Airworthiness Directives; International Aero Engines AG (IAE) V2500-A1 Series Turbofan Engines
airworthiness · Rule · Final rule. · Published 1999-03-01 · Effective 1999-04-30 · 64 FR 9910
Document
Document number
99-4793
Federal Register citation
64 FR 9910
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
International Aero
Publication date
1999-03-01
Effective date
1999-04-30
FAA docket
Docket No. 98-ANE-76-AD
Abstract
This amendment adopts a new airworthiness directive (AD), applicable to International Aero Engines AG (IAE) V2500-A1 series turbofan engines, that requires initial and repetitive inspections of certain High Pressure Turbine (HPT) stage 1 and stage 2 disks utilizing an improved ultrasonic method when the disks are exposed during a normal shop visit, and if a subsurface anomaly is found, removal from service and replacement with a serviceable part. This amendment is prompted by the results of a stage 1 HPT disk fracture investigation which has identified a population of HPT stage 1 and 2 disks that may have subsurface anomalies formed as a result of the processes used to manufacture the material. The actions specified by this AD are intended to prevent HPT disk fracture, which could result in an uncontained engine failure, and damage to the airplane.