[Federal Register: April 18, 2001 (Volume 66, Number 75)]
[Notices]
[Page 20022-20023]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr18ap01-110]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
[Summary Notice No. PE-2001-30]
Petitions for Exemption, Summary of Petitions Received;
Dispositions of Petitions Issued
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of dispositions of prior petitions.
-----------------------------------------------------------------------
SUMMARY: Pursuant to FAA's rulemaking provisions governing the
application, processing, and disposition of petitions for exemption
part 11 of Title 14, Code of Federal Regulations (14 CFR), this notice
contains a summary of certain dispositions of certain petitions
previously received, and corrections. 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 any petition or its final disposition.
FOR FURTHER INFORMATION CONTACT: Forest Rawls (202) 267-8033, or
Vanessa Wilkins (202) 267-8029 Office of Rulemaking (ARM-1), Federal
Aviation Administration, 800 Independence Avenue, SW., Washington, DC
20591.
This notice is published pursuant to Secs. 11.85 and 11.91.
Issued in Washington, DC, on March 16, 2001.
Donald P. Byrne,
Assistant Chief Counsel for Regulations.
Dispositions of Petitions
Docket No.: 29893.
Petitioner: The Boeing Company.
Section of the 14 CFR Affected: 14 CFR Sec. 25.335(e)(3).
Description of Relief Sought/Disposition: To allow Boeing (1)
design flap speeds, VF, to be calculated based on a power-on
stall speed with the critical engine inoperative and the operative
engines at the power setting appropriate for the flight condition, and
(2) design flap speed, VF, to be calculated using a
multiplying factor of 1.6 (rather than 1.8) applied to the power-on
stall speed, for the full flap configuration of the airplane only.
Grant, 03/27/2001, Exemption No. 7476
Docket No.: FAA-2001-9032 (formerly Docket No. 28787).
Petitioner: Ameriflight, Inc.
Section of the 14 CFR Affected: 14 CFR Secs. 61.3(a) and (c),
91.203(a) and (b), 121.153(a)(1) and 121.383(a)(2)
Description of Relief Sought/Disposition: To permit Ameriflight,
Inc. to operate temporarily its airplanes under parts 121 and 135
without (1) those aircraft's airworthiness and registration
certificates onboard (and properly displayed in the case of
airworthiness certificates) while obtaining replacements, and (2)
without the affected pilots having their pilot and medical certificates
in their personal possession. Grant, 03/30/2001, Exemption No. 7143A
Docket No.: FAA-2000-8436 (formerly Docket No. 10633).
Petitioner: FAA Technical Center.
Section of the 14 CFR Affected: 14 CFR Secs. 91.117(a), 91.119(c)
91.159(a), and 91.303(e)
Description of Relief Sought/Disposition: To permit the FAA
Technical Center to conduct flight operations in support of its
research and
[[Page 20023]]
development projects without meeting certain FAA Regulations governing
aircraft speed, minimum safe altitudes, cruising altitudes for flights
conducted under visual flight rules, and aerobatic flight. Grant, 04/
03/2001, Exemption No. 6883A
[FR Doc. 01-9604 Filed 4-17-01; 8:45 am]
BILLING CODE 4910-13-M