GE CF34-3B1

Service difficulty reports · 5,402

Newest first. General aviation reporting is voluntary.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE engine_model_key = 'CF343B1'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR ASOA05605Lamp · burned outDURING AN A-CHECK, THE RT FWD EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE RT FWD EXTERIOR EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Jul 15, 2005 · N905EV · Cndair CL6002B19 · Emergency LightingSDR VNAA0507011Radar · failedDURING CLIMB THE CREW REPORTED THAT THE WEATHER RADAR WAS PAINTING A LARGE RETURN ON THE RIGHT SIDE OF THE SCREEN WHEN THE AIRCRAFT BANKED. DUE TO WEATHER EN ROUTE AND AT DESTINATION THE CREW ELECTED TO RETURN TO CAK. MAINTENANCE REMOVED AND REPLACED THE WEJul 15, 2005 · N259PS · Cndair CL6002B19 · Independent Position Determining SystemSDR VNAA0507012Flap · unknownON FINAL APPROACH WITH FLAPS 20° THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT. MAINTENANCE COMPLIED WITH THE FLAP FAIL RESET PROCEDURES IAW CRJ200 RJ-SL-00-001. THE FLAPS OPERATIONALLY CHECK GOOD. THE AIJul 15, 2005 · N221PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200540244Angle · crackedRT FS 625, OBLIQUE ANGLE IS CRACKED. REMOVED CRACKED OBLIQUE ANGLE AND REPLACED WITH NOW IAW SRM. (K)Jul 15, 2005 · N420AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR REX2005F00016Control System · failed(REF NR: 05-087) FLAPS FAILED ON APPROACH, QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAPS AND PLACED SYSTEM ON 72 HOUR WATCH IAW AD 98-20-01. (K)Jul 15, 2005 · N801AY · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200540242Proximity Sensor · failedON GEAR RETRACTION, GEAR DISAGREE WARNING MESSAGE. COMPLIED WITH QRH. DOWNLOADED FDR AND FOUND BOTH LT AND RT MLG UPLOCKS INTERMITTENT UPA AND LOCKED. SUSPECT BAD PSEU, REMOVED AND REPLACED PSEU IAW MM. OPS CHECK GOOD. PERFORMED FUNCTION CHECKS OF LANDINGJul 14, 2005 · N467AW · Cndair CL6002B19 · Landing Gear Position and WarningSDR ASOA05602Light · inoperativeDURING A GROUND INSPECTION, EMERGENCY FLOOR LIGHTS FROM ROW 6 FORWARD WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED 4 EMERGENCY FLOOR LIGHT STRIPS FROM ROW 6 FORWARD AND ALSO DRIED OUT THE EMERGENCY FLOOR LIGHT TRACKS. OPERATIONAL CHECKS GOOJul 14, 2005 · N672BR · Cndair CL6002B19 · Emergency LightingSDR ASOA05603Light · inoperativeDURING A GROUND INSPECTION, THE EMERGENCY FLOOR LIGHTS ON THE RT SIDE FROM ROW 6 TO THE GALLEY WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLOOR LIGHT STRIPS FROM ROW 2 TO 5. