GE CF34-3B1

Service difficulty reports · 5,402

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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 CA051207006Windshield · crackedDURING APPROACH, LT COCKPIT SIDE WINDSHIELD SHATTERED. NO LOSS OF PRESSURIZATION. MAINTENANCE REPLACED LT SIDE WINDSHIELD, AIRCRAFT RETURNED TO SERVICE.Dec 4, 2005 · Cndair CL6002B19 · Flight Compartment WindowsSDR VNAA0512006Structure · bird strikeTHE CREW REPORTED A BIRD STRIKE DURING LANDING APPROACH. MAINTENANCE COMPLIED WITH A BIRD STRIKE INSPECTION AND FOUND A DENT ON THE RT FUSELAGE NOSE SECTION BELOW THE ADG DOOR, THE ADG DOOR WAS CRACKED, AND THE LT WING LEADING EDGE PANEL 530BL WAS DENTED. ALDec 3, 2005 · N247JS · Cndair CL6002B19 · Fuselage Structure (General)SDR ASOA051049Lens · crackedDURING C-CHECK, THE EMERGENCY EXIT LENS, FORWARD OF THE SERVICE DOOR, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE EMERGENCY EXIT LENS, FORWARD OF THE SERVICE DOOR. (K)Dec 3, 2005 · N882AS · Cndair CL6002B19 · Emergency LightingSDR ASOA051047Lamp · burned outDURING A GROUND INSPECTION, THE DEILING EMERGENCY LIGHT, AT ROW 9, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE CEILING EMERGENCY LIGHT, AT ROW 9. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Dec 2, 2005 · N823AS · Cndair CL6002B19 · Emergency LightingSDR ASOA051046Step · separatedDURING A HANGAR INSPECTION, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO BE SEPARATED AT THE ATTACHED STAY ROD BRACKET. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Dec 2, 2005 · N879AS · Cndair CL6002B19 · Entrance StairsSDR ASOA051045Angle · crackedDURING A HANGAR INSPECTION, THE PASSENGER DOOR STEP DRAG ANGLE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE PASSENGER DOOR STEP DRAG ANGLE IAW REO. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Dec 2, 2005 · N672BR · Cndair CL6002B19 · Entrance StairsSDR VNAA0512002Sensor · failedTHE DISPLAY COOL CAUTION MESSAGE ILLUMINATED DURING CRUISE. THE CREW FOLLOWED THE QRH AND DIVERTED TO CAK. MAINTENANCE REMOVED AND REPLACED THE DISPLAY COOLING SYSTEM LOW FLOW SENSOR. THE SYSTEM OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS THEN RELEASED FODec 1, 2005 · N258PS · Cndair CL6002B19 · Cabin Cooling SystemSDR VNAA0512003Radome · ground damageWHILE PARKED FOR THE NIGHT THE RADOME WAS STRUCK AND DAMAGED BY A LAV SERVICING TRUCK. AFTER INSPECTING THE AIRCRAFT MAINTENANCE REMOVED AND INSTALLED A SERVICEABLE RADOME. NO OTHER DAMAGE WAS FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE.Dec 1, 2005 · N209PS · Cndair CL6002B19 · Fuselage Structure (General)SDR VNAA0512004Door · openTHE GROUND AIR CONNECTION DOOR WAS FOUND OPEN AFTER THE FLIGHT. MAINTENANCE INSPECTED AND FOUND THE DOOR HINGE CRACKED. THE DOOR WAS REMOVED AND REPLACED WITH A SERVICEABLE UNIT. THE AIRCRAFT WAS RELEASED FOR SERVICE.Dec 1, 2005 · N256PS · Cndair CL6002B19 · Air Conditioning DoorsSDR ASOA051043Lamp · burned outDURING A HANGAR INSPECTION, THE RT CENTER EMERGENCY LIGHT ASSY WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN RT CENTER EMERGENCY LIGHT