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 SWIA200312039Bulb · burned outMAIN CABIN DOOR EXTERIOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BULB. OPS CHECK GOOD. (P/N 1308)May 24, 2003 · N459SW · Cndair CL6002B19 · Emergency LightingSDR CA030518001Gearbox · defective(CAN) WHEN PILOT RETARDED THROTTLE AT TOP OF DESCENT, LT ENGINE FLAMED OUT. UNEVENTFUL SINGLE ENGINE LANDING. TROUBLE SHOOTING REVEALED THROTTLE CONTROL GEARBOX DEFECTIVE.May 18, 2003 · Cndair CL6002B19 · Power LeverSDR CA030515006Line · chafed(CAN) THE CREW REPORTED AN ENGINE VIBRATION ON ENGINE NR 2. MAINTENANCE CARRIED OUT A VISUAL INSPECTION OF THE AFT EQUIPMENT BAY AND FOUND HYDRAULIC LINES AND A WIRE CHAFING. THE DAMAGED LINES AND FAIRLEAD WERE REPLACED, THE AIRCRAFT RETURNED TO SERVICE.May 14, 2003 · Cndair CL6002B19 · Hydraulic System, MainSDR SWIA200311995Wire · brokenPILOT STICK SHAKER INOP. BROKEN WIRE. DISCOVERED DURING C-CHECK. INSTALLED NEW TERMINAL ENDS ON PILOT SIDE STICK SHAKER WIRES IAW AWM CHAPTER 27-35-00. OPS TESTED SPS (PRE-FLIGHT TEST) IAW AMM TASK 27-35-01-710-801. TEST SERVICEABLE.May 14, 2003 · N433SW · Cndair CL6002B19 · Stall Warning SystemSDR SWIA200311996Floorbeam · crackedFLOORBEAM ATTACH ANGLES AT FS 280 LBL 9 ARE CRACKED. DISCOVERED DURING C-CHECK. ANGLES REPLACED IAW CRJ SRM 51-40-11 PAR 4, 51-42-20, 51-42-06 & RII53-401.May 14, 2003 · N433SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200311997Floorbeam · crackedFLOORBEAM ATTACH ANGLES AT FS 280 RBL 9 ARE CRACKED. DISCOVERED DURING C-CHECK. REPLACED ANGLES IAW CRJ SRM 51-40-11 PAR 4, 51-42-20, 51-42-06 & RII53-401.May 14, 2003 · N433SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200311998Intercostal · crackedCABLE FAIRLEAD INTERCOSTAL AT FS 484 IS CRACKED AT RBL 36. DISCOVERED DURING C-CHECK. REPAIRED INTERCOSTAL IAW CRJ REO 601R53-41-059 REV A (RII53-401).May 14, 2003 · N433SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200311999Floorbeam · crackedFS 621.00 LBL 36 FLOOR ANGLE CRACKED. DISCOVERED DURING C-CHECK. REPAIRED DAMAGE AREA IAW CRJ REO 601R-53-61-117 REV A & RII53-401.May 14, 2003 · N433SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR CA030515007Engine · overserviced(CAN) SMOKE/FUMES DETECTED IN FLT COMPARTMENT & CABIN, TOILET SMOKE WARNING ACTIVATED, QRH DRILL ACTIONED, PAN DECLARED, SMOKE CLEARED, RETURN, LANDED SAFELY. MAINT CARRIED OUT AN INSP & CONCLUDED THAT SMOKE/FUMES WERE RELATED TO NR 1 ENGINE HAVING BEEN OVERSMay 13, 2003 · Cndair CL6002B19 · Turbine Engine Oil SystemSDR CA030514001Windshield · cracked(CAN) DURING THE APPROACH, THE PILOT REPORTED THE LT WINDSHIELD OUTER PANE CRACKED. THE AIRCRAFT LANDEDUNEVENTFULLY. FOLLOWING THE WINDSHIELD REPLACEMENT, THE AIRCRAFT RETURNED TO SERVICE.May 9, 2003 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA030514002Link · worn(CAN) AFTER