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)Jul 14, 2005 · N844AS · Cndair CL6002B19 · Emergency LightingSDR ASOA05604Doubler · crackedDURING AN A-CHECK, THE FS 640 RT DOUBLER AT STRINGER 10 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FS 640 RT DOUBLER AT STRINGER 10. (K)Jul 14, 2005 · N915EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA05601Battery · dischargedDURING A GROUND INSPECTION, THE EMERGENCY FLOOR LIGHTS AT ROWS 2-4 WERE FOUND INOPERATIVE. MAINTENANCE CHARGED THE EMERGENCY LIGHT BATTERIES, CLEANED AND RESECURED THE CONNECTIONS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Jul 14, 2005 · N820AS · Cndair CL6002B19 · Emergency LightingSDR ASO2005F00001Battery · dischargedDURING GROUND INSPECTION, THE EMERGENCY FLOOR LIGHTS AT ROWS 2-4 WERE FOUND TO BE INOPERATIVE. MAINTENANCE CHARGE THE EMERGENCY LIGHT BATTERIES, CLEANED AND RESECURED THE CONNECTIONS. OPERTIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Jul 14, 2005 · N820AS · Cndair CL6002B19 · Emergency LightingSDR ASO2005F00002Battery · dischargedDURING GROUND INSPECTION, THE EMERGENCY FLOOR LIGHTS AT ROWS 2-4 WERE FOUND TO BE INOPERATIVE. MAINTENANCE CHARGED THE EMERGENCY LIGHT BATTERIES, CLEANED AND RESECURED THE CONNECTIONS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Jul 14, 2005 · N820AS · Cndair CL6002B19 · Emergency LightingSDR ASO2005F00003Battery · dischargedDURING A GROUND INSPECTION, THE EMERGENCY FLOOR LIGHTS AT ROWS 2-4 WERE FOUND TO BE INOPERATIVE. MAINTENANCE CHARGED THE EMERGENCY LIGHT BATTERIES, CLEANED AND RESECURED THE CONNECTIONS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Jul 14, 2005 · N820AS · Cndair CL6002B19 · Emergency LightingSDR REX2005F00017Switch · out of adjust(REF NR: 05-086) ON APPROACH, CREW RECEIVED A LT THRUST REVERSER UNLOCKED MESSAGE WHEN THE THRUST REVERSERS WERE ARMED. FLIGHT CREW DECLARED AN EMERGENCY AND COMPLETED THE MEMORY AND QRH ITEMS. AN OTHERWISE UNEVENTFUL APPROACH AND LANDING WITHOUT THRUST REVJul 14, 2005 · N8944B · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA200540235Clip · crackedRT FS 280 AT RBL 9 OB CLIP ANGLE IS CRACKED .5 INCH LONG. (K)Jul 13, 2005 · N409AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6AW200540237Clip · crackedLT FS 280 AT LBL 9 IB CLIP ANGLE IS CRACKED .5 INCH LONG. (K)Jul 13, 2005 · N409AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200540236Clip · crackedRT FS 280 AT RBL 9 IB CLIP ANGLE IS CRACKED .5 INCH LONG. (K)Jul 13, 2005 · N409AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200540247Stringer Clip · crackedRT FS 280 AT RBL 9, OB CLIP ANGLE IS CRACKED .5 INCH LONG. REPLACED CLIP IAW SRM. (K)Jul 13, 2005 · N409AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200540238Intercostal · crackedLT SIDE FS 484 INTERCOSTAL IS CRACKED AT LBL 36. CRACK IS APPROX 1.1 INCH LONG. REPAIRED LT SIDE FS 484 INTERCOSTAL AT LBL 36 IAW MFGREO. (K)Jul 13, 2005 · N409AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540234A/C Pack · leakingCABIN FILLED WITH SMOKE WHILE AT GATE WITH ENGINES OFF, APU AND BOTH PACKS RUNNING. INSPECTED AFT EQUIPMENT BAY AND FOUND AIR LEAK RT PACK WATER SEPARATOR PIPE. NO EVIDENCE OF SMOKE WITH APU AND BOTH PACK ON. (K)Jul 13, 2005 · N408AW · Cndair CL6002B19 · APU Oil SystemSDR A6WA200540239Intercostal · crackedRT