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Federal Register / Vol. 86, No. 92 / Friday, May 14, 2021 / Rules and Regulations
Note 2 to paragraph h1: For obtaining the procedures for Bombardier Challenger 300 Airplane Flight Manual Imperial Version, Publication No. CSP 1001, use Document Identification No. CH 300
AFMI.
2 Challenger 300 Airplane Flight Manual Imperial Version, Publication No. CSP 100
1, Revision 61, dated September 25, 2020.
3 Challenger 300 Airplane Flight Manual Imperial Version, Publication No. CSP 100
1, Revision 62, dated December 22, 2020.
i Other FAA AD Provisions The following provisions also apply to this AD:
1 Alternative Methods of Compliance AMOCs: The Manager, New York ACO
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 responsible Flight Standards Office, as appropriate. If sending information directly to the manager of the certification office, send it to ATTN: Program Manager, Continuing Operational Safety, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 5162287300; fax 5167945531. Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the responsible Flight Standards Office.
2 Contacting the Manufacturer: For any requirement in this AD to obtain instructions from a manufacturer, the instructions must be accomplished using a method approved by the Manager, New York ACO Branch, FAA; or Transport Canada Civil Aviation TCCA; or Bombardier, Inc.s TCCA Design Approval Organization DAO. If approved by the DAO, the approval must include the DAO-authorized signature.

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j Related Information 1 Refer to Mandatory Continuing Airworthiness Information MCAI TCCA AD
CF202047, dated November 18, 2020, for related information. This MCAI may be found in the AD docket on the internet at https www.regulations.gov by searching for and locating Docket No. FAA20210342.
2 For more information about this AD, contact Jiwan Karunatilake, Aerospace Engineer, Airframe and Propulsion Section, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590;
telephone 5162287300; fax 5167945531;
email 9-avs-nyaco-cos@faa.gov.
3 Service information identified in this AD that is not incorporated by reference is available at the addresses specified in paragraphs k3 and 4 of this AD.
k 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 Section 0204, Systems Limitations, of Chapter 02, LIMITATIONS, of the
VerDate Sep<11>2014

16:17 May 13, 2021

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Bombardier Challenger 300 Airplane Flight Manual Imperial Version, Publication No.
CSP 1001, Revision 63, dated April 1, 2021.
ii Section 0403 of Chapter 04, NORMAL PROCEDURES, of the Bombardier Challenger 300 Airplane Flight Manual Imperial Version, Publication No.
CSP 1001, Revision 63, dated April 1, 2021.
3 For service information identified in this AD, contact Bombardier, Inc., 200 Cote Vertu Road West, Dorval, Quebec H4S 2A3, Canada; North America toll-free telephone 1
8665381247 or direct-dial telephone 1
5148552999; email ac.yul@
aero.bombardier.com; internet https
www.bombardier.com.
Note 2 to paragraph j3: For obtaining the procedures for Bombardier Challenger 300 Airplane Flight Manual Imperial Version, Publication No. CSP 1001, use Document Identification No. CH 300 AFM
I.
4 You may view this service information 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.
5 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/ibrlocations.html.
Issued on April 23, 2021.
Lance T. Gant, Director, Compliance & Airworthiness Division, Aircraft Certification Service.
FR Doc. 202110259 Filed 51121; 4:15 pm BILLING CODE 491013P

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration 14 CFR Part 39
Docket No. FAA20210341; Project Identifier AD202100325T; Amendment 3921529; AD 20210915
RIN 2120AA64

Airworthiness Directives; Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Airplanes Federal Aviation Administration FAA, DOT.
ACTION: Final rule; request for comments.
AGENCY:

The FAA is adopting a new airworthiness directive AD for all Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Model 382, 382B, 382E, 382F, and 382G
airplanes, type certificated in any category; and Model C130A, C130B, C130BL, C130E, C130H, C130H30,
SUMMARY:

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C130J, C130J30, EC130Q, HC
130H, KC130H, NC130B, NC130, and WC130H airplanes, type certificated in the restricted or amateur category. This AD was prompted by a crack found on the web attachment flange of the center wing upper forward corner fitting. This AD requires an eddy current surface scan for cracks of the center wing upper and lower forward corner fittings and fasteners, a torque check of the left and right outer-wingto-center-wing front-beam-web-jointsplice-angle fasteners, and repair, retorqueing, or replacement if necessary.
The FAA is issuing this AD to address the unsafe condition on these products.
DATES: This AD is effective June 1, 2021.
The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD
as of June 1, 2021.
The FAA must receive comments on this AD by June 28, 2021.
ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:
Federal eRulemaking Portal: Go to https www.regulations.gov. Follow the instructions for submitting comments.
Fax: 2024932251.
Mail: U.S. Department of Transportation, Docket Operations, M
30, West Building Ground Floor, Room W12140, 1200 New Jersey Avenue SE, Washington, DC 20590.
Hand Delivery: Deliver to Mail address above between 9 a.m. and 5
p.m., Monday through Friday, except Federal holidays.
For service information identified in this final rule, contact Lockheed Martin Corporation/Lockheed Martin Aeronautics Company, Customer Support Center, Dept. 3E1M, Zone 0591, 86 S Cobb Drive, Marietta, GA 30063;
telephone 7704949131; email hercules.support@lmco.com; internet https www.lockheedmartin.com. You may view this service information 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 at https
www.regulations.gov by searching for and locating Docket No. FAA2021
0341.
Examining the AD Docket You may examine the AD docket at https www.regulations.gov by searching for and locating Docket No.
FAA20210341; or in person at Docket Operations between 9 a.m. and 5 p.m., Monday through Friday, except Federal
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