Document ID: chunk:federal_register_of_legislation:F2006B11016:body:0
Version: federal_register_of_legislation:F2006B11016
Segment Type: other
Provision Reference: 
Character Range: 0–1362

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

 Pratt and Whitney Turbine Engines - JT9D Series

AD/JT9D/23 First Stage High Pressure Turbine Airseal 2/91

            Applicability: JT9D-7R4D, -7R4D1, -7R4E, -7R4E1, -7R4E4, -7R4H1, -7R4G2, engines fitted with P/N 797576, 797576P48, 793707, 793707P48 first stage turbine airseals.

             Requirement: 1. Replace first stage high pressure turbine airseals as listed by serial number in PWA SB No JT9D-7R4-72-393 Rev 1, Para 2, Part A.

             2. Inspect, first stage high pressure turbine airseals not listed by serial in PWA SB No JT9D-7R4-72-393 Rev 1, Para 2, Part A, in accordance with PWA SB No JT9D- 7R4-72-393 Rev 1, Para 2, Part B.

            Note: FAA AD 90-23-19 refers.

             Compliance: 1. At next engine shop visit regardless of planned maintenance action or reason for engine removal.

            2. At next access to affected parts.

 Background: This Directive reflects advice of an uncontained JT9D-7R4H1 engine failure event.
            The failure was attributed to cracking of an Inconel-718 material airseal. Certain lower rated JT9D models may also be fitted with the same part number airseal. This Directive requires replacement or inspection of those airseals.