81 FR 12834 - Airworthiness Directives; Turbomeca S.A. Turboshaft Engines
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 81, Issue 48 (March 11, 2016)
Federal Aviation Administration
Federal Register Volume 81, Issue 48 (March 11, 2016)
| Page Range | 12834-12836 | |
| FR Document | 2016-05465 |
[Federal Register Volume 81, Number 48 (Friday, March 11, 2016)] [Proposed Rules] [Pages 12834-12836] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2016-05465] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2015-8257; Directorate Identifier 2015-NE-36-AD] RIN 2120-AA64 Airworthiness Directives; Turbomeca S.A. Turboshaft Engines AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM). ----------------------------------------------------------------------- SUMMARY: We propose to adopt a new airworthiness directive (AD) for all Turbomeca S.A. MAKILA 2A and MAKILA 2A1 turboshaft engines. This proposed AD was prompted by two occurrences of crack initiation on a ferrule of the diffuser. This proposed AD would require repetitive diffuser inspections and replacement of those diffusers that fail inspection. We are proposing this AD to prevent rupture of the ferrule of the diffuser, which could result in engine fire and damage to the helicopter. DATES: We must receive comments on this proposed AD by May 10, 2016. ADDRESSES: You may send comments by any of the following methods:Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments. Mail: Docket Management Facility, U.S. Department of Transportation, 1200 New Jersey Avenue SE., West Building [[Page 12835]] Ground Floor, Room W12-140, Washington, DC 20590-0001. Hand Delivery: Deliver to Mail address above between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. Fax: 202-493-2251. For service information identified in this proposed AD, contact Turbomeca S.A., 40220 Tarnos, France; phone: (33) 05 59 74 40 00; fax: (33) 05 59 74 45 15. You may view this service information at the FAA, Engine & Propeller Directorate, 1200 District Avenue, Burlington, MA 01803. 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-2015- 8257; or in person at the Docket Operations office between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this proposed AD, the mandatory continuing airworthiness information (MCAI), the regulatory evaluation, any comments received, and other information. The 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: Brian Kierstead, Aerospace Engineer, Engine Certification Office, FAA, Engine & Propeller Directorate, 1200 District Avenue, Burlington, MA 01803; email: [email protected]; phone: 781-238-7772; fax: 781-238-7199. SUPPLEMENTARY INFORMATION: Comments Invited We invite you to send any written relevant data, views, or arguments about this proposed AD. Send your comments to an address listed under the ADDRESSES section. Include ``Docket No. FAA-2015-8257; Directorate Identifier 2015-NE-36-AD'' at the beginning of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of this proposed AD. We will consider all comments received by the closing date and may amend this proposed AD based on 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 with FAA personnel concerning this proposed AD. Discussion The European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Community, has issued EASA AD 2015-0209, dated October 16, 2015 (referred to hereinafter as ``the MCAI''), to correct an unsafe condition for the specified products. The MCAI states: Two occurrences of crack initiation were reported on a ferrule of diffuser part number (P/N) 0298210100, which propagated and led to the ferrule rupture. The investigation shows in both cases that the ruptured ferrule contacted and punctured the main fuel supply line, resulting in a fuel leak. This condition, if not detected and corrected, could lead to an engine fire, consequently triggering an uncommanded engine in flight shut down, possibly resulting in an emergency landing. Prompted by these occurrences, Turbomeca published Mandatory Service Bulletin (MSB) No. 298 72 2832 to provide repetitive inspection instructions. This proposed AD would require repetitive inspections of the affected diffuser and removal of those diffusers that fail the required inspection. You may obtain further information by examining the MCAI in the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2015-8257. Related Service Information Under 1 CFR Part 51 Turbomeca S.A. has issued Alert Mandatory Service Bulletin (MSB) No. A298 72 2832, Version B, dated October 12, 2015. The Alert MSB describes procedures for repetitive inspections of the affected diffuser and depending on findings, accomplishment of the corrective action(s). Turbomeca S.A. has issued Service Bulletin (SB) No. 298 72 2833, Version A, dated July 29, 2015. The SB identifies post-TU52 HP gas generator modules that have been released with a new ferrule after repair or overhaul in a Repair Center. When applying Alert Mandatory Service Bulletin (MSB) No. A298 72 2832, it is necessary to know if an HP gas generator module released by a Repair Center is equipped with a new ferrule. 