Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model ERJ 170 Airplanes, 28628-28629 [E6-7474]

Download as PDF 28628 Federal Register / Vol. 71, No. 95 / Wednesday, May 17, 2006 / Proposed Rules Issued in Renton, Washington, on May 9, 2006. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. E6–7479 Filed 5–16–06; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2006–24788; Directorate Identifier 2006–NM–073–AD] DC, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. Contact Empresa Brasileira de Aeronautica S.A. (EMBRAER), P.O. Box 343—CEP 12.225, Sao Jose dos Campos—SP, Brazil, for service information identified in this proposed AD. FOR FURTHER INFORMATION CONTACT: Todd Thompson, Aerospace Engineer, International Branch, ANM–116, Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton, Washington 98055–4056; telephone (425) 227–1175; fax (425) 227–1149. SUPPLEMENTARY INFORMATION: RIN 2120–AA64 Comments Invited Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model ERJ 170 Airplanes Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Notice of proposed rulemaking (NPRM). mstockstill on PROD1PC61 with PROPOSALS AGENCY: SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD) for certain EMBRAER Model ERJ 170 airplanes. This proposed AD would require a one-time inspection for proper crimping of the terminal lugs for the power cables of each integrated drive generator (IDG), installing a new sleeve on the terminal, and re-crimping if necessary. This proposed AD results from a report that the terminal lugs for the power cables of the IDGs may not be adequately crimped, which could allow the cables to be pulled out of the terminals with no significant force. We are proposing this AD to prevent loss of all normal electrical power for the airplane, and consequent reduced controllability of the airplane. DATES: We must receive comments on this proposed AD by June 16, 2006. ADDRESSES: Use one of the following addresses to submit comments on this proposed AD. • DOT Docket Web site: Go to https://dms.dot.gov and follow the instructions for sending your comments electronically. • Government-wide rulemaking Web site: Go to https://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. • Fax: (202) 493–2251. • Hand Delivery: Room PL–401 on the plaza level of the Nassif Building, 400 Seventh Street, SW., Washington, VerDate Aug<31>2005 15:07 May 16, 2006 Jkt 208001 We invite you to submit any relevant written data, views, or arguments regarding this proposed AD. Send your comments to an address listed in the ADDRESSES section. Include the docket number ‘‘FAA–2006–24788; Directorate Identifier 2006–NM–073–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 received 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 https:// 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 that Web site, anyone can find and read the comments in any of our dockets, including the name of the individual who sent the comment (or signed the comment on behalf of an association, business, labor union, etc.). You may review the DOT’s complete Privacy Act Statement in the Federal Register published on April 11, 2000 (65 FR 19477–78), or you may visit https:// dms.dot.gov. Examining the Docket You may examine the AD docket on the Internet at https://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 Docket Management System receives them. PO 00000 Frm 00039 Fmt 4702 Sfmt 4702 Discussion The Departamento de Aviacao Civil ¸˜ (DAC), which is the airworthiness authority for Brazil, notified us that an unsafe condition may exist on certain EMBRAER Model ERJ 170 airplanes. The DAC advises that during a heavy maintenance action, it was discovered that four terminal lugs for the power cables of the integrated drive generators (IDGs) were not adequately crimped during installation, which could allow the cables to be pulled out of the terminals with no significant force. This condition, if not corrected, could result in loss of all normal electrical power for the airplane, and consequent reduced controllability of the airplane. Relevant Service Information EMBRAER has issued Service Bulletin 170–24–0028, dated January 4, 2006. The service bulletin describes procedures for doing an inspection of the crimping of terminal lugs for the power cables of each IDG, and corrective actions. The corrective actions are installing a new sleeve on the terminal, and re-crimping if necessary. Accomplishing the actions specified in the service information is intended to adequately address the unsafe condition. The DAC mandated the service information and issued Brazilian airworthiness directive 2006– 02–04, dated March 15, 2006, to ensure the continued airworthiness of these airplanes in Brazil. FAA’s Determination and Requirements of the Proposed AD This airplane model is manufactured in Brazil 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 DAC has kept the FAA informed of the situation described above. We have examined the DAC’s findings, evaluated all pertinent information, and determined that we need to issue an AD for airplanes 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. Clarification of Inspection Terminology In this proposed AD, the ‘‘detailed visual inspection’’ specified in the Brazilian airworthiness directive is referred to as a ‘‘detailed inspection.’’ We have included the definition for a E:\FR\FM\17MYP1.SGM 17MYP1 Federal Register / Vol. 71, No. 95 / Wednesday, May 17, 2006 / Proposed Rules detailed inspection in a note in the proposed AD. for a location to examine the regulatory evaluation. Costs of Compliance List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Safety. This proposed AD would affect about 54 airplanes of U.S. registry. The proposed actions would take about 1 work hour per airplane, at an average labor rate of $80 per work hour. The manufacturer states that it will supply required parts to the operators at no cost. Based on these figures, the estimated cost of the proposed AD for U.S. operators is $4,320, or $80 per airplane. 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. mstockstill on PROD1PC61 with PROPOSALS 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 and placed it in the AD docket. See the ADDRESSES section VerDate Aug<31>2005 15:07 May 16, 2006 Jkt 208001 The Proposed Amendment 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. § 39.13 [Amended] 2. The Federal Aviation Administration (FAA) amends § 39.13 by adding the following new airworthiness directive (AD): Empresa Brasileira de Aeronautica S.A. (EMBRAER): Docket No. FAA–2006– 24788; Directorate Identifier 2006–NM– 073–AD. Comments Due Date (a) The FAA must receive comments on this AD action by June 16, 2006. Affected ADs (b) None. Unsafe Condition (d) This AD results from a report that the terminal lugs for the power cables of the integrated drive generators (IDGs) may not be adequately crimped, which could allow the cables to be pulled out of the terminals with no significant force. We are issuing this AD to prevent the loss of all normal electrical power for the airplane, and consequent reduced controllability of the airplane. 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. Inspection and Corrective Actions (f) Within 600 flight hours after the effective date of this AD: Do a detailed inspection for proper crimping of terminal lugs for the power cables of each IDG, and install a new sleeve on the terminal. If the terminal lugs are not properly installed and crimped: Before further flight, re-crimp and install a new sleeve on the terminal. Do all actions in accordance with the Accomplishment Instructions of EMBREAR Service Bulletin 170–24–0028, dated January 4, 2006. Frm 00040 Note 1: For the purposes of this AD, a detailed inspection is: ‘‘An intensive examination of a specific item, installation, or assembly to detect damage, failure, or irregularity. Available lighting is normally supplemented with a direct source of good lighting at an intensity deemed appropriate. Inspection aids such as mirror, magnifying lenses, etc., may be necessary. Surface cleaning and elaborate procedures may be required.’’ Alternative Methods of Compliance (AMOCs) (g)(1) The Manager, ANM–116, Transport Airplane Directorate, FAA, has the authority to approve AMOCs for this AD, if requested in accordance with the procedures found in 14 CFR 39.19. (2) Before using any AMOC approved in accordance with § 39.19 on any airplane to which the AMOC applies, notify the appropriate principal inspector in the FAA Flight Standards Certificate Holding District Office. Related Information (h) Brazilian airworthiness directive 2006– 02–04, dated March 15, 2006, also addresses the subject of this AD. Issued in Renton, Washington, on May 9, 2006. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. E6–7474 Filed 5–16–06; 8:45 am] BILLING CODE 4910–13–P Applicability (c) This AD applies to EMBRAER Model ERJ 170–100 LR, –100 STD, –100 SE, and –100 SU airplanes, certificated in any category; as identified in EMBRAER Service Bulletin 170–24–0028, dated January 4, 2006. PO 00000 28629 Fmt 4702 Sfmt 4702 DEPARTMENT OF HOMELAND SECURITY Coast Guard 33 CFR Part 117 [USCG–2001–10881] RIN 1625–AA36 Drawbridge Operation Regulations; Amendment Coast Guard, DHS. Supplemental notice of proposed rulemaking. AGENCY: ACTION: SUMMARY: The Coast Guard is proposing a supplemental change to its notice of proposed rulemaking for modifying drawbridge operating regulations. This proposed supplemental change will consolidate all temporary changes to a drawbridge operating schedule into either a deviation or a rulemaking based on the length of time of the temporary change. This new proposed change is intended to provide more easily understood regulatory requirements. This proposed change will not affect the requirements for emergency closures or permanent changes to an operating schedule. E:\FR\FM\17MYP1.SGM 17MYP1

