[Federal Register: October 7, 2004 (Volume 69, Number 194)]
[Proposed Rules]
[Page 60100-60104]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr07oc04-13]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA 2004-18743; Directorate Identifier 2004-CE-23-AD]
RIN 2120-AA64
Airworthiness Directives; GARMIN International Inc. GTX 33, GTX
33D, GTX 330, and GTX 330D Mode S Transponders
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
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SUMMARY: The FAA proposes to supersede Airworthiness Directive (AD)
2004-10-15, which applies to certain GTX 330 and GTX 330D Mode S
transponders that are installed on airplanes. AD 2004-10-15 currently
requires you to install GTX 330/330D Software Upgrade Version 3.03,
3.04, or 3.05. This proposed AD applies to certain GTX 33, GTX 33D, GTX
330, and GTX 330D Mode S transponders that are installed on airplanes
and is the result of observations that the GTX 33/33D/330/330D may
detect, from other airplanes, the S1 (suppression) interrogating pulse
below the minimum trigger level (MTL) and, in some circumstances, not
reply. The GTX 33/33D/330/330D should still reply even if it detects S1
interrogating pulses below the MTL. Consequently, this proposed AD
would require you to install GTX 33/33D/330/330D Software Upgrade
Version 3.03 or 3.06. Software Upgrade Versions 3.03 and 3.06 correct a
TAS, TCAD, and TCAS I system ``whisper-shout'' problem that could
potentially lead to the aircraft not being visible at certain ranges.
TCAS II systems are not affected. We are issuing this proposed AD to
prevent interrogating aircraft from possibly receiving inaccurate
replies due to suppression from aircraft equipped with the GTX 33/33D/
330/330D Mode S transponders when the pulses are below the MTL. The
inaccurate replies could result in reduced vertical separation.
DATES: We must receive any comments on this proposed AD by November 15,
2004.
ADDRESSES: Use one of the following to submit comments on this proposed
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 20590-001.
Fax: 1-202-493-2251.
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.
To get the service information identified in this proposed AD,
contact GARMIN International Inc. 1200 East 151st Street, Olathe, KS
66062; telephone: 913-397-8200.
To view the comments to this proposed AD, go to http://dms.dot.gov.
This is docket number FAA 2004-18743.
FOR FURTHER INFORMATION CONTACT: Roger A. Souter, FAA, Wichita Aircraft
Certification Office (ACO), 1801 Airport Road, Room 100, Wichita,
Kansas 67209; telephone: 316-946-4134; facsimile: 316-946-4107; email
address: roger.souter@faa.gov.
SUPPLEMENTARY INFORMATION:
Comments Invited
How do I comment on this proposed AD? We invite you to submit any
[[Page 60101]]
written relevant data, views, or arguments regarding this proposal.
Send your comments to an address listed under ADDRESSES. Include the
docket number, ``FAA 2004-18743; Directorate Identifier 2004-CE-23-AD''
at the beginning of your comments. 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 proposed
rulemaking. Using the search function of our docket Web site, anyone
can find and read the comments received into 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.).
This is docket number FAA 2004-18743. 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.
Are there any specific portions of this proposed AD I should pay
attention to? We specifically invite comments on the overall
regulatory, economic, environmental, and energy aspects of this
proposed AD. If you contact us through a nonwritten communication and
that contact relates to a substantive part of this proposed AD, we will
summarize the contact and place the summary in the docket. We will
consider all comments received by the closing date and may amend this
proposed AD in light of those comments and contacts.
Docket Information
Where can I go to view the docket information? You may view the AD
docket that contains the proposal, any comments received, and any final
disposition in person at the DMS Docket Offices between 9 a.m. and 5
p.m. (eastern standard time), Monday through Friday, except Federal
holidays. The Docket Office (telephone 1-800-647-5227) is located on
the plaza level of the Department of Transportation NASSIF Building at
the street address stated in ADDRESSES. You may also view the AD docket
on the Internet at http://dms.dot.gov. The comments will be available
in the AD docket shortly after the DMS receives them.
