81 FR 70929 - Airworthiness Directives; Continental Motors, Inc. Reciprocating Engines
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 81, Issue 199 (October 14, 2016)
Federal Aviation Administration
Federal Register Volume 81, Issue 199 (October 14, 2016)
| Page Range | 70929-70931 | |
| FR Document | 2016-24794 |
[Federal Register Volume 81, Number 199 (Friday, October 14, 2016)] [Rules and Regulations] [Pages 70929-70931] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2016-24794] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2016-0069; Directorate Identifier 2016-NE-01-AD; Amendment 39-18685; AD 2016-21-04] RIN 2120-AA64 Airworthiness Directives; Continental Motors, Inc. Reciprocating Engines AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. ----------------------------------------------------------------------- SUMMARY: We are adopting a new airworthiness directive (AD) for certain Continental Motors, Inc. (CMI) TSIO-550-K, TSIOF-550-K, TSIO-550-C, TSIOF-550-D, and TSIO-550-N reciprocating engines. This AD was [[Page 70930]] prompted by a report of an uncommanded in-flight shutdown (IFSD) resulting in injuries and significant airplane damage. This AD requires replacing the oil cooler cross fitting assembly. We are issuing this AD to prevent failure of the oil cooler cross fitting and engine, IFSD, and loss of the airplane. DATES: This AD is effective November 18, 2016. The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of November 18, 2016. ADDRESSES: For service information identified in this final rule, contact Continental Motors, Inc., 2039 Broad Street, Mobile, Alabama 36615; phone: 800-326-0089; Internet: http://www.continentalmotors.aero. You may view this service information at the FAA, Engine & Propeller Directorate, 1200 District Avenue, Burlington, MA. For information on the availability of this material at the FAA, call 781-238-7125. Examining the AD Docket You may examine the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016- 0069; 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: Scott Hopper, Aerospace Engineer, Atlanta Aircraft Certification Office, FAA, Small Airplane Directorate, 1701 Columbia Avenue, College Park, GA 30337; phone: 404-474-5535; fax: 404-474-5606; email: [email protected]. SUPPLEMENTARY INFORMATION: Discussion We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by adding an AD that would apply to certain CMI TSIO-550-K, TSIOF-550-K, TSIO-550-C, TSIOF-550-D, and TSIO-550-N reciprocating engines. The NPRM published in the Federal Register on March 11, 2016 (81 FR 12833). The NPRM was prompted by a report of an uncommanded IFSD resulting in injuries and significant airplane damage. The NPRM proposed to require replacing the oil cooler cross fitting assembly. We are issuing this AD 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. Change to Cost of Compliance We increased our estimate of the cost of the affected parts in this AD from $0 to $261 per engine and increased the number of labor hours to perform the replacement from 1 to 2 hours. This increased the overall estimated cost of compliance from $111,095 to $563,317. Update to Service Information We revised our reference in this AD from CMI Critical Service Bulletin (CSB) CSB15-7, Revision A, dated November 10, 2015 (also referred to as CMI CSB CSB15-7A, dated November 10, 2015) to CMI CSB CSB15-7, Revision B, dated April 26, 2016 (also referred to as CMI CSB CSB15-7B) to reflect the latest service information published by CMI. Clarification of Part Number We clarified in this AD that the affected oil cooler cross fitting has a part number AN918-1J or AN918-2J. Conclusion We reviewed the relevant data and determined that air safety and the public interest require adopting this AD as proposed except for the changes noted above. We have determined that these changes:Are consistent with the intent that was proposed in the NPRM for correcting the unsafe condition; and Do not add any additional burden upon the public than was already proposed in the NPRM. Relevant Service Information Under 1 CFR part 51 We reviewed CMI CSB CSB15-2, Revision C, dated November 9, 2015 (also referred to as CMI CSB CSB15-2C, dated November 9, 2015), and CMI CSB CSB15-7, Revision B, dated April 26, 2016 (also referred to as CMI CSB CSB15-7B, dated April 26, 2016). The CSBs describe detailed procedures for replacing oil cooler cross fittings, nipples, and bushings with a redesigned oil cooler cross fitting. This service information is reasonably available because the interested parties have access to it through their normal course of business or by the means identified in the ADDRESSES section. Costs of Compliance We estimate that this AD affects 1,307 engines installed on airplanes of U.S. registry. We also estimate that it will take about 2 hours per engine to comply with this AD. The average labor rate is $85 per hour. Parts cost about $261 per engine. Based on these figures, we estimate the total cost of this AD to U.S. operators to be $563,317. Our cost estimate is exclusive of possible warranty coverage. 