T/O AT APPROX 4,000 FT CREW COMPLAINED ABOUT AN AIRFRAME HARMONIC VIBRATION. NO EICAS MSGS WERE POSTED & ENGINE VIBRATIONS AND PARAMETERS WERE NORMAL .AT 16,000 FT A/P DISCONNECTED, APPROX 10-20 SECONDS LATER A/C ROLLED TO THE RT, F/O BROUGHT THE May 8, 2003 · Cndair CL6002B19 · Aileron Control SystemSDR CA031001003Windshield · cracked(CAN) IN CRUISE, AT FL 300 THE INNER PLY OF THE RT WINDOW CRACKED. THE QRH WAS APPLIED AND THE FLT CONTINUED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS FERRIED WHERE THE WINDOW WAS REPLACED.May 8, 2003 · Cndair CL6002B19 · Wing Main, Frame StructureSDR SWIA200311991Floorbeam · crackedFS 280 RIGHT FLOORBEAM RBL 9.0 ATTACH ANGLES CRACKED. DISCOVERED DURING C-CHECK. ANGLES REPLACED IAW CRJ SRM 51-40-11.May 7, 2003 · N435SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200311993Floorbeam · crackedFS 621 LEFT FLOORBEAM ANGLE LBL 42 CRACKED. DISCOVERED DURING C-CHECK. REPAIRED DAMAGED AREA IAW CRJ REO 601R-53-61-117 REV A.May 7, 2003 · N435SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200311994Floorbeam · crackedFLOORBEAM ANGLES AT STR 14 FS 625 ARE CRACKED BOTH SIDES. DISCOVERED DURING C-CHECK. REPLACED ANGLES IAW CRJ SRM 51-40-11 AND 51-42-06.May 7, 2003 · N435SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200311939Pdu · malfunctionedON LANDING THE RIGHT THRUST REVERSER DID NOT DEPLOY, 14TH STAGE POPOUT VALVE WAS IN AND THRUST REVERSER WAS ARMED. MANUALLY RESET THE THRUST REVERSER PDU. OPERATED THE RIGHT THRUST REVERSER SEVERAL TIMES WITH NO FURTHER PROBLEMS.May 4, 2003 · N406SW · Cndair CL6002B19 · Engine Thrust ReverserSDR 2003FA0000454Solenoid · stuckDURING ENGINE MAINTENANCE, SMOKE WAS NOTED COMING FROM THE APU INLET DOOR. MECHANICS TRIED TO DRY MOTOR THE APU TO EXTINGUISH THE FLAMES, BUT WERE UNSUCCESSFUL. DRY CHEMICAL WAS USED TO EXTINGUISH THE FLAMES. DURING INVESTIGATION AND TEARDOWN OF THE APU AT THEMay 2, 2003 · N434AW · Cndair CL6002B19 · APU Engine Fuel and ControlSDR CA030507001Windshield · failed(CAN) DURING DESCENT AT APPROXIMATELY 11000 FT, THE CAPTAIN'S WINDSHIELD SHATTERED. QRH PROCEDURE FOLLOWED, FLIGHT CONTINUED AND LANDED SAFELY. AIRCRAFT RETURNED TO SERVICE FOLLOWING THE WINDSHIELD REPLACEMENT.May 1, 2003 · Cndair CL6002B19 · Flight Compartment WindowsSDR CA030501003Reservoir · leaking(CAN) DIVERSION DUE TO MECHANICAL. CREW REPORTED 'HYD 2 LOW PRESS LIGHT CAME ON IN FLIGHT(FL330) HYDRAULIC PRESSURE READ 0 PSI. ENGINE WAS RUN FOR 33 MINUTES ENROUTE TO DIVERSION LANDING KFWA. 