. SUPPLEMENTARY INFORMATION: Discussion On March 27, 2008, we issued AD 2008–07–11, Amendment 39–15452 (73 FR 18433, April 4, 2008). That AD required actions intended to address an unsafe condition on the products listed above. AD 2008–07–11, Amendment 39– 15452 (73 FR 18433, April 4, 2008) was based on results of a full-scale fatigue test of the pitch trim actuator on PILATUS AIRCRAFT LTD. Models PC– 12, PC–12/45, and PC–12/47 airplanes. The life-limit was extended and the time between overhaul (TBO) was reduced. In addition, based on the results of the fatigue test, a life-limit of the pitch trim actuator attachment had been established. These new limitations were incorporated into the airworthiness limitations section of the Pilatus PC–12 Airplane Maintenance Manual (AMM) 12–A/AMP–04, chapter 4, revision 10, dated October 26, 2007. The new limitations for the pitch trim actuator TBO were moved from Chapter 5: Time Limits/Maintenance Checks, to PO 00000 Frm 00001 Fmt 4700 Sfmt 4700 Chapter 4: Structural, Component and Miscellaneous—Airworthiness Limitations. Since both chapter 4 and chapter 5 are mandatory within the European and Swiss airworthiness systems, it was not necessary for the European Aviation Safety Agency (EASA) and the Federal Office of Civil Aviation (FOCA) to issue an AD to mandate these new limitations. The only way the FAA can mandate the implementation of changes to the airworthiness limitations section of an FAA-approved maintenance program is by AD action. On February 8, 2013, we issued AD 2012–26–16, Amendment 39–17311 (78 FR 11572, February 19, 2013). AD 2012– 26–16 also requires incorporating new revisions into the Limitations section, Chapter 4, of the Pilatus PC–12 AMM. The limitations were revised to include an inspection of the wing main spar fastener holes at rib 6 for cracks. After issuing AD 2012–26–16, Amendment 39–17311 (78 FR 11572, February 19, 2013), we determined that AD 2008–07–11 should have been superseded by AD 2012–26–16. Since AD 2008–07–11 requires incorporating an earlier version of the airworthiness limitations section of the AMM, it could cause confusion for the owners/ operators and could result in missed inspections and replacements required by AD 2012–26–16. Therefore, the need to continue to address this subject as an unsafe condition through AD 2008–07– 11 is no longer necessary. FAA’s Determination We are issuing this AD because we evaluated all available information and determined the existing AD is no longer necessary. AD Requirements This AD would rescind AD 2008–07– 11, Amendment 39–15452 (73 FR 18433, April 4, 2008). FAA’s Determination of the Effective Date An unsafe condition exists or could develop that requires the immediate adoption of this AD. The FAA has found that the risk to the flying public justifies waiving notice and comment prior to adoption of this rule because the unsafe condition addressed in AD 2008–07–11, Amendment 39–15452 (73 FR 18433, April 4, 2008) is currently addressed in AD 2012–26–16, Amendment 39–17311 E:\FR\FM\25MRR1.SGM 25MRR1 17866 Federal Register / Vol. 78, No. 57 / Monday, March 25, 2013 / Rules and Regulations (78 FR 11572, February 19, 2013). Allowing the airworthiness limitation section (ALS) required by AD 2008–07– 11 to remain valid could cause confusion as to what is required and this could introduce an unsafe condition if certain areas were not inspected. Therefore, we determined that notice and opportunity for public comment before issuing this AD are impracticable and that good cause exists for making this amendment effective in fewer than 30 days. srobinson on DSK4SPTVN1PROD with NOTICES Comments Invited This AD is a final rule that involves requirements affecting flight safety, and we did not precede it by notice and opportunity for public comment. We invite