82 FR 26982 - Airworthiness Directives; Lycoming Engines Reciprocating Engines
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 82, Issue 112 (June 13, 2017)
Federal Aviation Administration
Federal Register Volume 82, Issue 112 (June 13, 2017)
| Page Range | 26982-26985 | |
| FR Document | 2017-12075 |
[Federal Register Volume 82, Number 112 (Tuesday, June 13, 2017)] [Rules and Regulations] [Pages 26982-26985] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2017-12075] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2016-9512; Directorate Identifier 2016-NE-27-AD; Amendment 39-18909; AD 2017-11-10] RIN 2120-AA64 Airworthiness Directives; Lycoming Engines Reciprocating Engines AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule; request for comments. ----------------------------------------------------------------------- SUMMARY: We are adopting a new airworthiness directive (AD) for all Lycoming TIO-540-AJ1A reciprocating engines. This AD requires initial and repetitive inspections of engine exhaust system weld joints and torque checking the exhaust pipe flange mounting nuts. This AD was prompted by several reports of engine exhaust leaks. We are [[Page 26983]] issuing this AD to correct the unsafe condition on these products. DATES: This AD is effective June 28, 2017. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of June 28, 2017. We must receive comments on this AD by July 28, 2017. ADDRESSES: You may send comments, using the procedures found in 14 CFR 11.43 and 11.45, by any of the following methods:Federal eRulemaking Portal: Go to http://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. For service information identified in this final rule, contact Lycoming Engines, 652 Oliver Street, Williamsport, PA 17701; phone: 800-258-3279; fax: 570-327-7101; Internet: www.lycoming.com/Lycoming/SUPPORT/TechnicalPublications/ServiceBulletins.aspx. 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. It is also available on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2016-9512. 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- 9512; 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 (phone: 800-647-5527) is in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt. FOR FURTHER INFORMATION CONTACT: Norman Perenson, Aerospace Engineer, New York Aircraft Certification Office, FAA, Engine & Propeller Directorate, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: 516-228-7337; fax: 516-794-5531; email: [email protected]. SUPPLEMENTARY INFORMATION: Discussion We received several reports of cracked engine exhaust pipes and exhaust studs pulling out from cylinders on Lycoming TIO-540-AJ1A reciprocating engines. This AD requires initial and repetitive inspections of all engine exhaust system weld joints and torque checking the exhaust pipe flange mounting nuts. We are issuing this AD to prevent engine exhaust leaks, which could lead to uncontrolled engine fire, harmful exhaust gases entering the cabin resulting in crew incapacitation, and damage to the airplane. Related Service Information Under 1 CFR Part 51 We reviewed Lycoming Engines Mandatory Service Bulletin (MSB) No. 627C, dated November 17, 2016. The MSB describes procedures for exhaust system inspection and flange nut torque check. 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. Other Related Service Information We reviewed Lycoming Engines MSB No. 614A, dated October 10, 2014, which provides maintenance instructions on the exhaust system for certain Lycoming engines. The FAA issued AD 2015-10-06, Amendment 39- 18162 (80 FR 30345, May 28, 2015), (``AD 2015-10-06'') that mandates replacement of the turbocharger mounting bracket and inspection of the exhaust pipes in accordance with Lycoming Engines MSB No. 614A, dated October 10, 2014. The requirements in this AD are in addition to the requirements of AD 2015-10-06. Complying with AD 2015-10-06 and Lycoming Engines MSB No. 614A, dated October 10, 2014, does not constitute compliance with this AD. FAA's Determination We are issuing this AD because we evaluated all the relevant information and determined the unsafe condition described previously is likely to exist or develop in other products of the same type design. AD Requirements This AD requires initial and repetitive inspections of all engine exhaust system weld joints and torque checking the exhaust pipe flange mounting nuts. Differences Between This AD and the Service Information Table 1 of Lycoming Engines MSB No. 627C, dated November 17, 2016, provides a longer time between inspections of the engine exhaust system when an operational carbon monoxide detector is installed in the airplane. This AD does not consider whether an