[Federal Register Volume 84, Number 154 (Friday, August 9, 2019)]
[Rules and Regulations]
[Page 39175]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2019-17013]



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 Rules and Regulations
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 This section of the FEDERAL REGISTER contains regulatory documents 
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 to and codified in the Code of Federal Regulations, which is published 
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  Federal Register / Vol. 84, No. 154 / Friday, August 9, 2019 / Rules 
and Regulations  

[[Page 39175]]



DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 21

[Docket No. FAA-2019-0280]


Primary Category Design Standards; Cub Crafters, Inc., Model 
CC21-180 Airplane

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Issuance of final airworthiness design standards.

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SUMMARY: These airworthiness design standards are issued to Cub 
Crafters, Inc., for type certification of the Model CC21-180 airplane 
under the regulations for primary category aircraft.

DATES: These airworthiness design standards are effective September 9, 
2019.

FOR FURTHER INFORMATION CONTACT: Mr. Raymond N. Johnston, AIR-692, 
Federal Aviation Administration, Policy & Innovation Division, Small 
Airplane Standards Branch, 901 Locust, Room 301, Kansas City, MO 64106, 
telephone (816) 329-4159, FAX (816) 329-4090, email 
[email protected].

SUPPLEMENTARY INFORMATION: Any person may obtain a copy of this 
information by contacting the person named above under FOR FURTHER 
INFORMATION CONTACT.

Background

    The ``primary'' category for aircraft was created specifically for 
the simple, low performance personal aircraft. Section 21.17, 
Designation of applicable regulations, paragraph (f) provides a means 
for the FAA to determine appropriate airworthiness standards for the 
particular primary category aircraft. The FAA procedure establishing 
appropriate airworthiness standards includes reviewing and possibly 
revising an applicant's proposal, publication of the submittal in the 
Federal Register for public review and comment, and addressing the 
comments. After all necessary revisions, the standards are published as 
approved FAA airworthiness standards. This document prescribes 
airworthiness standards for the issuance of a type certificate for the 
Cub Crafters, Inc., Model CC21-180, a primary category airplane. These 
airworthiness standards have a long safe service history in similar 
airplanes; therefore, they provide an appropriate level of safety. 
These airworthiness standards are based on standards that were used to 
certificate the same design as a normal and utility category airplane, 
Cub Crafters Model CC19-180, in accordance with FAA Type Certiciate 
A00053SE.\1\
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    \1\ See http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/CACFCFE4D1346CEB862582D300654D21?OpenDocument&Highlight=a00053se.
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Comments

    Proposed Primary Category Design Standards; Cub Crafters, Inc., 
Model CC21-180 Airplane was published in the Federal Register on April 
17, 2019 (84 FR 15992). No comments were received, and the 
airworthiness design standards are adopted as proposed.

Applicability

    These airworthiness design standards under the primary category 
rule are applicable to the Cub Crafters, Inc., Model CC21-180 airplane. 
Should Cub Crafters, Inc. wish to apply these airworthiness design 
standards to other airplane models, it must submit a new airworthiness 
design standard application under the primary rule category.

Conclusion

    This action affects only certain airworthiness design standards on 
the Cub Crafters, Inc., Model CC21-180 airplane. It is not a standard 
of general applicability and it affects only the applicant who applied 
to the FAA for approval of these features on the rotorcraft.

Citation

    The authority citation for these airworthiness standards is as 
follows:

    Authority:  49 U.S.C. 106(g), 40113 and 44701.

Final Airworthiness Standards for Type Certification in the Primary 
Category

    For the airplane:
    Title 14, Code of Federal Regulations (14 CFR) part 23, effective 
December 18, 1964, as amended by 23-1 through 23-62, all sections 
except Sec.  23.562 Emergency Landing Dynamic Conditions, and as 
modified by the following:
    Equivalent Level of Safety (ELOS) No. TC10279SE-A-C-1 for the 
emergency exit requirements of Sec.  23.807 \2\
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    \2\ See http://rgl.faa.gov/Regulatory_ and_Guidance_Library/
rgELOS.nsf/0/
F3FC2C42E551237F86257FC60046467D?OpenDocument&Highlight=tc10279se-a-
c-1.
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    ELOS No. AT12936SE-A-S-1 for the electronic display instrument 
system requirements of Sec.  23.1311 \3\
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    \3\ See http://rgl.faa.gov/Regulatory_ and _Guidance_Library/
rgELOS.nsf/0/E441A4F21736F7E98625814500674B2A?OpenDocument.
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    ELOS No. TC10279SE-A-G-9 for corrections to technical errors in 
amendment 23-62 \4\
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    \4\ See http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgELOS.nsf/0/773696FE2DDEA61D86257FF50065B4B6?OpenDocument.
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    ELOS No. AT12949SE-A-F-1 for the longitudinal trim requirements of 
Sec.  23.161 \5\
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    \5\ See http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgELOS.nsf/0/0D9E358153C4CF028625825D005E5D15?OpenDocument.
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    For noise standards:
    14 CFR part 36 as amended by 36-1 through 36-30, appendix G.

    Issued in Kansas City, Missouri on August 1, 2019.
Pat Mullen,
Manager, Small Airplane Standards Branch, Policy and Innovation 
Division, Aircraft Certification Service.
[FR Doc. 2019-17013 Filed 8-8-19; 8:45 am]
 BILLING CODE 4910-13-P