81 FR 70928 - Airworthiness Directives; Bell Helicopter Textron Helicopters
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 | 70928-70929 | |
| FR Document | 2016-24741 |
[Federal Register Volume 81, Number 199 (Friday, October 14, 2016)] [Rules and Regulations] [Pages 70928-70929] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2016-24741] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2016-6551; Directorate Identifier 2013-SW-070-AD; Amendment 39-18682; AD 2016-21-01] RIN 2120-AA64 Airworthiness Directives; Bell Helicopter Textron Helicopters AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule. ----------------------------------------------------------------------- SUMMARY: We are adopting a new airworthiness directive (AD) for certain Bell Helicopter Textron (Bell) Model 430 helicopters. This AD requires establishing a life limit for a certain main rotor hub attachment bolt (bolt) and removing from service each bolt that has met or exceeded its life limit. This AD was prompted by a documentation error that omitted the life limit of a certain part-numbered bolt from the Airworthiness Limitations section of the maintenance manual. The actions of this AD are intended to establish a life limit for a certain part-numbered bolt to prevent failure of a bolt, failure of a main rotor hub, and subsequent loss of control of a helicopter. DATES: This AD is effective November 18, 2016. ADDRESSES: For service information identified in this final rule, contact Bell Helicopter Textron Canada Limited, 12,800 Rue de l'Avenir, Mirabel, Quebec J7J1R4; telephone (450) 437-2862 or (800) 363-8023; fax (450) 433-0272; or at http://www.bellcustomer.com/files/. You may review the referenced service information at the FAA, Office of the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy, Room 6N-321, Fort Worth, TX 76177. 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- 6551; 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 AD, the Transport Canada AD, the economic evaluation, any comments received, and other information. The street address for the Docket Operations Office (phone: 800-647-5527) is U.S. Department of Transportation, Docket Operations Office, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590. FOR FURTHER INFORMATION CONTACT: Matt Fuller, Senior Aviation Safety Engineer, Safety Management Group, Rotorcraft Directorate, FAA, 10101 Hillwood Pkwy, Fort Worth, TX 76177; telephone (817) 222-5110; email [email protected]. SUPPLEMENTARY INFORMATION: Discussion On May 10, 2016, at 81 FR 28766, the Federal Register published our notice of proposed rulemaking (NPRM), which proposed to amend 14 CFR part 39 by adding an AD that would apply to certain serial-numbered Bell Model 430 helicopters with bolt part number (P/N) MS21250-08083 installed. The NPRM proposed to require, within 10 hours time-in- service (TIS), revising the Airworthiness Limitations section of the applicable maintenance manual or Instructions for Continued Airworthiness (ICA) by establishing a life limit of 5,000 hours TIS for each bolt P/N MS21250-08083, determining the number of hours TIS for each bolt and using the helicopter's hours if the hours TIS of a bolt is unknown, and removing from service each bolt that has reached or exceeded its life limit. The proposed requirements were intended to establish a life limit for the bolt to prevent failure of a bolt, failure of a main rotor hub, and subsequent loss of control of a helicopter. Transport Canada, which is the aviation authority for Canada, has issued Canadian AD No. CF-2013-26, dated September 24, 2013, to correct an unsafe condition for certain serial-numbered Bell Model 430 helicopters. Transport Canada advises that bolt P/N MS21250-08083, which replaced bolt P/N 20-065-08083 in 2009, has a retirement life of 5,000 hours. However, the retirement life for the replacement bolt was inadvertently omitted from the limitations section of the Bell 430 maintenance manual. Transport Canada advises that this situation, if not corrected, could result in failure of a bolt and loss of control of the helicopter. Transport Canada AD No. CF-2013-26 requires reviewing the helicopter records to determine if bolt P/N MS21250-08083 is installed, creating a historical service record, and establishing an airworthiness life of 5,000 hours air time. Comments We gave the public the opportunity to participate in developing this AD, but we did not receive any comments on the NPRM (81 FR 28766, May 10, 2016). FAA's Determination These helicopters have been approved by the aviation authority of Canada and are approved for operation in the United States. Pursuant to our bilateral agreement with Canada, Transport Canada, its technical representative, has notified us of the unsafe condition described in its AD. We are issuing this AD because we evaluated all information provided by Transport Canada and determined the unsafe condition exists and is likely to exist or develop on other helicopters of the same type design and that air safety and the public interest require adopting the AD requirements as proposed. Differences Between This AD and the Transport Canada AD This AD requires compliance within 10 hours TIS, while the Transport Canada AD requires compliance within 60 days. Related Service Information We reviewed Bell Helicopter Alert Service Bulletin 