Document ID: chunk:federal_register_of_legislation:F2006B11184:body:0
Version: federal_register_of_legislation:F2006B11184
Segment Type: other
Provision Reference: 
Character Range: 0–1060

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 AlliedSignal (Lycoming) Turbine Engines - LTS 101 Series

 AD/LTS/7
 Amdt 2

 Power Turbine Rotor 3/91

            Applicability: All LTS 101 series engines fitted with Power Turbine Rotors part number 4-141-070- XX.

Requirement: Action in accordance with Textron Lycoming SB No LT 101-72-00-0093 Rev. 5

            Note: FAA AD 87-11-09 refers.

            Compliance:  Unless previously accomplished; within 50 hours time in service from 21 March 1991, and thereafter at intervals not to exceed 50 hours or 300 cycles, whichever occurs first.

            Background:  This Directive has been amended to reflect the manufacturers latest revision to the Requirement Document detailed in FAA AD 87-11-09. This amendment also reflects the release of an individually bladed power turbine rotor. LTS101 series engines fitted with individually bladed power turbine rotors are not affected by this Directive.