'NIL HYDRAULIC QUANITY. LANDING COMPLETED WITH OUT INCIDENT. MAINTEApr 25, 2003 · Cndair CL6002B19 · Hydraulic Reservoir, MainSDR REX2003F00000Line · disconnectedENROUTE, FLIGHT 5849 WAS LEVELING AT FL130 AND RECEIVED A RT ENG OIL PRESS MESSAGE ON EICAS. CREW CONTACTED MAINT AND SHUT DOWN RT ENGINE 2-3 MINUTES AFTER INITIAL MESSAGE, USING APPROVED CHECKLIST. CREW DECLARED AN EMERG WITH ATC AND WAS APPROVED TO CONTINUApr 24, 2003 · N8532G · Cndair CL6002B19 · Turbine Engine Oil SystemSDR SWIA200312060Floorbeam · crackedFS 280 PILOT'S BULKHEAD LBL 90 AFT FLOOR ANGLE CRACKED. DISCOVERED DURING C-CHECK. REPAIRED DAMAGED AREA IAW CRJ REO 601R-53-11-138 NC.Apr 21, 2003 · N410SW · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA200312061Skin · crackedFS 235 FUSELAGE SKIN RBL 6.0 NLG CUTOUT CRACKED. DISCOVERED DURING C-CHECK. REPAIRED DAMAGED AREA IAW CRJ REO 601R-53-11-048 REV B.Apr 21, 2003 · N410SW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR CA030426001Outflow Valve · malfunctioned(CAN) AIRCRAFT HAS RECEIVED A REPORT WHICH WE FEEL IS A REPORTABLE EVENT. THE CABIN ALTITUDE STARTED TO FLUCTUATE ERRACTICALLY AND BEGAN CLIMBING UNCONTROLLABLY. THE O2 MASK DROPPED AND COMMENCED EMERGENCY DESCENT TO MINIMUM SAFE ALTITUDE. THE LANDING WAS UNEVApr 19, 2003 · Cndair CL6002D24 · Pressure Regulator/Outflow ValveSDR SWIA200311881Fcu · malfunctionedFLAP FAIL MESSAGE IN FLIGHT. PERFORMED A NO FLAP LANDING. PULLED AND RESET FLAP CIRCUIT BREAKERS. OPS CHECK OF FLAPS GOOD. UPDATE 3/18/2003: FLAPS FAIL CAUTION MESSAGE ILLUMINATED ON APPROACH WHEN SELECTING FLAPS 8 DEGREES, FLAPS FAILED AT 0 DEGREES. FLAApr 14, 2003 · N924SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA200311876Wire · damagedSTICK SHAKER DOES NOT OPERATE CORRECTLY DURING TEST. REPAIRED WIRE TO LEFT STICK SHAKER. OPS CHECKED NORMAL.Apr 12, 2003 · N910SW · Cndair CL6002B19 · Navigation System WiringSDR CA030514017Apu · fire(CAN) APPROXIMATELY 5 MINUTES AFTER SHUTTING DOWN APU (ENGINES OFF NO GROUND POWER), DECIDED TO OPEN APU DOOR TO HELP COOL APU DOWN PRIOR TO LCV CHANGE. 2 MINUTES LATER, MAITNENANCE NOTICED THAT SMOKE AND FLAMES WERE COMING OUT OF THE APU INTAKE. MECHANIC RUApr 4, 2003 · Cndair CL6002B19 · APU Core EngineSDR CA030518002Gearbox · malfunctioned(CAN) THE RT ENGINE FLAMED OUT DURING DESCENT, WHEN THROTTLES WERE RETARDED TO IDLE, RT ENGINE CONTINUEDTO SPOOL DOWN ( TOP OF DESCENT ). TRIED RE-LIGHT ACCORDING QRH : N2 STAGNATION AT 40 PERCENT AND HIGH ITT, ABORTED ENGINE START AND PERFORMED UNEVENTFULL SIApr 4, 2003 · Cndair CL6002B19 · Power LeverSDR CA030406001Check Valve · damaged(CAN) FLT CREW REPORTED LOSS OF PRESSURIZATION AT FL330, CABIN RATE INCREASED AT 2000/3000 FT PER MIN.EMERGENCY DESCENT PERFORMED PER QRH.AIRCRAFT LANDED WITHOUT FUTHER INCIDENT.MTCE FOUND A DUCT BLOWN OFF THE LEFT WATER SEPARATOR AND THE LT BULKHEAD CHECK VALApr 2, 2003 · Cndair CL6002B19 · Air Distribution SystemSDR CA030404009Flapper Valve · damaged(CAN) AT CRUISE ALTITUDE 'ARINC COOL' & 'DISPLAY COOL'MESSAGES WERE GIVEN. FLIGHT ALTERNATE AND STANDBY SELECTIONS WERE TRIED BUT MESSAGE STAYED ON.AIRCRAFT PLANNED TO DIVERT BUT AT LOWER ALTITUDETHE MESSAGE WENT AWAY