
[Federal Register: June 15, 2009 (Volume 74, Number 113)]
[Notices]               
[Page 28322]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr15jn09-154]                         

-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

[Summary Notice No. PE-2009-21]

 
Petition for Exemption; Summary of Petition Received

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of petition for exemption received.

-----------------------------------------------------------------------

SUMMARY: This notice contains a summary of a petition seeking relief 
from specified requirements of 14 CFR. The purpose of this notice is to 
improve the public's awareness of, and participation in, this aspect of 
FAA's regulatory activities. 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 involved and must be received on or before July 6, 2009.

ADDRESSES: You may send comments identified by Docket Number FAA-2009-
0320 using any of the following methods:
     Government-wide rulemaking Web site: Go to http://
www.regulations.gov and follow the instructions for sending your 
comments electronically.
     Mail: Send comments to the Docket Management Facility; 
U.S. Department of Transportation (DOT), 1200 New Jersey Avenue, SE., 
West Building Ground Floor, Room W12-140, Washington, DC 20590.
     Fax: Fax comments to the Docket Management Facility at 
202-493-2251.
     Hand Delivery: Bring comments to the Docket Management 
Facility in Room W12-140 of the West Building Ground Floor at 1200 New 
Jersey Avenue, SE., Washington, DC, between 9 a.m. and 5 p.m., Monday 
through Friday, except Federal holidays.

Privacy: We will post all comments we receive, without change, to 
http://www.regulations.gov, including any personal information you 
provide. Using the search function of our docket Web site, anyone can 
find and read the comments received into any of our dockets, including 
the name of the individual sending the comment (or signing the comment 
for an association, business, labor union, etc.). You may review DOT's 
complete Privacy Act Statement in the Federal Register published on 
April 11, 2000 (65 FR 19477-78).
    Docket: To read background documents or comments received, go to 
http://www.regulations.gov at any time or to the Docket Management 
Facility in Room W12-140 of the West Building Ground Floor at 1200 New 
Jersey Avenue, SE., Washington, DC, between 9 a.m. and 5 p.m., Monday 
through Friday, except Federal holidays.

FOR FURTHER INFORMATION CONTACT: Maria G. Delgado, ANM-113, (425) 227-
2775, FAA, Transport Airplane Directorate, 1601 Lind Ave., SW., Renton, 
Washington 98057-3356; or Ralen Gao, ARM-200, (202) 267-3168, FAA, 
Office of Rulemaking, 800 Independence Ave., SW., Washington, DC 20591.
    This notice is published pursuant to 14 CFR 11.85.

    Issued in Washington, DC, on June 9, 2009.
Pamela Hamilton-Powell,
Director, Office of Rulemaking.

Petition for Exemption

    Docket No.: FAA-2009-0320.
    Petitioner: The Boeing Company.
    Sections of 14 CFR Affected: Sec. Sec.  25.301, 25.303, 25.305, 
25.307, 25.601, 25.603, 25.613, 25.901(b)(2), 25.901(c), 25.1103(d), 
25.1191, and 25.1301(d).
    Description of Relief Sought: The petitioner requests an exemption 
from the requirements for the thrust reverser inner wall structure and 
operating temperatures, and from the requirements for addressing a 
pneumatic duct failure condition. The exemption would apply to certain 
Boeing Model 777-200 and -300 series airplanes equipped with Rolls-
Royce RB211 Trent 800 series turbofan engines. The exemption, if 
granted, would be time-limited to permit the incorporation of 
incremental design improvements to the thrust reverser and engine as 
they become available, in order to reduce the risk of a hazardous 
thrust reverser inner wall failure.

[FR Doc. E9-13930 Filed 6-12-09; 8:45 am]

BILLING CODE 4910-13-P
