[Federal Register Volume 70, Number 105 (Thursday, June 2, 2005)]
[Proposed Rules]
[Pages 32273-32275]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 05-10948]
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Proposed Rules
Federal Register
________________________________________________________________________
This section of the FEDERAL REGISTER contains notices to the public of
the proposed issuance of rules and regulations. The purpose of these
notices is to give interested persons an opportunity to participate in
the rule making prior to the adoption of the final rules.
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Federal Register / Vol. 70, No. 105 / Thursday, June 2, 2005 /
Proposed Rules
[[Page 32273]]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2005-21174; Directorate Identifier 2005-CE-23-AD]
RIN 2120-AA64
Airworthiness Directives; The New Piper Aircraft, Inc., Models
PA-28-160, PA-28-161, PA-28-180, and PA-28-181 Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
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SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD)
for certain The New Piper Aircraft, Inc. (Piper) Models PA-28-160, PA-
28-161, PA-28-180, and PA-28-181 airplanes that incorporate Petersen
Aviation, Inc. Supplemental Type Certificate (STC) SA2660CE installed
between April 20, 1998, and April 1, 2005, and incorporate Petersen
Aviation, Inc. Service Bulletin SB98-1. This proposed AD would require
you to replace the AN894-6-4 bushing screw thread expanders on the
gascolator and bushing attached to the inlet of the top fuel pump with
NAS1564-6-4J reducers and AN818-6 nuts. This proposed AD results from
reports of fuel leaks during the post STC installation tests. We are
issuing this proposed AD to prevent fuel fittings used in STC SA2660CE
from leaking fuel in the engine compartment, which could result in an
engine fire. This condition could lead to loss of control of the
airplane.
DATES: We must receive any comments on this proposed AD by August 1,
2005.
ADDRESSES: Use one of the following to submit comments on this proposed
AD:
DOT Docket Web site: Go to http://dms.dot.gov and follow
the instructions for sending your comments electronically.
Government-wide rulemaking web site: Go to http://www.regulations.gov and follow the instructions for sending your
comments electronically.
Mail: Docket Management Facility; U.S. Department of
Transportation, 400 Seventh Street, SW., Nassif Building, Room PL-401,
Washington, DC 20590-001.
Fax: 1-202-493-2251.
Hand Delivery: Room PL-401 on the plaza level of the
Nassif Building, 400 Seventh Street, SW., Washington, DC, between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
To get the service information identified in this proposed AD,
contact Petersen Aviation, Inc., 984 K Road, Minden, Nebraska 68959;
telephone: (308) 832-2050; facsimile: (308) 832-2311.
To view the comments on this proposed AD, go to http://dms.dot.gov.
The docket number is FAA-2005-21174; Directorate Identifier 2005-CE-23-
AD.
FOR FURTHER INFORMATION CONTACT: James P. Galstad, Aerospace Engineer,
FAA, Wichita ACO, 1801 Airport Road, Mid-Continent Airport, Wichita,
Kansas 67209; telephone: (316) 946-4135; facsimile: (316) 946-4107.
SUPPLEMENTARY INFORMATION:
Comments Invited
How do I comment on this proposed AD? We invite you to submit any
written relevant data, views, or arguments regarding this proposal.
Send your comments to an address listed under ADDRESSES. Include the
docket number, ``FAA-2005-21174; Directorate Identifier 2005-CE-23-AD''
at the beginning of your comments. We will post all comments we
receive, without change, to http://dms.dot.gov, including any personal
information you provide. We will also post a report summarizing each
substantive verbal contact with FAA personnel concerning this proposed
rulemaking. 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 who sent the comment (or signed
the comment on behalf of an association, business, labor union, etc.).
This is docket number FAA-2005-21174; Directorate Identifier 2005-CE-
23-AD. You may review the DOT's complete Privacy Act Statement in the
Federal Register published on April 11, 2000 (65 FR 19477-78) or you
may visit http://dms.dot.gov.
Are there any specific portions of this proposed AD I should pay
attention to? We specifically invite comments on the overall
regulatory, economic, environmental, and energy aspects of this
proposed AD. If you contact us through a nonwritten communication and
that contact relates to a substantive part of this proposed AD, we will
summarize the contact and place the summary in the docket. We will
consider all comments received by the closing date and may amend this
proposed AD in light of those comments and contacts.
