[Federal Register: February 21, 2003 (Volume 68, Number 35)]
[Proposed Rules]
[Page 8473-8475]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr21fe03-6]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2002-NM-290-AD]
RIN 2120-AA64
Airworthiness Directives; Israel Aircraft Industries, Ltd., Model
1121, 1121A, 1121B, 1123, 1124, and 1124A Series Airplanes
AGENCY: Federal Aviation Administration, DOT.
ACTION: Notice of proposed rulemaking (NPRM).
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SUMMARY: This document proposes the adoption of a new airworthiness
directive (AD) that is applicable to all Israel Aircraft Industries,
Ltd., Model 1121, 1121A, 1121B, 1123, 1124, and 1124A series airplanes.
This proposal would require removing the existing oxygen shutoff valve
and installing a new oxygen shutoff valve. This action is necessary to
prevent rapid adiabatic compression within the oxygen line between the
oxygen shutoff valve and the pressure regulator due to a shutoff valve
that can be opened quickly, which could result in overheating of the
oxygen system, and consequent fire in the cockpit. This action is
intended to address the identified unsafe condition.
DATES: Comments must be received by March 24, 2003.
ADDRESSES: Submit comments in triplicate to the Federal Aviation
Administration (FAA), Transport Airplane Directorate, ANM-114,
Attention: Rules Docket No. 2002-NM-290-AD, 1601 Lind Avenue, SW.,
Renton, Washington 98055-4056. Comments may be inspected at this
location between 9 a.m. and 3 p.m., Monday through Friday, except
Federal holidays. Comments may be submitted via fax to (425) 227-1232.
Comments may also be sent via the Internet using the following address:
9-anm-nprmcomment@faa.gov. Comments sent via fax or the Internet must
contain ``Docket No. 2002-NM-290-AD'' in the subject line and need not
be submitted in triplicate. Comments sent via the Internet as attached
electronic files must be formatted in Microsoft Word 97 for Windows or
ASCII text.
The service information referenced in the proposed rule may be
obtained from Gulfstream Aerospace Corporation, P.O. Box 2206, Mail
Station D25, Savannah, Georgia 31402. This information may be examined
at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW.,
Renton, Washington.
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:
Comments Invited
Interested persons are invited to participate in the making of the
proposed rule by submitting such written data, views, or arguments as
they may desire. Communications shall identify the Rules Docket number
and be submitted in triplicate to the address specified above. All
communications received on or before the closing date for comments,
specified above, will be considered before taking action on the
proposed rule. The proposals contained in this action may be changed in
light of the comments received.
Submit comments using the following format:
[sbull] Organize comments issue-by-issue. For example, discuss a
request to change the compliance time and a request to change the
service bulletin reference as two separate issues.
[sbull] For each issue, state what specific change to the proposed
AD is being requested.
[sbull] Include justification (e.g., reasons or data) for each
request.
Comments are specifically invited on the overall regulatory,
economic, environmental, and energy aspects of the proposed rule. All
comments submitted will be available, both before and after the closing
date for comments, in the Rules Docket for examination by interested
persons. A report summarizing each FAA-public contact concerned with
the substance of this proposal will be filed in the Rules Docket.
Commenters wishing the FAA to acknowledge receipt of their comments
submitted in response to this action must submit a self-addressed,
stamped postcard on which the following statement is made: ``Comments
to Docket Number 2002-NM-290-AD.'' The postcard will be date stamped
and returned to the commenter.
[[Page 8474]]
Availability of NPRMs
Any person may obtain a copy of this NPRM by submitting a request
to the FAA, Transport Airplane Directorate, ANM-114, Attention: Rules
Docket No. 2002-NM-290-AD, 1601 Lind Avenue, SW., Renton, Washington
98055-4056.
Discussion
The Civil Aviation Administration of Israel (CAAI), which is the
airworthiness authority for Israel, notified the FAA that an unsafe
condition may exist on certain Israel Aircraft Industries, Ltd., Model
1121, 1121A, 1121B, 1123, 1124, and 1124A series airplanes. The CAAI
advises that a fire occurred in the cockpit on two airplanes during
taxiing, when the co-pilot turned on the oxygen system. Investigation
revealed that the existing design of the oxygen system allows high-
pressure oxygen into the cockpit, which is reduced at a pressure
regulator located on the airframe structure adjacent to the co-pilot.