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 of this NPRM. FAA's Determination and Requirements of This Proposed AD This product has been approved by the aviation authority of France, and is approved for operation in the United States. Pursuant to our bilateral agreement with the European Community, EASA has notified us of the unsafe condition described in the MCAI and service information referenced above. We are proposing this AD because we evaluated all information provided by EASA and determined the unsafe condition exists and is likely to exist or develop on other products of the same type design. This proposed AD would require repetitive inspections of the affected diffuser and depending on findings, accomplishment of the corrective action(s). Costs of Compliance We estimate that this proposed AD affects 10 engines installed on helicopters of U.S. registry. We also estimate that it would take about 2 hours per engine to comply with this proposed AD. The average labor rate is $85 per hour. Based on these figures, we estimate the cost of this proposed AD on U.S. operators to be $1,700. Authority for This Rulemaking Title 49 of the United States Code specifies the FAA's authority to issue rules on aviation safety. Subtitle I, section 106, describes the authority of the FAA Administrator. ``Subtitle VII: Aviation Programs,'' describes in more detail the scope of the Agency's authority. We are issuing this rulemaking under the authority described in ``Subtitle VII, Part A, Subpart III, Section 44701: General requirements.'' Under that section, Congress charges the FAA with promoting safe flight of civil aircraft in air commerce by prescribing regulations for practices, methods, and procedures the Administrator finds necessary for safety in air commerce. This regulation is within the scope of that authority because it addresses an unsafe condition that is likely to exist or develop on products identified in this rulemaking action. Regulatory Findings We determined that this proposed AD would not have federalism implications under Executive Order 13132. This proposed AD would not have a substantial direct effect on the States, on the relationship between the national Government and the States, or on the distribution of power and responsibilities among the various levels of government. For the reasons discussed above, I certify this proposed regulation: (1) Is not a ``significant regulatory action'' under Executive Order 12866, [[Page 12836]] (2) Is not a ``significant rule'' under the DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979), (3) Will not affect intrastate aviation in Alaska 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. The Proposed Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA proposes to amend 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): Turbomeca S.A.: Docket No. FAA-2015-8257; Directorate Identifier 2015-NE-36-AD. (a) Comments Due Date We must receive comments by May 10, 2016. (b) Affected ADs None. (c) Applicability This AD applies to Turbomeca S.A. MAKILA 2A and MAKILA 2A1 turboshaft engine models with a high-pressure (HP) gas generator module (M03) that has modification (mod) TU 52 installed. (d) Reason This AD was prompted by two occurrences of crack initiation on a ferrule of the diffuser, which propagated and led to the ferrule rupture. We are issuing this AD to prevent rupture of the ferrule of the diffuser, which could result in engine fire and damage to the helicopter. (e) Actions and Compliance Comply with this AD within the compliance times specified, unless already done. (1) Borescope inspect the centrifugal diffuser ferrule, part number (P/N) 0298210100, prior to the ferrule accumulating 700 hours, time since new or time since replacement or within 30 hours from the effective date of this AD, whichever is later. Use Accomplishment Instructions, paragraphs 2.4.1 through 2.4.2.2.1, of