[Federal Register Volume 69, Number 39 (Friday, February 27, 2004)]
[Rules and Regulations]
[Pages 9277-9282]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 04-4375]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 2003-CE-40-AD]
RIN 2120-AA64


Airworthiness Directives; Cessna Aircraft Company 120, 140, 140A, 
150, F150, 170, 172, F172, FR172, P172D, 175, 177, 180, 182, 185, 
A185E, 190, 195, 206, P206, U206, TP206, TU206, 207, T207, 210, T210, 
336, 337, and T337 Series Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Supplemental notice of proposed rulemaking (NPRM); reopening of 
the comment period.

-----------------------------------------------------------------------

SUMMARY: The FAA proposes to revise an earlier proposed airworthiness 
directive (AD) to supersede AD 86-26-04 that applies to certain Cessna 
Aircraft Company (Cessna) 120, 140, 140A, 150, F150, 170, 172, F172, 
FR172, P172D, 175, 177, 180, 182, 185, A185E, 190, 195, 205, 205A, 206, 
P206, P206E, TP206A, TU206, TU206E, U206, U206E, 207, T207, 210, T210, 
336, 337, and T337 series airplanes. The earlier NPRM proposed to 
retain the actions of AD 86-26-04, add additional airplanes to the 
applicability section, and incorporated revised manufacturer service 
information. This proposed AD is the result of the FAA inadvertently 
omitting 10 affected airplane serial numbers for Model TU206D airplanes 
from the applicability section of the earlier NPRM. This proposed AD 
would retain the actions of earlier NPRM and add additional airplanes 
to the applicability section of this proposed AD. Since these actions 
impose an additional burden over that proposed in the earlier NPRM, we 
are reopening the comment period to allow the public the chance to 
comment on these additional actions.

DATES: We must receive any comments on this proposed AD by April 9, 
2004.

ADDRESSES: Use one of the following to submit comments on this proposed 
AD:
     By mail: FAA, Central Region, Office of the Regional 
Counsel, Attention: Rules Docket No. 2003-CE-40-AD, 901 Locust, Room 
506, Kansas City, Missouri 64106.
     By fax: (816) 329-3771.
     By e-mail: [email protected]. Comments sent 
electronically must contain ``Docket No. 2003-CE-40-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 Cessna Aircraft Company, Product Support P.O. Box 7706, Wichita, 
Kansas 67277; telephone: (316) 517-5800; facsimile: (316) 942-9006.
    You may view the AD docket at FAA, Central Region, Office of the 
Regional Counsel, Attention: Rules Docket No. 2003-CE-40-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: Gary D. Park, Aerospace Engineer, FAA, 
Wichita Aircraft Certification Office, 1801 Airport Road, Room 100, 
Mid-Continent Airport, Wichita, Kansas 67209; telephone: (316) 946-
4123; facsimile: (316) 946-4107.

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-40-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

[[Page 9278]]

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 Is the Background of the Subject Matter?

    Cessna designed add-on shoulder harness assembly accessory kits for 
the pilot/co-pilot seats for certain Cessna airplanes. These shoulder 
harness assemblies incorporate a retainer spring in the adjuster on the 
upper and lower shoulder harness. The retainer spring may have been 
inadvertently installed on the belt friction pin. This installation of 
the spring in the upper shoulder harness adjuster will not allow the 
belt webbing to lock in place.
    This caused us to issue AD 86-26-04, Amendment 39-5503 (52 FR 520, 
January 7, 1987). AD 86-26-04 currently requires the following on 
certain Cessna 120, 140, 140A, 150, F150, 170, 172, F172, FR172, P172D, 
175, 177, 180, 182, 185, A185E, 190, 195, 205, 205A, 206, P206, P206E, 
TP206A, TU206, TU206E, U206, U206E, 207, T207, 210, T210, 336, 337, and 
T337 series airplanes:

 Inspecting the upper shoulder harness adjuster for the 
presence of a retainer spring;
 If retainer spring is found, removing the retainer spring; and
 Stamping out the--401 identification number.

What Happened Since AD 86-26-04 To Initiate the Earlier NPRM?

    We received reports that additional airplanes have the same unsafe 
condition. Cessna revised the service information to include these 
additional airplanes.
    Cessna also revised the service information to correct the 
reference to the part number (P/N) of the shoulder harness adjusters. 
The P/N referenced is referenced as 44030-401 in Cessna Single Engine 
Service Bulletin SEB86-8 and Cessna Multi-engine Service Bulletin 
MEB86-22, both dated November 21, 1986. The correct P/N is 443030-401.

