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 A6WA200540257Channel · crackedCHANNEL OF MAIN UNDERCARRIAGE AND UPLOCK APRON BENT AND CRACKED. REPAIRED IAW EO. (K)Jul 2, 2005 · N462AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR COMA0560373Transducer · malfunctionedRT ENGINE OIL PRESSURE WARNING. REPLACED OIL PRESSURE TRANSDUCER.Jul 1, 2005 · N498CA · Cndair CL6002B19 · Engine Oil PressureSDR VNAA0506014Skin · lightning strikeAFTER LANDING THE CREW REPORTED A LIGHTNING STRIKE. MAINTENANCE COMPLIED WITH LIGHTNING STRIKE INSPECTIONS IAW CRJ200 AMM 05-51-05-210-801 AND 05-51-05-220-801. LIGHTNING DAMAGE FOUND ON THE LEFT WING TIP WAS REPAIRED IAW BOMBARDIER REO 601R-57-30-001. NO AJun 28, 2005 · N241PS · Cndair CL6002B19 · Wing, Plate/SkinSDR REX2005F00019Control System · failed(REF NR: 05-084) FLAPS FAILED AT 8 DEGREES ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K)Jun 28, 2005 · N8914A · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200540223Drag Angle · damagedPAX DOOR AFT DRAG ANGLE CRACKED NEAR UPPER SUPPORT PULLEY. REPAIRED AFT DRAG ANGLE BY REMOVING DAMAGE, PERFORMED EDDY CURRENT INSPECTION, FABRICATED AND INSTALLED REPAIR PIECES IAW REO. (K)Jun 25, 2005 · N419AW · Cndair CL6002B19 · Passenger/Crew DoorsSDR VNAA0506012Switch · stuckDURING CLIMB THE FLIGHT ATTENDANT CALL SWITCH AT SEATS 11D/F BECAME STUCK IN THE ON POSITION CAUSING THE AURAL CHIME TO SOUND CONTINUOUSLY IN THE CABIN. WHEN THE FLIGHT ATTENDANT TRIED TO UNSTICK THE SWITCH THE OXYGEN MASKS ABOVE 11D/F DEPLOYED. THE CREW RETJun 24, 2005 · N244PS · Cndair CL6002B19 · Passenger Compartment EquipmentSDR REX2005F00023Fcu · failed(REF NR: 05-080) FLAP FAIL ON TAXI, RETURNED TO GATE. REMOVED AND REPLACED FLAP ELECTRONIC UNIT (FECU) IAW AMM, SYSTEM TESTS GOOD. (K)Jun 24, 2005 · N8524A · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REX2005F00024Control System · failed(REF NR: 05-079) FLAPS FAIL ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAP SYSTEM AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K)Jun 24, 2005 · N8524A · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR ASOA05549Lamp · burned outDURING A GROUND INSPECTION, AN EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN AN EXTERIOR EMERGENCY LIGHT. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)Jun 23, 2005 · N902EV · Cndair CL6002B19 · Emergency LightingSDR ASOA05550Support Beam · crackedDURING HANGAR MAINTENANCE, THE ENGINE SUPPORT BEAM WAS FOUND TO BE CRACKED IN THE TOP WEB AT THE FIRE LOOP BRACKET BEYOND LIMITS. MAINTENANCE REPAIRD THE ENGINE SUPPORT BEAM UPPER WEB AT THE FIRE LOOP BRAKCET IAW EO. (K)Jun 23, 2005 · N852AS · Cndair CL6002B19 · Fuselage, Powerplant Attach FittingsSDR ASOA05551Step · brokenDURING AN A-CHECK, THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN AT THE ATTACH LINK. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPS CHECK GOOD. (K)Jun 23, 2005 · N865AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA05552Frame · crackedDURING A C-CHECK, THE FS 280 FRAME AT RBL 9 LOWER ANGLE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FS 280 FRAME AT RBL 9 LOWER ANGLE IAW EO. (K)Jun 23, 2005 · N851AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA05553Floorbeam · corrodedDURING A C-CHECK, THE FORWARD AND AFT FLOOR SUPPORT ANGLES AT FS 280 BETWEEN LBL 9 AND RBL 9 WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FORWARD AND AFT FLOOR SUPPORT ANGLES AT FS 280 BETWEEN LBL 9 AND RBL 9 IAW EO. (K)Jun 23, 2005 · N851AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA05554Bulkhead · corrodedDURING