Voglio sapere a riguardo di…

Federal Register / Vol. 86, No. 187 / Thursday, September 30, 2021 / Rules and Regulations hoist control installed, before each hoist operation after December 16, 2020 the effective date of AD 20202403, accomplish a ground test of the UP/DOWN
switches for proper function. If there is any uncommanded hoist action, before further flight, remove the DUNLOP cyclic stick grip from service. Accomplishing the modification in paragraph 2 of EASA AD
20210023 constitutes terminating action for the requirements of this paragraph.
2 Except as specified in paragraph h of this AD: Comply with all required actions and compliance times specified in, and in accordance with, EASA AD 20210023.
h Exceptions to EASA AD 20210023
1 Where EASA AD 20210023 refers to October 8, 2020 the effective date of EASA
Emergency AD 20200217E, dated October 6, 2020 EASA AD 20200217E, this AD requires using the effective date of this AD.
2 Where the service information referenced in paragraph 1 of EASA AD
20210023 specifies that the work must be performed on the helicopter by the operator, this AD requires that the work be accomplished by a mechanic that meets the requirements of 14 CFR part 65 subpart D.
3 Where EASA AD 20210023 refers to its effective date, this AD requires using the effective date of this AD.
4 Where EASA AD 20210023 refers to flight hours FH, this AD requires using hours time-in-service.
5 Where the service information referenced in EASA AD 20210023 specifies to discard certain placards and Flight Manual pages that were required by EASA AD 2020
0217E, this AD requires removing them.
6 Where paragraph 3 of EASA AD 2021
0023 specifies to inform all flight crews and, thereafter, operate the helicopter accordingly, this AD does not require those actions.
7 Where paragraph 4 of EASA AD 2021
0023 allows modifying a Group 2 helicopter into a Group 1 helicopter, this AD also requires accomplishing the requirements of paragraph g1 of this AD.
8 The Remarks section of EASA AD
20210023 does not apply to this AD.

LOTTER on DSK11XQN23PROD with RULES1

i No Reporting Requirement Where the service information referenced in EASA AD 20210023 specifies to submit certain information to the manufacturer, this AD does not include that requirement.
j Alternative Methods of Compliance AMOCs 1 The Manager, International Validation Branch, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the manager of the International Validation Branch, send it to the attention of the person identified in paragraph k of this AD.
Information may be emailed to: 9-AVS-AIR730-AMOC@faa.gov.
2 Before using any approved AMOC, notify your appropriate principal inspector,
VerDate Sep<11>2014

17:35 Sep 29, 2021

Jkt 253001

or lacking a principal inspector, the manager of the local flight standards district office/
certificate holding district office.
k Related Information For more information about this AD, contact Daniel Poblete, Aerospace Engineer, Systems & Equipment Section, Los Angeles ACO Branch, Compliance & Airworthiness Division, 3960 Paramount Blvd., Lakewood, CA 90712; telephone 562 6275335; email daniel.d.poblete@faa.gov.
l Material Incorporated by Reference 1 The Director of the Federal Register approved the incorporation by reference IBR of the service information listed in this paragraph under 5 U.S.C. 552a and 1 CFR
part 51.
2 You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
i European Union Aviation Safety Agency EASA AD 20210023, dated January 19, 2021.
ii Reserved 3 For EASA AD 20210023, contact the EASA, Konrad-Adenauer-Ufer 3, 50668
Cologne, Germany; telephone +49 221 8999
000; email ADs@easa.europa.eu; internet www.easa.europa.eu. You may find this EASA AD on the EASA website at https
ad.easa.europa.eu.
4 You may view this service information at the FAA, Office of the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N321, Fort Worth, TX 76177. For information on the availability of this material at the FAA, call 8172225110. This material may be found in the AD docket at https www.regulations.gov by searching for and locating Docket No. FAA20210559.
5 You may view this material that is incorporated by reference at the National Archives and Records Administration NARA. For information on the availability of this material at NARA, email fr.inspection@nara.gov, or go to: https
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued on September 7, 2021.
Ross Landes, Deputy Director for Regulatory Operations, Compliance & Airworthiness Division, Aircraft Certification Service.
FR Doc. 202121117 Filed 92921; 8:45 am BILLING CODE 491013P

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration 14 CFR Part 39
Docket No. FAA20210212; Project Identifier 2018CE032AD; Amendment 3921715; AD 20211814
RIN 2120AA64

Airworthiness Directives; DG
Flugzeugbau GmbH Gliders Federal Aviation Administration FAA, DOT.

AGENCY:

PO 00000

Frm 00009

Fmt 4700

Sfmt 4700

ACTION:

54037

Final rule.

The FAA is adopting a new airworthiness directive AD for all DG
Flugzeugbau GmbH Models DG808C
and DG1000T gliders. This AD was prompted by mandatory continuing airworthiness information MCAI
originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI identifies the unsafe condition as damaged fuel hoses due to environmental and fatigue deterioration.
This AD requires inspecting the polyurethane PU fuel hoses, replacing the PU fuel hoses if there is damage, and establishing a life limit for the PU fuel hoses. The FAA is issuing this AD to address the unsafe condition on these products.

SUMMARY:

This AD is effective November 4, 2021.
The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD
as of November 4, 2021.
ADDRESSES: For service information identified in this final rule, contact DG
Flugzeugbau GmbH, Otto-Lilienthal Weg 2, D76646 Bruchsal, Germany;
phone: +49 07251 32020; email:
info@dg-flugzeugbau.de; website:
https www.dg-flugzeugbau.de/. You may view this service information at the FAA, Airworthiness Products Section, Operational Safety Branch, 901 Locust, Kansas City, MO 64106. For information on the availability of this material at the FAA, call 816 3294148. It is also available at https www.regulations.gov by searching for and locating Docket No.
FAA20210212.
DATES:

Examining the AD Docket You may examine the AD docket at https www.regulations.gov by searching for and locating Docket No.
FAA20210212; 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 final rule, the MCAI, any comments received, and other information. The address for Docket Operations is U.S.
Department of Transportation, Docket Operations, M30, West Building Ground Floor, Room W12140, 1200
New Jersey Avenue SE, Washington, DC
20590.
FOR FURTHER INFORMATION CONTACT: Jim Rutherford, Aviation Safety Engineer, General Aviation & Rotorcraft Section, International Validation Branch, FAA, 901 Locust, Room 301, Kansas City, MO
64106; phone: 816 3294165; fax: 816
3294090; email: jim.rutherford@
faa.gov.

E:FRFM30SER1.SGM

30SER1