

[Federal Register: November 6, 2007 (Volume 72, Number 214)]
[Rules and Regulations]               
[Page 62560-62562]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr06no07-2]                         

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2007-28957 Directorate Identifier 2007-CE-069-AD; 
Amendment 39-15252; AD 2007-23-06]
RIN 2120-AA64

 
Airworthiness Directives; CTRM Aviation Sdn. Bhd. (Formerly Eagle 
Aircraft (Malaysia) Sdn. Bhd.) Model Eagle 150B Airplanes

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

[[Page 62561]]


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:

    An operator has reported severe exfoliation corrosion on Wing/
Canard Flap Hinges, P/N 5731D01-16 (middle and outboard hinges) on 
his Eagle 150B. The corrosion has been detected during 100-hour 
inspection. The aircraft has accumulated more than 1000 flight 
hours. The corrosion is so severe that one of the Flap Hinges 
thickness has been reduced by 50%. The corrosion is not easily 
detected because the Flap Hinge is sandwiched between the Flap Hinge 
Support Bracket P/N 5731D01-01.

    The failure of the hinge bracket may result in disintegration of 
flap/canard wing thus leading to loss of control, with catastrophic 
consequences.

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

DATES: This AD becomes effective December 11, 2007.
    On December 11, 2007, 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.

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: 

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 September 14, 2007 
(72 FR 52519). That NPRM proposed to correct an unsafe condition for 
the specified products. The MCAI states:

    An operator has reported severe exfoliation corrosion on Wing/
Canard Flap Hinges, P/N 5731D01-16 (middle and outboard hinges) on 
his Eagle 150B. The corrosion has been detected during 100-hour 
inspection. The aircraft has accumulated more than 1000 flight 
hours. The corrosion is so severe that one of the Flap Hinges 
thickness has been reduced by 50%. The corrosion is not easily 
detected because the Flap Hinge is sandwiched between the Flap Hinge 
Support Bracket P/N 5731D01-01.
    The failure of the hinge bracket may result in disintegration of 
flap/canard wing thus leading to loss of control, with catastrophic 
consequences.

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 about 6 products of U.S. registry. We also estimate that it will 
take about 3 work-hours per product to comply with the basic 
requirements of this AD. The average labor rate is $80 per work-hour.
    Based on these figures, we estimate the cost of the AD to U.S. 
operators to be $1,440, or $240 per product.
    In addition, we estimate that any necessary follow-on actions will 
take about 4 work-hours and require parts costing $226, for a cost of 
$546 per product. We have no way of determining the number of products 
that may need these actions.

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,

[[Page 62562]]

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:

2007-23-06 CTRM Aviation Sdn. Bhd. (Formerly Eagle Aircraft 
(Malaysia) Sdn. Bhd.): Amendment 39-15252; Docket No. FAA-2007-
28957; Directorate Identifier 2007-CE-069-AD.

Effective Date

    (a) This airworthiness directive (AD) becomes effective December 
11, 2007.

Affected ADs

    (b) None.

Applicability

    (c) This AD affects Model Eagle 150B airplanes, all serial 
numbers, that are certificated in any category.

Subject

    (d) Air Transport Association of America (ATA) Code 57: Wings.

Reason

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

    An operator has reported severe exfoliation corrosion on Wing/
Canard Flap Hinges, P/N 5731D01-16 (middle and outboard hinges) on 
his Eagle 150B. The corrosion has been detected during 100-hour 
inspection. The aircraft has accumulated more than 1000 flight 
hours. The corrosion is so severe that one of the Flap Hinges 
thickness has been reduced by 50%. The corrosion is not easily 
detected because the Flap Hinge is sandwiched between the Flap Hinge 
Support Bracket P/N 5731D01-01.

    The failure of the hinge bracket may result in disintegration of 
flap/canard wing thus leading to loss of control, with catastrophic 
consequences.

The MCAI requires you to visually inspect the flap hinges and flap 
hinge support brackets for any corrosion. You are to take corrective 
action if you find any corrosion.

Actions and Compliance

    (f) Unless already done, do the following actions:
    (1) Within the next 25 hours time-in-service (TIS) after 
December 11, 2007 (the effective date of this AD), inspect the flap 
hinges and flap hinge support brackets for any corrosion, following 
CTRM Aviation Mandatory Service Bulletin SB 1126, dated July 19, 
2007.
    (2) Before further flight, if you find any corrosion as a result 
of any inspection required by paragraph (f)(1) of this AD, take 
corrective action following CTRM Aviation Mandatory Service Bulletin 
SB 1126, dated July 19, 2007.

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: Karl Schletzbaum, Aerospace Engineer, FAA, 
Small Airplane Directorate, 901 Locust, Room 301, Kansas City, 
Missouri 64106; telephone: (816) 329-4146; 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 Department of Civil Aviation Malaysia AD No. 
CAM AD 001-07-2007, dated July 20, 2007; and CTRM Aviation Mandatory 
Service Bulletin SB 1126, dated July 19, 2007, for related 
information.

Material Incorporated by Reference

    (i) You must use CTRM Aviation Mandatory Service Bulletin SB 
1126, dated July 19, 2007, 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 CTRM 
Aviation Sdn. Bhd. (formerly known as Eagle Aircraft Sdn. Bhd.), 
Locked Bag 1028, Pejabat Pos Besar Melaka, 75150 Melaka, Malaysia; 
telephone: 06 317 1007; fax: 06 317 7023.
    (3) You may review copies at the FAA, Central Region, Office of 
the Regional Counsel, 901 Locust, Room 506, Kansas City, Missouri 
64106; or 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/cfr/ibr-locations.html
.


    Issued in Kansas City, Missouri, on October 29, 2007.
Kim Smith,
Manager, Small Airplane Directorate, Aircraft Certification Service.
 [FR Doc. E7-21667 Filed 11-5-07; 8:45 am]

BILLING CODE 4910-13-P
