GE CF34-3B1

Service difficulty reports · 5,402

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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 MASA200400005Transducer · fluctuatesASH 6317 MTY-PHX, IN CRUISE AT FL390 GOT TRIPLE CHIME & LEFT ENGINE OIL PRESS MASTER WARNING, OIL PRESS FLUCTUATING BETWEEN 18 & 28 PSI. SHUT DOWN LEFT ENGINE AND DIVERTED TO ELP. MX REPLACED PRESSURE TRANSDUCER, OP CHECKS GOOD.Jan 3, 2004 · N77286 · Cndair CL6002B19 · Engine Oil Indicating SystemSDR CA040106002Engine · making metal(CAN) CREW REPORTED APPROXIMATELY 30 MINUTES FROM DESTINATION, THAT NR 2 ENGINE OIL PRESSURE HAD DROPPED BELOW MINIMUM. CREW ELECTED TO PERFORM IN FLIGHT SHUT DOWN. CREW REQUESTED CFR AND LANDED WITHOUT INCIDENT. INSPECTION REVEALED NR 2 ENGINE 2 QTS LOW WITHJan 2, 2004 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR ASOA03669Engine · malfunctionedFLT 4162 - DURING TAKEOFF ROLL FROM ATL TO PHL, THE CAPTAIN REPORTED THE LT ENGINE OIL PRESSURE WAS 20 LBS LESS THAN THE RT ENGINE, BUT STILL WITHIN LIMITS. AFTER TAKEOFF THE LT ENGINE OIL PRESSURE CONTINUED TO DECREASE WITH THE LOWEST PRESSURE BEING 49 LBS. Dec 24, 2003 · N848AS · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA040123002Strut · unsecure(CAN) SHORTLY AFTER TAKEOFF, THE CREW NOTED THAT LT ENGINE THROTTLE COULD NOT BE RETARDED FROM 92 PERCENT. CREW ELECTED TO SHUT ENGINE DOWN WITH FIRE/PUSH PBA. A/C MADE AN UNEVENTFUL LANDING. SUBSEQUENT INSPECTION REVEALED THAT THE CORE COWL SUPPORT STRUT HDec 20, 2003 · Cndair CL604 · Engine Cowling SystemSDR ASOA03663Engine · odorFLT 4637 - DURING CLIMB-OUT FROM BTR-DFW, THE CREW NOTICED A STRANGE OILY ODOR IN THE AIRCRAFT WHEN SWITCHING THE PACKS FROM THE APU TO THE TENTH STATE BLEEDS. THE ODOR BEGAN TO DISSIPATE WHEN THE BLEEDS WERE SWITCHED BACK TO THE APU. THE AIRCRAFT LANDED SAFDec 19, 2003 · N848AS · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR ASOA03661Engine · bird ingestionAFTER DEPARTURE, WHILE CLIMBING THROUGH 7,000 FT A/C EXPERIENCE MULTIPLE BIRDSTRIKES. FLT ATTENDANT REPORTED SOUND OF IMPACT PLUS A HIGH FREQUENCY VIBRATION TOWARDS THE REAR OF THE AIRCRAFT. THERE WERE NO ABNORMAL INDICATIONS PRESENT IN THE COCKPIT INCLUDINGDec 18, 2003 · N719EV · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR MASA200300492Engine · seizedASH 6021 ICT-PHX. ON DESCENT FROM FLT 310 TO 290 NR 1 ENGINE ABRUPTLY SHUT DOWN WITH A LOUD VIBRATION NOISE. THE CREW ADVISED MX CNTRL OF THE ENGINE FAILURE WITH N2 -0- ROTATION. AFTER AN UNEVENTFUL LANDING MX WAS CALLED TO INSPECT THE ENGINE. MX REPLACINGDec 15, 2003 · N7291Z · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA200312699Track · looseON CLIMBOUT THROUGH 15,000 FT RIGHT REV UNLOCK MESSAGE. RETURNED TO FIELD. FOUND (2) BOLTS AT LOWER INBOARD THRUST REVERSER ACTUATOR TRACK LOOSE. REPOSITIONED ACTUATOR TRACK AND TIGHTENED BOLTS IAW 78-32-05 AND 78-37-01. ALL OPS CHECK GOOD.Dec 15, 2003 · N958SW · Cndair CL6002B19 · Engine Thrust ReverserSDR WVE2004F00000Carbon Seal · leakingDURING 400/800/12 MO INSPECTION THE RT ENGINE NR 1 CARBON SEAL WAS FOUND TO BE LEAKING OIL EXCESSIVELY. THE NR 1 CARBON SEAL WAS CHANGED THREE TIMES PREVIOUSLY: AT 1/22/00 TT: 1274:44 TC: 663, AT 8/3/00 TT: 1902:37 TC:953: AND 1/25/02 TT: 3448:35 TC: 1805Dec 15, 2003 · N316FX · Cndair CL604 · Turbine Engine Oil SystemSDR CA031222006Gearbox · inoperative(CAN) ON DESCENT FROM 310 TO 290, NR 1 ENGINE ABRUPTLY SHUT DOWN WITH A LOUD VIBRATION NOISE. 