81 FR 27057 - Airworthiness Directives; Airbus Helicopters Deutschland GmbH Helicopters
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 81, Issue 87 (May 5, 2016)
Federal Aviation Administration
Federal Register Volume 81, Issue 87 (May 5, 2016)
| Page Range | 27057-27059 | |
| FR Document | 2016-10285 |
[Federal Register Volume 81, Number 87 (Thursday, May 5, 2016)] [Proposed Rules] [Pages 27057-27059] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2016-10285] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2015-3941; Directorate Identifier 2015-SW-052-AD] RIN 2120-AA64 Airworthiness Directives; Airbus Helicopters Deutschland GmbH 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 Deutschland GmbH (Airbus Helicopters) Model MBB-BK 117A-3, MBB-BK 117A-4, MBB-BK 117B-1, MBB-BK 117B-2, and MBB-BK 117C-1 helicopters. This proposed AD would require removing adhesive seals from the exterior and interior door jettisoning system on the left and right sliding doors. This proposed AD is prompted by reports that the adhesive seal prevented the doors from jettisoning properly. The proposed actions are intended to remove the adhesive seal to allow the doors to jettison properly so occupants can exit the helicopter during an emergency. DATES: We must receive comments on this proposed AD by July 5, 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- 3941; 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, [[Page 27058]] any comments received, and other 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: 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: 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 aviation authority for the Member States of the European Union, has issued EASA AD No. 2015-0163, dated August 6, 2015, to correct an unsafe condition for Airbus Helicopters Model MBB-BK 117A-3, MBB-BK 117A-4, MBB-BK 117B-1, MBB-BK 117B-2, and MBB-BK 117C-1 helicopters. EASA advises that difficulties were reported regarding the jettisoning of doors. The malfunction was caused by the adhesive seal, which hampered the free movement of the inner handle. According to EASA, a subsequent investigation showed that the adhesive seal has mechanical and physical properties that do not meet relevant certification requirements. EASA states that this condition, if not detected and corrected, could lead to a malfunction of the door's jettisoning mechanism, reducing or preventing the evacuation of the helicopter during an emergency, possibly resulting in injury to occupants. To address this condition, the EASA AD requires inspecting the exterior and interior door jettisoning system on the left and right sliding doors for adhesive seal part number (P/N) 117-800201.01 and removing any adhesive seals that are installed. FAA's Determination These helicopters have been approved by the aviation authority of Germany and are approved for operation in the United States. Pursuant to our bilateral agreement with Germany, 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 MBB-BK117- 20A-114, Revision 1, dated July 30, 2015 (ASB) for Model MBB-BK 117A-3, MBB-BK 117A-4, MBB-BK 117B-1, MBB-BK 117B-2, and MBB-BK 117C-1 helicopters. The ASB reports that the proper functioning of the sliding door jettison system is hampered by an adhesive seal. The seal was not manufactured correctly, and therefore did not perform as the test seal did during door jettisoning tests. The ASB calls for removing any adhesive seals on the exterior and interior door jettison system and discarding any adhesive seals that have not yet been installed. 