ASSY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Dec 1, 2005 · N978EV · Cndair CL6002B19 · Emergency LightingSDR ASOA051042Lamp · burned outDURING A GROUND INSPECTION, THE EMERGENCY LIGHT ASSY, NEAR THE PASSENGER DOOR, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMPS IN THE EMERGENCY LIGHT ASSY, NEAR THE PASSENGER DOOR. (K)Dec 1, 2005 · N860AS · Cndair CL6002B19 · Emergency LightingSDR ASOA051041Lamp · burned outDURING A GROUND INSPECTION, THE EMERGENCY EXIT LIGHT, AT THE PASSENGER DOOR, WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT, AT THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Dec 1, 2005 · N879AS · Cndair CL6002B19 · Emergency LightingSDR VNAA0511024Seal · tornA LEAK WAS REPORTED AT THE PASSENGER DOOR AND THE AIRCRAFT WOULD NOT MAINTAIN PRESSURIZATION WHEN POWER WAS REDUCED. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR SEAL. CABIN PRESSURIZATION OPERATIONALLY CHECKED GOONov 30, 2005 · N216PS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA051040Connector · disconnectedDURING A GROUND INSPECTION, THE CENTER AISLE EMERGENCY LIGHT STRIP WAS FOUND TO BE DISCONNECTED AT THE AFT POSITION. MAINTENANCE RECONNECTED THE CENTER AISLE EMERGENCY LIGHT STRIP AT THE AFT POSITION. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Nov 30, 2005 · N981EV · Cndair CL6002B19 · Emergency LightingSDR REXA200500141Compressor · failedPASSING THROUGH 2500 FT MSL ON CLIMBOUT FROM, THE FLIGHT CREW HEARD SEVERAL LOUD (BANGS) FROM THE RT ENGINE. THIS WAS FOLLOWED BY ERRATIC ENGINE INDICATIONS AND A REPORT FROM THE FLIGHT ATTENDANT OF A (BURNING SMELL) IN THE CABIN. THE FLIGHT CREW PERFORMED THENov 29, 2005 · N8588D · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR ASOA051039Anchor Fitting · crackedDURING A HANGAR INSPECTION, THE PASSENGER DOOR AFT ANCHOR FITTING WAS TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE PASSENGER DOOR AFT ANCHOR FITTING. (K)Nov 29, 2005 · N850AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA051037Door · bindingDURING A GROUND INSPECTION, THE PASSENGER DOOR WAS BINDING. MAINTENANCE OPERATED THE PASSENGER DOOR WITH NO DEFECTS NOTED. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Nov 29, 2005 · N975EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA051036Handle · lack of lubeDURING A GROUND INSPECTION, THE PASSENGER DOOR WAS DIFFICULT TO OPEN. MAINTENANCE LUBRICATED THE PASSENGER DOOR HANDLE ROLLER CAM. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Nov 29, 2005 · N826AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA051035Lamp · burned outDURING A HANGAR INSPECTION, THE AFT CABIN CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE AFT CABIN CEILING EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Nov 29, 2005 · N908EV · Cndair CL6002B19 · Emergency LightingSDR CA051130007Landing Gear · malfunctionedAFTER TAKEOFF DURING GEAR RETRACTION, RECEIVED THE FOLLOWING WARNING MESSAGES: NOSE DOOR OPEN, GEAR DISAGREE. AIRCRAFT HAD DEPARTED FROM CONTAMINATED RUNWAY. AIRCRAFT CONTINUED TO DESTINATION AND USED ALTERNATE EXTENSION TO LOWER GEAR. AIRCRAFT LANDED