83 FR 20751 - Airworthiness Directives; Airbus Helicopters
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 83, Issue 89 (May 8, 2018)
Federal Aviation Administration
Federal Register Volume 83, Issue 89 (May 8, 2018)
| Page Range | 20751-20753 | |
| FR Document | 2018-09740 |
[Federal Register Volume 83, Number 89 (Tuesday, May 8, 2018)] [Proposed Rules] [Pages 20751-20753] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2018-09740] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2017-1124; Product Identifier 2017-SW-073-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 AS332C, AS332C1, AS332L, and AS332L1 helicopters. This proposed AD would require inspecting the jettisoning mechanism of the left-hand (LH) and right-hand (RH) cabin sliding plug doors. This proposed AD is prompted by a report that during a scheduled inspection a cabin door failed to jettison. The actions of this proposed AD are intended to correct an unsafe condition on these products. DATES: We must receive comments on this proposed AD by July 9, 2018. 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-2017- 1124; or in person at Docket Operations 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 information. The street address for Docket Operations (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.helicopters.airbus.com/website/en/ref/Technical-Support_73.html. 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: Matt Fuller, Senior Aviation Safety Engineer, Safety Management Section, Rotorcraft Standards Branch, FAA, 10101 Hillwood Pkwy., Fort Worth, TX 76177; telephone (817) 222-5110; email [email protected]. SUPPLEMENTARY INFORMATION: [[Page 20752]] 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. 2017-0022, dated February 8, 2017, to correct an unsafe condition for Airbus Helicopters (previously Eurocopter) Model AS332C, AS332C1, AS332L, and AS332L1 helicopters equipped with a cabin sliding plug door modified in accordance with Airbus Helicopters modification (MOD) 0722338. Helicopters with Eurocopter MOD 0725366 are exempt from the EASA AD's requirements. EASA advises that the emergency jettison test of a cabin lateral sliding plug door failed during a scheduled inspection and test of the door's jettison mechanism. According to EASA, an investigation revealed that the jettison handle cable interfered with the cable clamps. EASA states that this condition could lead to jamming of the door jettisoning mechanism, preventing jettisoning of the affected door during an emergency, possibly obstructing evacuation of the occupants. The EASA AD consequently requires repetitive inspections of the jettisoning mechanism of the LH and RH door, followed by corrective actions if needed. 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. AS332- 52.00.56, Revision 0, dated January 30, 2017, which specifies pulling on the inner jettison handle to determine whether the cables come into contact with the cable clamps. If there is contact, this service information specifies changing the position of the cable clamps to prevent interference. 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 also reviewed Eurocopter Service Bulletin No. 332-52.00.28, Revision 1, dated April 29, 1998, which contains procedures to improve the door jettison system. Eurocopter identifies compliance with this service information as MOD 0725366. Proposed AD Requirements This proposed AD would require before flight over water or within 110 hours time-in-service (TIS), whichever occurs first, inspecting the jettisoning mechanism of the LH and RH cabin doors for correct operation by pulling on the inner jettison handle to determine whether the cable clamp contacts the top and bottom horizontal cables. If there is contact between cable clamp and the horizontal cables, this proposed AD would require changing the position of the cable clamps to remove any contact. Differences Between This Proposed AD and the EASA AD The EASA AD requires that the initial inspection occur during the next jettisoning test of the doors or within 110 flight hours, whichever occurs first, and thereafter during certain maintenance tasks. This proposed AD would require a one-time inspection within 110 hours TIS or prior to flying over water. Costs of Compliance We estimate that this proposed AD would affect 19 helicopters of U.S. Registry and that labor costs average $85 per work-hour. Based on these estimates, we expect that inspecting the jettisoning mechanism and changing the orientation of the cable clamps, if necessary, would require 4 work-hours. No parts would be required for a total cost of $340 per helicopter and $6,460 