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 ASOA05316Lamp · burned outDURING A GROUND INSPECTION, THE 2ND OVERHEAD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINT REMOVED AND REPLACED THE LAMP IN THE 2ND OVERHEAD EMERGENCY LIGHT. OPS CHECK GOOD. AC OK FOR SERVICE. (K)Apr 7, 2005 · N909EV · Cndair CL6002B19 · Emergency LightingSDR ASOA05315Rib · crackedDURING A C-CHECK, THE LT BATT RIB ASSY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LT BATT RIB ASSY AT WS 53.60 IAW EO. (K)Apr 6, 2005 · N820AS · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA200540139Engine · malfunctionedLOW OIL ENGINE PRESSURE WARNING. INDICATED LOW ON GAGE LOW PRESSURE. COMPLIED WITH QRH. ENGINE SHUTDOWN INFLIGHT. (M)Apr 5, 2005 · N431AW · Cndair CL6002B19 · Turbine Engine Oil SystemSDR ASOA05318Latch · misalignedDURING A C-CHECK, THE LT OVERWING EMERGENCY EXIT FAILED THE PULL TEST. MAINT ADJUSTED THE LATCH FITTNGS ON THE LT OVERWING EMERGENCY EXIT. OPS CHECK GOOD. (K)Apr 5, 2005 · N862AS · Cndair CL6002B19 · Emergency ExitsSDR A6WA200540128Clip · crackedFLOOR SUPPORT BEAM CLIP AS FS280, LBL 9.0, OB IS CRACKED IN RADIUS APPROX 0.30. REMOVED AND REPLACED ANGLE P/N 601R31113-57 IAW CRJ 200 SRM 51-42-06, 51-42-21 AND BRAS EO 601R-53-6212. (M)Apr 4, 2005 · N416AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200540130Clip · crackedFLOOR SUPPORT BEAM CLIP AT FS 280, LBL 9, IB IS CRACKED IN RADIUS APPROX (0.33 INCH). (K)Apr 4, 2005 · N416AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200540131Clip · crackedFLOOR SUPPORT BEAM CLIP AT FS 280, RBL 9 IB IS CRACKED IN RADIUS APPROX ( 0.50 INCH). (K)Apr 4, 2005 · N416AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200540132Clip · crackedFLOOR SUPPORT BEAM CLIP AT FS 280, RBL 9 OB IS CRACKED IN RADIUS APPROX 0.52 INCH. (K)Apr 4, 2005 · N416AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA200540133Clip · crackedFLOOR SUPPORT BEAM CLIP AT FS484, LBL 36, IS CRACKED FROM TOP RIVET HOLE TO EDGE APPROX. (0.30 INCH). (K)Apr 4, 2005 · N416AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA05306Fitting · crackedDURING A (C) CHECK, THE FITTING IN THE RT SIDE PRESSURE FLOOR UNDER 262CRF AT APPROX FS 454.00 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE FITTING IN THE RT SIDE PRESSURE FLOOR UNDER 262CRF AT APPROXIMATELY FS 454.00. (K)Apr 3, 2005 · N820AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA05305Step · brokenDURING A GROUND INSPECTON, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPS CHECK GOOD. AC OK FOR SERVICE. (K)Apr 3, 2005 · N836AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA05304Relay · defectiveDURING A GROUND INSPECTION, THE EMERGENCY LIGHTING REMAINED ILLUMINATED WHEN IN THE ARM POSITION. MAINTENANCE FOUND RELAY K1XD DEVECTIVE, REMOVED AND REPLACED IT IAW AMM. OPS CHECK GOOD. AC OK FOR SERVICE. (K)Apr 3, 2005 · N906EV · Cndair CL6002B19 · Light System WiringSDR ASOA05297Clip · crackedDURING A C-CHECK, THE ATTACH CLIP