[Federal Register: December 30, 2003 (Volume 68, Number 249)]
[Proposed Rules]
[Page 75174-75179]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr30de03-23]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. 2003-CE-39-AD]
RIN 2120-AA64
Airworthiness Directives; GARMIN International Inc. GTX 330 Mode
S Transponders and GTX 330D Diversity Mode S Transponders
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
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SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD)
for certain GARMIN International Inc. GTX 330/GTX 330D Mode S
transponders. This proposed AD would require you to install GTX 330/
330D Software Upgrade Version 3.03. This proposed AD is the result of
observations that the GTX 330 and GTX 330D may detect, from other
aircraft, the S1 (suppression) interrogating pulse below the Minimum
Trigger Level (MTL) and, in some circumstances, not reply. The GTX 330/
330D should still reply even if it detects
[[Page 75175]]
S1 interrogating pulses below the MTL. We are issuing this proposed AD
to prevent interrogating aircraft from possibly receiving inaccurate
replies due to suppression from aircraft equipped with the GTX 330/330D
Mode S Transponders when the pulses are below the MTL. The inaccurate
replies could result in reduced vertical separation or unsafe TCAS
resolution advisories.
DATES: We must receive any comments on this proposed AD by February 3,
2004.
ADDRESSES: Use one of the following to submit comments on this proposed
AD:
[sbull] By mail: FAA, Central Region, Office of the Regional
Counsel, Attention: Rules Docket No. 2003-CE-39-AD, 901 Locust, Room
506, Kansas City, Missouri 64106.
[sbull] By fax: (816) 329-3771.
[sbull] By e-mail: 9-ACE-7-Docket@faa.gov. Comments sent
electronically must contain ``Docket No. 2003-CE-39-AD'' in the subject
line. If you send comments electronically as attached electronic files,
the files must be formatted in Microsoft Word 97 for Windows or ASCII.
You may get the service information identified in this proposed AD
from GARMIN International Inc., 1200 East 151st Street, Olathe, KS
66062, 913-397-8200.
You may view the AD docket at FAA, Central Region, Office of the
Regional Counsel, Attention: Rules Docket No. 2003-CE-39-AD, 901
Locust, Room 506, Kansas City, Missouri 64106. Office hours are 8 a.m.
to 4 p.m., Monday through Friday, except Federal holidays.
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 written relevant data, views, or
arguments regarding this proposal. Send your comments to an address
listed under ADDRESSES. Include ``AD Docket No. 2003-CE-39-AD'' in the
subject line of your comments. If you want us to acknowledge receipt of
your mailed comments, send us a self-addressed, stamped postcard with
the docket number written on it. We will date-stamp your postcard and
mail it back to you.
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.
Discussion
What Events Have Caused This Proposed AD?
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. GARMIN
International Inc. suspected the suppression problem after observation
between GARMIN company aircraft that were equipped with the GTX 330 and
Ryan Traffic and Collision Alert Device (TCAD). Engineering bench tests
and test flights confirmed that this suppression problem existed.
What Are The Consequences If the Condition Is Not Corrected?
Interrogating aircraft could possibly receive inaccurate replies
due to suppression from aircraft equipped with the GTX 330/330D Mode S
Transponders when the pulses are below the MTL. The inaccurate replies
could result in reduced vertical separation or unsafe TCAS resolution
advisories.
Is There Service Information That Applies To This Subject?
GARMIN International Inc. has issued the Software Service Bulletin
No.: 0304, Rev B, dated June 12, 2003.
What Are the Provisions of This Service Information?
The service bulletin includes:
--Modification instructions for upgrading to software version 3.03 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. Therefore, we are proposing AD action.
What Would This Proposed AD Require?
This proposed AD would require you to incorporate the actions in
the previously-referenced service bulletin.
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 1300 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 cover all workhours and parts cost
associated with this modification under warranty. The proposed AD would
not impose any cost upon the owners/operators of any airplane that has
the GTX 330/330D Software Upgrade to Version 3.03 installed.
Compliance Time of This Proposed AD
What Would Be the Compliance Time of This Proposed AD?
The compliance time of this proposed AD is within 30 days after the
effective date of the AD.
Why Is the Compliance Time Presented in Calendar Time Instead of Hours
Time-In-Service (TIS)?
The unsafe condition exists or could develop on airplanes equipped
with the affected equipment regardless of airplane operation. For
example, the unsafe condition has the same chance of occurring on an
airplane with 50 hours TIS as it does on one with 5,000 hours TIS.
Therefore, we are presenting the compliance time of the proposed AD in
calendar time instead of hours TIS.
[[Page 75176]]
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, 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. 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 adding the following new
airworthiness directive (AD):
GARMIN International Inc.: Docket No. 2003-CE-39-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 February 3, 2004.
What Other ADs Are Affected By This Action?
(b) None.
What Products Are Affected by This AD?
(c) This AD affects GARMIN International Inc. GTX 330/330D 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, N-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.
[[Page 75177]]
(11) Cessna Aircraft................... 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 Aeronautica EMB-110P1, EMB-110P2.
S.A. EMBRAER.
(18) Extra Flugzeugbau Gmbh............ A300, 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.
(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.
[[Page 75178]]
(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, 65A80-
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 Corporation BC-1A, AT-6 (SNJ-2), AT-6A (SNJ-
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 Aircraft LLC................ 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-
Corporation. S, 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.
(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.
------------------------------------------------------------------------
[[Page 75179]]
What Is the Unsafe Condition Presented in This AD?
(d) 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 330/330D
Mode S Transponders when the pulses are below the Minimum Trigger
Level (MTL). The inaccurate replies could result in reduced vertical
separation or unsafe TCAS resolution advisories.
What Must I Do To Address This Problem?
(e) To address this problem, you must accomplish the following:
------------------------------------------------------------------------
Action Compliance Procedures
------------------------------------------------------------------------
Install GTX 330/330D Install the software Follow GARMIN
software upgrade to version upgrade within 30 International Inc.
3.03. days after the Service Bulletin
effective date of No.: 0304, Rev B,
this AD, unless dated June 12,
already 2003.
accomplished.
------------------------------------------------------------------------
How Do I Get Copies of the Documents Referenced in This AD?
(g) You may get copies of the documents referenced in this AD
from GARMIN International Inc. 1200 East 151st Street, Olathe, KS
66062. You may view these documents at FAA, Central Region, Office
of the Regional Counsel, 901 Locust, Room 506, Kansas City, Missouri
64106.
Issued in Kansas City, Missouri, on December 19, 2003.
Michael Gallagher,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 03-31978 Filed 12-29-03; 8:45 am]
BILLING CODE 4910-13-P