operational carbon monoxide detector is installed in the airplane. Interim Action We consider this AD interim action. Lycoming is determining the root cause for the unsafe condition identified in this AD. Once a root cause is determined, we will consider additional rulemaking. FAA's Justification and Determination of the Effective Date An unsafe condition exists 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 engine exhaust leaks could lead to uncontrolled engine fire, harmful exhaust gases entering the cabin resulting in crew incapacitation, and damage to the airplane. Therefore, we find that notice and opportunity for prior public comment are impracticable and that good cause exists for making this amendment effective in less than 30 days. Comments Invited This AD is a final rule that involves requirements affecting flight safety and was not preceded by notice and an opportunity for public comment. However, we invite you to send any written data, views, or arguments about this AD. Send your comments to an address listed under the ADDRESSES section. Include the docket number FAA-2016-9512 and Directorate Identifier 2016-NE-27-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 http://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. [[Page 26984]] Costs of Compliance We estimate that this AD affects 758 engines, installed on airplanes of U.S. registry. We estimate the following costs to comply with this AD: Estimated Costs ---------------------------------------------------------------------------------------------------------------- Cost per Action Labor cost Parts cost product Cost on U.S. operators ---------------------------------------------------------------------------------------------------------------- Inspection and torque check......... 1 work-hour x $85 per hour $0.00 $85.00 $64,430.00 per = $85 per inspection cycle. inspection cycle. ---------------------------------------------------------------------------------------------------------------- Paperwork Reduction Act A federal agency may not conduct or sponsor, and a person is not required to respond to, nor shall a person be subject to penalty for failure to comply with a collection of information subject to the requirements of the Paperwork Reduction Act unless that collection of information displays a current valid OMB control number. The control number for the collection of information required by this AD is 2120- 0056. The paperwork cost associated with this AD has been detailed in the Costs of Compliance section of this document and includes time for reviewing instructions, as well as completing and reviewing the collection of information. Therefore, all reporting associated with this AD is mandatory. Comments concerning the accuracy of this burden and suggestions for reducing the burden should be directed to the FAA at 800 Independence Ave. SW., Washington, DC 20591. ATTN: Information Collection Clearance Officer, AES-200. 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, 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 adding the following new airworthiness directive (AD): 2017-11-10 Lycoming Engines Reciprocating Engines (Type Certificate previously held by Textron Lycoming Division, AVCO Corporation): Amendment 39-18909; Docket No. FAA-2016-9512; Directorate Identifier 2016-NE-27-AD. (a) Effective Date This AD is effective June 28, 2017. (b) Affected ADs None. (c) Applicability This AD applies to all Lycoming TIO-540-AJ1A reciprocating engines. (d) Subject Joint Aircraft System Component (JASC) Code 7800, Engine Exhaust System. (e) Unsafe Condition This AD was prompted by several reports of engine exhaust leaks. We are issuing this AD to prevent engine exhaust leaks, which could lead to uncontrolled engine fire, harmful exhaust gases entering the cabin resulting in crew incapacitation, and damage to the airplane. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Required Actions (1) For all engines, perform an initial exhaust system inspection within 10 hours time in service (TIS) after the effective date of this AD as follows: (i) Use the Required Action, paragraph 1. of Lycoming Engines Mandatory Service Bulletin (MSB) No. 627C, dated November 17, 2016, to do the inspection. (ii) For any part that fails the inspection required by paragraph (g)(1)(i) of this AD, before further flight, replace the failed part with a part eligible for installation. (iii) Use the Required Action, paragraph 3. of Lycoming MSB No. 627C, dated November 17, 2016, to submit a survey to Lycoming Engines within 10 days of performing the inspection. (2) For all engines, perform an initial torque check of the exhaust system flange nuts within 10 hours TIS