15 results found (3656ms)
Airworthiness Directives; International Aero Engines LLC Engines
Unsafe Condition: Fan blade fracture events, which can result in a fuel leak and uncontrolled engine fire, leading to damage to the airplane.
Why matched: Airworthiness Directives; International Aero Engines LLC Engines
Airworthiness Directives; International Aero Engines, LLC
Unsafe Condition: The fracture of a low-pressure compressor (LPC) 1st-stage integrally bladed rotor (IBR-1) caused by an aerodynamic excitation from a misaligned inlet guide vane (IGV) located directly upstream of t...
Why matched: Airworthiness Directives; International Aero Engines, LLC
Airworthiness Directives; International Aero Engines, LLC Engines
Unsafe Condition: Operating in a condition where the HPC 2nd stage rotors and HPC 4th stage rotors have potentially degraded knife-edge seals and abrasive coating of the rear wing 4th stage rotor due to having been ...
Why matched: Airworthiness Directives; International Aero Engines, LLC Engines
Airworthiness Directives; International Aero Engines, LLC Engines
Unsafe Condition: The condition, if not addressed, could result in uncontained hub failure, release of high-energy debris, damage to the engine, damage to the airplane, and loss of the airplane.
Why matched: Airworthiness Directives; International Aero Engines, LLC Engines
Airworthiness Directives; International Aero Engines, LLC Engines
Unsafe Condition: heat-induced cracking at the forward and aft knife edge seals and uncontained separation of the HPC rear hub, which could result in uncontained debris release, damage to the engine, damage to the a...
Why matched: Airworthiness Directives; International Aero Engines, LLC Engines
Airworthiness Directives; International Aero Engines, LLC Engines
Unsafe Condition: The high-pressure turbine (HPT) 1st-stage hub and HPT 2nd-stage hub are susceptible to failure due to a material anomaly, which could result in uncontained disk failure, release of high-energy debr...
Why matched: Airworthiness Directives; International Aero Engines, LLC Engines
Airworthiness Directives; International Aero Engines, LLC Turbofan Engines
Unsafe Condition: The failure of the HPT disk due to an undetected subsurface material defect that may affect the life of the part, which could result in uncontained HPT disk failure, release of high-energy debris, ...
Why matched: Airworthiness Directives; International Aero Engines, LLC Turbofan Engines
Airworthiness Directives; International Aero Engines LLC, Turbofan Engines
Unsafe Condition: Failures of certain low-pressure turbine (LPT) 3rd-stage blades.
Why matched: Airworthiness Directives; International Aero Engines LLC, Turbofan Engines
Airworthiness Directives; International Aero Engines LLC Turbofan Engines
Unsafe Condition: multiple reports of in-flight engine shutdowns as the result of high-cycle fatigue causing fracture of certain parts of the main gearbox (MGB) assembly
Why matched: Airworthiness Directives; International Aero Engines LLC Turbofan Engines
Airworthiness Directives; International Aero Engines, LLC Turbofan Engines
Unsafe Condition: Wear and fracture of the turbine piston seal releasing debris that impacted the LPT 3rd-stage blades.
Why matched: Airworthiness Directives; International Aero Engines, LLC Turbofan Engines
Airworthiness Directives; International Aero Engines, LLC Turbofan Engines
Unsafe Condition: Failure of the LPT 3rd-stage blades, failure of one or more engines, loss of thrust control, and loss of the airplane.
Why matched: Airworthiness Directives; International Aero Engines, LLC Turbofan Engines
Airworthiness Directives; International Aero Engines Turbofan Engines
Unsafe Condition: The discovery of incorrect serial numbers in the identification of LPT disks in AD 2018-24-01.
Why matched: Airworthiness Directives; International Aero Engines Turbofan Engines
Airworthiness Directives; International Aero Engines (IAE) Turbofan Engines
Unsafe Condition: Reports of in-flight engine shutdowns and aborted take-offs as the result of certain parts affecting the durability of the rear high-pressure compressor (HPC) rotor hub knife edge seal.
Why matched: Airworthiness Directives; International Aero Engines (IAE) Turbofan Engines
Airworthiness Directives; International Aero Engines Turbofan Engines
Unsafe Condition: corrosion found on the HPC front hub, part number (P/N) 30G2401, installed
Why matched: Airworthiness Directives; International Aero Engines Turbofan Engines
Airworthiness Directives; International Aero Engines Turbofan Engines
Unsafe Condition: Damage to the engine fan hub found during an engine shop visit of an IAE PW1100G-series turbofan engine, believed to be the result of the installation of the inlet cone without using alignment pins...
Why matched: Airworthiness Directives; International Aero Engines Turbofan Engines