AD/JT9D/23 - First Stage High Pressure Turbine Airseal

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B11016 In force Legislative Instrument

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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.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.