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); 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. [[Page 20753]] 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-2017-1124; Product Identifier 2017-SW-073-AD. (a) Applicability This AD applies to Airbus Helicopters Model AS332C, AS332C1, AS332L, and AS332L1 helicopters, certificated in any category, with a cabin sliding plug door installed in accordance with Airbus Helicopters modification (MOD) 0722338, except helicopters with a plug door jettison system installed in accordance with MOD 0725366. (b) Unsafe Condition This AD defines the unsafe condition as failure of a cabin sliding door to jettison, which could prevent helicopter occupants from evacuating the helicopter during an emergency. (c) Comments Due Date We must receive comments by July 9, 2018. (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 110 hours time-in-service (TIS) or before the next operation over water, whichever occurs first, inspect the jettisoning mechanism of the left-hand and right-hand cabin doors for correct operation: (1) Pull the jettisoning handle and determine whether the cable clamp contacts the top or bottom horizontal cables, using as a reference the photographs under paragraph 3.B.2 of Airbus Helicopters ASB No. AS332-52.00.56, Revision 0, dated January 30, 2017 (ASB). (2) If there is contact between a cable clamp and a horizontal cable, before further flight, install both cable clamps as depicted in the bottom photograph under paragraph 3.B.2 of the ASB. (f) Alternative Methods of Compliance (AMOCs) (1) The Manager, Safety Management Section, Rotorcraft Standards Branch, FAA, may approve AMOCs for this AD. Send your proposal to: Matt Fuller, Senior Aviation Safety Engineer, Safety Management Section, Rotorcraft Standards Branch, 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) Eurocopter Service Bulletin No. 332-52.00.28, Revision 1, dated April 29, 1998, which is not incorporated by reference, contains additional information about the subject of this AD. For service information identified in this AD, 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.helicopters.airbus.com/website/en/ref/Technical-Support_73.html. 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. (2) The subject of this AD is addressed in European Aviation Safety Agency (EASA) AD No. 2017-0022, dated February 8, 2017. You may view the EASA AD on the internet at http://www.regulations.gov in the AD Docket. (h) Subject Joint Aircraft Service Component (JASC) Code: 5200, Doors. Issued in Fort Worth, Texas, on May 1, 2018. Lance T. Gant, Director, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. 2018-09740 Filed 5-7-18; 8:45 am] BILLING CODE 4910-13-P
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Document (TL); or within 90 days after the principal inspector, or lacking a principal proposed AD would require inspecting
effective date of this AD; whichever occurs inspector, the manager of the local flight the jettisoning mechanism of the left-
later, except for those certification standards district office/certificate holding hand (LH) and right-hand (RH) cabin
maintenance requirements (CMRs) tasks district office.
sliding plug doors. This proposed AD is
identified in figure 1 to paragraphs (g) and (h) (2) Contacting the Manufacturer: For any
of this AD. requirement in this AD to obtain corrective prompted by a report that during a
actions from a manufacturer, the action must scheduled inspection a cabin door failed
FIGURE 1 TO PARAGRAPHS (g) AND (h) be accomplished using a method approved to jettison. The actions of this proposed
OF THIS AD—GRACE PERIOD FOR by the Manager, International Section, AD are intended to correct an unsafe
Transport Standards Branch, FAA; or the condition on these products.
CMR TASKS European Aviation Safety Agency (EASA); or DATES: We must receive comments on
ATR–GIE Avions de Transport Régional’s
CMR/
EASA Design Organization Approval (DOA).
this proposed AD by July 9, 2018.
maintenance Compliance time ADDRESSES: You may send comments by
significant item If approved by the DOA, the approval must
(MSI) task include the DOA-authorized signature. any of the following methods:
213100–2A Within 550 flight hours or 90 (l) Related Information • Federal eRulemaking Docket: Go to
213100–2B days, whichever occurs first, http://www.regulations.gov. Follow the
(1) Refer to Mandatory Continuing
213100–3A after the effective date of this
Airworthiness Information (MCAI) EASA AD
online instructions for sending your
213100–3B AD. comments electronically.
2017–0222R1, dated December 15, 2017, for
related information. This MCAI may be • Fax: 202–493–2251.