Turbomeca S.A. Alert Mandatory Service Bulletin (MSB) No. 298 72 2832, Version B, dated October 12, 2015, to do the borescope inspections required by this AD. (2) Repeat the borescope inspection required by this AD every 50 hours since last inspection. (3) If any crack, loss of contact between the ferrule and diffuser axial vane, or any contact between the injection manifold supply pipe and the diffuser ferrule is found, remove the diffuser case and replace the ferrule with a part eligible for installation. (f) Credit for Previous Actions You may take credit for the actions required by paragraph (e) of this AD if you performed Turbomeca S.A. MSB No. 298 72 2832, Version A, dated September 3, 2015 before the effective date of this AD. (g) Alternative Methods of Compliance (AMOCs) The Manager, Engine Certification Office, FAA, may approve AMOCs for this AD. Use the procedures found in 14 CFR 39.19 to make your request. You may email your request to: [email protected]. (h) Related Information (1) For more information about this AD, contact Brian Kierstead, Aerospace Engineer, Engine Certification Office, FAA, Engine & Propeller Directorate, 1200 District Avenue, Burlington, MA 01803; phone: 781-238-7772; fax: 781-238-7199; email: [email protected]. (2) Refer to MCAI European Aviation Safety Agency AD 2015-0209, dated October 16, 2015, for more information. You may examine the MCAI in the AD docket on the Internet at http://www.regulations.gov by searching for and locating it in Docket No. FAA-2015-8257. (3) Turbomeca S.A. Alert MSB No. A298 72 2832, Version B, dated October 12, 2015, can be obtained from Turbomeca S.A., using the contact information in paragraph (h)(5) of this proposed AD. (4) Turbomeca S.A. Service Bulletin (SB) No. 298 72 2833, Version A, dated July 29, 2015, can be obtained from Turbomeca S.A., using the contact information in paragraph (h)(5) of this proposed AD. (5) For service information identified in this proposed AD, contact Turbomeca S.A., 40220 Tarnos, France; phone: (33) 05 59 74 40 00; fax: (33) 05 59 74 45 15. (6) You may view this service information at the FAA, Engine & Propeller Directorate, 1200 District Avenue, Burlington, MA 01803. For information on the availability of this material at the FAA, call 781-238-7125. Issued in Burlington, Massachusetts, on February 29, 2016. Colleen M. D'Alessandro, Manager, Engine & Propeller Directorate, Aircraft Certification Service. [FR Doc. 2016-05465 Filed 3-10-16; 8:45 am] BILLING CODE 4910-13-P
![12834 Federal Register / Vol. 81, No. 48 / Friday, March 11, 2016 / Proposed Rules
hour. Parts would cost about $0 per PART 39—AIRWORTHINESS Atlanta Aircraft Certification Office, FAA,
engine. Based on these figures, we DIRECTIVES 1701 Columbia Avenue, College Park, GA
estimate the total cost of this proposed 30337; phone: 404–474–5535; fax: 404–474–
■ 1. The authority citation for part 39 5606; email: scott.hopper@faa.gov.
AD to U.S. operators to be $111,095.
continues to read as follows: (2) CMI CSB No. CSB15–7A, dated
Our cost estimate is exclusive of November 10, 2015 and CMI CSB No.
possible warranty coverage. Authority: 49 U.S.C. 106(g), 40113, 44701. CSB15–2C, dated November 9, 2015 can be
Authority for This Rulemaking obtained from CMI using the contact
§ 39.13 [Amended]
information in paragraph (h)(3) of this AD.
Title 49 of the United States Code ■ 2. The FAA amends § 39.13 by adding (3) For service information identified in
specifies the FAA’s authority to issue the following new airworthiness this AD, contact Continental Motors, Inc.,
rules on aviation safety. Subtitle I, directive (AD): 2039 Broad Street, Mobile, Alabama 36615;
section 106, describes the authority of Continental Motors, Inc. (Type Certificate phone: 800–326–0089; Internet: http://
the FAA Administrator. Subtitle VII: previously held by Teledyne Continental www.continentalmotors.aero.
Aviation Programs, describes in more Motors) Reciprocating Engines: Docket (4) You may view this service information
No. FAA–2016–0069; Directorate at the FAA, Engine & Propeller Directorate,
detail the scope of the Agency’s 1200 District Avenue, Burlington, MA. For
authority. Identifier 2016–NE–01–AD.
information on the availability of this
We are issuing this rulemaking under (a) Comments Due Date material at the FAA, call 781–238–7125.
the authority described in Subtitle VII, We must receive comments by May 10, Issued in Burlington, Massachusetts, on
Part A, Subpart III, Section 44701: 2016. March 2, 2016.