20 MINUTES OUT, NR 1 ENGINE SHUT DOWN OWN IT'S OWN WITH A LOUD VIBRATION. ENGINE WAS SECURED AND THE AC LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT ANDec 15, 2003 · Cndair CL6002B19 · Accessory GearboxesSDR ASOA03642Engine · failedDURING DESCENT, AT APPROX 24,000 FT THE CREW HEARD A LOUD POP FOLLOWED BY A VIBRATION INDICATION ON THE RT ENGINE GAUGE. QRH PROCEDURES WERE COMPLIED WITH. THE CREW REDUCED RT ENGINE POWER TO BELOW FIFTY PERCENT AND THE VIBRATION SUBSIDED. AN EMERGENCY WAS Dec 12, 2003 · N828AS · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA031211004Tube · chafed(CAN) DURING TROUBLESHOOTING OF POSSIBLE OIL LEAK ON NR 1 ENGINE, MAINTENANCE FOUND OIL LINE FROM HEAT EXCHANGER TO LUBE SCAVENGE PUMP DEEPLY CHAFED ON FLANGE OF A AND B SUMP SUPPLY LINE. LINE REPLACED. A AND B SUMP SUPPLY LINE REPOSITIONED AND ADDITIONAL CLADec 4, 2003 · Cndair CL6002B19 · Engine Oil Distribution (Airframe Furnished)SDR SWIA200312648Control Unit · failedOUTBOARD GROUND SPOILER FAULT AND FLIGHT SPOILER FAULT STATUS MESSAGE ON GROUND. RETURNED TO GATE. REPLACED NR 1 SECU. OPS CHECKS GOOD IAW 27-00-00. P/N: 44-164-05, S/N OFF: 1244.Dec 2, 2003 · N907SW · Cndair CL6002B19 · Drag Control SystemSDR CA040306001Duct · detached(CAN) THE A/C WAS DISPATCHED WITH PACK NR 1 INOPERATIVE IAW MEL. AFTER T/O, WHEN TRANSFERRING THE BLEED AIR FROM APU TO THE ENGINES, CABIN ALT CAUTION INDICATION CAME ON ON THE EICAS. THE CREW BEGAN TO FOLLOW QRH PROCEDURE AND, SUDDENLY, CABIN ALT WARNING Nov 29, 2003 · Cndair CL6002B19 · Heating SystemSDR SWIA200312722Control Unit · malfunctionedRT AILERON CONTROL HAS (UNUSUAL FEELING), CLICKING NOISE. (DISCOVERED DURING C-CHECK INSPECTION) SERVICE LETTER NR RJ-SL-27-045 COMPLIED WITH IAW CRJ AMM 27-11-05-420-001 PARAGRAPH 11.Nov 24, 2003 · N423SW · Cndair CL6002B19 · Aileron Control SystemSDR SWIA200312616Handle · malfunctionedNOSE DOOR OPENED AT 20,000 FT. GEAR DISAGREE MESSAGE AND PROX SENSOR FAIL MESSAGE. REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE. OPS CHECK GOOD IAW MM 32-31-01.Nov 23, 2003 · N409SW · Cndair CL6002B19 · Landing Gear SelectorSDR 03323621Fuel Control · out of adjustDURING UNKNOWN PHASE OF AIRCRAFT OPERATION THE RT THRUST REVERSER WAS REPORTED BINDING AT MAX POWER AND UPON DEPLOYMENT OF THRUST REVERSER. THE FUEL CONTROL RIGGING WAS FOUND TO BE OUT OF ADJUSTMENT AND WAS RE-RIGGED. A SATISFACTORY OPERATIONAL CHECK WAS PERNov 19, 2003 · N621BR · Cndair CL6002B19 · Fuel Controlling SystemSDR SWIA200312605Switch · failedSTAB TRIM AND MACH TRIM FAILED DURING FLT. REPLACED CAPTAIN'S TRIM DISCONNECT SWITCH. OPS CHECKS GOOD.Nov 16, 2003 · N439SW · Cndair CL6002B19 · Stabilizer Control SystemSDR SWIA200312598Control Unit · malfunctionedSTAB 1 