SIDE FS 484 INTERCOSTAL IS CRACKED AT RBL 36. CRACK IS APPROX 0.4 INCH LONG. REPAIRED RT SIDE FS 484 INTERCOSTAL IAW MFG REO. (K)Jul 13, 2005 · N409AW · Cndair CL6002B19 · Fuselage Main, StructureSDR A6WA200540240Angle · crackedLT FS 280 AT LBL 9 OB CLIP ANGLE IS CRACKED .5 INCH LONG. REPLACED CLIP IAW SRM. (K)Jul 13, 2005 · N409AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540241Engine · odorINFLIGHT DETECTED OILY ODOR AFTER BLEED AIR CHANGE OVER FROM APU TO ENGINE AIR IN COCKPIT. FERRIED FOR ENGINE NR 1 CHANGE. (K) REMOVED AND REPLACED COALESCER SOCKS IN LEFT AND RIGHT WATER SEPARATORS, NO FURTHER ODOR NOTED. (M)Jul 13, 2005 · N457AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR A6WA200540246Angle · crackedRT FS 280 AT RBL 9 IB CLIP ANGLE IS CRACKED .5 INCH LONG. REPLACED CLIP IAW SRM. (K)Jul 13, 2005 · N409AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA05598Engine · malfunctionedDURING CLIMB OUT, AT APPROXIMATELY 12,000 FEET THE CREW RECEIVED A (RT ENGINE OIL PRESSURE) WARNING WITH THE OIL TEMPERATURE INCREASING TO 153 DEGREES CENTIGRADE AND THE OIL PRESSURE FLUCTUATING BETWEEN 24-36 PSI. QRH WAS COMPLIED WITH AND AN EMERGENCY WAS DEJul 13, 2005 · N871AS · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR ASOA05599Tire · separatedDURING TAKEOFF, TOWER INFORMED CREW THAT TIRE DEBRIS WAS NOTICED ON RUNWAY AFTER DEPARTURE. THERE WERE NO INDICATIONS OF ENGINE DAMAGE AND AC CONTINUED. EMERGENCY WAS DECLARED AND EMERGENCY VEHICLES WERE REQUESTED TO BE ON STANDBY AS PRECAUTION. AC LANDED SJul 13, 2005 · N902EV · Cndair CL6002B19 · TireSDR ASO2005F00004Flap · damagedDURING TAKEOFF, TOWER INFORMED CREW THAT TIRE DEBRIS WAS NOTICED ON RUNWAY AFTER DEPARTURE. THERE WERE NO INDICATIONS OF ENGINE DAMAGE AND AC CONTINUED. EMERGENCY WAS DECLARED AND EMERGENCY VEHICLES WERE REQUESTED TO BE ON STANDBY AS PRECAUTION. AC LANDED SJul 13, 2005 · N9023V · Cndair CL6002B19 · Trailing Edge FlapsSDR ASO2005F00005Fairing · damagedDURING TAKEOFF, TOWER INFORMED CREW THAT TIRE DEBRIS WAS NOTIED ON RUNWAY AFTER DEPARTURE. THERE WERE NO INDICATIONS OF ENGINE DAMAGE AND AC CONTINUED. EMERGENCY WAS DECLARED AND EMERGENCY VEHICLES WERE REQUESTED TO BE ON STANDBY AS PRECAUTION. AC LANDED SAJul 13, 2005 · N902EV · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASO2005F00006Fairing · damagedDURING TAKEOFF, TOWER INFORMED CREW THAT TIRE DEBRIS WAS NOTICED ON RUNWAY AFTER DEPARTURE. THERE WERE NO INDICATIONS OF ENGINE DAMAGE AND AC CONTINUED. EMERGENCY WAS DECLARED AND EMERGENCY VEHICLES WERE REQUESTED TO BE ON STANDBY AS PRECAUTION. AC LANDED SJul 13, 2005 · N902EV · Cndair CL6002B19 · Aerodynamic FairingsSDR A6WA200540237Angle · crackedLT FS 280.00 AT LBL 9 IB CLIP ANGLE IS CRACKED .5 INCH LONG. REPLACED CLIP IAW SRM. (K)Jul 13, 2005 · N409AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA05595Warning Light · illuminatedDURING CRUISE, AT APPROX 30,000 FT, CREW RECEIVED