‘‘General requirements.’’ Under that
(b) Affected ADs Colleen M. D’Alessandro,
section, Congress charges the FAA with
promoting safe flight of civil aircraft in None. Manager, Engine & Propeller Directorate,
Aircraft Certification Service.
air commerce by prescribing regulations (c) Applicability
for practices, methods, and procedures [FR Doc. 2016–05467 Filed 3–10–16; 8:45 am]
This AD applies to Continental Motors,
the Administrator finds necessary for Inc. (CMI) TSIO–550–K, TSIOF–550–K,
BILLING CODE 4910–13–P
safety in air commerce. This regulation TSIO–550–C, TSIOF–550–D, and TSIO–550–
is within the scope of that authority N reciprocating engines with an engine serial
because it addresses an unsafe condition number below 1012296 and an oil cooler DEPARTMENT OF TRANSPORTATION
that is likely to exist or develop on cross fitting, part number AN918–1J,
installed. Federal Aviation Administration
products identified in this rulemaking
action. (d) Unsafe Condition 14 CFR Part 39
Regulatory Findings This AD was prompted by a report of an
uncommanded in-flight shutdown (IFSD) [Docket No. FAA–2015–8257; Directorate
We determined that this proposed AD resulting in injuries and significant airplane Identifier 2015–NE–36–AD]
would not have federalism implications damage. We are issuing this AD to prevent
under Executive Order 13132. This failure of the oil cooler cross fitting and RIN 2120–AA64
proposed AD would not have a engine, IFSD and loss of the airplane.
substantial direct effect on the States, on Airworthiness Directives; Turbomeca
(e) Compliance S.A. Turboshaft Engines
the relationship between the national Comply with this AD within the
Government and the States, or on the compliance times specified, unless already AGENCY: Federal Aviation
distribution of power and done. Administration (FAA), DOT.
responsibilities among the various (1) Within 12 months or 100 flight hours ACTION: Notice of proposed rulemaking
levels of government. from the effective date of the AD, whichever
(NPRM).
For the reasons discussed above, I occurs first, replace the oil cooler cross
certify this proposed regulation: fitting, nipple, and bushing. Use the Action SUMMARY: We propose to adopt a new
(1) Is not a ‘‘significant regulatory Required paragraphs III.1 through III.8 of CMI
Critical Service Bulletin (CSB) No. CSB15–
airworthiness directive (AD) for all
action’’ under Executive Order 12866, Turbomeca S.A. MAKILA 2A and
7A, dated November 10, 2015 or the Action
(2) Is not a ‘‘significant rule’’ under Required paragraphs III.1 through III.8 of CMI MAKILA 2A1 turboshaft engines. This
the DOT Regulatory Policies and CSB No. CSB15–2C, dated November 9, 2015, proposed AD was prompted by two
Procedures (44 FR 11034, February 26, to perform the replacement. occurrences of crack initiation on a
1979), (2) Reserved. ferrule of the diffuser. This proposed
(3) Will not affect intrastate aviation AD would require repetitive diffuser
(f) Credit for Previous Actions
in Alaska, and inspections and replacement of those
(4) Will not have a significant You may take credit for the replacement
that is required by paragraph (e) of this AD, diffusers that fail inspection. We are
economic impact, positive or negative, proposing this AD to prevent rupture of
if the replacement was performed before the
on a substantial number of small entities effective date of this AD using CMI CSB No. the ferrule of the diffuser, which could
under the criteria of the Regulatory CSB15–2B, dated November 6, 2015 or earlier result in engine fire and damage to the
Flexibility Act. versions; or CSB No. CSB15–7, dated helicopter.
November 6, 2015.
List of Subjects in 14 CFR Part 39 DATES: We must receive comments on
asabaliauskas on DSK3SPTVN1PROD with PROPOSALS
Air transportation, Aircraft, Aviation (g) Alternative Methods of Compliance this proposed AD by May 10, 2016.
(AMOCs) ADDRESSES: You may send comments by
safety, Incorporation by reference,
Safety. The Manager, Atlanta Certification Office, any of the following methods:
FAA, may approve AMOCs for this AD. Use • Federal eRulemaking Portal: Go to
The Proposed Amendment the procedures found in 14 CFR 39.19 to http://www.regulations.gov. Follow the
make your request.