CH INOP STATUS MESSAGE DISPLAYED ON FINAL APPROACH. REMOVED AND REPLACED HSTCU IAW CRJ MM 27-40-00. OPS CHECK GOOD.Nov 14, 2003 · N926SW · Cndair CL6002B19 · Stabilizer Control SystemSDR MASA200300448Fuel Control · out of rigCREW REPORTED NR 1 ENG FLAME-OUT AFTER LANDING AND TURN OFF ON TAXI WAY. MX WAS CALLED. MX RIGGED FUEL CONTROL, OPS CHECKS GOOD.Nov 12, 2003 · N27314 · Cndair CL6002B19 · Fuel Controlling SystemSDR SWIA200312588Floorbeam · crackedFS 280 RIGHT FLOORBOARD RBL 9.0 INBOARD AND OUTBOARD ATTACH ANGLES CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM 51-40-11 & RII 53-401.Nov 12, 2003 · N418SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR MASA200300440Engine · damagedON DESCENT TO YOW PILOT FELT THE A/C SHUTTER. THE PILOT THAN NOTICED THE NR 2 ENGINE VIBS FOLLOWED BY HIGH ITT AND LOW OIL PRESSURE. AN IN-FLIGHT SHUTDOWN WAS INITIATED. AFTER AN UNEVENTFUL LANDING MX WAS CALLED. AFTER A BORESCOPE OF THE ENGINE IT WAS DETENov 6, 2003 · N47202 · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA031107011Pump · failed(CAN) AFTER T/O, CREW NOTICED ENG NOISES WERE ROUGH. AUDIO CK AT AFT BLKHD IND RT ENG. NO ABNORMAL IND, AT 15,000 FT DURING PRESS CHECKS, HYD 2LO PRESS AMBER MSG POSTED ON AND OFF. ENG FLOW LINE WAS GREEN/AMBER ON AND OFF, 2800 PSI. QTY WAS NML, TEMP OF 47Nov 2, 2003 · Cndair CL6002D24 · Hydraulic Pump (Electric/Engine), MainSDR CA031110008Controller · burned(CAN)AFTER T/O, CREW NOTICED OVERHEATING ELECTRONIC SMELL, SMALL AMOUNT OF SMOKE FROM PASSENGER'S OXY CNTL PANEL. CREW DIVERTED AC, HEADED BACK TO AIRPORT OF ORIGIN. LIGHT DIMMER ASSY (PS1LN) WIRE LN15C22 FEEDING 5 VAC TO OXYGEN CTRL PANEL (P/N 6044441011, WINov 1, 2003 · Cndair CL604 · Crew Oxygen SystemSDR CA031103001Wire Harness · pinched(CAN) CLIMBING THRU 10,000 FT CREW RECEIVED PASS AND SERVICE DOOR FLASHING RED. DURING APPROACH CARGO INDICATION AS WELL. AT GATE FOUND CB DOOR INDICATOR POPPED. ON INVESTIGATION FOUND SERVICE DOOR HARNESS PINCHED IN DOOR. F.M.R. ISSUED TO CHECK OTHER A/C IN Oct 30, 2003 · Cndair CL6002B19 · Door System WiringSDR SWIA200312572Computer · malfunctionedSTALL FAIL MESSAGE AFTER TAKEOFF. REPLACED STALL COMPUTER. OPS CHECK GOOD. S/N OFF: 887Oct 29, 2003 · N918SW · Cndair CL6002B19 · Stall Warning SystemSDR CA031107010Line · cracked(CAN) NR 2 HYDRAULIC SYSTEM LEAKING. QUANITY READS ZERO. MAINTENANCE FOUND RESERVOIR FILL TUBE ASSEMBLY FOR NR 2 SYSTEM IN REAR EQUIPMENT BAY CRACKED ABOUT ONE INCH FROM FILL ADAPTER PORT.Oct 29, 2003 · Cndair CL6002B19 · Hydraulic System, MainSDR CA031105001Lock · broken(CAN) ON GROUND CREW UNABLE TO OPEN FLIGHT DECK DOOR. DOOR UNHINGED TO ALLOW EXIT FROM C/P. A/C FERRIED BACK FOR REPAIRS. AFTER DISASSEMBLY AN INTERNAL PART WAS FOUND BROKEN.Oct 28, 2003 · Cndair CL6002B19 · Fixed Inner DoorsSDR SWIA200312528Roller · lack of lubeLEFT MLG WOULD NOT COME DOWN WHEN THE GEAR LEVER WAS SELECTED DOWN. USED THE MANUAL GEAR RELEASE PER QRH. CLEANED AND LUBED ROLLER AS REQUIRED. ALL OPS CHECKS GOOD.Oct 25, 2003 · N958SW · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA200312559Wire · brokenDURING