Airworthiness Directives; Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-120, -120ER, -120FC, -120QC, and -120RT Airplanes in Operation, 28256-28257 [06-4502]
Download as PDF
28256
Federal Register / Vol. 71, No. 94 / Tuesday, May 16, 2006 / Rules and Regulations
Records Administration (NARA). For
information on the availability of this
material at the NARA, call (202) 741–6030,
or go to https://www.archives.gov/
federal_register/code_of_federal_regulations/
ibr_locations.html.
Issued in Renton, Washington, on May 8,
2006.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 06–4503 Filed 5–15–06; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2006–24120; Directorate
Identifier 2006–NM–021–AD; Amendment
39–14593; AD 2006–10–09]
RIN 2120–AA64
Airworthiness Directives; Empresa
Brasileira de Aeronautica S.A.
(EMBRAER) Model EMB–120, –120ER,
–120FC, –120QC, and –120RT
Airplanes in Operation
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
cprice-sewell on PROD1PC66 with RULES
AGENCY:
SUMMARY: The FAA is adopting a new
airworthiness directive (AD) for all
Empresa Brasileira de Aeronautica S.A.
(EMBRAER) Model EMB–120, –120ER,
–120FC, –120QC, and –120RT airplanes
in operation. This AD requires replacing
the protective tubes and conduits of the
wiring harnesses of the refueling vent
and pilot valves with non-conductive
hoses; modifying the harness wiring and
supports; and rerouting the harnesses to
prevent interference with adjacent
strobe light connectors; as applicable.
This AD results from a fuel system
review conducted by the manufacturer.
We are issuing this AD to prevent a
potential source of ignition near a fuel
tank, which, in combination with
flammable fuel vapors, could result in a
fuel tank explosion.
DATES: This AD becomes effective June
20, 2006.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in the AD
as of June 20, 2006.
ADDRESSES: You may examine the AD
docket on the Internet at https://
dms.dot.gov or in person at the Docket
Management Facility, U.S. Department
of Transportation, 400 Seventh Street,
SW., Nassif Building, Room PL–401,
Washington, DC.
VerDate Aug<31>2005
15:11 May 15, 2006
Jkt 208001
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 AD.
FOR FURTHER INFORMATION CONTACT: Dan
Rodina, Aerospace Engineer,
International Branch, ANM–116,
Transport Airplane Directorate, FAA,
1601 Lind Avenue, SW., Renton,
Washington 98055–4056; telephone
(425) 227–2125; fax (425) 227–1149.
SUPPLEMENTARY INFORMATION:
Examining the Docket
You may examine the airworthiness
directive (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 street address stated in the
ADDRESSES section.
Discussion
The FAA issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 to include an AD that would
apply to all Empresa Brasileira de
Aeronautica S.A. (EMBRAER) EMB–
120( ) airplane models in operation.
That NPRM was published in the
Federal Register on March 14, 2006 (71
FR 13058). That NPRM proposed to
require replacing the protective tubes
and conduits of the wiring harnesses of
the refueling vent and pilot valves with
non-conductive hoses; modifying the
harness wiring and supports; and
rerouting the harnesses to prevent
interference with adjacent strobe light
connectors; as applicable.
Comments
We provided the public the
opportunity to participate in the
development of this AD. We received no
comments on the NPRM or on the
determination of the cost to the public.
Explanation of Change to Applicability
We have revised the applicability of
the existing AD to identify model
designations as published in the most
recent type certificate data sheet for the
affected models.
Conclusion
We have carefully reviewed the
available data and determined that air
safety and the public interest require
adopting the AD with the change
described previously. We have
determined that this change will neither
increase the economic burden on any
PO 00000
Frm 00028
Fmt 4700
Sfmt 4700
operator nor increase the scope of the
AD.
Costs of Compliance
This AD will affect about 180
airplanes of U.S. registry. The required
actions will take between 4 and 24 work
hours per airplane, at an average labor
rate of $65 per work hour. Required
parts will cost between $555 and $6,179
per airplane. Based on these figures,
which depend upon airplane
configuration, the estimated cost of this
AD for U.S. operators is between
$146,700 and $1,393,020, or between
$815 and $7,739 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 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 that 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.
See the ADDRESSES section for a location
to examine the regulatory evaluation.
