2026-14-03
final ruleAirworthiness Directives; General Electric Company Engines
Unsafe Condition: unsafe condition on these products.
Why matched: Airworthiness Directives; General Electric Company Engines
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2,502 results found (999ms)
2026-14-06 Recurring
final ruleAirworthiness Directives; CFM International, S.A. Engines
Unsafe Condition: Accelerated high-pressure turbine (HPT) rotor stage 1 blade deterioration and airfoil distress in engines operating in the South Asia region.
Why matched: Airworthiness Directives; CFM International, S.A. Engines
2026-13-06 Recurring
final ruleAirworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines
Unsafe Condition: The main fuel hose assembly of the fuel manifold may exhibit softness, non-compliance, resistance, shrinkage, cracks, chafing, dents, kinks, necking, and degradation of the hose braid wire.
Why matched: Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines
2026-13-09 Recurring
final ruleAirworthiness Directives; Pratt & Whitney Canada Corp. Engines
Unsafe Condition: Circumferential cracks at the turbine exhaust frame external surface caused by thermal stress from engine starts.
Why matched: Airworthiness Directives; Pratt & Whitney Canada Corp. Engines
2026-10-21 Recurring
final ruleAirworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines
Unsafe Condition: Cracking, damage, or air leakage wear in the intermediate-pressure stage 8 (IP8) and high-pressure stage 3 (HP3) air transfer tubes and front bearing housing IP8 air feed tubes.
Why matched: Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines
2026-12-06 Recurring
final ruleAirworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines
Unsafe Condition: Axial cracks in the high-pressure turbine (HPT) blades could result in uncontained engine failure.
Why matched: Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines
2026-09-02 Recurring
final ruleAirworthiness Directives; Pratt & Whitney RTX Corporation (Type Certificate Previously Held by Pratt & Whitney Division United Technologies Corporation) Engines
Unsafe Condition: Separation of the high-pressure compressor (HPC) 7th-stage integrally bladed rotor (IBR-7) due to crack indications in the HPC 15th-stage disks, front turbine hubs, high pressure turbine (HPT) 1st-...
Why matched: Airworthiness Directives; Pratt & Whitney RTX Corporation (Type Certificate Previously Held by Pratt & Whitney Division United Technologies Corporation) Engines
2026-08-12
final ruleAirworthiness Directives; Safran Helicopter Engines, S.A. (Type Certificate Previously Held by Turbomeca, S.A.) Engines
Unsafe Condition: The unsafe condition involves the affected fuel control unit (FCU) potentially failing due to a manufacturing defect, which could result in engine power loss or shutdown.
Why matched: Airworthiness Directives; Safran Helicopter Engines, S.A. (Type Certificate Previously Held by Turbomeca, S.A.) Engines
2026-07-06 Recurring
final ruleAirworthiness Directives; Pratt & Whitney Engines
Unsafe Condition: High-pressure compressor (HPC) 7th-stage integrally bladed rotor (IBR-7) separation resulting in engine shutdown and aborted takeoff.
Why matched: Airworthiness Directives; Pratt & Whitney Engines
2026-04-13 Recurring
final ruleAirworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines
Unsafe Condition: Fracture of the IP8 and HP3 air tubes could remain undetected for longer than assumed, leading to reduced efficiency of internal cooling and sealing flows, failure of the air tubes, damage to the e...
Why matched: Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines
2026-04-11 Recurring
final ruleAirworthiness Directives; Lycoming Engines
Unsafe Condition: Reports of connecting rod failures, which resulted in uncontained engine failure and in-flight shutdowns.
Why matched: Airworthiness Directives; Lycoming Engines
2026-04-02
final ruleAirworthiness Directives; BRP-Rotax GmbH & Co KG (Formerly BRP-POWERTRAIN GMBH & CO KG and Bombardier-Rotax GmbH) Engines
Unsafe Condition: an occurrence was reported of the M40 x 1.5 collar nut that had not been installed on the propeller gearbox of a recently manufactured engine, which could result in the propeller shaft being pulled...