What Is the Potential Impact if FAA Took No Action?

    If not corrected, the shoulder harness could fail to maintain 
proper belt length adjustment and tension. Such failure could result in 
pilot/co-pilot injury.

Has FAA Taken Any Action to This Point?

    We issued a proposal to amend part 39 of the Federal Aviation 
Regulations (14 CFR part 39) to include an AD that would apply to 
certain Cessna Models 120, 140, 140A, 150, F150, 170, 172, F172, FR172, 
P172D, 175, 177, 180, 182, 185, A185E, 190, 195, 206, P206, U206, 
TP206, TU206, 207, T207, 210, T210, 336, 337, and T337 series 
airplanes. This proposal was published in the Federal Register as a 
notice of proposed rulemaking (NPRM) on November 13, 2003 (68 FR 
64290). The NPRM proposed to supersede AD 86-26-04 with a new AD that 
would require you to:
 Inspect the upper shoulder harness adjuster for the presence 
of a retainer spring;
 If retainer spring is found, remove the retainer spring; and
 Stamp out the--401 identification number.

Was the Public Invited To Comment?

    The FAA encouraged interested persons to participate in developing 
this amendment. We did not receive any comments on the proposed rule or 
on our determination of the cost to the public.

What Events Have Caused FAA To Issue a Supplemental NPRM?

    The FAA inadvertently omitted 10 affected airplane serial numbers 
for Model TU206D airplanes from the applicability section of the 
earlier NPRM.

FAA's Determination and Requirements of This Proposed AD

What Has FAA Decided?

    After examining the circumstances and reviewing all available 
information related to the incidents described above, we have 
determined that:
 The unsafe condition referenced in this document exists or 
could develop on other Cessna Models 120, 140, 140A, 150, F150, 170, 
172, F172, FR172, P172D, 175, 177, 180, 182, 185, A185E, 190, 195, 206, 
P206, U206, TP206, TU206, 207, T207, 210, T210, 336, 337, and T337 
series airplanes of the same type design that are on the U.S. registry;
 We should change the NPRM to add additional affected airplane 
serial numbers to the applicability section; and
 We should take AD action to correct this unsafe condition.

The Supplemental NPRM

How Will the Changes to the NPRM Impact the Public?

    Proposing that the NPRM apply to additional Model TU206D airplanes 
goes beyond the scope of what was originally proposed in the NPRM. 
Therefore, we are reopening the comment period and allowing the public 
the chance to comment on these additional actions.

What Are the Provisions of the Supplemental NPRM?

    This proposed AD would require you to:

 Inspect the upper shoulder harness adjuster for the presence 
of a retainer spring;
 If retainer spring is found, remove the retainer spring; and
 Stamp out the--401 identification number.

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 75,329 airplanes in the 
U.S. registry.

What Would Be the Cost Impact of This Proposed AD on Owners/Operators 
of the Affected Airplanes?

    We estimate the following costs to accomplish this proposed 
inspection:

----------------------------------------------------------------------------------------------------------------
                                                          Total cost per
            Labor cost                  Parts cost           airplane          Total cost on U.S.  operators
----------------------------------------------------------------------------------------------------------------
1 workhour x $65 per hour = $65..  No parts required...             $65   $65 x 75,329 = $4,896,385
----------------------------------------------------------------------------------------------------------------


[[Page 9279]]

    We estimate the following costs to accomplish any necessary 
modification that would be required based on the results of this 
proposed inspection. We have no way of determining the number of 
airplanes that may need this modification:

------------------------------------------------------------------------
                                                          Total cost per
            Labor cost                  Parts cost           airplane
------------------------------------------------------------------------
1 workhour x $65 per hour = $65..  No parts required...             $65
------------------------------------------------------------------------

What Is the Difference Between the Cost Impact of the Earlier NPRM and 
the Cost Impact of This Proposed Supplemental NPRM?

    The difference is the addition of 10 airplanes to the applicability 
section of this proposed AD. There is no difference in cost to perform 
the proposed inspection and the proposed modification.

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-40-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) 86-26-04, Amendment 39-5503 (52 FR 520, January 7, 1987), and by 
adding a new AD to read as follows:

Cessna Aircraft Company: Docket No. 2003-CE-40-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 April 9, 2004.

What Other ADs Are Affected by This Action?

