GE CF34-3B1

Service difficulty reports · 5,402

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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 ASOA05460Step · missingDURING A GROUND INSPECTION, THE EMERGENCY EGRESS STEP LOCATED ON TOP OF THE COPILOTS SEAT ASSEMBLY WAS FOUND MISSING. MAINTENANCE INSTALLED THE EMERGENCY EGRESS STEP ON TOP OF THE COPILOTS SEAT ASSY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)May 25, 2005 · N874AS · Cndair CL6002B19 · Flight Compartment EquipmentSDR ASOA05461Step · crackedDURING A GROUND INSPECTION, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)May 25, 2005 · N889AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA05464Fire Warning · false activationDURING DESCENT, THE CREW RECEIVED AN APU FIRE WARNING. THE QRH WAS COMPLIED WITH AND THE MESSAGE EXTINGUISHED PRIOR TO DISCHARGING THE APU FIRE BOTTLE. THE TOWER DECLARED AN EMERGENCY AND THE AIRCARFT LANDED SAFELY. EMERGENCY VEHICLES MET AND FOLLOWED THE AMay 25, 2005 · N833AS · Cndair CL6002B19 · Fire DetectionSDR A6WA200540185Skin · dentedRT IB FLAP LOWER SKIN 4.5 INCH FROM T/E ND 17. INCH FROM IB EDGE. DENT IS 2 INCHES X 2 INCHES X 0.45 INCHES. PERFORMED MAJOR REPAIR BY INSTALLING NON-FLUSH REPAIR IAW SRM. (K)May 25, 2005 · N456ZW · Cndair CL6002B19 · Trailing Edge FlapsSDR CA050923002Engine · overheated(CAN) MFG HAS RECEIVED A REPORT WHICH WE FEEL IS A REPORTABLE EVENT. THE FLIGHT CREW REJECTED TAKE-OFF WHEN THEY NOTICED THE AIRCRAFT VEERING TO THE RT ASSOCIATED WITH ENGINE NR 2 OIL PRESSURE AND ITT ABNORMALITIES. TAKE-OFF WAS ABORTED AT APPROXIMATELY 100 May 25, 2005 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR A6WA200540181Skin · dentedLT IB FLAP HAS A DENT 22 INCHES FROM IB EDGE AND 14 INCHES FROM THE DENT IS 2 INCH X 2 INCH X 0.55 INCH. LOWER SKIN. PERFORMED A MAJOR REPAIR B4 INSTALLING A 8 INCH X 16 INCH NON-FLUSH REPAIR. (K)May 24, 2005 · N455AW · Cndair CL6002B19 · Trailing Edge FlapsSDR VNAA0505009Skin · dentedDURING THE INTERMEDIATE EXTERNAL INSPECTION THE CREW DISCOVERED A DENT ON THE BOTTOM OF THE LEFT INBOARD FLAP. MAINTENANCE REMOVED & REPLACED THE FLAP IAW CRJ 200 AMM 27-54-01-000-801 AND 27-54-01-400-801. THE SYSTEM WAS RIGGED AND OPERATIONALLY CHECKED GOODMay 24, 2005 · N257PS · Cndair CL6002B19 · Trailing Edge FlapsSDR VNAA0505011Tire · damagedEN ROUTE TO DAY THE CREW WAS NOTIFIED OF POSSIBLE NOSE WHEEL DAMAGE DUE TO A MISSING TOW BAR SHEAR PIN IN PHL. THE CREW CONTINUED TO DAY AND MADE AN UNEVENTFUL LANDING. MAINTENANCE FOUND THE RT NLG TIRE CHINE DAMAGED. THE WHEEL & TIRE ASSEMBLY WAS REMOVED &May 24, 2005 · N251PS · Cndair CL6002B19 · TireSDR ASOA05459Odor · detectedDURING TAKEOFF AND LANDING, THE CREW NOTICED A HOT BRAKE ODOR. THE AC LANDED SAFELY. MAINTENANCE JACKED THE MAIN LANDING GEARS WITH BRAKES RELEASED. BOTH IB AND OB BRAKES OPERATED FREELY AND ALL GEAR INDICATIONS WERE GOOD. MAINTENANCE ALSO TESTED THE ANTI-May 24, 2005 · N833AS · Cndair CL6002B19 · Air