CATALYST AVIATION, LLC.
Also recorded as: CATALYST AVIATION, LLC., Catalyst Aviation LLC, Catalyst Aviation, LLC., N/A
Accident & enforcement record
Events that happened, regardless of the operator's own reporting. Each links to its public source.
NTSB accidents & incidents
Operated by Catalyst Aviation LLC (per NTSB report)
Operated by Catalyst Aviation LLC (per NTSB report)
FAA enforcement actions
FAA enforcement records haven't been loaded into GroundCheck yet, so none can be shown — a gap in our data, not evidence of a clean enforcement history.
Maintenance disclosure history
Service Difficulty Reports are self-reported maintenance findings. The NUMBER of reports is not a measure of reliability — diligent operators file more, not fewer. These are shown for transparency, not as a negative signal.
73 reports on file — showing most recent 50.
RIGHT LOWER WING PLANK DRAIN VALVE ATTACH HOLE SHOWS DEFECT INDICATION AT WS 0.0, STRINGER 5. OVERSIZED SCREW HOLE TO REMOVE DEFECTS AND INSTALLED A FREEZE PLUG IAW EA 10-5721-02848.
LEFT LOWER WING PLANK DRAIN VALVE ATTACH HOLE SHOWS DEFECT INDICATION AT WS 0.0, STRINGER 15. OVERSIZED SCREW HOLE TO REMOVE DEFECTS AND INSTALLED A FREEZE PLUG IAW EA 10-5721-02848.
LEFT LOWER WING PLANK DRAIN VALVE ATTACH HOLE SHOWS DEFECT INDICATION AT WS 65.75, STRINGER 15. OVERSIZED SCREW HOLE TO REMOVE DEFECTS AND INSTALLED A FREEZE PLUG IAW EA 10-5721-02848.
RIGHT LOWER WING PLANK DRAIN VALVE ATTACH HOLE SHOWS DEFECT INDICATION AT WS 65.75, STRINGER 15. OVERSIZED SCREW HOLE TO REMOVE DEFECTS AND INSTALLED A FREEZE PLUG IAW EA 10-5721-02848.
FLIGHT 5416. GALLEY EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LAMPS. (A)
DURING HMV-5 INSPECTION EDDY CURRENT OF AFT PRESSURE BULKHEAD, FOUND 3 CRACKS AROUND LINTEL ATTACHMENT FITTING. REPAIRED CRACKS TO AFT PRESSURE BULKHEAD AROUND LINTEL FITTING AS PER REO 601R-53-61-1230 AND REO 601R-53-61-2463.
DURING HMV-5 INSPECTION, FOUND CRACK AT LOWER END OF VERTICAL STIFFENER. CUT OUT DAMAGE AND INSTALLED DOUBLER IAW BOMBARDIER REO 601R-53-41-056.
DURING 559 EDDY CURRENT INSPECTION FOUND A CRACK ON THE 559 WEB. CUT OUT DAMAGE AND INSTALLED DOUBLER IAW SR10-5341-001 REV A SECTION 1 PERMANENT REPAIR.
CABIN FLOOR LATERAL BEAM CRACKED ON LOWER FLANGE. COMPLIED WITH REO601R-53-11-1308 BY CUTTING OUT DAMAGE AND APPLYING DOUBLER.
DURING 559 INSPECTION FOUND .6 INCH CRACK ON INBOARD SIDE AND .8 INCH CRACK AT OUTBOARD SIDE OF VERTICAL STIFFENERS. REMOVED DAMAGE AND INSTALLED DOUBLERS PER BOMBARDIER REO 601R-53-41-057.
LONGITUDINAL FLOORBEAM ATTACH CLIP CRACKED FS 280, LBL 10 OUTBOARD SIDE OF BEAM. REMOVED AND REPLACED CLIP IAW CRJ SRM 51-42-21.
LONGITUDINAL FLOORBEAM ATTACH CLIP CRACKED AND HAS LOOSE FASTENERS, INBOARD SIDE OF BEAM FS 280, LBL 9. REMOVED AND REPLACED CLIP IAW CRJ SRM 51-42-21.
