[Federal Register Volume 63, Number 23 (Wednesday, February 4, 1998)]
[Proposed Rules]
[Pages 5763-5764]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 98-2643]
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Proposed Rules
Federal Register
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This section of the FEDERAL REGISTER contains notices to the public of
the proposed issuance of rules and regulations. The purpose of these
notices is to give interested persons an opportunity to participate in
the rule making prior to the adoption of the final rules.
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Federal Register / Vol. 63, No. 23 / Wednesday, February 4, 1998 /
Proposed Rules
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 97-CE-30-AD]
RIN 2120-AA64
Airworthiness Directives; AlliedSignal Aerospace KT 76A Air
Traffic Control (ATC) Transponders
AGENCY: Federal Aviation Administration, DOT.
ACTION: Notice of proposed rulemaking (NPRM).
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SUMMARY: This document proposes to adopt a new airworthiness directive
(AD) that would apply to certain AlliedSignal Aerospace (AlliedSignal)
KT 76A ATC transponders that are installed on aircraft. The proposed AD
would require incorporating a modification on the affected transponders
that consists of replacing two resistor network modules with glass-
coated modules. The proposed AD is the result of reports of these ATC
transponders transmitting misleading encoding altimeter information to
ground-based ATC radar sites and nearby Traffic Alert and Collision
Avoidance System (TCAS)-equipped aircraft. The actions specified by the
proposed AD are intended to prevent the transmission of misleading
encoding altimeter information between affected aircraft caused by the
inability of these ATC transponders to coordinate with ground-based ATC
radar sites and nearby TCAS-equipped aircraft.
DATES: Comments must be received on or before April 10, 1998.
ADDRESSES: Submit comments in triplicate to the Federal Aviation
Administration (FAA), Central Region, Office of the Regional Counsel,
Attention: Rules Docket No. 97-CE-30-AD, Room 1558, 601 E. 12th Street,
Kansas City, Missouri 64106. Comments may be inspected at this location
between 8 a.m. and 4 p.m., Monday through Friday, holidays excepted.
Service information that applies to the proposed AD may be obtained
from AlliedSignal Inc., General Aviation Avionics, 400 N. Rogers Road,
Olathe, Kansas 66062-1212. This information also may be examined at the
Rules Docket at the address above.
FOR FURTHER INFORMATION CONTACT: Mr. Roger A. Souter, Aerospace
Engineer, Wichita Aircraft Certification Office, FAA, 1801 Airport
Road, Mid-Continent Airport, Wichita, Kansas 67209; telephone: (316)
946-4134; facsimile: (316) 946-4407.
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 should 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 that summarizes 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 No. 97-CE-30-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, Central Region, Office of the Regional Counsel, Attention:
Rules Docket No. 97-CE-30-AD, Room 1558, 601 E. 12th Street, Kansas
City, Missouri 64106.
Discussion
Several customer complaints relating to the altitude reporting
accuracy of AlliedSignal KT 76A ATC transponders; part number (P/N)
066-1062-00/10/02; serial numbers 93,000 through 109,999, that are
installed on aircraft prompted AlliedSignal to conduct testing of these
transponder systems. From this testing, AlliedSignal identified that
these ATC transponders are transmitting misleading encoding altimeter
information to ground-based ATC radar sites and nearby TCAS-equipped
aircraft.
The condition is the result of ``silver migration'' on the
substrate of a resistor network that is connected to the Gilham
Altitude outputs of an external encoding altimeter. This creates low
impedance paths between adjacent resistors in the network, which causes
the transponder unit to incorrectly interpret the output of the
encoding altimeter. Blocking diodes that are internal to the
AlliedSignal KT 76A ATC transponders prevent this ``silver migration''
problem from affecting other users of the Gilham outputs.
Relevant Service Information
AlliedSignal has issued Service Bulletin SB KT 76A-7, dated July
1996, which includes procedures for replacing two resistor network
modules, RM401 and RM402, with new glass-coated parts. When
accomplished, this replacement is referred to as Mod 7.
The FAA's Determination
After examining the circumstances and reviewing all available
information related to the incidents described above, including the
referenced service information, the FAA has determined that AD action
should be taken to prevent the transmission of misleading encoding
altimeter information between affected aircraft caused by the inability
of these ATC transponders to coordinate with ground-based ATC radar
sites and nearby TCAS-equipped aircraft.
Explanation of the Provisions of the Proposed AD
Since an unsafe condition has been identified that is likely to
exist or develop in airplanes that have AlliedSignal KT 76A ATC
transponders; part number (P/N) 066-1062-00/10/02; serial numbers
93,000 through 109,999, the FAA is proposing AD action. The
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proposed AD would require replacing two resistor network modules, RM401
and RM402, with new glass-coated parts. When accomplished, this
replacement is referred to as Mod 7. Accomplishment of the proposed
replacement would be required in accordance with AlliedSignal Service
Bulletin SB KT 76A-7, dated July 1996.