A C-CHECK, THE PILOTS BULKHEAD WEB AT FS 280 BETWEEN LBL 9 AND RBL 9 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE PILOTS BULKHEAD WEB AT FS 280 BETWEEN LBL 9 AND RBL 9 IAW EO. (K)Jun 23, 2005 · N851AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA200540218Angle · crackedRT FS 621.00 ANGLE IS CRACKED .5 INCH LONG ON OB RADIUS. REPAIRED BY REMOVING DAMAGED SECTION OF ANGLE, FABRICATING ANGLES AND STRAP, INSTALLING REPAIR PART IAW MFG REO. (K)Jun 22, 2005 · N423AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540217Threshold · crackedCARGO DOOR THRESHOLD PLATE HAS A .2500 INCH CRACK AT FS 589.00, LBL 41.5. REPAIRED BY REMOVING DAMAGED SECTION OF FLOOR LANDING PERFORMING EDDY CURRENT INSP, PAINTING REPAIR AREA AND FILLED REDUNDANT HOLE IAW MFG REO. (K)Jun 22, 2005 · N423AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540219Angle · crackedLT FS 621.00 ANGLE IS CRACKED .5 INCH LONG ON OB RADIUS. REPAIRED BY REMOVING DAMAGED SECTION OF ANGLE, FABRICATING REPAIR ANGLES AND STRAP, INSTALLING REPAIR PARTS IAW MFG REO. (K)Jun 22, 2005 · N423AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA0506013Skin · dentedTHE CREW REPORTED TWO DENTS ON THE AFT FUSELAGE BELOW THE CARGO DOOR. THE AIRCRAFT WAS FERRIED TO CKB WHERE BOMBARDIER REPAIRED AND INSPECTED THE DAMAGE IAW BOMBARDIER REGIONAL AIRCRAFT SERVICES ENGINEERING ORDER 601R-53-6747. REF AML 4282.27 AND BOMBARDIER Jun 22, 2005 · N250PS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA05546Sill · crackedDURING C-CHECK, THE CARGO COMPARTMENT FLOOR SILL PLATE WAS FOUND TO BE CRACKED AND CORRODED AROUND THE SCREW HOLES BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CARGO COMPARTMENT FLOOR SILL PLATE. (K)Jun 22, 2005 · N851AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA05547Seat Track · corrodedDURING A C-CHECK, THE SEAT RAIL FLOOR AT FS 379, LBL 9 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE SEAT RAIL FLOOR AT FS 379, LBL 9. (K)Jun 22, 2005 · N851AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA05548Pressure Panel · corrodedDURING A C-CHECK, THE PRESSURE FLOOR AT LBL 36, RBL 36 FROM FS 409+128 TO FS 559 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE PRESSURE FLOOR AT LBL 36, RBL 36 FROM FS 409+128 TO FS 559 IAW EO. (K)Jun 22, 2005 · N851AS · Cndair CL6002B19 · Fuselage Floor PanelSDR REX2005F00025Control System · malfunctioned(REF NR: 05-078) FLAPS FAIL ON APPROACH AT 20 ON APPROACH, QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K)Jun 22, 2005 · N8758D · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REX2005F00026Control System · malfunctioned(REF NR 05-077) FLAPS FAIL ON APPROACH AT 30, QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD-98-20-01. (K)Jun 22, 2005 · N8721B · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200540210A/C Pack · smokeRT PACK HIGH TEMP MESSAGE, PACK SHUTDOWN, SMOKE IN CABIN AND COCKPIT. (K)Jun 21, 2005 · N404AW · Cndair CL6002B19 · Cabin Cooling SystemSDR A6WA200540215Intercostal · crackedRT FS 484.00 INTRCOSTAL AT LBL 36.0 HAS A .5 INCH LONG CRACK. FABRICATED ANGLE IAW EO. REMOVED FLANGE AND INSTALLED ANGLE IAW MFG REO. (K)Jun 21, 2005 · N423AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540216Angle · crackedRT FS 460.00 ANGLE AT RBL 9 HAS A .5 INCH CRACK. REMOVED CRACK ANGLE AND INSTALL NEW ANGLE AT RBL 9. (K)Jun 21, 2005 · N423AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200540214Angle · crackedLT OBLIQUE ANGLE AT FS 625, CRACKED ON AFT SIDE .5 INCHES LONG. REMOVED OBLIQUE ANGLE LT FS 625, INSTALLED NEW SERVICEABLE ANGLE IAW SRM. (K)Jun 21, 2005 · N419AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA05545Door · stiffDURING A GROUND INSPECTION, FA REPORTED THE PASSENGER DOOR DIFFICULT TO CLOSE FROM INSIDE. MAINTENANCE OPENED AND CLOSED THE PASSENGER DOOR SEVERAL TIMES WITH NO DEFECTS NOTED. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (K)Jun 21, 2005 · N821AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR A6WA200540245Angle · crackedRT OBLIQUE ANGLE AT FS 625 CRACKED ON AFT EDGE APPROX 1 INCH LONG. REMOVED OBLIQUE ANGLE RT FS 625, INSTALLED NEW SERVICEABLE ANGLE IAW SRM. (K)Jun 21, 2005 · N419AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR CA050625001Piccolo Tube · cracked(CAN) WHILE CARRYING OUT INSPECTION IAW S/B 601R-30-029, MAINTENANCE FOUND 2 CRACKS IN THE OB PICCOLO TUBE ASSY. BOTH CRACKS ARE APPROX 1INCH IN LENGTH, THE FIRST CRACK IS 77.5 INCH FROM THE OB END, THE SECOND CRACK IS 83 INCH FROM OB END.Jun 20, 2005 · Cndair CL6002B19 · Airfoil Anti/De-ice SystemSDR ASOA05544Clip · crackedDURING A C-CHECK, THE CLIP AT FS 625 LT AFT PRESSURE BULKHEAD WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CLIP AT FS 625 LT AFT PRESSURE BULKHEAD IAW SRM. (K)Jun 20, 2005 · N851AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR REX2005F00027Control System · failed(REF NR: 05-076) FLAP FAIL ON APPROACH WHEN GOING FROM 20 TO 30, QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAP SYSTEM AND PLACED ON 72 HOUR WATCH IAW AD-98-20-01. (K)Jun 20, 2005 · N8905F · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200540209Window · crackedLT SIDE WINDOW CRACKED IN COCKPIT (ON APPROACH). REMOVED AND REPLACED LT SIDE WINDOW IAW MM. (K)Jun 17, 2005 · N450AW · Cndair CL6002B19 · Flight Compartment WindowsSDR CA050713006Bolt · missingNOTICED BY MAINTENANCE THAT THE NR 2 NOSE WHEEL ASSEMBLY WAS MISSING ONE TIE BOLT. NOSE WHEEL WAS REPLACED. A SECOND OCCURANCE A FEW DAYS LATER ON ANOTHER AIRCRAFT WAS REPORTED AFTER THE CREW NOTED THAT THE NOSE WHEEL SEEMED TO BE SPINNING LONGER THAN USUAL.Jun 17, 2005 · Cndair CL6002B19 · Wheel/Ski/FloatSDR VNAA0506009Tire · failedINSPECTION AFTER LANDING REVEALED THE NR 2 TIRE TREAD HAD SEPARATED DURING LANDING, CAUSING DAMAGE TO THE LT INBD FLAP AND TO THE NR 1 ENGINE FAN BLADES. A BURST TIRE DAMAGE INSPECTION WAS PERFORMED IAW CRJ200 AMM 05-51-29-210-801. ALL DAMAGED COMPONENTS WERJun 16, 2005 · N250PS · Cndair CL6002B19 · TireSDR CA050704003O-Ring · flat(CAN) ON APPROACH, ENG NR 1 OIL PRESS WAS FLUCTUATING THEN 'ENG 1 OIL PRESS' WARNING MESSAGE WAS RECEIVED ON ED1. THE ENGINE NR 1 WAS SHUT DOWN. AIRCRAFT LANDED IN VALENCIA. 5 QUARTS WERE ADDED TO ENGINE NR 1 AND FOUR C-SUMP O-RINGS WERE REPLACED. THE PARTJun 14, 2005 · Cndair CL6002B19 · Turbine Engine Oil SystemSDR MASA200500467None · noneASH 6169 LAS - ABORTED TAKEOFF DUE TO THE NR 2 ENGINE OVERTEMP ON TAKEOFF ROLL 904 DEG FOR 4 SECONDS. MX FOUND THE ENGINE TO NOT EXCEED AMM LIMITS. MAINTENANCE PERFORMED A COMP WASH.Jun 14, 2005 · N87353 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR VNAA0506008Fcu · failedTHE FLAPS FAIL CAUTION MESSAGE ILLUMINATED WITH BOTH FLAPS AT 45 DEGRESS ON FINAL APPROACH. MAINTENANCE CYCLED THE CIRCUIT BREAKERS AND OPERATIONALLY TESTED THE FLAP SYSTEM IAW CRJ 200 AMM 27-54-00-710-801. ALL OPS CHECKS WERE GOOD. THE AIRCRAFT WAS THEN REJun 13, 2005 · N241PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200540197Hinge · crackedCREW ESCAPE HATCH HINGES ARE CRACKED AROUND BASE. REPLACED BOTH HINGE ARMS WITH NEW HINGE ARMS IAW REO SRM. (K)Jun 13, 2005 · N419AW · Cndair CL6002B19 · Emergency ExitsSDR