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 25 hours time-in-service, removing the adhesive seal from the interior and exterior of each door. This proposed AD would also prohibit installing adhesive seal P/N 117- 800201.01 on any helicopter sliding door. Differences Between This Proposed AD and the EASA AD The EASA AD requires removing adhesive seal, P/N 117-800201.01, within 30 days. The proposed AD would require removing the adhesive seal within 25 hours TIS. Costs of Compliance We estimate that this proposed AD would affect 69 helicopters of U.S. Registry and that labor costs would average $85 per work-hour. Based on these estimates, we expect that removing the adhesive seals would require a half work-hour for a labor cost of about $43 per helicopter. No parts would be needed, so the cost for the U.S. fleet would total $2,967. 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 27059]] 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 Deutschland GmbH: Docket No. FAA-2015-3941; Directorate Identifier 2015-SW-052-AD. (a) Applicability This AD applies to Airbus Helicopters Deutschland GmbH (Airbus Helicopters) Model MBB-BK 117A-3, MBB-BK 117A-4, MBB-BK 117B-1, MBB- BK 117B-2, and MBB-BK 117C-1 helicopters with an adhesive seal part number (P/N) 117-800201.01 installed on an exterior or interior sliding door, certificated in any category. (b) Unsafe Condition This AD defines the unsafe condition the presence of sealant on a sliding door (door). This condition could result in the door failing to jettison, preventing helicopter occupants from exiting the helicopter during an emergency. (c) Comments Due Date We must receive comments by July 5, 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 (1) Within 25 hours time-in-service, remove adhesive seal P/N 117-800201.01 from the interior and exterior of each door. The areas where the seal is installed are shown in Figure 1 and Figure 2 of Airbus Helicopters Alert Service Bulletin MBB-BK117-20A-114, Revision 1, dated July 30, 2015. (2) After the effective date of this AD, do not install adhesive seal P/N 117-800201.01 on any helicopter sliding door. (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 The subject of this AD is addressed in European Aviation Safety Agency (EASA) AD No. 2015-0163, dated August 6, 2015. 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: 5220, Emergency Exits. Issued in Fort Worth, Texas, on April 19, 2016. Scott A. Horn, Acting Manager, Rotorcraft Directorate, Aircraft Certification Service. [FR Doc. 2016-10285 Filed 5-4-16; 8:45 am] BILLING CODE 4910-13-P
![Federal Register / Vol. 81, No. 87 / Thursday, May 5, 2016 / Proposed Rules 27057
(i) Visually inspect the exposed areas of the are no edge voids and no cracks, refinish the DEPARTMENT OF TRANSPORTATION
lower grip pad and upper and lower grip sanded area.
plates of each M/R blade for a crack and any (viii) If any parent material is removed Federal Aviation Administration
corrosion. during any sanding or trimming in
(ii) On the upper and lower exposed paragraphs (f)(2)(vi) or (f)(2)(vii) of this AD,
surfaces of each M/R blade from blade
14 CFR Part 39
repair the M/R blade if the damage is within
stations 24.5 to 35 for the chord width, [Docket No. FAA–2015–3941; Directorate
visually inspect each layered doubler and maximum repair damage limits, or replace
Identifier 2015–SW–052–AD]
blade skin for a crack and any corrosion. Pay the M/R blade with an airworthy M/R blade.
particular attention for any cracking in a RIN 2120–AA64
(g) Special Flight Permit
doubler or skin near or at the same blade
station as the blade retention bolt hole (blade Special flight permits are prohibited. Airworthiness Directives; Airbus
station 28). Helicopters Deutschland GmbH
(h) Alternative Methods of Compliance
(iii) Visually inspect the exposed areas of Helicopters
(AMOCs)
each bond line at the edges of the lower grip
pad, upper and lower grip plates, and each (1) The Manager, Fort Worth Aircraft AGENCY: Federal Aviation
layered doubler (bond lines) on the upper Certification Office, FAA, may approve Administration (FAA), DOT.
and lower surfaces of each M/R blade for the AMOCs for this AD. Send your proposal to: ACTION: Notice of proposed rulemaking
entire length and chord width for an edge Charles Harrison, Project Manager, Fort (NPRM).
