Document ID: chunk:federal_register_of_legislation:F2006B11142:front:0
Version: federal_register_of_legislation:F2006B11142
Segment Type: other
Provision Reference: 
Character Range: 0–969

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
    SCHEDULE OF AIRWORTHINESS DIRECTIVES

    Gates Learjet 24 & 25 Series Aeroplanes

                       AD/LEARJET/25  Automatic Flight Control System - Deactivation and Modification

               Applicability:  All models 24 with S/Nos. 24-100 and subsequent; All models 25 with S/Nos. 25-003 and subsequent; All models 28 with S/Nos. 28-001 and subsequent; All models 29 with S/Nos. 29-001 and subsequent.

4/81
                 Requirement: 1. Deactivate the pitch function of the FC-110 Automatic Flight Control System (AFCS) or Automatic Flight Control Stability System (AFC/SS), as indicated below, by pulling the AFCS Pitch DC Circuit Breaker to the off position, banding it to prevent use of this function and checking to assure this function is the only deactivated circuit or control.

SERIES  SERIAL NUMBERS                  LOCATION