Distribution SystemSDR VNAA0505010Skin · puncturedDURING THE INTERMEDIATE EXTERNAL INSPECTION THE CREW DISCOVERED TWO HOLES PUNCTURED IN THE FUSELAGE SKIN BELOW AND AFT OF THE CARGO DOOR. THE HOLES WERE TEMP REPAIRED AND THE AIRCRAFT WAS FERRIED TO DAY. MAINTENANCE REPAIRED DAMAGED STRINGERS 22L & 23L IAW CMay 23, 2005 · N206PS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA05458Step · crackedDURING HANGAR MAINTENANCE, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR IAW AMM. (K)May 23, 2005 · N902EV · Cndair CL6002B19 · Fuselage Main, StructureSDR VNAA0505007Flap System · unknownINBOUND TO DCA THE FLAPS FAILED AT 20 DEGREES. THE CREW ELECTED TO DIVERT TO IAD. MAINTENANCE TROUBLESHOT THE SYSTEM IAW CRJ 200 FIM 27-50-00. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.May 22, 2005 · N206PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA0505005Skin · lightning strikeDURING POST FLIGHT INSPECTION THE CREW REPORTED EVIDENCE OF A LIGHTNING STRIKE ON THE FRONT LEFT NOSE SECTION OF THE FUSELAGE. THE AIRCRAFT WAS FERRIED TO DAY WHERE LIGHTNING STRIKE INSPECTIONS WERE COMPLIED WITH IAW CRJ 200 AMM 05-51-05-210-801 AND 05-51-05-May 20, 2005 · N223JS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA200540179Bushing · migratedRT AFT MAIN LANDING GEAR TRUNNION BUSHING MIGRATED .058 INCH. REMOVED RT AFT MLG TRUNNION BUSHING AND INSTALLED NEW SERVICEABLE BUSHING IAW MFG REO. (K)May 19, 2005 · N455AW · Cndair CL6002B19 · Main Landing Gear Attach SectionSDR A6WA200540180Bushing · migratedLT AFT MLG TRUNNION BUSHING MIGRATED .053 INCH. REMOVED LT AFT MLG TRUNNION BUSHING AND INSTALLED NEW SERVICEABLE BUSHING IAW MFG REO. (K)May 19, 2005 · N455AW · Cndair CL6002B19 · Main Landing GearSDR MASA200500370Warning Light · unknownASH 6491 PHX TO ICT - THE CREW ABORTED TAKEOFF DUE TO HIGH ITT. MAINTENANCE INSPECTED THE PLANE AND ENGINE BUT COULD NOT DUPLICATE THE PROBLEM.May 19, 2005 · N77302 · Cndair CL6002B19 · Engine Indicating SystemSDR A6WA200540178Apu · flamed outAPU AUTOSHUT AND GRD CREW ADVISED FLAME COME OUT OF INTAKE. LOUD BANG WHEN SHUTDOWN. DISCHARGED BOTTLES. INSP APU AREA, NO EVIDENCE OF FIRE, C/W (M) ACTION IAW MEL. (K)May 18, 2005 · N412AW · Cndair CL6002B19 · APU Engine Fuel and ControlSDR REX2005F00036Smoke Detector · false indication(REF NR: 05-067) RECEIVED (CARGO SMOKE) WARNING IN FLIGHT. EMERGENCY DECLARED, QRH FOLLOWED EXTINGUISHING SYSTEM ACTIVATED WITH UNEVENTFUL LANDING AND PASSENGER EVACUATION ON TAXI WAY. INVESTIGATED, FOUND TO BE FALSE WARNING. SYSTEM DEFERED IAW MEL. (K)May 18, 2005 · N8721B · Cndair CL6002B19 · Smoke DetectionSDR REX2005F00037Control System · out of rig(REF NR: 05-066) FLAPS FIAL ON TAXI. QRH FOLLOWED, RETURNED TO BLOCKS. FLAP SYSTEM RIGGED IAW AMM. OPS CHECKED GOOD. (K)May 18, 2005 · N825AY · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200540175Skin · dentedRT IB FLAP LOWER SKIN HAS A DENT 2 INCHES X 2.5 INCHES AND .077 INCH DEEP. DENT IS 24 INCHES