81 FR 12836 - Airworthiness Directives; Airbus Helicopters
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 | 12836-12838 | |
| FR Document | 2016-05369 |
[Federal Register Volume 81, Number 48 (Friday, March 11, 2016)] [Proposed Rules] [Pages 12836-12838] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2016-05369] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2015-6033; Directorate Identifier 2015-SW-019-AD] RIN 2120-AA64 Airworthiness Directives; Airbus Helicopters AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM). ----------------------------------------------------------------------- SUMMARY: We propose to adopt a new airworthiness directive (AD) for Airbus Helicopters Model AS 365 N3 helicopters. This proposed AD would require inspecting the cabin and cockpit for labels, placards, or markings that provide jettison procedure instructions for cabin doors, removing any labels, placards, or markings that are in an incorrect location, and installing placards where they are missing. This proposed AD is prompted by the determination that placards had not been installed according to specifications on newly manufactured helicopters. The proposed actions are intended to provide exit procedures during an emergency. 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 Docket: Go to http://www.regulations.gov. Follow the online instructions for sending your comments electronically. Fax: 202-493-2251. Mail: Send comments to the U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE., Washington, DC 20590-0001. Hand Delivery: Deliver to the ``Mail'' address between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. 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- 6033; 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 European Aviation Safety Agency (EASA) AD, the economic evaluation, any comments received, and other [[Page 12837]] information. The street address for the Docket Operations Office (telephone 800-647-5527) is in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt. For service information identified in this proposed rule, contact Airbus Helicopters, 2701 N. Forum Drive, Grand Prairie, TX 75052; telephone (972) 641-0000 or (800) 232-0323; fax (972) 641-3775; or at http://www.airbushelicopters.com/techpub. 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. FOR FURTHER INFORMATION CONTACT: David Hatfield, 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: Comments Invited We invite you to participate in this rulemaking by submitting written comments, data, or views. We also invite comments relating to the economic, environmental, energy, or federalism impacts that might result from adopting the proposals in this document. The most helpful comments reference a specific portion of the proposal, explain the reason for any recommended change, and include supporting data. To ensure the docket does not contain duplicate comments, commenters should send only one copy of written comments, or if comments are filed electronically, commenters should submit only one time. We will file in the docket all comments that we receive, as well as a report summarizing each substantive public contact with FAA personnel concerning this proposed rulemaking. Before acting on this proposal, we will consider all comments we receive on or before the closing date for comments. We will consider comments filed after the comment period has closed if it is possible to do so without incurring expense or delay. We may change this proposal in light of the comments we receive. Discussion EASA, which is the Technical Agent for the Member States of the European Union, has issued EASA AD No. 2015-0068-E, dated April 29, 2015, to correct an unsafe condition for Airbus Helicopters Model AS 365 N3 helicopters without external life rafts installed, except those helicopters modified in accordance with Airbus Helicopters modification (MOD) 0711B68, and Model AS 365 N3 helicopters with external life rafts installed, except those helicopters modified in accordance Airbus Helicopters MOD 0711B67 and MOD 0711B68. EASA advises that, during helicopter delivery after manufacturing, Airbus Helicopters identified that placards providing jettison procedure instructions for the cabin doors were not systematically installed or not installed in a proper location. This condition, if not corrected, could prevent the timely evacuation of the helicopter during an emergency. The EASA AD consequently requires determining whether any placards are missing or incorrectly located, installing any missing placards, and replacing any incorrectly located placards. FAA's Determination These helicopters have been approved by the aviation authority of France and are approved for operation in the United States. Pursuant to our bilateral agreement with France, EASA, its technical representative, has notified us of the unsafe condition described in its AD. We are proposing this AD because we evaluated all known relevant information and determined that an unsafe condition is likely to exist or develop on other products of the same type design. Related Service Information Under 1 CFR Part 51 We reviewed Airbus Helicopters Alert Service Bulletin No. AS365- 11.00.02, Revision 2, dated April 23, 2015 (ASB). The service information describes procedures for replacing and installing cabin internal evacuation markings. The ASB reports that deviations in the locations of the cabin internal evacuation markings and missing markings were noted during the delivery of new helicopters. The ASB provides instructions about the locations of, characteristics of, and information contained in the markings. 