Why matched: Airworthiness Directives; BRP-Rotax GmbH & Co KG (Formerly BRP-POWERTRAIN GMBH & CO KG and Bombardier-Rotax GmbH) Engines
2026-04-09
final ruleAirworthiness Directives; General Electric Company Engines
Unsafe Condition: Fracture and subsequent uncontained release of certain HPC stage 5 blisks due to a nonconforming indication in a single forged ingot used to manufacture the affected parts.
Why matched: Airworthiness Directives; General Electric Company Engines
2026-02-04 Recurring
final ruleAirworthiness Directives; CFM International, S.A. Engines
Unsafe Condition: Wear on the No. 3 bearing spring finger housing can lead to high levels of non-synchronous vibration (NSV), which could induce high-pressure compressor (HPC) stall.
Why matched: Airworthiness Directives; CFM International, S.A. Engines
2026-02-08
final ruleAirworthiness Directives; CFM International, S.A. Engines
Unsafe Condition: aborted takeoffs after engines did not advance to the desired takeoff fan speed due to icing in the pressure sensor line, which, if not addressed, could result in loss of engine thrust control and ...
Why matched: Airworthiness Directives; CFM International, S.A. Engines
2025-26-04
final ruleAirworthiness 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
2025-25-07
final ruleAirworthiness Directives; General Electric Company Engines
Unsafe Condition: High-pressure turbine (HPT) stage 1 and HPT stage 2 disks manufactured from powder metal material suspected to contain iron inclusion, which may cause reduced material properties and a lower fatigu...
Why matched: Airworthiness Directives; General Electric Company Engines
2025-26-03 Recurring
final ruleAirworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines
Unsafe Condition: The manufacturer identified a possibility of release of an HPC mini-disc anti-rotation block into the HPC assembly stage 5 and 6 discs and at the HPC rear drum during an engine operation.
Why matched: Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines
2025-21-03 Recurring
final ruleAirworthiness Directives; CFM International, S.A. Engines
Unsafe Condition: cracks in the high-pressure turbine (HPT) rotor stage 1 blades
Why matched: Airworthiness Directives; CFM International, S.A. Engines
2025-23-10
final ruleAirworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines
Unsafe Condition: certain low-pressure compressor (LPC) fan blades are at risk of cracking due to incorrect dressing, which may have been performed on areas of low wall thickness and high localized internal stress l...
Why matched: Airworthiness Directives; Rolls-Royce Deutschland Ltd & Co KG Engines
2025-20-18
final ruleAirworthiness Directives; Continental Aerospace Technologies GmbH Engines
Unsafe Condition: Cracks in the cylinder heads can cause engine coolant to leak into the combustion chamber, leading to engine overheat and eventual failure or seizure.
Why matched: Airworthiness Directives; Continental Aerospace Technologies GmbH Engines
2025-19-13
final ruleAirworthiness Directives; International Aero Engines AG Engines
Unsafe Condition: A quality escape following angled ultrasonic inspections performed on certain high-pressure turbine (HPT) 1st-stage hubs and HPT 2nd-stage hubs, which could result in an uncontained hub failure, re...
Why matched: Airworthiness Directives; International Aero Engines AG Engines
2025-18-08 Recurring
final ruleAirworthiness Directives; GE Aviation Czech s.r.o. (Type Certificate Previously Held by WALTER Engines a.s., Walter a.s., and MOTORLET a.s.) Engines
Unsafe Condition: Failure of the centrifugal compressor case.
Why matched: Airworthiness Directives; GE Aviation Czech s.r.o. (Type Certificate Previously Held by WALTER Engines a.s., Walter a.s., and MOTORLET a.s.) Engines
2025-17-16
final ruleAirworthiness Directives; International Aero Engines AG Engines
Unsafe Condition: Uncontained failure of a high-pressure turbine (HPT) 1st-stage hub that resulted in high-energy debris penetrating the engine cowling.
Why matched: Airworthiness Directives; International Aero Engines AG Engines
2025-14-08
final ruleAirworthiness Directives; CFM International, S.A. Engines
Unsafe Condition: fracture and subsequent uncontained failure of certain HPT rotor stage 1 disks and a certain compressor rotor stages 6-10 spool due to material properties reduced by iron inclusion
Why matched: Airworthiness Directives; CFM International, S.A. Engines