SO FLIGHT CONTINUED TO ORIGINAL DESTINATIOApr 2, 2003 · Cndair CL6002B19 · Air Distribution FanSDR SWIA200311867Structure · burnedLEFT OUTBOARD FLAP TRAILING EDGE HAS SEVERAL BURNED AREAS AS A RESULT OF A LIGHTNING STRIKE. INSTALLED SERVICEABLE FLAP ON LEFT OUTBOARD POSITION IAW 27-54-01 AND 27-54-05. S/N OFF: SB/RJ/731.Mar 31, 2003 · N445SW · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA200311863Computer · malfunctionedFLAPS FAILED DURING APPROACH FOR LANDING AT DEN. LANDED WITHOUT INCIDENT. INSPECTED FLAPS FOR KINKS. NO DEFECTS NOTED. CYCLED POWER. RESET COMPUTER. OPS CHECK GOOD.Mar 27, 2003 · N924SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR CA030401007Line · chafed(CAN) NR 1 EDP HYDRAULIC CASE DRAIN LINE WAS CHAFING AGAINST NR 1 EDP HYDRAULIC PX LINE, DUE TO INSUFFICIENT CLEARANCE/SYSTEM VIBRATION. CHAFING OCCURRED OVER A LENGTH OF APPROXIMATELY 4 INCHES, AND WAS BEYOND ALLOWABLE LIMITS.Mar 27, 2003 · Cndair CL604 · Hydraulic System, MainSDR CA030328002Display · failed(CAN) ON AIRCRAFT POWER UP CDU NR 3 SHOWED A BLACK SCREEN. THE MAINTENANCE DIAGNOSTIC COMPUTOR (MDC) LINE REPLACEABLE UNIT (LRU) STATUS INDICATED CODE: CDU 3 FAILED - NO CDU-2OUT. MDC LRU DIAGNOSTICS INDICATED CODE: CDU 3 354 - FAILED. NEW CDU INSTALLED AND SMar 26, 2003 · Cndair CL604 · Flight Management Computing Hardware SystemSDR CA030330002Pulley · seized(CAN) FLT CREW REPORTED A/P TRIM CAUTION MSG ACCOMPANIED WITH FLASHING 'A' ON THE PFD WHILE CLIMBING THROUGH 25,000 FT (OAT -25C). AFTER A/P WAS DISENGAGED, THE AILERONS WERE NOTABLY STIFF. AN EMERGENCY WAS DECLARED AND THE CREW ELECTED TO DIVERT.UPON REACHINMar 25, 2003 · Cndair CL6002B19 · Aileron Control SystemSDR ASOA03127Engine · malfunctionedDURING CLIMB-OUT AT APPROXIMATELY 6,500 FT THE CREW RECEIVED A RED FLAG ON THE LT INTERSTAGE TURBINE TEMPERATURE GAUGE OF APPROXIMATELY 886 DEGREES. THE CREW REDUCED POWER SLIGHTLY ON THE LT ENGINE WITH THE TEMPERATURE RETURNING TO NORMAL, THEN INCREASED POWEMar 23, 2003 · N836AS · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR CA030317001Trim Panel · failed(CAN) 6 TO 7 MINUTES AFTER TAKE OFF RUDDER STARTED MOVING FULL RIGHT, RUDDER TRIM. APPLIED LT TRIM - STOPPED AT 1.25 RT DEFLECTION. RUDDER TRIM STUCK. EMERGENCY DECLARED AND DIVERTED TO TPA. R&R'D AILERON TRIM PANELMar 15, 2003 · Cndair CL6002B19 · Rudder Tab Control SystemSDR CA030319005Fuel Control · leaking(CAN) MAINTENANCE FOUND EXCESSIVE FUEL LEAK FROM NR 2 ENGINE FCU. UPON EXAMINATION FOUND THAT FUEL WAS LEAKING FROM AROUND THROTTLE SPLINE SHAFT. FCU WAS REPLACED.Mar 13, 2003 · Cndair CL6002B19 · Fuel Controlling SystemSDR CA030403004Skin · delaminated(CAN) CREW REPORTED (LEFT OUTBOARD FLAP UPPER PANEL HAS 6 INCH DELAMINATION). OUTBOARD FLAP UPPER SKIN FOUND TO HAVE 2 CRACKS NEAR INBOARD END BEGINNING AT LEADING EDGE OF SKIN PANEL.Mar 12, 