NORMANov 29, 2005 · Cndair CL6002B19 · Nose/Tail Landing GearSDR A6WA200540335Control Cable · frayedSPOILERON FAULT, AILERON FEELS ROUGH WHEN TURNED TO THE RIGHT. AC HAS FRAYED AILERON CABLES DUE TO INCORRECT INSTALLATION, REPLACED CABLES.Nov 28, 2005 · N425AW · Cndair CL6002B19 · Aileron Control SystemSDR A6WA200540333Pivot Assy · seizedHORIZONTAL STABILIZER RT OUTER PIVOT PIN FOUND TO BE SEIZED IN OUTER BUSHING CAUSING BUSHING TO ROTATE IN LUG. MAINTENANCE REMOVED AND REPLACED HORIZONTAL STABILIZER RT OUTER BUSHING AND REAMED THE LUG TO 2ND OVERSIZE IAW SB. (K)Nov 27, 2005 · N427ZW · Cndair CL6002B19 · Horizontal Stabilizer StructureSDR VNAA0511023Skin · ground damageTHE RIGHT WINGLET SUSTAINED LEADING EDGE DAMAGE AFTER HITTING A BAGGAGE CART WHILE AIRCRAFT WAS BEING MARSHALLED INTO THE GATE. MAINTENANCE REMOVED & REPLACED THE RIGHT WINGLET LEADING EDGE ASSEMBLY. NO FURTHER DAMAGE WAS FOUND. THE AIRCRAFT WAS RELEASED FNov 26, 2005 · N244PS · Cndair CL6002B19 · Wing, Plate/SkinSDR CA051128001Turnbuckle · fractured(CAN) TO DATE, (3) CF34-3B1 STAGE 2 HPC TURNBUCKLES AFFECTING 2 ENG HAVE FAILED DURING SERVICE. SEPARATION OF VG SHAFT SIDE TURNBUCKLE ROD END. SEPARATION POINT ON ROD END OCCURRED IN THREADED PORTION WHERE IT MEETS JAM NUT ON TURNBUCKLE ASSY. CAUSE CONFIRMEDNov 25, 2005 · Turbine Engine Compressor SectionSDR COMA0560643Pump · malfunctionedFLIGHT 5779 - RT ENGINE LOW OIL PRESSURE WARNING. REPLACED THE ENGINE OIL PUMP.Nov 25, 2005 · N510CA · Cndair CL6002B19 · Turbine Engine Oil SystemSDR VNAA0511022Flap System · malfunctionedTHE FLAPS FAIL CAUTION MESSAGE ILLUMINATED WITH FLAPS AT 8 DEGREES. THE CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET AND OPERATIONALLY CHECKED THE FLAP SYSTEM. ALL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.Nov 24, 2005 · N202PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR COMA0560635Transducer · faultyENROUTE, THE RT ENGINE OIL PRESSURE INDICATION WAS ERRATIC RANGING FROM 8 TO 30 PSI. CREW DECLARED AN EMERGENCY, REDUCED POWER ON THE RT ENGINE TO IDLE AND LANDED WITHOUT INCIDENT. REPLACED THE RT ENGINE OIL PRESSURE TRANSDUCER.Nov 22, 2005 · N479CA · Cndair CL6002B19 · Engine Oil PressureSDR A6WA200540334Skin · corrodedLT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT FOR PANEL 540CB HAS MINOR CORROSION ON OB 5 INCH LONG X .1250 INCH WIDE AND .002 INCH DEEP AND IB 4 INCH LONG X .1250 INCH WIDE AND .002 INCH DEEP. MAINTENANCE PERFORMED A MAJOR REPAIRED TO LT WING LOWER PLANK Nov 22, 2005 · N427ZW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200540330Rheostat · faultyWHEN F/O SELECTED FLOOD LIGHTS ON, SMOKE ERUPTED FROM BEHIND SW PANEL FLOOD LABEL DSTLA ON FO`S SIDE PANEL AND CBP3 C1 POPPED AND WAS NOT RESET. INSPECTED AND FOUND FO`S FLOOD LIGHT RHEOSTAT FAULTED. NO OTHER SYS AFFECTED. (K)Nov 22, 2005 · N405AW · Cndair CL6002B19 · Flight Compartment LightingSDR VNAA0511021Warning Light · illuminatedDURING CRUISE THE PASSENGER DOOR WARNING MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH AND MADE AN UNEVENTFUL LANDING AT DESTINATION. MAINTENANCE INSPECTED THE PASSENGER