after the effective date of this AD, or within 100 hours TIS after the last exhaust system maintenance (ESM), whichever occurs later, as follows: (i) Use the Required Action, paragraph 2. of Lycoming Engines MSB No. 627C, dated November 17, 2016 to torque check the flange nuts. (ii) For any part that fails the check required by paragraph (g)(2)(i) of this AD, before further flight, replace the failed part with a part eligible for installation. (iii) Use the Required Action, paragraph 3. of Lycoming MSB No. 627C, dated November 17, 2016, to submit a survey to Lycoming Engines within 10 days of performing the check. (3) For all engines with 1,000 hours TIS or less since the last ESM: [[Page 26985]] (i) Repeat the actions required by paragraphs (g)(1)(i) through (iii) of this AD inclusive, every 25 hours TIS since the last ESM, or exhaust system inspection, whichever occurs later. (ii) Repeat the actions required by paragraphs (g)(2)(i) through (iii) of this AD inclusive, every 100 hours TIS after the last ESM, or torque check of the exhaust system flange nuts, whichever occurs later. (4) For all engines with more than 1,000 hours TIS since the last ESM: (i) Repeat the actions required by paragraphs (g)(1)(i) through (iii) of this AD inclusive, every 50 hours TIS since the last ESM, or exhaust system inspection, whichever occurs later. (ii) Repeat the actions required by paragraphs (g)(2)(i) through (iii) of this AD inclusive, every 100 hours TIS since the last ESM, or torque check of the exhaust system flange nuts, whichever occurs later. (h) Definitions For the purposes of this AD, ESM is any maintenance that requires the removal and replacement of any exhaust system pipe or turbocharger mounting bracket, or the re-torqueing of the exhaust flange mounting nuts. (i) Terminating Action The requirement in Required Action paragraph 3., to submit a survey to Lycoming Engines ends one year after the effective date of this AD, but, the exhaust system inspections in Required Actions paragraph 1., and torque checks of the exhaust system flange nuts, in Required Actions paragraph 2., are still required. (j) Paperwork Reduction Act Burden Statement A federal agency may not conduct or sponsor, and a person is not required to respond to, nor shall a person be subject to a penalty for failure to comply with a collection of information subject to the requirements of the Paperwork Reduction Act unless that collection of information displays a current valid OMB Control Number. The OMB Control Number for this information collection is 2120-0056. Public reporting for this collection of information is estimated to be approximately 5 minutes per response, including the time for reviewing instructions, completing and reviewing the collection of information. All responses to this collection of information are mandatory. Comments concerning the accuracy of this burden and suggestions for reducing the burden should be directed to the FAA at: 800 Independence Ave. SW., Washington, DC 20591, Attn: Information Collection Clearance Officer, AES-200. (k) Alternative Methods of Compliance (AMOCs) The Manager, New York Aircraft Certification Office, FAA, may approve AMOCs for this AD. Use the procedures found in 14 CFR 39.19 to make your request. (l) Related Information (1) For more information about this AD, contact Norman Perenson, Aerospace Engineer, New York Aircraft Certification Office, FAA, Engine & Propeller Directorate, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: 516-228-7337; fax: 516-794-5531; email: [email protected]. (2) Lycoming Engines MSB No. 614A, dated October 10, 2014, which is not incorporated by reference in this AD, can be obtained from Lycoming Engines using the contact information in paragraph (m)(3) of this AD. (m) 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) Lycoming Engines Mandatory Service Bulletin No. 627C, dated November 17, 2016. (ii) Reserved. (3) For Lycoming Engines service information identified in this AD, contact Lycoming Engines, 652 Oliver Street, Williamsport, PA 17701; phone: 800-258-3279; fax: 570-327-7101; Internet: www.lycoming.com/Lycoming/SUPPORT/TechnicalPublications/ServiceBulletins.aspx. (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 May 24, 2017. Carlos A. Pestana, Acting Assistant Directorate Manager, Engine & Propeller Directorate, Aircraft Certification Service. [FR Doc. 2017-12075 Filed 6-12-17; 8:45 am] BILLING CODE 4910-13-P
![26982 Federal Register / Vol. 82, No. 112 / Tuesday, June 13, 2017 / Rules and Regulations
PART 39—AIRWORTHINESS (4) Use, as applicable, either the 7772; fax: 781–238–7199; email:
DIRECTIVES Accomplishment Instructions, ‘‘For Engines brian.kierstead@faa.gov.
