Document ID: chunk:federal_register_of_legislation:F2006B11200:front:0:p1
Version: federal_register_of_legislation:F2006B11200
Segment Type: other
Provision Reference: 
Character Range: 12–3354

AIRWORTHINESS DIRECTIVE
For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.1 (1) of CAR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.

 Lycoming Piston Engines

 AD/LYC/108 Crankshaft Material Inspection 12/2002

DM

               Applicability: 1. Textron Lycoming TIO-540 and LTIO-540 series engines with a rated take-off power of 300 horsepower or greater; and

               2.        Textron Lycoming IO-540 series engines modified by a Supplemental Type Certificate (STC) listed in Table 1 of this directive, regardless of the rated horsepower

            Note 1: Applicable IO-540 powered aircraft include the Ted Smith/Piper PA-60 601 and 601P models.

            Note 2: FAA Airworthiness Directive 2002-19-03 Amdt 39-12883 refers.

               Requirement: 1. Textron Lycoming TIO-540 and LTIO-540 series engines with a rated take-off power of 300 horsepower or greater and listed by serial number in Table 2 of this directive:

                  1. A CAR 42ZC (6) authorised representative of Textron Lycoming to obtain a sample of the crankshaft material for the purpose of metallurgical evaluation in accordance with Textron Lycoming Mandatory Service Bulletin (MSB) 553; and

                  2. Following compliance with Requirement 1a of this Directive; applicable engines may only be returned to service following receipt of Textron Lycoming documented evidence that confirms the material sample was found not to exhibit any metallurgical anomalies; and

c.         The Textron Lycoming notification of the result of the metallurgical evaluation is to be retained in the engine logbook as an engine record.

               2. Textron Lycoming TIO-540 and LTIO-540 series engines with a rated take-off power of 300 horsepower or greater and listed by serial number in Table 3 of this directive:

               A sample of the crankshaft material is to be taken in accordance with Requirement 1 (a), (b) and (c) of this directive.

             3.                                                                                                                                                                                                                                    Textron Lycoming IO-540 series engines modified under an STC listed in Table
              1 of this directive to incorporate a turbocharger, regardless of horsepower rating and TIO-540 and LTIO-540 engines with a rated take-off power of 300 horsepower or greater and have had a new crankshaft installed since 1 March
              1997 that is listed by serial number in Table 4 of this directive:
              A sample of the crankshaft material is to be taken in accordance with
              Requirement 1 (a), (b) and (c) of this directive.
4.            Textron Lycoming IO-540 series engines modified