AD 2005-15-04 Airworthiness Directives; Bombardier Model CL-600-1A11 (CL-600), Model CL-600-2A12 (CL-601), and Model CL-600-2B16 (CL-601-3A, CL-601-3R, and CL-604) Airplanes

This AD applies to the Bombardier airplane models, certificated in any category, listed in Table 1 of this AD. Table 1.—Applicability Bombardier model— As identified in Bombardier service bulletin— CL-600-1A11 (CL-600) airplanes 600-0710, Revision 01, dated December 15, 2003. CL-600-2A12 (CL-601) and CL-600-2B16 (CL-601-3A, and CL-601-3R) airplanes 601-0546, Revision 01, dated December 15, 2003. CL-600-2B16 (CL-604) airplanes 604-32-014, dated May 31, 2002.

You are responsible for having the actions required by this AD performed within the compliance times specified, unless the actions have already been done. Add Serial Numbers or Part Numbers (f) At the applicable compliance time specified in paragraph (f)(1), (f)(2), or (f)(3) of this AD: Add serial numbers and part numbers, as applicable, to the parts identified in the service bulletins. Do all actions in accordance with the applicable service bulletin. (1) For parts identified in the Bombardier Service Bulletin 600-0710, Revision 01, dated December 15, 2003; and Bombardier Service Bulletin 601-0546, Revision 01, dated December 15, 2003; as having a compliance time of “five years for the parts listed in Part A': Within 60 months after the effective date of this AD. (2) For parts identified in Bombardier Service Bulletin 600-0710, Revision 01, dated December 15, 2003; and Bombardier Service Bulletin 601-0546, Revision 01, dated December 15, 2003; as having a compliance time of “ten years for the parts listed in Part B': Within 120 months after the effective date of this AD. (3) For parts identified in the Bombardier Service Bulletin 604-32-014, dated May 31, 2002, as having a compliance time of “no later than a calendar time of 8 years': Within 96 months after the effective date of this AD. Note 1: The Bombardier service bulletins refer to the Messier-Dowty service bulletins in Table 2 of this AD as additional sources of service information for adding part numbers or serial numbers by vibro-peening the numbers on main landing gear (MLG) and nose landing gear (NLG) components that do not have them; and for determining the number of landings for parts without a part number or serial number on which the time since new (TSN) and cycles since new (CSN) have not been tracked. Table 2.—Messier-Dowty Service Bulletins Messier-Dowty service bulletin Model Landing gear corresponding Component Bombardier service bulletin(s) M-DT SB104467009/010-32-1, dated March 19, 2001 CL-600-1A11 (CL-600), CL-600-2A12 (CL-601) and CL-600-2B16 (CL-601-3A and CL-601-3R) airplanes MLG side strut retraction actuator eye bolt 600-0710 and 601-0546. M-DT SB19090-32-4, dated March 19, 2001 CL-600-2B16 (CL-604) airplanes MLG shock strut 604-32-014. M-DT SB20020-32-5, dated July 12, 2001 CL-600-2B16 (CL-604) airplanes NLG shock strut 604-32-014. M-DT SB200814001-32-3, dated March 19, 2001 CL-600-1A11 (CL-600), CL-600-2A12 (CL-601) and CL-600-2B16 (CL-601-3A and CL-601-3R) airplanes NLG drag brace hinge pin 600-0710 and 601-0546. M-DT SB200922001/2-32-6, dated March 19, 2001 CL-600-1A11 (CL-600) airplanes MLG shock strut 600-0710. M-DT SB200924003/004-32-16, dated July 12, 2001 CL-600-1A11 (CL-600) airplanes NLG shock strut 600-0710. M-DT SB6100-32-10, dated March 19, 2001 CL-600-2A12 (CL-601) and CL-600-2B16 (CL-601-3A and CL-601-3R) airplanes MLG shock strut pin 601-0546. M-DT SB6500-32-1, dated March 19, 2001 CL-600-1A11 (CL-600), CL-600-2A12 (CL-601) and CL-600-2B16 (CL-601-3A and CL-601-3R) airplanes MLG side strut retraction actuator 600-0710 and 601-0546. M-DT SB7200-32-6, dated March 19, 2001 CL-600-1A11 (CL-600), CL-600-2A12 (CL-601) and CL-600-2B16 (CL-601-3A and CL-601-3R) airplanes NLG drag brace hinge pin 600-0710 and 601-0546. M-DT SB7300-32-16, dated July 12, 2001 CL-600-2A12 (CL-601) and CL-600-2B16 (CL-601-3A and CL-601-3R) airplanes NLG shock strut 601-0546. Establish the Number of Landings (g) At the applicable time specified in paragraph (f) of this AD: If a component does not have a serial number and the CSN or TSN were not tracked, use the formula in the applicable Messier-Dowty service bulletin in Table 2 of this AD to establish the number of landings (TSN or CSN), and record the newly calculated TSN or CSN in the aircraft log books. Revise the Airworthiness Limitations Section (ALS) (h) Within 30 days after the effective date of this AD, revise the ALS of the applicable Instructions for Continued Airworthiness to reflect the new life limits of the landing gear parts by inserting copies of the Canadair temporary revisions (TR) in Table 3 of this AD into the ALS of the applicable Canadair Time-Limits/Maintenance Check Manual. When the contents of the TRs are included in the general revisions of the ALS, these TRs may be removed provided the relevant information in the ALS is identical to that in the TRs. Table 3.—Canadair Temporary Revisions Temporary revision Applicable Canadair time-limits/maintenance check manual Manual section Model 5-116, dated April 11, 2002 PSP 605 5-10-10 CL-600-1A11 (CL-600) airplanes. 