Discussion
Has FAA taken any action to this point? The GTX 330/GTX 330D may
detect from other aircraft the S1 (suppression) interrogating pulse
below the MTL and, in some circumstances, does not reply. The GTX 330/
330D should still reply even if it detects S1 interrogating pulses
below the MTL, and this caused FAA to issue AD 2004-10-15, Amendment
39-13645 (69 FR 29212, dated May 21, 2004). AD 2004-10-15 currently
requires the incorporation of GTX 330/330D Software Upgrade to at least
Version, 3.03, 3.04, or 3.05 on certain GTX 330 and GTX 330D Mode S
transponders that are installed on airplanes.
What has happened since AD 2004-10-15 to initiate this proposed
action? After the issuance of AD 2004-10-15, GARMIN International Inc.
discovered that minor changes made to GTX 330/330D Software Upgrades
3.04 and 3.05 inadvertently removed the correction to not suppress the
S1 pulse below MTL. Garmin also discovered the Software Upgrade must be
installed on GTX 33 and GTX 33D Mode S transponders as well as the GTX
330 and GTX 330D Mode S transponders.
What is the potential impact if FAA took no action? We are issuing
this proposed AD to incorporate these changes and to prevent
interrogating aircraft from possibly receiving inaccurate replies due
to suppression from aircraft equipped with the GTX 33/33D/330/330D Mode
S transponders when the pulses are below the MTL. Software Upgrade
Version 3.03 and 3.06 correct a TAS, TCAD, and TCAS I system ``whisper-
shout'' problem that could potentially lead to the aircraft not being
visible at certain ranges. TCAS II systems are not affected. The
inaccurate replies could result in reduced vertical separation.
Is there service information that applies to this subject? GARMIN
International Inc. has issued the Service Bulletin No. 0304, Revision
B, dated June 12, 2003 (which incorporates Software Upgrade 3.03), and
Service Bulletin No. 0409, dated July 19, 2004 (which incorporates
Software Upgrade 3.06).
What are the provisions of this service information? The service
bulletins include:
--modification instructions for upgrading to software version 3.03 or
3.06 and
--a listing of parts required to perform the modification.
FAA's Determination and Requirements of This Proposed AD
What has FAA decided? We have evaluated all pertinent information
and identified an unsafe condition that is likely to exist or develop
on other products of this same type design. For this reason, we are
proposing AD action.
What would this proposed AD require? This proposed AD would
supersede AD 2004-10-15 with a new AD that would require you to install
Garmin GTX 33/33D/330/330D Software Upgrade Version 3.03 or 3.06.
How does the revision to 14 CFR part 39 affect this proposed AD? On
July 10, 2002, we published a new version of 14 CFR part 39 (67 FR
47997, July 22, 2002), which governs FAA's AD system. This regulation
now includes material that relates to altered products, special flight
permits, and alternative methods of compliance. This material
previously was included in each individual AD. Since this material is
included in 14 CFR part 39, we will not include it in future AD
actions.
Costs of Compliance
How many airplanes would this proposed AD impact? We estimate that
this proposed AD affects 5400 airplanes in the U.S. registry.
What would be the cost impact of this proposed AD on owners/
operators of the affected airplanes? Garmin International Inc. will
provide warranty only for Service Bulletin No. 0409, dated July 19,
2004 (which incorporates Software Upgrade 3.06) installation as
specified in the service information. Although Software Upgrade 3.03 is
still in compliance with this proposed AD, if previously installed,
Software Upgrade 3.03 is no longer available through Garmin.
What is the difference between the cost impact of this proposed AD
and the cost impact of AD 2004-10-15? Garmin provided warranty credit
for AD 2004-10-15 and will provide warranty credit only for
installation of Service Bulletin No. 0409, dated July 19, 2004 (which
incorporates Software Upgrade 3.06) in the proposed AD.
Regulatory Findings
Would this proposed AD impact various entities? We have determined
that this proposed AD would not have federalism implications under
Executive Order 13132. This proposed AD 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.