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 This AD will not have federalism implications under Executive Order 13132. This AD will not have a substantial direct effect on the States, on the relationship between the national government and the States, or on the distribution of power and responsibilities among the various levels of government. For the reasons discussed above, I certify that this AD: (1) Is not a ``significant regulatory action'' under Executive Order 12866, (2) Is not a ``significant rule'' under DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979), (3) Will not affect intrastate aviation in Alaska to the extent that it justifies making a regulatory distinction, 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. [[Page 70931]] 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 adding the following new airworthiness directive (AD): 2016-21-04 Continental Motors, Inc. (Type Certificate previously held by Teledyne Continental Motors) Reciprocating Engines: Amendment 39-18685; Docket No. FAA-2016-0069; Directorate Identifier 2016-NE-01-AD. (a) Effective Date This AD is effective November 18, 2016. (b) Affected ADs None. (c) Applicability This AD applies to Continental Motors, Inc. (CMI) TSIO-550-K, TSIOF-550-K, TSIO-550-C, TSIOF-550-D, and TSIO-550-N reciprocating engines with an engine serial number below 1012296 and an oil cooler cross fitting, part number AN918-1J or AN918-2J, installed. (d) Unsafe Condition This AD was prompted by a report of an uncommanded in-flight shutdown (IFSD) resulting in injuries and significant airplane damage. We are issuing this AD to prevent failure of the oil cooler cross fitting and engine, IFSD, and loss of the airplane. (e) Compliance Comply with this AD within the compliance times specified, unless already done. (1) Within 12 months or 100 flight hours after the effective date of the AD, whichever occurs first, replace the oil cooler cross fitting, nipple, and bushing. Use the Action Required paragraphs III.1 through III.8 of CMI Critical Service Bulletin (CSB) CSB15-2, Revision C, dated November 9, 2015 (also referred to as CMI CSB CSB15-2C, dated November 9, 2015), or the Action Required paragraphs III.1 through III.8 of CMI CSB CSB15-7, Revision B, dated April 26, 2016 (also referred to as CMI CSB15-7B, dated April 26, 2016), to perform the replacement. (2) Reserved. (f) Credit for Previous Actions You may take credit for the replacement that is required by paragraph (e) of this AD, if the replacement was performed before the effective date of this AD using CMI CSB CSB15-2B, dated November 6, 2015 or earlier versions; or CSB CSB15-7A, dated November 10, 2015 or earlier version. (g) Alternative Methods of Compliance (AMOCs) The Manager, Atlanta Certification Office, FAA, may approve AMOCs for this AD. Use the procedures found in 14 CFR 39.19 to make your request. (h) Related Information For more information about this AD, contact Scott Hopper, Aerospace Engineer, Atlanta Aircraft Certification Office, FAA, Small Airplane Directorate, 1701 Columbia Avenue, College Park, GA 30337; phone: 404-474-5535; fax: 404-474-5606; email: [email protected]. (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) Continental Motors, Inc. (CMI) Critical Service Bulletin (CSB) CSB15-2, Revision C, dated November 9, 2015 (also referred to as CMI CSB CSB15-2C, dated November 9, 2015). (ii) CMI CSB CSB15-7, Revision B, dated April 26, 2016 (also referred to as CMI CSB CSB15-7B, dated April 26, 2016). (3) For CMI service information identified in this AD, contact Continental Motors, Inc., 2039 Broad Street, Mobile, Alabama 36615; phone: 800-326-0089; Internet: http://www.continentalmotors.aero. (4) You may view this service information at FAA, Engine & Propeller Directorate, 1200 District Avenue, Burlington, MA. For information on the availability of this material at the FAA, call 781-238-7125. (5) You may view this service information 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 Burlington, Massachusetts, on October 7, 2016. Colleen M. D'Alessandro, Manager, Engine & Propeller Directorate, Aircraft Certification Service. [FR Doc. 2016-24794 Filed 10-13-16; 8:45 am] BILLING CODE 4910-13-P
![Federal Register / Vol. 81, No. 199 / Friday, October 14, 2016 / Rules and Regulations 70929
Costs of Compliance List of Subjects in 14 CFR Part 39 Management Group, Rotorcraft Directorate,
FAA, 10101 Hillwood Pkwy, Fort Worth, TX
We estimate that this AD affects 43 Air transportation, Aircraft, Aviation 76177; telephone (817) 222–5110; email
helicopters of U.S. Registry. safety, Incorporation by reference, 9-ASW-FTW-AMOC-Requests@faa.gov.
