Document ID: chunk:federal_register_of_legislation:F2009L00690:body:0:p3
Version: federal_register_of_legislation:F2009L00690
Segment Type: other
Provision Reference: 
Character Range: 5718–8735

and Procedures:

                A. Ferry Flight with gear extended and pinned.

                B. Landing to be conducted at a minimum descent rate.

                C. Minimize braking on landing.

                D. Flight to be conducted per Aircraft Operating Manual (AOM) Section 4.8.

                E. Essential crew only on board.

                F. Flight in known or forecast icing condition is prohibited.

             Maintenance Procedures:

                (i) Inspect the left hand and right hand main landing gear retract actuator jam nut to ensure the wire lock is in place and the nut is secure.

                (ii) Perform the general visual inspections as defined in accordance with Bombardier All Operators Message No. 236 Rev A or later revisions.

                (iii) If items 1 and 2 results are satisfactory, insert main landing gear ground lock pins and lockwire in place.

                (iv) Ensure the nose landing gear ground lock is engaged.

             Note 3:  Transport Canada AD CF-2007-20 R2 dated 6 February 2009 refers.
Compliance:  For Requirement 1 - Remains unchanged as detailed in the original issue of this AD as:

                Before further flight after 14 September 2007 (the effective date of the original issue of this AD), unless previously accomplished.

   For Requirement 2a - Remains unchanged as detailed in the original issue of this AD as:

      Before further flight after 14 September 2007, unless previously accomplished.

   For Requirement 2b - At intervals not to exceed 250 landings or one month from the previous inspection, whichever occurs first.

   For Requirement 3a - Remains unchanged as detailed in the original issue of this AD as:

      For aircraft main landing gear retract actuator (p/n 46550-7 or 46550-9) that have accumulated 8,000 or more landings or in service for more than 4 years since new, whichever occurs first at 14 September 2007 - before further flight after
      14 September 2007.

      For aircraft main landing gear retract actuator (p/n 46550-7 or 46550-9) that have accumulated between 4,000 to 7,999 landings or in service between 2 to 4 years since new at 14 September 2007 - Within 500 flight hours or 3 months after the effective date of this AD, whichever occurs first.

      For aircraft main landing gear retract actuator (p/n 46550-7 or 46550-9) that have accumulated less than 4,000 landings or less than 2 years service in service since new, at 14 September 2007 - Prior to reaching 4,500 landings or 27 months in service new, whichever occurs first.

      For aircraft main landing gear retract actuator (p/n 46550-11) - Prior to reaching 4,500 landings or 27 months in service new, whichever occurs first.

   For Requirement 3b - At intervals not to exceed 2,000 landings or one calendar year from the previous inspection, whichever occurs first.

      For Requirement 4 - Within 7 days after each inspection.

      For Requirement 5

      For aircraft main