82 FR 10859 - Airworthiness Directives; PILATUS AIRCRAFT LTD. Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 82, Issue 31 (February 16, 2017)
Federal Aviation Administration
Federal Register Volume 82, Issue 31 (February 16, 2017)
| Page Range | 10859-10860 | |
| FR Document | 2017-02772 |
[Federal Register Volume 82, Number 31 (Thursday, February 16, 2017)] [Rules and Regulations] [Pages 10859-10860] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2017-02772] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2016-7003; Directorate Identifier 2016-CE-015-AD; Amendment 39-18766; AD 2016-26-08] RIN 2120-AA64 Airworthiness Directives; PILATUS AIRCRAFT LTD. Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule; correction. ----------------------------------------------------------------------- SUMMARY: The FAA is correcting an airworthiness directive (AD) that published in the Federal Register. That AD applies to all PILATUS AIRCRAFT LTD. Models PC-12, PC-12/45, PC-12/47, and PC-12/47E airplanes. The second reference to the main landing gear (MLG) in paragraph (f)(6) is incorrect. This document corrects that error. In all other respects, the original document remains the same; however we are publishing the entire rule in the Federal Register. DATES: This final rule is effective February 16, 2017. The effective date of AD 2016-26-08 remains February 9, 2017. The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of February 9, 2017 (82 FR 1172, January 5, 2017). ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016- 7003; 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 address for the Docket Office (phone: 800-647- 5527) is 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: 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: Airworthiness Directive 2016-26-08, Amendment 39-18766 (82 FR 1172, January 5, 2017), requires incorporating new revisions into the Limitations section, Chapter 4, of the FAA-approved maintenance program (e.g., maintenance manual). The limitations were revised to include repetitive inspections of the main landing gear (MLG) attachment bolts. As published, in paragraph (f)(6) there is a typographical error to the second reference of the MLG. The published reference is MLB and it is should be MLG. Although no other part of the preamble or regulatory information has been corrected, we are publishing the entire rule in the Federal Register. The effective date of this AD remains February 9, 2017. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. Adoption of the Correction 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 [Corrected] 0 2. The FAA amends Sec. 39.13 by removing 39-18005 (79 FR 67343, November 13, 2014) and adding the following new AD: 2016-26-08 PILATUS AIRCRAFT LTD.: Amendment 39-18766; Docket No. FAA-2016-7003; Directorate Identifier 2016-CE-015-AD. [[Page 10860]] (a) Effective Date This airworthiness directive (AD) is effective February 9, 2017. (b) Affected ADs This AD replaces AD 2014-22-01, 39-18005 (79 FR 67343, November 13, 2014). (c) Applicability This AD applies to PILATUS AIRCRAFT LTD. Models PC-12, PC-12/45, PC-12/47, and PC-12/47E airplanes, all manufacturer serial numbers (MSNs), certificated in any category. (d) Subject Air Transport Association of America (ATA) Code 5: Time Limits. (e) Reason This AD was prompted by 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 a need to incorporate new revisions into the Limitations section, Chapter 4, of the FAA-approved maintenance program (e.g., maintenance manual). The limitations were revised to include repetitive inspections of the main landing gear (MLG) attachment bolts. These actions are required to ensure the continued operational safety of the affected airplanes. (f) Actions and Compliance Unless already done, do the actions in paragraphs (f)(1) through (6) of this AD: (1) Before further flight after February 9, 2017 (the effective date of this AD), insert the following revisions into the Limitations section of the FAA-approved maintenance program (e.g., maintenance manual). Compliance with an electronic version of the Limitations section is acceptable provided the specifically referenced sections are followed even though there may be differences with the pagination: (i) STRUCTURAL, COMPONENT AND MISCELLANEOUS--AIRWORTHINESS LIMITATIONS, Data module code 12-A-04-00-00-00A-000A-A, dated July 12, 2016, of the Pilatus Model type--PC-12, PC-12/45, PC-12/47 MSN- 101-888, Aircraft Maintenance Manual (AMM), Document No. 02049, 12- A-AM-00-00-00-I, revision 32, dated July 18, 2016; and (ii) STRUCTURAL AND COMPONENT LIMITATIONS--AIRWORTHINESS LIMITATIONS, Data module code 12-B-04-00-00-00A-000A-A, dated July 19, 2016, of the Pilatus Model type--PC-12/47E MSN-1001-UP, Aircraft Maintenance Manual (AMM), Document No. 02300, 12-B-AM-00-00-00-I, revision 15, dated July 30, 2016. (2) The new limitations