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 CA050114002Engine · malfunctioned(CAN) ON INITIAL CLIMB, HEARD A SUDDEN AND LOUD NOISE BETWEEN 4000 AND 4500 FT AND THE RT ENGINE SHUTDOWN ITSELF IN FLT. AFTER ASSESSING THE SITUATION AND FOLLOWING QRH AND MEMORY ITEMS, THE CREW NOTIFIED THE FLT ATTENDANT, PAX AND MX OF THE SITUATION. AN EMEJan 9, 2005 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR A6WA200540016Flex Line · leakingOXYGEN LOW PRESSURE. WHILE TROUBLESHOOTING FOUND LINE (PN 3801950110) TO CAPTAINS MASK BOX LEAKING. REMOVED AND REPLACED OXYGEN FLEX LINE TO BOTTOM OF CAPTAINS SIDE OXYGEN MASK RETAINER BOX TO COCKPIT FLOOR. LEAK CHECK GOOD. (K)Jan 8, 2005 · N427ZW · Cndair CL6002B19 · Crew Oxygen SystemSDR A6WA200540017Fire Bottle · lowLT ENGINE SQUIB LIGHT WILL NOT ILLUMINATE. FOUND LT ENGINE FIRE BOTTLE LOW PRESSURE. REMOVED AND REPLACED BOTTLE. (K)Jan 8, 2005 · N412AW · Cndair CL6002B19 · Fire Bottle, FixedSDR A6WA200540018Windscreen · crackedCAPTAINS WINDSHIELD SHATTERED IN CRUISE. REMOVED AND REPLACED CAPTAINS WINDSCREEN. OPS CHECK GOOD. (K)Jan 8, 2005 · N456ZW · Cndair CL6002B19 · Flight Compartment WindowsSDR VNAA0501003Pitot Line · obstructedON A REPOSITIONING FLIGHT, DURING TAKEOFF ROLL AT DAY, THE CAPTAIN LOST IAS READOUT ON HIS PRIMARY FLIGHT DISPLAY AND PREFORMED A REJECTED TAKEOFF AT 95 KTS. PSA MAINTENACE FOUND WATER IN THE PILOT'S AND COPILOT'S PITOT LINES. THE CONTAMINATION WAS REMOVED FJan 7, 2005 · N209PS · Cndair CL6002B19 · Stall Warning SystemSDR A6WA200540013Bushing · migratedTHE RT MLG AFT TRUNION BUSHING IS MIGRATED .059 INCH. REMOVED AND REPLACED RT MLG AFT TRUNNION BUSHING IAW REO. (K)Jan 7, 2005 · N446AW · Cndair CL6002B19 · Main Landing GearSDR A6WA200540014Bushing · migratedTHE LT MLG AFT TRUNNION BUSHING IS MIGRATED .045 INCH. REMOVED AND REPLACED LT MLG AFT TRUNNION BUSHING IAW REO. (K)Jan 7, 2005 · N446AW · Cndair CL6002B19 · Main Landing GearSDR ASOA05017Step · crackedDURING AN A-CHECK, THE LOWER STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE LOWER STEP ON THE PASSENGER DOOR.Jan 7, 2005 · N830AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA05018Lamp · burned outDURING OVERNIGHT SERVICE, THE EMERGENCY LIGHT AT THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT LAMP AT THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Jan 7, 2005 · N835AS · Cndair CL6002B19 · Emergency LightingSDR ASOA05019Light · missingDURING A HANGAR CHECK, SEVERAL SECTIONS OF THE EMERGENCY FLOOR LIGHT STRIP WERE FOUND MISSING. MAINTENANCE INSTALLED EMERGENCY FLOOR LIGHTING STRIPS IN THE MISSING SECTION. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)Jan 7, 2005 · N922EV · Cndair CL6002B19 · Emergency LightingSDR ASOA05015Skin · crackedDURING A C-CHECK, THE RT AFT CORNER OF THE NLG CUTOUT WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RT FUSELAGE SKIN RADIUS AT FS 235 IAW EO. (K)Jan 6, 2005 · N826AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR CA050114001Ballast · burned(CAN) BURNING SMELL PRESENT IN CABIN DURING TURNAROUND. FOUND TOILET LIGHTS NOT WORKING AND SMELL CAUSED BY TOILET BALLAST UNIT. BALLAST UNIT REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.Jan 6, 2005 · Cndair CL6002B19 · Passenger Compartment LightingSDR A6WA200540009Skin · dentedDENT ON LT SKIN FROM FS 193, 00 TP FS 202.75 BETWEEN STR 18L AND STR 20L. REPAIRED DENT IN FUSELAGE SKIN FROM FS 193.00 TO FS 202.75 BETWEEN STR 18L AND 20L IAW BRAS EO. (K)Jan 5, 2005 · N463AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA05014Pressure