TDATA NOTE: As published,  the text in the Procedures column of Table 2 in
            paragraph (g)(1) of this  AD incorrectly states "... fabricate
            the placard required  in  paragraph (g)(1)(i) of this AD ...",
            and the text should  refer  to  paragraph (g)(1)(ii).  In  all
            other respects, the original document remains the same.

(a) EFFECTIVE DATE

This AD is effective September 12, 2011.

(b) AFFECTED ADS

This  AD  revises  AD  2009-10-09 R1,  Amendment  39-16074  (74  FR 57408,
November 6, 2009).

(c) APPLICABILITY

This AD applies to the  following airplane models and serial  numbers that
are certificated in any category:

                            TABLE 1 - APPLICABILITY
    ______________________________________________________________________
    MODELS                      SERIAL NUMBERS
    ______________________________________________________________________
    (1) 150F                    15061533 through 15064532

    (2) 150G                    15064533 through 15064969 and 15064971
                                through 15067198

    (3) 150H                    15067199 through 15069308 and 649

    (4) 150J                    15069309 through 15071128

    (5) 150K                    15071129 through 15072003

    (6) 150L                    15072004 through 15075781

    (7) 150M                    15075782 through 15079405

    (8) A150K                   A1500001 through A1500226

    (9) A150L                   A1500227 through A1500432 and A1500434
                                through A1500523

    (10) A150M                  A1500524 through A1500734 and 15064970

    (11) F150F                  F150-0001 through F150-0067

    (12) F150G                  F150-0068 through F150-0219

    (13) F150H                  F150-0220 through F150-0389

    (14) F150J                  F150-0390 through F150-0529

    (15) F150K                  F15000530 through F15000658

    (16) F150L                  F15000659 through F15001143

    (17) F150M                  F15001144 through F15001428

    (18) FA150K                 FA1500001 through FA1500081

    (19) FA150L                 FA1500082 through FA1500120

    (20) FA150L or FRA150L      FA1500121 through FA1500261 that are
                                equipped with FKA150-2311 and FKA150-2316,
                                or FRA1500121 through FRA1500261

    (21) FA150M or FRA150M      FA1500262 through FA1500336 that are
                                equipped with FKA150-2311 and FKA150-2316,
                                or FRA1500262 through FRA1500336

    (22) 152                    15279406 through 15286033

    (23) A152                   A1520735 through A1521049, A1500433, and
                                681

    (24) F152                   F15201429 through F15201980

    (25) FA152                  FA1520337 through FA1520425
    ______________________________________________________________________

NOTE: AD 2009-10-09  R1 (74  FR 57408,  November 6,  2009)  clarified  the
applicability of AD  2009-10-09 (74 FR  22429, May 3,  2009), eliminated a
duplicate requirement  for replacement  of safety  wire with  jamnuts, and
clarified  the   intent  of   the  conditional   acceptability  of   using
modification kit part number  (P/N) SK152-25 as a  terminating requirement
to the AD. No further action  is required for those already in  compliance
with AD 2009-10-09 R1, which  included verification of full rudder  travel
as part of the kit work.

(d) SUBJECT

Joint Aircraft System Component (JASC)/Air Transport Association (ATA)  of
America Code 2720, Rudder Control System.

(e) UNSAFE CONDITION

Aircraft in full conformity with type design can exceed the travel  limits
set by the rudder stops. We are issuing this AD to prevent the rudder from
traveling past the normal travel limit. Operation in this non-certificated
control position is unacceptable and could cause undesirable consequences,
such as contact between the rudder and the elevator.

(f) COMPLIANCE

Comply with this AD within the compliance times specified, unless  already
done.

(g) ACTIONS

To address this  problem, you must  do either the  actions in option  1 or
option 2 of this AD, unless already done:

                 TABLE 2 – ACTIONS, COMPLIANCE AND PROCEDURES
    ______________________________________________________________________


    ACTIONS » » »

    (1) Option 1: For all airplanes that do not have modification kits P/N
        SK152-25B or P/N SK152-24B installed (or the other kits allowed by
        Table 3), do the following:

    (i) Insert the following text into the Limitations section of the FAA
        approved  airplane  flight  manual  (AFM),  and  pilot’s operating
        handbook (POH):
        "INTENTIONAL   SPINS  AND   OTHER  ACROBATIC/AEROBATIC   MANEUVERS
        PROHIBITED  PER AD  2009-10-09. NOTE:  THIS AD  DOES NOT  PROHIBIT
        PERFORMING INTENTIONAL STALLS."

