[Federal Register: September 7, 2005 (Volume 70, Number 172)]
[Rules and Regulations]
[Page 53058-53060]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr07se05-5]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2005-22306; Directorate Identifier 2005-NM-169-AD;
Amendment 39-14253; AD 2005-18-13]
RIN 2120-AA64
Airworthiness Directives; Israel Aircraft Industries, Ltd., Model
1124 and 1124A Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; request for comments.
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SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all
Israel Aircraft Industries, Ltd., Model 1124 and 1124A airplanes. This
AD requires a one-time inspection for chafing of the electrical bundles
in the overhead circuit breaker panel, and for adequate clearance
between the fuselage frame and adjacent structures; and repair and
rework if necessary. This AD results from reports of fire and smoke
occurring in the passenger cabin. This AD also requires certain
preventive actions. We are issuing this AD to prevent chafing of the
electrical bundles in the overhead circuit breaker panel, which could
result in a short circuit and consequent fire and smoke in the
airplane.
DATES: This AD becomes effective September 22, 2005.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in the AD as of September 22,
2005.
We must receive comments on this AD by November 7, 2005.
ADDRESSES: Use one of the following addresses to submit comments on
this AD.
DOT Docket Web site: Go to http://dms.dot.gov and follow
the instructions for sending your comments electronically.
Government-wide rulemaking Web site: Go to http://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 Gulfstream Aerospace Corporation, P.O. Box 2206, Mail
Station D-25, Savannah, Georgia 31402-2206, for service information
identified in this AD.
FOR FURTHER INFORMATION CONTACT: Mike Borfitz, Aerospace Engineer,
International Branch, ANM-116, FAA, Transport Airplane Directorate,
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425)
227-2677; fax (425) 227-1149.
SUPPLEMENTARY INFORMATION:
Discussion
The Civil Aviation Administration of Israel (CAAI), which is the
airworthiness authority for Israel, notified us that an unsafe
condition may exist on all Israel Aircraft Industries, Ltd., Model 1124
and 1124A airplanes. The CAAI advises that reports have been received
of fire and smoke in the passenger cabins due to chafing between
electrical bundles and the adjacent structure in the hinge area of the
overhead circuit breaker panel. This condition, if not corrected, could
result in a short circuit and consequent fire and smoke in the
airplane.
Relevant Service Information
Israel Aircraft Industries has issued 1124 Westwind Alert Service
Bulletin (ASB) 1124-24A-154, dated March 22, 2004. The ASB describes
procedures for a one-time visual inspection for chafing of the
electrical bundles in the overhead circuit breaker panel, and for
adequate clearance between the fuselage frame and the ``No Smoking--
Fasten Seat Belt'' sign; and repair and rework if necessary. The ASB
also describes certain preventive actions including installing spiral
wrap, insulated self-bondable tape, and a Teflon sheet at fuselage
station 83.78. Accomplishing the actions specified in the service
information is intended to adequately address the unsafe condition. The
CAAI approved the ASB and issued Israeli Airworthiness Directive 24-05-
02-32, dated March 15, 2005, to ensure the continued airworthiness of
these airplanes in Israel.
FAA's Determination and Requirements of This AD
These airplane models are manufactured in Israel and are 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 CAAI has kept the FAA informed
of the situation described above. We have examined the CAAI's findings,
evaluated all pertinent information, and determined that we need to
issue an AD for products of this type design that are certificated for
operation in the United States.
Therefore, we are issuing this AD to prevent chafing of the
electrical bundles in the overhead circuit breaker panel, which could
result in a short circuit and consequent fire and smoke in the
airplane. This AD requires accomplishing the actions specified in the
service information described previously, except as discussed under
``Differences Between the AD and the Israeli airworthiness directive.''
Clarification of Inspection
Although the Israeli airworthiness directive and the ASB specify
performing certain ``inspections,'' this AD specifies performing
``general visual
[[Page 53059]]
inspections.'' For the purposes of this AD, Note 1 provides the
definition of ``general visual inspections.''