AT FS 625 LT ABOVE THE BOX BEAM WAS FOUND TO BE CRACKED BEYOUND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE ATTACH CLIP AT FS 625 LT. (K)Apr 3, 2005 · N820AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA05296Frame · crackedDURING A C-CHECK, THE FRAME FS 640 BETWEEN STRINGER 9 AND 12 LT WAS FOUND TO BE CRACKED BEYOND LIMITS IN THE RADIUS FORWARD SIDE ABOVE THE BOX BEAM. MAINTENANCE IS REPAIRING THE FRAME FS 640 BETWEEN STRINGER 9 AND 12 LT IAW EO. (K)Apr 3, 2005 · N820AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA05295Support Beam · crackedDURING C-CHECK, THE ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL0 WAS FOUND TO BE CRACKED BEYOND LIMIST. MAINTENANCE IS REPAIRING THE ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL0 IAW EO. (K)Apr 3, 2005 · N862AS · Cndair CL6002B19 · Fuselage Main, StructureSDR VNAA0504001Display · failedDURING FLIGHT 2491 (CLT TO PIT) THE CAPTAIN'S DISPLAY CONTROL PANEL FAILED. THE CREW FOLLOWED THE QRH, TRANSFERRED CONTROLS, AND MADE AN UNEVENTFUL LANDING AT DESTINATION. MAINTENANCE FOUND CIRCUIT BREAKER C9 ON PANEL 4 OPEN. THE CIRCUIT BREAKER WAS CLOSED Apr 2, 2005 · N223JS · Cndair CL6002B19 · Instrument PanelSDR A6WA200540134Tire · damagedREQUEST INSPECTION LT MLG TIRE FOR WEAR. AC PASSENGERS AND CARGO WERE UNLOADED, AIRCRAFT DEFUELED. AIRCRAFT WAS TOWED ONT RAMP AREA. WITHOUT INJURY OR DAMAGE TO AIRCRAFT, GEAR SWING AND MLG BAY ACCOMPLISHED AND REMOVAL/REPLACEMENT LT MLG TIRES AS A PRECAUTIApr 2, 2005 · N437AW · Cndair CL6002B19 · TireSDR ASOA05317Light · crackedDURING A C-CHECK, THE EMERGENCY EXIT LIGHT BY THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE AND CRACKED. MAINT REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT BY THE SERVICE DOOR. OPS CHECK GOOD. (K)Apr 2, 2005 · N862AS · Cndair CL6002B19 · Emergency LightingSDR ASOA05294Light · crackedDURING A C-CHECK, THE EMERGENCY EXIT LIGHT BY THE SERVICE DOOR WAS FOUND TO BE CRACKED AND INOPERATIVE. MAINTENANCE IS REMOVING AND REPLACING THE EMERGENCY EXIT LIGHT ASSY BY THE SERVICE DOOR. (K)Apr 2, 2005 · N862AS · Cndair CL6002B19 · Emergency LightingSDR COMA0560229Carbon Seal · leakingFLIGHT 5640 DURING CLIMB OUT OF STL, THE LT ENGINE OIL PRESSURE INDICATED 25-35 PSI, CREW DECLARED AN EMERGENCY, SHUT DOWN THE ENGINE AND DIVERTED TO CVG. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED CARBON SEALS AT AXIS, F, D AND BB.Apr 1, 2005 · N473CA · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA050405001Carbon Seal · leaking(CAN) BOMBARDIER AEROSPACE REGIONAL AIRCRAFT HAS RECEIVED A REPORT WHICH WE FEEL IS A REPORTABLE EVENT. CLIMBING THROUGH FL310, LEFT ENGINE OIL PRESSURE WARNING MESSAGE WITH PRESSURE AT 25-35 PSI., EVENTUALLY STABILIZED AT 25 PSI. PRECAUTIONARY ENGINE SHUTDOApr 1, 2005 · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA050418001Handle · cracked(CAN) WHEN CREW ARRIVED AT AIRCRAFT, THEY WERE NOT ABLE TO OPEN THE MAIN CABIN DOOR. TROUBLESHOOTING BY MAINTENANCE