section revisions listed in paragraphs (f)(1)(i) and (ii) of this AD specify the following: (i) Establish inspections of the MLG attachment bolts, (ii) Specify replacement of components before or upon reaching the applicable life limit, and (iii) Specify accomplishment of all applicable maintenance tasks within certain thresholds and intervals. (3) Only authorized Pilatus Service Centers can do the Supplemental Structural Inspection Document (SSID) as required by the documents in paragraphs (f)(1)(i) and (ii) of this AD because deviations from the type design in critical locations could make the airplane ineligible for this life extension. (4) If no compliance time is specified in the documents listed in paragraphs (f)(1)(i) and (ii) of this AD when doing any corrective actions where discrepancies are found as required in paragraph (f)(2)(iii) of this AD, do these corrective actions before further flight after doing the applicable maintenance task. (5) During the accomplishment of the actions required in paragraph (f)(2) of this AD, including all subparagraphs, if a discrepancy is found that is not identified in the documents listed in paragraphs (f)(1)(i) and (ii) of this AD, before further flight after finding the discrepancy, contact PILATUS AIRCRAFT LTD. at the address specified in paragraph (h) of this AD for a repair scheme and incorporate that repair scheme. (6) Before or upon accumulating 6 years time-in-service (TIS) on the MLG attachment bolts or within the next 3 months TIS after February 9, 2017 (the effective date of this AD), whichever occurs later, inspect the MLG attachment bolts for cracks and corrosion and before further flight take all necessary corrective actions. (g) Other FAA AD Provisions 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: 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. (i) 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. (ii) AMOCs approved for AD 2014-22-01, 39-18005 (79 FR 67343, November 13, 2014) are not approved as AMOCs for this AD. (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. (h) Related Information Refer to MCAI European Aviation Safety Agency (EASA) AD No. 2016-0083, dated April 28, 2016, for related information. You may examine the MCAI on the Internet at https://www.regulations.gov/document?D=FAA-2016-7003-0002. (i) Material Incorporated by Reference (1) The Director of the Federal Register approved the incorporation by reference (IBR) of the service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51. (2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise. (i) STRUCTURAL, COMPONENT AND MISCELLANEOUS--AIRWORTHINESS LIMITATIONS, Data module code 12-A-04-00-00-00A-000A-A, dated July 12, 2016, of the Pilatus Model type--PC-12, PC-12/45, PC-12/47 MSN- 101-888, Aircraft Maintenance Manual (AMM), Document No. 02049, 12- A-AM-00-00-00-I, revision 32, dated July 18, 2016. (ii) STRUCTURAL AND COMPONENT LIMITATIONS--AIRWORTHINESS LIMITATIONS, Data module code 12-B-04-00-00-00A-000A-A, dated July 19, 2016, of the Pilatus Model type--PC-12/47E MSN-1001-UP, Aircraft Maintenance Manual (AMM), Document No. 02300, 12-B-AM-00-00-00-I, revision 15, dated July 30, 2016. (3) For PILATUS AIRCRAFT LTD. service information identified in this AD, contact PILATUS AIRCRAFT LTD., Customer Service Manager, CH-6371 STANS, Switzerland; telephone: +41 (0) 41 619 33 33; fax: +41 (0) 41 619 73 11; Internet: http://www.pilatus-aircraft.com or email: aircraft.com">SupportPC12@pilatus-aircraft.com. (4) You may view this service information at FAA, FAA, Small Airplane Directorate, 901 Locust, Kansas City, Missouri 64106. For information on the availability of this material at the FAA, call (816) 329-4148. In addition, you can access this service information on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016-7003. (5) You may view this service information that is incorporated by reference 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: http://www.archives.gov/federal-register/cfr/ibr-locations.html. Issued in Kansas City, Missouri, on January 24, 2017. Melvin Johnson, Acting Manager, Small Airplane Directorate, Aircraft Certification Service. [FR Doc. 2017-02772 Filed 2-15-17; 8:45 am] BILLING CODE 4910-13-P
![Federal Register / Vol. 82, No. 31 / Thursday, February 16, 2017 / Rules and Regulations 10859
(n) Credit for Previous Actions (4) You may view this service information contains this AD, the regulatory
This paragraph provides credit for the at the FAA, Transport Airplane Directorate, evaluation, any comments received, and
actions required by paragraph (h) of this AD, 1601 Lind Avenue SW., Renton, WA. For other information. The address for the
if those actions were performed before the information on the availability of this
Docket Office (phone: 800–647–5527) is
effective date of this AD using Boeing Special material at the FAA, call 425–227–1221.