E:\FR\FM\16MYR1.SGM
16MYR1
Federal Register / Vol. 71, No. 94 / Tuesday, May 16, 2006 / Rules and Regulations
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
Adoption of the Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as
follows:
I
harnesses with non-conductive hoses; in
accordance with Part I of the
Accomplishment Instructions of the service
bulletin.
(2) For all remaining airplanes as identified
in paragraph 1.1.2 of the service bulletin:
Replace the protective tubes of the wiring
harnesses of the refueling vent and pilot
valves with non-conductive hoses; in
accordance with Part II of the
Accomplishment Instructions of the service
bulletin.
PART 39—AIRWORTHINESS
DIRECTIVES
Credit for Prior Revision of Service
Information
1. The authority citation for part 39
continues to read as follows:
(g) Actions accomplished before the
effective date of this AD in accordance with
EMBRAER Service Bulletin 120–28–0014,
dated April 19, 2004, are considered
acceptable for compliance with the
corresponding requirements of this AD.
I
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):
I
Effective Date
(a) This AD becomes effective June 20,
2006.
Affected ADs
(b) None.
Applicability
(c) This AD applies to all EMBRAER Model
EMB–120, –120ER, –120FC, –120QC, and
–120RT airplanes in operation, certificated in
any category.
Unsafe Condition
(d) This AD results from a fuel system
review conducted by the manufacturer. We
are issuing this AD to prevent a potential
source of ignition near a fuel tank, which, in
combination with flammable fuel vapors,
could result in a fuel tank explosion.
cprice-sewell on PROD1PC66 with RULES
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.
Rerouting Harnesses and Replacing Harness
Conduits
(f) Within 5,000 flight hours after the
effective date of this AD, perform the actions
specified in paragraph (f)(1) or (f)(2) of this
AD, as applicable, in accordance with the
Accomplishment Instructions of EMBRAER
Service Bulletin 120–28–0014, Revision 01,
dated November 4, 2004.
(1) For Group I airplanes as identified in
paragraph 1.1.1(a) or for Group II airplanes as
identified in paragraph 1.1.1(b) of the service
bulletin, as applicable: Modify the supports
and wiring of the refueling vent and pilot
valves wiring harnesses; reroute the
harnesses to prevent interference with
adjacent strobe light connectors; and replace
the protective tubes and conduits of the
15:11 May 15, 2006
Jkt 208001
Issued in Renton, Washington, on May 8,
2006.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 06–4502 Filed 5–15–06; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2006–24118; Directorate
Identifier 2006–NM–034–AD; Amendment
39–14594; AD 2006–10–10]
RIN 2120–AA64
Alternative Methods of Compliance
(AMOCs)
2006–10–09 Empresa Brasileira de
Aeronautica S.A. (EMBRAER):
Amendment 39–14593. Docket No.
FAA–2006–24120; Directorate Identifier
2006–NM–021–AD.
VerDate Aug<31>2005
28257
Airworthiness Directives; Bombardier
Model BD–100–1A10 Airplanes
(h)(1) The Manager, International Branch,
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.
AGENCY:
Related Information
(i) Brazilian airworthiness directive 2005–
12–04, effective January 19, 2006, also
addresses the subject of this AD.
Material Incorporated by Reference
(j) You must use EMBRAER Service
Bulletin 120–28–0014, Revision 01, dated
November 4, 2004, to perform the actions
that are required by this AD, unless the AD
specifies otherwise. The Director of the
Federal Register approved the incorporation
by reference of this document in accordance
with 5 U.S.C. 552(a) and 1 CFR part 51.
EMBRAER Service Bulletin 120–28–0014,
Revision 01, dated November 4, 2004,
contains the following effective pages:
Page No.
Revision
level shown
on page
1–4 .............
5–71 ...........
01 ..............
Original ......
Date shown on
page
Nov. 4, 2004.
April 19, 2004.
Contact Empresa Brasileira de Aeronautica
S.A. (EMBRAER), P.O. Box 343—CEP 12.225,
Sao Jose dos Campos—SP, Brazil, for a copy
of this service information. You may review
copies at the Docket Management Facility,
U.S. Department of Transportation, 400
Seventh Street, SW., Room PL–401, Nassif
Building, Washington, DC; on the Internet at
https://dms.dot.gov; or at the National
Archives and Records Administration
(NARA). For information on the availability
of this material at the NARA, call (202) 741–
6030, or go to https://www.archives.gov/
federal_register/code_of_federal_regulations/
ibr_locations.html.
