83 FR 23829 - Airworthiness Directives; Robinson Helicopter Company Helicopters
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 83, Issue 100 (May 23, 2018)
Federal Aviation Administration
Federal Register Volume 83, Issue 100 (May 23, 2018)
| Page Range | 23829-23831 | |
| FR Document | 2018-10919 |
[Federal Register Volume 83, Number 100 (Wednesday, May 23, 2018)] [Proposed Rules] [Pages 23829-23831] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2018-10919] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2017-0947; Product Identifier 2017-SW-059-AD] RIN 2120-AA64 Airworthiness Directives; Robinson Helicopter Company Helicopters AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM). ----------------------------------------------------------------------- SUMMARY: We propose to adopt a new airworthiness directive (AD) for Robinson Helicopter Company (Robinson) Model R44 and R44 II helicopters. This proposed AD would require visually checking each tail rotor blade for a crack. This proposed AD is prompted by a report of cracking in certain tail rotor blades. The actions of this proposed AD are intended to address an unsafe condition on these products. DATES: We must receive comments on this proposed AD by July 23, 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- 0947; 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 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 Robinson Helicopter Company, 2901 Airport Drive, Torrance, CA 90505; telephone (310) 539-0508; fax (310) 539-5198; or at http://www.robinsonheli.com/servelib.htm. 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: James Guo, Aerospace Engineer, Los Angeles ACO Branch, Compliance & Airworthiness Division, FAA, 3960 Paramount Blvd., Lakewood, California 90712; telephone (562) 627-5357; email james.guo@faa.gov. 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 [[Page 23830]] 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 We propose to adopt a new AD for Robinson R44 and R44 II helicopters with a tail rotor blade part number (P/N) C029-1 or P/N C029-2 installed. This proposed AD would require checking the tail rotor blades for cracks within 50 hours time-in-service (TIS) and thereafter before each flight. This proposed AD is prompted by reports of P/N C029-1 and P/N C029- 2 tail rotor blades with fatigue cracks at the leading edge. The cracks were caused by high fatigue stresses due to resonance when the blades were at high pitch angles from large left pedal inputs. Robinson consequently issued R44 Service Bulletin SB-83, dated May 30, 2012 (SB- 83). At the time SB-83 was issued, the reports of cracking on the tail rotor blade were isolated and infrequent. Since 2015, five events have been reported of helicopters with cracking on tail rotor blades. Therefore, we are proposing actions that are intended to detect a cracked tail rotor blade and prevent loss of the blade and subsequent loss of directional control. FAA's Determination We are proposing this AD because we evaluated all known relevant information and determined that an unsafe condition exists and is likely to exist or develop on other products of these same type designs. Related Service Information We have reviewed Robinson SB-83 which specifies, within 10 flight hours or by June 30, 2012, whichever occurs first, inserting a caution page into the Pilot's Operating Handbook. The caution page specifies inspecting the leading edges of each tail rotor blade for a crack before each flight. The caution page also advises that to reduce fatigue stress damage to the tail rotor blades, pilots should avoid maneuvers that require large left pedal inputs. SB-83 specifies that the caution page may be removed when the tail rotor blades are replaced with tail rotor blade P/N C029-3. Proposed AD Requirements This proposed AD would require within 50 hours TIS and thereafter before each flight, visually checking each tail rotor blade for a crack in the tail leading edge, paying particular attention to the most inboard white paint stripe. An owner/operator (pilot) may perform the required visual check and must enter compliance with the applicable paragraph of the AD into the helicopter maintenance records in accordance with 14 CFR 43.9(a)(1) through (4) and 91.417(a)(2)(v). A pilot may perform this check because it involves only a visual check and can be performed equally well by a pilot or a mechanic. This check is an exception to our standard maintenance regulations. This proposed AD also would require before further flight, replacing any cracked tail rotor blade. Differences Between This Proposed AD and the Service Information Robinson SB SB-83 requires compliance within 10 flight hours or by June 30, 2012, whichever occurs first. This proposed AD would require compliance within 50 hours TIS. Given the helicopter's history and the type of operations conducted by the current fleet, we determined that this compliance time is adequate to reduce the risk of a crack on the tail rotor blade to an acceptable level. Costs of Compliance We estimate that this proposed AD would affect 1,631 helicopters of U.S. Registry and that labor costs average $85 per work-hour. Visually checking the tail rotor blades for a crack would require 0.2 hour for a cost of $17 per helicopter and $27,727 for the U.S. fleet per check cycle. Replacing a tail rotor blade, if required, would require 2 work- hours and parts would cost $3,080 for a cost of $3,250 per blade. 