Blkhd · crackedDURING A C-CHECK, THE FORWARD PRESSURE BULKHEAD IN THE HYDRAULIC BAY AT FS 202.75, BL23.71 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FORWARD PRESSURE BULKHEAD IN THE HYDRAULIC BAY AT FS 202.75, BL 23.71 WAS FOUND TO BE CRACKED BEYONDJan 5, 2005 · N826AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA05016Light · brokenDURING HANGAR MAINTENANCE, THE EMERGENCY EXIT LIGHT AT THE PASSENGER DOOR IN THE FORWARD LOWER SECTION WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY AT THE PASSENGER DOOR IN THE FORWARD LOWER SECTION. OPERATIONAL CHECKSJan 5, 2005 · N914EV · Cndair CL6002B19 · Emergency LightingSDR VNAA0501001Scavenge Pump · malfunctionedDURING CRUISE AT FL 350 THE CREW OF FLIGHT 2293 (CLT TO MSP) REPORTED OIL PRESSURE FLUCTUATING 22-42 PSI AND OIL TEMPERATURE HIGHER THAN NORMAL ON THE NR 2 ENGINE. THE AIRCRAFT DIVERTED TO DAY AND MADE AN UNEVENTFUL LANDING. AFTER TROUBLESHOOTING THE SYSTEM Jan 4, 2005 · N223JS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR ASOA05011Floorbeam · corrodedDURING A C-CHECK, THE CARGO COMPARTMENT FLOORBEAM CAP STRIP AT FS 589 BETWEEN LBL 9 AND LBL 27 WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CARGO COMPARTMENT FLOOR BEAM CAP STRIP AT FS 589 BETWEEN LBL 9 AND LBL 27. (K)Jan 4, 2005 · N823AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA05012APlate · corrodedDURING A C-CHECK, THE PASSENGER DOOR FORWARD CABLE ANCHOR FITTING AND PLATE WERE FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE PASSENGER DOOR FORWARD CABLE ANCHOR FITTING AND PLATE. (K)Jan 4, 2005 · N823AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA05013Clip · crackedDURING A C-CHECK, THE LT UPPER SURFACE OF THE PRESSURE FLOOR, FS 484 BRACKET ON THE IB AND OB WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE LT IB FS 484, LBL 27 CLIP IAW EO. (K)Jan 4, 2005 · N826AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA0501005Warning Light · illuminatedDURING DESCENT INTO PHL THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. POSITION OF THE FLAPS WAS NOT REPORTED. THE CREW OF FLIGHT 2445 FOLLOWED THE CRJ 200 QRH PROCEDURES AND MADE AN UNEVENTFUL LANDING. PSA MAINTENANCE CYCLED THE FLAP CONTROL CHANNEL 1 & 2 CIRJan 3, 2005 · N261PS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR ASOA05007Sill · corrodedDURING A C-CHECK, THE CARGO COMPARTMENT DOOR SILL PLATE WAS FOUND TO BE CORRODD, CHAFED AND CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE CARGO COMPARTMENT DOOR SILL PLATE IAW SRM. (K)Jan 3, 2005 · N826AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA05006Doubler · crackedDURING C-CHECK, THE PASSENGER DOOR FRAME DOUBLER AT THE AFT AREA UPPER IB OF THE UPPER AFT SEAL WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE PASSENGER DOOR FRAME DOUBLER AND OUTER SKIN IAW EO. (K)Jan 3, 2005 · N826AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA05005Line · looseDURING CLIMB OUT, CREW NOTICED FLUCTUATION IN RT ENG OIL PRESS OF 45-80 PSI WITH ALL OTHER INSTRUMENTS INDICATING NORMAL. AS CLIMB OUT PROGRESSED, OIL PRESS FLUCTUATIONS BEGAN DROPPING TOWARD 25 PSI ACCOMPANIED BY RT ENG OIL PRESS MESSAGE. QRH WAS COMPLIED WJan 3, 2005 · N875AS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR ASOA05003Step · crackedDURING HANGAR MAINTENANCE, THE LOWER STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE LOWER STEP ON THE PASSENGER DOOR. (K)Jan 2, 2005 · N884AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA05008Light · damagedDURING A C-CHECK, THE EMERGENCY EXIT LIGHT COVER