you to send any written relevant data, views, or arguments about this AD. Send your comments to an address listed under the ADDRESSES section. Include ‘‘Docket No. FAA–2008–0070; Directorate Identifier 2007–CE–098– AD’’ at the beginning of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of this AD. We will consider all comments received by the closing date and may amend this AD because of those comments. We will post all comments we receive, without change, to https:// www.regulations.gov, including any personal information you provide. We will also post a report summarizing each substantive verbal contact we receive about this AD. 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 VerDate Mar<15>2010 16:01 Mar 22, 2013 Jkt 229001 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 the DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979), (3) Will not affect intrastate aviation in Alaska, and (4) 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. Issued in Kansas City, Missouri on March 11, 2013. Earl Lawrence, Manager, Small Airplane Directorate, Aircraft Certification Service. List of Subjects in 14 CFR Part 39 HHS. 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 [Amended] 2. The FAA amends § 39.13 by removing AD 2008–07–11, Amendment 39–15452 (73 FR 18433, April 4, 2008), and adding the following new AD: ■ 2008–07–11 R1 PILATUS AIRCRAFT LTD.: Amendment 39–17398; Docket No. FAA–2008–0070; Directorate Identifier 2007–CE–098–AD. (a) Effective Date This airworthiness directive (AD) becomes effective April 15, 2013. (b) Affected ADs This AD rescinds AD 2008–07–11, Amendment 39–15452 (73 FR 18433, April 4, 2008). (c) Applicability This AD applies to PILATUS AIRCRAFT LTD. Models PC–12, PC–12/45, and PC–12/ 47 airplanes, all serial numbers, certificated in any category. (d) Subject Air Transport Association of America (ATA) Code 27: Flight Controls. PO 00000 Frm 00002 Fmt 4700 Sfmt 4700 [FR Doc. 2013–06169 Filed 3–22–13; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF HEALTH AND HUMAN SERVICES Food and Drug Administration 21 CFR Parts 510, 522, 524, and 529 [Docket No. FDA–2013–N–0002] New Animal Drug Approvals; Change of Sponsor; Change of Sponsor’s Drug Labeler Code; Gonadorelin Acetate; Isoflurane; Praziquantel; Propofol; Sevoflurane; Triamcinolone Acetonide AGENCY: ACTION: Food and Drug Administration, Final rule. The Food and Drug Administration (FDA) is amending the animal drug regulations to reflect approval actions for new animal drug applications (NADAs) and abbreviated new animal drug applications (ANADAs) during January 2013. FDA is also informing the public of the availability of summaries the basis of approval and of environmental review documents, where applicable. The animal drug regulations are also being amended to reflect changes of sponsorship for an NADA and ANADA, and a change of a sponsor’s drug labeler code. DATES: This rule is effective March 25, 2013. FOR FURTHER INFORMATION CONTACT: George K. Haibel, Center for Veterinary Medicine (HFV–6), Food and Drug Administration, 7519 Standish Pl., Rockville, MD 20855, 240–276–9019, email: george.haibel@fda.hhs.gov. SUPPLEMENTARY INFORMATION: FDA is amending the animal drug regulations to reflect approval actions for NADAs and ANADAs during January 2013, as listed in table 1. In addition, FDA is informing the public of the availability, where applicable, of documentation of environmental review required under the National Environmental Policy Act (NEPA) and, for actions requiring review of safety or effectiveness data, summaries of the basis of approval (FOI Summaries) under the Freedom of Information Act (FOIA). These public documents may be seen in the Division of Dockets Management (HFA–305), Food and Drug Administration, 5630 SUMMARY: E:\FR\FM\25MRR1.SGM 25MRR1