If the shutoff valve is opened quickly, a rapid adiabatic compression
within the oxygen line between the oxygen shutoff valve and the
pressure regulator occurs. This condition, if not corrected, could
result in overheating of the oxygen system, and consequent fire in the
cockpit.
Other Relevant Rulemaking
The oxygen systems on certain Gulfstream Aerospace LP Model Astra
SPX and 1125 Westwind Astra series airplanes are identical to those on
the affected Israel Aircraft Industries, Ltd., Model 1121, 1121A,
1121B, 1123, 1124 and 1124A series airplanes. Therefore, the FAA has
issued NPRM, Rules Docket 2002-NM-281-AD, to address the identified
unsafe condition on certain Gulfstream Aerospace LP Model Astra SPX and
1125 Westwind Astra series airplanes as well.
Explanation of Relevant Service Information
The manufacturer has issued the following service bulletins, which
describe procedures for removing the existing oxygen shutoff valve and
installing a new oxygen shutoff valve:
Table--Service Bulletins
----------------------------------------------------------------------------------------------------------------
For model-- Service bulletin-- Including--
----------------------------------------------------------------------------------------------------------------
1121, 1121A, 1121B series airplanes..... 1121 Commodore Jet (Israel Aircraft Service Bulletin
Industries) Service Bulletin 1121-35-024, Certificate of
dated September 23, 2002. Compliance.
1123 series airplanes................... 1123-Westwind (Israel Aircraft Industries) Service Bulletin
Service Bulletin 1123-35-048, dated Certificate of
September 23, 2002. Compliance.
1124 and 1124A series airplanes......... 1124-Westwind (Israel Aircraft Industries) Service Bulletin
Service Bulletin 1124-35-137, dated Certificate of
September 23, 2002. Compliance.
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Accomplishment of the actions specified in the applicable service
bulletin is intended to adequately address the identified unsafe
condition. The CAAI classified these service bulletins as mandatory and
issued Israeli airworthiness directive 35-02-10-12, dated October 17,
2002, in order to assure the continued airworthiness of these airplanes
in Israel.
FAA's Conclusions
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. The FAA has examined the findings of
the CAAI, reviewed all available information, and determined that AD
action is necessary for products of this type design that are
certificated for operation in the United States.
Explanation of Requirements of Proposed Rule
Since an unsafe condition has been identified that is likely to
exist or develop on other airplanes of the same type design registered
in the United States, the proposed AD would require accomplishment of
the actions specified in the applicable service bulletin described
previously, except as discussed below.
Differences Between Proposed AD and Israeli Airworthiness Directive
The proposed AD would differ from the parallel Israeli
airworthiness directive in that it would require accomplishment of the
removal and installation of the oxygen shutoff valve within 250 flight
hours after the effective date of this AD. The parallel Israeli
airworthiness directive recommends accomplishment of those actions
within 200 flight hours. As described previously under the heading
``Other Relevant Rulemaking,'' we have issued NPRM, Rules Docket 2002-
NM-281-AD, to address the identified unsafe condition on certain
Gulfstream Aerospace LP Model Astra SPX and 1125 Westwind Astra series
airplanes. The compliance time in that NPRM, which parallels Israeli
airworthiness directive 35-02-07-02, dated August 18, 2002, is within
250 flight hours after the effective date of the AD. Because the
identified unsafe condition in both NPRMs and the subject oxygen
systems installed on the affected airplane models are identical, we
have determined that the compliance time of both of these NPRMs should
be the same. In light of these factors, we find a compliance time of
within 250 flight hours after the effective date of this AD for
completing the required actions to be warranted, in that it represents
an appropriate interval of time allowable for affected airplanes to
continue to operate without compromising safety. The compliance time
has been coordinated and concurred with by the CAAI.
Differences Between Proposed AD and Relevant Service Bulletin
Operators should note that, although the referenced service
bulletins describe procedures for completing a Service Bulletin
Certificate of Compliance to record compliance with the service
bulletin, this proposed AD would not require those actions.
Cost Impact
The FAA estimates that 300 Israel Aircraft Industries, Ltd., Model
1121, 1121A, 1121B, 1123, 1124, and 1124A series airplanes of U.S.
registry would be affected by this proposed AD, that it would take
approximately 8 work hours per airplane to accomplish the proposed
actions, and that the average labor rate is $60 per work hour. Required
parts would cost approximately $900 per airplane. Based on these
figures, the cost impact of the proposed AD on U.S. operators is
estimated to be $414,000, or $1,380 per airplane.