Would this proposed AD involve a significant rule or regulatory
action? For the reasons discussed above, I certify that this proposed
AD:
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,
[[Page 60102]]
on a substantial number of small entities under the criteria of the
Regulatory Flexibility Act.
We prepared a summary of the costs to comply with this proposed AD
and placed it in the AD Docket. You may get a copy of this summary by
sending a request to us at the address listed under ADDRESSES. Include
``AD Docket No. FAA 2004-18743; Directorate Identifier 2003-CE-39-AD''
in your request.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Safety.
The Proposed Amendment
Accordingly, under the authority delegated to me by the
Administrator, the Federal Aviation Administration proposes to amend 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. The FAA amends Sec. 39.13 by removing Airworthiness Directive
(AD) 2004-10-15, Amendment 39-13645 (69 FR 29212-15, dated May 21,
2004), and by adding a new AD to read as follows:
GARMIN International Inc.: Docket No. FAA 2004-18743; Directorate
Identifier 2004-CE-23-AD
When Is the Last Date I Can Submit Comments on This Proposed AD?
(a) We must receive comments on this proposed airworthiness
directive (AD) by November 15, 2004.
What Other ADs Are Affected by This Action?
(b) This AD supersedes AD 2004-10-15, Amendment 39-13645.
What Airplanes Are Affected by This AD?
(c) This AD affects GARMIN International Inc. GTX 33, GTX 33D,
GTX 330, and GTX 330D Mode S transponders that are installed on, but
not limited to, the following airplanes, certificated in any
category:
------------------------------------------------------------------------
Manufacturer Model
------------------------------------------------------------------------
(1) Aermacchi S.p.A.................. S.205-18/F, S.205-18/R, S.205-20/
R, S.205-22/R, S208, S.208A,
F.260, F.260B, F.260C, F.260D,
F.260E, F.260F, S.211A.
(2) Aeronautica Macchi S.p.A......... AL 60, AL 60-B, AL 60-F5, AL 60-
C5, AM-3.
(3) Aerostar Aircraft Corporation.... PA-60-600 (Aerostar 600), PA-60-
601 (Aerostar 601), PA-60-601P
(Aerostar 601P), PA-60-602P
(Aerostar 602P), PA-60-700P
(Aerostar 700P), 360, 400.
(4) Alexandria Aircraft, LLC......... 14-19, 14-19-2, 14-19-3, 14-19-
3A, 17-30, 17-31, 17-31TC, 17-
30A, 17-31A, 17-31ATC.
(5) Alliance Aircraft Group LLC...... 15A, 20, H-250, H-295 (USAFU-
10D), HT-295, H391 (USAFYL-24),
H391B, H-395 (USAFL-28A or U-
10B), H-395A, H-700, H-800, HST-
550, HST-550A (USAF AU-24A),
500.
(6) American Champion Aircraft Corp.. 402, 7GCA, 7GCB, 7KC, 7GCBA,
7GCAA, 7GCBC, 7KCAB, 8KCAB,
8GCBC.
(7) Sky International Inc............ A-1, A-1A, A-1B, S-1S, S-1T, S-2,
S-2A, S-2S, S-2C.
(8) B-N Group Ltd.................... BN-2, BN-2A, BN-2A-2, BN-2A-3, BN-
2A-6, BN-2A-8, BN-2A-8, BN-2A-
20, BN-2A-21, BN-2A-26, BN-2A-
27, BN-2B-20, BN-2B-21, BN-2A-
26, BN-2A-27, BN-2B-20, BN-2B-
21, BN-2B-26, BN-2B-27, BN-2T,
BN-2T-4R, BN-2A MK.III, BN2A MK.
III-2, BN2A MK. 111-3.
(9) Bellanca......................... 14-13, 14-13-2, 14-13-3, 14-13-
3W.
(10) Bombardier Inc.................. (Otter) DHC-3, DHC-6-1, DHC-6-
100, DHC-6-200, DHC-6-300.
