Airworthiness Directive

AD 2016-18-17 81 FR 67100

Federal Aviation Administration · 14 CFR part 39

FR document
2016-23263
Amendment
39-18648
Published
2016-09-30
Models covered
1
Last live check
2026-08-17
AD

2016-18-17

FR doc 2016-23263 · 81 FR 67100

AD 2016-18-17Published 2016-09-30Effective 2016-11-04

Requires removal of the 2nd stage compressor impeller.

Full official abstract

We are adopting a new airworthiness directive (AD) for certain Honeywell International Inc. (Honeywell) TPE331 model turboprop engines and TSE331-3U model turboshaft engines. This AD was prompted by the discovery of cracks in a 2nd stage compressor impeller during a routine shop visit. This AD requires removal of the 2nd stage compressor impeller. We are issuing this AD to prevent failure of the compressor impeller, uncontained part release, damage to the engine, and damage to the airplane.

Applies to 1 model in our index