Agencies

[Federal Register Volume 71, Number 95 (Wednesday, May 17, 2006)]
[Proposed Rules]
[Pages 28628-28629]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E6-7474]


-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2006-24788; Directorate Identifier 2006-NM-073-AD]
RIN 2120-AA64


Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. 
(EMBRAER) Model ERJ 170 Airplanes

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

ACTION: Notice of proposed rulemaking (NPRM).

-----------------------------------------------------------------------

SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD) 
for certain EMBRAER Model ERJ 170 airplanes. This proposed AD would 
require a one-time inspection for proper crimping of the terminal lugs 
for the power cables of each integrated drive generator (IDG), 
installing a new sleeve on the terminal, and re-crimping if necessary. 
This proposed AD results from a report that the terminal lugs for the 
power cables of the IDGs may not be adequately crimped, which could 
allow the cables to be pulled out of the terminals with no significant 
force. We are proposing this AD to prevent loss of all normal 
electrical power for the airplane, and consequent reduced 
controllability of the airplane.

DATES: We must receive comments on this proposed AD by June 16, 2006.

ADDRESSES: Use one of the following addresses to submit comments on 
this proposed AD.
     DOT Docket Web site: Go to https://dms.dot.gov and follow 
the instructions for sending your comments electronically.
     Government-wide rulemaking Web site: Go to https://
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.
     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.
    Contact Empresa Brasileira de Aeronautica S.A. (EMBRAER), P.O. Box 
343--CEP 12.225, Sao Jose dos Campos--SP, Brazil, for service 
information identified in this proposed AD.

FOR FURTHER INFORMATION CONTACT: Todd Thompson, Aerospace Engineer, 
International Branch, ANM-116, Transport Airplane Directorate, FAA, 
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 
227-1175; 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 in the ADDRESSES section. Include the docket number ``FAA-2006-
24788; Directorate Identifier 2006-NM-073-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 received 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 https://
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 
that Web site, anyone can find and read the comments in any of our 
dockets, including the name of the individual who sent the comment (or 
signed the comment on behalf of an association, business, labor union, 
etc.). You may review the DOT's complete Privacy Act Statement in the 
Federal Register published on April 11, 2000 (65 FR 19477-78), or you 
may visit https://dms.dot.gov.

Examining the Docket

    You may examine the AD docket on the Internet at https://
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 Docket Management System 
receives them.

Discussion

    The Departamento de Aviac[atilde]o Civil (DAC), which is the 
airworthiness authority for Brazil, notified us that an unsafe 
condition may exist on certain EMBRAER Model ERJ 170 airplanes. The DAC 
advises that during a heavy maintenance action, it was discovered that 
four terminal lugs for the power cables of the integrated drive 
generators (IDGs) were not adequately crimped during installation, 
which could allow the cables to be pulled out of the terminals with no 
significant force. This condition, if not corrected, could result in 
loss of all normal electrical power for the airplane, and consequent 
reduced controllability of the airplane.