AND BASE BY THE SERVICE DOOR WAS FOUND DAMAGED. MAINTENANCE IS REMOVING AND REPLACING THE EMERGENCY EXIT LIGHT ASSEMBLY BY THE SERVICE DOOR. (K)Jan 2, 2005 · N826AS · Cndair CL6002B19 · Emergency LightingSDR ASOA05009Step · crackedDURING A C-CHECK, THE LOWER STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE LOWER STEP ON THE PASSENGER DOOR. (K)Jan 2, 2005 · N826AS · Cndair CL6002B19 · Entrance StairsSDR ASOA05002Intercostal · crackedDURING A C-CHECK, THE LT IB FS 484 INTERCOSTAL AT BL 27 TO 36 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LT IB FS 484 INTERCOSTAL AT BL 27 TO 36 IAW EO. (K)Jan 1, 2005 · N823AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA05001Lamp · burned outDURING A GROUND INSPECTION, THE LEFT FORWARD EXTERIOR EMERGEINCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LT FORWARD EXTERIOR EMERGENCY LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.Jan 1, 2005 · N848AS · Cndair CL6002B19 · Emergency LightingSDR REXA05002Bpsu · failedFLAPS FAILED AT ZERO AT FLIGHT LEVEL 310. QRH FOLLOWED, DECLARED EMERGENCY, UNEVENTFUL ZERO FLAPS LANDING MADE. SYSTEM WOULD NOT RESET. REPLACED RT BPSU (BRAKE POSITION SENSING UNIT) IAW AMM. OPERATIONALLY TESTED GOOD. (K)Jan 1, 2005 · N8674A · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA05001Bpsu · failedFLAPS FAILED AT 30 ON APPROACH, QRH FOLLOWED UNEVENTFUL LANDING. SYSTEM WOULD NOT RESET. REPLACED RT BPSU (BRAKE POSITION SENSING UNIT) IAW AMM. (K)Dec 31, 2004 · N8416B · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR A6WA200540015Angle · crackedLT SIDE 484 ANGLE IS CRACKED AT INTERCOSTAL FLANGE AT LBL 36. REPAIRED LT SIDE 484 ANGLE AT LBL 36 IAW REO. (K)Dec 28, 2004 · N411ZW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA05004Light · brokenDURING A C-CHECK, THE EMERGENCY EXIT LIGHT COVER AND TRIM AT THE SERVICE DOOR WERE FOUND BROKEN. MAINTENANCE IS REMOVING AND REPLACING THE EMERGENCY EXIT LIGHT ASSEMBLY AT THE SERVICE DOOR. (K)Dec 28, 2004 · N823AS · Cndair CL6002B19 · Emergency LightingSDR REXA04053Control System · failedFLAPS FAILED AT ZERO WHEN SELECTD TO 20 ON APPROACH. QRH FOLLOWED, DECLARED EMERGENCY WITH UNEVENTFUL LANDING. RESET SYSTEM AND PLACED FLAPS ON 72 HOUR MONITORING IAW AD. (K)Dec 28, 2004 · N8505Q · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA04054Control System · malfunctionedFLAPS FAILED AT ZERO, WHEN SELECTED TO 20 ON APPROACH. QRH FOLLOWED, DECLARED EMERGENCY. DIVERTED, WHERE AN UNEVENTFUL LANDING WAS MADE. REMOVED, LUBED AND REINSTALLED FLEX SHAFTS. PLACED FLAPS ON 72 HOUR MONITORING IAW AD. (K)Dec 28, 2004 · N8611A · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR MASA200400730Pump · failedCLOSED - ASH 6484 PHX TO MFR. - AIRCRAFT RETURNED TO THE FIELD AND DECLARED AN EMERGENCY DUE TO THE NR 2 ENGINE OIL PRESSURE FLUCTUATION. MX IS IN THE PROCESS OF TROUBLESHOOTING. OPEN PENDING RESOLUTION. 12/27 MAINTENANCE REMOVED AND REPLACED NR 2 EDP, OPS Dec 27, 2004 · N17358 · Cndair CL6002B19 · Turbine Engine Oil SystemSDR VNAA0412004Warning Light · illuminatedTHE PILOTS OF FLIGHT 2434, DCA TO YYZ, REPORTED A PASSENGER DOOR OUTER HANDLE CAUTION MESSAGE ON THE EICAS PRIMARY DISPLAY. THE AIRCRAFT DIVERTED TO PIT AND MADE AN UNEVENTFUL LANDING. PSA MAINTENANCE TROUBLESHOT THE PASSENGER DOOR SYSTEM IAW CRJ200 FIM 52-7Dec 24, 2004 · N220PS · Cndair CL6002B19 · Door Warning SystemSDR A6WA200440231Thrust Reverser · frozenAFTER APPLICATION OF TAKEOFF POWER RT REVERSER UNLOCK CAS MESSAGE. ABORTED TAKEOFF PRIOR TO 80 KNOTS. ALL BRAKE TEMPS NORMAL. FOUND ICE