Installed on the Aircraft,’’ paragraphs 3.(I)
(k) Material Incorporated by Reference
through 3.(J), or the Accomplishment
■ 1. The authority citation for part 39 (1) The Director of the Federal Register
Instructions, ‘‘For Engines Removed from the
continues to read as follows: Aircraft,’’ paragraphs 3.(D) through 3.(E), of approved the incorporation by reference
Authority: 49 U.S.C. 106(g), 40113, 44701. PW Alert Service Bulletin (ASB) No. PW2000 (IBR) of the service information listed in this
A72–765, Revision No. 2, dated August 12, paragraph under 5 U.S.C. 552(a) and 1 CFR
§ 39.13 [Amended] 2016 to do the ECI as follows: part 51.
(i) Perform an initial inspection within the (2) You must use this service information
■ 2. The FAA amends § 39.13 by as applicable to do the actions required by
following period, whichever occurs later:
removing Airworthiness Directive (AD) (A) Within 5,500 cycles since new or since this AD, unless the AD specifies otherwise.
2014–05–32, Amendment 39–17804 (79 M-flange replacement, or (i) Pratt & Whitney (PW) Service Bulletin
FR 17856, March 31, 2014), and adding (B) Within 2,500 cycles since last piece- No. PW2000 72–763, Revision No. 1, dated
the following new AD: part FPI inspection, or August 30, 2013.
(C) Within 1,000 cycles from the effective (ii) PW Alert Service Bulletin No. PW2000
2017–11–06 Pratt & Whitney: Amendment A72–765, Revision No. 2, dated August 12,
39–18905; Docket No. FAA–2013–0740; date of this AD.
(ii) If no crack indications are found, re- 2016.
Directorate Identifier 2013–NE–24–AD. (3) For PW service information identified
inspect within 2,500 cycles since last ECI or
(a) Effective Date last piece-part FPI inspection, whichever in this AD, contact Pratt & Whitney,400 Main
occurs later. St., East Hartford, CT 06118; phone: 860–
This AD is effective July 18, 2017.
(iii) If bolthole ID crack indications are 565–0140; fax: 860–565–5442; email:
(b) Affected ADs found, measure the length and determine the HELP24@pw.utc.com.
This AD replaces AD 2014–05–32, re-inspect interval in accordance with: (4) You may view this service information
Amendment 39–17804 (79 FR 17856, March (A) Paragraphs 5.(C) through 5.(D) of PW at the FAA, Engine & Propeller Directorate,
31, 2014). ASB No. PW2000 A72–765, Revision No. 2, 1200 District Avenue, Burlington, MA. For
dated August 12, 2016 ‘‘For Engines Installed information on the availability of this
(c) Applicability on the Aircraft’’; or material at the FAA, call 781–238–7125.
This AD applies to all Pratt & Whitney (B) Paragraphs 4.(C) through 4.(D) of PW (5) You may view this service information
(PW) PW2037, PW2037D, PW2037M, ASB No. PW2000 A72–765, Revision No. 2, at the National Archives and Records
PW2040, PW2040D, PW2043, PW2143, dated August 12, 2016, ‘‘For Engines Administration (NARA). For information on
PW2643, and F117–PW–100 turbofan Removed from the Aircraft.’’ the availability of this material at NARA, call
engines. (iv) Remove from service diffuser cases 202–741–6030, or go to: http://
with bolthole ID cracks exceeding 0.170 www.archives.gov/federal-register/cfr/ibr-
(d) Subject locations.html.
inches.
Joint Aircraft System Component (JASC) Issued in Burlington, Massachusetts, on
Code 72, Turbine/Turboprop Engine. (g) Definition
May 17, 2017.
For the purpose of this AD, piece-part
(e) Unsafe Condition Robert J. Ganley,
opportunity is defined as when the part is
This AD was prompted by a rupture of the completely disassembled. Acting Manager, Engine & Propeller
diffuser-to-high-pressure turbine (HPT) case Directorate, Aircraft Certification Service.