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. 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. [[Page 23831]] Sec. 39.13 [Amended] 0 2. The FAA amends Sec. 39.13 by adding the following new airworthiness directive (AD): Robinson Helicopter Company: Product No. FAA-2017-0947; Product Identifier 2017-SW-059-AD. (a) Applicability This AD applies to Robinson Helicopter Company (Robinson) Model R44 and R44 II helicopters, certificated in any category, with a tail rotor blade part number (P/N) C029-1 or P/N C029-2 installed. (b) Unsafe Condition This AD defines the unsafe condition as a crack in a tail rotor blade. This condition could result in the loss of the tail rotor and subsequent loss of control of the helicopter. (c) Comments Due Date We must receive comments by July 23, 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 50 hours TIS after the effective date of this AD and thereafter before each flight: (1) Visually check each tail rotor blade for a crack in the tail leading edge, paying particular attention to the area in the most inboard white paint stripe. Wipe the blades clean, if necessary, to ensure any potential crack is visible. The actions required by this paragraph may be performed by the owner/operator (pilot) holding at least a private pilot certificate and must be entered into the aircraft records showing compliance with this AD in accordance with 14 CFR 43.9(a)(1) through (4) and 14 CFR 91.417(a)(2)(v). The record must be maintained as required by 14 CFR 91.417, 121.380, or 135.439. (2) If there is a crack, before further flight, replace the tail rotor blade. (f) Alternative Methods of Compliance (AMOC) (1) The Manager, Los Angeles ACO Branch, FAA, may approve AMOCs for this AD. Send your proposal to: James Guo, Aerospace Engineer, Los Angeles ACO Branch, Compliance & Airworthiness Division, FAA, 3960 Paramount Blvd., Lakewood, California 90712; telephone (562) 627-5357; email james.guo@faa.gov. (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 Robinson Helicopter Company R44 Service Bulletin SB-83, dated May 30, 2012, which is not incorporated by reference, contains additional information about the subject of this AD. For service information identified in this AD, contact Robinson Helicopter Company, 2901 Airport Drive, Torrance, CA 90505; telephone (310) 539-0508; fax (310) 539-5198; or at http://www.robinsonheli.com/servelib.htm. You may review a copy of information at the FAA, Office of the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N-321, Fort Worth, TX 76177. (h) Subject Joint Aircraft Service Component (JASC) Code: 6410, Tail Rotor Blades. Issued in Fort Worth, Texas, on May 14, 2018. Scott A. Horn, Deputy Director for Regulatory Operations, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. 2018-10919 Filed 5-22-18; 8:45 am] BILLING CODE 4910-13-P
![Federal Register / Vol. 83, No. 100 / Wednesday, May 23, 2018 / Proposed Rules 23829
4. Will not have a significant (2) For operations conducted under a 14 certain tail rotor blades. The actions of
economic impact, positive or negative, CFR part 119 operating certificate or under this proposed AD are intended to
on a substantial number of small entities 14 CFR part 91, subpart K, we suggest that address an unsafe condition on these
you notify your principal inspector, or
under the criteria of the Regulatory products.
lacking a principal inspector, the manager of
Flexibility Act. the local flight standards district office or DATES: We must receive comments on
We prepared an economic evaluation certificate holding district office before this proposed AD by July 23, 2018.
of the estimated costs to comply with operating any aircraft complying with this ADDRESSES: You may send comments by
this proposed AD and placed it in the AD through an AMOC. any of the following methods:
AD docket. • Federal eRulemaking Docket: Go to
(g) Additional Information
List of Subjects in 14 CFR Part 39 (1) Leonardo Helicopters Bollettino http://www.regulations.gov. Follow the
Air transportation, Aircraft, Aviation Tecnico (BT) No. 189–038, Revision B, and online instructions for sending your
safety, Incorporation by reference, BT No. 189–070, Revision A, both dated comments electronically.
Safety. October 13, 2016, which are not incorporated • Fax: 202–493–2251.
by reference, contain additional information • Mail: Send comments to the U.S.