We estimate that operators may incur Safety. (2) For operations conducted under a 14
the following costs to comply with this Adoption of the Amendment CFR part 119 operating certificate or under
AD. At an average labor cost of $85 per 14 CFR part 91, subpart K, we suggest that
work-hour, we estimate reviewing and Accordingly, under the authority you notify your principal inspector, or
revising the records requires 1 work- delegated to me by the Administrator, lacking a principal inspector, the manager of
the FAA amends 14 CFR part 39 as the local flight standards district office or
hour for a cost of about $85 per
follows: certificate holding district office, before
helicopter and $3,655 for the U.S. fleet. operating any aircraft complying with this
We estimate replacing a bolt that has AD through an AMOC.
PART 39—AIRWORTHINESS
exceeded its life limit requires 0.5 work-
DIRECTIVES (g) Additional Information
hour plus $290 for a replacement bolt,
for a total cost of $333 per bolt. ■ 1. The authority citation for part 39 (1) Bell Helicopter Alert Service Bulletin
430–12–47, dated November 14, 2012, which
Authority for This Rulemaking continues to read as follows:
is not incorporated by reference, contains
Title 49 of the United States Code Authority: 49 U.S.C. 106(g), 40113, 44701. additional information about the subject of
this final rule. For service information
specifies the FAA’s authority to issue § 39.13 [Amended] identified in this final rule, contact Bell
rules on aviation safety. Subtitle I, Helicopter Textron Canada Limited, 12,800
■ 2. The FAA amends § 39.13 by adding
section 106, describes the authority of Rue de l’Avenir, Mirabel, Quebec J7J1R4;
the following new airworthiness
the FAA Administrator. Subtitle VII: telephone (450) 437–2862 or (800) 363–8023;
directive (AD):
Aviation Programs, describes in more fax (450) 433–0272; or at http://
detail the scope of the Agency’s 2016–21–01 Bell Helicopter Textron: www.bellcustomer.com/files/. You may
authority. Amendment 39–18682; Docket No. review a copy of the service information at
We are issuing this rulemaking under FAA–2016–6551; Directorate Identifier the FAA, Office of the Regional Counsel,
2013–SW–070–AD. Southwest Region, 10101 Hillwood Pkwy,
the authority described in Subtitle VII,
(a) Applicability Room 6N–321, Fort Worth, TX 76177.
Part A, Subpart III, Section 44701:
(2) The subject of this AD is addressed in
‘‘General requirements.’’ Under that This AD applies to Model 430 helicopters, Transport Canada AD No. CF–2013–26, dated
section, Congress charges the FAA with serial number 49001 through 49129, with a September 24, 2013. You may view the
promoting safe flight of civil aircraft in main rotor head attachment bolt (bolt) part Transport Canada AD on the Internet at
air commerce by prescribing regulations number (P/N) MS21250–08083 installed, http://www.regulations.gov in Docket No.
for practices, methods, and procedures certificated in any category. FAA–2016–6551.
the Administrator finds necessary for (b) Unsafe Condition (h) Subject
safety in air commerce. This regulation This AD defines the unsafe condition as a Joint Aircraft Service Component (JASC)
is within the scope of that authority bolt remaining in service beyond its fatigue Code: 6220 Main Rotor Head.
because it addresses an unsafe condition life. This condition could result in failure of
that is likely to exist or develop on a bolt, failure of the main rotor hub and Issued in Fort Worth, Texas, on October 3,
helicopters identified in this rulemaking subsequent loss of control of a helicopter. 2016.
action. (c) Effective Date Lance T. Gant,
Manager, Rotorcraft Directorate, Aircraft
Regulatory Findings This AD becomes effective November 18,
Certification Service.
2016.
This AD will not have federalism [FR Doc. 2016–24741 Filed 10–13–16; 8:45 am]
implications under Executive Order (d) Compliance BILLING CODE 4910–13–P
13132. This AD will not have a You are responsible for performing each
substantial direct effect on the States, on action required by this AD within the
the relationship between the national specified compliance time unless it has DEPARTMENT OF TRANSPORTATION
already been accomplished prior to that time.
