83 FR 19134 - Petition for Exemption; Summary of Petition Received; Rolls-Royce plc

DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration

Federal Register Volume 83, Issue 84 (May 1, 2018)

This notice contains a summary of a petition seeking relief from specified requirements of Federal Aviation Regulations. The purpose of this notice is to improve the public's awareness of, and participation in, the FAA's exemption process. Neither publication of this notice nor the inclusion or omission of information in the summary is intended to affect the legal status of the petition or its final disposition.

[Federal Register Volume 83, Number 84 (Tuesday, May 1, 2018)]
[Notices]
[Pages 19134-19135]
From the Federal Register Online  [www.thefederalregister.org]
[FR Doc No: 2018-09194]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

[Summary Notice No. PE-2018-22]


Petition for Exemption; Summary of Petition Received; Rolls-Royce 
plc

AGENCY: Federal Aviation Administration (FAA), Department of 
Transportation (DOT).

ACTION: Notice of petition for exemption received.

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SUMMARY: This notice contains a summary of a petition seeking relief 
from specified requirements of Federal Aviation Regulations. The 
purpose of this notice is to improve the public's awareness of, and 
participation in, the

[[Page 19135]]

FAA's exemption process. Neither publication of this notice nor the 
inclusion or omission of information in the summary is intended to 
affect the legal status of the petition or its final disposition.

DATES: Comments on this petition must identify the petition docket 
number and must be received on or before May 11, 2018.

ADDRESSES: Send comments identified by docket number FAA-2018-0143 
using any of the following methods:
     Federal eRulemaking Portal: Go to http://www.regulations.gov and follow the online instructions for sending your 
comments electronically.
     Mail: Send comments to Docket Operations, M-30; U.S. 
Department of Transportation (DOT), 1200 New Jersey Avenue SE, Room 
W12-140, West Building Ground Floor, Washington, DC 20590-0001.
     Hand Delivery or Courier: Take comments to Docket 
Operations in Room W12-140 of the West Building Ground Floor at 1200 
New Jersey Avenue SE, Washington, DC 20590-0001, between 9 a.m. and 5 
p.m., Monday through Friday, except Federal holidays.
     Fax: Fax comments to Docket Operations at (202) 493-2251.
    Privacy: In accordance with 5 U.S.C. 553(c), DOT solicits comments 
from the public to better inform its rulemaking process. DOT posts 
these comments, without edit, including any personal information the 
commenter provides, to http://www.regulations.gov, as described in the 
system of records notice (DOT/ALL-14 FDMS), which can be reviewed at 
http://www.dot.gov/privacy.
    Docket: Background documents or comments received may be read at 
http://www.regulations.gov at any time. Follow the online instructions 
for accessing the docket or go to the Docket Operations in Room W12-140 
of the West Building Ground Floor at 1200 New Jersey Avenue SE, 
Washington, DC 20590-0001, between 9 a.m. and 5 p.m., Monday through 
Friday, except Federal holidays.

FOR FURTHER INFORMATION CONTACT: Tara Fitzgerald, Federal Aviation 
Administration, Engine and Propeller Standards Branch, AIR-6A2. 1200 
District Avenue, Burlington, Massachusetts 01803-5529; (781) 238-7130; 
facsimile: (781) 238-7199; email: [email protected].

SUPPLEMENTARY INFORMATION: This notice is published pursuant to 14 CFR 
11.85.

    Issued in Burlington, Massachusetts, on April 24, 2018.
Robert J. Ganley,
Manager, Engine and Propeller Standards Branch, Aircraft Certification 
Service.

Petition for Exemption

    Docket No.: FAA-2018-0143.
    Petitioner: Rolls-Royce plc.
    Section(s) of 14 CFR Affected: Sec.  33.27(c)(2)(v) at amendment 
33-10.
    Description of Relief Sought: Rolls-Royce requests an exemption 
from 14 CFR 33.27(c)(2)(v) at amendment 33-10 for the Rolls-Royce Trent 
1000-A, 1000-C, 1000-D, 1000-E, 1000-G, and 1000-H engine models. 
Rolls-Royce seeks to exclude a failure of the HP shaft system from 
consideration in determining 105 percent of the highest overspeed that 
would result from a complete loss of load on the HP turbine.

[FR Doc. 2018-09194 Filed 4-30-18; 8:45 am]
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