Accordingly, under the authority instructions for submitting comments.
delegated to me by the Administrator, (h) Related Information • Mail: Docket Management Facility,
the FAA proposes to amend 14 CFR part (1) For more information about this AD, U.S. Department of Transportation, 1200
39 as follows: contact Scott Hopper, Aerospace Engineer, New Jersey Avenue SE., West Building
VerDate Sep<11>2014 16:25 Mar 10, 2016 Jkt 238001 PO 00000 Frm 00003 Fmt 4702 Sfmt 4702 E:\FR\FM\11MRP1.SGM 11MRP1](https://thefederalregister.org/doc/81_FR_12882/page/1.svg)
![12836 Federal Register / Vol. 81, No. 48 / Friday, March 11, 2016 / Proposed Rules
(2) Is not a ‘‘significant rule’’ under paragraphs 2.4.1 through 2.4.2.2.1, of DEPARTMENT OF TRANSPORTATION
the DOT Regulatory Policies and Turbomeca S.A. Alert Mandatory Service
Procedures (44 FR 11034, February 26, Bulletin (MSB) No. 298 72 2832, Version B, Federal Aviation Administration
1979), dated October 12, 2015, to do the borescope
(3) Will not affect intrastate aviation inspections required by this AD. 14 CFR Part 39
in Alaska to the extent that it justifies (2) Repeat the borescope inspection
required by this AD every 50 hours since last [Docket No. FAA–2015–6033; Directorate
making a regulatory distinction, and Identifier 2015–SW–019–AD]
(4) Will not have a significant inspection.
economic impact, positive or negative, (3) If any crack, loss of contact between the RIN 2120–AA64
on a substantial number of small entities ferrule and diffuser axial vane, or any contact
under the criteria of the Regulatory between the injection manifold supply pipe Airworthiness Directives; Airbus
Flexibility Act. and the diffuser ferrule is found, remove the Helicopters
diffuser case and replace the ferrule with a
List of Subjects in 14 CFR Part 39 part eligible for installation. AGENCY: Federal Aviation
Administration (FAA), DOT.
Air transportation, Aircraft, Aviation (f) Credit for Previous Actions
ACTION: Notice of proposed rulemaking
safety, Incorporation by reference, You may take credit for the actions
Safety. (NPRM).
required by paragraph (e) of this AD if you
The Proposed Amendment performed Turbomeca S.A. MSB No. 298 72 SUMMARY: We propose to adopt a new
2832, Version A, dated September 3, 2015 airworthiness directive (AD) for Airbus
Accordingly, under the authority before the effective date of this AD. Helicopters Model AS 365 N3
delegated to me by the Administrator,
(g) Alternative Methods of Compliance
helicopters. This proposed AD would
the FAA proposes to amend 14 CFR part
(AMOCs) require inspecting the cabin and cockpit
39 as follows:
for labels, placards, or markings that
The Manager, Engine Certification Office,
PART 39—AIRWORTHINESS provide jettison procedure instructions
FAA, may approve AMOCs for this AD. Use
DIRECTIVES for cabin doors, removing any labels,
the procedures found in 14 CFR 39.19 to
make your request. You may email your
placards, or markings that are in an
■ 1. The authority citation for part 39 request to: ANE-AD-AMOC@faa.gov. incorrect location, and installing
continues to read as follows: placards where they are missing. This
(h) Related Information proposed AD is prompted by the
Authority: 49 U.S.C. 106(g), 40113, 44701.
(1) For more information about this AD, determination that placards had not
§ 39.13 [Amended] contact Brian Kierstead, Aerospace Engineer, been installed according to
■ 2. The FAA amends § 39.13 by adding Engine Certification Office, FAA, Engine & specifications on newly manufactured
the following new airworthiness Propeller Directorate, 1200 District Avenue, helicopters. The proposed actions are
directive (AD): Burlington, MA 01803; phone: 781–238– intended to provide exit procedures
7772; fax: 781–238–7199; email: during an emergency.
Turbomeca S.A.: Docket No. FAA–2015– brian.kierstead@faa.gov.
8257; Directorate Identifier 2015–NE– DATES: We must receive comments on
(2) Refer to MCAI European Aviation
36–AD. this proposed AD by May 10, 2016.
