[Federal Register Volume 59, Number 90 (Wednesday, May 11, 1994)]
[Unknown Section]
[Page 0]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 94-11352]
[[Page Unknown]]
[Federal Register: May 11, 1994]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 94-NM-41-AD]
Airworthiness Directives; British Aerospace Model ATP 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 British Aerospace Model
ATP airplanes. This proposal would require modification of the power
supply for the communications system. This proposal is prompted by
reports of loss of power to the communications system due to an
electrical fault in the ground crew jack box or the handset of the
public address (PA) system. The actions specified by the proposed AD
are intended to prevent the inability of the flight crew to communicate
with passengers via the PA system and with air traffic control due to
loss of power to the communication system, which may lead to unsafe
operation of the airplane.
DATES: Comments must be received by July 5, 1994.
ADDRESSES: Submit comments in triplicate to the Federal Aviation
Administration (FAA), Transport Airplane Directorate, ANM-103,
Attention: Rules Docket No. 94-NM-41-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.
The service information referenced in the proposed rule may be
obtained from Jetstream Aircraft, Incorporated, P.O. Box 16029, Dulles
International Airport, Washington, DC 20041-6029. This information may
be examined at the FAA, Transport Airplane Directorate, 1601 Lind
Avenue SW., Renton, Washington.
FOR FURTHER INFORMATION CONTACT: William Schroeder, Aerospace Engineer,
Standardization Branch, ANM-113, FAA, Transport Airplane Directorate,
1601 Lind Avenue SW., Renton, Washington 98055-4056; telephone (206)
227-2148; fax (206) 227-1320.
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 94-NM-41-AD.'' The postcard will be date stamped and
returned to the commenter.
Availability of NPRMs
Any person may obtain a copy of this NPRM by submitting a request
to the FAA, Transport Airplane Directorate, ANM-103, Attention: Rules
Docket No. 94-NM-41-AD, 1601 Lind Avenue SW., Renton, Washington 98055-
4056.
Discussion
The Civil Aviation Authority (CAA), which is the airworthiness
authority for the United Kingdom, recently notified the FAA that an
unsafe condition may exist on certain British Aerospace Model ATP
airplanes. The CAA advises that it has received reports of loss of
power to both essential and emergency power supplies for the
communications systems due to a ground fault in the communications jack
box of the ground crew-to-flight crew communications system in the bay
of the nose landing gear or the handset of the public address (PA)
system. This condition, if not corrected, could result in the inability
of the flight crew to communicate with passengers via the PA system and
with air traffic control, which may lead to unsafe operation of the
airplane.
Jetstream has issued Service Bulletin ATP-23-21-35288A, Revision 2,
dated February 15, 1994, that describes procedures for modification of
the power supply for the communications system. This modification
(Modification 35288A) entails installing two diodes on the terminal
block and the associated wiring to ensure that, in the event of an
electrical fault in the jack box for the ground crew-to-flight crew
communications system or the handset of the PA system, the
communications circuits will continue to operate. The CAA classified
this service bulletin as mandatory in order to assure the continued
airworthiness of these airplanes in the United Kingdom.
This airplane model is manufactured in the United Kingdom and is
type certificated for operation in the United States under the
provisions of Section 21.29 of the Federal Aviation Regulations and the
applicable bilateral airworthiness agreement. Pursuant to this
bilateral airworthiness agreement, the CAA has kept the FAA informed of
the situation described above. The FAA has examined the findings of the
CAA, 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.
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 modification of the
power supply for the communications system. The actions would be
required to be accomplished in accordance with the service bulletin
described previously.
The FAA estimates that 10 airplanes of U.S. registry would be
affected by this proposed AD, that it would take approximately 30 work
hours per airplane to accomplish the proposed actions, and that the
average labor rate is $55 per work hour. Required parts would be
provided at no cost to the operator. Based on these figures, the total
cost impact of the proposed AD on U.S. operators is estimated to be
$16,500, or $1,650 per airplane.
The total 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.
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 14
CFR part 39 of the Federal Aviation Regulations as follows:
PART 39--AIRWORTHINESS DIRECTIVES-
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. App. 1354(a), 1421 and 1423; 49 U.S.C.
106(g); and 14 CFR 11.89.
Sec. 39.13 [Amended]
2. Section 39.13 is amended by adding the following new
airworthiness directive:
British Aerospace: Docket 94-NM-41-AD.
Applicability: Model ATP airplanes having constructor's numbers
2002 through 2063 inclusive, certificated in any category.
Compliance: Required as indicated, unless accomplished
previously.
To prevent the inability of the flight crew to communicate with
passengers via the public address system and with air traffic
control due to loss of power to the communication system, which may
lead to unsafe operation of the airplane, accomplish the following:
(a) Within 675 hours time-in-service after the effective date of
this AD, modify the power supply of the communications system
(Modification 35288A) in accordance with Jetstream Service Bulletin
ATP-23-21-35288A, Revision 2, dated February 15, 1994.
(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, Standardization Branch, ANM-113,
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,
Standardization Branch, ANM-113.
Note: Information concerning the existence of approved
alternative methods of compliance with this AD, if any, may be
obtained from the Standardization Branch, ANM-113.
(c) Special flight permits may be issued in accordance with
Secs. 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.
Issued in Renton, Washington, on May 5, 1994.
S.R. Miller,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 94-11352 Filed 5-10-94; 8:45 am]
BILLING CODE 4910-13-U