The Proposed Amendment about the subject of this AD. For service Department of Transportation, Docket
information identified in this AD, contact Operations, M–30, West Building
Accordingly, under the authority
Leonardo S.p.A. Helicopters, Matteo Ragazzi, Ground Floor, Room W12–140, 1200
delegated to me by the Administrator, Head of Airworthiness, Viale G.Agusta 520,
the FAA proposes to amend 14 CFR part New Jersey Avenue SE, Washington, DC
21017 C.Costa di Samarate (Va) Italy;
39 as follows: 20590–0001.
telephone +39–0331–711756; fax +39–0331–
229046; or at http://www.leonardocompany
• Hand Delivery: Deliver to the
PART 39—AIRWORTHINESS .com/-/bulletins. You may review the ‘‘Mail’’ address between 9 a.m. and 5
DIRECTIVES referenced service information at the FAA, p.m., Monday through Friday, except
Office of the Regional Counsel, Southwest Federal holidays.
■ 1. The authority citation for part 39 Region, 10101 Hillwood Pkwy., Room 6N–
continues to read as follows: 321, Fort Worth, TX 76177.
Examining the AD Docket
Authority: 49 U.S.C. 106(g), 40113, 44701. (2) The subject of this AD is addressed in You may examine the AD docket on
European Aviation Safety Agency (EASA) AD the internet at http://
§ 39.13 [Amended] No. 2016–0161, dated August 8, 2016. You www.regulations.gov by searching for
■ 2. The FAA amends § 39.13 by adding may view the EASA AD on the internet at and locating Docket No. FAA–2017–
http://www.regulations.gov in the AD Docket. 0947; or in person at Docket Operations
the following new airworthiness
directive (AD): (h) Subject between 9 a.m. and 5 p.m., Monday
AgustaWestland S.p.A.: Docket No. FAA– Joint Aircraft Service Component (JASC) through Friday, except Federal holidays.
2017–1081; Product Identifier 2017–SW– Code: 5510, Horizontal Stabilizer Structure. The AD docket contains this proposed
090–AD. Issued in Fort Worth, Texas, on May 15,
AD, the economic evaluation, any
(a) Applicability 2018. comments received, and other
Scott A. Horn,
information. The street address for
This AD applies to AgustaWestland S.p.A. Docket Operations (telephone 800–647–
Model AW189 helicopters, certificated in any Deputy Director for Regulatory Operations,
category, with a tail plane lower fitting P/N Compliance & Airworthiness Division,
5527) is in the ADDRESSES section.
8G5350A07051 installed. Aircraft Certification Service. Comments will be available in the AD
[FR Doc. 2018–10918 Filed 5–22–18; 8:45 am]
docket shortly after receipt.
(b) Unsafe Condition For service information identified in
BILLING CODE 4910–13–P
This AD defines the unsafe condition as a this proposed rule, contact Robinson
crack on a tail plane fitting, which could Helicopter Company, 2901 Airport
result in failure of the tail plane fitting and Drive, Torrance, CA 90505; telephone
loss of helicopter control. DEPARTMENT OF TRANSPORTATION
(310) 539–0508; fax (310) 539–5198; or
(c) Comments Due Date Federal Aviation Administration at http://www.robinsonheli.com/
We must receive comments by July 23, servelib.htm. You may review the
2018. 14 CFR Part 39 referenced service information at the
FAA, Office of the Regional Counsel,
(d) Compliance [Docket No. FAA–2017–0947; Product Southwest Region, 10101 Hillwood
You are responsible for performing each Identifier 2017–SW–059–AD]
Pkwy., Room 6N–321, Fort Worth, TX
action required by this AD within the
specified compliance time unless it has
RIN 2120–AA64 76177.
already been accomplished prior to that time. FOR FURTHER INFORMATION CONTACT:
Airworthiness Directives; Robinson
(e) Required Actions James Guo, Aerospace Engineer, Los
Helicopter Company Helicopters
Angeles ACO Branch, Compliance &
Within 50 hours time-in-service, install tail
AGENCY: Federal Aviation Airworthiness Division, FAA, 3960
plane retromodification kit part number
8G0000P00511. Administration (FAA), DOT. Paramount Blvd., Lakewood, California
ACTION: Notice of proposed rulemaking 90712; telephone (562) 627–5357; email
(f) Alternative Methods of Compliance james.guo@faa.gov.
(AMOCs)
(NPRM).