    (b) This AD supersedes AD 86-26-04, Amendment 39-5503.

What Airplanes Are Affected by This AD?

    (c) This AD affects the following airplane models and serial 
numbers that are certificated in any category and incorporate one of 
the Cessna accessory kits specified in paragraph (d) of this AD.

------------------------------------------------------------------------
                 Model                              Serial No.
------------------------------------------------------------------------
(1) 120................................  8000 through 15075.
(2) 140................................  8000 through 15075.
(3) 140A...............................  15200 through 15724.
(4) 150................................  617, 17001 through 17999, and
                                          59001 through 59018.
(5) 150A...............................  628 and 15059019 through
                                          15059350.
(6) 150B...............................  15059351 through 15059700.
(7) 150C...............................  15059701 through 15060087.
(8) 150D...............................  15060088 through 15060772.
(9) 150E...............................  644 and 15060773 through
                                          15061532.
(10) 150F..............................  15061533 through 15064532.
(11) 150G..............................  15064533 through 15064969 and
                                          15064971 through 15067198.
(12) 150H..............................  649 and 15067199 through
                                          15069308.
(13) 150J..............................  15069309 through 15071128.
(14) 150K..............................  15071129 through 15072003.
(15) 170...............................  18000 through 18729.
(16) 170A..............................  18730 through 19400 and 19402
                                          through 20266.
(17) 170B..............................  20267 through 20999 and 25000
                                          through 27169.
(18) 172...............................  610, 612, 615, 28000 through
                                          29999, 36000 through 36999,
                                          and 46001 through 46754.
(19) 172A..............................  622, 625, and 46755 through
                                          47746.
(20) 172B..............................  630 and 17247747 through
                                          17248734.
(21) 172C..............................  17248735 through 17249544.
(22) 172D..............................  17249545 through 17250572.
(23) 172E..............................  639 and 17250573 through
                                          17251822.
(24) 172F..............................  17251823 through 17253392.
(25) 172G..............................  17253393 through 17254892.
(26) 172H..............................  638, 17254893 through 17256492,
                                          and 17256494 through 17256512.
(27) 172I..............................  17256513 through 17257161.

[[Page 9280]]

