[Federal Register Volume 67, Number 78 (Tuesday, April 23, 2002)]
[Corrections]
[Pages 19809-19810]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: C2-7645]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. 2001-CE-42-AD; Amendment 39-12695; AD 2002-07-01]
RIN 2120-AA64


Airworthiness Directives; Cessna Aircraft Company P206, TP206, 
TU206, U206, 207, T207, 210, P210, and T210 Series Airplanes

Correction

    In rule document 02-7645 beginning on page 15714 in the issue of 
Wednesday April 3, 2002, the table is corrected make the following 
correction:


Sec. 39.13  [Corrected]

    On page 15716, in the first column, in Sec. 39.14, the table should 
read as set forth below:
    (d) What actions must I accomplish to address this problem? To 
address this problem, you must accomplish the following:

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                      Actions                                 Compliance                     Procedures
----------------------------------------------------------------------------------------------------------------
(1) Maintenance Records Check:                      Within the next 50 hours time- No special procedures
                                                     in-service (TIS) after May     required to check the
                                                     13, 2002 (the effective date   logbook.
                                                     of this AD), unless already
                                                     accomplished.
    (i) Check the maintenance records to determine
     whether a horizontal stabilizer attachment
     reinforcement bracket, part number (P/N)
     1232624-1, shipped by Cessna from February
     27, 1998, through March 17, 2000, is
     installed. The owner/operator holding at
     least a private pilot certificate as
     authorized by section 43.7 of the Federal
     Aviation Regulations (14 CFR 43.7) may
     perform this check.
    (ii) If, by checking the maintenance records,
     the owner/operator can positively show that a
     horizontal stabilizer attachment
     reinforcement bracket, P/N 1232624-1, shipped
     by Cessna from February 27, 1998, through
     March 17, 2000, is not installed, then the
     inspection requirement of paragraph (d)(2)
     and the replacement requirement of paragraph
     (d)(3) of this AD do not apply. You must make
     an entry into the aircraft records that shows
     compliance with this portion of the AD, in
     accordance with section 43.9 of the Federal
     Aviation Regulations (14 CFR 43.9).
(2) Inspection: Visually inspect the right and      Within the next 50 hours TIS   In accordance with the
 left horizontal stabilizer attachment               after May 13, 2002 (the        Accomplishment Instructions
 reinforcement brackets, part number (P/N) 1232624-  effective date of this AD),    in Cessna Service Bulletin
 1, for the existence of seam welds along both the   unless already accomplished.   SEB00-10, dated November 6,
 lower inboard and outboard wall/flange.                                            2000, and the applicable
                                                                                    maintenance manual.
(3) Replacement:                                    Accomplish any necessary       In accordance with the
                                                     replacements prior to          Accomplishment Instructions
                                                     further flight after the       in Cessna Service Bulletin
                                                     inspection required by         SEB00-10, dated November 6,
                                                     paragraph (d)(2) of this AD,   2000, and the applicable
                                                     unless already accomplished.   maintenance manual.

[[Page 19810]]

 
    (i) If no seam weld is found along both the
     lower inboard and outboard wall/flange on the
     right and left horizontal stabilizer
     attachment reinforcement bracket during the
     inspection required in paragraph (d)(2) of
     this AD, replace with a new or airworthy P/N
     1232624-1 horizontal stabilizer attachment
     reinforcement bracket..
    (ii) If the right and left horizontal
     stabilizer attachment reinforcement bracket
     has seam welds along both the lower inboard
     and outboard wall/flange, no further action
     is required.
    (4) Installation Prohibition: Do not install    As of May 13, 2002 (the        Not applicable.
     any P/N 1232624-1 horizontal stabilizer         effective date of this AD).
     attachment reinforcement bracket (or FAA-
     approved equivalent part) unless the bracket:.
    (i) is inspected as required in paragraph
     (d)(2) of this AD; and.
    (ii) has seam welds along both the lower
     inboard and outboard wall/flange..
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[FR Doc. C2-7645 Filed 4-22-02; 8:45 am]
BILLING CODE 1505-01-D