[Federal Register Volume 70, Number 34 (Tuesday, February 22, 2005)]
[Proposed Rules]
[Pages 8547-8549]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 05-3286]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2005-20414; Directorate Identifier 2004-NM-116-AD]
RIN 2120-AA64


Airworthiness Directives; Dornier Model 328-300 Series Airplanes

AGENCY: Federal Aviation Administration (FAA), Department of 
Transportation (DOT).

ACTION: Notice of proposed rulemaking (NPRM).

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SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD) 
for all Dornier Model 328-300 series airplanes. This proposed AD would 
require installing an additional mounting angle for the respective de-
icing pipes at rib 9 in the leading edge area of the left- and right-
hand wings. This proposed AD is prompted by chafed de-icing lines in 
the wing leading edge area. We are proposing this AD to prevent chafing 
of the de-icing lines, which could result in a reduction in 
functionality of the anti-ice system, and possibly reduced 
controllability and performance of the airplane in icing conditions.

DATES: We must receive comments on this proposed AD by March 24, 2005.

ADDRESSES: Use one of the following addresses 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.
     By 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 
AvCraft Aerospace GmbH, P.O. Box 1103, D-82230 Wessling, Germany.
    You can examine the contents of this AD docket on the Internet at 
http://dms.dot.gov, or in person at the Docket Management Facility, 
U.S. Department of Transportation, 400 Seventh Street SW., room PL-401, 
on the plaza level of the Nassif Building, Washington, DC. This docket 
number is FAA-2005-20414; the directorate identifier for this docket is 
2004-NM-116-AD.

FOR FURTHER INFORMATION CONTACT: Dan Rodina, Aerospace Engineer, 
International Branch, ANM-116, FAA, Transport Airplane Directorate, 
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 
227-2125; fax (425) 227-1149.

SUPPLEMENTARY INFORMATION:

Comments Invited

    We invite you to submit any relevant written data, views, or 
arguments regarding this proposed AD. Send your comments to an address 
listed under ADDRESSES. Include ``Docket No. FAA-2005-20414; 
Directorate Identifier 2004-NM-116-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 submitted 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 with FAA 
personnel concerning this proposed AD. Using the search function of our 
docket Web site, anyone can find and read the comments in any of our 
dockets, including the name of the individual

[[Page 8548]]

who sent the comment (or signed the comment on behalf of an 
association, business, labor union, etc.). You can review the DOT's 
complete Privacy Act Statement in the Federal Register published on 
April 11, 2000 (65 FR 19477-78), or you can visit http://dms.dot.gov.

Examining the Docket

    You can examine the AD docket on the Internet at http://dms.dot.gov, or in person at the Docket Management Facility office 
between 9 a.m. and 5 p.m., Monday through Friday, except Federal 
holidays. The Docket Management Facility office (telephone (800) 647-
5227) is located on the plaza level of the Nassif Building at the DOT 
street address stated in the ADDRESSES section. Comments will be 
available in the AD docket shortly after the DMS receives them.

Discussion

    The Luftfahrt-Bundesamt (LBA), which is the airworthiness authority 
for Germany, notified us that an unsafe condition may exist on all 
Dornier Model 328-300 series airplanes. The LBA advises that, during 
inspections, de-icing lines were found chafed in the leading edge area 
of the left- and right-hand wings. The chafing was caused by 
insufficient clearance from the de-icing lines to the adjacent airplane 
structure. This condition, if not corrected, could result in a 
reduction in functionality of the anti-ice system, and possibly reduced 
controllability and performance of the airplane in icing conditions.

Relevant Service Information

    Dornier has issued Service Bulletin SB-328J-30-190, dated July 16, 
2003. The service bulletin describes procedures for installing an 
additional mounting angle for the respective de-icing pipes at rib 9 in 
the leading edge area of the left- and right-hand wings. Accomplishing 
the actions specified in the service information is intended to 
adequately address the unsafe condition. The LBA mandated the service 
information and issued German airworthiness directive D-2004-049, dated 
February 1, 2004, to ensure the continued airworthiness of these 
airplanes in Germany.

FAA's Determination and Requirements of the Proposed AD

    This airplane model is manufactured in Germany and is 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. Pursuant to this 
bilateral airworthiness agreement, the LBA has kept the FAA informed of 
the situation described above. We have examined the LBA's findings, 
evaluated all pertinent information, and determined that we need to 
issue an AD for products of this type design that are certificated for 
operation in the United States.
    Therefore, we are proposing this AD, which would require 
accomplishing the actions specified in the service information 
described previously.

Costs of Compliance

    The following table provides the estimated costs for U.S. operators 
to comply with this proposed AD.

                                                                     Estimated Costs
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                                                                                                                            Number  of
                                                                          Average  labor                     Cost per          U.S.-
                         Action                             Work  hours   rate  per hour       Parts         airplane       registered      Fleet  cost
                                                                                                                             airplanes
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Installation............................................              8             $65            $252            $772              49         $37,828
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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. See the ADDRESSES section for a location 
to examine the regulatory evaluation.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Safety.

The Proposed Amendment

0
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 
airworthiness directive (AD):

Fairchild Dornier GMBH (Formerly Dornier Luftfahrt GmbH): Docket No. 
FAA-2005-20414; Directorate Identifier 2004-NM-116-AD.

Comments Due Date

    (a) The Federal Aviation Administration must receive comments on 
this AD action by March 24, 2005.

Affected ADs

    (b) None.

[[Page 8549]]

Applicability

    (c) This AD applies to all Dornier Model 328-300 series 
airplanes, certificated in any category.

Unsafe Condition

    (d) This AD was prompted by chafed de-icing lines in the wing 
leading edge area. We are issuing this AD to prevent chafing of the 
de-icing lines, which could result in a reduction in functionality 
of the anti-ice system, and possibly reduced controllability and 
performance of the airplane in icing conditions.

Compliance

    (e) You are responsible for having the actions required by this 
AD performed within the compliance times specified, unless the 
actions have already been done.

Installation

    (f) Within 90 days after the effective date of this AD, install 
an additional mounting angle at rib 9 in the leading edge area of 
the left- and right-hand wings in accordance with the Accomplishment 
Instructions of Dornier Service Bulletin SB-328J-30-190, dated July 
16, 2003.

Alternative Methods of Compliance (AMOCs)

    (g) The Manager, International Branch, ANM-116, FAA, Transport 
Airplane Directorate, has the authority to approve AMOCs for this 
AD, if requested in accordance with the procedures found in 14 CFR 
39.19.

Related Information

    (h) German airworthiness directive D-2004-049, dated February 1, 
2004, also addresses the subject of this AD.

    Issued in Renton, Washington, on February 14, 2005.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 05-3286 Filed 2-18-05; 8:45 am]
BILLING CODE 4910-13-P