void, any corrosion, loose or damaged Worth Aircraft Certification Office, FAA,
adhesive squeeze-out, and an edge SUMMARY: We propose to adopt a new
10101 Hillwood Pkwy, Fort Worth, TX
delamination. Pay particular attention to any airworthiness directive (AD) for Airbus
crack in the paint finish that follows the 76177; telephone (817) 222–5140; email 7-
outline of a grip pad, grip plate, or doubler, AVS-ASW-170@faa.gov. Helicopters Deutschland GmbH (Airbus
and to any loose or damaged adhesive (2) For operations conducted under a 14 Helicopters) Model MBB–BK 117A–3,
squeeze-out, as these may be the indication CFR part 119 operating certificate or under MBB–BK 117A–4, MBB–BK 117B–1,
of an edge void. 14 CFR part 91, subpart K, we suggest that MBB–BK 117B–2, and MBB–BK 117C–
(2) If there is a crack, any corrosion, an you notify your principal inspector, or 1 helicopters. This proposed AD would
edge void, loose or damaged adhesive lacking a principal inspector, the manager of require removing adhesive seals from
squeeze-out, or an edge delamination during the local flight standards district office or the exterior and interior door jettisoning
any inspection in paragraph (f)(1) of this AD, certificate holding district office before system on the left and right sliding
before further flight, do the following: operating any aircraft complying with this doors. This proposed AD is prompted
(i) If there is a crack in a grip pad or any
AD through an AMOC. by reports that the adhesive seal
grip plate or doubler, replace the M/R blade
with an airworthy M/R blade. (i) Additional Information
prevented the doors from jettisoning
(ii) If there is a crack in the M/R blade skin properly. The proposed actions are
Bell Helicopter Alert Service Bulletin intended to remove the adhesive seal to
that is within maximum repair damage
limits, repair the M/R blade. If the crack (ASB) No. UH–1H–13–09, dated January 14, allow the doors to jettison properly so
exceeds maximum repair damage limits, 2013, and ASB No. 204–75–1 and ASB No. occupants can exit the helicopter during
replace the M/R blade with an airworthy M/ 205–75–5, both Revision C and both dated an emergency.
R blade. April 25, 1979, which are not incorporated
DATES: We must receive comments on
(iii) If there is any corrosion within by reference, contain additional information
maximum repair damage limits, repair the M/ about the subject of this AD. For service this proposed AD by July 5, 2016.
R blade. If the corrosion exceeds maximum information identified in this AD, contact ADDRESSES: You may send comments by
repair damage limits, replace the M/R blade Bell Helicopter Textron, Inc., P.O. Box 482, any of the following methods:
with an airworthy M/R blade. Fort Worth, TX 76101; telephone (817) 280– • Federal eRulemaking Docket: Go to
(iv) If there is an edge void in the grip pad 3391; fax (817) 280–6466; or at http:// http://www.regulations.gov. Follow the
or in a grip plate or doubler, determine the online instructions for sending your
www.bellcustomer.com/files/. You may
length and depth using a feeler gauge. Repair
review the service information at the FAA, comments electronically.
the M/R blade if the edge void is within
maximum repair damage limits, or replace Office of the Regional Counsel, Southwest • Fax: 202–493–2251.
the M/R blade with an airworthy M/R blade. Region, 10101 Hillwood Pkwy, Room 6N– • Mail: Send comments to the U.S.
(v) If there is an edge void in a grip plate 321, Fort Worth, TX 76177. Department of Transportation, Docket
or doubler near the outboard tip, tap inspect Operations, M–30, West Building
(j) Subject
the affected area to determine the size and Ground Floor, Room W12–140, 1200
shape of the void. Repair the M/R blade if the Joint Aircraft Service Component (JASC) New Jersey Avenue SE., Washington,
edge void is within maximum repair damage Code: 6210, Main Rotor Blades. DC 20590–0001.
limits, or replace the M/R blade with an • Hand Delivery: Deliver to the
Issued in Fort Worth, Texas, on April 15,
airworthy M/R blade.
2016. ‘‘Mail’’ address between 9 a.m. and 5
(vi) If there is any loose or damaged
adhesive squeeze-out along any of the bond Scott A. Horn, p.m., Monday through Friday, except
lines, trim or scrape away the adhesive Federal holidays.