430-12-47, dated November 14, 2012 (ASB). The ASB states that original bolt P/N 20-065- 08083 has a retirement life of 5,000 hours but has been replaced by standard bolt P/N MS21250-08083, which does not have a life limit listed in the maintenance manual. The purpose of the ASB is to establish a life limit of 5,000 hours for the replacement bolt. Bell specifies reviewing the aircraft records back to January 2009 to determine which part-numbered bolts are installed. If a replacement bolt P/N MS21250-08083 is installed, the ASB specifies using data from aircraft records to create a historical service record for the replacement bolts and reflecting the 5,000 hours life limit. The ASB also specifies updating the Bell 430 maintenance manual. [[Page 70929]] Costs of Compliance We estimate that this AD affects 43 helicopters of U.S. Registry. We estimate that operators may incur the following costs to comply with this AD. At an average labor cost of $85 per work-hour, we estimate reviewing and revising the records requires 1 work-hour for a cost of about $85 per helicopter and $3,655 for the U.S. fleet. We estimate replacing a bolt that has exceeded its life limit requires 0.5 work-hour plus $290 for a replacement bolt, for a total cost of $333 per bolt. 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 helicopters 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. We prepared an economic evaluation of the estimated costs to comply with this AD and placed it in the AD docket. 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): 2016-21-01 Bell Helicopter Textron: Amendment 39-18682; Docket No. FAA-2016-6551; Directorate Identifier 2013-SW-070-AD. (a) Applicability This AD applies to Model 430 helicopters, serial number 49001 through 49129, with a main rotor head attachment bolt (bolt) part number (P/N) MS21250-08083 installed, certificated in any category. (b) Unsafe Condition This AD defines the unsafe condition as a bolt remaining in service beyond its fatigue life. This condition could result in failure of a bolt, failure of the main rotor hub and subsequent loss of control of a helicopter. (c) Effective Date This AD becomes effective November 18, 2016. (d) Compliance You are responsible for performing each action required by this AD within the specified compliance time unless it has already been accomplished prior to that time. (e) Required Actions Within 10 hours time-in-service (TIS): (1) Revise the Airworthiness Limitations section of the applicable maintenance manual or Instructions for Continued Airworthiness (ICA) to establish a life limit of 5,000 hours TIS for each bolt P/N MS21250-08083. (2) Determine the number of hours TIS for each bolt and update the helicopter's historical records. If the hours TIS is unknown, calculate the number of hours TIS by counting the helicopter's hours TIS beginning January 1, 2009. (3) Remove from service each bolt that has reached or exceeded its life limit. (f) Alternative Methods of Compliance (AMOCs) (1) The Manager, Safety Management Group, FAA, may approve AMOCs for this AD. Send your proposal to: Matt Fuller, Senior Aviation Safety Engineer, Safety Management Group, Rotorcraft Directorate, FAA, 10101 Hillwood Pkwy, Fort Worth, TX 76177; telephone (817) 222- 5110; email [email protected]. (2) For operations conducted under a 14 CFR part 119 operating certificate or under 14 CFR part 91, subpart K, we suggest that you notify your principal inspector, or lacking a principal inspector, the manager of the local flight standards district office or certificate holding district office, before operating any aircraft complying with this AD through an AMOC. (g) Additional Information (1) Bell Helicopter Alert Service Bulletin 430-12-47, dated November 14, 2012, which is not incorporated by reference, contains additional information about the subject of this final rule. For service information identified in this final rule, contact Bell Helicopter Textron Canada Limited, 12,800 Rue de l'Avenir, Mirabel, Quebec J7J1R4; telephone (450) 437-2862 or (800) 363-8023; fax (450) 433-0272; or at http://www.bellcustomer.com/files/. You may review a copy of the service information at the FAA, Office of the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy, Room 6N-321, Fort Worth, TX 76177. (2) The subject of this AD is addressed in Transport Canada AD No. CF-2013-26, dated September 24, 2013. You may view the Transport Canada AD on the Internet at http://www.regulations.gov in Docket No. FAA-2016-6551. (h) Subject Joint Aircraft Service Component (JASC) Code: 6220 Main Rotor Head. Issued in Fort Worth, Texas, on October 3, 2016. Lance T. Gant, Manager, Rotorcraft Directorate, Aircraft Certification Service. [FR Doc. 2016-24741 Filed 10-13-16; 8:45 am] BILLING CODE 4910-13-P
![70928 Federal Register / Vol. 81, No. 199 / Friday, October 14, 2016 / Rules and Regulations
information on the availability of this Examining the AD Docket maintenance manual. Transport Canada
material at the FAA, call 781–238–7125. advises that this situation, if not
(5) You may view this service information You may examine the AD docket on
the Internet at http:// corrected, could result in failure of a
at the National Archives and Records
Administration (NARA). For information on www.regulations.gov by searching for bolt and loss of control of the helicopter.