 
(28) 172K..............................  17257162 through 17258486 and
                                          17258487 through 17259223.
(29) P172D.............................  P17257120 through P17257188.
(30) 175...............................  626, 640, 28700A, and 55001
                                          through 56238.
(31) 175A..............................  619 and 56239 through 56777.
(32) 175B..............................  17556778 through 17557002.
(33) 175C..............................  17557003 through 17557119.
(34) 177...............................  661, 17700001, and 17700003
                                          through 17701164.
(35) 177A..............................  17701165 through 17701370.
(36) 177B..............................  17701371 through 17701471 and
                                          17701473 through 17701530.
(37) 180...............................  604, 614, 30000 through 32661.
(38) 180A..............................  32662 through 32999 and 50001
                                          through 50355.
(39) 180B..............................  50356 through 50661.
(40) 180C..............................  624 and 50662 through 50911.
(41) 180D..............................  18050912 through 18051063.
(42) 180E..............................  18051064 through 18051183.
(43) 180F..............................  18051184 through 18051312.
(44) 180G..............................  18051313 through 18051445.
(45) 180H..............................  18051446 through 18052175.
(46) 182...............................  613 and 33000 through 33842.
(47) 182A..............................  33843 through 34753, 34755
                                          through 34999, and 51001
                                          through 51556.
(48) 182B..............................  34754, 51557 through 51622, and
                                          51624 through 52358.
(49) 182C..............................  631 and 52359 through 53007.
(50) 182D..............................  51623 and 18253008 through
                                          18253598.
(51) 182E..............................  18253599 through 18254423.
(52) 182F..............................  18254424 through 18255058.
(53) 182G..............................  18255059 through 18255844.
(54) 182H..............................  634 and 18255846 through
                                          18256684.
(55) 182J..............................  18256685 through 18257625.
(56) 182K..............................  18255845, 18257626 through
                                          18257698, and 18257700 through
                                          18258505.
(57) 182L..............................  18258506 through 18259305.
(58) 182M..............................  662, 18257699, and 18259306
                                          through 18260055.
(59) 182N..............................  18260056 through 18260445.
(60) 185...............................  632 and 185-0001 through 185-
                                          0237.
(61) 185A..............................  185-0238 through 185-0512.
(62) 185B..............................  185-0513 through 185-0653.
(63) 185C..............................  185-0654 through 185-0776.
(64) 185D..............................  185-0777 through 185-0967.
(65) 185E..............................  185-0968 through 185-1149.
(66) A185E.............................  185-0968 through 185-1599 and
                                          18501600 through 18501832.
(67) 190...............................  7001 through 7999 and 16000
                                          through 16183.
(68) 195...............................  7001 through 7999 and 16000
                                          through 16183.
(69) 206...............................  206-0001 through 206-0275.
(70) P206..............................  P206-0001 through P206-0160.
(71) P206A.............................  P206-0161 through P206-0306.
(72) P206B.............................  P206-0307 through P206-0419.
(73) P206C.............................  P206-0420 through P206-0519.
(74) P206D.............................  P206-0520 through P206-0603.
(75) P206E.............................  P20600604 through P20600647.
(76) U206..............................  U206-0276 through U206-0437.
(77) U206A.............................  U206-0438 through U206-0656.
(78) U206B.............................  U206-0657 through U206-0914.
(79) U206C.............................  U206-0915 through U206-1234.
(80) U206D.............................  U206-1235 through U206-1444 and
                                          U20601445 through U20601587.
(81) TP206A............................  P206-0161 through P206-0306.
(82) TP206B............................  P206-0307 through P206-0419.
(83) TP206C............................  P206-0420 through P206-0519.
(84) TP206D............................  P206-0520 through P206-0603.
(85) TP206E............................  P20600604 through P20600647.
(86) TU206A............................  U206-0487 through U206-0656.
(87) TU206B............................  U206-0657 through U206-0914.
(88) TU206C............................  U206-0915 through U206-1234.
(89) TU206D............................  U206-1235 through U206-1444 and
                                          U20601445 through U20601587.
(90) 207...............................  20700001 through 20700190.
(91) T207..............................  20700001 through 20700190.
(92) 210...............................  618 and 57001 through 57575.
(93) 210-5 (205).......................  641, 648, and 205-0001 through
                                          205-0480.
(94) 210-5 (205A)......................  205-0481 through 205-0577.
(95) 210A..............................  616 and 21057576 through
                                          21057840.
(96) 210B..............................  21057841 through 21058085.
(97) 210C..............................  21058086 through 21058139 and
                                          21058141 through 21058220.
(98) 210D..............................  21058221 through 21058510.
(99) 210E..............................  21058511 through 21058715.

[[Page 9281]]

 
(100) 210F.............................  21058716 through 21058818.
(101) 210G.............................  21058819 through 21058936.
(102) 210H.............................  21058937 through 21059061.
(103) 210J.............................  21059062 through 21059199.
(104) 210K.............................  21059200 through 21059351.
(105) T210F............................  T210-0001 through T210-0197.
(106) T210G............................  T210-0198 through T210-0307.
(107) T210H............................  T210-0308 through T210-0392.
(108) T210J............................  T210-0393 through T210-0454.
(109) T210K............................  21059200 through 21059351.
(110) F150G............................  F150-0068 through F150-0219.
(111) F150H............................  F150-0220 through F150-0389.
(112) F150J............................  F150-0390 through F150-0529.
(113) F150K............................  F15000530 through F15000658.
(114) F172D............................  F172-0001 through F172-0018.
(115) F172E............................  F172-0019 through F172-0085.
(116) F172F............................  F172-0086 through F172-0179.
(117) F172G............................  F172-0180 through F172-0319.
(118) F172H............................  F172-0320 through F172-0654 and
                                          F17200655 through F17200754.
(119) FR172E...........................  FR17200001 through FR17200060.
(120) FR172F...........................  FR17200061 through FR17200145.
(121) FR172G...........................  FR17200146 through FR17200225.
(122) 336..............................  633, 636, and 336-0001 through
                                          336-0195.
(123) 337..............................  647 and 337-0002 through 337-
                                          0239.
(124) 337A.............................  337-0240 through 337-0305, 337-
                                          0307 through 337-0469, and 337-
                                          0471 through 337-0525.
(125) 337B.............................  656, 337-0001, 337-0470, 337-
                                          0526 through 337-0568, and 337-
                                          0570 through 337-0755.
(126) 337C.............................  337-0756 through 337-0978.
(127) 337D.............................  337-0979 through 337-1193.
(128) 337E.............................  33701194 through 33701316.
(129) T337B............................  337-0001, 337-0470, 337-0526
                                          through 337-0568, and 37-0570
                                          through 337-0755.
(130) T337C............................  337-0756 through 337-0978.
(131) T337D............................  337-0979 through 337-1193.
(132) T337E............................  33701194 through 33701316.
------------------------------------------------------------------------

What Cessna Accessory Kits Are Affected by This AD?

