Document ID: chunk:federal_register_of_legislation:F2006B07519:body:0:p2
Version: federal_register_of_legislation:F2006B07519
Segment Type: other
Provision Reference: 
Character Range: 2930–3554

refers.

 Compliance: PART 1: Within 50 hours time in service after 31 March 1983.

           PART 2: Before further flight after compliance with Part 1 of this Directive and thereafter at intervals of 200 hours time in service.

           The inspections required by this Directive may be discontinued when the turbine housing is replaced with a Roto-master P/No. 600510-04 (TCM P/N 643931).

           Background:  To prevent the possibility of a fire in the powerplant nacelle and/or heat damage to the powerplant installation caused by the engine exhaust gases escaping through a cracked turbocharger turbine housing.