REX2005F00028Control System · malfunctionedFLAPS FAILED AFTER LANDING WHEN SELECTED UP DURING TAXI. RESET SYSTEM AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K)Jun 13, 2005 · N8936A · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR MASA200500463Bleed Valve · failedABORTED TAKEOFF DUE TO A NR 2 ENG ITT ACCIDENCE. MAINTENANCE IS IN THE PROCESS OF EVALUATING THE ENGINE AND PERFORMING A HIGH ENERGY RTO INSPECTION. MAINTENANCE IS IN THE PROCESS OF EVALUATING THE ENGINE AND PERFORMING A HIGH ENERGY RTO INSPECTION. MX REPLAJun 13, 2005 · N87353 · Cndair CL6002B19 · Compressor Bleed ValveSDR CA050613001Switch · contaminated(CAN) DURING CRJ SERVICE CHECK ON ROUTINE MAINTENANCE. THE MECHANIC WAS UNABLE TO PUSH-IN EITHER LT OR RT (FIRE EXT PUSH-OFF) SWITCHES/PBA. BOTH PBA ASSEMBLIES FOUND CONTAMINATED (CORROSION) WITH A WHITE POWDER DEPOSIT. REPLACED BOTH PBA ASSEMBLIES. AIRCRAFJun 12, 2005 · Cndair CL6002B19 · Extinguishing SystemSDR CA050617001Landing Gear · failed(CAN) A/C LANDED NOSE GEAR UP, CREW UNABLE TO EXTEND NLG BY NORMAL OR MANUAL. THE NLG IS THE ORIGINAL INSTALLATION FROM PRODUCTION. STILL UNDER INVESTIGATION.Jun 12, 2005 · Cndair CL6002B19 · Nose/Tail Landing GearSDR VNAA0506004Control Unit · malfunctionedTHE FLAPS FAIL CAUTION MESSAGE ILLUMINATED ON SHORT FINAL WITH FLAPS AT 45 DEGREES. MAINTENANCE CHECKED THE FLAP ELECTRONIC CONTROL UNIT AND SKEW DETECTION SYSTEM FOR CODES IAW RJ-SL-27-84. SYSTEM FAULTS CLEARED. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT Jun 11, 2005 · N241PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA0506005Control Unit · malfunctionedTHE FLAPS FAIL CAUTION MESSAGE ILLUMINATED AFTER FLAPS REACHED 45 DEGREES ON APPROACH. MAINTENANCE RESET THE FLAP ELECTRONIC CONTROL UNIT IAW RJ-SL-00-001. OPERATIONAL CHECKS WERE NORMAL. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.Jun 11, 2005 · N241PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA0506006Unknown · unknownUPON POWER APPLICATION FOR TAKEOFF THE AIRCRAFT VEERED LEFT WITH NO RESPONSE TO RUDDER INPUT. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE INSPECTED THE NOSE LANDING GEAR AND FOUND NO DEFECTS. A HIGH SPEED TAXI WAS PERFORMED WITH THE CJun 11, 2005 · N260JS · Cndair CL6002B19 · Nose/Tail Landing GearSDR REX2005F00029Control System · failed(REF NR: 05-074) FLAPS FAIL MESSAGE AT ZERO WHEN RETRACTED. EMERGENCY DECLARED QRH FOLLOWED UNEVENTFUL LANDING WITH FLAPS 0. RESET FLAPS AND PLAED ON 72 HOUR WATCH IAW AD 98-20-01. (K)Jun 11, 2005 · N8524A · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REX2005F00030Control System · failed(REF NR 05-073) FLAPS FAIL MESSAGE WHEN GOING FROM 20 TO 30 DEGREES. EMERGENCY DECLARED QRH FOLLOWED UNEVENTFUL LANDING WITH FLAPS 20. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K)Jun 11, 2005 · N8598B · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA050617008Engine · flamed out(CAN) RT ENGINE ROLLED BACK, FLAMED OUT DURING CRUISE, AT FL380. NO ABNORMAL INDICATIONS SHOWN. CREW DECLARED EMERGENCY, DESCENDED TO FL210 AND RESTARTED ENGINE USING CROSS BLEED. UNEVENTFUL LANDING AT DIVERSION AIRPORT. NO LEAKS FOUND DURING GROUND RUNS. FUELJun 8, 2005 · Cndair CL604 · Engine (Turbine/Turboprop)SDR ASOA05499Relay · shortedDURING A GROUND INSPECTION, AN AC ESS BUSS FAULT MESSAGE WAS RECEIVED AND THE EMERGENCY LIGHTS REMAINED ON. MAINTENANCE REMOVED AND REPLACED THE AC ESS TRANSFER RELAY. OPERATIONAL CHECKS GOOD AIRCRAFT OK FOR SERVICE. (K)Jun 7, 2005 · N838AS · Cndair CL6002B19 · Emergency Lighting
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