[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
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(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