(11) Cessna Aircraft Company......... 170, 170A, 170B, 172, 172A, 172B,
172C, 172D, 172E, 172F (USAF T-
41A), 172G, 172H (USAF T041A),
172I, 172K, 172L, 172M, 172N,
172P, 172Q, 172R, 172S, 172RG,
P172D, R172E (USAF T-41 B) (USAF
T-41 C AND D), R172F (USAF T-41
D), R175G, R172H (USAF T-41 D),
R172J, R172K, 175, 175A, 175B,
175C, 177, 177A, 177B, 177RG,
180, 180A, 180B, 180C, 180D,
180E, 180F, 180G, 180H, 180J,
180K, 182, 182A, 182B, 182C,
182D, 182E, 182F, 182G, 182H,
182J, 182K, 182L, 182M, 182N,
182P, 182Q, 182R, 182S, 182T,
R182, T182, TR182, T182T, 185,
185A, 185B, 185C, 185D, 185E,
A185E, A185F, 190, (LC-126A, B,
C) 195, 195A, 195B, 210, 210A,
210B, 210C, 210D, 210E, 210F,
T210F, 210G, T210G, 210H, T210H,
210J, T210J, 210K, T210K, 210L,
T210L, 210M, T210M, 210N, P210N,
T210N, 210R, P210R, T210R, 210-5
(205), 210-5A (205A), 206, P206,
P206A, P206B, P206C, P206D,
P206E, TP206A, TP206B, TP206C,
TU206D, TU206E, TU206F, TU206G,
206H, T206H, 207, 207A, T207,
T207A, 208, 208A, 208B, 310,
310A (USAF U-3A), 310B, 310C,
310D, 310E (USAF U-3B), 310F,
310G, 310H, E310H, 310I, 310J,
310J-1, E310J, 310K, 310L, 310N,
310P, T310P, 310Q, T310Q, 310R,
T310R, 320, 320A, 320B, 320C,
320D, 320E, 320F, 320-1, 335,
340, 340A, 336, 337, 337A (USAF
02B), 337B, T337B, 337C, 337E,
T337E, T337C, 337D, T337D, M337B
(USAF 02A), 337F, T337F, T337G,
337G, 337H, P337H, T337H, T337H-
SP, 401, 401A, 401B, 402, 402A,
402B, 402C, 411, 411A, 414,
414A, 421, 421A, 421B, 421C,
425, 404, 406, 441.
(12) Cirrus Design Corporation....... SR20, SR22.
(13) Commander Aircraft Company...... 112, 112TC, 112B, 112TCA, 114,
114A, 114B, 114TC.
(14) de Havilland Inc................ DHC-2 Mk. I, DHC-2 Mk.II, DHC-2
Mk. III.
(15) Dynac Aerospace Corporation..... (Volaire) 10, (Volaire) 10A,
(Aero Commander) 100, (Aero
Commander) 100A, (Aero
Commander) 100-180.
(16) Diamond Aircraft Industries..... DA 20-A1, DA20-C1, DA 40.
(17) Empressa Brasileira de EMB-110P1, EMB-110P2.
Aeronautica S.A. EMBRAER.
(18) Extra Flugzeugbau Gmbh.......... EA300, EA300L, EA300S, EA300/200,
EA-400.
(19) Fairchild Aircraft Corporation.. SA26-T, SA26-AT, SA226-T, SA226-
AT, SA226-T(B), SA227-AT, SA227-
TT, SA226-TC, SA227-AC (C-26A),
SA227-CC, SA227-DC (C-26B).
(20) Global Amphibians, LLC.......... Colonial C-1, Colonial C-2, Lake
LA-4, Lake LA-4A, Lake LA-4P,
Lake LA-4-200, Lake Model 250.
(21) Grob-Werke...................... G115, G115A, G115B, G115C,
G115C2, G115D, G115D2, G115EG,
G120A.
(22) Lancair Company................. LC40-550FG.
[[Page 60103]]
(23) LanShe Aerospace, LLC........... MAC-125C, MAC-145, MAC-145A, MAC-
145B.
(24) Learjet Inc..................... 23.
(25) Lockheed Aircraft Corporation... 18.
(26) Luscombe Aircraft Corporation... 11A, 11E.