(h) Initial Compliance Times for Certain
CMR Tasks found in the AD docket on the internet at • Mail: Send comments to the U.S.
http://www.regulations.gov by searching for Department of Transportation, Docket
For the CMR tasks listed in figure 1 to and locating Docket No. FAA–2018–0366.
paragraphs (g) and (h) of this AD, the initial
Operations, M–30, West Building
(2) For more information about this AD, Ground Floor, Room W12–140, 1200
compliance time for accomplishing the tasks contact Shahram Daneshmandi, Aerospace
is at the applicable time specified in ATR42– New Jersey Avenue SE, Washington, DC
Engineer, International Section, Transport
400/–500 Temporary Revision TR01/17, Standards Branch, FAA, 2200 South 216th
20590–0001.
dated May 3, 2017, to the ATR42–400/–500 St., Des Moines, WA 98198; telephone and • Hand Delivery: Deliver to the
Time Limits Document (TL); or within the fax 206–231–3220. ‘‘Mail’’ address between 9 a.m. and 5
compliance time specified in figure 1 to (3) For service information identified in p.m., Monday through Friday, except
paragraphs (g) and (h) of this AD; whichever this AD, contact ATR–GIE Avions de Federal holidays.
occurs later. Transport Régional, 1, Allée Pierre Nadot,
(i) No Alternative Actions, Intervals, and/or 31712 Blagnac Cedex, France; telephone +33 Examining the AD Docket
Critical Design Configuration Control (0) 5 62 21 62 21; fax +33 (0) 5 62 21 67 18; You may examine the AD docket on
Limitations (CDCCLs) email continued.airworthiness@atr- the internet at http://
aircraft.com; internet http://www.atr-
After the maintenance or inspection
aircraft.com. You may view this service
www.regulations.gov by searching for
program, as applicable, has been revised as and locating Docket No. FAA–2017–
required by paragraph (g) of this AD, no information at the FAA, Transport Standards
Branch, 2200 South 216th St., Des Moines, 1124; or in person at Docket Operations
alternative actions (e.g., inspections), between 9 a.m. and 5 p.m., Monday
intervals, and/or CDCCLs may be used unless WA. For information on the availability of
the actions, intervals, and/or CDCCLs are this material at the FAA, call 206–231–3195. through Friday, except Federal holidays.
approved as an alternative method of Issued in Des Moines, Washington, on The AD docket contains this proposed
compliance (AMOC) in accordance with the April 27, 2018. AD, the European Aviation Safety
procedures specified in paragraph (k)(1) of Michael Kaszycki, Agency (EASA) AD, the economic
this AD.
Acting Director, System Oversight Division,
evaluation, any comments received, and
(j) Terminating Action for Certain ADs Aircraft Certification Service. other information. The street address for
Docket Operations (telephone 800–647–
Accomplishing the actions required by [FR Doc. 2018–09731 Filed 5–7–18; 8:45 am]
paragraph (g) of this AD terminates all
5527) is in the ADDRESSES section.
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requirements of AD 2000–23–04 R1 and all Comments will be available in the AD
requirements of the ADs specified in docket shortly after receipt.
paragraphs (j)(1) and (j)(2) of this AD for DEPARTMENT OF TRANSPORTATION For service information identified in
ATR–GIE Avions de Transport Régional this proposed rule, contact Airbus
Model ATR42–500 airplanes only. Federal Aviation Administration Helicopters, 2701 N. Forum Drive,
(1) AD 2008–04–19 R1. Grand Prairie, TX 75052; telephone
(2) AD 2015–26–09.
14 CFR Part 39 (972) 641–0000 or (800) 232–0323; fax
(k) Other FAA AD Provisions (972) 641–3775; or at http://
[Docket No. FAA–2017–1124; Product www.helicopters.airbus.com/website/
The following provisions also apply to this
Identifier 2017–SW–073–AD] en/ref/Technical-Support_73.html.
AD:
(1) Alternative Methods of Compliance RIN 2120–AA64 You may review the referenced
(AMOCs): The Manager, International service information at the FAA, Office
Section, Transport Standards Branch, FAA, Airworthiness Directives; Airbus of the Regional Counsel, Southwest
has the authority to approve AMOCs for this Helicopters Region, 10101 Hillwood Pkwy, Room
AD, if requested using the procedures found
in 14 CFR 39.19. In accordance with 14 CFR 6N–321, Fort Worth, TX 76177.