FLIGHT 5425 - EMERGENCY LIGHT ON CEILING BY LAV INOP. REMOVED AND REPLACED LAMP.
FLIGHT 4945 - EN ROUTE CVG-OKC RECEIVED A LEFT ENGINE OIL PRESSURE FLUCTUATION WITH INTERMITTENT OIL PRESSURE WARNING. CREW DECLARED AN EMERGENCY AND FLIGHT RETURNED TO CVG LANDING WITHOUT INCIDENT. INSTALLED A STARTER MATING SEAL.
FLIGHT 5598 - RECEIVED GEAR DISAGREE WARNING AFTER TAKEOFF. RETURNED TO SAV AND LANDED WITHOUT INCIDENT. FOUND MLG UPLOCK PROXIMITY SENSOR OUT OF ADJUSTMENT AND TARGET LOOSE. ADJUSTED SENSOR AND SECURED TARGET. NO FURTHER DEFECTS.
FLIGHT 5385- HYD SYS NR 2 LOW PRESS (SYS QTY SHOWED 5 PERCENT) A/C DIVERTED TO RIC AND LANDED SAFELY. REMOVED AND REPLACED HYD SYS NR 2 CASE DRAIN TUBE ASSY.
FLIGHT 5885 - DURING TAKEOFF ROLL RECEIVED A PROXIMITY SYSTEM FAULT MESSAGE, CREW ABORTED TAKEOFF AND RETURNED TO THE GATE. PERFORMED SYSTEM TEST ON PSEU, DISCREPANCY COULD NOT BE DUPLICATED BY MAINTENANCE.
FLIGHT 5500 - DURING TAKEOFF ROLL RECEIVED A RIGHT AIR CONDITIONING PACK HIGH PRESSURE CAUTION, ABORTED TAKEOFF AND RETURNED TO THE GATE. PERFORMED AN OPERATIONAL CHECK OF THE AIR CONDITIONING PACKS, DISCREPANCY COULD NOT BE DUPLICATED.
FLIGHT 5057 - AFTER TAKEOFF FROM DAY RECEIVED A GEAR DISAGREE/NOSE DOOR OPEN MESSAGE, FLIGHT RETURNED TO THE FIELD. REPLACED THE NLG STRUT LOWER CYLINDER.
FLIGHT 5463 - NLG WILL NOT RETRACT. NLG CENTERED, PROX SWITCH TARGET BENT. C/W TEMPORARY REPAIR TO PROX SWITCH TARGET.
FLIGHT 4998 - NR 2 HYDRAULIC SYSTEM HIGH TEMP AND LOW PRESSURE WARNING. REPLACED THE RT ENGINE HYDRAULIC PUMP.
GEAR DISAGREE. SERVICED NLG SHOCK STRUT, GEAR SWINGS SATISFACTORY.
FLIGHT 5309 RT OVERWING EMERGENCY LIGHT IS INOP. REPLACED LIGHT BULB.
FLIGHT 5812 CABIN DOOR HANDLE CAUTION MESSAGE. FOUND DOOR HANDLE NOT STOWED. OPERATIONAL CHECK OF DOOR SATISFACTORY. NO DEFECTS FOUND.
FLIGHT 5888 RT AC PACK HIGH PRESSURE CAUTION. COULD NOT DUPLICATE. AIR CONDITION SYSTEM OPERATES NORMAL.
FLIGHT 5724 PARKING BRAKE SOV CAUTION MESSAGE. REPLACED THE PARKING BRAKE SOV.
FLIGHT 5282 RIGHT ENGINE OIL PRESSURE WARNING DURING T/O. REPLACED THE OIL PRESSURE TRANSDUCER.
FLIGHT 5073 FLAPS FAIL CAUTION MESSAGE. REPLACED THE FECU.