    (d) The following is a list of the affected Cessna accessory 
kits:

Cessna Accessory Kit

AK140-10
AK150-7
AK150-121
AK170-10
AK177-10
AK182-75
AK195-10
AK210-77
AK210-93
AK210-171
AK210-172
AK210-173
AK210-174
AK336-32
AK336-36
AK336-103

What Is the Unsafe Condition Presented in This AD?

    (e) The actions specified in this AD are intended to prevent 
slippage of the pilot/co-pilot shoulder harness, which could result 
in failure of the shoulder harness to maintain proper belt length 
adjustment and tension. Such failure could result in pilot/co-pilot 
injury.

What Must I Do To Address This Problem?

    (f) To address this problem, you must do the following, unless 
already done:

------------------------------------------------------------------------
           Actions                 Compliance            Procedures
------------------------------------------------------------------------
(1) Inspect only the upper    Within the next 25    Follow Cessna Single
 shoulder harness adjuster     hours time-in-        Engine Service
 (part number (P/N) 443030-    service (TIS) after   Bulletin SEB86-8,
 401) for the presence of a    the effective date    Revision 1, and
 retainer spring.              of this AD.           Cessna Multi-engine
                                                     Service Bulletin
                                                     MEB 86-22, Revision
                                                     1, both dated July
                                                     28, 2003.
(2) If a retainer spring is   Prior to further      Follow Cessna Single-
 found during the inspection   flight after the      Engine Service
 of the upper shoulder         effective date of     Bulletin SEB86-8,
 harness adjuster (P/N         this AD.              Revision 1, and
 443030-401) required in                             Cessna Multi-engine
 paragraph (f)(1) of this                            Service Bulletin
 AD:                                                 MEB 86-22, Revision
                                                     1, both dated July
                                                     28, 2003.
    (i) remove the spring by
     cutting each side; and
    (ii) stamp out the -401
     identification number.
(3) If a retainer spring is   Prior to further      Follow Cessna Single
 not found during the          flight after the      Engine Service
 inspection of the upper       effective date of     Bulletin SEB86-8,
 shoulder harness adjuster     this AD.              Revision 1, and
 (P/N 443030-401) required                           Cessna Multi-engine
 in paragraph (f)(1) of this                         Service Bulletin
 AD, no additional action is                         MEB 86-22, Revision
 required.                                           1, both dated July
                                                     28, 2003.

[[Page 9282]]

 
(4) Only incorporate Cessna   As of the effective   Follow Cessna Single
 Accessory Kits identified     date of this AD.      Engine Service
 in paragraph (d) of this AD                         Bulletin SEB86-8,
 that have been inspected                            Revision 1, and
 and modified in accordance                          Cessna Multi-engine
 with paragraphs (f)(1),                             Service Bulletin
 (f)(2), (f)(2)(i), and                              MEB 86-22, Revision
 (f)(2)(ii) of this AD.                              1, both dated July
                                                     28, 2003.
------------------------------------------------------------------------

    (g) If you did the actions of this AD using Cessna Single Engine 
Service Bulletin SEB86-8 and Cessna Multi-engine Service Bulletin 
MEB86-22, both dated November 21, 1986, no further action is 
required as long as you used shoulder harness adjuster, P/N 443030-
401.

May I Request an Alternative Method of Compliance?

    (h) 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, Manager, Wichita Aircraft 
Certification Office (ACO), FAA. For information on any already 
approved alternative methods of compliance, contact Gary D. Park, 
Aerospace Engineer, FAA, Wichita Aircraft Certification Office, 1801 
Airport Road, Room 100, Mid-Continent Airport, Wichita, Kansas 
67209; telephone: (316) 946-4123; facsimile: (316) 946-4107.
    (i) You may get copies of the documents referenced in this AD 
from Cessna Aircraft Company, Product Support P.O. Box 7706, 
Wichita, Kansas 67277; telephone: (316) 517-5800; facsimile: (316) 
942-9006. 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 February 19, 2004.
Dorenda D. Baker,
Manager, Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 04-4375 Filed 2-26-04; 8:45 am]
BILLING CODE 4910-13-P