(27) Maule Aerospace Technology Inc.. Bee Dee M-4, M-4, M-4C, M-4S, M-
4T, M-4180C, M-4-180S, M-4-180T,
M-4-210, M-4-210C, M-4-210S, M-4-
210T, M-4-220, M-4-220S, M-4-
220T, M-5-180C, M-5-200, M-5-
210C, M-5-210TC, M-5-220C, M-5-
235C, M-6-180, M-6-235, M-7-235,
MX-7-235, MX-7-180, MX-7-420,
MXT-7-180, MT-7-235, M-8-235, MX-
7-160, MXT-7-160, MX-7-180A, MXT-
7-180A, MX-7-180B, M-7-235B, M-7-
235A, M-7-235C, MX-7-180C, M-7-
260, MT-7-260, M-7-260C, M-7-
420AC, MX-7-160C, MX-7-180AC, M-
7-420A, MT-7-420.
(28) Mitsubishi Heavy Industries, Ltd MU-2B-25, MU-2B-35, MU-2B-26, MU-
2B-36, MU-2B-26A, MU-2B-36A, MU-
2B-40, MU-2B-60, MU-2B, MU-2B-
20, MU-2B-20, MU-2B-15.
(29) Mooney Airplane Company, Inc.... M20, M20A, M20B, M20C, M20D,
M20E, M20F, M20G, M20J, M20K,
M20L, M20M, M20R, M20S, M22.
(30) Moravan a.s..................... Z-242L, Z-143L.
(31) Navion Aircraft Company, Ltd.... NAVION, Navion (L-17A), Navion
(L17B), Navion (L-17C), Navion
B, Navion D, Navion E, Navion F,
Navion G, Navion H.
(32) New Piper Aircraft, Inc......... PA-12, PA-12S, PA-18, PA-18S, PA-
18 ``105'' (Special), PA-18S
``105'' (Special), PA-18A, PA-18
``125'' (Army L-21A), PA-18S
``125,'' PA-18AS ``125,'' PA-18
``135'' (Army L-21B), PA-18A
``135,'' PA-18S ``135,'' PA-18
``150,'' PA-18A ``150,'' PA-18S
``150,'' PA-18AS ``150,'' PA-19
(Army L-18B), PA-19S, PA-20, PA-
20S, PA-20 ``115,'' PA-20S
``115,'' PA-20 ``135,'' PA-20S
``135,'' PA-22, PA-22-108, PA-22-
135, PA-22S-135, PA-22-150, PA-
22S-150, PA-22-160, PA-22S-160,
PA-23, PA-23-160, PA-23-235, PA-
23-250, PA-E23-250, PA-24, PA-24-
250, PA-24-260, PA-24-400, PA-28-
140, PA-28-150, PA-28-151, PA-28-
160, PA-28-161, PA-28-180, PA-28-
235, PA-28S-160, PA-28R-180, PA-
28S-180, PA-28-181, PA-28R-200,
PA-28R-201, PA-28R-201T, PA-28RT-
201, PA-28RT-201T, PA-28-201T,
PA-28-236, PA-30, PA-39, PA-40,
PA-31P, PA-31T, PA-31T1, PA-
31T2, PA-31T3, PA-31P-350, PA-32-
260, PA-32-300, PA-32S-300, PA-
32R-300, PA-32RT-300, PA-32RT-
300T, PA-32R-301 (SP), PA-32R-
301 (HP), PA-32R-301T, PA-32-
301, PA-32-301T, PA-34-200, PA-
34-200T, PA-34-220T, PA-42, PA-
42-720, PA-42-1000, PA-42-720R,
PA-44-180, PA-44-180T, PA-46-
310P, PA-46-350P, PA-46-500TP.
(33) Ostmecklenburgische Flugzeugbau OMF-100-160.
GmgH.
(34) Piaggio Aero Industries S.p.A... P-180.