Acting Manager, Rotorcraft Directorate,
without damaging the adjacent surfaces or Aircraft Certification Service. Examining the AD Docket
parent material of the M/R blade. Determine
[FR Doc. 2016–10523 Filed 5–4–16; 8:45 am] You may examine the AD docket on
if there is an edge void or any corrosion by
lightly sanding the trimmed area smooth BILLING CODE 4910–13–P the Internet at http://
using 280 or finer grit paper. If there is no www.regulations.gov by searching for
edge void or corrosion, refinish the sanded and locating Docket No. FAA–2015–
ehiers on DSK5VPTVN1PROD with PROPOSALS
area. 3941; or in person at the Docket
(vii) If there is an edge delamination along
Operations Office between 9 a.m. and 5
any of the bond lines or a crack in the paint
finish, determine if there is an edge void or p.m., Monday through Friday, except
a crack in the grip pad, grip plate, doubler, Federal holidays. The AD docket
or skin by removing paint from the affected contains this proposed AD, the
area by lightly sanding in a span-wise European Aviation Safety Agency
direction using 180–220 grit paper. If there (EASA) AD, the economic evaluation,
VerDate Sep<11>2014 14:43 May 04, 2016 Jkt 238001 PO 00000 Frm 00009 Fmt 4702 Sfmt 4702 E:\FR\FM\05MYP1.SGM 05MYP1](https://thefederalregister.org/doc/81_FR_27144/page/1.svg)
![Federal Register / Vol. 81, No. 87 / Thursday, May 5, 2016 / Proposed Rules 27059
3. Will not affect intrastate aviation in BK117–20A–114, Revision 1, dated July 30, including an award of benefits based on
Alaska to the extent that it justifies 2015. a finding that the individual’s mental
making a regulatory distinction; and (2) After the effective date of this AD, do impairment meets or medically equals
4. Will not have a significant not install adhesive seal P/N 117–800201.01
the requirements of section 12.00 of the
on any helicopter sliding door.
economic impact, positive or negative, Listing of Impairments (Listings) and
on a substantial number of small entities (f) Alternative Methods of Compliance receipt of benefits through a
under the criteria of the Regulatory (AMOCs) representative payee. We propose to
Flexibility Act. (1) The Manager, Safety Management provide pertinent information about
We prepared an economic evaluation Group, FAA, may approve AMOCs for this these individuals to the Attorney
of the estimated costs to comply with AD. Send your proposal to: Matt Fuller, General on not less than a quarterly
this proposed AD and placed it in the Senior Aviation Safety Engineer, Safety basis. As required by the NIAA, at the
AD docket. Management Group, Rotorcraft Directorate,
FAA, 10101 Hillwood Pkwy., Fort Worth, TX commencement of the adjudication
List of Subjects in 14 CFR Part 39 76177; telephone (817) 222–5110; email 9- process we would also notify
ASW-FTW-AMOC-Requests@faa.gov. individuals, both orally and in writing,
Air transportation, Aircraft, Aviation (2) For operations conducted under a 14 of their possible Federal prohibition on
safety, Incorporation by reference, CFR part 119 operating certificate or under possessing or receiving firearms, the
Safety. 14 CFR part 91, subpart K, we suggest that consequences of such inclusion, the
you notify your principal inspector, or criminal penalties for violating the Gun
The Proposed Amendment lacking a principal inspector, the manager of Control Act, and the availability of relief
Accordingly, under the authority the local flight standards district office or
certificate holding district office before from the prohibitions imposed by
delegated to me by the Administrator,
operating any aircraft complying with this Federal law. Finally, we also propose to
the FAA proposes to amend 14 CFR part
AD through an AMOC. establish a program that permits
39 as follows:
individuals to request relief from the
(g) Additional Information
PART 39—AIRWORTHINESS Federal firearms prohibitions based on
The subject of this AD is addressed in our adjudication. The proposed rule
DIRECTIVES European Aviation Safety Agency (EASA) AD would allow us to fulfill responsibilities
No. 2015–0163, dated August 6, 2015. You
■ 1. The authority citation for part 39 may view the EASA AD on the Internet at
that we have under the NIAA.
continues to read as follows: http://www.regulations.gov in the AD Docket. DATES: To ensure that your comments
Authority: 49 U.S.C. 106(g), 40113, 44701. are considered, we must receive them
(h) Subject
no later than July 5, 2016.
