Document ID: FAA-2009-0123-0003
Agency: faa
Document Type: Rule
Title: Airworthiness Directives: DORNIER LUFTFAHRT GmbH Models Dornier 228 100 Airplanes et al.
Posted Date: 2009-04-06T04:00Z

[Federal Register: April 6, 2009 (Volume 74, Number 64)]
[Rules and Regulations]               
[Page 15369-15371]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr06ap09-3]                         

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2009-0123 Directorate Identifier 2009-CE-005-AD; 
Amendment 39-15868; AD 2009-07-09]
RIN 2120-AA64

 
Airworthiness Directives; DORNIER Luftfahrt GmbH Models Dornier 
228-100, Dornier 228-101, Dornier 228-200, Dornier 228-201, Dornier 
228-202, and Dornier 228-212 Airplanes

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

ACTION: Final Rule.

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SUMMARY: We are adopting a new airworthiness directive (AD) for the 
products listed above. This AD results from mandatory continuing 
airworthiness information (MCAI) issued by an aviation authority of 
another country to identify and correct an unsafe condition on an 
aviation product. The MCAI describes the unsafe condition as:

    It has been evidenced in-service that aileron trim actuator and 
rod spring lever attachment bracket--between frame 18 and 19 LH--on 
some aircraft may present loose rivets. If left uncorrected, this 
condition could lead to the separation of the attachment bracket 
which could result in loss of aileron trim and loss of artificial 
force feedback, and consequent reduced controllability of the 
airplane.

We are issuing this AD to require actions to correct the unsafe 
condition on these products.

DATES: This AD becomes effective May 11, 2009.
    On May 11, 2009, the Director of the Federal Register approved the 
incorporation by reference of certain publications listed in this AD.

ADDRESSES: You may examine the AD docket on the Internet at http://
www.regulations.gov or in person at Document Management Facility, U.S. 
Department of Transportation, Docket Operations, M-30, West Building 
Ground Floor, Room W12-140, 1200 New Jersey Avenue, SE., Washington, DC 
20590.

[[Page 15370]]

FOR FURTHER INFORMATION CONTACT: Greg Davison, Aerospace Engineer, FAA, 
Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 
64106; telephone: (816) 329-4130; fax: (816) 329-4090.

SUPPLEMENTARY INFORMATION: 

Discussion

    We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR 
part 39 to include an AD that would apply to the specified products. 
That NPRM was published in the Federal Register on February 13, 2009 
(74 FR 7200). That NPRM proposed to correct an unsafe condition for the 
specified products. The MCAI states:

    It has been evidenced in-service that aileron trim actuator and 
rod spring lever attachment bracket--between frame 18 and 19 LH--on 
some aircraft may present loose rivets. If left uncorrected, this 
condition could lead to the separation of the attachment bracket 
which could result in loss of aileron trim and loss of artificial 
force feedback, and consequent reduced controllability of the 
airplane.

Comments

    We gave the public the opportunity to participate in developing 
this AD. We received no comments on the NPRM or on the determination of 
the cost to the public.

Conclusion

    We reviewed the available data and determined that air safety and 
the public interest require adopting the AD as proposed.

Differences Between This AD and the MCAI or Service Information

    We have reviewed the MCAI and related service information and, in 
general, agree with their substance. But we might have found it 
necessary to use different words from those in the MCAI to ensure the 
AD is clear for U.S. operators and is enforceable. In making these 
changes, we do not intend to differ substantively from the information 
provided in the MCAI and related service information.
    We might also have required different actions in this AD from those 
in the MCAI in order to follow FAA policies. Any such differences are 
highlighted in a NOTE within the AD.

Costs of Compliance

    Based on the service information, we estimate that this AD will 
affect 17 products of U.S. registry. We also estimate that it will take 
about 5 work-hours per product to comply with the basic requirements of 
this AD. The average labor rate is $80 per work-hour. Required parts 
will cost about $5 per product.
    Based on these figures, we estimate the cost of this AD to the U.S. 
operators to be $6,885 or $405 per product.

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 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, or on the distribution of power and 
responsibilities among the various levels of government.
    For the reasons discussed above, I certify this AD:
    (1) Is not a ``significant regulatory action'' under Executive 
Order 12866;
    (2) Is not a ``significant rule'' under 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 AD and placed it in the AD Docket.

Examining the AD Docket

    You may examine the AD docket on the Internet at http://
www.regulations.gov; or in person at the Docket Management Facility 
between 9 a.m. and 5 p.m., Monday through Friday, except Federal 
holidays. The AD docket contains the NPRM, the regulatory evaluation, 
any comments received, and other information. The street address for 
the Docket Office (telephone (800) 647-5527) is 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, Incorporation by 
reference, Safety.

Adoption of the Amendment

0
Accordingly, under the authority delegated to me by the Administrator, 
the FAA amends 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. The FAA amends Sec.  39.13 by adding the following new AD:

2009-07-09 DORNIER Luftfahrt GmbH: Amendment 39-15868; Docket No. 
FAA-2009-0123; Directorate Identifier 2009-CE-005-AD.

Effective Date

    (a) This airworthiness directive (AD) becomes effective May 11, 
2009.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to Dornier 228-100, Dornier 228-101, Dornier 
228-200, Dornier 228-201, Dornier 228-202, and Dornier 228-212 
airplanes, all serial numbers, certificated in any category.