(5) You may view this service information Document Management Facility, U.S.
Attention Service Bulletin 737–53–1065, Department of Transportation, Docket
Revision 2, dated April 19, 2001, which was that is incorporated by reference at the
incorporated by reference in AD 2005–13–30. National Archives and Records Operations, M–30, West Building
Administration (NARA). For information on Ground Floor, Room W12–140, 1200
(o) Alternative Methods of Compliance the availability of this material at NARA, call New Jersey Avenue SE., Washington,
(AMOCs) 202–741–6030, or go to: http:// DC 20590.
(1) The Manager, Los Angeles Aircraft www.archives.gov/federal-register/cfr/ibr-
locations.html. FOR FURTHER INFORMATION CONTACT:
Certification Office (ACO), FAA, has the
authority to approve AMOCs for this AD, if Doug Rudolph, Aerospace Engineer,
Issued in Renton, Washington, on January FAA, Small Airplane Directorate, 901
requested using the procedures found in 14 11, 2017.
CFR 39.19. In accordance with 14 CFR 39.19, Locust, Room 301, Kansas City,
send your request to your principal inspector Michael Kaszycki, Missouri 64106; telephone: (816) 329–
or local Flight Standards District Office, as Acting Manager, Transport Airplane 4059; fax: (816) 329–4090; email:
appropriate. If sending information directly Directorate, Aircraft Certification Service. doug.rudolph@faa.gov.
to the manager of the ACO, send it to the [FR Doc. 2017–03112 Filed 2–15–17; 8:45 am]
attention of the person identified in SUPPLEMENTARY INFORMATION:
BILLING CODE 4910–13–P
paragraph (p) of this AD. Information may be Airworthiness Directive 2016–26–08,
emailed to: 9-ANM-LAACO-AMOC- Amendment 39–18766 (82 FR 1172,
Requests@faa.gov.
DEPARTMENT OF TRANSPORTATION January 5, 2017), requires incorporating
(2) Before using any approved AMOC, new revisions into the Limitations
notify your appropriate principal inspector, section, Chapter 4, of the FAA-approved
Federal Aviation Administration
or lacking a principal inspector, the manager maintenance program (e.g., maintenance
of the local flight standards district office/
certificate holding district office. 14 CFR Part 39 manual). The limitations were revised to
(3) An AMOC that provides an acceptable include repetitive inspections of the
[Docket No. FAA–2016–7003; Directorate main landing gear (MLG) attachment
level of safety may be used for any repair, Identifier 2016–CE–015–AD; Amendment
modification, or alteration required by this 39–18766; AD 2016–26–08]
bolts.
AD if it is approved by the Boeing As published, in paragraph (f)(6) there
Commercial Airplanes Organization RIN 2120–AA64 is a typographical error to the second
Designation Authorization (ODA) that has reference of the MLG. The published
been authorized by the Manager, Los Angeles Airworthiness Directives; PILATUS
reference is MLB and it is should be
ACO, to make those findings. To be AIRCRAFT LTD. Airplanes
approved, the repair method, modification
MLG.
deviation, or alteration deviation must meet AGENCY: Federal Aviation Although no other part of the
the certification basis of the airplane, and the Administration (FAA), DOT. preamble or regulatory information has
approval must specifically refer to this AD. ACTION: Final rule; correction. been corrected, we are publishing the
(4) AMOCs approved previously for AD entire rule in the Federal Register.
