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Federal Register / Vol. 86, No. 136 / Tuesday, July 20, 2021 / Rules and Regulations installation within 550 hours TIS after accomplishment of the measurement specified in paragraph 3.1. of DGAC AD
2001061053A and DGAC AD 2001283
025A.
5 Where the service information referred to in DGAC AD 2001061053A and DGAC
AD 2001283025A specifies to perform a dye penetrant crack inspection if in doubt, this AD requires performing a dye penetrant inspection.
6 Where paragraph 3.2.2. of DGAC AD
2001061053A and DGAC AD 2001283
025A specifies to do various actions specified in paragraphs 3.2.2.a, b, and c of those ADs, for this AD, if any frame is cracked, before further flight, repair the frame. Acceptable U.S. alternatives to the fasteners and materials needed to perform repairs or modifications are listed in American Eurocopter Engineering Report No.
AEC/03RE005, Addendum ASB 53.00.42
and 53.00.43 AS365, dated January 29, 2003.
7 Where the Note in paragraph 3.2.2. of DGAC AD 2001061053A and DGAC AD
2001283025A specifies the instructions are no longer applicable after a customized repair has been carried out, for this AD, modifying or repairing the frame constitutes terminating action for the requirements of this AD.
i Special Flight Permit Special flight permits, as described in 14
CFR 21.197 and 21.199, are prohibited.
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, or lacking a principal inspector, the manager of the local flight standards district office/
certificate holding district office.

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k Related Information For more information about this AD, contact Blaine Williams, Aerospace Engineer, Cabin Safety & Environmental Systems Section, Los Angeles ACO Branch, Compliance & Airworthiness Division, 3960
Paramount Blvd., Lakewood, CA 90712;
telephone 5626275371; email blaine.williams@faa.gov.
l Material Incorporated by Reference 1 The Director of the Federal Register approved the incorporation by reference 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 the AD specifies otherwise.

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i Direction Generale de lAviation Civile DGAC AD 2001061053A, dated February 21, 2001.
ii DGAC AD 2001283025A, dated July 11, 2001.
iii American Eurocopter Engineering Report No. AEC/03RE005, Addendum ASB 53.00.42 and 53.00.43 AS365, dated January 29, 2003.
3 For DGAC AD 2001061053A and DGAC AD 2001283025A, contact the European Union Aviation Safety Agency 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 these DGAC ADs on the EASA website at https
ad.easa.europa.eu.
4 For American Eurocopter material identified in this AD, contact Airbus Helicopters, 2701 N Forum Drive, Grand Prairie, TX 75052; telephone 9726410000
or 8002320323; fax 9726413775; or at https www.airbus.com/helicopters/services/
technical-support.html.
5 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 817 2225110.
6 You may view this service information that is incorporated by reference at the National Archives and Records Administration NARA. For information on the availability of this material at NARA, email: fedreg.legal@nara.gov, or go to:
https www.archives.gov/federal-register/cfr/
ibr-locations.html.
Issued on July 2, 2021.
Ross Landes, Deputy Director for Regulatory Operations, Compliance & Airworthiness Division, Aircraft Certification Service.
FR Doc. 202115302 Filed 71921; 8:45 am
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration 14 CFR Part 39
Docket No. FAA20210031; Project Identifier MCAI202001420T; Amendment 3921625; AD 20211320
RIN 2120AA64

Airworthiness Directives; Airbus Canada Limited Partnership Type Certificate Previously Held by C Series Aircraft Limited Partnership CSALP;
Bombardier, Inc. Airplanes Federal Aviation Administration FAA, Department of Transportation DOT.
ACTION: Final rule.
AGENCY:

The FAA is adopting a new airworthiness directive AD for certain Airbus Canada Limited Partnership
SUMMARY:

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Model BD5001A10 and BD500
1A11 airplanes. This AD was prompted by reports of corrosion on the waste box, waste access doubler, and waste service door of the rear fuselage due to contamination from waste valve leakage.
This AD requires an inspection for corrosion of the waste box, waste access doubler, and waste service door, and corrective actions if necessary, as specified in a Transport Canada Civil Aviation TCCA AD, which is incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products.
This AD is effective August 24, 2021.
The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD
as of August 24, 2021.

DATES:

For material incorporated by reference IBR in this AD, contact TCCA, Transport Canada National Aircraft Certification, 159 Cleopatra Drive, Nepean, Ontario, K1A 0N5, Canada; telephone 8886633639; email AD-CN@tc.gc.ca; internet https
tc.canada.ca/en/aviation. You may view this IBR material at the FAA, Airworthiness Products Section, Operational Safety Branch, 2200 South 216th St., Des Moines, WA. For information on the availability of this material at the FAA, call 2062313195.
It is also available in the AD docket on the internet at https
www.regulations.gov by searching for and locating Docket No. FAA2021
0031.

ADDRESSES:

Examining the AD Docket
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You may examine the AD docket on the internet at https
www.regulations.gov by searching for and locating Docket No. FAA2021
0031; 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, 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:

Siddeeq Bacchus, Aerospace Engineer, Mechanical Systems and Administrative Services Section, FAA, New York ACO
Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 5162287362; fax 5167945531; email 9-avs-nyaco-cos@faa.gov.
SUPPLEMENTARY INFORMATION:

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