FRETTING DAMAGE ON LEFT HAND LOWER WING PLANK FUEL ACCESS HOLE CUTOUT AT 550EB. BLENDED DAMAGE OUT AND ROTO-PEENED AFT OUTBAORD HATCHED AREA IN ACCORDANCE WITH REO 601R-57-21-030.
FLIGHT 5803 RT ENGINE LOST OIL PRESSURE IFSD. REPLACED THE RT ACCESSORY GEAR BOX OIL SEALS.
FLIGHT 5141 RIGHT THRUST REVERSER UNLOCKED CAUTION DURING TAKEOFF. SECURED AND DEFERRED MAINTENANCE ON THRUST REVERSER PER MEL.
FLIGHT 9457 NR 2 HYDRAULIC SYSTEM HIGH TEMP CAUTION. REPLACED THE NR 2 HYDRAULIC RESERVOIR.
FLIGHT 5378 CREW REPORTED "AILERONS BINDING". COULD NOT DUPLICATE - NO AILERON BINDING NOTED - C/W COMAIR EO 27-075 FOR TROUBLESHOOTING.
FLIGHT 5686 UNCONTROLLED MOMENTARY ROLL DURING CRUISE FLIGHT, FOLLOWED BY SPOILERONS FAULT MESSAGE. REPLACED THE RT INBOARD SPOILERON PCU.
FLIGHT 5239 LEFT 14TH STAGE BLEED AIR DUCT WARNING.TIGHTENED LOOSE BLEED AIR COUPLING AT THE T/R PDU
FLIGHT 5848 LEFT ENG FAN VIB WARNING, ITT IN RED. IFSDREPLACED THE LEFT ENGINE.
FLIGHT 5575 CABIN DOOR OUTER HANDLE CAUTION MESSAGE.COULD NOT DUPLCITE. OPERATION OF CABIN DORO NORMAL.
FLIGHT 5275 SMOKE IN CABIN AND COCKPIT WHEN BLEEDS SOURCE SELECTED TO APU.PLACED APU ON DEFERRED MAINT LIST PER MEL.
FLIGHT 5966 LEFT ENGINE OIL PRESSURE WARNING.REPAIRED CHAFED WIRE AT OIL PRESSURE SWITCH.
FLIGHT 5635 UNCOMMANDED RUDDER OSCILLATIONS.REPLACED THE #2 DCU.
THE L/H SIDE FRAME AND AFT DOUBLER AT FS718.0 WERE CRACKED BETWEEN STRINGERS 10 AND 12.REMOVED THE CRACKED AFT DOUBLER AND DAMAGED SECTION OF FRAME. INSTALLED NEW SECTION OF FRAME SPLICE AND NEW AFT DOUBLER I/A/W REO 601R-53-61-193 REV A.
VERTICAL STABILIZER, L/II HORIZONTAL ATTACH LUG BUSHING MIGRATED.REPLACED BUSHING P/N #600-21061-7 IAW SERVICE BULLETIN 601R-55-007, REF MAINT LOG PAGE #243117 AND COMAIR W/O #169071.
FLAPS FAILED AT 16 DEGREES.REPLACED THE FLAP PDU.
FLAP FAILED AT 17 DEGREES.REPLACED THE LEFT HAND BPSU.
FLAPS FAILED AT 13 DEGREES.REPLACED THE R/H #4 FLAP ACTUATOR.
FLAPS FAILED AT 13 DEGREES.REPLACED THE LEFT HAND BPSU.
FLAPS FAILED AT 17 DEGREES. RESET FLAP SYSTEM AND DEFERRED MAINTENANCE PER AD 98-20-01.
LOWER WING ACCESS HOLES CRACKED AT 550BB WS 188.040 550CB WS 209.040 AND 550EB WS 253.022. BLENDED DAMAGE AND ROTO-PEENED IAW REO 601R-57-21-030.
LEFT ENGINE N2 VIB WARNING. REPLACED THE LEFT ENGINE.
FLAPS FAILED AT 8 DEGREES. REPLACED THE FECU.