[Federal Register: March 15, 2001 (Volume 66, Number 51)]
[Notices]
[Page 15162-15163]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr15mr01-120]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
[Policy Statement No. ANE-1998-33.69-R1]
Policy for Evaluating Ignitions System Requirements
AGENCY: Federal Aviation Administration, DOT
ACTION: Notice of availability, policy statement.
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SUMMARY: The Federal Aviation Administration (FAA) announced the
availability of policy for evaluating compliance with the airworthiness
certification standards for ignition systems on turbine powered
aircraft engines. This policy revises the previous policy to include
derivative engine models with significant service experience.
DATES: The FAA issued policy statement number ANE-1998-33.69-R1 on
February 26, 2001.
FOR FURTHER INFORMATION CONTACT: John Fisher, FAA, Engine and Propeller
Standards Staff, ANE-110, 12 New England Executive Park, Burlington, MA
[[Page 15163]]
01803; e-mail: john.fisher@faa.gov>; telephone: (781) 238-7149; fax:
(781) 238-7199. The policy statement is available on the Internet at
the following address: http://www.faa.gov/avr/air/ane/ane110/page.htm.
If you do not have access to the Internet, you may request a copy of
the policy by contacting the individual listed in this section.
SUPPLEMENTARY INFORMATION: The FAA published a notice in the Federal
Register on January 10, 2001 (66 FR 2043) to announce the availability
of the proposed policy and invite interested parties to comment. The
FAA did not receive any comments on the proposed policy before the
closing date of the comment period.
Background
This policy statement supersedes FAA policy statement number 1998-
33.69-R0, dated October 23, 1998. the intent of this policy is to
clarify the policy regarding Sec. 33.69 Title 14 of the Code of Federal
Regulations. This policy assists the Aircraft Certification Offices
(ACOs) in evaluating applications for aircraft engine type
certification. The FAA has revised this policy to include guidance for
evaluating derivative engine models with significant service
experience. This policy does not create any new requirements.
Authority: 49 U.S.C. 106(g), 40113, 44701-44702, 44704.
Issued in Burlington, Massachusetts, on March 2, 2001.
David A. Downey,
Assistant Manager, Engine and Propeller Directorate, Aircraft
Certification Service.
[FR Doc. 01-6376 Filed 3-14-01; 8:45 am]
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