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. Proposed AD Requirements This proposed AD would require, within 50 hours time-in-service (TIS), inspecting the cabin and cockpit for labels, placards, or markings that provide jettison procedure instructions for cabin doors in certain locations. If a label, placard, or marking is not located as required or is not visible and legible to every occupant, this proposed AD would require installing a placard in the required locations before further flight. Differences Between This Proposed AD and the EASA AD The EASA AD requires compliance within 14 days after the effective date of the EASA AD. This AD requires compliance within 50 hours TIS. Costs of Compliance We estimate that this proposed AD would affect 15 helicopters of U.S. Registry and that labor costs would average $85 a work-hour. Based on these estimates, we expect that inspecting the helicopter to determine the proper location and presence of cabin door jettison procedure placards and replacing and installing them would require 4 work hours and a parts cost of $70. We estimate a total cost of $410 per helicopter, and $6,150 for the U.S. fleet. 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, I certify this proposed regulation: 1. Is not a ``significant regulatory action'' under Executive Order 12866; 2. Is not a ``significant rule'' under the DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979); [[Page 12838]] 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 proposed 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. 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): Airbus Helicopters: Docket No. FAA-2015-6033; Directorate Identifier 2015-SW-019-AD. (a) Applicability This AD applies to Airbus Helicopters Model AS 365 N3 helicopters, certificated in any category. (b) Unsafe Condition This AD defines the unsafe condition as missing or incorrectly located information for exiting a helicopter. This condition could result in failure to jettison cabin doors during an emergency, resulting in death or injury of helicopter occupants. (c) Comments Due Date We must receive comments by May 10, 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 50 hours time-in-service: (1) Inspect the cabin and cockpit for labels, placards, and markings that provide jettison procedure instructions for cabin doors. (2) For the left and right side, remove any existing label, placard, and marking and install placards in accordance with the Accomplishment Instructions, paragraph 3.B.2 and Figures 1 through 6, of Airbus Helicopters Alert Service Bulletin No. AS365-11.00.02, Revision 2, dated April 23, 2015. (f) Credit for Previously Completed Actions Actions accomplished before the effective date of this AD in accordance with Airbus Helicopters Modification (MOD) 0711B68 for helicopters without external life rafts or MOD 0711B68 and MOD 0711B67 for helicopters with external life rafts are considered acceptable for compliance with this AD. (g) Alternative Methods of Compliance (AMOCs) (1) The Manager, Safety Management Group, FAA, may approve AMOCs for this AD. Send your proposal to: David Hatfield, 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. (h) Additional Information The subject of this AD is addressed in the European Aviation Safety Agency (EASA) AD No. 2015-0068-E, dated April 29, 2015. You may view the EASA AD on the Internet at http://www.regulations.gov by searching for and locating it in Docket No. FAA-2015-6033. (i) Subject Joint Aircraft Service Component (JASC) Code: 1100, Placards and Markings. Issued in Fort Worth, Texas, on February 29, 2016. Scott A. Horn, Acting Manager, Rotorcraft Directorate, Aircraft Certification Service. [FR Doc. 2016-05369 Filed 3-10-16; 8:45 am] BILLING CODE 4910-13-P
![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_12884/page/1.svg)
![12838 Federal Register / Vol. 81, No. 48 / Friday, March 11, 2016 / Proposed Rules
3. Will not affect intrastate aviation in AS365–11.00.02, Revision 2, dated April 23, Agusta Model AB139 and AW139
Alaska to the extent that it justifies 2015. helicopters. This proposed AD would
making a regulatory distinction; and (f) Credit for Previously Completed Actions require performing operational checks
4. Will not have a significant of both hydraulic systems. This
Actions accomplished before the effective
economic impact, positive or negative, date of this AD in accordance with Airbus proposed AD is prompted by an
on a substantial number of small entities Helicopters Modification (MOD) 0711B68 for assessment of the hydraulic systems of
under the criteria of the Regulatory helicopters without external life rafts or MOD the helicopter following an accident.
Flexibility Act. 0711B68 and MOD 0711B67 for helicopters The proposed actions are intended to
We prepared an economic evaluation with external life rafts are considered prevent loss of hydraulic power to the
of the estimated costs to comply with acceptable for compliance with this AD. flight controls and subsequent loss of
this proposed AD and placed it in the (g) Alternative Methods of Compliance control of the helicopter.
AD docket. (AMOCs) DATES: We must receive comments on
List of Subjects in 14 CFR Part 39 (1) The Manager, Safety Management this proposed AD by May 10, 2016.
Group, FAA, may approve AMOCs for this ADDRESSES: You may send comments by
Air transportation, Aircraft, Aviation AD. Send your proposal to: David Hatfield, any of the following methods:
safety, Incorporation by reference, Aviation Safety Engineer, Safety Management • Federal eRulemaking Docket: Go to
Safety. Group, Rotorcraft Directorate, FAA, 10101 http://www.regulations.gov. Follow the
The Proposed Amendment Hillwood Pkwy, Fort Worth, TX 76177; online instructions for sending your
telephone (817) 222–5110; email 9–ASW– comments electronically.
Accordingly, under the authority FTW–AMOC-Requests@faa.gov. • Fax: 202–493–2251.
delegated to me by the Administrator, (2) For operations conducted under a 14 • Mail: Send comments to the U.S.
the FAA proposes to amend 14 CFR part CFR part 119 operating certificate or under
Department of Transportation, Docket
39 as follows: 14 CFR part 91, subpart K, we suggest that
you notify your principal inspector, or Operations, M–30, West Building
lacking a principal inspector, the manager of Ground Floor, Room W12–140, 1200
PART 39—AIRWORTHINESS
the local flight standards district office or New Jersey Avenue SE., Washington,
DIRECTIVES
certificate holding district office before DC 20590–0001.
