[Federal Register: March 30, 2006 (Volume 71, Number 61)]
[Rules and Regulations]
[Page 16027-16029]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr30mr06-6]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2005-23023; Directorate Identifier 2005-CE-49-AD;
Amendment 39-14533; AD 2006-07-06]
RIN 2120-AA64
Airworthiness Directives; Cirrus Design Corporation Models SR20
and SR22 Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
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SUMMARY: The FAA adopts a new airworthiness directive (AD) for certain
Cirrus Design Corporation (CDC) Models SR20 and SR22 airplanes. This AD
requires you to inspect the fuel line and wire bundles for any chafing
damage; replace any damaged fuel line and repair any damaged wires or
sheathing of the wire harness if any chafing damage is found; and
install (to prevent any chafing damage to the fuel line and wire
bundles) the forward loop clamp, fuel line shield, aft loop clamp, and
anti-chafe tubing. This AD results from reports of fuel line leaks
resulting from wire chafing on the fuel lines. We are issuing this AD
to detect, correct, and prevent damage to the fuel line and wire
bundles, which could result in fuel leaks. This failure could lead to
unsafe fuel vapor within the cockpit and possible fire.
DATES: This AD becomes effective on May 11, 2006.
As of May 11, 2006, the Director of the Federal Register approved
the incorporation by reference of certain publications listed in the
regulation.
ADDRESSES: To get the service information identified in this AD,
contact Cirrus Design Corporation, 4515 Taylor Circle, Duluth,
Minnesota 55811; telephone: (218) 727-2737, or on the Internet at
http://www.cirrusdesign.com.
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 20590-001 or on the Internet at http://dms.dot.gov.
The docket number is FAA-2005-23023; Directorate
Identifier 2005-CE-49-AD.
FOR FURTHER INFORMATION CONTACT: Wess Rouse, Aerospace Engineer, ACE-
117C, Chicago Aircraft Certification Office, 2300 East Devon Avenue,
Room 107, Des Plaines, Illinois 60018; telephone: (847) 294-8113;
facsimile: (847) 294-7834.
[[Page 16028]]
SUPPLEMENTARY INFORMATION:
Discussion
The FAA has received two reports of fuel line leaks within a
compartment in the center console of Model SR22 airplanes. This
compartment is drained to the belly of the aircraft. Investigation
found that the leaks resulted from wire chafing on the fuel lines.
This condition, if not corrected, could result in unsafe fuel vapor
within the cockpit and possible fire.
We issued a proposal to amend part 39 of the Federal Aviation
Regulations (14 CFR part 39) to include an AD that would apply to
certain Cirrus Design Corporation (CDC) Models SR20 and SR22 airplanes.
This proposal was published in the Federal Register as a notice of
proposed rulemaking (NPRM) on December 8, 2005 (70 FR 72945). The NPRM
proposed to require you to inspect the fuel line and wire bundles for
any chafing damage; replace any damaged fuel line and repair any
damaged wires or sheathing of the wire harness if any chafing damage is
found; and install the forward loop clamp, fuel line shield, aft loop
clamp, and anti-chafe tubing.
Comments
We provided the public the opportunity to participate in developing
this AD. The following presents the comment received on the proposal
and FAA's response to the comment:
Comment Issue: Revision Date for Cirrus Design Corporation Service
Bulletin
The commenter notes that throughout the NPRM the date of Service
Bulletin SB 2X-28-04 R1, Issued: November 1, 2005, Revised: November 8,
2005, should read, ``Revised: November 14, 2005.''
The FAA agrees with the commenter. We will change the final rule to
include the correct revised date for the service bulletin.
Conclusion
We have carefully reviewed the available data and determined that
air safety and the public interest require adopting the AD as proposed
except for minor editorial corrections. We have determined that these
minor corrections:
--Are consistent with the intent that was proposed in the NPRM for
correcting the unsafe condition; and
--Do not add any additional burden upon the public than was already
proposed in the NPRM.
Changes to 14 CFR Part 39--Effect on the AD
How does the revision to 14 CFR part 39 affect this AD? On July 10,
2002, the FAA published a new version of 14 CFR part 39 (67 FR 47997,
July 22, 2002), which governs the 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
We estimate that this AD affects 2,135 airplanes in the U.S.
registry.
We estimate the following costs to do the inspection of the fuel
line and wire harness for any chafing damage:
----------------------------------------------------------------------------------------------------------------
Total cost per
Labor cost Parts cost airplane Total cost on U.S. operators
----------------------------------------------------------------------------------------------------------------
1 work hour x $80 = $80........... Not Applicable...... $80 2,135 x $80 = $170,800
----------------------------------------------------------------------------------------------------------------
We estimate the following costs to do necessary replacements of any
damaged fuel line or repair any damaged wires or sheathing of the wire
harness that would be required based on the results of this inspection.