    (ii) Fabricate  a  placard (using at least 1/8-inch letters) with  the
         following words and install  the  placard on the instrument panel
         within the pilot’s clear view:
         "INTENTIONAL  SPINS   AND  OTHER   ACROBATIC/AEROBATIC  MANEUVERS
         PROHIBITED PER AD 2009-10-09."

    (iii) The AFM and POH limitations in paragraph (g)(1)(i) of the AD and
          the placard in  paragraph (g)(1)(ii) of  this AD may  be removed
          after either paragraph (g)(2)(i) or paragraph (g)(2)(ii) of this
          AD is done.

                COMPLIANCE » » »

                Within  the  next 100  hours  time-in-service (TIS)  after
                December 11,  2009 (the  effective date  retained from  AD
                2009-10-09 R1 (74 FR 57408, November 6, 2009)), or  within
                the next 12 months after December 11, 2009 (the  effective
                date  retained from  AD 2009-10-09  R1), whichever  occurs
                first.

                            PROCEDURES » » »

                            A person authorized to perform maintenance  as
                            specified  in  14  CFR  section  43.3  of  the
                            Federal  Aviation  Administration  Regulations
                            (14 CFR 43.3) is required to make the AFM  and
                            POH changes, fabricate the placard required in
                            paragraph (g)(1)(ii) of this  AD, and  make an
                            entry  into   the  aircraft   logbook  showing
                            compliance  with  the portion  of  the AD  per
                            compliance with 14 CFR 43.9.
    ______________________________________________________________________


    ACTIONS » » »

    (2) Option 2: Install a rudder stop modification kit:

    (i) For airplanes with  a  forged bulkhead,  replace the rudder stops,
        rudder stop bumpers, and  attachment hardware with the  new rudder
        stop modification kit P/N SK152-25B.

    (ii) For airplanes with  a sheet metal bulkhead,  replace  the  rudder
         stops, rudder stop bumpers, and attachment hardware with the  new
         rudder stop modification kit P/N SK152-24B.

    (iii) Refer  to  Table 3  in  paragraph  (g)  of  this  AD  for  other
          applicable kit P/Ns.

                COMPLIANCE » » »

                Within the next 100 hours TIS after December 11, 2009 (the
                effective  date  retained  from AD  2009-10-09  R1  (74 FR
                57408, November 6,  2009)), or within  the next 12  months
                after December 11, 2009 (the effective date retained  from
                AD 2009-10-09 R1), whichever occurs first.

                            PROCEDURES » » »

                            Follow   Cessna   Aircraft   Company   Service
                            Bulletin SEB01-1, Revision 1,  dated March 22,
                            2011;  and,   as  applicable,   either  Cessna
                            Aircraft Company Service Kit SK152-25B,  dated
                            March  22,  2011, or  Cessna  Aircraft Company
                            Service Kit SK152-24B, dated March 22, 2011.
    ______________________________________________________________________

(h) KIT PART NUMBER APPLICABILITY

Table 3 of this AD identifies when a kit P/N that has already been ordered
may be used to comply with  this AD. All future orders received  by Cessna
for  kits  P/Ns  SK152-24,  SK152-25,  SK152-24A,  and  SK  152-25A   will
automatically be filled with P/Ns SK152-24B and SK152-25B, respectively.

                         TABLE 3 - KIT APPLICABILITY
    ______________________________________________________________________
                                       CAN IT BE INSTALLED TO COMPLY WITH
                                       THIS AD, OR WILL CREDIT BE GIVEN
                                       FOR COMPLIANCE WITH PREVIOUS
    KIT P/N        TYPE OF BULKHEAD    REVISIONS OF THIS AD?
    ______________________________________________________________________
    (1) SK152-24      sheet metal      NO

    (2) SK152-25      forged           ONLY if washer P/N NAS1149F0332P is
                                       used (and this is recorded in the
                                       maintenance log), AND full rudder
                                       travel can be verified.

    (3) SK152-24A     sheet metal      ONLY if full rudder travel can be
                                       verified.

