Document ID: chunk:federal_register_of_legislation:F2009L03111:body:0:p1
Version: federal_register_of_legislation:F2009L03111
Segment Type: other
Provision Reference: 
Character Range: 0–3165

AIRWORTHINESS DIRECTIVE
For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.001(1) of CASR 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.

Bombardier (Canadair) CL-600 (Challenger) Series Aeroplanes
AD/CL-600/116  Air Driven Generator Strut  9/2009

Applicability:  Bombardier Inc. Models:

                CL-600-2B19, Serial Numbers (S/N) 7305 through 8051.

                CL-600-2C10, S/Ns 10003 through 10260.

                CL-600-2D15 and CL-600-2D24, S/Ns 15001 through 15106.
Requirement:       1. Identification Check:

                   Check the Part Number (P/N) of the installed Air Driven Generator (ADG):

                     a. If the ADG has Hamilton Sundstrand P/N 1711405, the strut wall thickness is within specification.  No further action is required and compliance with this AD is complete.

                     b. If the ADG has a Hamilton Sundstrand P/N in the 761339 series, check the ADG S/N and proceed as follows:

                        i. If the S/N of the ADG is 2000 or higher, the strut wall thickness is within specification.  No further action is required and compliance with this AD is complete.

                        ii. If the S/N of the ADG is in the range 0101 through 1999 and symbol
                        24-3 is marked in the S/N block of the identification plate, the strut wall thickness is within specification.  No further action is required and compliance with this AD is complete.

                        iii. If the S/N of the ADG is in the range 0101 through 1999 and symbol
                        24-3 is not marked in the S/N block of the identification plate, check the S/N of the strut and generator housing assembly (for location, see
                        Figure 1, Sheet 1 of Hamilton Sundstrand Service Bulletin (SB) ERPS10AG-24-3) and proceed as follows:

                           A. If the S/N of the strut and generator housing assembly is in the range 0001 through 2503, a fluorescent penetrant inspection is required.  Proceed to Requirement 2 of this AD.

              B. If the S/N of the strut and generator housing assembly is 2504 or higher, the strut wall thickness is within specification.  No further action is required and compliance with this AD is complete.

           iv. If the S/N of the strut and generator housing assembly is not checked, fluorescent penetrant inspection is required.  Proceed to Requirement 2 of this AD.

   Note 1:  Requirement 1 may be conducted visually, which requires the ADG to be lowered, or by checking the maintenance records.

      2. Fluorescent Penetrant Inspection:

        a.