[Federal Register: June 29, 2004 (Volume 69, Number 124)]
[Rules and Regulations]
[Page 38823-38824]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr29jn04-9]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2003-NM-65-AD; Amendment 39-13695; AD 2004-13-13]
RIN 2120-AA64
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A.
(EMBRAER) Model EMB-120 Series Airplanes
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule.
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SUMMARY: This amendment adopts a new airworthiness directive (AD),
applicable to certain EMBRAER Model EMB-120 series airplanes, that
requires a one-time inspection of the access door ramp of the fueling
control panel for damage or deformation, and applicable corrective
actions. This action is necessary to prevent inadvertent fuel transfer
in flight due to fuel service personnel not repositioning the defuel
valve switch control to the closed position after utilization on the
ground, which could cause in-flight fuel starvation. This action is
intended to address the identified unsafe condition.
DATES: Effective August 3, 2004.
The incorporation by reference of certain publications listed in
the regulations is approved by the Director of the Federal Register as
of August 3, 2004.
ADDRESSES: The service information referenced in this AD may be
obtained from Empresa Brasileira de Aeronautica S.A. (EMBRAER), P.O.
Box 343--CEP 12.225, Sao Jose dos Campos--SP, Brazil. This information
may be examined at the Federal Aviation Administration (FAA), Transport
Airplane Directorate, Rules Docket, 1601 Lind Avenue, SW., Renton,
Washington; 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/code_of_federal_regulations/ibr_locations.html
.
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: A proposal to amend part 39 of the Federal
Aviation Regulations (14 CFR part 39) to include an airworthiness
directive (AD) that is applicable to certain EMBRAER Model EMB-120
series airplanes was published in the Federal Register on April 6, 2004
(69 FR 17989). That action required a one-time inspection of the access
door ramp of the fueling control panel for damage or deformation, and
applicable corrective actions.
Comments
Interested persons have been afforded an opportunity to participate
in the making of this amendment. No comments have been submitted on the
proposed AD or on the determination of the cost to the public.
Conclusion
After careful review of the available data, the FAA has determined
that air safety and the public interest require the adoption of the
rule as proposed.
Cost Impact
The FAA estimates that 220 airplanes of U.S. registry will be
affected by this AD, that it will take approximately 4 work hours per
airplane to accomplish each required action, and that the average labor
rate is $65 per work hour. Required parts will cost approximately $200
per airplane. Based on these figures, the cost impact of the AD on U.S.
operators is estimated to be $101,200, or $460 per airplane.
The cost impact figure discussed above is based on assumptions that
no operator has yet accomplished any of the requirements of this AD
action, and that no operator would accomplish those actions in the
future if this AD were not adopted. The cost impact figures discussed
in AD rulemaking actions represent only the time
[[Page 38824]]
necessary to perform the specific actions actually required by the AD.
These figures typically do not include incidental costs, such as the
time required to gain access and close up, planning time, or time
necessitated by other administrative actions.
Regulatory Impact
The regulations adopted herein 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. Therefore, it
is determined that this final rule does not have federalism
implications under Executive Order 13132.
For the reasons discussed above, I certify that this action (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. A final evaluation has been prepared for this action
and it is contained in the Rules Docket. A copy of it may be obtained
from the Rules Docket at the location provided under the caption
ADDRESSES.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Amendment
0
Accordingly, pursuant to 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. Section 39.13 is amended by adding the following new airworthiness
directive:
2004-13-13 Empresa Brasileira de Aeronautica S.A. (EMBRAER):
Amendment 39-13695. Docket 2003-NM-65-AD.
Applicability: Model EMB-120 series airplanes, serial numbers
120003, 120004, and 120006 through 120358 inclusive; certificated in
any category.
Compliance: Required as indicated, unless accomplished
previously.
To prevent inadvertent fuel transfer in flight due to fuel
service personnel not repositioning the defuel valve switch control
to the closed position after utilization on the ground, which could
cause in-flight fuel starvation, accomplish the following:
Inspection of Existing Ramp and Corrective Actions
(a) For airplanes that have a ramp on the access door of the
fueling control panel: Within 1,200 flight hours or 8 months after
the effective date of this AD, whichever occurs first, perform a
general visual inspection of the access door ramp for damage or
deformation; and do all applicable corrective actions by
accomplishing all the actions in accordance with paragraph 2.2.3 of
the Accomplishment Instructions of EMBRAER Service Bulletin 120-57-
0038, dated June 26, 2002. Do the actions per the service bulletin.
Accomplish any applicable corrective actions before further flight.
Note 1: For the purposes of this AD, a general visual inspection
is defined as: ``A visual examination of an interior or exterior
area, installation, or assembly to detect obvious damage, failure,
or irregularity. This level of inspection is made from within
touching distance unless otherwise specified. A mirror may be
necessary to enhance visual access to all exposed surfaces in the
inspection area. This level of inspection is made under normally
available lighting conditions such as daylight, hangar lighting,
flashlight, or droplight and may require removal or opening of
access panels or doors. Stands, ladders, or platforms may be
required to gain proximity to the area being checked.''
Modification
(b) For airplanes that do not have a ramp on the access door of
the fueling control panel: Within 1,200 flight hours or 8 months
after the effective date of this AD, whichever occurs first, modify
the access door by accomplishing all the actions in paragraph 2.1.3
of the Accomplishment Instructions of EMBRAER Service Bulletin 120-
57-0038, dated June 26, 2002. Do the actions per the service
bulletin. Accomplish any applicable corrective actions before
further flight.
Alternative Methods of Compliance
(c) In accordance with 14 CFR 39.19, the Manager, International
Branch, ANM-116, FAA, Transport Airplane Directorate, is authorized
to approve alternative methods of compliance for this AD.
Incorporation by Reference
(d) The actions shall be done in accordance with EMBRAER Service
Bulletin 120-57-0038, dated June 26, 2002. This incorporation by
reference was approved by the Director of the Federal Register in
accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Copies may be
obtained from Empresa Brasileira de Aeronautica S.A. (EMBRAER), P.O.
Box 343--CEP 12.225, Sao Jose dos Campos--SP, Brazil. Copies may be
inspected at the Federal Aviation Administration (FAA), Transport
Airplane Directorate, Rules Docket, 1601 Lind Avenue, SW., Renton,
Washington; 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/code_of_federal_regulations/ibr_locations.html
.
Note 2: The subject of this AD is addressed in Brazilian
airworthiness directive 2002-12-02, effective January 6, 2003.
Effective Date
(e) This amendment becomes effective on August 3, 2004.
Issued in Renton, Washington, on June 16, 2004.
Ali Bahrami,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 04-14569 Filed 6-28-04; 8:45 am]
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