    (4) SK152-25A     forged           ONLY if full rudder travel can be
                                       verified.

    (5) SK152-24B     sheet metal      YES

    (6) SK152-25B     forged           YES
    ______________________________________________________________________

(i) CREDIT FOR ACTIONS ACCOMPLISHED USING PREVIOUS SERVICE INFORMATION

Credit will be given  for the actions in  paragraphs (g)(1) and (g)(2)  of
this AD if  already done and  you were able  to verify full  rudder travel
before the effective date  of this AD per  AD 2009-10-09 R1, Amendment  39
-16074 (74 FR  57408, November 6,  2009); Cessna Aircraft  Company Service
Bulletin  SEB01-1,  dated January  22,  2001; and,  as  applicable, either
Cessna Aircraft Company Service Kit SK152-25A, Revision A, dated  February
9, 2001,  or Cessna  Aircraft Company  Service Kit  SK152-24A, Revision A,
dated March 9, 2001.

(j) ALTERNATIVE METHODS OF COMPLIANCE (AMOCS)

(1) The Manager, Wichita ACO, FAA,  has the authority to approve AMOCs for
    this AD, if requested using the  procedures found in 14 CFR 39.19.  In
    accordance with  14 CFR  39.19, send  your request  to your  principal
    inspector or local Flight  Standards District Office, as  appropriate.
    If sending information directly to the manager of the ACO, send it  to
    the  attention of  the person  identified in  the Related  Information
    section of this AD.

(2) Before using any  approved AMOC,  notify  your  appropriate  principal
    inspector, or lacking a principal inspector, the manager of the  local
    flight standards district office/certificate holding district office.

(3) AMOCs  approved  for  AD 2009-10-09 (74 FR 22429, May 3, 2009) and  AD
    2009-10-09 R1 (74  FR 57408, November  6, 2009) are  approved as AMOCs
    for this AD.

(k) RELATED INFORMATION

For  more  information  about  this  AD,  contact  Ann  Johnson, Aerospace
Engineer, FAA, Wichita Aircraft  Certification Office, 1801 Airport  Road,
Room 100,  Wichita, Kansas  67209; telephone:  (316) 946-4105;  fax: (316)
946-4107; email: ann.johnson@faa.gov.

(l) MATERIAL INCORPORATED BY REFERENCE

(1) You  must  use  the  following  service  information to do the actions
    required by this AD, unless  the AD specifies otherwise. The  Director
    of the Federal Register approved the incorporation by reference  (IBR)
    under 5  U.S.C. 552(a)  and 1  CFR part  51 of  the following  service
    information on September 12, 2011:

(i) Cessna Aircraft Company Service Bulletin SEB01-1,  Revision  1,  dated
    March 22, 2011;

(ii) Cessna Aircraft Company Service Kit SK152-25B,  dated March 22, 2011;
     and

(iii) Cessna Aircraft Company Service Kit SK152-24B, dated March 22, 2011.

(2) For service information identified in this AD, contact Cessna Aircraft
    Company, Product Support, P.O. Box 7706, Wichita, KS 67277; telephone:
    (316) 517-5800; fax: (316) 517-7271; Internet: http://www.cessna.com.

(3) You may review copies  of  the  service information at the FAA,  Small
    Airplane Directorate,  901 Locust,  Kansas City,  Missouri 64106.  For
    information on  the availability  of this  material at  the FAA,  call
    (816) 329-4148.

(4) You may  also  review  copies  of  the  service  information  that  is
    incorporated  by  reference  at  the  National  Archives  and  Records
    Administration (NARA).  For information  on the  availability of  this
    material at an NARA facility, call 202-741-6030, or go to
    http://www.archives.gov/federal_register/code_of_federal_regulations/i
    br_locations.html.

Issued in Kansas City, Missouri,  on August 11, 2011. John  Colomy, Acting
Manager, Small Airplane Directorate, Aircraft Certification Service.

FOR FURTHER  INFORMATION CONTACT:  Ann Johnson,  Aerospace Engineer,  FAA,
Wichita  Aircraft  Certification  Office,  1801  Airport  Road,  Room 100,
Wichita, Kansas  67209; telephone:  (316) 946-4105;  fax: (316)  946-4107;
email: ann.johnson@faa.gov.