(35) Pilatus Aircraft Ltd............ PILATUS PC-12, PILATUS PC-12/45,
PC-6, PC-6-H1, PC-6-H2, PC-6/
350, PC-6/350-H1, PC-6/350-H2,
PC-6/A, PC-6/A-H1, PA-6/A-H2, PC-
6/B-H2, PC-6/B1-H2, PC-6/B2-H2,
PC-6/B2-H4, PC-6/C-H2, PC-6/C1-
H2, PC-7.
(36) Prop-Jets, Inc.................. 200, 200A, 200B, 200C, 200D, 400.
(37) Panstwowe Zakladv Lotnicze (PZL) PZL-104 WILGA 80, PZL-104M WILGA
2000, PZL-WARSZAWA, PZL-KOLIBER
150A, PZL-KOLIBER 160A.
(38) PZL WSK/Mielec Obrsk............ PZL M20 03, PZL M26 01.
(39) Raytheon........................ 35-33, 35-A33, 35-B33, 35-C33, 35-
C33A, E33, E33A, E33C, F33,
F33A, F33C, G33, H35, J35, K35,
M35, N35, P35, S35, V35, V35A,
V35B, 36, A36, A36TC, B36TC, 35,
A35, B35, C35, D35, E35, F35,
G35, 35R, F90, 76, 200, 200C,
200CT, 200T, A200, B200, B200C,
B200CT, B200T, 300, 300LW, B300,
B300C, 1900, 1900C, 1900D, A100-
1 (U-21J), A200 (C-12A), A200 (C-
12C), A200C (UC-12B), A200CT (C-
12D), A200CT (FWC-12D), A200CT
(RC-12D), A200CT (C-12F), A200CT
(RC-12G), A200CT (RC-12H),
A200CT (RC-12K), A200CT (RC-
12P), A200CT (RC-12Q), B200C (C-
12F), B200C (UC-12F), B200C (UC-
12M), B200C (C-12R), 1900C (C-
12J), 65, A65, A65-8200, 65-80,
65-A80, 65-A80-8800, 65-B80, 65-
88, 65-A90, 70, B90, C90, C90A,
E90, H90, 65-A90-1, 65-A90-2, 65-
A90-3, 65-A90-4, 95, B95, B95A,
D95A, E95, 95-55, 95-A55, 95-
B55, 95-B55A, 95-B55B (T-42A),
95-C55, 95-C55A, D55, D55A, E55,
E55A, 56TC, A56TC, 58, 58A, 58P,
58PA, 58TC, 58TCA, 99, 99A, 99A
(FACH), A99, A99A, B99, C99,
100, A100 (U-21F), A100A, A100C,
B100, 2000, 3000, 390, 19A, B19,
M19A, 23, A23, A23A, A23-19, A23-
24, B23, C23, A24, A24R, B24R,
C24R, 60, A60, B60, 18D, A18A,
A18D, S18D, SA18A, SA18D, 3N,
3NM, 3TM, JRB-6, D18C, D18S,
E18S, RC-45J (SNB-5P), E18S-
9700, G18S, H18, C-45G, TC-45G,
C-45H, TC-45H, TC-45J, UC-45J
(SNB-5), 50 (L-23A), B50 (L-
23B), C50, D50 (L-23E), D50A,
D50B, D50C, D50E-5990, E50 (L-
23D, RL-23D), F50, G50, H50,
J50, 45 (YT-34), A45 (T-34A or B-
45), D45 (T-34B).
(40) Rockwell International BC-1A, AT-6 (SNJ-2), AT-6A (SNJ-
Corporation. 3), AT-6B, AT-6C (SNJ-4), AT-6D
(SNJ-5), AT-6F (SNF-6), SNJ-7, T-
6G, NOMAD NA-260.
(41) Short Brothers & Harland Ltd.... SC-7 Series 2, SC-7 Series 3.
(42) Slingsby Aviation Ltd........... T67M260, T67M260-T3A.
(43) SOCATA--Group Aerospatiale...... TB9, TB10, TB20, TB21, TB200, TBM
700, M.S. 760, M.S. 760 A, M.S.