flange. We are issuing this AD to prevent (h) Credit for Previous Actions [FR Doc. 2017–12078 Filed 6–12–17; 8:45 am]
failure of the diffuser-to-HPT case flange, (1) You may take credit for the diffuser BILLING CODE 4910–13–P
which could lead to uncontained engine case and HPT case inspections required by
failure and damage to the airplane. paragraphs (f)(1) and (3) of this AD if you
performed: DEPARTMENT OF TRANSPORTATION
(f) Compliance
(i) An ECI of the diffuser case and the HPT
Unless already done, comply with this AD case M-flange using the Accomplishment
within the compliance times specified. Federal Aviation Administration
Instructions of PW SB No. PW2000 72–763,
(1) For diffuser case, part number (P/N) Revision No. 1, dated August 30, 2013, or an
1B7461, serial numbers (S/Ns) DGGUAK1306 earlier version; or 14 CFR Part 39
and DGGUAK1308, and HPT case, P/N (ii) a high sensitivity FPI of the diffuser
1B2440, S/N DKLBCS1032: case and the HPT case at a piece-part [Docket No. FAA–2016–9512; Directorate
(i) Within 100 flight cycles or 30 days after opportunity after January 1, 2010. Identifier 2016–NE–27–AD; Amendment 39–
May 5, 2014, whichever is later, eddy current (2) You may take credit for only the 18909; AD 2017–11–10]
inspect the diffuser case and the HPT case M- diffuser case inspections required by
flange. Use PW Service Bulletin (SB) No. RIN 2120–AA64
paragraphs (f)(1) and (3) of this AD if you
PW2000 72–763, Revision No. 1, dated performed an ECI of the M-flange using the
August 30, 2013, to do the inspection. Accomplishment Instructions of PW SB No.
Airworthiness Directives; Lycoming
(ii) Reserved. PW2000 A72–765, Revision No. 1, dated July Engines Reciprocating Engines
(2) For all diffuser and HPT cases, at the 13, 2016, or an earlier version.
next piece-part opportunity and every piece- AGENCY: Federal Aviation
part opportunity thereafter, perform a high (i) Alternative Methods of Compliance Administration (FAA), DOT.
sensitivity fluorescent-penetrant inspection (AMOCs) ACTION: Final rule; request for
(FPI) of the entire diffuser case rear flange The Manager, Engine Certification Office, comments.
(M-flange) and boltholes, and the entire HPT FAA, may approve AMOCs for this AD. Use
case forward flange (M-flange) and boltholes. the procedures found in 14 CFR 39.19 to SUMMARY: We are adopting a new
(3) For diffuser cases that have not make your request. You may email your airworthiness directive (AD) for all
incorporated PW SB PW2000–72–364 or have request to: ANE-AD-AMOC@faa.gov. Lycoming TIO–540–AJ1A reciprocating
nlaroche on DSK30NT082PROD with RULES
incorporated either PW SB PW2000–72–700 engines. This AD requires initial and
or PW2000 Series Engine Manual, Repair-28, (j) Related Information
Task 72–41–01–300–028 (M-flange For more information about this AD, repetitive inspections of engine exhaust
replacement), perform initial and repetitive contact Brian Kierstead, Aerospace Engineer, system weld joints and torque checking
eddy current inspections (ECIs) of the M- Engine Certification Office, FAA, Engine & the exhaust pipe flange mounting nuts.
flange of the diffuser case in accordance with Propeller Directorate, 1200 District Avenue, This AD was prompted by several
paragraph (f)(4) of this AD. Burlington, MA 01803; phone: 781–238– reports of engine exhaust leaks. We are
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Costs of Compliance We estimate the following costs to
We estimate that this AD affects 758 comply with this AD:
engines, installed on airplanes of U.S.
registry.
ESTIMATED COSTS
Cost per
Action Labor cost Parts cost Cost on U.S. operators
product
Inspection and torque check 1 work-hour × $85 per hour = $85 per inspection cycle .. $0.00 $85.00 $64,430.00 per inspection
cycle.
Paperwork Reduction Act 13132. This AD will not have a (c) Applicability
A federal agency may not conduct or substantial direct effect on the States, on This AD applies to all Lycoming TIO–540–
sponsor, and a person is not required to the relationship between the national AJ1A reciprocating engines.
respond to, nor shall a person be subject government and the States, or on the (d) Subject
to penalty for failure to comply with a distribution of power and
responsibilities among the various Joint Aircraft System Component (JASC)
collection of information subject to the Code 7800, Engine Exhaust System.
requirements of the Paperwork levels of government.