Agencies

[Federal Register Volume 78, Number 57 (Monday, March 25, 2013)]
[Rules and Regulations]
[Pages 17865-17866]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2013-06169]



========================================================================
Rules and Regulations
                                                Federal Register
________________________________________________________________________

This section of the FEDERAL REGISTER contains regulatory documents 
having general applicability and legal effect, most of which are keyed 
to and codified in the Code of Federal Regulations, which is published 
under 50 titles pursuant to 44 U.S.C. 1510.

The Code of Federal Regulations is sold by the Superintendent of Documents. 
Prices of new books are listed in the first FEDERAL REGISTER issue of each 
week.

========================================================================


Federal Register / Vol. 78, No. 57 / Monday, March 25, 2013 / Rules 
and Regulations

[[Page 17865]]



DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2008-0070; Directorate Identifier 2007-CE-098-AD; 
Amendment 39-17398; AD 2008-07-11 R1]
RIN 2120-AA64


Airworthiness Directives; PILATUS AIRCRAFT LTD. Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; rescission; request for comments

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

SUMMARY: We are rescinding an airworthiness directive (AD) for all 
PILATUS AIRCRAFT LTD. Models PC-12, PC-12/45, and PC-12/47 airplanes. 
This AD results from mandatory continuing airworthiness information 
(MCAI) issued by the aviation authority of another country to identify 
and correct an unsafe condition on an aviation product. We issued that 
AD to mandate new life limits for the pitch trim actuator and pitch 
trim actuator attachment parts. If these new limitations were not 
mandated, the pitch trim actuator and the pitch trim actuator 
components could fail. This failure could lead to an unsafe flying 
configuration. Since we issued that AD, we have determined that the 
unsafe condition addressed in that AD is now addressed in another AD.

DATES: This AD is effective March 25, 2013.
    We must receive comments on this AD by May 9, 2013.

ADDRESSES: You may send comments by any of the following methods:
     Federal eRulemaking Portal: Go to https://www.regulations.gov. Follow the instructions for submitting comments.
     Fax: (202) 493-2251.
     Mail: U.S. Department of Transportation, Docket 
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New 
Jersey Avenue SE., Washington, DC 20590.
     Hand Delivery: U.S. Department of Transportation, Docket 
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New 
Jersey Avenue SE., Washington, DC 20590, between 9 a.m. and 5 p.m., 
Monday through Friday, except Federal holidays.

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 this AD, 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.

FOR FURTHER INFORMATION CONTACT: Doug Rudolph, Aerospace Engineer, FAA, 
Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 
64106; telephone: (816) 329-4059; fax: (816) 329-4090; email: 
doug.rudolph@faa.gov.

SUPPLEMENTARY INFORMATION: 

Discussion

    On March 27, 2008, we issued AD 2008-07-11, Amendment 39-15452 (73 
FR 18433, April 4, 2008). That AD required actions intended to address 
an unsafe condition on the products listed above.
    AD 2008-07-11, Amendment 39-15452 (73 FR 18433, April 4, 2008) was 
based on results of a full-scale fatigue test of the pitch trim 
actuator on PILATUS AIRCRAFT LTD. Models PC-12, PC-12/45, and PC-12/47 
airplanes. The life-limit was extended and the time between overhaul 
(TBO) was reduced. In addition, based on the results of the fatigue 
test, a life-limit of the pitch trim actuator attachment had been 
established.
    These new limitations were incorporated into the airworthiness 
limitations section of the Pilatus PC-12 Airplane Maintenance Manual 
(AMM) 12-A/AMP-04, chapter 4, revision 10, dated October 26, 2007.
    The new limitations for the pitch trim actuator TBO were moved from 
Chapter 5: Time Limits/Maintenance Checks, to Chapter 4: Structural, 
Component and Miscellaneous--Airworthiness Limitations. Since both 
chapter 4 and chapter 5 are mandatory within the European and Swiss 
airworthiness systems, it was not necessary for the European Aviation 
Safety Agency (EASA) and the Federal Office of Civil Aviation (FOCA) to 
issue an AD to mandate these new limitations.
    The only way the FAA can mandate the implementation of changes to 
the airworthiness limitations section of an FAA-approved maintenance 
program is by AD action.
    On February 8, 2013, we issued AD 2012-26-16, Amendment 39-17311 
(78 FR 11572, February 19, 2013). AD 2012-26-16 also requires 
incorporating new revisions into the Limitations section, Chapter 4, of 
the Pilatus PC-12 AMM. The limitations were revised to include an 
inspection of the wing main spar fastener holes at rib 6 for cracks.
    After issuing AD 2012-26-16, Amendment 39-17311 (78 FR 11572, 
February 19, 2013), we determined that AD 2008-07-11 should have been 
superseded by AD 2012-26-16. Since AD 2008-07-11 requires incorporating 
an earlier version of the airworthiness limitations section of the AMM, 
it could cause confusion for the owners/operators and could result in 
missed inspections and replacements required by AD 2012-26-16. 
Therefore, the need to continue to address this subject as an unsafe 
condition through AD 2008-07-11 is no longer necessary.