■ 1. The authority citation for part 39 operating any aircraft complying with this • Hand Delivery: Deliver to the
continues to read as follows: AD through an AMOC. ‘‘Mail’’ address between 9 a.m. and 5
(h) Additional Information
p.m., Monday through Friday, except
Authority: 49 U.S.C. 106(g), 40113, 44701. Federal holidays.
The subject of this AD is addressed in the
§ 39.13 [Amended] European Aviation Safety Agency (EASA) AD Examining the AD Docket
■ 2. The FAA amends § 39.13 by adding No. 2015–0068–E, dated April 29, 2015. You You may examine the AD docket on
the following new airworthiness may view the EASA AD on the Internet at
http://www.regulations.gov by searching for
the Internet at http://
directive (AD): www.regulations.gov by searching for
and locating it in Docket No. FAA–2015–
Airbus Helicopters: Docket No. FAA–2015– 6033. and locating Docket number FAA–
6033; Directorate Identifier 2015–SW– 2016–4278 or in person at the Docket
019–AD. (i) Subject Operations Office between 9 a.m. and 5
(a) Applicability Joint Aircraft Service Component (JASC) p.m., Monday through Friday, except
Code: 1100, Placards and Markings. Federal holidays. The AD docket
This AD applies to Airbus Helicopters
Model AS 365 N3 helicopters, certificated in Issued in Fort Worth, Texas, on February contains this proposed AD, the
any category. 29, 2016. European Aviation Safety Agency
Scott A. Horn, (EASA) AD, the economic evaluation,
(b) Unsafe Condition any comments received, and other
Acting Manager, Rotorcraft Directorate,
This AD defines the unsafe condition as Aircraft Certification Service. information. The street address for the
missing or incorrectly located information for Docket Operations Office (telephone
[FR Doc. 2016–05369 Filed 3–10–16; 8:45 am]
exiting a helicopter. This condition could 800–647–5527) is in the ADDRESSES
result in failure to jettison cabin doors during BILLING CODE 4910–13–P
section. Comments will be available in
an emergency, resulting in death or injury of
helicopter occupants. the AD docket shortly after receipt.
DEPARTMENT OF TRANSPORTATION For service information identified in
(c) Comments Due Date this proposed rule, contact
We must receive comments by May 10, Federal Aviation Administration AgustaWestland, Product Support
2016. Engineering, Via del Gregge, 100, 21015
(d) Compliance 14 CFR Part 39 Lonate Pozzolo (VA) Italy, ATTN:
Maurizio D’Angelo; telephone 39–0331–
You are responsible for performing each [Docket No. FAA–2016–4278; Directorate
664757; fax 39 0331–664680; or at
action required by this AD within the Identifier 2012–SW–022–AD]
specified compliance time unless it has
http://www.agustawestland.com/
already been accomplished prior to that time. RIN 2120–AA64 technical-bulletins. You may review the
referenced service information at the
(e) Required Actions Airworthiness Directives; FAA, Office of the Regional Counsel,
asabaliauskas on DSK3SPTVN1PROD with PROPOSALS
Within 50 hours time-in-service: AgustaWestland S.p.A. (Agusta) Southwest Region, 10101 Hillwood
(1) Inspect the cabin and cockpit for labels, Helicopters Parkway, Fort Worth, Texas 76177.
placards, and markings that provide jettison FOR FURTHER INFORMATION CONTACT: Matt
procedure instructions for cabin doors. AGENCY: Federal Aviation
Administration (FAA), DOT. Wilbanks, Aviation Safety Engineer,
(2) For the left and right side, remove any
existing label, placard, and marking and ACTION: Notice of proposed rulemaking Safety Management Group, Rotorcraft
install placards in accordance with the (NPRM). Directorate, FAA, 10101 Hillwood
Accomplishment Instructions, paragraph Parkway, Fort Worth, Texas 76177;
3.B.2 and Figures 1 through 6, of Airbus SUMMARY: We propose to adopt a new telephone (817) 222–5110; email
Helicopters Alert Service Bulletin No. airworthiness directive (AD) for certain matt.wilbanks@faa.gov.
VerDate Sep<11>2014 16:25 Mar 10, 2016 Jkt 238001 PO 00000 Frm 00007 Fmt 4702 Sfmt 4702 E:\FR\FM\11MRP1.SGM 11MRP1](https://thefederalregister.org/doc/81_FR_12884/page/3.svg)
Document Created: 2016-03-11 01:51:55
Document Modified: 2016-03-11 01:51:55
| 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 | David Hatfield, 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 12836 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
2025 Federal Register | Disclaimer | Privacy Policy
USC | CFR | eCFR