FROM IB EDGE AND 2 INCHES FROM TRAILING EDGE. REPAIRED RT IB FLAP LOWER SKIN BY INSTALLING FLUSH REPAIR IAW BRAS EO. (K)May 17, 2005 · N452AW · Cndair CL6002B19 · Trailing Edge FlapsSDR CA050523001Handle · brokenAFTER LIFT OFF 'GEAR DISAGREE' MESSAGE APPEARED. THE NOSE WHEEL WOULD NOT RETRACT AND NOSE DOORS DID NOT CLOSE. AIRCRAFT RETURNED TO POINT OF DEPARTURE. WHEN DOING THE EMERGENCY EXTEND THE HANDLE BROKE OFF.May 17, 2005 · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR REX2005F00038Control System · failed(REF NR: 05-065) FLAPS FAILED AT 30 ON APPROACH. RESET SYSTEM, PLACED FLAPS ON 72 HOUR WATCH IAW AD 98-20-01. (K)May 17, 2005 · N800AY · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR MASA200500365Oil System · malfunctionedASH FLT 6145 PHX TO SBA - THE PILOT RETURNED TO FIELD WITH THE NR 2 ENGINE OIL PRESSURE AT 35 PSI AND THE NR 2 OIL TEMP AT 157 DEGREES. MAINTENANCE DRAINED AND RESERVICED THE NR 2 ENGINE OIL.May 17, 2005 · N17275 · Cndair CL6002B19 · Turbine Engine Oil SystemSDR A6WA200540176Skin · dentedRT AFT FUSELAGE SKIN AT FS 590, 11 INCHES BELOW LOW PRESSURE EXT AIR DOOR HAS DENT AND GOUGE. REPAIRED LOWER AFT FUSELAGE SKIN AT FS 590 BETWEEN STRINGERS 21L AND 25R BY REMOVING EXISTING REPAIR AND INSTALLING A LARGER EXTERNAL DOUBLER IAW BRAS EO. (K)May 16, 2005 · N452AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR CA050518003Monitor · burnedTHE AIRCRAFT WAS IN THE PROCESS OF RETURNING BACK TO THE AIRPORT DUE TO AN ADG DROP. TURNED AROUND TO FACE THE CUSTOMERS AND SAW SPARKS OUT OF THE CORNER OF MY EYE AND SMOKE BEGAN TO LIGHTLY COME OUT FROM THE AREA OF THE FLIGHT ATTENDANT PANEL/PHONE AND GO TOMay 15, 2005 · Cndair CL6002B19 · External Power SystemSDR ASOA05436Engine · failedFLT 4109 - DURING CRUISE FROM ATL-DCA, AT APPROXIMATELY 27,000 FEET, THE CREW NOTICED THE RIGHT ENGINE OIL TEMPERATURE TURNED RED AND INDICATED ABOVE ONE HUNDRED AND SEVENTY DEGREES CENTIGRADE. THE QRH WAS COMPLIED WITH AND THE CREW SHUT DOWN THE RIGHT ENGINEMay 14, 2005 · N876AS · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR ASOA05474Skin Panel · crackedDURING A C-CHECK, THE LOWER WING PLANK AT WS 148.019 LT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LOWER WING PLANK AT WS 148.019 LT SIDE IAW EO. (K)May 13, 2005 · N829AS · Cndair CL6002B19 · Wing, Plate/SkinSDR REX2005F00039Engine · failed(REF NR: 05-064) ON CLIMB OUT, AT ABOUT FL303, THERE WAS A LOUD BANG AND THE NR 2 ENGINE ITT SPIKED. THIS WAS FOLLOWED BY A LOSS OF N1 AND OIL PRESSURE. FLIGHT CREW FOLLOWED THE QRH PROCEDURES AND DECLARED AN EMERGENCY. THE PIC REQUESTED AND RECEIVED PERMMay 13, 2005 · N8390A · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR ASOA05473Rib · crackedDURING A C-CHECK, THE RT MAIN LANDING GEAR WHEEL WELL BATT RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RT MAIN LANDING GEAR WHEEL WELL BATT RIB ASSEMBLY AT WS 53.60 IAW EO. (K)May 11, 2005 · N829AS · Cndair CL6002B19 · Wing, Rib/BulkheadSDR