5-190, dated April 11, 2002 PSP 601-5 5-10-10 CL-600-2A12 (CL-601) and CL-600-2B16 (CL-601-3A and CL-601-3R) airplanes. 5-191, dated April 11, 2002 PSP 601-5 5-10-11 CL-600-2A12 (CL-601) and CL-600-2B16 (CL-601-3A and CL-601-3R) airplanes. 5-192, dated April 11, 2002 PSP 601-5 5-10-12 CL-600-2A12 (CL-601) and CL-600-2B16 (CL-601-3A and CL-601-3R) airplanes. 5-2-6, dated April 11, 2002 CL-604 5-10-10 CL-600-2B16 (CL-604) airplanes. 5-204, dated April 11, 2002 PSP 601A-5 5-10-10 CL-600-2A12 (CL-601) and CL-600-2B16 (CL-601-3A and CL-601-3R) airplanes. 5-205, dated April 11, 2002 PSP 601A-5 5-10-11 CL-600-2A12 (CL-601) and CL-600-2B16 (CL-601-3A and CL-601-3R) airplanes. 5-206, dated April 11, 2002 PSP 601A-5 5-10-12 CL-600-2A12 (CL-601) and CL-600-2B16 (CL-601-3A and CL-601-3R) airplanes. Parts Installation (i) As of the effective date of this AD, no person may install on any airplane a landing gear part, unless it has had the applicable part number or serial number added in accordance with paragraph (f) of this AD; and had the number of landings established in accordance with paragraph (g) of this AD. No Reporting Required (j) Although the service bulletins identified in paragraph (f) of this AD specify that operators submit incorporation notices to Bombardier after each new part number or serial number and landings assigned to these parts is added, this AD does not include that action. Actions Done in Accordance With Previous Issues of Service Bulletins (k) Actions done before the effective date of this AD in accordance with Bombardier Service Bulletin 601-0546, dated May 31, 2002; and Bombardier Service Bulletin 600-0710, dated May 31, 2002; are acceptable for compliance with the corresponding actions specified in this AD. Alternative Methods of Compliance (AMOCs) (l) The Manager, New York Aircraft Certification Office, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. Related Information (m) Canadian airworthiness directives CF-2003-18R1, dated January 17, 2005; CF-2003-20, dated July 24, 2003; and CF-2003-21R1, dated January 21, 2005; also address the subject of this AD. Material Incorporated by Reference (n) You must use the service information identified in Tables 4, 5, and 6 of this AD to perform the actions that are required by this AD, unless the AD specifies otherwise. The Director of the Federal Register approved the incorporation by reference of these documents in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Contact Bombardier, Inc., Canadair, Aerospace Group, P.O. Box 6087, Station Centre-ville, Montreal, Quebec H3C 3G9, Canada, for a copy of this service information. You may review copies at the Docket Management Facility, U.S. Department of Transportation, 400 Seventh Street SW., Room PL-401, Nassif Building, Washington, DC; on the Internet at http://dms.dot.gov; or at the National Archives and Records Administration (NARA). For information on the availability of this material at the NARA, call (202) 741-6030, or go to http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html. Table 4.—Bombardier Service Bulletins Incorporated by Reference Bombardier Service Bulletins (including the Component Time Tracking Log Card and Attachments Listed in Table 5 of this AD) Revision level Date 600-0710 01 December 15, 2003. 601-0546 01 December 15, 2003. 604-32-014 Original May 31, 2002. Table 5.—Messier-Dowty Service Bulletins Incorporated by Reference Messier-Dowty Service Bulletin (attachments) Date Attached to Bombardier Service Bulletin(s)— M-DT SB104467009/010-32-1 March 19, 2001 600-0710, 601-0546 M-DT SB19090-32-4 March 19, 2001 604-32-014 M-DT SB20020-32-5 July 12, 2001 604-32-014 M-DT SB200814001-32-3 March 19, 2001 600-0710, 601-0546 M-DT SB200922001/2-32-6 March 19, 2001 600-0710 M-DT SB200924003/004-32-16 July 12, 2001 600-0710 M-DT SB6100-32-10 March 19, 2001 601-0546 M-DT SB6500-32-1 March 19, 2001 600-0710, 601-0546 M-DT SB7200-32-6 March 19, 2001 600-0710, 601-0546 M-DT SB7300-32-16 July 12, 2001 601-0546 Table 6.—Canadair Temporary Revisions Incorporated by Reference Canadair temporary revision Date Applicable Canadair time-limits/maintenance check manual Manual section 5-116 April 11, 2002 PSP 605 5-10-10 5-190 April 11, 2002 PSP 601-5 5-10-10 5-191 April 11, 2002 PSP 601-5 5-10-11 5-192 April 11, 2002 PSP 601-5 5-10-12 5-2-6 April 11, 2002 CL-604 5-10-10 5-204 April 11, 2002 PSP 601A-5 5-10-10 5-205 April 11, 2002 PSP 601A-5 5-10-11 5-206 April 11, 2002 PSP 601A-5 5-10-12 Issued in Renton, Washington, on July 11, 2005. Ali Bahrami, Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 05-14175 Filed 7-25-05; 8:45 am] BILLING CODE 4910-13-P

This AD was prompted by reports that landing gear parts that have safe-life limits but do not have serial numbers or part numbers can be removed from one landing gear and re-installed on another, making tracking difficult. We are issuing this AD to prevent life-limited landing gear parts from being used beyond their safe-life limits, which could lead to collapse of the landing gear.