Docket Information
Where can I go to view the docket information? You may view the AD
docket that contains the proposal, any comments received, and any final
disposition in person at the DMS Docket Offices between 9 a.m. and 5
p.m. (eastern standard time), Monday through Friday, except Federal
holidays. The Docket Office (telephone 1-800-647-5227) is located on
the plaza level of the Department of Transportation NASSIF Building at
the street address stated in ADDRESSES. You may also view the AD docket
on the Internet at http://dms.dot.gov. The comments will be available
in the AD docket shortly after the DMS receives them.
Discussion
What events have caused this proposed AD? We have received reports
of fuel leaks found during post fuel pump checks on Piper Models PA-28-
160, PA-28-161, PA-28-180, and PA-28-181 airplanes after STC SA2660CE
was incorporated.
STC SA2660CE enables the referenced airplanes to run on leaded and
unleaded automotive gasoline, 91 minimum antiknock index (RON+MON).
The STC replaces the Piper electric boost pump with two different
electric boost pumps. Subsequently, Petersen Aviation, Inc. Service
Bulletin 98-1 provides for installation of a fuel flow bypass that
incorporates an o-ring seal fuel fitting (AN894-6-4 bushing screw
thread expander) on the flared tube fitting (AN826-6 tee). The internal
shape of the AN894-6-4 bushing screw thread expander is intended to use
an o-ring seal, but there is no corresponding o-ring seal location on
the AN826-6 tee.
[[Page 32274]]
The AN894-6-4 bushing screw thread expander has clearance machining
cut for the mating screw threads but does not provide a seal against
the cone surface of the AN826-6 tee.
What is the potential impact if FAA took no action? If not
prevented, fuel fittings used in STC SA2660CE could leak fuel in the
engine compartment. Failure of these fittings could result in an engine
fire. This condition could lead to loss of control of the airplane.
Is there service information that applies to this subject? Petersen
Aviation, Inc. has issued Service Bulletin PA-28-160, -161, -180, -181,
Bulletin No. SB-05-2, dated April 12, 2005.
What are the provisions of this service information? The service
bulletin includes procedures for replacing the two AN894-6-4 bushing
screw thread expanders on the two AN826-6 tees with AN818-6 nuts and
NAS1564-6-4J reducers.
FAA's Determination and Requirements of This Proposed AD
What has FAA decided? We have evaluated all pertinent information
and identified an unsafe condition that is likely to exist or develop
on other products of this same type design. For this reason, we are
proposing AD action.
What would this proposed AD require? This proposed AD would require
you to incorporate the actions in the previously-referenced service
bulletin.
How does the revision to 14 CFR part 39 affect this proposed AD? On
July 10, 2002, we published a new version of 14 CFR part 39 (67 FR
47997, July 22, 2002), which governs FAA's AD system. This regulation
now includes material that relates to altered products, special flight
permits, and alternative methods of compliance. This material
previously was included in each individual AD. Since this material is
included in 14 CFR part 39, we will not include it in future AD
actions.
Costs of Compliance
How many airplanes would this proposed AD impact? We estimate that
this proposed AD affects 50 airplanes in the U.S. registry.
What would be the cost impact of this proposed AD on owners/
operators of the affected airplanes? We estimate the following costs to
accomplish this proposed modification:
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Total cost on U.S.
Labor cost Parts cost Total cost per airplane operators
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1 work hour x $65 per hour = $65..... Petersen Aviation will Peterson Aviation will Petersen Aviation will
provide parts at no cover the cost for cover the cost for
cost. labor. parts and labor.
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Authority for This Rulemaking
What authority does FAA have for issuing this proposed rulemaking
action? Title 49 of the United States Code specifies the FAA's
authority to issue rules on aviation safety. Subtitle I, Section 106
describes the authority of the FAA Administrator. Subtitle VII,
Aviation Programs, describes in more detail the scope of the agency's
authority.
We are issuing this proposed rulemaking under the authority
described in Subtitle VII, part A, subpart III, section 44701,
``General requirements.'' Under that section, Congress charges the FAA
with promoting safe flight of civil aircraft in air commerce by
prescribing regulations for practices, methods, and procedures the
Administrator finds necessary for safety in air commerce. This
regulation is within the scope of that authority because it addresses
an unsafe condition that is likely to exist or develop on products
identified in this proposed AD.