ASOA05456Handle · crackedDURING A C-CHECK, THE AVIONICS BAY DOOR OUTER HANDLE CUP WAS FOUND CRACKED AROUND THE HANDLE BOSS. MAINTENANCE REMOVED AND REPLACED THE AVIONICS BAY DOOR HANDLE ASSEMBLY IAW AMM AND SRM. OPS CHECK GOOD. (K)May 10, 2005 · N867AS · Cndair CL6002B19 · Electrical/Electronic Compartment DoorsSDR ASOA05471Frame · crackedDURING A C-CHECK, THE PASSENGER DOOR AFT FRAME AT FS 338.90 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE PASSENGER DOOR AFT FRAME AT FS 338.90 IAW EO. (K)May 10, 2005 · N829AS · Cndair CL6002B19 · Fuselage Main, StructureSDR ASOA05472Angle · crackedDURING C-CHECK, THE RT OB FS 484 ANGLE AT BL 27 TO 36 IAW EO. (K)May 10, 2005 · N829AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR CA050509003Line · cracked(CAN) PILOT REPORTED (TAIL TANK AUTO INHIBIT LIGHT ON) BEFORE DEPARTURE. UPON INVESTIGATION, A CRACK ON THE TAIL TANK PRESSURE FUEL LINE WAS FOUND. IPC 28-13-22 ITEM 115.May 9, 2005 · Cndair CL604 · Aircraft Fuel Distribution SystemSDR A6WA200540183Skin · dented2 DENTS RT SIDE AF FS409 + 32 BETWEEN STR 21R AND 22R. 3.5 INCHES LONG X 1.65 INCHES WIDE X 0.39 INCHES DEEP. 2.5 INCHES LONG X 1.5 INCHES WIDE X .022 INCHES DEEP. REPAIRED DAMAGE AT FS 409 +32 BETWEEN STR 21R AND 22R IAW SRM. (K)May 9, 2005 · N454AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR REX2005F00040Control System · failed(REF NR: 05-063) FLAP FAILED AT 20 ON APPROACH. RESET SYSTEM AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K)May 9, 2005 · N8888D · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REX2005F00041Downlock Target · dirty(REF NR: 05-062) ON APPROACH, AFTER SELECTING GEAR DOWN, RECEIVED (GEAR DISAGREE) NOSE NOT GREEN. FOLLOWED QRH. CHECKED AND CLEANED DOWN LOCK TARGETS. PERFORMED GEAR SWING IAW AMM, NO DEFECTS NOTED. (K)May 9, 2005 · N8847A · Cndair CL6002B19 · Landing Gear Position and WarningSDR REX2005F00042Fcu · failed(REF NR: 05-061) FLAPS FAIL AT ZERO ON CLIMB-OUT. QRH FOLLOWED, EMERGENCY DECLARED RETURNED TO DEPARTURE WITH UNEVENTFUL LANDING. REMOVED AND REPLACED FLAP ELECTRONIC CONTROL UNIT. (FECU) (K)May 6, 2005 · N826AY · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA050518001Windshield · crackedLEFT WINDSHIELD CRACKED DURING CLIMB AT FL180. DIVERTED FLIGHT BACK TO DEPARTURE AIRPORT. LEFT WINDSHIELD REPLACED AND TESTED ACCORDING TO AMM PROCEDURE.May 5, 2005 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA050512002Tube · chafedCREW REPORTED A HYDRAULIC PROBLEM, 'HYD 1 LO PRESS' LOSS OF QUANITY - '0'. FLIGHT CONTINUED AND LANDED ON RUNWAY WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE NR 1 SYSTEM SUCTION TUBE ASSEMBLY CHAFFED AT A POINT 18 FT FROM THE FORWARD END. P/ N 601R75286-3May 5, 2005 · Cndair CL6002B19 · Hydraulic System, MainSDR REX2005F00043Bpsu · failed(REF NR: 05-060) FLAP FAIL MESSAGE UPON POWER UP. REMOVED AND REPLACED RT BRAKE POSITION SENSING UNIT (BPSU). (K)May 5, 2005 · N826AY · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR ASOA05396Light · shortedDURING A GROUND INSPECTION, THE FORWARD SECTION OF EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AN EMERGENCY FLOOR LIGHT STRIP IN THE FORWARD SECTION. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)May 3, 2005 · N843AS · Cndair CL6002B19 · Emergency LightingSDR ASOA05397Step · crackedDURING A-CHECK, THE PASSENGER DOOR BOTTOM STEP WAS FOUND CRACKED AT THE HANDRAIL HINGE. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP IAW MM. OPERATIONAL CHECKS GOOD. (K)May 3, 2005 · N845AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA05398Mechanism · contaminatedDURING A GROUND INSPECTION, THE PASSENGER DOOR WOULD NOT CLOSE AND A PASSENGER DOOR LATCH CAUTION MESSAGE WAS RECEIVED. MAINTENANCE REMOVED SAND AND GRIT FROM ALL THE ROLLING COMPONENTS ON THE PASSENGER DOOR AND CHECKED THE ADJUSTMENT ON THE LINKAGES. MAINTEMay 3, 2005 · N860AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA050518002Window · crackedINBOUND THE CAPTAINS SIDE WINDOW CRACKED. REPLACED WINDOW.May 2, 2005 · Cndair CL6002B19 · Flight Compartment WindowsSDR REX2005F00044Proximity Switch · out of adjust(REF NR: 05-059) RECEIVED (GEAR DISAGREE) MESSAGE ON APPROACH. QRH FOLLOWED GEAR MANUALLY EXTENDED. EMERGENCY DECLARED UNEVENTFUL LANDING. ADJUSTED NOSE GEAR PROXIMITY SWITCH IAW AMM. GEAR SWINGS PERFORMED. (K)May 2, 2005 · N8587E · Cndair CL6002B19 · Landing Gear Position and WarningSDR ASOA05388Anchor Fitting · crackedDURING HANGAR MAINTENANCE, THE FORWARD ANCHOR FITTING ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVE AND REPLACED THE FORWARD ANCHOR FITTING ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)May 1, 2005 · N882AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR VNAA0504008Tire · separatedDURING POSTFLIGHT INSPECTION AFTER LANDING AT PHL, THE CREW OF FLIGHT 2437 (PWM TO PHL) REPORTED THAT TREAD WAS MISSING FROM THE RT INBOARD MLG TIRE AND THE RT INBOARD FLAP WAS DENTED. PSA MAINTENANCE REMOVED AND REPLACED THE RT INBOARD MLG WHEEL & TIRE ASSEMApr 30, 2005 · N241PS · Cndair CL6002B19 · TireSDR REXA2005056Proximity Sensor · out of adjustGEAR DISAGREE LIGHT ON SHORT FINAL. UNEVENTFUL LANDING. ADJUSTED NLG OLEO PROX SENSOR IAW AMM. PERFORMED GEAR SWING, OPS CHECKED GOOD IAW AMM. OK FOR SERVICE. (K)Apr 28, 2005 · N8698A · Cndair CL6002B19 · Landing Gear Position and WarningSDR REXA2005057Smoke Detector · false activationSMOKE TOILET MESSAGE AFTER TAKEOFF. REMOVED AND REPLACED LAV SMOKE DETECTOR IAW AMM. OPS CHECK NORMAL. NO SMOKE EVER FOUND. AC READY FOR SERVICE. (K)Apr 28, 2005 · N8444F · Cndair CL6002B19 · Smoke DetectionSDR REXA2005058Smoke Detector · malfunctionedSMOKE TOILET MESSAGE ON FINAL. LANDING UNEVENTFUL. PERFORMED OPERATIONAL TEST OF LAV SMOKE SYSTEM, IAW AMM AND OF THE LAV SMOKE DETECTOR IAW AMM. BOTH OPS CHECK GOOD. (K)Apr 28, 2005 · N8775A · Cndair CL6002B19 · Smoke Detection
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