760 B, Rallye 100S, Rallye
150ST, Rallye 150T, Rallye 235E,
Rallye 235C, MS 880B, MS 885, MS
894A, MS 893A, MS 892A-150, MS
892E-150, MS 893E, MS 894E, GA-
7.
(44) Tiger AircraftLLC............... AA-1, AA-1A, AA-1B, AA-1C, AA-5,
AA-5A, AA-5B, AG-5B.
(45) Twin Commander Aircraft 500, 500-A, 500-B, 500-U, 500-S,
Corporation. 520, 560, 560-A, 560-E, 560F,
680, 680E, 680F, 680FL,
680FL(P), 680T, 680V, 680W, 681,
685, 690, 690A, 690B, 690C,
690D, 695, 695A, 695B, 720, 700.
(46) Univair Aircraft Corporation.... 108, 108-1, 108-2, 108-3, 108-5.
[[Page 60104]]
(47) Vulcanair S.p.A................. P68, P68B, P68C, P68C-TC, P68
``Observer,'' P68 ``Observer
2,'' P68TC ``Observer,''
AP68TP300 ``Spartacus,'' AP68TP
600 ``Viator''.
(48) Zenair Ltd...................... CH2000.
------------------------------------------------------------------------
What Is the Unsafe Condition Presented in This AD?
(d) This AD is the result of observations that the GTX 33/33D/
330/330D may detect, from other airplanes, the S1 (suppression)
interrogating pulse below the minimum trigger level (MTL) and, in
some circumstances, not reply. The GTX 33/33D/330/330D should still
reply even if it detects S1 interrogating pulses below the MTL. The
actions specified in this AD are intended to prevent interrogating
aircraft from possibly receiving inaccurate replies, due to
suppression, from aircraft equipped with the GTX 33/33D/330/330D
Mode S transponders when the pulses are below the minimum trigger
level (MTL). Software Upgrade Versions 3.03 and 3.06 correct a TAS,
TCAD, and TCAS I system ``whisper-shout'' problem that could
potentially lead to the aircraft not being visible at certain
ranges. TCAS II systems are not affected. The inaccurate replies
could result in reduced vertical separation.
What Must I Do To Address This Problem?
(e) To address this problem, you must do the following:
------------------------------------------------------------------------
Actions Compliance Procedures
------------------------------------------------------------------------
Install GTX 33/33D/330/330D Install the Follow GARMIN
Software Upgrade to at least software upgrade Mandatory
Version 3.03 or 3.06. within 180 days Software Service
after the Bulletin No.:
effective date of 0304, Rev B,
this AD, unless dated June 12,
already 2003 (Software
accomplished. Upgrade 3.03) or
GARMIN Mandatory
Software Service
Bulletin No.:
0409, July 19,
2004 (Software
Upgrade 3.06).
------------------------------------------------------------------------
May I Request an Alternative Method of Compliance?
(f) You may request a different method of compliance or a
different compliance time for this AD by following the procedures in
14 CFR 39.19. Unless FAA authorizes otherwise, send your request to
your principal inspector. The principal inspector may add comments
and will send your request to the Manager, Wichita Aircraft
Certification Office (ACO), FAA. For information on any already
approved alternative methods of compliance, contact Roger A. Souter,
FAA, Wichita Aircraft Certification Office (ACO), 1801 Airport Road,
Room 100, Wichita, Kansas 67209; telephone: 316-946-4134; facsimile:
316-946-4107; e-mail address: roger.souter@faa.gov.
May I Get Copies of the Documents Referenced in This AD?
(g) To get copies of the documents referenced in this AD,
contact GARMIN International Inc. 1200 East 151st Street, Olathe, KS
66062; telephone: 913-397-8200. To view the AD docket, go to the
Docket Management Facility; U.S. Department of Transportation, 400
Seventh Street, SW., Nassif Building, Room PL-401, Washington, DC,
or on the Internet at http://dms.dot.gov. The docket number is FAA
2004-18743.
Issued in Kansas City, Missouri, on September 29, 2004.
Dorenda D. Baker,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 04-22586 Filed 10-6-04; 8:45 am]
BILLING CODE 4910-13-P