Compliance Time of the Proposed AD
The condition specified by the proposed AD is not caused by actual
hours time-in-service (TIS) of the aircraft where the affected ATC
transponders are installed. The need for the hardware modification has
no correlation to the number of times the equipment is utilized or the
age of the equipment. For this reason, the compliance time of the
proposed AD is presented in calendar time instead of hours TIS.
Cost Impact
The FAA estimates that 20,000 transponder units could be affected
by the proposed AD if all were installed in aircraft of U.S. registry.
Approximately 2 workhours would be needed to accomplish the proposed
action, at an average labor rate of $60 an hour. Parts will be provided
by AlliedSignal at no cost to the owners/operators of airplanes with
the affected transponder units installed. Based on these figures, the
total cost impact of the proposed AD on U.S. operators is estimated to
be $2,400,000, or $120 per airplane.
These figures are based on the presumption that all of the affected
transponder units are installed in aircraft and the units do not
incorporate Mod 7. AlliedSignal has informed the FAA that parts have
been distributed to incorporate Mod 7 on approximately 300 transponder
units. Presuming that each set of parts has been installed on an
airplane equipped with one of the affected transponder units, the cost
impact of the proposed AD would be reduced $36,000 from $2,400,000 to
$2,364,000.
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 action (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) 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 has been placed 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 a new airworthiness directive
(AD) to read as follows:
AlliedSignal Inc.: Docket No. 97-CE-30-AD.
Applicability: AlliedSignal KT 76A Air Traffic Control (ATC)
transponders; part number (P/N) 066-1062-00/10/02; serial numbers
93,000 through 109,999, as installed on, but not limited to the
following airplanes (all serial numbers), certificated in any
category:
Cessna Aircraft Company: 172, 182, R182, T182, 206, P206, U206,
TP206, 210, T210, P210, 310, E310, T310, and 421 series airplanes.
Twin Commander Aircraft Company: 500, 520, 560, 680, 681, 685,
690, 695, and 720 series airplanes.
The New Piper Aircraft Corporation: PA-31, PA-32, and PA-34
series airplanes.
Raytheon Aircraft Company: E33, F33, G33, 35, J35, K35, L35,
K35, M35, P35, S35, V35, 36, A26, B36, D55, E55, 56, A56, 58, 58A,
95, B95, D95, and E95 series airplanes.
Mooney Aircraft Corporation: M20 series airplanes.
McDonnell Douglas Helicopter Company: Model 500N rotorcraft.
Note 1: This AD applies to each airplane equipped with a
transponder that is 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 (d) 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 within the next 6 months after the
effective date of this AD, unless already accomplished.
To prevent the transmission of misleading encoding altimeter
information between affected aircraft caused by the inability of the
affected ATC transponders to coordinate with ground-based air
traffic control (ATC) radar sites and nearby Traffic Alert and
Collision Avoidance System (TCAS)-equipped aircraft, accomplish the
following:
(a) Replace the two resistor network modules, RM401 and RM402,
with new glass-coated parts in accordance with the MODIFICATION
PROCEDURE section of AlliedSignal Service Bulletin SB KT 76A-7,
dated July 1996. When accomplished, this replacement is referred to
as Mod 7.
(b) As of the effective date of this AD, no person may install
an AlliedSignal KT 76A ATC transponder; part number (P/N) 066-1062-
00/10/02; serial numbers 93,000 through 109,999, in an aircraft
without first incorporating Mod 7 as specified in paragraph (a) of
this AD.
(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.
(d) An alternative method of compliance or adjustment of the
compliance time that provides an equivalent level of safety may be
approved by the Manager, Wichita Aircraft Certification Office
(ACO), 1801 Airport Road, Room 100, Mid-Continent Airport, Wichita,
Kansas 67209. The request shall be forwarded through an appropriate
FAA Maintenance Inspector, who may add comments and then send it to
the Manager, Wichita ACO.
Note 2: Information concerning the existence of approved
alternative methods of compliance with this AD, if any, may be
obtained from the Wichita ACO.
(e) All persons affected by this directive may obtain copies of
the document referred to herein upon request to AlliedSignal Inc.,
General Aviation Avionics, 400 N. Rogers Road, Olathe, Kansas 66062-
1212; or may examine this document at the FAA, Central Region,
Office of the Regional Counsel, Room 1558, 601 E. 12th Street,
Kansas City, Missouri 64106.
Issued in Kansas City, Missouri, on January 28, 1998.
Terry L. Chasteen,
Acting Manager, Small Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 98-2643 Filed 2-3-98; 8:45 am]
BILLING CODE 4910-13-U