§ 39.13 [Amended] Joint Aircraft Service Component (JASC) ADDRESSES: You may submit comments
■ 2. The FAA amends § 39.13 by adding Code: 5220, Emergency Exits.
by any one of three methods—Internet,
the following new airworthiness Issued in Fort Worth, Texas, on April 19, fax, or mail. Do not submit the same
directive (AD): 2016. comment multiple times or by more
Airbus Helicopters Deutschland GmbH: Scott A. Horn, than one method. Regardless of which
Docket No. FAA–2015–3941; Directorate Acting Manager, Rotorcraft Directorate, method you choose, please state that
Identifier 2015–SW–052–AD. Aircraft Certification Service. your comments refer to Docket No.
(a) Applicability [FR Doc. 2016–10285 Filed 5–4–16; 8:45 am] SSA–2016–0011 so that we may
BILLING CODE 4910–13–P associate your comments with the
This AD applies to Airbus Helicopters
Deutschland GmbH (Airbus Helicopters) correct regulation.
Model MBB–BK 117A–3, MBB–BK 117A–4, Caution: You should be careful to
MBB–BK 117B–1, MBB–BK 117B–2, and SOCIAL SECURITY ADMINISTRATION include in your comments only
MBB–BK 117C–1 helicopters with an information that you wish to make
adhesive seal part number (P/N) 117– 20 CFR Part 421 publicly available. We strongly urge you
800201.01 installed on an exterior or interior not to include in your comments any
[Docket No. SSA–2016–0011]
sliding door, certificated in any category. personal information, such as Social
(b) Unsafe Condition RIN 0960–AH95 Security numbers or medical
This AD defines the unsafe condition the
information.
Implementation of the NICS 1. Internet: We strongly recommend
presence of sealant on a sliding door (door). Improvement Amendments Act of 2007
This condition could result in the door that you submit your comments via the
failing to jettison, preventing helicopter AGENCY: Social Security Administration. Internet. Please visit the Federal
occupants from exiting the helicopter during ACTION: Notice of proposed rulemaking. eRulemaking portal at http://
an emergency. www.regulations.gov. Use the ‘‘Search’’
(c) Comments Due Date
SUMMARY: We propose to implement function to find docket number SSA–
provisions of the NICS Improvement 2016–0011. The system will issue a
We must receive comments by July 5, 2016. Amendments Act of 2007 (NIAA) that tracking number to confirm your
(d) Compliance require Federal agencies to provide submission. You will not be able to
You are responsible for performing each relevant records to the Attorney General view your comment immediately
action required by this AD within the for inclusion in the National Instant because we must post each comment
specified compliance time unless it has Criminal Background Check System manually. It may take up to a week or
already been accomplished prior to that time. (NICS). Under the proposed rule, we
ehiers on DSK5VPTVN1PROD with PROPOSALS
more for your comment to be viewable.
(e) Required Actions would identify, on a prospective basis, 2. Fax: Fax comments to (410) 966–
individuals who receive Disability 2830.
(1) Within 25 hours time-in-service,
remove adhesive seal P/N 117–800201.01
Insurance benefits under title II of the 3. Mail: Mail your comments to NICS
from the interior and exterior of each door. Social Security Act (Act) or Comments, Social Security
The areas where the seal is installed are Supplemental Security Income (SSI) Administration, 3100 West High Rise
shown in Figure 1 and Figure 2 of Airbus payments under title XVI of the Act and Building, 6401 Security Boulevard,
Helicopters Alert Service Bulletin MBB– also meet certain other criteria, Baltimore, Maryland 21235–6401.
VerDate Sep<11>2014 14:43 May 04, 2016 Jkt 238001 PO 00000 Frm 00011 Fmt 4702 Sfmt 4702 E:\FR\FM\05MYP1.SGM 05MYP1](https://thefederalregister.org/doc/81_FR_27144/page/3.svg)
Document Created: 2016-05-05 01:15:56
Document Modified: 2016-05-05 01:15:56
| 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 5, 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 27057 | |
| 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