Airworthiness directives: Cessna; correction,

[Federal Register: April 23, 2002 (Volume 67, Number 78)]

[Corrections]

[Page 19809-19810]

From the Federal Register Online via GPO Access [wais.access.gpo.gov]

[DOCID:fr23ap02-141]

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 02-7645beginning 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:

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..

[FR Doc. C2-7645Filed4-22-02; 8:45 am]

BILLING CODE 1505-01-D