Safety Agency AD 2015–0209, dated October
(a) Comments Due Date 16, 2015, for more information. You may ADDRESSES: You may send comments by
examine the MCAI in the AD docket on the any of the following methods:
We must receive comments by May 10,
2016. Internet at http://www.regulations.gov by • Federal eRulemaking Docket: Go to
searching for and locating it in Docket No. http://www.regulations.gov. Follow the
(b) Affected ADs FAA–2015–8257. online instructions for sending your
None. (3) Turbomeca S.A. Alert MSB No. A298 72 comments electronically.
(c) Applicability
2832, Version B, dated October 12, 2015, can • Fax: 202–493–2251.
be obtained from Turbomeca S.A., using the • Mail: Send comments to the U.S.
This AD applies to Turbomeca S.A. contact information in paragraph (h)(5) of Department of Transportation, Docket
MAKILA 2A and MAKILA 2A1 turboshaft this proposed AD.
engine models with a high-pressure (HP) gas Operations, M–30, West Building
(4) Turbomeca S.A. Service Bulletin (SB) Ground Floor, Room W12–140, 1200
generator module (M03) that has
No. 298 72 2833, Version A, dated July 29, New Jersey Avenue SE., Washington,
modification (mod) TU 52 installed.
2015, can be obtained from Turbomeca S.A., DC 20590–0001.
(d) Reason using the contact information in paragraph • Hand Delivery: Deliver to the
This AD was prompted by two occurrences (h)(5) of this proposed AD.
‘‘Mail’’ address between 9 a.m. and 5
of crack initiation on a ferrule of the diffuser, (5) For service information identified in
p.m., Monday through Friday, except
which propagated and led to the ferrule this proposed AD, contact Turbomeca S.A.,
40220 Tarnos, France; phone: (33) 05 59 74
Federal holidays.
rupture. We are issuing this AD to prevent
rupture of the ferrule of the diffuser, which 40 00; fax: (33) 05 59 74 45 15. Examining the AD Docket
could result in engine fire and damage to the (6) You may view this service information
helicopter. at the FAA, Engine & Propeller Directorate, You may examine the AD docket on
1200 District Avenue, Burlington, MA 01803. the Internet at http://
(e) Actions and Compliance www.regulations.gov by searching for
asabaliauskas on DSK3SPTVN1PROD with PROPOSALS
For information on the availability of this
Comply with this AD within the material at the FAA, call 781–238–7125. and locating Docket No. FAA–2015–
compliance times specified, unless already 6033; or in person at the Docket
done. Issued in Burlington, Massachusetts, on
Operations Office between 9 a.m. and 5
(1) Borescope inspect the centrifugal February 29, 2016.
p.m., Monday through Friday, except
diffuser ferrule, part number (P/N) Colleen M. D’Alessandro,
0298210100, prior to the ferrule
Federal holidays. The AD docket
Manager, Engine & Propeller Directorate, contains this proposed AD, the
accumulating 700 hours, time since new or
Aircraft Certification Service. European Aviation Safety Agency
time since replacement or within 30 hours
from the effective date of this AD, whichever [FR Doc. 2016–05465 Filed 3–10–16; 8:45 am] (EASA) AD, the economic evaluation,
is later. Use Accomplishment Instructions, BILLING CODE 4910–13–P any comments received, and other
VerDate Sep<11>2014 16:25 Mar 10, 2016 Jkt 238001 PO 00000 Frm 00005 Fmt 4702 Sfmt 4702 E:\FR\FM\11MRP1.SGM 11MRP1](https://thefederalregister.org/doc/81_FR_12882/page/3.svg)
Document Created: 2016-03-11 01:50:38
Document Modified: 2016-03-11 01:50:38
| 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 | Proposed Rules | |
| Action | Notice of proposed rulemaking (NPRM). | |
| Dates | We must receive comments on this proposed AD by May 10, 2016. | |
| Contact | Brian Kierstead, Aerospace Engineer, Engine Certification Office, FAA, Engine & Propeller Directorate, 1200 District Avenue, Burlington, MA 01803; email: [email protected]; phone: 781-238-7772; fax: 781-238-7199. | |
| FR Citation | 81 FR 12834 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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