Reduction Act unless that collection of For the reasons discussed above, I (e) Unsafe Condition
information displays a current valid certify that this AD: This AD was prompted by several reports
(1) Is not a ‘‘significant regulatory of engine exhaust leaks. We are issuing this
OMB control number. The control
action’’ under Executive Order 12866, AD to prevent engine exhaust leaks, which
number for the collection of information (2) Is not a ‘‘significant rule’’ under could lead to uncontrolled engine fire,
required by this AD is 2120–0056. The DOT Regulatory Policies and Procedures harmful exhaust gases entering the cabin
paperwork cost associated with this AD (44 FR 11034, February 26, 1979), resulting in crew incapacitation, and damage
has been detailed in the Costs of (3) Will not affect intrastate aviation to the airplane.
Compliance section of this document in Alaska, and (f) Compliance
and includes time for reviewing (4) Will not have a significant
instructions, as well as completing and Comply with this AD within the
economic impact, positive or negative, compliance times specified, unless already
reviewing the collection of information. on a substantial number of small entities done.
Therefore, all reporting associated with under the criteria of the Regulatory
this AD is mandatory. Comments Flexibility Act. (g) Required Actions
concerning the accuracy of this burden (1) For all engines, perform an initial
and suggestions for reducing the burden List of Subjects in 14 CFR Part 39 exhaust system inspection within 10 hours
should be directed to the FAA at 800 Air transportation, Aircraft, Aviation time in service (TIS) after the effective date
Independence Ave. SW., Washington, safety, Incorporation by reference, of this AD as follows:
DC 20591. ATTN: Information Safety. (i) Use the Required Action, paragraph 1.
Collection Clearance Officer, AES–200. of Lycoming Engines Mandatory Service
Adoption of the Amendment Bulletin (MSB) No. 627C, dated November
Authority for This Rulemaking 17, 2016, to do the inspection.
Accordingly, under the authority (ii) For any part that fails the inspection
Title 49 of the United States Code delegated to me by the Administrator, required by paragraph (g)(1)(i) of this AD,
specifies the FAA’s authority to issue the FAA amends 14 CFR part 39 as before further flight, replace the failed part
rules on aviation safety. Subtitle I, follows: with a part eligible for installation.
section 106, describes the authority of (iii) Use the Required Action, paragraph 3.
the FAA Administrator. ‘‘Subtitle VII: PART 39—AIRWORTHINESS of Lycoming MSB No. 627C, dated November
Aviation Programs’’ describes in more DIRECTIVES 17, 2016, to submit a survey to Lycoming
detail the scope of the Agency’s Engines within 10 days of performing the
authority. ■ 1. The authority citation for part 39 inspection.
We are issuing this rulemaking under continues to read as follows: (2) For all engines, perform an initial
torque check of the exhaust system flange
the authority described in Subtitle VII, Authority: 49 U.S.C. 106(g), 40113, 44701.
nuts within 10 hours TIS after the effective
Part A, Subpart III, Section 44701: date of this AD, or within 100 hours TIS after
‘‘General requirements.’’ Under that § 39.13 [Amended]
the last exhaust system maintenance (ESM),
section, Congress charges the FAA with ■ 2. The FAA amends § 39.13 by adding whichever occurs later, as follows:
promoting safe flight of civil aircraft in the following new airworthiness (i) Use the Required Action, paragraph 2.
air commerce by prescribing regulations directive (AD): of Lycoming Engines MSB No. 627C, dated
for practices, methods, and procedures November 17, 2016 to torque check the flange
2017–11–10 Lycoming Engines
the Administrator finds necessary for Reciprocating Engines (Type Certificate nuts.
safety in air commerce. This regulation previously held by Textron Lycoming (ii) For any part that fails the check
is within the scope of that authority Division, AVCO Corporation): required by paragraph (g)(2)(i) of this AD,
Amendment 39–18909; Docket No. before further flight, replace the failed part
because it addresses an unsafe condition with a part eligible for installation.
nlaroche on DSK30NT082PROD with RULES
that is likely to exist or develop on FAA–2016–9512; Directorate Identifier
2016–NE–27–AD. (iii) Use the Required Action, paragraph 3.
products identified in this rulemaking of Lycoming MSB No. 627C, dated November
action. (a) Effective Date 17, 2016, to submit a survey to Lycoming
This AD is effective June 28, 2017. Engines within 10 days of performing the
Regulatory Findings
check.