SUPPLEMENTARY INFORMATION:
daltland on DSKBBV9HB2PROD with PROPOSALS
(1) The Manager, Safety Management SUMMARY: We propose to adopt a new
Section, Rotorcraft Standards Branch, FAA, airworthiness directive (AD) for Comments Invited
may approve AMOCs for this AD. Send your Robinson Helicopter Company We invite you to participate in this
proposal to: Martin R. Crane, Aviation Safety
Engineer, Regulations & Policy Section,
(Robinson) Model R44 and R44 II rulemaking by submitting written
Rotorcraft Standards Branch, FAA, 10101 helicopters. This proposed AD would comments, data, or views. We also
Hillwood Pkwy., Fort Worth, TX 76177; require visually checking each tail rotor invite comments relating to the
telephone (817) 222–5110; email 9-ASW- blade for a crack. This proposed AD is economic, environmental, energy, or
FTW-AMOC-Requests@faa.gov. prompted by a report of cracking in federalism impacts that might result
VerDate Sep<11>2014 16:37 May 22, 2018 Jkt 244001 PO 00000 Frm 00003 Fmt 4702 Sfmt 4702 E:\FR\FM\23MYP1.SGM 23MYP1](https://thefederalregister.org/doc/83_FR_23929/page/1.svg)
![Federal Register / Vol. 83, No. 100 / Wednesday, May 23, 2018 / Proposed Rules 23831
§ 39.13 [Amended] this AD. For service information identified in subsequent amendments can be viewed
■ 2. The FAA amends § 39.13 by adding this AD, contact Robinson Helicopter on line at http://www.faa.gov/air_
the following new airworthiness Company, 2901 Airport Drive, Torrance, CA traffic/publications/. For further
90505; telephone (310) 539–0508; fax (310)
directive (AD): 539–5198; or at http://
information, you can contact the
Robinson Helicopter Company: Product No. www.robinsonheli.com/servelib.htm. You Airspace Policy Group, Federal Aviation
FAA–2017–0947; Product Identifier may review a copy of information at the Administration, 800 Independence
2017–SW–059–AD. FAA, Office of the Regional Counsel, Avenue SW, Washington, DC 20591;
Southwest Region, 10101 Hillwood Pkwy., telephone: (202) 267–8783. The Order is
(a) Applicability Room 6N–321, Fort Worth, TX 76177. also available for inspection at the
This AD applies to Robinson Helicopter National Archives and Records
Company (Robinson) Model R44 and R44 II (h) Subject
Joint Aircraft Service Component (JASC) Administration (NARA). For
helicopters, certificated in any category, with
a tail rotor blade part number (P/N) C029–1 Code: 6410, Tail Rotor Blades. information on the availability of FAA
or P/N C029–2 installed. Order 7400.11B at NARA, call (202)
Issued in Fort Worth, Texas, on May 14,
2018.
741–6030, or go to https://
(b) Unsafe Condition www.archives.gov/federal-register/cfr/
This AD defines the unsafe condition as a Scott A. Horn,
ibr-locations.html.
crack in a tail rotor blade. This condition Deputy Director for Regulatory Operations,
FAA Order 7400.11, Airspace
could result in the loss of the tail rotor and Compliance & Airworthiness Division,
Aircraft Certification Service. Designations and Reporting Points, is
subsequent loss of control of the helicopter.
published yearly and effective on
[FR Doc. 2018–10919 Filed 5–22–18; 8:45 am]
(c) Comments Due Date September 15.
BILLING CODE 4910–13–P
We must receive comments by July 23, FOR FURTHER INFORMATION CONTACT: John
2018. Fornito, Operations Support Group,
(d) Compliance DEPARTMENT OF TRANSPORTATION Eastern Service Center, Federal Aviation
You are responsible for performing each Administration, 1701 Columbia Ave.,
action required by this AD within the Federal Aviation Administration College Park, GA 30337; telephone (404)
specified compliance time unless it has 305–6364.