DOOR LATCHING AND WARNING SYSTEMS. NO DISCREPANCIES WERE FOUND AND THE PROBLEM COULD NNov 22, 2005 · N251PS · Cndair CL6002B19 · Door Warning SystemSDR VNAA0511019Skin · unknownDURING AN FAA RAMP CHECK, THE INSPECTOR REPORTED EVIDENCE OF LIGHTNING DAMAGE ON THE LT WINGTIP. MAINTENANCE COMPLIED WITH EN ROUTE AND DETAILED LIGHTNING STRIKE INSPECTIONS. NO DAMAGE OR EVIDENCE OF A LIGHTNING STRIKE WAS FOUND. THE AIRCRAFT WAS RELEASED FNov 22, 2005 · N202PS · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200540332Intercostal · crackedLT SIDE FS621 TO 625.30 INTERCOSTAL AT STR 14L IS CRACKED NEAR RADIUS APPROX 1.1 INCH LONG. MAINTENANCE REPLACED INTERCOSTAL IAW SRM. (K)Nov 21, 2005 · N427ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540331Intercostal · crackedRT SIDE FS 621.00 TO FS 625.30 INTERCOSTAL AT STR 14R IS CRACKED NEAR RADIUS APPROX 1.0 INCH LONG. MAINTENANCE REPLACED INTERCOSTAL IAW SRM. (K)Nov 21, 2005 · N427ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540340Rib · crackedAWAC WO 89248, MWC 143. LT BATT RIB ASSY AT WS 53.60 UPPER AFT RADIUS IS CRACKED 2 INCH LONG. INSTALLED REPAIR DOUBLER AND FILLER IAW REO. (K)Nov 21, 2005 · N427ZW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR VNAA0511018Fcu · failedTHE FLAPS FAIL CAUTION MESSAGE ILLUMINATED WHEN FLAPS 45 DEGREE WAS SELECTED. THE CREW FOLLOWED THE QRH, CONTINUED THE APPROACH, AND LANDED. MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT. THE FLAPS OPERATIONALLY CHECKED GOOD. THE AIRCRANov 19, 2005 · N248PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200540329Control Unit · malfunctionedSTAB TRIM AND MACH TRIM MESSAGE APPEARED DURING CLIMB. COMPLIED WITH QRH, MESSAGE PERSISTED. REMOVED AND REPLACED HSTCU PN 7060-9, IAW AMM. OPS CHECK GOOD.Nov 18, 2005 · N420AW · Cndair CL6002B19 · Stabilizer Control SystemSDR COMA0560634Control Lever · faultyFLIGHT 5114- FLAPS FAIL CAUTION. REPLACED THE FLAP CONTROL LEVER.Nov 17, 2005 · N910EV · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA0511017Skin · scratchedAFTER LANDING THE CREW REPORTED A SCRATCH ON THE FUSELAGE BELOW THE CARGO DOOR. MAINTENANCE INSPECTED AND FOUND THE DAMAGE TO BE BEYOND ALLOWABLE LIMITS. THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE PERFORMED A TEMPORARY REPAIR IAW BOMBARDIER REO 601R-5Nov 17, 2005 · N237PS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR VNAA0511016Controller · malfunctionedTHE ANTI-ICE DUCT WARNING MESSAGE ILLUMINATED WHEN WING ANTI-ICE WAS SELECTED ON. THE LEFT WING INDICATED OVERHEAT ON THE ANTI-ICE SYNOPTIC PAGE. THE CREW FOLLOWED THE QRH AND MADE AN UNEVENTFUL LANDING AT THEIR DESTINATION. MAINTENANCE REMOVED, INSPECTED, Nov 16, 2005 · N216PS · Cndair CL6002B19 · Ice/Rain Protection SystemSDR A6WA200540327Aileron · unknownREQUEST INSPECTION OF RT AND LT AILERONS. THAWED ICE FROM AILERON, INSPECTED SURFACE MOVEMENT AND SURFACES. NO DEFECTS NOTED. (K)Nov 15, 2005 · N431AW · Cndair CL6002B19 · Aileron Control SystemSDR CA051117001Windshield · cracked(CAN) AT 33000 FT DURING DESCENT, THE COPILOT'S WINDSHIELD SHATTERED. THE LANDING WAS