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 SWIA200617360Computer · malfunctionedFLAPS FAIL CAUTION ON DEPARTURE. RETURNED TO BASE. RESET FLAP COMPUTER AND PERFORMED SYSTEM TEST ON FECU AND COULD NOT DUPLICATE. OPERATIONAL CHECKS GOOD.Oct 27, 2006 · N905SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR TRAX200600953Handle · corrodedCREW OVHD ESCAPE HATCH OUTER HANDLE SHAFT IS VERY CORRODED. REMOVED AND REPLACED HANDLE ASSY ON OVHD CREW HATCH IAW CRJ 200 SRM 51 42 06 RIG AND OPS CHECK C/W SATISFACTORY (CLOSED 11/03/06)Oct 26, 2006 · N907EV · Cndair CL6002B19 · Emergency ExitsSDR SWIA200617361Switch · malfunctionedRT REVERSE UNLOCK CAUTION IN FLIGHT. ENGINE SHUTDOWN. REPLACED THE RT ENGINE THRUST REVERSER STOW SWITCH AND RIGGED IAW CRJ 200 MM 78-37-01 AND 78-30-00. OPERATIONAL CHECKS GOOD, PN: 228-50741-115-88308Oct 24, 2006 · N405SW · Cndair CL6002B19 · Engine Thrust ReverserSDR CA061025002Switch · inoperative(CAN) WHILE CARRYING OUT A 12 MONTH CABIN OXYGEN FUNCTIONAL TEST, FOUND THE OXYGEN CONTROL PANEL SEMI-FUNCTIONAL. THE ROTARY KNOB WOULD NOT GO TO THE "CLOSED" POSITION WITHOUT EXCESSIVE FORCE. ROTATING TO THE "OVERRIDE" POSITION FUNCTIONED PROPERLY BUT OXYGEN Oct 24, 2006 · Cndair CL604 · Passenger Oxygen SystemSDR REXA200600096Drive Shaft · unknownFLAP FAILURE IN CRUISE, SECOND OCCURRENCE IN 72 HOURS. REMOVED, CLEANED, LUBED AND REINSTALLED ALL FLEXIBLE ACTUATOR DRIVE SHAFTS IAW AMM.Oct 22, 2006 · N8718E · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA200600094Flap System · malfunctionedFLAP FAIL INDICATION ON APPROACH. DECLARED EMERGENCY LANDED WITHOUT ISSUES. SYSTEM RESET AND PLACED ON 72 HOUR WATCH IAW AD 2006-12-21.Oct 21, 2006 · N8718E · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR REXA200600093Flap System · malfunctionedFLAP FAILURE INDICATION AFTER PUSHBACK. SYSTEM RESET AND PLACED ON 72 HOUR WATCH IAW AD 2006-12-21.Oct 20, 2006 · N800AY · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR VNAA0610033Tire · failedCREW REPORTED A LOUD NOISE ON TAKEOFF ROLL. MAINTENANCE INSPECTED AND FOUND THE LEFT HAND NOSE TIRE HAD SUFFERED TREAD SEPARATION. MAINTENANCE REMOVED AND REPLACED BOTH NOSE TIRES. FUSELAGE AND GEAR DOOR WERE REPAIRED. OPERATIONAL CHECKS WERE PERFORMED. AOct 20, 2006 · N216PS · Cndair CL6002B19 · TireSDR VNAA0610034Engine · failedCREW REPORTED SMOKE IN COCKPIT AND CABIN ON TAKEOFF. CREW REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE INSPECTED AND FOUND COKING ON 10TH STAGE DUCTING. MAINTENANCE REMOVED AND REPLACED THE NR 2 ENGINE. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAOct 20, 2006 · N253PS · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR VNAA0610031Brake · failedCREW REPORTED A FLAPS HALF SPEED ADVISORY MESSAGE. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND MOTOR BRAKE UNIT. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE.Oct 19, 2006 · N223JS · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA200617347Wire · disconnectedFLOOR LEVEL EMERGENCY LIGHTING AT ROW 1 INOP. RECONNECTED FIRST SECTION OF EMERGENCY FLOOR TRACK LIGHTING IAW MM 33-51-01. OPERATIONAL CHECKS GOOD.Oct 19, 2006 · N405SW · Cndair CL6002B19 · Light System WiringSDR TRAX200600895Doubler · crackedRT FS 640 DOUBLER HAS 1.5 INCH LONG CRACK AT STRINGER 10, FLT 4844 CX.Oct 18, 2006 · N909EV · Cndair CL6002B19 · Fuselage Main, StructureSDR TRAX200600896Doubler · crackedLT FS 640 DOUBLER HAS .7500 INCH CRACK AT STRINGER 10. REPAIRED & MODIFIED FRAME 640 BETWEEN STR 9 AND 12 ON LT & RT SIDE REF: SB601R-53-061 APP B. REPAIRED THE BONDED SKIN DOUBLER AT FRAME 640 REF REO: 601R-53-61-506. REPAIRED RIGHT SIDE LOWER BOX BEAM WEB Oct 18, 2006 · N909EV · Cndair CL6002B19 · Fuselage Main, StructureSDR TRAX200600897Beam · crackedENGINE BOX BEAM HAS A CRACK AT RT LOWER ACCESS PANEL FORWARD IB CORNER. CRACK IS APPROXIMATELY 1.5- 2 INCHES LONG. REPAIRED RIDE SIDE LOWER BOX BEAM WEB AT ACCES PANEL REF REO 11/01/06 01R-53-61-366 (CLOSED 11/01/06)Oct 18, 2006 · N909EV · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR CA061022009Window · cracked(CAN) LEFT SIDE WINDOW CRACKED (NOT SHATTERED) AT FL 350 (TC# 20061022009)Oct 15, 2006 · Cndair CL6002B19 · Flight Compartment WindowsSDR VNAA0610027Unknown · smokeCREW REPORTED SMOKE IN CABIN. AIRCRAFT RETURNED TO CLT WITHOUT INCIDENT. MAINTENANCE INSPECTED AND CLEANED ACM. MAINTENANCE ALSO SERVICED ACM OIL. OPERATIONAL CHECKS WERE PERFORMED. NO DEFECTS NOTED. AIRCRAFT WAS RELEASED FOR SERVICE.Oct 14, 2006 · N253PS · Cndair CL6002B19 · Air Distribution SystemSDR TRAX200600864Sign · inoperativeEMERGENCY EXIT SIGN NEXT TO SERVICE DOOR INOP.Oct 13, 2006 · N926EV · Cndair CL6002B19 · Emergency LightingSDR TRAX200600852Frame · crackedRT SIDE FRAME 640 BRACKET HAS EVIDENCE OF CRACKED UPPER SECTION. FABRICATED AND INSTALLED NEW FRAME ANGLE AND 640 DOUBLER ON RT. SIDE IAW SB 601R-53-61. JOB COMPLETE (SUPPLEMENTAL - SDR CLOSED)Oct 12, 2006 · N914EV · Cndair CL6002B19 · Fuselage Main, FrameSDR TRAX200600853Frame · crackedLT SIDE FRAME 640 BRACKET HAS EVIDENCE OF CRACKED UPPER SECTION. FABRICATED AND INSTALLED NEW FRAME ANGLE AND 640 DOUBLER ON RT. SIDE IAW SB 601R-53-61. JOB COMPLETE (SUPPLEMENTAL - SDR CLOSED)Oct 12, 2006 · N914EV · Cndair CL6002B19 · Fuselage Main, FrameSDR TRAX200600855Door · stiffCREW REPORTS ASD HARD TO OPERATE.Oct 12, 2006 · N884AS · Cndair CL6002B19 · Entrance StairsSDR VNAA0610021Apu · failedCREW REPORTED SMOKE IN THE COCKPIT AND THE CABIN. MAINTENANCE CHECKED AIRCRAFT FOR SOURCE OF SMOKE. MAINTENANCE DETERMINED THE SOURCE AS THE APU. MAINTENANCE REMOVED AND REPLACED THE APU. AIRCRAFT WAS RELEASED FOR SERVICE.Oct 12, 2006 · N216PS · Cndair CL6002B19 · APU Core EngineSDR MASA200602422Wire Harness · unknownCREW RETURNED TO GATE DUE TO A PAX DOOR WARNING. MX REPLACED THE WIRING HARNESS.Oct 11, 2006 · N7264V · Cndair CL6002B19 · Door System WiringSDR VNAA0610019Antenna · failedCREW REPORTED A LIGHTNING STRIKE ON DESCENT. MAINTENANCE INSPECTED AIRCRAFT. RADAR ANTENNA WAS REPLACED. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE.Oct 11, 2006 · N251PS · Cndair CL6002B19 · Weather Radar SystemSDR TRAX200600862Structure · crackedRANRC 350. 280.00 SEB CRACKED AT RBL13 NEAR LWR FLANGE. REMOVED EXISTING FASTENERS REQUIRED FOR REPAIR. MADE CUT OUT IN LOWER WEB AS REQUIRED. FABRICATED -8 FILLER. LOCATED ADDITIONAL HOLES FOR REPAIR. FABRICATED -4 DOUBLER USING S6144-33. LOCATED ALL FASTENEOct 11, 2006 · N880AS · Cndair CL6002B19 · Fuselage Main, StructureSDR TRAX200600863Web · crackedRANRC 351. 