A (R ENG OIL PRESS) WARNING MESSAGE. QRH WAS COMPLIED WITH AND THE POWER LEVER WAS BROUGHT TO IDLE WITH THE OIL PRESSURE STABILIZING AT 25-30 PSI. DURING DESCENT THROUGH 10, 000 FEET THE OIL PRSSURE STABILIZEJul 12, 2005 · N871AS · Cndair CL6002B19 · Engine Oil System (Airframe Furnished)SDR ASOA05596Pressure Switch · malfunctionedDURING CLIMB OUT, AT APPROXIMATELY 16,000 FEET, THE CREW RECEIVED A (R ENG OIL PRESS) MESSAGE. QRH WAS COMPLIED WITH AND POWER WAS BROUGHT BACK TO IDLE ON THE RT ENGINE. OIL PRESSURE STABILIZED AND THE AC CONTINUED ON. AN EMERGENCY WAS DECLARED AND THE AIRCJul 12, 2005 · N871AS · Cndair CL6002B19 · Engine Oil Indicating SystemSDR MASA200500542Fire Loop · malfunctionedASH 2786 PHL. RIGHT HAND 14TH STAGE DUCT WARNING. CREW SHUTDOWN THE ENGINE AND MX IS CURRENTLY TROUBLESHOOTING THE FAULT. MAINTENANCE REMOVED AND REPLACED THE 14TH STAGE SENSE LOOP.Jul 12, 2005 · N571ML · Cndair CL6002B19 · Fire DetectionSDR A6WA200540233Idg · failedIDG NR 1 CAUTION MESSAGE ON TAKEOFF ROLL, ABORTED TAKEOFF, IDG MESSAGE EXTINGUISHED AND REPLACED WITH GEN NR1 OFF CAUTION MESSAGE. FOLLOWED QRH, MESSAGE CLEARED ALL. ABORTED TAKEOFF AT 40 KNOTS. REMOVED AND REPLACED IDG NR 1, OP CHECK AND LEAK CHECK GOOD. Jul 11, 2005 · N402AW · Cndair CL6002B19 · Alternator-Generator DriveSDR ASOA05594Connector · disconnectedDURING A GROUND INSPECTION, THE AFT SECTION OF EMERGENCY FLOOR TRACK LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE RECONNECTED THE AFT SECTION OF EMERGENCY FLOOR TRACK LIGHTS. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)Jul 11, 2005 · N878AS · Cndair CL6002B19 · Emergency LightingSDR ASO2005F00007Carbon Seal · wornSTARTER CARBON SEAL, WORN. (K)Jul 11, 2005 · N875AS · Cndair CL6002B19 · Accessory GearboxesSDR ASOA05618Intercostal · crackedDURING A C-CHECK, THE PASSENGER DOOR INTERCOSTAL AND INNER SKIN WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE PASSENGER DOOR INTERCOSTAL AND INNER SKIN IAW EO. (K)Jul 10, 2005 · N852AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200540227Control Unit · malfunctioned(CONFIG SPOILER) CAS MESSAGE ILLUMINATED ON TAKEOFF, ABORTED TAKEOFF. PERFORMED BELOW 20 KNOTS. REMOVED AND REPLACED SECU NR 1 IAW AMM. OPS CHECK GOOD. (K)Jul 9, 2005 · N429AW · Cndair CL6002B19 · Drag Control SystemSDR CA050923001Selector Valve · failed(CAN) ON APPROACH THE 3A AND 3B HYD PUMPS WERE TURNED ON. SHORTLY THEREAFTER THE SYSTEM 3 HIGH TEMP MSG CAME ON. QRH FOLLOWED AND TURNED OFF 3A PUMP TO ISOLATE PROBLEM. THE HIGH TEMP WENT OUT. ON SHORT FINAL THE CREW PUT GEAR DOWN, THE GEAR DISAGREE MSG CAJul 9, 2005 · Cndair CL6002B19 · Landing Gear SelectorSDR A6WA200540228Skin · corrodedMWC 59 WING PLANK, RT WING, UNDER FUEL ACCESS PANEL 650EB IS SEVERLY CORRODED AROUND ENTIRE CIRCUMFERENCE OF OPENING, .150 INCH WIDE X .005 INCH DEEP. BLENDED LOWER WING PLANK IAW MFG REO. (K)Jul 8, 2005 · N461AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200540229Skin · dentedMWC 1 DENT IN AFT FUSELAGE AT FS 672 BETWEEN STRINGERS 26L AND 27L. CUT OUT DAMAGED AREA AND INSTALLED FABRICATED FILLER PARTS IAW EO. (K)Jul 8, 2005 · N461AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR VNAA0507007Selector Valve · failedTHE NOSE DOOR OPEN WARNING ILLUMINATED AND SOUNDED AFTER GEAR RETRACTION. THE FLIGHT RETURNED TO SDF. THE AIRCRAFT WAS FERRIED TO PHL WHERE MAINTENANCE REMOVED & REPLACED THE NLG DOOR SELECTOR VALVE IAW CRJ200 AMM 32-22-20-000-801 AND 32-22-20-400-801. LEAKJul 7, 2005 · N226JS · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR ASOA05617Angle · crackedDURING A C-CHECK, THE LT OB FS 484 ANGLE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRE THE LT OB FS 484 ANGLE IAW EO. (K)Jul 7, 2005 · N852AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0560383Warning Light · illuminatedFLIGHT 5549 - EN ROUTE BOS-PWM DURING DESCENT RECEIVED A LEFT THRUST REVERSER UNLOCK MESSAGE. CREW DECLARED AN EMERGENCY AND SHUTDOWN THE LEFT ENGINE. AIRCRAFT LANDED WITHOUT INCIDENT. DEFERRED THE LEFT THRUST REVERSER PER MEL.Jul 6, 2005 · N457CA · Cndair CL6002B19 · Engine Thrust ReverserSDR VNAA0507005Warning Light · illuminatedTHE NOSE DOOR OPEN WARNING ILLUMINATED AND SOUNDED ON SHORT FINAL. MAINTENANCE INSPECTED THE NLG DOORS IAW CRJ200 AMM 32-20-00-210-801. OPERATIONAL CHECKS WERE NORMAL. NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE.Jul 6, 2005 · N226JS · Cndair CL6002B19 · Landing Gear Position and WarningSDR REX2005F00018Control System · failed(REF NR: 05-085) FLAP FAILED ON APPROACH. RESET SYSTEM AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K)Jul 6, 2005 · N8554A · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR ASOA05616Plate · crackedDURING C-CHECK, THE CARGO DOOR FLOOR LANDING PLATE WAS FOUND TO BE CRACKED FROM THE CENTER 2 RIVETS BEYOND LIMITS. MAINTENANCE REPAIRED THE CARGO DOOR FLOOR LANDING PLATE IAW EO. (K)Jul 5, 2005 · N852AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0560377Idg · underservicedNR 1 IDG CAUTION. SERVICED IDG OIL. OPERATION CHECKS SATISFACTORY.Jul 3, 2005 · N957CA · Cndair CL6002B19 · AC Generator-AlternatorSDR VNAA0507002Skin · lightning strikeTHE CREW REPORTED A LIGHTNING STRIKE DURING DESCENT. MAINTENANCE COMPLIED WITH A DETAILED LIGHTNING STRIKE INSPECTION IAW CRJ200 AMM 05-51-05-220-801. THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE REPAIRED THE LIGHTNING DAMAGE AND RELEASED THE AIRCRAFT FJul 3, 2005 · N202PS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR VNAA0507001Skin · lightning strikeAFTER LANDING MAINTENANCE DISCOVERED EVIDENCE OF LIGHTNING DAMAGE ON THE LT WING TIP. A DETAILED LIGHTNING STRIKE INSPECTION WAS PERFORMED IAW CRJ200 AMM 05-51-05-220-801. ALL DAMAGE WAS REPAIRED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.Jul 2, 2005 · N220PS · Cndair CL6002B19 · Wing, Plate/Skin
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