UNEVENTFUL. MAINTENANCE WAS DISPATCHED TO REPLACE THE WINDSHIELD AND THE AIRCRAFT RETURNED TO SERVICE.Nov 15, 2005 · Cndair CL6002B19 · Flight Compartment WindowsSDR VNAA0511014Target · looseAFTER TAKEOFF WITH THE GEAR HANDLE SELECTED UP THE GEAR DISAGREE WARNING MESSAGE ILLUMINATED. THE RIGHT MAIN LANDING GEAR DID NOT SHOW LOCKED IN THE UP POSITION. THE CREW FOLLOWED THE QRH, RETURNED TO TYS, AND MADE AN UNEVENTFUL LANDING. THE AIRCRAFT WAS FNov 15, 2005 · N260JS · Cndair CL6002B19 · Landing Gear Position and WarningSDR VNAA0511015Thermal Switch · malfunctionedTHE ANTI-ICE DUCT WARNING MESSAGE ILLUMINATED WITH THE ANTI-ICE SYNOPTIC PAGE INDICATING A LEFT WING FAULT. THE CREW FOLLOWED THE QRH AND MADE AN UNEVENTFUL LANDING. THE AIRCRAFT WAS FERRIED TO DAY. MAINTENANCE TROUBLESHOT THE SYSTEM AND FOUND NO DISCREPANCNov 15, 2005 · N216PS · Cndair CL6002B19 · Fire Protection SystemSDR A6WA200540324Idg · faultyON TAKEOFF ROLL IDG NR 1 FAULT FOLLOWED GEN NR 1 FAULT ABORTED 40 KNOTS BTMS INDICATION 2,2,22 LIGHT BREAKING. SERVICED IDG NR 1 IAW AMM. COMPLIED WITH ENGINE RUN. OPS CHECK GOOD. NOT LEAKS NOTED IAW AMM. NO HIGH ENERGY STOP INSPECTION REQUIRED. (K)Nov 15, 2005 · N417AW · Cndair CL6002B19 · Alternator-Generator DriveSDR VNAA0511011Control Unit · unserviceableAFTER TAKEOFF THE L 14TH DUCT WARNING MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH, RETURNED TO PIT, AND MADE AN UNEVENTFUL OVERWEIGHT LANDING. MAINTENANCE TROUBLESHOT THE SYSTEM AND FOUND NO DISCREPANCIES. THE LT BLEED AIR LEAK CONTROL UNIT WAS REMOVED ANov 14, 2005 · N258PS · Cndair CL6002B19 · Engine Bleed Air SystemSDR VNAA0511012Fire Loop · out of positionTHE RT 14TH DUCT WARNING MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH, DIVERTED TO ILH, AND MADE AN UNEVENTFUL LANDING. THE AIRCRAFT WAS FERRIED TO CLT WHERE MAINTENANCE TROUBLESHOT THE SYSTEM IAW CRJ200 FIM 36-20-00. THE RT PYLON LOOPS WERE INSPECTED ANDNov 14, 2005 · N257PS · Cndair CL6002B19 · Smoke DetectionSDR VNAA0511013Control Unit · failedTHE STAB TRIM FAILED IN FLIGHT. THE CREW FOLLOWED THE QRH AND MADE AN UNEVENTFUL LANDING. MAINTENANCE REMOVED & REPLACED THE HORIZONTAL STAB TRIM CONTROL UNIT IAW CRJ200 AMM 24-41-01-000(400)-801. THE STAB TRIM OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WASNov 14, 2005 · N228PS · Cndair CL6002B19 · Stabilizer Position IndicatingSDR A6WA200540348Handle · corrodedMWC 258 CREW ESCAPE HATCH OUTER HANDLE SHAFT HAS PITTING, CORROSION. REMOVED OUTER HANDLE ASSY AND INSTALLED NEW HANDLE ASSY, PN H341937, IAW AMM. (K)Nov 14, 2005 · N426AW · Cndair CL6002B19 · Emergency ExitsSDR A6WA200540325Support Angle · crackedLT FS621 FLOOR SUPPORT ANGLE IS CRACKED MAINTENANCE PERFORMED REPAIR TO LT FS 621.00 FLOOR SUPPORT ANGLE IAW REO. (K)Nov 13, 2005 · N426AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540326Floor Support · crackedRT FS 621.00 FLOOR SUPPORT ANGLE IS CRACKED. MAINTENANCE PERFORMED REPAIR TO RT FS 621.00 FLOOR SUPPORT ANGLE IAW REO. (K)Nov 13, 2005 · N426AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
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