EASA Regulations for General Electric Passport 20

2 airworthiness directives and regulations affecting General Electric Passport 20.

EASA AD US-2022-13-12

Engine - Fuel Core Compartment - Inspection / Re-torque

The document titled "Engine - Fuel Core Compartment - Inspection / Re-torque" is a Federal Aviation Administration (FAA) Airworthiness Directive (AD 2022-13-12) addressing all General Electric Company GE Passport 20-17BB1A, 20-18BB1A, and 20-19BB1A model turbofan engines. This AD mandates inspections and maintenance actions to prevent fuel leakage and potential engine fires. It applies specifically to these GE Passport turbofan engines installed on aircraft such as the Bombardier Global 7500.

Jun 30, 2022

Airworthiness DirectiveMaintenanceSafety MgmtGeneral Electric Passport 20Bombardier Global 7500

EASA AD US-2022-03-19

Time Limits / Maintenance Checks — Airworthiness Limitations Section - Amendment

The Federal Register document titled "Time Limits / Maintenance Checks — Airworthiness Limitations Section - Amendment" is a final rule airworthiness directive issued by the FAA for General Electric Company Passport 20-17BB1A, 20-18BB1A, and 20-19BB1A model turbofan engines. It addresses a manufacturing quality issue affecting certain high-pressure turbine rotor stage 1 disks. The directive mandates revisions to the airworthiness limitations section of the maintenance manual and the operator's continuous airworthiness maintenance program to reduce the life limit of these disks.

Feb 15, 2022

Airworthiness DirectiveMaintenanceSafety MgmtGeneral Electric Passport 20