Regulatory Findings
Would this proposed AD impact various entities? We have determined
that this proposed AD would not have federalism implications under
Executive Order 13132. This proposed AD would not have a substantial
direct effect on the States, on the relationship between the national
Government and the States, or on the distribution of power and
responsibilities among the various levels of government.
Would this proposed AD involve a significant rule or regulatory
action? For the reasons discussed above, I certify that this proposed
AD:
1. Is not a ``significant regulatory action'' under Executive Order
12866;
2. Is not a ``significant rule'' under the DOT Regulatory Policies
and Procedures (44 FR 11034, February 26, 1979); and
3. Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
We prepared a summary of the costs to comply with this proposed AD
(and other information as included in the Regulatory Evaluation) and
placed it in the AD Docket. You may get a copy of this summary by
sending a request to us at the address listed under ADDRESSES. Include
``AD Docket FAA-2005-21174; Directorate Identifier 2005-CE-23-AD'' in
your request.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Safety.
The Proposed Amendment
Accordingly, under the authority delegated to me by the
Administrator, the Federal Aviation Administration proposes to amend 14
CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
2. The FAA amends Sec. 39.13 by adding the following new
airworthiness directive (AD):
The New Piper Aircraft, Inc.: Docket No. FAA-2005-21174; Directorate
Identifier 2005-CE-23-AD
When Is the Last Date I Can Submit Comments on This Proposed AD?
(a) We must receive comments on this proposed airworthiness
directive (AD) by August 1, 2005.
What Other ADs Are Affected by This Action?
(b) None.
What Airplanes Are Affected by This AD?
(c) This AD affects Model PA-28-160, PA-28-161, PA-28-180, and
PA-28-181 airplanes, serial numbers 28-671 through 28-5859, 28-
7105001 through 28-7505261, 28-7690001 through 28-8590001, and all
serial numbers thereafter, that:
(1) are certificated in any category;
(2) incorporate Peterson Aviation, Inc. Supplemental Type
Certificate (STC) SA2660CE installed between April 20, 1998 and
April 1, 2005; and
(3) incorporate Peterson Aviation, Inc. Service Bulletin SB98-1.
What Is the Unsafe Condition Presented in This AD?
(d) This AD is the result of reports of fuel leaks during the
post STC installation tests. The actions specified in this AD are
intended to prevent fuel fittings used in STC SA2660CE from leaking
fuel in the engine compartment, which could result in an engine
fire. This condition could lead to loss of control of the airplane.
[[Page 32275]]
What Must I Do To Address This Problem?
(e) To address this problem, you must do the following:
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Actions Compliance Procedures
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Replace the two AN894-6-4 At the next 100-hour Follow Petersen
bushing screw thread or annual Aviation, Inc.
expanders on the two AN826- inspection that Service Bulletin PA-
6 tees (one on the occurs following 30 28-160, -161, -180,
gascolator and the other days after the -181 Bulletin No.
one attached to a bushing effective date of SB 05-2, dated
(AN912-2J) attached to the this AD, whichever April 12, 2005.
inlet on the top of the top occurs first.
fuel pump) with NAS1564-6-
4J reducers and AN818-6
nuts.
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May I Request an Alternative Method of Compliance?
(f) You may request a different method of compliance or a
different compliance time for this AD by following the procedures in
14 CFR 39.19. Unless FAA authorizes otherwise, send your request to
your principal inspector. The principal inspector may add comments
and will send your request to the Manager, Wichita Aircraft
Certification Office (ACO), FAA. For information on any already
approved alternative methods of compliance, contact James P.
Galstad, Aerospace Engineer, FAA Wichita ACO, 1801 Airport Road,
Mid-Continent Airport, Wichita, Kansas 67209; telephone: (316) 946-
4135; facsimile: (316) 946-4107.
May I Get Copies of the Documents Referenced in This AD?
(g) To get copies of the documents referenced in this AD,
contact Petersen Aviation, Inc., 984 K Road, Minden, Nebraska 68959;
telephone: (308) 832-2050; facsimile: (308) 832-2311. To view the AD
docket, go to the Docket Management Facility; U.S. Department of
Transportation, 400 Seventh Street, SW., Nassif Building, Room PL-
401, Washington, DC, or on the Internet at http://dms.dot.gov. The
docket number is Docket No. FAA-2005-21174; Directorate Identifier
2005-CE-23-AD.
Issued in Kansas City, Missouri, on May 25, 2005.
David R. Showers,
Acting Manager, Small Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 05-10948 Filed 6-1-05; 8:45 am]
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