STALL TEST, SHAKER DOES NOT ACTIVATE. REPAIRED BROKEN WIRE IAW CL 600 WDM 20-00-00. OPS CHECK GOOD.Oct 25, 2003 · N433SW · Cndair CL6002B19 · Navigation System WiringSDR MASA200300426Control Quadrant · obstructedASH 7331 DEN. AIRCRAFT ABORTED TAKEOFF DUE TO NR 2 ENG W/N PRODUCE T/O THRUST. MX REMOVED FOD FROM THROTTLE QUADRANT AREA. OP CHECKS GOOD.Oct 25, 2003 · N77331 · Cndair CL6002B19 · Power LeverSDR SWIA200312548Socket · damagedDURING TAXI OUT, WHEN F/A CALL BUTTON WAS SELECTED, BOTH CALL AND EMERGENCY ILLUMINATED ON PANEL, ALL LIGHTS BUT PA ILLUMINATED ON F/A'S PANEL. NO COCKPIT/CABIN COMM OR PA ANNOUNCEMENTS WERE POSSIBLE. FOUND A MELTED LIGHT SOCKET ON AFT OVERWING COCKPIT CALL Oct 19, 2003 · N466SW · Cndair CL6002B19 · Electrical Power SystemSDR CA031014007Door · missing(CAN) A/C TAXIED TO GATE AFTER LANDING. THE LOWER LEFT FIXED COWL DOOR WAS MISSING FROM AIRCRAFT. SEVERAL MOMENTS LATER THE COWL WAS FOUND OUT ON TAXI WAY AND RECOVERED BY AIRPORT AUTHORITIES.A NUMBER OF CAMLOC FASTENERS WERE FOUND IN COWL.THE REMAINDER OF FAOct 14, 2003 · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR SWIA200312501Handle · corrodedOVERHEAD CREW ESCAPE HATCH OUTER HANDLE SHAFT CORRODED. (DISCOVERED DURING C-CHECK)REMOVED AND REPLACED CREW ESCAPE HATCH OUTER HANDLE IAW HARTWELL CORP. CMM 52-22-03.Oct 10, 2003 · N905SW · Cndair CL6002B19 · Emergency ExitsSDR SWIA200312503Intercostal · crackedFS 484 RT INTERCOSTAL OB FLANGE RBL 36 CRACKED. DISCOVERED DURING C-CHECK. REPAIRED INTERCOSTAL IAW CRJ REO 601R-53-41-059 REV (A) RII 53-401.Oct 10, 2003 · N905SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200312504Floor Support · crackedCARGO FLOOR SUPPORT ANGLE IS CRACKED AT FS 621.0; RBL 43.0. DISCOVERED DURING C-CHECK. DAMAGE REPAIRED IAW CRJ REO 601R-53-61-117 REV A AND RII 53-401. P/N: 601R53-61-117-2.Oct 10, 2003 · N905SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200312495Actuator · malfunctionedFLAPS FAIL MESSAGE WHEN SELECTED TO 45 DEGREES. FLAPS STOPPED AT 33 DEGREES. QRH COMPLIED. REMOVED AND REPLACED RIGHT INBOARD FLAP INBOARD ACTUATOR AND RIGHT INBOARD FLAP OUTBOARD ACTUATOR IAW CRJ MM 27-53-01 AND 27-53-05. P/N OFF: 852D100-11, S/N OFF: 3Oct 5, 2003 · N915SW · Cndair CL6002B19 · Trailing Edge Flap ActuatorSDR SWIA200312475Floorbeam · crackedFS 280 LT FLOORBEAM LBL 9.0 INBOARD AND OUTBOARD ATTACH ANGLES CRACKED. (DISCOVERED DURING C-CHECK INSPECTION)ANGLES REPLACED IAW CRJ SRM 51-40-11. P/N: 601R31113-57Oct 2, 2003 · N917SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200312476Floorbeam · crackedFS 280 RT FLOORBEAM RBL 9.0 I/B AND O/B ATTACH ANGLES CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) ANGLES REPLACED IAW CRJ SRM 51-40-11. P/N: 601R31113-58Oct 2, 2003 · N917SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200312477Handle · crackedPAX DOOR OUTER HANDLE IS CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) OUTER HANDLE REMOVED AND REPLACED IAW CRJ AMM 52-11-03. P/N: 601R31763-1Oct 2, 2003 · N917SW · Cndair CL6002B19 · Passenger/Crew DoorsSDR CA031020001Selector Valve · leaking(CAN) THE PILOT