PO 00000
Frm 00029
Fmt 4700
Sfmt 4700
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
SUMMARY: The FAA is adopting a new
airworthiness directive (AD) for certain
Bombardier Model BD–100–1A10
airplanes. This AD requires an
inspection for signs of arcing or heat
damage of the electrical connections of
the terminal blocks, ground studs, and
the end of the wires and surrounding
insulation for the windshield and side
window anti-ice systems; and repairing
any arced or damaged electrical
connection. This AD also requires retorquing electrical connections of the
terminal blocks and ground studs for the
windshield and side window anti-ice
systems. This AD results from an inservice incident involving smoke and
odor in the cockpit. We are issuing this
AD to prevent loose electrical
connections that could arc and overheat,
and cause wiring damage of the
windshield and side window anti-ice
systems. Such wiring damage could
result in smoke and/or fire in the flight
compartment.
DATES: This AD becomes effective June
20, 2006.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in the AD
as of June 20, 2006.
ADDRESSES: You may examine the AD
docket on the Internet at https://
dms.dot.gov or in person at the Docket
Management Facility, U.S. Department
of Transportation, 400 Seventh Street,
SW., Nassif Building, Room PL–401,
Washington, DC.
Contact Bombardier, Inc., Bombardier
Regional Aircraft Division, 123 Garratt
Boulevard, Downsview, Ontario M3K
E:\FR\FM\16MYR1.SGM
16MYR1
Agencies
[Federal Register Volume 71, Number 94 (Tuesday, May 16, 2006)]
[Rules and Regulations]
[Pages 28256-28257]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 06-4502]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2006-24120; Directorate Identifier 2006-NM-021-AD;
Amendment 39-14593; AD 2006-10-09]
RIN 2120-AA64
Airworthiness Directives; Empresa Brasileira de Aeronautica S.A.
(EMBRAER) Model EMB-120, -120ER, -120FC, -120QC, and -120RT Airplanes
in Operation
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all
Empresa Brasileira de Aeronautica S.A. (EMBRAER) Model EMB-120, -120ER,
-120FC, -120QC, and -120RT airplanes in operation. This AD requires
replacing the protective tubes and conduits of the wiring harnesses of
the refueling vent and pilot valves with non-conductive hoses;
modifying the harness wiring and supports; and rerouting the harnesses
to prevent interference with adjacent strobe light connectors; as
applicable. This AD results from a fuel system review conducted by the
manufacturer. We are issuing this AD to prevent a potential source of
ignition near a fuel tank, which, in combination with flammable fuel
vapors, could result in a fuel tank explosion.
DATES: This AD becomes effective June 20, 2006.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in the AD as of June 20,
2006.
ADDRESSES: You may examine the AD docket on the Internet at https://
dms.dot.gov or in person at the Docket Management Facility, U.S.
Department of Transportation, 400 Seventh Street, SW., Nassif Building,
Room PL-401, Washington, DC.
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 AD.
FOR FURTHER INFORMATION CONTACT: Dan Rodina, Aerospace Engineer,
International Branch, ANM-116, Transport Airplane Directorate, FAA,
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425)
227-2125; fax (425) 227-1149.
SUPPLEMENTARY INFORMATION:
Examining the Docket
You may examine the airworthiness directive (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 street address stated in the ADDRESSES section.
Discussion
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 to include an AD that would apply to all Empresa Brasileira
de Aeronautica S.A. (EMBRAER) EMB- 120( ) airplane models in operation.
That NPRM was published in the Federal Register on March 14, 2006 (71
FR 13058). That NPRM proposed to require replacing the protective tubes
and conduits of the wiring harnesses of the refueling vent and pilot
valves with non-conductive hoses; modifying the harness wiring and
supports; and rerouting the harnesses to prevent interference with
adjacent strobe light connectors; as applicable.
Comments
We provided the public the opportunity to participate in the
development of this AD. We received no comments on the NPRM or on the
determination of the cost to the public.
Explanation of Change to Applicability
We have revised the applicability of the existing AD to identify
model designations as published in the most recent type certificate
data sheet for the affected models.
Conclusion
We have carefully reviewed the available data and determined that
air safety and the public interest require adopting the AD with the
change described previously. We have determined that this change will
neither increase the economic burden on any operator nor increase the
scope of the AD.