Relevant Service Information

    EMBRAER has issued Service Bulletin 170-24-0028, dated January 4, 
2006. The service bulletin describes procedures for doing an inspection 
of the crimping of terminal lugs for the power cables of each IDG, and 
corrective actions. The corrective actions are installing a new sleeve 
on the terminal, and re-crimping if necessary. Accomplishing the 
actions specified in the service information is intended to adequately 
address the unsafe condition. The DAC mandated the service information 
and issued Brazilian airworthiness directive 2006-02-04, dated March 
15, 2006, to ensure the continued airworthiness of these airplanes in 
Brazil.

FAA's Determination and Requirements of the Proposed AD

    This airplane model is manufactured in Brazil 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 DAC has kept the FAA informed of 
the situation described above. We have examined the DAC's findings, 
evaluated all pertinent information, and determined that we need to 
issue an AD for airplanes 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.

Clarification of Inspection Terminology

    In this proposed AD, the ``detailed visual inspection'' specified 
in the Brazilian airworthiness directive is referred to as a ``detailed 
inspection.'' We have included the definition for a

[[Page 28629]]

detailed inspection in a note in the proposed AD.

Costs of Compliance

    This proposed AD would affect about 54 airplanes of U.S. registry. 
The proposed actions would take about 1 work hour per airplane, at an 
average labor rate of $80 per work hour. The manufacturer states that 
it will supply required parts to the operators at no cost. Based on 
these figures, the estimated cost of the proposed AD for U.S. operators 
is $4,320, or $80 per airplane.

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 and placed it in the AD docket. 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

    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 Federal Aviation Administration (FAA) amends Sec.  39.13 by 
adding the following new airworthiness directive (AD):

Empresa Brasileira de Aeronautica S.A. (EMBRAER): Docket No. FAA-
2006-24788; Directorate Identifier 2006-NM-073-AD.

Comments Due Date

    (a) The FAA must receive comments on this AD action by June 16, 
2006.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to EMBRAER Model ERJ 170-100 LR, -100 STD, -
100 SE, and -100 SU airplanes, certificated in any category; as 
identified in EMBRAER Service Bulletin 170-24-0028, dated January 4, 
2006.

Unsafe Condition

    (d) This AD results from a report that the terminal lugs for the 
power cables of the integrated drive generators (IDGs) may not be 
adequately crimped, which could allow the cables to be pulled out of 
the terminals with no significant force. We are issuing this AD to 
prevent the loss of all normal electrical power for the airplane, 
and consequent reduced controllability of the airplane.

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.

Inspection and Corrective Actions

    (f) Within 600 flight hours after the effective date of this AD: 
Do a detailed inspection for proper crimping of terminal lugs for 
the power cables of each IDG, and install a new sleeve on the 
terminal. If the terminal lugs are not properly installed and 
crimped: Before further flight, re-crimp and install a new sleeve on 
the terminal. Do all actions in accordance with the Accomplishment 
Instructions of EMBREAR Service Bulletin 170-24-0028, dated January 
4, 2006.


    Note 1: For the purposes of this AD, a detailed inspection is: 
``An intensive examination of a specific item, installation, or 
assembly to detect damage, failure, or irregularity. Available 
lighting is normally supplemented with a direct source of good 
lighting at an intensity deemed appropriate. Inspection aids such as 
mirror, magnifying lenses, etc., may be necessary. Surface cleaning 
and elaborate procedures may be required.''

Alternative Methods of Compliance (AMOCs)

    (g)(1) The Manager, ANM-116, Transport Airplane Directorate, 
FAA, has the authority to approve AMOCs for this AD, if requested in 
accordance with the procedures found in 14 CFR 39.19.
    (2) Before using any AMOC approved in accordance with Sec.  
39.19 on any airplane to which the AMOC applies, notify the 
appropriate principal inspector in the FAA Flight Standards 
Certificate Holding District Office.

Related Information

    (h) Brazilian airworthiness directive 2006-02-04, dated March 
15, 2006, also addresses the subject of this AD.

    Issued in Renton, Washington, on May 9, 2006.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
 [FR Doc. E6-7474 Filed 5-16-06; 8:45 am]
BILLING CODE 4910-13-P
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