the availability of this material at NARA, call and locating Docket No. FAA–2016– Transport Canada AD No. CF–2013–26
202–741–6030, or go to: http:// 6551; or in person at the Docket requires reviewing the helicopter
www.archives.gov/federal-register/cfr/ibr- Operations Office between 9 a.m. and 5 records to determine if bolt P/N
locations.html. p.m., Monday through Friday, except MS21250–08083 is installed, creating a
Issued in Burlington, Massachusetts, on Federal holidays. The AD docket historical service record, and
September 30, 2016. contains this AD, the Transport Canada establishing an airworthiness life of
Colleen M. D’Alessandro, AD, the economic evaluation, any 5,000 hours air time.
Manager, Engine & Propeller Directorate, comments received, and other
information. The street address for the Comments
Aircraft Certification Service.
[FR Doc. 2016–24795 Filed 10–13–16; 8:45 am] Docket Operations Office (phone: 800– We gave the public the opportunity to
BILLING CODE 4910–13–P
647–5527) is U.S. Department of participate in developing this AD, but
Transportation, Docket Operations we did not receive any comments on the
Office, M–30, West Building Ground NPRM (81 FR 28766, May 10, 2016).
DEPARTMENT OF TRANSPORTATION Floor, Room W12–140, 1200 New Jersey
Avenue SE., Washington, DC 20590. FAA’s Determination
Federal Aviation Administration FOR FURTHER INFORMATION CONTACT: Matt
Fuller, Senior Aviation Safety Engineer, These helicopters have been approved
14 CFR Part 39 Safety Management Group, Rotorcraft by the aviation authority of Canada and
Directorate, FAA, 10101 Hillwood are approved for operation in the United
[Docket No. FAA–2016–6551; Directorate Pkwy, Fort Worth, TX 76177; telephone States. Pursuant to our bilateral
Identifier 2013–SW–070–AD; Amendment agreement with Canada, Transport
39–18682; AD 2016–21–01]
(817) 222–5110; email matthew.fuller@
faa.gov. Canada, its technical representative, has
RIN 2120–AA64 notified us of the unsafe condition
SUPPLEMENTARY INFORMATION:
described in its AD. We are issuing this
Airworthiness Directives; Bell Discussion AD because we evaluated all
Helicopter Textron Helicopters On May 10, 2016, at 81 FR 28766, the information provided by Transport
Federal Register published our notice of Canada and determined the unsafe
AGENCY: Federal Aviation condition exists and is likely to exist or
Administration (FAA), DOT. proposed rulemaking (NPRM), which
proposed to amend 14 CFR part 39 by develop on other helicopters of the same
ACTION: Final rule. type design and that air safety and the
adding an AD that would apply to
certain serial-numbered Bell Model 430 public interest require adopting the AD
SUMMARY: We are adopting a new
helicopters with bolt part number (P/N) requirements as proposed.
