AD/CESSNA 210/70 - Horizontal Stabiliser Attachment Brackets
View image in the official sourceView image in the official sourceAIRWORTHINESS DIRECTIVE
View image in the official sourceFor the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.1 (1) of CAR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.
Cessna 210 Series Aeroplanes
AD/CESSNA 210/70 Horizontal Stabiliser Attachment
Brackets
7/2002
| Applicability: | Model 210G210H | Serial Numbers21058819 through 2105893621058937 through 21059061 |
|---|---|---|
| 210J210K and T210K | 21059062 through 2105919921059200 through 21059502 | |
| 210L and T210L210M and T210M210N and T210N | 21059503 through 21061041, 21061043 through 2106157321061042, 21061574 through 2106295421062955 through 21064897 | |
| P210NT210G | P21000001 through P21000834T210-0198 through T210-0307 | |
| T210HT210J | T210-0308 through T210-0392T210-0393 through T210-0454, 21058140 |
Requirement: 1. Check the maintenance records, and determine whether a horizontal stabiliser attachment reinforcement bracket (bracket) part number (P/N) 1232624-1 is installed that was shipped by Cessna from 27 February 1998 through 17 March 2000. If the installed brackets were not shipped by Cessna between 27 February 1998 and 17 March 2000, no further action is required by this Directive.
2. If the above check reveals that affected P/N 1232624-1 brackets are installed, visually inspect the left and right brackets for existence of seam welds along both the lower inboard and outboard wall/flange.
Cessna 210 Series Aeroplanes
AD/CESSNA 210/70 (Continued)
3. If no seam weld is found on the left or right bracket during the Requirement 2 inspection, before further flight, replace with a new or serviceable P/N 1232624- 1 bracket. If the left and right brackets have seam welds along both the lower inboard and outboard wall/flange, no further action is required.
Note: FAA AD 2002-07-01 Amdt 39-12695 refers.
Compliance: Within 50 hours time in service after 11 July 2002, unless already accomplished.
This Airworthiness Directive becomes effective on 11 July 2002.
Background: The FAA received a report that certain horizontal stabiliser attachment reinforcement brackets were manufactured without seam welds. This Directive specifies actions to detect and replace structurally deficient attachment brackets. Continued use of such brackets could result in structural failure of the horizontal stabiliser.
View image in the official source
David Alan Villiers
Delegate of the Civil Aviation Safety Authority 28 May 2002
View image in the official sourceThe above AD is notified in the Commonwealth of Australia Gazette on 19 June 2002.