FAA's Determination

    We are issuing this AD because we evaluated all available 
information and determined the existing AD is no longer necessary.

AD Requirements

    This AD would rescind AD 2008-07-11, Amendment 39-15452 (73 FR 
18433, April 4, 2008).

FAA's Determination of the Effective Date

    An unsafe condition exists or could develop that requires the 
immediate adoption of this AD. The FAA has found that the risk to the 
flying public justifies waiving notice and comment prior to adoption of 
this rule because the unsafe condition addressed in AD 2008-07-11, 
Amendment 39-15452 (73 FR 18433, April 4, 2008) is currently addressed 
in AD 2012-26-16, Amendment 39-17311

[[Page 17866]]

(78 FR 11572, February 19, 2013). Allowing the airworthiness limitation 
section (ALS) required by AD 2008-07-11 to remain valid could cause 
confusion as to what is required and this could introduce an unsafe 
condition if certain areas were not inspected. Therefore, we determined 
that notice and opportunity for public comment before issuing this AD 
are impracticable and that good cause exists for making this amendment 
effective in fewer than 30 days.

Comments Invited

    This AD is a final rule that involves requirements affecting flight 
safety, and we did not precede it by notice and opportunity for public 
comment. We invite you to send any written relevant data, views, or 
arguments about this AD. Send your comments to an address listed under 
the ADDRESSES section. Include ``Docket No. FAA-2008-0070; Directorate 
Identifier 2007-CE-098-AD'' at the beginning of your comments. We 
specifically invite comments on the overall regulatory, economic, 
environmental, and energy aspects of this AD. We will consider all 
comments received by the closing date and may amend this AD because of 
those comments.
    We will post all comments we receive, without change, to https://www.regulations.gov, including any personal information you provide. We 
will also post a report summarizing each substantive verbal contact we 
receive about this AD.

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 that this AD:
    (1) Is not a ``significant regulatory action'' under Executive 
Order 12866,
    (2) Is not a ``significant rule'' under the DOT Regulatory Policies 
and Procedures (44 FR 11034, February 26, 1979),
    (3) Will not affect intrastate aviation in Alaska, and
    (4) 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.

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

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 removing AD 2008-07-11, Amendment 39-
15452 (73 FR 18433, April 4, 2008), and adding the following new AD:

2008-07-11 R1 PILATUS AIRCRAFT LTD.: Amendment 39-17398; Docket No. 
FAA-2008-0070; Directorate Identifier 2007-CE-098-AD.

(a) Effective Date

    This airworthiness directive (AD) becomes effective April 15, 
2013.

(b) Affected ADs

    This AD rescinds AD 2008-07-11, Amendment 39-15452 (73 FR 18433, 
April 4, 2008).

(c) Applicability

    This AD applies to PILATUS AIRCRAFT LTD. Models PC-12, PC-12/45, 
and PC-12/47 airplanes, all serial numbers, certificated in any 
category.

(d) Subject

    Air Transport Association of America (ATA) Code 27: Flight 
Controls.

    Issued in Kansas City, Missouri on March 11, 2013.
Earl Lawrence,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 2013-06169 Filed 3-22-13; 8:45 am]
BILLING CODE 4910-13-P

This site is protected by reCAPTCHA and the Google Privacy Policy and Terms of Service apply.