airworthiness directive (AD) for certain
Bell Helicopter Textron (Bell) Model MS21250–08083 installed. The NPRM Differences Between This AD and the
430 helicopters. This AD requires proposed to require, within 10 hours
Transport Canada AD
establishing a life limit for a certain time-in-service (TIS), revising the
main rotor hub attachment bolt (bolt) Airworthiness Limitations section of the This AD requires compliance within
and removing from service each bolt applicable maintenance manual or 10 hours TIS, while the Transport
that has met or exceeded its life limit. Instructions for Continued Canada AD requires compliance within
This AD was prompted by a Airworthiness (ICA) by establishing a 60 days.
documentation error that omitted the life limit of 5,000 hours TIS for each
bolt P/N MS21250–08083, determining Related Service Information
life limit of a certain part-numbered bolt
from the Airworthiness Limitations the number of hours TIS for each bolt
We reviewed Bell Helicopter Alert
section of the maintenance manual. The and using the helicopter’s hours if the
hours TIS of a bolt is unknown, and Service Bulletin 430–12–47, dated
actions of this AD are intended to November 14, 2012 (ASB). The ASB
establish a life limit for a certain part- removing from service each bolt that has
reached or exceeded its life limit. The states that original bolt P/N 20–065–
numbered bolt to prevent failure of a 08083 has a retirement life of 5,000
bolt, failure of a main rotor hub, and proposed requirements were intended to
establish a life limit for the bolt to hours but has been replaced by standard
subsequent loss of control of a bolt P/N MS21250–08083, which does
helicopter. prevent failure of a bolt, failure of a
main rotor hub, and subsequent loss of not have a life limit listed in the
DATES: This AD is effective November control of a helicopter. maintenance manual. The purpose of
18, 2016. Transport Canada, which is the the ASB is to establish a life limit of
ADDRESSES: For service information aviation authority for Canada, has 5,000 hours for the replacement bolt.
identified in this final rule, contact Bell issued Canadian AD No. CF–2013–26, Bell specifies reviewing the aircraft
Helicopter Textron Canada Limited, dated September 24, 2013, to correct an records back to January 2009 to
12,800 Rue de l’Avenir, Mirabel, Quebec unsafe condition for certain serial- determine which part-numbered bolts
J7J1R4; telephone (450) 437–2862 or numbered Bell Model 430 helicopters. are installed. If a replacement bolt P/N
(800) 363–8023; fax (450) 433–0272; or Transport Canada advises that bolt P/N MS21250–08083 is installed, the ASB
ehiers on DSK5VPTVN1PROD with RULES
at http://www.bellcustomer.com/files/. MS21250–08083, which replaced bolt specifies using data from aircraft records
You may review the referenced service P/N 20–065–08083 in 2009, has a to create a historical service record for
information at the FAA, Office of the retirement life of 5,000 hours. However, the replacement bolts and reflecting the
Regional Counsel, Southwest Region, the retirement life for the replacement 5,000 hours life limit. The ASB also
10101 Hillwood Pkwy, Room 6N–321, bolt was inadvertently omitted from the specifies updating the Bell 430
Fort Worth, TX 76177. limitations section of the Bell 430 maintenance manual.
VerDate Sep<11>2014 13:00 Oct 13, 2016 Jkt 241001 PO 00000 Frm 00006 Fmt 4700 Sfmt 4700 E:\FR\FM\14OCR1.SGM 14OCR1](https://thefederalregister.org/doc/81_FR_71127/page/1.svg)
![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
VerDate Sep<11>2014 13:00 Oct 13, 2016 Jkt 241001 PO 00000 Frm 00007 Fmt 4700 Sfmt 4700 E:\FR\FM\14OCR1.SGM 14OCR1](https://thefederalregister.org/doc/81_FR_71127/page/2.svg)
Document Created: 2016-10-14 00:00:33
Document Modified: 2016-10-14 00:00:33
| 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 | Matt Fuller, Senior Aviation Safety Engineer, Safety Management Group, Rotorcraft Directorate, FAA, 10101 Hillwood Pkwy, Fort Worth, TX 76177; telephone (817) 222-5110; email [email protected] | |
| FR Citation | 81 FR 70928 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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