EASA Regulations for Honeywell International TPE331

2 airworthiness directives and regulatory documents affecting Honeywell International TPE331.

EASA AD US-2018-22-01

Engine - Second Stage Turbine Rotors - Removal

The Federal Aviation Administration's Airworthiness Directive 2018-22-01 addresses Honeywell International Inc. TPE331 turboprop engines, specifically models TPE331-8, -10, -10N, -10R, -10U, -10UA, -10UF, -10UG, -10UGR, -10UR, and -11U equipped with certain second stage turbine rotor assemblies. This directive mandates the removal of specific second stage turbine rotors at reduced life limits to prevent unsafe conditions. It was issued following reports of uncontained rotor separation and discovery of cracks in the turbine rotors.

Dec 10, 2018

Airworthiness DirectiveMaintenanceSafety MgmtHoneywell International TPE331

EASA AD US-2018-17-15

Engine - Combustion Chamber Case Assembly - Inspection / Replacement / Removal

The Federal Aviation Administration's Airworthiness Directive 2018-17-15 addresses certain Honeywell International Inc. TPE331 turboprop and TSE331 turboshaft engines. It mandates inspection, replacement, and removal of combustion chamber case assemblies with specific part numbers to prevent cracks and ruptures. This directive applies to multiple TPE331 engine models including the newly added TPE331-12B and certain TSE331 models.

Sep 18, 2018

Airworthiness DirectiveMaintenanceSafety MgmtHoneywell International TPE331Honeywell International TSE331-3U