The cost impact figure discussed above is based on assumptions that
no
[[Page 8475]]
operator has yet accomplished any of the proposed 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. The manufacturer may cover the cost of
replacement parts associated with this proposed AD, subject to warranty
conditions. Manufacturer warranty remedies may also be available for
labor costs associated with this proposed AD. As a result, the costs
attributable to the proposed AD may be less than stated above.
Regulatory Impact
The regulations proposed herein 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. Therefore, it
is determined that this proposal would not have federalism implications
under Executive Order 13132.
For the reasons discussed above, I certify that this 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) if promulgated, 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 copy of the draft
regulatory evaluation prepared for this action is contained in the
Rules Docket. A copy of it may be obtained by contacting the Rules
Docket at the location provided under the caption ADDRESSES.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Safety.
The Proposed Amendment
Accordingly, pursuant to the authority delegated to me by the
Administrator, the Federal Aviation Administration proposes to amend
part 39 of the Federal Aviation Regulations (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. Section 39.13 is amended by adding the following new
airworthiness directive:
Israel Aircraft Industries, Ltd.: Docket 2002-NM-290-AD.
Applicability: All Model 1121, 1121A, 1121B, 1123, 1124, and
1124A series airplanes; certificated in any category.
Note 1: This AD applies to each airplane identified in the
preceding applicability provision, regardless of whether it has been
modified, altered, or repaired in the area subject to the
requirements of this AD. For airplanes that have been modified,
altered, or repaired so that the performance of the requirements of
this AD is affected, the owner/operator must request approval for an
alternative method of compliance in accordance with paragraph (b) of
this AD. The request should include an assessment of the effect of
the modification, alteration, or repair on the unsafe condition
addressed by this AD; and, if the unsafe condition has not been
eliminated, the request should include specific proposed actions to
address it.
Compliance: Required as indicated, unless accomplished
previously.
To prevent rapid adiabatic compression within the oxygen line
between the oxygen shutoff valve and the pressure regulator due to a
shutoff valve that can be opened quickly, which could result in
overheating of the oxygen system, and consequent fire in the
cockpit, accomplish the following:
Removal and Installation of Oxygen Shutoff Valve
(a) Within 250 flight hours after the effective date of this AD,
remove the existing oxygen shutoff valve and install a new oxygen
shutoff valve, per the Accomplishment Instructions of the applicable
service bulletin specified in the following table:
Table--Service Bulletins
----------------------------------------------------------------------------------------------------------------
For model-- Service bulletin-- Excluding--
----------------------------------------------------------------------------------------------------------------
1121, 1121A, 1121B series airplanes..... 1121 Commodore Jet (Israel Aircraft Service Bulletin
Industries) Service Bulletin 1121-35-024, Certificate of
dated September 23, 2002. Compliance.
1121 series airplanes................... 1123-Westwind (Israel Aircraft Industries) Service Bulletin
Service Bulletin 1123-35-048, dated Certificate of
September 23, 2002. Compliance.
1124 and 1124A series airplanes......... 1124-Westwind (Israel Aircraft Industries) Service Bulletin
Service Bulletin 1124-35-137, dated Certificate of
September 23, 2002. Compliance.
----------------------------------------------------------------------------------------------------------------
Alternative Methods of Compliance
(b) An alternative method of compliance or adjustment of the
compliance time that provides an acceptable level of safety may be
used if approved by the Manager, International Branch, ANM-116, FAA,
Transport Airplane Directorate. Operators shall submit their
requests through an appropriate FAA Principal Maintenance Inspector,
who may add comments and then send it to the Manager, International
Branch, ANM-116.
Note 2: Information concerning the existence of approved
alternative methods of compliance with this AD, if any, may be
obtained from the International Branch, ANM-116.
Special Flight Permits
(c) Special flight permits may be issued in accordance with
sections 21.197 and 21.199 of the Federal Aviation Regulations (14
CFR 21.197 and 21.199) to operate the airplane to a location where
the requirements of this AD can be accomplished.
Note 3: The subject of this AD is addressed in Israeli
airworthiness directive 35-02-10-12, dated October 17, 2002.
Issued in Renton, Washington, on February 13, 2003.
Ali Bahrami,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 03-4167 Filed 2-20-03; 8:45 am]
BILLING CODE 4910-13-P