AGENCY: Federal Aviation
sradovich on DSK3GMQ082PROD with PROPOSALS
39.19, send your request to your principal Administration (FAA), DOT. FOR FURTHER INFORMATION CONTACT: Matt
inspector or local Flight Standards District Fuller, Senior Aviation Safety Engineer,
Office, as appropriate. If sending information ACTION: Notice of proposed rulemaking
Safety Management Section, Rotorcraft
directly to the International Section, send it (NPRM).
Standards Branch, FAA, 10101
to the attention of the person identified in
SUMMARY: We propose to adopt a new Hillwood Pkwy., Fort Worth, TX 76177;
paragraph (l)(2) of this AD. Information may
be emailed to: 9-ANM-116-AMOC- airworthiness directive (AD) for Airbus telephone (817) 222–5110; email
REQUESTS@faa.gov. Before using any Helicopters Model AS332C, AS332C1, matthew.fuller@faa.gov.
approved AMOC, notify your appropriate AS332L, and AS332L1 helicopters. This SUPPLEMENTARY INFORMATION:
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List of Subjects in 14 CFR Part 39 (f) Alternative Methods of Compliance proposing to amend its auditor
(AMOCs) independence rules to refocus the
Air transportation, Aircraft, Aviation (1) The Manager, Safety Management analysis that must be conducted to
safety, Incorporation by reference, Section, Rotorcraft Standards Branch, FAA, determine whether an auditor is
Safety. may approve AMOCs for this AD. Send your independent when the auditor has a
proposal to: Matt Fuller, Senior Aviation lending relationship with certain
The Proposed Amendment Safety Engineer, Safety Management Section,
Rotorcraft Standards Branch, FAA, 10101 shareholders of an audit client at any
Accordingly, under the authority Hillwood Pkwy., Fort Worth, TX 76177; time during an audit or professional
delegated to me by the Administrator, telephone (817) 222–5110; email 9-ASW- engagement period. The proposed
the FAA proposes to amend 14 CFR part FTW-AMOC-Requests@faa.gov. amendments would focus the analysis
39 as follows: (2) For operations conducted under a 14 solely on beneficial ownership rather
CFR part 119 operating certificate or under than on both record and beneficial
PART 39—AIRWORTHINESS 14 CFR part 91, subpart K, we suggest that ownership; replace the existing 10
DIRECTIVES you notify your principal inspector, or
lacking a principal inspector, the manager of
percent bright-line shareholder
the local flight standards district office or ownership test with a ‘‘significant
■ 1. The authority citation for part 39 certificate holding district office before influence’’ test; add a ‘‘known through
continues to read as follows: operating any aircraft complying with this reasonable inquiry’’ standard with
Authority: 49 U.S.C. 106(g), 40113, 44701. AD through an AMOC. respect to identifying beneficial owners
(g) Additional Information of the audit client’s equity securities;
§ 39.13 [Amended] and amend the definition of ‘‘audit
(1) Eurocopter Service Bulletin No. 332–
■ 2. The FAA amends § 39.13 by adding 52.00.28, Revision 1, dated April 29, 1998, client’’ for a fund under audit to exclude
the following new airworthiness which is not incorporated by reference, funds that otherwise would be
directive (AD): contains additional information about the considered affiliates of the audit client.
subject of this AD. For service information The Commission is also requesting
Airbus Helicopters: Docket No. FAA–2017– identified in this AD, contact Airbus comment on certain other potential
1124; Product Identifier 2017–SW–073– Helicopters, 2701 N Forum Drive, Grand
AD. amendments to its auditor
Prairie, TX 75052; telephone (972) 641–0000 independence rules.
(a) Applicability or (800) 232–0323; fax (972) 641–3775; or at
http://www.helicopters.airbus.com/website/ DATES: Comments should be received on
This AD applies to Airbus Helicopters en/ref/Technical-Support_73.html. You may or before July 9, 2018.