Difference Between the AD and the Israeli Airworthiness Directive
Although the Israeli airworthiness directive specifies a compliance
time of ``within 50 flight hours,'' this AD specifies a compliance time
of ``within 60 days.'' We have determined that, based on the fleet's
average utilization rate, a 60-day compliance time is appropriate, in
that it will allow more time to comply for airplanes with a relatively
higher utilization rate without compromising safety. We have
coordinated this difference with the CAAI.
FAA's Determination of the Effective Date
An unsafe condition exists that requires the immediate adoption of
this AD; therefore, providing notice and opportunity for public comment
before the AD is issued is impracticable, and good cause exists to make
this AD effective in less than 30 days.
Comments Invited
This AD is a final rule that involves requirements that affect
flight safety and was not preceded by notice and an opportunity for
public comment; however, we invite you to submit any relevant written
data, views, or arguments regarding this AD. Send your comments to an
address listed in the ADDRESSES section. Include ``Docket No. FAA-2005-
22306; Directorate Identifier 2005-NM-169-AD'' at the beginning of your
comments. We specifically invite comments on the overall regulatory,
economic, environmental, and energy aspects of the AD that might
suggest a need to modify it.
We will post all comments we receive, without change, to http://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 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
http://dms.dot.gov.
Examining the Docket
You may examine the AD docket on the Internet at http://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.
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 the 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 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, 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):
2005-18-13 Israel Aircraft Industries, Ltd.: Amendment 39-14253.
Docket No. FAA-2005-22306; Directorate Identifier 2005-NM-169-AD.
Effective Date
(a) This AD becomes effective September 22, 2005.
Affected ADs
(b) None.
Applicability
(c) This AD applies to all Israel Model 1124 and 1124A
airplanes, certificated in any category.
Unsafe Condition
(d) This AD results from reports of fire and smoke occurring in
the passenger cabin. We are issuing this AD to prevent chafing of
the electrical bundles in the overhead circuit breaker panel, which
could result in a short circuit and consequent fire and smoke in 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 of the Electrical Bundles
(f) Within 60 days after the effective date of this AD, perform
a one-time general visual inspection for chafing of the electrical
bundles in the overhead circuit breaker panel and for adequate
clearance between the fuselage frame and the ``No Smoking--Fasten
Seat Belt'' sign, and perform the preventive actions, in accordance
with 1124-Westwind (Israel Aircraft Service Industries) Alert
Service Bulletin (ASB) 1124-24A-154, dated March 22, 2004.
Note 1: For the purposes of this AD, a general visual inspection
is: ``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
ensure visual access to all surfaces in the inspection area. This
level of inspection is made under normally available lighting
conditions such as daylight, hangar lighting, flashlight, or
[[Page 53060]]
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.''
Corrective Actions
(g) If any chafing of the electrical bundles or inadequate
clearance is detected during the inspection required by paragraph
(f) of this AD, before further flight, repair and rework, as
applicable; in accordance with 1124-Westwind (Israel Aircraft
Industries) Alert Service Bulletin 1124-24A-154, dated March 22,
2005.
Alternative Methods of Compliance (AMOCs)
(h) The Manager, International Branch, ANM-116, FAA, Transport
Airplane Directorate, has the authority to approve AMOCs for this
AD, if requested in accordance with the procedures found in 14 CFR
39.19.
Related Information
(i) Israeli airworthiness directive 24-05-02-32, dated March 15,
2005, also addresses the subject of this AD.
Material Incorporated by Reference
(j) You must use 1124-Westwind (Israel Aircraft Industries)
Alert Service Bulletin 1124-24A-154, dated March 22, 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. Contact Gulfstream Aerospace
Corporation, P.O. Box 2206, Mail Station D-25, Savannah, Georgia
31402-2206, 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 http://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 http://www.archives.gov /federal--register/
code--of--federal--regulations /ibr--locations.html.
Issued in Renton, Washington, on August 24, 2005.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 05-17600 Filed 9-6-05; 8:45 am]
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