Document ID: chunk:federal_register_of_legislation:F2006B05249:body:0
Version: federal_register_of_legislation:F2006B05249
Segment Type: other
Provision Reference: 
Character Range: 0–2964

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

    Cessna 206 Series Aeroplanes

AD/CESSNA 206/44 Electrical Power Distribution and Control 8/86

Applicability:  All Cessna Model U206G and FAA STC SA2353NM (Soloy  TU206G aeroplanes modified in accordance with U.S. Turbine Conversion) with the following serial
                numbers:
                CESSNA SERIAL NUMBER                                        SOLOY DATA PLATE NO
                U20603989                                                   763-013
                U20604266                                                   763-001
                U20604287                                                   763-003
                U20604881                                                   763-014
                U20605232                                                   763-005
                U20605567                                                   763-002
                U20605584                                                   763-015
                U20605745                                                   763-008
                U20605936                                                   763-006
                U20606065                                                   763-007
                U20606227                                                   763-004
                U20606381                                                   763-011
                U20606628                                                   763-010
                U20606768                                                   763-012
                U20606816                                                   763-009

               Requirement: 1. Replace the voltage regulator in accordance with Soloy Service Bulletin 04-763. 2. For aeroplanes with S/Nos. U20604266, U20604287, U20605232, U20605567,
                 U20605745, U20605936, U20606065 and U20606227, modify the electrical system circuit breaker installation in accordance with Soloy Service Bulletin 02- 763.

               Note: FAA AD 86-11-07 Amendment 39-5324 refers.

               Compliance: For Para 1: Within 100 hours time in service after 31 August 1986. For Para 2:              Within 200 hours time in service after 31 August 1986.
 COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

             Background: 1. The existing voltage regulator installation has been shown to interfere with the ADF system such as to cause erroneous bearing information to be displayed.

             2. The engine start circuit and the auto feather circuit are at present connected to the same circuit breaker. Opening this circuit breaker by an electrical fault or by pilot action will render both circuits inoperative.