Model AS332C, AS332C1, AS332L, and review the referenced service information at ADDRESSES: Comments may be
AS332L1 helicopters, certificated in any the FAA, Office of the Regional Counsel, submitted by any of the following
category, with a cabin sliding plug door Southwest Region, 10101 Hillwood Pkwy., methods:
installed in accordance with Airbus Room 6N–321, Fort Worth, TX 76177.
Helicopters modification (MOD) 0722338, (2) The subject of this AD is addressed in Electronic Comments
except helicopters with a plug door jettison European Aviation Safety Agency (EASA) AD
system installed in accordance with MOD No. 2017–0022, dated February 8, 2017. You • Use the Commission’s internet
0725366. may view the EASA AD on the internet at comment form (http://www.sec.gov/
http://www.regulations.gov in the AD Docket. rules/proposed.shtml); or
(b) Unsafe Condition
(h) Subject
• Send an email to rule-comments@
This AD defines the unsafe condition as sec.gov. Please include File Number S7–
failure of a cabin sliding door to jettison, Joint Aircraft Service Component (JASC) 10–18 on the subject line.
which could prevent helicopter occupants Code: 5200, Doors.
from evacuating the helicopter during an Paper Comments
Issued in Fort Worth, Texas, on May 1,
emergency.
2018. • Send paper comments to Brent J.
(c) Comments Due Date Lance T. Gant, Fields, Secretary, Securities and
We must receive comments by July 9, 2018. Director, Compliance & Airworthiness Exchange Commission, 100 F Street NE,
Division, Aircraft Certification Service. Washington, DC 20549–1090.
(d) Compliance All submissions should refer to File
[FR Doc. 2018–09740 Filed 5–7–18; 8:45 am]
You are responsible for performing each Number S7–10–18. This file number
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action required by this AD within the should be included on the subject line
specified compliance time unless it has if email is used. To help us process and
already been accomplished prior to that time. review your comments more efficiently,
SECURITIES AND EXCHANGE
(e) Required Actions COMMISSION please use only one method. The
Within 110 hours time-in-service (TIS) or Commission will post all comments on
before the next operation over water, 17 CFR Part 210 the Commission’s website (http://
whichever occurs first, inspect the jettisoning www.sec.gov/rules/proposed.shtml).
[Release No. 33–10491; 34–83157; IC– Comments are also available for website
mechanism of the left-hand and right-hand
33091; IA–4904; FILE NO. S7–10–18]
cabin doors for correct operation: viewing and printing in the
(1) Pull the jettisoning handle and RIN 3235–AM01 Commission’s Public Reference Room,
determine whether the cable clamp contacts 100 F Street NE, Washington, DC 20549,
the top or bottom horizontal cables, using as Auditor Independence With Respect to on official business days between the
sradovich on DSK3GMQ082PROD with PROPOSALS
a reference the photographs under paragraph Certain Loans or Debtor-Creditor hours of 10:00 a.m. and 3:00 p.m. All
3.B.2 of Airbus Helicopters ASB No. AS332– Relationships comments received will be posted
52.00.56, Revision 0, dated January 30, 2017
(ASB). AGENCY: Securities and Exchange without change. Persons submitting
(2) If there is contact between a cable Commission. comments are cautioned that we do not
clamp and a horizontal cable, before further ACTION: Proposed rule. redact or edit personal identifying
flight, install both cable clamps as depicted information from comment submissions.
in the bottom photograph under paragraph SUMMARY:The Securities and Exchange You should submit only information
3.B.2 of the ASB. Commission (‘‘Commission’’) is that you wish to make available
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Document Created: 2018-05-08 01:31:28
Document Modified: 2018-05-08 01:31:28
| 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 July 9, 2018. | |
| Contact | Matt Fuller, Senior Aviation Safety Engineer, Safety Management Section, Rotorcraft Standards Branch, FAA, 10101 Hillwood Pkwy., Fort Worth, TX 76177; telephone (817) 222-5110; email [email protected] | |
| FR Citation | 83 FR 20751 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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