AD 2004-14-24

[Federal Register Volume 69, Number 137 (Monday, July 19, 2004)]
[Rules and Regulations]
[Pages 42861-42862]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 04-16032]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 2003-NM-81-AD; Amendment 39-13733; AD 2004-14-24]
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 supersedes an existing airworthiness directive 
(AD), applicable to certain Empresa Brasileira de Aeronautica S.A. 
(EMBRAER) Model EMB-120 series airplanes, that currently requires 
measuring the gap between the bellcrank and the body of the rotary 
variable inductive transducers (RVITs) of the aileron and elevator, 
performing corrective action if necessary, and torquing the bolt that 
attaches the bellcrank to the RVIT shaft. This amendment requires 
replacing the aileron and elevator RVIT bellcranks with new, improved 
bellcranks. The actions specified by this AD are intended to prevent 
restricted movement of the aileron or elevator, which could result in 
reduced controllability of the airplane. This action is intended to 
address the identified unsafe condition.

DATES: Effective August 23, 2004.
    The incorporation by reference of EMBRAER Service Bulletin 120-31-
0046, Revision 01, dated December 27, 2002, as listed in the 
regulations, is approved by the Director of the Federal Register as of 
August 23, 2004.
    The incorporation by reference of EMBRAER Alert Service Bulletin 
120-31-A046, dated July 13, 2001, as listed in the regulations, was 
approved previously by the Director of the Federal Register as of 
August 27, 2001 (66 FR 43076, August 17, 2001).

ADDRESSES: The service information referenced in this AD may be 
obtained from Empresa Brasileira de Aeronautica S.A. (EMBRAER), PO. 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: <a href="http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html">http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html</a>.

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) by superseding AD 2001-17-01, 
amendment 39-12392 (66 FR 43076, August 17, 2001), which is applicable 
to certain Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-
120 series airplanes, was published in the Federal Register on May 3, 
2004 (69 FR 24105). The action proposed to require replacing the 
aileron and elevator RVIT bellcranks with new, improved bellcranks.

Comments

    Interested persons have been afforded an opportunity to participate 
in the making of this amendment. No comments were submitted in response 
to the proposal or the FAA's determination of the cost to the public.

Conclusion

    The FAA has determined that air safety and the public interest 
require the adoption of the rule as proposed.

Cost Impact

    There are approximately 201 Model EMB-120 series airplanes of U.S. 
registry that will be affected by this AD.
    The actions that are currently required by AD 2001-17-01 take 
approximately 1 or 2 work hours per airplane to accomplish, at an 
average labor rate of $65 per work hour. Based on these figures, the 
cost impact of the currently required actions on U.S. operators is 
estimated to be between $13,065 and $26,130; or between $65 and $130 
per airplane.
    The new actions that are required by this new AD will take 
approximately 1 or 2 work hours per airplane to accomplish, at an 
average labor rate of $65 per work hour. Required parts will cost 
approximately $810 per airplane. Based on these figures, the cost 
impact of the new requirements of this AD on U.S. operators is 
estimated to be between $175,875 and $188,940; or between $875 and $940 
per airplane.
    The cost impact figures discussed above are 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 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

[[Page 42862]]

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 removing amendment 39-12392 (66 FR 
43076, August 17, 2001), and by adding a new airworthiness directive 
(AD), amendment 39-13733, to read as follows:

2004-14-24 Empresa Brasileira de Aeronautica S.A. (EMBRAER): 
Amendment 39-13733. Docket 2003-NM-81-AD. Supersedes AD 2001-17-01, 
Amendment 39-12392.

    Applicability: Model EMB-120 series airplanes, certificated in 
any category; with serial numbers 120004 and 120006 through 120355 
inclusive; that have been modified in accordance with EMBRAER 
Service Bulletin 120-31-0039, 120-31-0040, 120-31-0041, or 120-31-
0042.
    Compliance: Required as indicated, unless accomplished 
previously.
    To prevent restricted movement of the aileron or elevator, which 
could result in reduced controllability of the airplane, accomplish 
the following:

Restatement of the Requirements of AD 2001-17-01: Inspection and 
Corrective Action, if Necessary

    (a) Within 50 flight hours after August 27, 2001 (the effective 
date of AD 2001-17-01, amendment 39-12392), measure the gap between 
the bellcrank and the body of the rotary variable inductive 
transducers (RVITs) of the elevator and aileron, in accordance with 
EMBRAER Alert Service Bulletin 120-31-A046, dated July 13, 2001.
    (1) If the gap is within the limits specified by the alert 
service bulletin: Prior to further flight, tighten the bolt that 
attaches the bellcrank to the RVIT shaft to a torque of 40-45 inch 
pounds, in accordance with the alert service bulletin.
    (2) If the gap is not within the limits specified by the alert 
service bulletin: Prior to further flight, accomplish all applicable 
corrective actions (including inspecting to detect damage of the 
connecting rod, replacing any damaged rod with a new rod having the 
same part number, and adjusting the gap between the bellcrank and 
the RVIT body), and tighten the bolt that attaches the bellcrank to 
the RVIT shaft to a torque of 40-45 inch pounds; in accordance with 
the alert service bulletin.

New Actions Required by This AD: Corrective Action

    (b) Within 4,000 flight hours after the effective date of this 
AD: Replace the aileron and elevator RVIT bellcranks having part 
number (P/N) 123-82549-007 or P/N 123-82549-009, as applicable, with 
new, improved bellcranks having P/N 145-51146-001 or P/N 145-51147-
001, respectively, in accordance with Paragraph 2.8 of the 
Accomplishment Instructions of EMBRAER Service Bulletin 120-31-0046, 
Revision 01, dated December 27, 2002.
    (c) Replacement of the bellcranks accomplished before the 
effective date of this AD per EMBRAER Service Bulletin 120-31-0046, 
dated February 20, 2002, are considered acceptable for compliance 
with the corresponding action specified in this AD.

Alternative Methods of Compliance

    (d) 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

    (e) The actions shall be done in accordance with EMBRAER Service 
Bulletin 120-31-0046, Revision 01, dated December 27, 2002; and 
EMBRAER Alert Service Bulletin 120-31-A046, dated July 13, 2001; as 
applicable.
    (1) The incorporation by reference of EMBRAER Service Bulletin 
120-31-0046, Revision 01, dated December 27, 2002, is approved by 
the Director of the Federal Register in accordance with 5 U.S.C. 
552(a) and 1 CFR part 51.
    (2) The incorporation by reference of EMBRAER Alert Service 
Bulletin 120-31-A046, dated July 13, 2001, was approved previously 
by the Director of the Federal Register as of August 27, 2001 (66 FR 
43076, August 17, 2001).
    (3) 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 FAA, Transport 
Airplane Directorate, 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: <a href="http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html">http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html</a>.

    Note 1:
    The subject of this AD is addressed in Brazilian airworthiness 
directive 2001-07-01R1, dated February 10, 2003.

Effective Date

    (f) This amendment becomes effective on August 23, 2004.


    Issued in Renton, Washington, on July 8, 2004.
Kevin M. Mullin,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 04-16032 Filed 7-16-04; 8:45 am]
BILLING CODE 4910-13-P