[Federal Register: March 29, 2006 (Volume 71, Number 60)]
[Proposed Rules]
[Page 15647-15649]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr29mr06-26]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2006-24095; Directorate Identifier 2006-CE-21-AD]
RIN 2120-AA64
Airworthiness Directives; DORNIER LUFTFAHRT GmbH Models 228-100,
228-101, 228-200, 228-201, 228-202, and 228-212 Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Notice of proposed rulemaking (NPRM).
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SUMMARY: We propose to adopt a new airworthiness directive (AD) for all
DORNIER LUFTFAHRT GmbH (DORNIER) Models 228-100, 228-101, 228-200, 228-
201, 228-202, and 228-212 airplanes. This proposed AD would require you
to repetitively inspect the wiring in the flight deck overhead panels
(locations 5VE and 6VE) for chafing and damage and repair any chafed or
damaged wires. Regardless of the results of each inspection, this
proposed AD would require you to assure correct installation of the
wiring in the flight deck overhead panels by reattaching or replacing
the wire tie attachment holders and securing any loose wires to the
wire tie attachment holders with plastic wire ties. This proposed AD
results from mandatory continuing airworthiness information (MCAI)
issued by the airworthiness authority for Germany. We are proposing
this AD to detect, correct, and prevent chafed or damaged wires in the
flight deck overhead panels, which could result in short-circuiting of
related wiring. This condition could lead to electrical failure of
affected systems and potential fire in the flight deck.
DATES: We must receive comments on this proposed AD by April 27, 2006.
ADDRESSES: Use one of the following addresses to comment 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 20590-0001.
Fax: (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.
For service information identified in this proposed AD, contact
RUAG Services GmbH, P.O. Box 1253, D-82231 Wessling; telephone: (08153)
302506; fax: (08153) 304601.
FOR FURTHER INFORMATION CONTACT: Karl Schletzbaum, Aerospace Engineer,
FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City,
Missouri 64106; telephone: (816) 329-4146; fax: (816) 329-4090.
SUPPLEMENTARY INFORMATION:
Comments Invited
We invite you to send any written relevant data, views, or
arguments regarding this proposed AD. Send your comments to an address
listed under the ADDRESSES section. Include the docket number, ``FAA-
2006-24095; Directorate Identifier 2006-CE-21-AD'' at the beginning of
your comments. We specifically invite comments on the overall
regulatory, economic, environmental, and energy aspects of the proposed
AD. We will consider all comments received by the closing date and may
amend the proposed AD in light of those 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 we
receive concerning this proposed AD.
Discussion
The Luftfahrt-Bundesamt (LBA), which is the airworthiness authority
for Germany, notified FAA that an unsafe condition may exist on all
DORNIER Models 228-100, 228-101, 228-200, 228-201, 228-202, and 228-212
airplanes. The LBA reports that vibrations are causing the plastic wire
tie attachment holder in the flight deck overhead panels to lose its
adhesiveness and become detached.
When the wire tie attachment holder becomes detached, the wiring in
the flight deck overhead panels is loose and may rub against the pins
of the switches in the overhead panel causing chafing and damage to the
wiring insulation.
This condition, if not corrected, could result in electrical
failure of affected systems and potential fire in the flight deck.
Relevant Service Information
We have reviewed RUAG AOT Dornier 228, All Operators Telefax
service information No. AOT-228-24-028, Date of Issue: November 9,
2005.
The service information specifies:
Repetitively inspecting the wiring in the flight deck
overhead panels (locations 5VE and 6VE) for chafing and damage;
Repairing any chafed or damaged wire(s); and
Assuring correct installation of the wiring in the flight
deck overhead panels by reattaching or replacing the wire tie
attachment holders and securing any loose wires to the wire tie
attachment holders with plastic wire ties.
Foreign Airworthiness Authority Information
The LBA classified the service information as mandatory and issued
German AD Number D-2005-438, Effective Date: December 14, 2005, to
ensure the continued airworthiness of these airplanes in Germany.
These DORNIER Models 228-100, 228-101, 228-200, 228-201, 228-202,
and 228-212 airplanes are manufactured in Germany and are type-
certificated for operation in the United States under the provisions of
section 21.29 of the Federal Aviation Regulations (14 CFR 21.29) and
the applicable bilateral airworthiness agreement.
Under this bilateral airworthiness agreement, the LBA has kept us
informed of the situation described above.
[[Page 15648]]
FAA's Determination and Requirements of the Proposed AD
We are proposing this AD because we have examined the LBA's
findings, evaluated all information and determined the unsafe condition
described previously is likely to exist or develop on other products of
the same type design that are certificated for operation in the United
States.
This proposed AD would require you to repetitively inspect the
wiring in the flight deck overhead panels (locations 5VE and 6VE) for
chafing and damage and repair any chafed or damaged wires. Regardless
of the results of each inspection, this proposed AD would require you
to assure correct installation of the wiring in the flight deck
overhead panels by reattaching or replacing the wire tie attachment
holders and securing any loose wires to the wire tie attachment holders
with plastic wire ties.