2005–13–30, are approved as AMOCs for the SUMMARY: The FAA is correcting an The effective date of this AD remains
corresponding provisions of paragraph (h) of airworthiness directive (AD) that February 9, 2017.
this AD. published in the Federal Register. That
(p) Related Information AD applies to all PILATUS AIRCRAFT List of Subjects in 14 CFR Part 39
For more information about this AD, LTD. Models PC–12, PC–12/45, PC–12/ Air transportation, Aircraft, Aviation
contact Jennifer Tsakoumakis, Aerospace 47, and PC–12/47E airplanes. The safety, Incorporation by reference,
Engineer, Airframe Branch, ANM–120L, second reference to the main landing Safety.
FAA, Los Angeles ACO, 3960 Paramount gear (MLG) in paragraph (f)(6) is
Boulevard, Lakewood, CA 90712–4137; incorrect. This document corrects that Adoption of the Correction
phone: 562–627–5264; fax: 562–627–5210; error. In all other respects, the original
email: jennifer.tsakoumakis@faa.gov.
Accordingly, under the authority
document remains the same; however delegated to me by the Administrator,
(q) Material Incorporated by Reference we are publishing the entire rule in the the FAA amends 14 CFR part 39 as
(1) The Director of the Federal Register Federal Register. follows:
approved the incorporation by reference DATES: This final rule is effective
(IBR) of the service information listed in this February 16, 2017. The effective date of PART 39—AIRWORTHINESS
paragraph under 5 U.S.C. 552(a) and 1 CFR AD 2016–26–08 remains February 9, DIRECTIVES
part 51. 2017.
(2) You must use this service information ■ 1. The authority citation for part 39
The Director of the Federal Register
as applicable to do the actions required by continues to read as follows:
this AD, unless the AD specifies otherwise. approved the incorporation by reference
(i) Boeing Special Attention Service of certain publications listed in this AD Authority: 49 U.S.C. 106(g), 40113, 44701.
Bulletin 737–53–1065, Revision 3, dated June as of February 9, 2017 (82 FR 1172,
January 5, 2017). § 39.13 [Corrected]
30, 2015.
(ii) Reserved. ADDRESSES: You may examine the AD ■ 2. The FAA amends § 39.13 by
jstallworth on DSK7TPTVN1PROD with RULES
(3) For Boeing service information docket on the Internet at http:// removing 39–18005 (79 FR 67343,
identified in this AD, contact Boeing
www.regulations.gov by searching for November 13, 2014) and adding the
Commercial Airplanes, Attention:
Contractual & Data Services (C&DS), 2600 and locating Docket No. FAA–2016– following new AD:
Westminster Blvd., MC 110–SK57, Seal 7003; or in person at the Docket 2016–26–08 PILATUS AIRCRAFT LTD.:
Beach, CA 90740–5600; telephone 562–797– Management Facility between 9 a.m. Amendment 39–18766; Docket No.
1717; Internet https:// and 5 p.m., Monday through Friday, FAA–2016–7003; Directorate Identifier
www.myboeingfleet.com. except Federal holidays. The AD docket 2016–CE–015–AD.
VerDate Sep<11>2014 11:26 Feb 15, 2017 Jkt 241001 PO 00000 Frm 00005 Fmt 4700 Sfmt 4700 E:\FR\FM\16FER1.SGM 16FER1](https://thefederalregister.org/doc/82_FR_10890/page/1.svg)
![10860 Federal Register / Vol. 82, No. 31 / Thursday, February 16, 2017 / Rules and Regulations
(a) Effective Date (3) Only authorized Pilatus Service Centers paragraph under 5 U.S.C. 552(a) and 1 CFR
This airworthiness directive (AD) is can do the Supplemental Structural part 51.
effective February 9, 2017. Inspection Document (SSID) as required by (2) You must use this service information
the documents in paragraphs (f)(1)(i) and (ii) as applicable to do the actions required by
(b) Affected ADs of this AD because deviations from the type this AD, unless the AD specifies otherwise.