DISCOVERED THE HANDLE CRACKED IN TWO LOCATIONS ON THE SHAFT. THE ONE CRACK WAS ALMOST COMPLETELY AROUND THE CIRCUMFERANCE OF THE SHAFT. IPC REFMar 31, 2005 · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA05271Uplock · misalignedDURING APPROACH, CREW RECEIVED A GEAR DISAGREE WARNING MESSAGE ON THE NOSE GEAR. THE QRH WAS COMPLIED WITH AND EMERGENCY WAS DECLARED. AC PERFORMED A FLYBY BUT TOWER WAS UNABLE TO COMFIRM IF NOSE GEAR WAS IN THE DOWN POSITION. UPON FURTHER COMPLETION OF THEMar 30, 2005 · N850AS · Cndair CL6002B19 · Nose/Tail Landing GearSDR COMA0560220Computer · malfunctionedFLIGHT 5250 FUEL CHANNEL 1 AND 2 FAIL. NO FUEL INDICATION. REPLACED THE FUEL COMPUTER.Mar 29, 2005 · N443CA · Cndair CL6002B19 · Fuel Controlling SystemSDR VNAA0503013Stall Warning · malfunctionedON CLIMBOUT (PHL TO YOW) THE STALL FAIL CAUTION MESSAGE ILLUMINATED. THE CREW OF FLIGHT 2566 RETURNED TO PHL AND LANDED WITHOUT INCIDENT. PSA MAINTENANCE RESET POWER AND OPERATIONALLY TESTED THE STALL PROTECTION SYSTEM IAW CRJ 200 AMM 27-35-01-750-802. THEMar 27, 2005 · N209PS · Cndair CL6002B19 · Stall Warning SystemSDR A6WA200540127Line · chafedHYDRAULIC NR 1 LOW PRESSURE MESSAGE INFLIGHT ON CLIMBOUT. QUANTITY INDICATES ZERO. REMOVED AND REPLACED HYDRAULIC SUPPLY LINE TO CASE DRAIN ASSY REF 29-11-02, RAN ENGINE LEAK CHECK. OPS CHECK GOOD. (K)Mar 27, 2005 · N414ZW · Cndair CL6002B19 · Hydraulic System, MainSDR ASOA05303Warning Light · illuminatedDURING APPROACH, UPON SELECTING THE GEAR DOWN AND FLAPS TO 30 DEGREES, THE CREW RECEIVED A GREEN GEAR DOWN INDICATION FOR THE MLG FOLLOWED BY A NOSE GEAR DISAGREE WARNING MESSAGE ON EICAS. AT APPROX 1,000 FT, THE CREW INITIATED A GO AROUND AND DECLARED AN EMEMar 27, 2005 · N856AS · Cndair CL6002B19 · Landing Gear Position and WarningSDR A6WA200540126Warning Light · illuminatedAT 32,000 FT, A FUEL IMBALANCE CAS MESSAGE APPEARED ON EICAS. THE PROBLEM WAS NOT CORRECTABLE USING AUTO, MANUAL OR GRAVITY CROSSFLOW. LT WING HEAVY AT LANDING AN IMBALANCE 1700 LBS C/W QRH. SHUTDOWN ENG NR 2, LANDING WEIGHT WAS NOT EXCEEDED. PERFORMED SYSMar 25, 2005 · N438AW · Cndair CL6002B19 · Fuel Indicating SystemSDR A6WA200540124Skin · scratched2 SCRATCHES IN FUSELAGE AT CARGO DOOR CUT-OUT, (APPROX 1 INCH LONG AND .5 INCH LONG.) PERFORMED A MAJOR REPAIR AT FS 549, STR 14-16 IAW EO. (K)Mar 25, 2005 · N415AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR COMA0560202Warning Light · illuminatedFLIGHT 5084, RECEIVED A LT T/R UNLOCK CAUTION MESSAGE DURING CRUISE FLIGHT, CREW DECLARED AN EMERGENCY AND DIVERTED. AIRCRAFT LANDED WITHOUT INCIDENT. DEFERRED THRUST REVERSER IAW MEL 78-30-01.Mar 23, 2005 · N494CA · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA200540AConnector · contaminatedOVERBOARD COOL CAUTION AND IB COOL STATUS MESSAGE. INSPECTED DOOR AND FOUND CONNECTOR INSIDE DOOR WET. CLEANED AND DRIED CONNECTOR PLUG. OPS CHECK GOOD. (K)Mar 23, 2005 · N404AW · Cndair CL6002B19 · Cabin Cooling SystemSDR ASOA05263Battery · dischargedDURING A GROUND INSPECTION IN ATL, THE EMERGENCY LIGHTS CAME ON WITH THE SWITCH IN THE OFF AND ARMED POSITIONS. MAINTENANCE FOUND CIRCUIT BREAKER P4-C2 POPPED AND THE EMERGENCY LIGHTS BATTERY PACKS LOW RESULTING FROM BOTH MAIN AND AUXILIARY POWER UNIT BATTERIMar 23, 2005 · N855AS · Cndair CL6002B19 · Emergency LightingSDR A6WA200540116Idg · lack of lubeIDG NR 2 CAS MESSAGE ON TAKEOFF, ABORTED TAKEOFF, BELOW 60 KNOTS TO 70 KNOTS, TOTAL WEIGHT 47000. ALL BRAKES IN GREEN LT TO RT 4,3,3,4 AND CONFIG WARNING ILLUMINATED. SERVICED IDG NR 2 IAW 24-12-00. OPS CHECK GOOD AT THIS TIME. BTMS CHECKS NORMAL AT THIS TMar 21, 2005 · N436AW · Cndair CL6002B19 · AC Generator-AlternatorSDR VNAA0503010Warning System · activatedMULTIBLE TIMES DURING THE FLIGHT THE CREW RECEIVED ANTI-ICE DUCT WARNING MESSAGES. THE CREW OF FLIGHT 2471 FOLLOWED THE QRH AND MADE AN UNEVENTFUL LANDING AT DESTINATION. MAINTENANCE PERFORMED AN OPERATIONAL TEST OF THE BLEED-AIR LEAK DETECTION AND WARNING SMar 21, 2005 · N242JS · Cndair CL6002B19 · Ice/Rain Protection SystemSDR VNAA0503011Piston · damagedIN FLIGHT (CLT TO ROC) THE L REV UNLOCKED CAUTION MESSAGE ILLUMINATED. THE CREW OF FLIGHT 2532 FOLLOWED THE QRH, RETURNED TO CLT, AND MADE AN UNEVENTFUL LANDING. PSA MAINTENANCE DEFERRED THE LT THRUST REVERSER AND C/W THE M FUNCTION IAW CRJ 200 MEL 78-30-01 Mar 21, 2005 · N241PS · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA200540117Bushing · migratedRT MLG AFT TRUNNION BUSHING IS MIGRATED 0.15 INCH. REMOVED BUSHING, REAMED BARE AND INSTALLED 1ST OVERSIZE BUSHING IAW MFG REO. (K)Mar 20, 2005 · N415AW · Cndair CL6002B19 · Wing, Landing Gear Attach FittingsSDR A6WA200540114Coalescer Bag · dirtySTRONG FUEL SMELL IN COCKPIT AT CRUISE. SMELL INCREASED WITH TEMP SELECTED IN MANUAL MODE. SELECTED LT PACK OFF, SMELL WENT AWAY. INSPECTED APU AREA, PACK NR 1 AND NR 2, NO LEAKS NOTED. NO EVIDENCE OF FUEL AROUND ENGINES OR APU. REAM ENGINE AND BOTH PACKSMar 20, 2005 · N469AW · Cndair CL6002B19 · Humidity Control SystemSDR A6WA200540115Unknown · malfunctionedDURING APPROACH, WHEN SELECTING FLAPS FROM 30 TO 45 AIRCRAFT STARTED ROLLING LT, REQUIRED HALF AVAILABLE AILERON TRIM AND RT CONTROL WHEEL INPUT TO KEEP WINGS LEVEL. FLAP TRAVEL APPEARS UNEVEN. PERFORMED FLAP RIG CHECK, OPS CHECK GOOD. SPOILER SYSTEMS OPS CMar 20, 2005 · N426AW · Cndair CL6002B19 · Flight Control SystemSDR VNAA0503009Warning System · malfunctionedDURING TAKEOFF ROLL AT DAY THE CREW RECEIVED ANTI-ICE DUCT WARNING MESSAGES. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. PSA MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE WING ANTI-ICE CONTROL & INDICATION SYSTEM IAW CRJ 200 AMM 30-12-00-710-801Mar 20, 2005 · N242JS · Cndair CL6002B19 · Central WarningSDR ASOA05257Switch · malfunctionedDURING CLIMB OUT, BETWEEN 3,000 TO 4,000 FT, CREW RECEIVED A STAB TRIM AND MACH TRIM DISCONNECT CAUTION MESSAGE. CREW LEVELED AC OFF TO 4,000 FT, SLOWED TO 200 KNOTS TO COMPLY WITH