ON THRUST REVERSER NOT ALLOWING THRUST REVERSER TO STOW AND LOCK. ON-CALL DEACTIVATED THRUST REVERSER, AIRCRAFT FERRIED Dec 21, 2004 · N433AW · Cndair CL6002B19 · Engine Thrust ReverserSDR CA041223006Windshield · cracked(CAN) RT WINDSHIELD CRACKED DURING CRUISE AT FL330. A/C DIVERTED WHERE THE WINDSHIELD WAS REPLACED.Dec 21, 2004 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA041226002Switch · defective(CAN) RT THRUST REVERSER UNLOCKED MESSAGE IN CLIMB. PROCEDURE ACCORDING QRH PERFORMED. RT ENGINE SHUTDOWN DUE TO THRUST LEVER/THRUST SPLIT UP TO 9 PERCENT IN LEVEL FLT AT 4000 FT. RT REVERSER FOUND STOWED. DEACTIVATED ACCORDING TO MEL PROCEDURES. RESISTANCDec 21, 2004 · Cndair CL6002B19 · Engine Thrust ReverserSDR A6WA200440225Strut · lack of lubeGEAR DISAGREE UPON GEAR RETRACTION COMPLIED WITH. SERVICED NOSE STRUT WITH OIL AND NITROGEN IAW AMM. IAW AMM GEAR SWING, OPS CHECK GOOD IAW 32-30-00.Dec 19, 2004 · N402AW · Cndair CL6002B19 · Nose/Tail Landing Gear Strut/AxleSDR A6WA200440223Control Unit · malfunctionedMACH TRIM CAUTION MESSAGE IN FLIGHT. COMPLIED WITH QRH, MESSAGE RE-OCCURRED. REMOVED AND REPLACED HORIZONTAL STAB TRIM CONTROL UNIT. OPS CHECK GOOD.Dec 19, 2004 · N439AW · Cndair CL6002B19 · Stabilizer Control SystemSDR A6WA200440224Connector · dirtyENGINE NR 1 READS 0 PERCENT IN FLIGHT, ALL OTHER PARAMETERS NORMAL. CLEANED ALL CONNECTOR PLUGS, NR 1 ALTERNATOR AND SOCKET GROUND RAN TO TAKEOFF POWER, OPS CHECK GOOD. NO DEFECTS NOTED IAW AMM.Dec 19, 2004 · N405AW · Cndair CL6002B19 · Power Indicating SystemSDR A6WA200440227Landing Gear · malfunctionedNOSE GEAR WOULD NOT EXTEND. MANUAL EXTENSION OK. COMPLIED WITH GEAR SWING 8 TIMES. (5 TIMES REGULAR/ 3 TIMES ON EMERGENCY) OPS CHECK GOOD. (K)Dec 19, 2004 · N423AW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR ASOA041005Lamp · burned outDURING HANGAR MAINTENANCE, THE RT FORWARD EXTERNAL EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RT FORWARD EXTERNAL EMERGENCY LIGHT LAMP. OPS CHECK GOOD. AC OK FOR SERVICE. (K)Dec 18, 2004 · N856AS · Cndair CL6002B19 · Emergency LightingSDR A6WA200440226Skin · dentedFLAP LOWER SKIN DENTED AT WS NEAR T/E. DENT MEASURES 2 INCHES ROUND BY .085 INCH DEEP. INSTALLED EXTERNAL REPAIR TO LT IB FLAP LOWER SKIN AT WS 106, 5 INCHES FROM T/E IAW REO.Dec 17, 2004 · N408AW · Cndair CL6002B19 · Trailing Edge FlapsSDR VNAA0412003Outflow Valve · failedAFTER TAKEOFF THE CREW OF FLIGHT 2401 NOTED THAT THE AIRCRAFT WAS NOT PRESSURIZING. THE AIRCRAFT RETURNED TO PHL AND MADE AN UNEVENTFUL LANDING. PSA MAINTENANCE AT PHL MEL'D THE PRESSURIZATION SYSTEM. THE AIRCRAFT FLEW TO CAK WHERE PSA MAINTENANCE FOUND THEDec 15, 2004 · N206PS · Cndair CL6002B19 · Pressure Regulator/Outflow ValveSDR A6WA200440211Floor Support · crackedRT FS 621 FLOOR SUPPORT ANGLE CRACKED.Dec 14, 2004 · N408AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200440207Floor Support · crackedRT FS 621 FLOOR SUPPORT ANGLE CRACKED.Dec 14, 2004 · N408AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200440212Angle · crackedLT FS 484.00 AT LBL 36 ANGLE CRACKED.Dec 14, 2004 · N408AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR VNAA0412002Seal · dirtyDURING CLIMBOUT AFTER TAKEOFF FROM PIT THE CREW OF FLIGHT 2377 NOTED THE CABIN ALTITUDE READING 11,000FT, IT THEN WENT TO 7000 FT AND THE CABIN ALTITUDE WAS CLIMBING WITH THE AIRCRAFT. THE CREW HEARD A LOUD NOISE AND FELT AIR ESCAPING FROM THE COCKPIT ESCAPE Dec 14, 2004 · N237PS · Cndair CL6002B19 · Emergency Exits
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