This AD replaces AD 2014–22–01, 39– design in critical locations could make the (i) STRUCTURAL, COMPONENT AND
18005 (79 FR 67343, November 13, 2014). airplane ineligible for this life extension. MISCELLANEOUS—AIRWORTHINESS
(4) If no compliance time is specified in the LIMITATIONS, Data module code 12–A–04–
(c) Applicability documents listed in paragraphs (f)(1)(i) and 00–00–00A–000A–A, dated July 12, 2016, of
This AD applies to PILATUS AIRCRAFT (ii) of this AD when doing any corrective the Pilatus Model type—PC–12, PC–12/45,
LTD. Models PC–12, PC–12/45, PC–12/47, actions where discrepancies are found as PC–12/47 MSN–101–888, Aircraft
and PC–12/47E airplanes, all manufacturer required in paragraph (f)(2)(iii) of this AD, do Maintenance Manual (AMM), Document No.
serial numbers (MSNs), certificated in any these corrective actions before further flight 02049, 12–A–AM–00–00–00–I, revision 32,
category. after doing the applicable maintenance task. dated July 18, 2016.
(5) During the accomplishment of the (ii) STRUCTURAL AND COMPONENT
(d) Subject actions required in paragraph (f)(2) of this LIMITATIONS—AIRWORTHINESS
Air Transport Association of America AD, including all subparagraphs, if a LIMITATIONS, Data module code 12–B–04–
(ATA) Code 5: Time Limits. discrepancy is found that is not identified in 00–00–00A–000A–A, dated July 19, 2016, of
the documents listed in paragraphs (f)(1)(i) the Pilatus Model type—PC–12/47E MSN–
(e) Reason
and (ii) of this AD, before further flight after 1001–UP, Aircraft Maintenance Manual
This AD was prompted by mandatory finding the discrepancy, contact PILATUS (AMM), Document No. 02300, 12–B–AM–00–
continuing airworthiness information (MCAI) AIRCRAFT LTD. at the address specified in 00–00–I, revision 15, dated July 30, 2016.
originated by an aviation authority of another paragraph (h) of this AD for a repair scheme (3) For PILATUS AIRCRAFT LTD. service
country to identify and correct an unsafe and incorporate that repair scheme. information identified in this AD, contact
condition on an aviation product. The MCAI (6) Before or upon accumulating 6 years PILATUS AIRCRAFT LTD., Customer Service
describes the unsafe condition as a need to time-in-service (TIS) on the MLG attachment Manager, CH–6371 STANS, Switzerland;
incorporate new revisions into the bolts or within the next 3 months TIS after telephone: +41 (0) 41 619 33 33; fax: +41 (0)
Limitations section, Chapter 4, of the FAA- February 9, 2017 (the effective date of this 41 619 73 11; Internet: http://www.pilatus-
approved maintenance program (e.g., AD), whichever occurs later, inspect the MLG aircraft.com or email: SupportPC12@pilatus-
maintenance manual). The limitations were attachment bolts for cracks and corrosion and
revised to include repetitive inspections of aircraft.com.
before further flight take all necessary (4) You may view this service information
the main landing gear (MLG) attachment corrective actions.
bolts. These actions are required to ensure at FAA, FAA, Small Airplane Directorate,
the continued operational safety of the (g) Other FAA AD Provisions 901 Locust, Kansas City, Missouri 64106. For
affected airplanes. information on the availability of this
The following provisions also apply to this
material at the FAA, call (816) 329–4148. In
AD:
(f) Actions and Compliance addition, you can access this service
(1) Alternative Methods of Compliance
Unless already done, do the actions in (AMOCs): The Manager, Standards Office, information on the Internet at http://
paragraphs (f)(1) through (6) of this AD: FAA, has the authority to approve AMOCs www.regulations.gov by searching for and
(1) Before further flight after February 9, for this AD, if requested using the procedures locating Docket No. FAA–2016–7003.
2017 (the effective date of this AD), insert the found in 14 CFR 39.19. Send information to (5) You may view this service information
following revisions into the Limitations ATTN: Doug Rudolph, Aerospace Engineer, that is incorporated by reference at the
section of the FAA-approved maintenance FAA, Small Airplane Directorate, 901 Locust, National Archives and Records
program (e.g., maintenance manual). Room 301, Kansas City, Missouri 64106; Administration (NARA). For information on
Compliance with an electronic version of the telephone: (816) 329–4059; fax: (816) 329– the availability of this material at NARA, call
Limitations section is acceptable provided 4090; email: doug.rudolph@faa.gov. 202–741–6030, or go to: http://
the specifically referenced sections are (i) Before using any approved AMOC on www.archives.gov/federal-register/cfr/ibr-
followed even though there may be any airplane to which the AMOC applies, locations.html.
differences with the pagination: notify your appropriate principal inspector Issued in Kansas City, Missouri, on January
(i) STRUCTURAL, COMPONENT AND (PI) in the FAA Flight Standards District 24, 2017.