This AD will not have federalism (b) Affected ADs (3) For all engines with 1,000 hours TIS or
implications under Executive Order None. less since the last ESM:
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![Federal Register / Vol. 82, No. 112 / Tuesday, June 13, 2017 / Rules and Regulations 26985
(i) Repeat the actions required by Office, FAA, Engine & Propeller Directorate, This AD was prompted by analysis and
paragraphs (g)(1)(i) through (iii) of this AD 1600 Stewart Avenue, Suite 410, Westbury, by cracks found in the high-pressure
inclusive, every 25 hours TIS since the last NY 11590; phone: 516–228–7337; fax: 516– turbine (HPT) wheel during an
ESM, or exhaust system inspection, 794–5531; email: Norman.Perenson@faa.gov.
(2) Lycoming Engines MSB No. 614A,
inspection. This AD requires
whichever occurs later.
(ii) Repeat the actions required by dated October 10, 2014, which is not replacement of the affected HPT wheels
paragraphs (g)(2)(i) through (iii) of this AD incorporated by reference in this AD, can be at new, lower life limits. We are issuing
inclusive, every 100 hours TIS after the last obtained from Lycoming Engines using the this AD to correct the unsafe condition
ESM, or torque check of the exhaust system contact information in paragraph (m)(3) of on these products.
flange nuts, whichever occurs later. this AD. DATES: This AD is effective July 18,
(4) For all engines with more than 1,000 2017.
(m) Material Incorporated by Reference
hours TIS since the last ESM: The Director of the Federal Register
(i) Repeat the actions required by (1) The Director of the Federal Register
paragraphs (g)(1)(i) through (iii) of this AD approved the incorporation by reference approved the incorporation by reference
inclusive, every 50 hours TIS since the last (IBR) of the service information listed in this of a certain publication listed in this AD
ESM, or exhaust system inspection, paragraph under 5 U.S.C. 552(a) and 1 CFR as of July 18, 2017.
whichever occurs later. part 51. ADDRESSES: For service information
(ii) Repeat the actions required by (2) You must use this service information identified in this final rule, contact
paragraphs (g)(2)(i) through (iii) of this AD as applicable to do the actions required by
Rolls-Royce Corporation, 450 South
inclusive, every 100 hours TIS since the last this AD, unless the AD specifies otherwise.
(i) Lycoming Engines Mandatory Service Meridian Street, Mail Code NB–01–06,
ESM, or torque check of the exhaust system
flange nuts, whichever occurs later. Bulletin No. 627C, dated November 17, 2016. Indianapolis, IN 46225; phone: 317–
(ii) Reserved. 230–3774; email: indy.pubs.services@
(h) Definitions (3) For Lycoming Engines service rolls-royce.com; Internet: www.rolls-
For the purposes of this AD, ESM is any information identified in this AD, contact royce.com. You may view this service
maintenance that requires the removal and Lycoming Engines, 652 Oliver Street, information at the FAA, Engine &
replacement of any exhaust system pipe or Williamsport, PA 17701; phone: 800–258– Propeller Directorate, 1200 District
turbocharger mounting bracket, or the re- 3279; fax: 570–327–7101; Internet:
Avenue, Burlington, MA. For
torqueing of the exhaust flange mounting www.lycoming.com/Lycoming/SUPPORT/
nuts. TechnicalPublications/ServiceBulletins.aspx. information on the availability of this
(4) You may view this service information material at the FAA, call 781–238–7125.
(i) Terminating Action at FAA, Engine & Propeller Directorate, 1200 It is also available on the Internet at
The requirement in Required Action District Avenue, Burlington, MA. For http://www.regulations.gov by searching
paragraph 3., to submit a survey to Lycoming information on the availability of this for and locating Docket No. FAA–2016–
Engines ends one year after the effective date material at the FAA, call 781–238–7125. 9553.
of this AD, but, the exhaust system (5) You may view this service information
inspections in Required Actions paragraph at the National Archives and Records Examining the AD Docket
1., and torque checks of the exhaust system Administration (NARA). For information on You may examine the AD docket on
flange nuts, in Required Actions paragraph the availability of this material at NARA, call
2., are still required. the Internet at http://
202–741–6030, or go to: http://
www.archives.gov/federal-register/cfr/ibr-
www.regulations.gov by searching for
(j) Paperwork Reduction Act Burden and locating Docket No. FAA–2016–
Statement locations.html.