Costs of Compliance
How many airplanes would this proposed AD impact? We estimate that
this proposed AD would affect 14 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
do the proposed inspection:
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Total cost
Labor cost Parts cost per Total cost on U.S. operators
airplane
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2 work hours x $80 per hour = $160... Not applicable.......... $160 $160 x 14 = $2,240
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We estimate the following costs to do any necessary repairs that
would be required based on the results of the proposed inspection. We
have no way of determining the number of airplanes that may need this
repair:
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Labor cost Parts cost Total cost per airplane
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3 work hours x $80 per hour = $100 $240 + $100 = $340
$240.
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Note: The cure time for the adhesive that is recommended in the
service information is 48 hours at 25 degrees Celsius (77 degrees
Fahrenheit) or 2 hours at 65 degrees Celsius (149 degrees
Fahrenheit).
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
rulemaking action.
Regulatory Findings
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.
For the reasons discussed above, I certify that the proposed
regulation:
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 regulatory evaluation of the estimated costs to
comply with this proposed AD and placed it in the AD docket.
Examining the AD Docket
You may examine the AD docket that contains the proposed AD, the
regulatory evaluation, any comments received, and other information on
the Internet at http://dms.dot.gov; or in person at the Docket
Management Facility between 9 a.m. and 5 p.m., Monday through Friday,
except Federal holidays. The Docket Office (telephone (800) 647-5227)
is located at the street address stated in the ADDRESSES section.
Comments will be available in the AD docket shortly after receipt.
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 FAA 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 AD:
DORNIER LUFTFAHRT GmbH: Docket No. FAA-2006-24095; Directorate
Identifier 2006-CE-21-AD.
Comment Due Date
(a) We must receive comments on this airworthiness directive
(AD) action by April 27, 2006.
Affected ADs
(b) None.
Applicability
(c) This AD affects Models 228-100, 228-101, 228-200, 228-201,
228-202, and 228-212 airplanes, all serial numbers, that are
certificated in any category.
Unsafe Condition
(d) This AD results from mandatory continuing airworthiness
information (MCAI) issued by the airworthiness authority for
Germany. We are issuing this AD to detect, correct, and prevent
chafed or damaged wires in the flight deck overhead panels, which
could result in short-circuiting of related wiring. This condition
could lead to electrical failure of affected systems and potential
fire in the flight deck.
Compliance
(e) To address this problem, you must do the following:
[[Page 15649]]
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Actions Compliance Procedures
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(1) Inspect the wiring in Within the next 100 Follow RUAG AOT
the flight deck overhead hours time-in- Dornier 228, All
panels (locations 5VE and service (TIS) after Operators Telefax
6VE) for chafing and damage. the effective date service information
of this AD. No. AOT-228-24-028,
Repetitively Date of Issue:
inspect thereafter November 9, 2005.
at intervals not to
exceed 12 months.
(2) If you find any chafed Before further Follow RUAG AOT
or damaged wires during any flight after each Dornier 228, All
inspection required in inspection required Operators Telefax
paragraph (e)(1) of this in paragraph (e)(1) service information
AD, repair the affected of this AD. No. AOT-228-24-028,
wire(s) and assure correct Continue to Date of Issue:
installation of the wiring repetitively November 9, 2005.
in the flight deck overhead inspect as
panels by reattaching or specified in
replacing the wire tie paragraph (e)(1) of
attachment holders and this AD.
securing any loose wires to
the wire tie attachment
holders with plastic wire
ties.
(3) If you do not find any Before further Follow RUAG AOT
chafed or damaged wires flight after each Dornier 228, All
during any inspection inspection required Operators Telefax
required in paragraph in paragraph (e)(1) service information
(e)(1) of this AD, assure of this AD. No. AOT-228-24-028,
correct installation of the Continue to Date of Issue:
wiring in the flight deck repetitively November 9, 2005.
overhead panels by inspect as
reattaching or replacing specified in
the wire tie attachment paragraph (e)(1) of
holders and securing any this AD.
loose wires to the wire tie
attachment holders with
plastic wire ties.
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Alternative Methods of Compliance (AMOCs)
(f) The Manager, Standards Office, Small Airplane Directorate,
FAA, ATTN: Karl Schletzbaum, Aerospace Engineer, FAA, Small Airplane
Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106;
telephone: (816) 329-4146; fax: (816) 329-4090, has the authority to
approve AMOCs for this AD, if requested using the procedures found
in 14 CFR 39.19.
Related Information
(g) German AD Number D-2005-438, Effective Date: December 14,
2005, also addresses the subject of this AD. To get copies of the
documents referenced in this AD, contact RUAG Services GmbH, P.O.
Box 1253, D-82231 Wessling; telephone: (08153) 302506; fax: (08153)
304601. 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-2006-24095;
Directorate Identifier 2006-CE-21-AD.
Issued in Kansas City, Missouri, on March 22, 2006.
William J. Timberlake,
Acting Manager, Small Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E6-4556 Filed 3-28-06; 8:45 am]
BILLING CODE 4910-13-P