government and the States, or on the
distribution of power and (e) Required Actions Federal Aviation Administration
responsibilities among the various Within 10 hours time-in-service (TIS):
levels of government. (1) Revise the Airworthiness Limitations 14 CFR Part 39
For the reasons discussed above, I section of the applicable maintenance [Docket No. FAA–2016–0069; Directorate
certify that this AD: manual or Instructions for Continued Identifier 2016–NE–01–AD; Amendment 39–
(1) Is not a ‘‘significant regulatory Airworthiness (ICA) to establish a life limit 18685; AD 2016–21–04]
action’’ under Executive Order 12866; of 5,000 hours TIS for each bolt P/N
MS21250–08083. RIN 2120–AA64
(2) Is not a ‘‘significant rule’’ under
(2) Determine the number of hours TIS for
DOT Regulatory Policies and Procedures each bolt and update the helicopter’s Airworthiness Directives; Continental
(44 FR 11034, February 26, 1979); historical records. If the hours TIS is Motors, Inc. Reciprocating Engines
(3) Will not affect intrastate aviation unknown, calculate the number of hours TIS
in Alaska to the extent that it justifies by counting the helicopter’s hours TIS AGENCY: Federal Aviation
making a regulatory distinction; and beginning January 1, 2009. Administration (FAA), DOT.
(4) Will not have a significant (3) Remove from service each bolt that has ACTION: Final rule.
economic impact, positive or negative, reached or exceeded its life limit.
ehiers on DSK5VPTVN1PROD with RULES
on a substantial number of small entities (f) Alternative Methods of Compliance SUMMARY: We are adopting a new
under the criteria of the Regulatory (AMOCs) airworthiness directive (AD) for certain
Flexibility Act. (1) The Manager, Safety Management Continental Motors, Inc. (CMI) TSIO–
We prepared an economic evaluation Group, FAA, may approve AMOCs for this 550–K, TSIOF–550–K, TSIO–550–C,
of the estimated costs to comply with AD. Send your proposal to: Matt Fuller, TSIOF–550–D, and TSIO–550–N
this AD and placed it in the AD docket. Senior Aviation Safety Engineer, Safety reciprocating engines. This AD was
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![Federal Register / Vol. 81, No. 199 / Friday, October 14, 2016 / Rules and Regulations 70931
Adoption of the Amendment (g) Alternative Methods of Compliance SUMMARY: This amendment adopts
(AMOCs) miscellaneous amendments to the
Accordingly, under the authority
delegated to me by the Administrator, The Manager, Atlanta Certification Office, required IFR (instrument flight rules)
FAA, may approve AMOCs for this AD. Use altitudes and changeover points for
the FAA amends 14 CFR part 39 as
the procedures found in 14 CFR 39.19 to certain Federal airways, jet routes, or
follows: make your request. direct routes for which a minimum or
PART 39—AIRWORTHINESS (h) Related Information maximum en route authorized IFR
DIRECTIVES For more information about this AD, altitude is prescribed. This regulatory
contact Scott Hopper, Aerospace Engineer, action is needed because of changes
■ 1. The authority citation for part 39 Atlanta Aircraft Certification Office, FAA, occurring in the National Airspace
continues to read as follows: Small Airplane Directorate, 1701 Columbia System. These changes are designed to
Authority: 49 U.S.C. 106(g), 40113, 44701. Avenue, College Park, GA 30337; phone: provide for the safe and efficient use of
404–474–5535; fax: 404–474–5606; email: the navigable airspace under instrument
§ 39.13 [Amended] scott.hopper@faa.gov. conditions in the affected areas.
■ 2. The FAA amends § 39.13 by adding (i) Material Incorporated by Reference DATES: Effective 0901 UTC, November
the following new airworthiness (1) The Director of the Federal Register 10, 2016.
directive (AD): approved the incorporation by reference FOR FURTHER INFORMATION CONTACT:
2016–21–04 Continental Motors, Inc. (Type (IBR) of the service information listed in this Thomas J Nichols, Flight Procedure
Certificate previously held by Teledyne paragraph under 5 U.S.C. 552(a) and 1 CFR Standards Branch (AMCAFS–420),
Continental Motors) Reciprocating part 51. Flight Technologies and Programs
Engines: Amendment 39–18685; Docket (2) You must use this service information
Division, Flight Standards Service,
No. FAA–2016–0069; Directorate as applicable to do the actions required by
this AD, unless the AD specifies otherwise. Federal Aviation Administration, Mike
Identifier 2016–NE–01–AD. Monroney Aeronautical Center, 6500
(i) Continental Motors, Inc. (CMI) Critical
(a) Effective Date Service Bulletin (CSB) CSB15–2, Revision C, South MacArthur Blvd., Oklahoma City,
This AD is effective November 18, 2016. dated November 9, 2015 (also referred to as OK, 73169 (Mail Address: P.O. Box
CMI CSB CSB15–2C, dated November 9, 25082, Oklahoma City, OK 73125).
(b) Affected ADs 2015). Telephone: (405) 954–4164.