9553; or in person at the Docket
A federal agency may not conduct or Issued in Burlington, Massachusetts, on Management Facility between 9 a.m.
sponsor, and a person is not required to May 24, 2017.
and 5 p.m., Monday through Friday,
respond to, nor shall a person be subject to Carlos A. Pestana, except Federal holidays. The AD docket
a penalty for failure to comply with a Acting Assistant Directorate Manager, Engine
collection of information subject to the contains this AD, the regulatory
& Propeller Directorate, Aircraft Certification evaluation, any comments received, and
requirements of the Paperwork Reduction Service.
Act unless that collection of information other information. The address for the
[FR Doc. 2017–12075 Filed 6–12–17; 8:45 am]
displays a current valid OMB Control Docket Office (phone: 800–647–5527) is
Number. The OMB Control Number for this BILLING CODE 4910–13–P Document Management Facility, U.S.
information collection is 2120–0056. Public Department of Transportation, Docket
reporting for this collection of information is Operations, M–30, West Building
estimated to be approximately 5 minutes per DEPARTMENT OF TRANSPORTATION Ground Floor, Room W12–140, 1200
response, including the time for reviewing
instructions, completing and reviewing the Federal Aviation Administration New Jersey Avenue SE., Washington,
collection of information. All responses to DC 20590.
this collection of information are mandatory. 14 CFR Part 39 FOR FURTHER INFORMATION CONTACT: Kyri
Comments concerning the accuracy of this Zaroyiannis, Aerospace Engineer,
burden and suggestions for reducing the [Docket No. FAA–2016–9553; Directorate Chicago Aircraft Certification Office,
burden should be directed to the FAA at: 800 Identifier 2016–NE–29–AD; Amendment 39–
Small Airplane Directorate, FAA, 2300
Independence Ave. SW., Washington, DC 18904; AD 2017–11–05]
E. Devon Ave., Des Plaines, IL 60018;
20591, Attn: Information Collection
Clearance Officer, AES–200.
RIN 2120–AA64 phone: 847–294–7836; fax: 847–294–
7834; email: kyri.zaroyiannis@faa.gov.
(k) Alternative Methods of Compliance Airworthiness Directives; Rolls-Royce SUPPLEMENTARY INFORMATION:
(AMOCs) Corporation Turbofan Engines
The Manager, New York Aircraft Discussion
AGENCY: Federal Aviation
Certification Office, FAA, may approve We issued a notice of proposed
nlaroche on DSK30NT082PROD with RULES
AMOCs for this AD. Use the procedures
Administration (FAA), DOT.
ACTION: Final rule. rulemaking (NPRM) to amend 14 CFR
found in 14 CFR 39.19 to make your request.
part 39 by adding an AD that would
(l) Related Information SUMMARY: We are adopting a new apply to certain RRC AE 3007C and
(1) For more information about this AD, airworthiness directive (AD) for certain 3007C1 model turbofan engines. The
contact Norman Perenson, Aerospace Rolls-Royce Corporation (RRC) AE NPRM published in the Federal
Engineer, New York Aircraft Certification 3007C and 3007C1 turbofan engines. Register on February 22, 2017 (82 FR
VerDate Sep<11>2014 14:51 Jun 12, 2017 Jkt 241001 PO 00000 Frm 00007 Fmt 4700 Sfmt 4700 E:\FR\FM\13JNR1.SGM 13JNR1](https://thefederalregister.org/doc/82_FR_27094/page/4.svg)
Document Created: 2017-06-13 00:21:52
Document Modified: 2017-06-13 00:21:52
| 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; request for comments. | |
| Dates | This AD is effective June 28, 2017. | |
| Contact | Norman Perenson, Aerospace Engineer, New York Aircraft Certification Office, FAA, Engine & Propeller Directorate, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: 516-228-7337; fax: 516-794-5531; email: [email protected] | |
| FR Citation | 82 FR 26982 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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