REPORTED UPON APPROACH, THE MLG DID NOT EXTEND AND THE DISAGREE MSG APPEARED. A SECOND ATTEMPT PRODUCED THE SAME RESULTS. THE LANDING GEAR WAS SUCCESSFULLY EXTENDED MANUALLY IAW EMERGENCY PROCEDURE. THE AIRCRAFT RETURNED TO SERVICE FOLLOWING RSep 19, 2003 · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR ASOA03440Engine · failedDURING CLIMB-OUT FROM CHS-DFW, AT APPROXIMATELY 21,000 FT THE CREW RECEIVED A LOW OIL PRESSURR WARNING ON THE LT ENGINE. BEFORE THE CREW COULD BEGIN INITIATING QRH PROCEDURES, OIL PRESSURE ON THE LT ENGINE DROPPED RAPIDLY AND SUBSEQUENTLY SHUT ITSELF DOWN, FOSep 15, 2003 · N826AS · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA200312384Bpsu · malfunctioned''FLAPS FAIL'' CAUTION MESSAGE IN FLIGHT WITH FLAPS 0. (OCCURED ON DESCENT WITHOUT FLAP HANDLE BEING MOVED.)REMOVED AND REPLACED LEFT BPSU, REF MM 27-51-10. OPS CHECKS GOOD.Sep 5, 2003 · N590SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA031001000Windshield · cracked(CAN) DURING FLIGHT, LT WINDSHIELD CRACKED. OLD STYLE WINDSHIELDSep 4, 2003 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA031014008Landing Gear · malfunctioned(CAN) PILOT REPORTED NOSE GEAR NOT DOWN AND LOCKED. TOWER COULD NOT VERIFY NOSE GEAR DOWN. COMPANY AIRCRAFT DID A FLY BY AND VERIFIED NOSE GEAR DOORS OPEN BUT NOSE GEAR NOT DOWN AND LOCKED. AIRCRAFT WAS RUNNING LOW ON FUEL.CREW DECLARED EMERGENCY AND LANDEDSep 4, 2003 · Cndair CL6002B19 · Nose/Tail Landing GearSDR ASOA03407Carbon Seal · leakingDURING CLIMB-OUT FROM DFW-SAT, AT APPROX 19,000 FT THE CREW RECEIVED A RIGHT ENGINE OIL PRESSURE WARNING. QRH PROCEDURES WERE COMPLIED WITH AND THE CREW REDUCED THE RIGHT ENGINE TO IDLE. THE OIL PRESSURE CONTINUED TO FLUCTUATE BETWEEN 40 TO 45 PSI AND SHORTLAug 31, 2003 · N851AS · Cndair CL6002B19 · Turbine Engine Oil SystemSDR SWIA200312344Ecu · malfunctionedFLT SPLRS FAULT STATUS MESSAGE INTERMITTENT. REMOVED AND REPLACED SECU. OPS CHECK GOOD IAW CRJ MM 27-00-00. S/N OFF: 01548.Aug 29, 2003 · N923SW · Cndair CL6002B19 · Drag Control SystemSDR A6WA200340128Engine · failedUPON TAKEOFF NOTED NR 1 ENGINE ITT AT 900. DURING CLIMB NOTED ITT AT 858-874. AT FL280 HEARD THUMP AND NR 1 ENGINE SPOOLED DOWN. SECURED PER QRH AND COMPLIED WITH SINGLE ENGINE OPERATIONS. REMOVED AND REPLACED NR 1 ENGINE. SHOP REPORT REMARKS, REPLACED NR Aug 29, 2003 · N440AW · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR ASOA03400Engine · bird ingestionDURING TAKEOFF, AT APPROX 4,000 A BIRD WAS INGESTED INTO THE RIGHT ENGINE AND IT SHUT DOWN. THE CREW COMPLIED WITH QRH PROCEDURES, DECLARED AN EMERGENCY AND THE AIRCRAFT RETURNED TO ATL, LANDING SAFELY. MAINTENANCE REMOVED AND REPLACED THE RIGHT ENGINE. OPSAug 26, 2003 · N855AS · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR SWIA200312350Dampener · malfunctionedYAW DAMPNER NR 1 FAILED ON PUSHBACK/WILL NOT STAY ENGAGED. REMOVED AND REPLACED NR 1 YAW DAMPNER WITH A SERVICEABLE UNIT IAW CL600 AMM 22-22-01. OPS CHECK GOOD. S/N OFF: 2762.Aug 23, 2003 · N587SW · Cndair CL6002B19 · Autopilot System
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