Document ID: chunk:federal_register_of_legislation:F2006B09465:body:0:p2
Version: federal_register_of_legislation:F2006B09465
Segment Type: other
Provision Reference: 
Character Range: 2941–3777

threaded diameter.

           Note 2: Embraer Alert SB 110-27-0070 and Brazil CTA AD 83-02-01 R3 refers.

             Compliance: 1. Unless already accomplished; within 10 hours time in service after 12 January 1992, inspect in accordance with Requirement 1, until Requirement 2 is accomplished.

           2. Prior to 29 February 1992.

           The compliance of the previous issue of this Directive was: within 10 hours time in service after 15 February 1983 and thereafter as per requirement.

           Background: The manufacturer has been notified of a structural failure of the control wheel spindle, which resulted in the detachment of the control wheel in flight. Amendment 1 is issued to align this Directive with a revision of the relevant country of origin AD which requires terminating action in lieu of inspections.