QRH, WHICH DID NOT RESOLVE PROBLEM. THE AC RETURNED TO DEPARTURE. UPON APPROMar 20, 2005 · N821AS · Cndair CL6002B19 · Stabilizer Control SystemSDR A6WA200540121Spar · misdrilledDUE TO HOLES SPACING ON RT LOWER WING SPAR AT WS 148, JOINT STRAP 601R100465-4 S/B CANNOT BE INSTALLED IAW SB 601R-57-037. REPAIRED RT WING SPAR AT WS 148, SHIFTED CUTLINE ON T/E RT WING AT WS 148. FABRICATED A NEW DOUBLE JOINT STRAP OUT OF 2024-T3.050 PO NRMar 19, 2005 · N413AW · Cndair CL6002B19 · Wing SparSDR A6WA200540113Apu · making metalAPU FAULT CONDITION IN FLIGHT. SMOKE APPEARED IN CABIN. CLOSED PACKS AND SHUTDOWN APU. INSPECTED APU COMPARTMENT, NO FUEL OR OIL LEAKS NOTED CHECKED BOTH ACM`S IAW AMM. OIL LEVEL CHECK GOOD. CHECKED APU OIL LEVEL IAW AMM. OIL LEVEL GOOD. FOUND METAL INSMar 18, 2005 · N419AW · Cndair CL6002B19 · APU Core EngineSDR A6WA200540243Aileron · out of rigWITH AILERON TRIM CENTERED, AIRCRAFT HAS A STRONG ROLL TO THE RT. WITH LARGE AMOUNT OF LT WING DOWN TRIM, THE AIRCRAFT CAN BE MADE TO FLY LEVEL. AUTO-PILOT WAS OFF. FOUND RT AILERON SLIGHTLY OUT OF RIG. RE-RIGGED RT AILERON IAW AMM. (K)Mar 18, 2005 · N412AW · Cndair CL6002B19 · Aileron Tab Control SystemSDR A6WA200540106Access Panel · corrodedLT LOWER WING PLANK FUEL TANK ACCESS PANEL CUT-OUT BETWEEN SS 0.00 AND WS 29.42 HAS MINOR FRETTING ON FAYING SURFACE LESS THAN .006 INCH DEEP. C/A PENDING (K)Mar 17, 2005 · N415AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200540107Access Panel · corrodedRT LOWER WING PLANK FUEL TANK ACCESS PANEL CUT-OUT BETWEEN SS 50.54 AND WS 66.2 HAS MINOR FRETTING AND FAYING SURFACE LESS THAT .006 INCH DEEP. (K) BLEED MINOR FRETTING ON RT LOWER WING PLANK BETWEEN WS 50-54 AND 66.2 IAW REO. (K)Mar 17, 2005 · N415AW · Cndair CL6002B19 · Wing, Plate/SkinSDR A6WA200540100Intercostal · crackedLT INTERCOSTAL AT FS 484.0 AT LBL 36 CRACKED, .5 INCH LONG. PERFORMED A REPAIR AT 484.0 LBL 36 BY CUTTING OUT DAMAGED AREA AND INSTALLING NEW ANGLE IAW REO. (K)Mar 16, 2005 · N413AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540109Floorbeam · crackedFLOORBEAM ANGLE AT FS 621 LT SIDE IS CRACKED 1 INCH. PERFORMED REPAIR TO RT FS 621 FLOORBEAM ANGLE IAW BOMBARDIER REO 601R-53-117 REV C. (M)Mar 16, 2005 · N415AW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR A6WA200540110Floor Support · crackedFLOOR SUPPORT ANGLE AT FS 621 RT SIDE IS CRACKED 1 INCH. PERFORMED REPAIR TO RT FS621, FLOOR SUPPORT ANGLE IAW REO. (K)Mar 16, 2005 · N415AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540122Rib · crackedLT HAND MLG WHEEL WELL AT SS 48.30, FS 523.8, BATT RIB IS CRACKED 1.2500 INCH LONG. REPAIRED LT WING BATT RIB AT WS 53.60 IAW MFG REO. (K)Mar 16, 2005 · N413AW · Cndair CL6002B19 · Wing, Rib/BulkheadSDR A6WA200540108Attach Angle · crackedFOUND FS 280, FRAME RBL 9, ATTACHMENT ANGLE TO BE CRACKED APPROX 1 INCH LENGTH.Mar 16, 2005 · N415AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
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