MISCELLANEOUS—AIRWORTHINESS Office (FSDO), or lacking a PI, your local
LIMITATIONS, Data module code 12–A–04– Melvin Johnson,
FSDO.
00–00–00A–000A–A, dated July 12, 2016, of (ii) AMOCs approved for AD 2014–22–01, Acting Manager, Small Airplane Directorate,
the Pilatus Model type—PC–12, PC–12/45, 39–18005 (79 FR 67343, November 13, 2014) Aircraft Certification Service.
PC–12/47 MSN–101–888, Aircraft are not approved as AMOCs for this AD. [FR Doc. 2017–02772 Filed 2–15–17; 8:45 am]
Maintenance Manual (AMM), Document No. (2) Airworthy Product: For any requirement BILLING CODE 4910–13–P
02049, 12–A–AM–00–00–00–I, revision 32, in this AD to obtain corrective actions from
dated July 18, 2016; and a manufacturer or other source, use these
(ii) STRUCTURAL AND COMPONENT actions if they are FAA-approved. Corrective
LIMITATIONS—AIRWORTHINESS
DEPARTMENT OF TRANSPORTATION
actions are considered FAA-approved if they
LIMITATIONS, Data module code 12–B–04– are approved by the State of Design Authority
00–00–00A–000A–A, dated July 19, 2016, of
Federal Aviation Administration
(or their delegated agent). You are required
the Pilatus Model type—PC–12/47E MSN– to assure the product is airworthy before it
1001–UP, Aircraft Maintenance Manual is returned to service. 14 CFR Part 39
(AMM), Document No. 02300, 12–B–AM–00– [Docket No. FAA–2013–0797; Directorate
00–00–I, revision 15, dated July 30, 2016. (h) Related Information
Identifier 2013–NM–007–AD; Amendment
(2) The new limitations section revisions Refer to MCAI European Aviation Safety 39–18776; AD 2017–01–09]
listed in paragraphs (f)(1)(i) and (ii) of this Agency (EASA) AD No. 2016–0083, dated
AD specify the following: April 28, 2016, for related information. You RIN 2120–AA64
jstallworth on DSK7TPTVN1PROD with RULES
(i) Establish inspections of the MLG may examine the MCAI on the Internet at
attachment bolts, https://www.regulations.gov/ Airworthiness Directives; The Boeing
(ii) Specify replacement of components document?D=FAA-2016-7003-0002. Company Airplanes
before or upon reaching the applicable life
limit, and (i) Material Incorporated by Reference AGENCY: Federal Aviation
(iii) Specify accomplishment of all (1) The Director of the Federal Register Administration (FAA), DOT.
applicable maintenance tasks within certain approved the incorporation by reference
ACTION: Final rule; correction.
thresholds and intervals. (IBR) of the service information listed in this
VerDate Sep<11>2014 11:26 Feb 15, 2017 Jkt 241001 PO 00000 Frm 00006 Fmt 4700 Sfmt 4700 E:\FR\FM\16FER1.SGM 16FER1](https://thefederalregister.org/doc/82_FR_10890/page/2.svg)
Document Created: 2018-02-01 15:02:21
Document Modified: 2018-02-01 15:02:21
| Category | Regulatory Information | |
| Collection | Federal Register | |
| sudoc Class | AE 2.7: GS 4.107: AE 2.106: | |
| Publisher | Office of the Federal Register, National Archives and Records Administration | |
| Section | Rules and Regulations | |
| Action | Final rule; correction. | |
| Dates | This final rule is effective February 16, 2017. The effective date of AD 2016-26-08 remains February 9, 2017. | |
| 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: [email protected] | |
| FR Citation | 82 FR 10859 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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