already been accomplished prior to that time. 14 CFR Part 71 SUPPLEMENTARY INFORMATION:
(e) Required Actions [Docket No. FAA–2018–0255; Airspace Authority for This Rulemaking
Within 50 hours TIS after the effective date Docket No. 18–ASO–6]
of this AD and thereafter before each flight: The FAA’s authority to issue rules
RIN 2120–AA66
(1) Visually check each tail rotor blade for regarding aviation safety is found in title
a crack in the tail leading edge, paying Proposed Revocation of Class E 49 of the United States Code. Subtitle I,
particular attention to the area in the most Airspace; St Marys, GA Section 106 describes the authority of
inboard white paint stripe. Wipe the blades the FAA Administrator. Subtitle VII,
clean, if necessary, to ensure any potential AGENCY: Federal Aviation Aviation Programs, describes in more
crack is visible. The actions required by this Administration (FAA), DOT. detail the scope of the agency’s
paragraph may be performed by the owner/ ACTION: Notice of proposed rulemaking authority. This proposed rulemaking is
operator (pilot) holding at least a private pilot
certificate and must be entered into the
(NPRM). promulgated under the authority
aircraft records showing compliance with described in Subtitle VII, Part A,
SUMMARY: This action proposes to Subpart I, Section 40103. Under that
this AD in accordance with 14 CFR 43.9(a)(1) remove Class E airspace extending
through (4) and 14 CFR 91.417(a)(2)(v). The section, the FAA is charged with
record must be maintained as required by 14
upward from 700 feet above the surface prescribing regulations to assign the use
CFR 91.417, 121.380, or 135.439. at St Marys, GA, because St Marys of airspace necessary to ensure the
(2) If there is a crack, before further flight, Airport has closed, and controlled safety of aircraft and the efficient use of
replace the tail rotor blade. airspace is no longer required at this
airspace. This regulation is within the
location.
(f) Alternative Methods of Compliance scope of that authority as it would
(AMOC) DATES: Comments must be received on remove Class E airspace extending
(1) The Manager, Los Angeles ACO Branch, or before July 9, 2018. upward from 700 feet above the surface
FAA, may approve AMOCs for this AD. Send ADDRESSES: Send comments on this rule at St Marys Airport, St Marys, GA, due
your proposal to: James Guo, Aerospace to: U.S. Department of Transportation, to the closing of this airport.
Engineer, Los Angeles ACO Branch, Docket Operations, 1200 New Jersey
Compliance & Airworthiness Division, FAA, Comments Invited
Avenue SE, West Bldg Ground Floor,
3960 Paramount Blvd., Lakewood, California Rm W12–140, Washington, DC 20590; Interested persons are invited to
90712; telephone (562) 627–5357; email Telephone: 800–647–5527, or (202) comment on this rule by submitting
james.guo@faa.gov.
366–9826. You must identify the Docket such written data, views, or arguments,
(2) For operations conducted under a 14
CFR part 119 operating certificate or under No. FAA–2018–0255; Airspace Docket as they may desire. Comments that
14 CFR part 91, subpart K, we suggest that No. 18–ASO–6, at the beginning of your provide the factual basis supporting the
you notify your principal inspector, or comments. You may also submit and views and suggestions presented are
lacking a principal inspector, the manager of review received comments through the particularly helpful in developing
the local flight standards district office or internet at http://www.regulations.gov. reasoned regulatory decisions on the
daltland on DSKBBV9HB2PROD with PROPOSALS
certificate holding district office before You may review the public docket proposal. Comments are specifically
operating any aircraft complying with this containing the proposal, any comments invited on the overall regulatory,
AD through an AMOC. received, and any final disposition in aeronautical, economic, environmental,
(g) Additional Information person in the Dockets Office between and energy-related aspects of the
Robinson Helicopter Company R44 Service 9:00 a.m. and 5:00 p.m., Monday proposal.
Bulletin SB–83, dated May 30, 2012, which through Friday, except federal holidays. Communications should identify both
is not incorporated by reference, contains FAA Order 7400.11B, Airspace docket numbers (FAA Docket No. FAA–
additional information about the subject of Designations and Reporting Points, and 2018–0255; Airspace Docket No. 18–
VerDate Sep<11>2014 16:37 May 22, 2018 Jkt 244001 PO 00000 Frm 00005 Fmt 4702 Sfmt 4702 E:\FR\FM\23MYP1.SGM 23MYP1](https://thefederalregister.org/doc/83_FR_23929/page/3.svg)
Document Created: 2018-05-22 23:48:42
Document Modified: 2018-05-22 23:48:42
| 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 23, 2018. | |
| Contact | James Guo, Aerospace Engineer, Los Angeles ACO Branch, Compliance & Airworthiness Division, FAA, 3960 Paramount Blvd., Lakewood, California 90712; telephone (562) 627-5357; email [email protected] | |
| FR Citation | 83 FR 23829 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
2024 Federal Register | Disclaimer | Privacy Policy
USC | CFR | eCFR