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