Subject

    (d) Air Transport Association of America (ATA) Code 27: Flight 
Controls.

Reason

    (e) The mandatory continuing airworthiness information (MCAI) 
states:

    It has been evidenced in-service that aileron trim actuator and 
rod spring lever attachment bracket--between frame 18 and 19 LH--on 
some aircraft may present loose rivets. If left uncorrected, this 
condition could lead to the separation of the attachment bracket 
which could result in loss of aileron trim and loss of artificial 
force feedback, and consequent reduced controllability of the 
airplane.
    For the reasons described above, this Airworthiness Directive 
requires first an inspection of the trim lever attachment bracket 
and as a second step the replacement of the 4 existing rivets by Hi-
Lock rivets.

Actions and Compliance

    (f) Unless already done, do the following actions:
    (1) Within the next 10 hours time-in-service (TIS) after May 11, 
2009 (the effective date of this AD), do the inspection for 
``unequal aileron steering wheel force'' in

[[Page 15371]]

accordance with paragraphs 2.A.(1) through 2.A.(3) of the 
ACCOMPLISHMENT INSTRUCTIONS of RUAG Aerospace Defence Technology 
Dornier 228 Service Bulletin No. SB-228-275, Revision No.: 0, dated 
October 8, 2008. If any defect is found, before further flight, 
modify the attachment bracket riveting in accordance with paragraph 
2.B. of the ACCOMPLISHMENT INSTRUCTIONS of RUAG Aerospace Defence 
Technology Dornier 228 Service Bulletin No. SB-228-275, Revision 
No.: 0, dated October 8, 2008.
    (2) Within 300 hours TIS after May 11, 2009 (the effective date 
of this AD), unless accomplished as required per paragraph (f)(1) of 
this AD, modify the attachment bracket riveting in accordance with 
paragraph 2.B. of the ACCOMPLISHMENT INSTRUCTIONS of RUAG Aerospace 
Defence Technology Dornier 228 Service Bulletin No. SB-228-275, 
Revision No.: 0, dated October 8, 2008.

FAA AD Differences

    Note: This AD differs from the MCAI and/or service information 
as follows: No differences.

Other FAA AD Provisions

    (g) The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager, 
Standards Office, FAA, has the authority to approve AMOCs for this 
AD, if requested using the procedures found in 14 CFR 39.19. Send 
information to ATTN: Greg Davison, Glider Program Manager, FAA, 
Small Airplane Directorate, 901 Locust, Room 301, Kansas City, 
Missouri 64106; telephone: (816) 329-4130; fax: (816) 329-4090. 
Before using any approved AMOC on any airplane to which the AMOC 
applies, notify your appropriate principal inspector (PI) in the FAA 
Flight Standards District Office (FSDO), or lacking a PI, your local 
FSDO.
    (2) Airworthy Product: For any requirement in this AD to obtain 
corrective actions from a manufacturer or other source, use these 
actions if they are FAA-approved. Corrective actions are considered 
FAA-approved if they are approved by the State of Design Authority 
(or their delegated agent). You are required to assure the product 
is airworthy before it is returned to service.
    (3) Reporting Requirements: For any reporting requirement in 
this AD, under the provisions of the Paperwork Reduction Act (44 
U.S.C. 3501 et seq.), the Office of Management and Budget (OMB) has 
approved the information collection requirements and has assigned 
OMB Control Number 2120-0056.

Related Information

    (h) Refer to MCAI European Aviation Safety Agency AD No.: 2008-
0217, dated December 10, 2008; and RUAG Aerospace Defence Technology 
Dornier 228 Service Bulletin No. SB-228-275, Revision No.: 0, dated 
October 8, 2008, for related information.

Material Incorporated by Reference

    (i) You must use RUAG Aerospace Defence Technology Dornier 228 
Service Bulletin No. SB-228-275, Revision No.: 0, dated October 8, 
2008, to do the actions required by this AD, unless the AD specifies 
otherwise.
    (1) The Director of the Federal Register approved the 
incorporation by reference of this service information under 5 
U.S.C. 552(a) and 1 CFR part 51.
    (2) For service information identified in this AD, contact RUAG 
Aerospace Services GmbH, Dornier 228 Customer Support, P.O. Box 
1253, 82231 Wessling, Federal Republic of Germany, telephone: +49 
(0) 8153-30-2280; fax: +49 (0) 8153-30-3030; E-mail: 
custsupport.dorner228@ruag.com; Internet: http://www.ruag.com/.
    (3) You may review copies of the service information 
incorporated by reference for this AD at the FAA, Central Region, 
Office of the Regional Counsel, 901 Locust, Kansas City, Missouri 
64106. For information on the availability of this material at the 
Central Region, call (816) 329-3768.
    (4) You may also review copies of the service information 
incorporated by reference for this AD at the National Archives and 
Records Administration (NARA). For information on the availability 
of this material at NARA, call (202) 741-6030, or go to: http://
www.archives.gov/federal_register/code_of_federal_regulations/
ibr_locations.html.

    Issued in Kansas City, Missouri, on March 24, 2009.
John Colomy,
Acting Manager, Small Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. E9-7071 Filed 4-3-09; 8:45 am]

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