Costs of Compliance
This AD will affect about 180 airplanes of U.S. registry. The
required actions will take between 4 and 24 work hours per airplane, at
an average labor rate of $65 per work hour. Required parts will cost
between $555 and $6,179 per airplane. Based on these figures, which
depend upon airplane configuration, the estimated cost of this AD for
U.S. operators is between $146,700 and $1,393,020, or between $815 and
$7,739 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 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 that 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. See the ADDRESSES
section for a location to examine the regulatory evaluation.
[[Page 28257]]
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,
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 Federal Aviation Administration (FAA) amends Sec. 39.13 by
adding the following new airworthiness directive (AD):
2006-10-09 Empresa Brasileira de Aeronautica S.A. (EMBRAER):
Amendment 39-14593. Docket No. FAA-2006-24120; Directorate
Identifier 2006-NM-021-AD.
Effective Date
(a) This AD becomes effective June 20, 2006.
Affected ADs
(b) None.
Applicability
(c) This AD applies to all EMBRAER Model EMB-120, -120ER, -
120FC, -120QC, and -120RT airplanes in operation, certificated in
any category.
Unsafe Condition
(d) This AD results from a fuel system review conducted by the
manufacturer. We are issuing this AD to prevent a potential source
of ignition near a fuel tank, which, in combination with flammable
fuel vapors, could result in a fuel tank explosion.
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.
Rerouting Harnesses and Replacing Harness Conduits
(f) Within 5,000 flight hours after the effective date of this
AD, perform the actions specified in paragraph (f)(1) or (f)(2) of
this AD, as applicable, in accordance with the Accomplishment
Instructions of EMBRAER Service Bulletin 120-28-0014, Revision 01,
dated November 4, 2004.
(1) For Group I airplanes as identified in paragraph 1.1.1(a) or
for Group II airplanes as identified in paragraph 1.1.1(b) of the
service bulletin, as applicable: Modify the supports and wiring of
the refueling vent and pilot valves wiring harnesses; reroute the
harnesses to prevent interference with adjacent strobe light
connectors; and replace the protective tubes and conduits of the
harnesses with non-conductive hoses; in accordance with Part I of
the Accomplishment Instructions of the service bulletin.
(2) For all remaining airplanes as identified in paragraph 1.1.2
of the service bulletin: Replace the protective tubes of the wiring
harnesses of the refueling vent and pilot valves with non-conductive
hoses; in accordance with Part II of the Accomplishment Instructions
of the service bulletin.
Credit for Prior Revision of Service Information
(g) Actions accomplished before the effective date of this AD in
accordance with EMBRAER Service Bulletin 120-28-0014, dated April
19, 2004, are considered acceptable for compliance with the
corresponding requirements of this AD.
Alternative Methods of Compliance (AMOCs)
(h)(1) The Manager, International Branch, 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
(i) Brazilian airworthiness directive 2005-12-04, effective
January 19, 2006, also addresses the subject of this AD.
Material Incorporated by Reference
(j) You must use EMBRAER Service Bulletin 120-28-0014, Revision
01, dated November 4, 2004, to perform the actions that are required
by this AD, unless the AD specifies otherwise. The Director of the
Federal Register approved the incorporation by reference of this
document in accordance with 5 U.S.C. 552(a) and 1 CFR part 51.
EMBRAER Service Bulletin 120-28-0014, Revision 01, dated November 4,
2004, contains the following effective pages:
------------------------------------------------------------------------
Revision level
Page No. shown on page Date shown on page
------------------------------------------------------------------------
1-4........................... 01.............. Nov. 4, 2004.
5-71.......................... Original........ April 19, 2004.
------------------------------------------------------------------------
Contact Empresa Brasileira de Aeronautica S.A. (EMBRAER), P.O. Box
343--CEP 12.225, Sao Jose dos Campos--SP, Brazil, for a copy of this
service information. You may review copies at the Docket Management
Facility, U.S. Department of Transportation, 400 Seventh Street,
SW., Room PL-401, Nassif Building, Washington, DC; on the Internet
at https://dms.dot.gov; or at the National Archives and Records
Administration (NARA). For information on the availability of this
material at the NARA, call (202) 741-6030, or go to https://
www.archives.gov/federal_register/code_of_federal_regulations/
ibr_locations.html.
Issued in Renton, Washington, on May 8, 2006.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 06-4502 Filed 5-15-06; 8:45 am]
BILLING CODE 4910-13-P