None. (ii) CMI CSB CSB15–7, Revision B, dated SUPPLEMENTARY INFORMATION: This
April 26, 2016 (also referred to as CMI CSB
(c) Applicability CSB15–7B, dated April 26, 2016).
amendment to part 95 of the Federal
This AD applies to Continental Motors, (3) For CMI service information identified Aviation Regulations (14 CFR part 95)
Inc. (CMI) TSIO–550–K, TSIOF–550–K, in this AD, contact Continental Motors, Inc., amends, suspends, or revokes IFR
TSIO–550–C, TSIOF–550–D, and TSIO–550– 2039 Broad Street, Mobile, Alabama 36615; altitudes governing the operation of all
N reciprocating engines with an engine serial phone: 800–326–0089; Internet: http:// aircraft in flight over a specified route
number below 1012296 and an oil cooler www.continentalmotors.aero. or any portion of that route, as well as
cross fitting, part number AN918–1J or (4) You may view this service information the changeover points (COPs) for
AN918–2J, installed. at FAA, Engine & Propeller Directorate, 1200 Federal airways, jet routes, or direct
District Avenue, Burlington, MA. For routes as prescribed in part 95.
(d) Unsafe Condition
information on the availability of this
This AD was prompted by a report of an material at the FAA, call 781–238–7125. The Rule
uncommanded in-flight shutdown (IFSD) (5) You may view this service information
resulting in injuries and significant airplane at the National Archives and Records
The specified IFR altitudes, when
damage. We are issuing this AD to prevent Administration (NARA). For information on used in conjunction with the prescribed
failure of the oil cooler cross fitting and the availability of this material at NARA, call changeover points for those routes,
engine, IFSD, and loss of the airplane. 202–741–6030, or go to: http:// ensure navigation aid coverage that is
(e) Compliance www.archives.gov/federal-register/cfr/ibr- adequate for safe flight operations and
locations.html. free of frequency interference. The
Comply with this AD within the reasons and circumstances that create
compliance times specified, unless already Issued in Burlington, Massachusetts, on
done. October 7, 2016. the need for this amendment involve
(1) Within 12 months or 100 flight hours Colleen M. D’Alessandro, matters of flight safety and operational
after the effective date of the AD, whichever Manager, Engine & Propeller Directorate, efficiency in the National Airspace
occurs first, replace the oil cooler cross Aircraft Certification Service. System, are related to published
fitting, nipple, and bushing. Use the Action [FR Doc. 2016–24794 Filed 10–13–16; 8:45 am] aeronautical charts that are essential to
Required paragraphs III.1 through III.8 of CMI the user, and provide for the safe and
BILLING CODE 4910–13–P
Critical Service Bulletin (CSB) CSB15–2, efficient use of the navigable airspace.
Revision C, dated November 9, 2015 (also In addition, those various reasons or
referred to as CMI CSB CSB15–2C, dated circumstances require making this
November 9, 2015), or the Action Required DEPARTMENT OF TRANSPORTATION
paragraphs III.1 through III.8 of CMI CSB
amendment effective before the next
CSB15–7, Revision B, dated April 26, 2016 Federal Aviation Administration scheduled charting and publication date
(also referred to as CMI CSB15–7B, dated of the flight information to assure its
April 26, 2016), to perform the replacement. 14 CFR Part 95 timely availability to the user. The
(2) Reserved. effective date of this amendment reflects
[Docket No. 31102; Amdt. No. 529] those considerations. In view of the
(f) Credit for Previous Actions
close and immediate relationship
ehiers on DSK5VPTVN1PROD with RULES
You may take credit for the replacement IFR Altitudes; Miscellaneous between these regulatory changes and
that is required by paragraph (e) of this AD, Amendments
if the replacement was performed before the
safety in air commerce, I find that notice
effective date of this AD using CMI CSB AGENCY: Federal Aviation and public procedure before adopting
CSB15–2B, dated November 6, 2015 or earlier Administration (FAA), DOT. this amendment are impracticable and
versions; or CSB CSB15–7A, dated November contrary to the public interest and that
ACTION: Final rule.
10, 2015 or earlier version. good cause exists for making the
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Document Created: 2016-10-14 00:00:53
Document Modified: 2016-10-14 00:00:53
| 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. | |
| Dates | This AD is effective November 18, 2016. | |
| Contact | Scott Hopper, Aerospace Engineer, Atlanta Aircraft Certification Office, FAA, Small Airplane Directorate, 1701 Columbia Avenue, College Park, GA 30337; phone: 404-474-5535; fax: 404-474-5606; email: [email protected] | |
| FR Citation | 81 FR 70929 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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