280.00 WEB CRACKED AT LBL13 NEAR UPPER FLANGE. ALL WORK DONE IAW ASA EO 600-53-91 L/W TH302. (CLOSED 10/31/06)Oct 11, 2006 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA200640364Carbon Seal · leakingRT ENGINE OIL LOW PRESSURE ILLUMINATED EN ROUTE, WITH THROTTLE RETARDED, OIL PRESSURE DROPPED FROM 48 TO 28 PSI. ENGINE WAS SHUTDOWN MANUALLY. PERFORMED ENGINE OIL CONSUMPTION CHECK PER AWAC SUPPLEMENT 06-025. FOUND STARTER CARBON SEAL LEAKING. REMOVED ANDOct 11, 2006 · N465AW · Cndair CL6002B19 · Turbine Engine Oil SystemSDR TRAX200600861Attach Fitting · crackedRANRC NR 319U, 280.00 CLIPS AT RBL 9 AND LBL9 OB CRACKED. REMOVED RT AND LT OB CLIPS. DUPLICATED OB CLIP USING 2024-T3 .050 PO8398-1. MATERIAL ID FROM SRM 53-21-43. OK TO PRIME AND PAINT. PRIMED AND PAINTED IAW SRM 51-25-06. OK TO INSTALL. INSTALLED OB CLIOct 11, 2006 · N880AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR CA061013006Bpsu · malfunctioned(CAN) ON SELECTING FLAPS FOR APPROACH (FLAP FAIL) MESSAGE DISPLAYED. DUE TO WEATHER CONDITION AIRCRAFT PROCEEDED WITH MISSED APPROACH. UNABLE TO RETRACT FLAPS. AIRCRAFT DIVERTED TO NEAREST ALTERNATE AIRPORT WITH IMPROVED WEATHER , WITH FLAPS REMAINING EXTENDEOct 11, 2006 · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR TRAX200600848Anchor Fitting · crackedAFT ASD ANCHOR FITTING CRACKED. CRACK IS .547 INCH.Oct 10, 2006 · N980EV · Cndair CL6002B19 · Entrance StairsSDR TRAX200600849Floor Panel · crackedRANRC NR 188// LT FLOOR EDGE POSSIBLY CRACKED AT FS605 AND FS589 FROM FAST. TO EDGE OF PART (MARKED).Oct 10, 2006 · N880AS · Cndair CL6002B19 · Fuselage Floor PanelSDR TRAX200600850Angle · corrodedRANRC NR 202// FLOOR LEVEL ANGLE; 621 BULKHEAD LBL27-LBL37; BARE METAL AND SURFACE CORROSION.Oct 10, 2006 · N880AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR TRAX200600851Floor Support · corrodedRANRC NR 203// RT SIDE FLOOR EDGE MEMBER FROM FS621-FS574 SURFACE CORROSION AND RUSTED FAST. AROUND NUTPLATES (MARKED).Oct 10, 2006 · N880AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR TRAX200600859Window · crackedF/O`S SIDE WINDOW CRACKED, DECLARED AN EMERGENCY.Oct 10, 2006 · N821AS · Cndair CL6002B19 · Flight Compartment WindowsSDR VNAA0610017Warning Message · false activationCREW REPORTED SMOKE AND TOILET MESSAGE. MAINTENANCE CHECKED AIRCRAFT FOR SOURCE OF SMOKE, NONE FOUND. AIRCRAFT WAS RELEASED FOR SERVICE.Oct 9, 2006 · N253PS · Cndair CL6002B19 · Smoke DetectionSDR CA061013005Fuel Line · leaking(CAN) RAMP CREW SERVICING AIRCRAFT REPORTED FUEL LEAKING FROM NR 1 ENGINE ON TAXI OUT. SHUTDOWN NR 1 ENGINE. FUEL DRIPPING FROM LOWER COWL. MAINTENANCE INSPECTION FOUND VARIABLE GUIDE VANE FUEL LINE LEAKING. LINE P/N J1175D0244AA REPLACED. LEAK CHECKED AND AIROct 8, 2006 · Cndair CL6002B19 · Engine Fuel DistributionSDR MASA200602389Controller · dirtyCREW REPORTED AN APU FIRE WARNING IN FLIGHT. CREW ACTUATED THE APU FUEL SOV AND THE MESSAGE CLEARED. CONTRACT MX INSPECTED THE APU AND SURROUNDING AREAS AND DETERMINED NO ACTUAL FIRE OCCURRED. MX CLEANED LOOPS AND REPLACED THE CONTROLLER.Oct 4, 2006 · N17217 · Cndair CL6002B19 · Fire DetectionSDR VNAA0610007Fan Blade · damagedCREW REPORTED DAMAGE TO NR 2 ENGINE FAN BLADES. MAINTENANCE INSPECTED AND FOUND DAMAGE TO TWELVE BLADES. MAINTENANCE REMOVED AND REPLACED DAMAGED BLADES. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE.Oct 2, 2006 · N241PS · Cndair CL6002B19 · Turbine Engine Compressor SectionSDR 2006FA0001008Control Unit · malfunctionedREPORTED IN-FLIGHT SQUAWK, (STAB TRIM FAIL IN FLIGHT) ON AC. HSTCU WAS REMOVED AND SENT FOR TEST AND REPAIR. DURING BENCH TEST/INSPECTION THE FOLLOWING ITEMS WERE NOTED. UNIT MEMORY INDICATED (CP PITCH TRIM SWITCH JAMMED) (AC SWITCH). DURING AUTO TEST, (HSOct 2, 2006 · N87353 · Cndair CL6002B19 · Stabilizer Control SystemSDR VNAA0610008Warning System · malfunctionedCREW REPORTED A STAB TRIM AND MACH TRIM CAUTION MESSAGE ON CLIMBOUT. CREW ELECTED TO RETURN TO CLT WITHOUT INCIDENT. MAINTENANCE RESET SYSTEM. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE.Oct 1, 2006 · N248PS · Cndair CL6002B19 · Central WarningSDR MASA200602337Packing · defectiveASH 7203 IAD. CAPTAIN REPORTED EXHAUST/FUEL SMELL IN CABIN AND FLIGHT DECK. MX REMOVED AND REPLACED PACKING ON APU FCU. (9-26-06)Sep 23, 2006 · N37342 · Cndair CL6002B19 · APU Engine Fuel and ControlSDR VNAA0609020Sensor · malfunctionedCREW REPORTED LEFT ENGINE POWER LOSS. AIRCRAFT RETURNED TO BHM WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE T2 SENSOR. CHECKS WERE ACCOMPLISHED AND AIRCRAFT WAS RELEASED FOR SERVICE.Sep 20, 2006 · N216PS · Cndair CL6002B19 · Engine Indicating SystemSDR TRAX200600756Light · brokenEMERGENCY LIGHT JUST INSIDE OF PAX DOOR JUST BELOW ARROW ON FWD WALL BROKEN.Sep 19, 2006 · N882AS · Cndair CL6002B19 · Emergency LightingSDR VNAA0609019Fuel Control · malfunctionedCREW REPORTED LT ENGINE POWER LOSS UP TO 10-15 PERCENT. FUEL FLOW INDICATION LOW, ALL ENGINE INDICATIONS FLUCTUATED, AND ENGINE VIBRATION OCCURED. AFTER A FEW MINUTES PROBLEM DISAPPEARED AND ALL INDICATIONS NORMAL. AIRCRAFT RETURNED TO BHM WITHOUT INCIDENT.Sep 19, 2006 · N215PS · Cndair CL6002B19 · Fuel Controlling SystemSDR COMA0660546Oil Tank · overservicedFLIGHT 5011 - RIGHT ENGINE OIL PRESSURE MESSAGE IN FLIGHT EN ROUTE FROM SAV TO LGA. FLIGHT DIVERTED TO GSO AND LANDED WITHOUT INCIDENT. FOUND OIL TANK OVER SERVICED. DRAINED AND RESERVICED PER CRJ AMM, OPS CHECKS GOOD.Sep 18, 2006 · N510CA · Cndair CL6002B19 · Turbine Engine Oil SystemSDR MASA200060231Mechanism · dirtyASH 7136 UAL. PAX DOOR BINDING. MX CLEANED AND LUBED THE DOOR ASSY.Sep 18, 2006 · N653ML · Cndair CL6002B19 · Passenger/Crew DoorsSDR TRAX200600749Door · stiffPAX DOOR HARD TO SECURE.Sep 15, 2006 · N826AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR MASA200602284Unknown · odorASH 7476 UAL. CREW REPORTED OF SMELL OF FUEL IN COCKPIT IN FLIGHT WHEN TEMP SELECTED TO WARM. MX RAN ENGINES AND FOUND NO SIGN OF FUEL SMELL.Sep 15, 2006 · N37342 · Cndair CL6002B19 · Air Distribution SystemSDR VNAA0609013Blade · brokenCREW REPORTED ON CLIMB FROM CLT THAT THE RIGHT HAND WINDSHIELD WIPER BLADE WAS BROKEN. CREW ELECTED TO RETURN TO CLT AND LANDING WAS UNEVENTFUL. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND WINDSHIELD WIPER BLADE. AIRCRAFT WAS RELEASED FOR SERVICE.Sep 13, 2006 · N248PS · Cndair CL6002B19 · Windshield/Door Rain/Ice RemovalSDR TRAX200600728Floorbeam · crackedAFT ANGLE CRACKED AT FS 280 FLOORBEAM JUST OB OF LBL 9.Sep 10, 2006 · N925EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR TRAX200600729Floorbeam · crackedAFT ANGLE CRACKED AT FS 280 FLOORBEAM JUST OB OF RBL 9.Sep 10, 2006 · N925EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
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