We have no way of determining the number of airplanes that may need
these repairs or replacements:
------------------------------------------------------------------------
Total cost per
Labor cost Parts cost airplane
------------------------------------------------------------------------
6 work hours x $80 = $480............... $67 $547
------------------------------------------------------------------------
We estimate the following costs to do the installation of the
forward loop clamp, fuel line shield, aft loop clamp, and anti-chafe
tubing:
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Total cost per
Labor cost Parts cost airplane Total cost on U.S. operators
----------------------------------------------------------------------------------------------------------------
1 work hour x $80 = $80.............. $146 $226 2,135 x $246 = $482,510
----------------------------------------------------------------------------------------------------------------
Warranty credit for parts and labor costs is referenced in the
service bulletin.
Authority for This Rulemaking
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 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 AD.
Regulatory Findings
We have determined that this AD will not have federalism
implications under Executive Order 13132. This AD will not have a
substantial direct effect on the States, on the relationship between
the national government and the States,
[[Page 16029]]
or on the distribution of power and responsibilities among the various
levels of government.
For the reasons discussed above, I certify that this 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 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 ``Docket
No. FAA-2005-23023; Directorate Identifier 2005-CE-49-AD'' in your
request.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Amendment
0
Accordingly, under the authority delegated to me by the Administrator,
the Federal Aviation Administration amends part 39 of the Federal
Aviation Regulations (14 CFR part 39) as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0
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]
0
2. FAA amends Sec. 39.13 by adding a new AD to read as follows:
2006-07-06 Cirrus Design Corporation: Amendment 39-14533; Docket No.
FAA-2005-23023; Directorate Identifier 2005-CE-49-AD.
Effective Date
(a) This AD becomes effective on May 11, 2006.
Affected ADs
(b) None.
Applicability
(c) This AD affects the following airplane models and serial
numbers that are certificated in any category:
------------------------------------------------------------------------
Model Serial Nos.
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SR20...................................... 1005 through 1581.
SR22...................................... 0002 through 1643 and 1645
through 1662.
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Unsafe Condition
(d) This AD is the result of reports of fuel line leaks
resulting from wire chafing on the fuel lines. The actions specified
in this AD are intended to detect, correct, and prevent damage to
the fuel line and wire bundles, which could result in fuel leaks.
This failure could lead to unsafe fuel vapor within the cockpit and
possible fire.
Compliance
(e) To address this problem, you must do the following:
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Actions Compliance Procedures
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(1) Inspect the fuel line Within the next 50 Follow Cirrus Design
and wire harness for any hours time-in- Corporation Service
chafing damage. service (TIS) after Bulletin SB 2X-28-
May 11, 2006 (the 04 R1, Issued:
effective date of November 1, 2005,
this AD). Revised: November
14, 2005.
(2) If any chafing damage is Before further Follow Cirrus Design
found as a result of the flight after the Corporation Service
inspection required by inspection required Bulletin SB 2X-28-
paragraph (e)(1) of this by paragraph (e)(1) 04 R1, Issued:
AD: of this AD. November 1, 2005,
(i) Replace any damaged fuel Revised: November
line; and 14, 2005.
(ii) Repair any damaged
wires or sheathing of the
wire harness
(3) Install the following: Within the next 50 Follow Cirrus Design
(i) Forward loop clamp; hours time-in- Corporation Service
(ii) Fuel line shield; service (TIS) after Bulletin SB 2X-28-
(iii) Aft loop clamp; and May 11, 2006 (the 04 R1, Issued:
(iv) Anti-chafe tubing effective date of November 1, 2005,
this AD). Revised: November
14, 2005.
------------------------------------------------------------------------
Alternative Methods of Compliance (AMOCs)
(f) The Manager, Chicago Aircraft Certification Office (ACO),
FAA, ATTN: Wess Rouse, Aerospace Engineer, ACE-117C, Chicago
Aircraft Certification Office, 2300 East Devon Avenue, Room 107, Des
Plaines, Illinois 60018; telephone: (847) 294-8113; fax: (847) 294-
7834, has the authority to approve AMOCs for this AD, if requested
using the procedures found in 14 CFR 39.19.
Material Incorporated by Reference
(g) You must do the actions required by this AD following the
instructions in Cirrus Design Corporation Service Bulletin SB 2X-28-
04 R1, Issued: November 1, 2005, Revised: November 14, 2005. The
Director of the Federal Register approved the incorporation by
reference of this service bulletin in accordance with 5 U.S.C.
552(a) and 1 CFR part 51. To get a copy of this service information,
contact Cirrus Design Corporation, 4515 Taylor Circle, Duluth,
Minnesota 55811; telephone: (218) 727-2737 or on the Internet at
http://www.cirrusdesign.com. To review copies of this service
information, go to the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, go to: http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html
or call (202) 741-6030. 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 20590-001 or on the Internet
at http://dms.dot.gov. The docket number is FAA-2005-23023;
Directorate Identifier 2005-CE-49-AD.
Issued in Kansas City, Missouri, on March 20, 2006.
Kim Smith,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 06-2982 Filed 3-29-06; 8:45 am]
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