EASA Regulations for Rolls-Royce Corporation (Usa) AE 2100

2 airworthiness directives and regulations affecting Rolls-Royce Corporation (Usa) AE 2100.

EASA AD US-2020-22-18

Engine - Propeller Gearbox Shaft and Carrier Assembly - Usage Hours Assignment / Replacement

The Federal Aviation Administration's Airworthiness Directive 2020-22-18 addresses all Rolls-Royce Corporation AE 2100A, AE 2100D2, AE 2100D2A, and AE 2100P turboprop engines. This directive responds to a fatigue crack issue found in the propeller gearbox shaft and carrier assembly that caused high vibration during manufacturer testing. It mandates usage hour assignment and replacement of these assemblies before exceeding newly established life limits to ensure continued airworthiness.

Nov 11, 2020

Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Corporation (Usa) AE 2100

EASA AD US-2018-17-04

Engine - Turbine Wheels - Removal / Replacement

The Federal Aviation Administration's Airworthiness Directive 2018-17-04 addresses certain Rolls-Royce Corporation AE 2100D2A and AE 2100D3 turboprop engines and AE 3007A2 turbofan engines. It focuses on the removal and replacement of specific 1st-stage gas generator turbine wheels and 1st-stage high-pressure turbine wheels due to potential low-cycle fatigue failure. This directive applies to engines with specified part and serial numbers to ensure continued airworthiness and safety.

Aug 21, 2018

Airworthiness DirectiveMaintenanceSafety MgmtRolls-Royce Corporation (Usa) AE 2100Rolls-Royce Corporation (Usa) AE 3007