[Federal Register Volume 64, Number 123 (Monday, June 28, 1999)]
[Proposed Rules]
[Pages 34588-34590]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 99-16328]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 99-NM-48-AD]
RIN 2120-AA64
Airworthiness Directives; Airbus Industrie Model A320 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 certain Airbus Industrie Model
A320 series airplanes. This proposal would require replacement of the
disc valve and spring in the low pressure non-return valve of the
airborne ground check module (AGCM) of the ram air turbine (RAT). This
proposal is prompted by issuance of mandatory continuing airworthiness
information by a foreign civil airworthiness authority. The actions
specified by the proposed AD are intended to prevent malfunction of the
low pressure non-return valve in the AGCM. If the RAT is being used due
to the loss of other systems, a malfunction of the valve could result
in loss of the blue hydraulic system, and consequent loss of certain
flight control and electrical systems of the airplane.
DATES: Comments must be received by July 28, 1999.
ADDRESSES: Submit comments in triplicate to the Federal Aviation
Administration (FAA), Transport Airplane Directorate, ANM-114,
Attention: Rules Docket No. 99-NM-48-AD, 1601 Lind Avenue, SW., Renton,
Washington 98055-4056. Comments may be inspected at this location
between 9:00 a.m. and 3:00 p.m., Monday through Friday, except Federal
holidays.
The Airbus Industrie service bulletin referenced in the proposed
rule may be obtained from Airbus Industrie, 1 Rond Point Maurice
Bellonte, 31707 Blagnac Cedex, France. The Sundstrand service bulletin
referenced in the proposed rule may be obtained from Sundstrand
Aerospace, 4747 Harrison Avenue, P.O. Box 7002, Rockford, Illinois
61125-7002. These service bulletins may be examined at the FAA,
Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton,
Washington.
FOR FURTHER INFORMATION CONTACT: Norman B. Martenson, Manager,
International Branch, ANM-116, FAA, Transport Airplane Directorate,
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425)
227-2110; 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 notice may be changed in
light of the comments received.
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 notice must submit a self-addressed,
stamped postcard on which the following statement is made: ``Comments
to Docket Number 99-NM-48-AD.'' The postcard will be date stamped and
returned to the commenter.
[[Page 34589]]
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. 99-NM-48-AD, 1601 Lind Avenue, SW., Renton, Washington
98055-4056.
Discussion
The Direction Generale de l'Aviation Civile (DGAC), which is the
airworthiness authority for France, notified the FAA that an unsafe
condition may exist on certain Airbus Industrie Model A320 series
airplanes. The DGAC advises that, during two in-flight events and
during one functional test of the airborne ground check module (AGCM)
of the ram air turbine (RAT), a blockage of the low pressure check
valve was observed. Investigation revealed that the blockage was caused
by a malfunction of the low pressure non-return valve in the AGCM. If
the RAT is being used due to the loss of other systems, the malfunction
of the valve could result in loss of the blue hydraulic system, and
consequent loss of certain flight control and electrical systems of the
airplane.
Explanation of Relevant Service Information
Airbus Industrie has issued Service Bulletin A320-29-1086, dated
October 19, 1998, and Revision 01, dated March 9, 1999, which describes
procedures for replacement of the disc valve and spring in the low
pressure non-return valve of the AGCM of the RAT. This service bulletin
references Sundstrand Service Bulletin ERPS13GCM-29-3, dated June 24,
1998, as an additional source of service information for accomplishment
of the replacement.
Accomplishment of the action specified in the service bulletins is
intended to adequately address the identified unsafe condition. The
DGAC classified the Airbus Industrie service bulletin as mandatory and
issued French airworthiness directive 98-537-124(B), dated December 30,
1998, in order to assure the continued airworthiness of these airplanes
in France.
FAA's Conclusions
This airplane model is manufactured in France 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 DGAC has kept the FAA informed
of the situation described above. The FAA has examined the findings of
the DGAC, 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 action specified in the service bulletins described previously.
Cost Impact
The FAA estimates that 165 airplanes of U.S. registry would be
affected by this proposed AD, that it would take approximately 1 work
hour per airplane to accomplish the proposed replacement, and that the
average labor rate is $60 per work hour. Required parts would be
provided by the manufacturer at no cost to the operators. Based on
these figures, the cost impact of the proposed AD on U.S. operators is
estimated to be $9,900, or $60 per airplane.
The cost impact figure discussed above is based on assumptions that
no 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.
Regulatory Impact
The regulations proposed herein would not have substantial direct
effects 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, in
accordance with Executive Order 12612, it is determined that this
proposal would not have sufficient federalism implications to warrant
the preparation of a Federalism Assessment.
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:
Airbus Industrie: Docket 99-NM-48-AD.
Applicability: Model A320 series airplanes, except those
airplanes on which
Airbus Industrie modification 27728 has been installed in
production, or on which Airbus Industrie Service Bulletin A320-29-
1086 has been accomplished; certificated in any category.
Note 1: This AD applies to each airplane identified in the
preceding applicability provision, regardless of whether it has been
otherwise 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 malfunction of the low pressure non-return valve in
the airborne ground check module (AGCM) of the ram air turbine
(RAT), which could result in loss of the blue hydraulic system, and
consequent loss of certain flight control and electrical systems,
accomplish the following:
Replacement
(a) Within 12 months after the effective date of this AD,
replace the disc valve and spring in the low pressure non-return
valve in the AGCM with a new poppet, and re-identify the AGCM name
plate, in accordance with Airbus Industrie Service Bulletin A320-29-
1086, dated October 19, 1998, or Revision 01, dated March 9, 1999;
and Sundstrand Service Bulletin ERPS13GCM-29-3, dated June 24, 1998.
[[Page 34590]]
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
Sec. Sec. 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 French
airworthiness directive 98-537-124(B), dated December 30, 1998.
Issued in Renton, Washington, on June 22, 1999.
D.L. Riggin,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 99-16328 Filed 6-25-99; 8:45 am]
BILLING CODE 4910-13-U