2003 · Cndair CL6002B19 · Trailing Edge FlapsSDR CA030419001Line · chafed(CAN) AT FLIGHT LEVEL 33000, YELLOW CAS MESSAGE, HYD NR 2 LOW PSI ILLUMINATED.REF /A/ - IPC 29-11-00, ITEM35, P/N 601-75238-43, HYD PUMP PRESS SYS 2 TUBE ASSYREF /B/ - IPC 29-11-00, ITEM 215, P/N 601R75286-51, CASE DRAIN SYS 2 TUBE ASSYIT WAS FOUND BY THE MAINMar 7, 2003 · Cndair CL6002B19 · Hydraulic System, MainSDR SWIA200311909Access Panel · corrodedLEFT WING FUEL PANEL REBATES HAVE CORROSION UNDER PANELS 510AB, 540AB, 540CB, 540DB, 540FB, 550AB. FOUND DURING C-CHECK INSPECTION. DAMAGE REPAIRED IAW CRJ REO 601R-57-21-030 REV A UNDER PANEL 510AB MAX MAT'L LOSS .002, 540CB MAX MAT'L LOSS .008, 540DB MAX MMar 3, 2003 · N587SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA200311911Panel · crackedRIGHT LOWER WING PLANK WS 148.019 FOUND CRACKED. FOUND DURING C-CHECK INSPECTION. NDT-HFEC CARRIED OUT IAW REO 601R-57-21-13 IAW WS 148.019. NO CRACKS NOTED. DAMAGED AREA OF RIGHT LOWER WING PLANK REPAIRED IAW REO 601R-57-21-130 REV D AND REO 601R-57-21-1Mar 3, 2003 · N587SW · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA200311837Drive Shaft · damagedLEFT WING NR 4 FROM INBOARD FLEXIBLE DRIVE SHAFT IS DAMAGED AT HEX END. FOUND DURING C-CHECK INSPECTION. FLEX DRIVE REPLACED IAW CRJ MM 27-53-10-400-803. P/N: 11045D100-401, S/N OFF: 4864, S/N ON: 8082.Feb 21, 2003 · N908SW · Cndair CL6002B19 · Trailing Edge Flap Control SystemSDR SWIA200311838Intercostal · crackedFS 625 STR 14 LT AND 14 RT INTERCOSTAL ANGLE CRACKED. FOUND DURING C-CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM 51-40-11, 51-42-06. P/N: 601-35012-51.Feb 21, 2003 · N908SW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA200311793Circuit Breaker · poppedABORTED TAKEOFF IN SJC FOR AILERON TRIM WARNING. AILERON TRIM CB POPPED, RESET CB. OPERATED SYSTEM THROUGH SEVERAL TIMES. AILERON TRIM OPS CHECK GOOD AT THIS TIME IAW CRJ MM 27-11-00.Feb 19, 2003 · N437SW · Cndair CL6002B19 · Aileron Tab Control SystemSDR SWIA200311799Strut · dischargedAFTER SELECTING GEAR UP, TWO RED EICAS MESSAGES NOSE DOOR OPEN, GEAR DISAGREE. AMBER MESSAGE STEERING INOP AND WOW INPUT. SERVICED NOSE STRUT IAW CRJ MM 12-12-32. JACKED AIRCRAFT AND PERFORMED GEAR SWING. OPS CHECKS GOOD.Feb 18, 2003 · N441SW · Cndair CL6002B19 · Nose/Tail Landing GearSDR SWIA200311811Display · malfunctionedFIRST OFFICERS MULTIFUNCTION DISPLAY FAILED IN FLIGHT. REMOVED AND REPLACED FIRST OFFICERS EFD. OPS CHECK GOOD.Feb 17, 2003 · N453SW · Cndair CL6002B19 · Attitude and Direction Data SystemSDR SWIA200311812Wire · corrodedEMERGENCY ROW EXIT LIGHTS OUT IN THE BACK SECTION. FOUND WIRE PIGTAIL FOR AFT LIGHT SECTION TO BE CORRODED. REPLACED PIGTAIL. OPS CHECK GOOD.Feb 17, 2003 · N443SW · Cndair CL6002B19 · Light System WiringSDR SWIA200311788Latch · unsecureAFTER TAKEOFF HEARD A LOUD WHISTLE COMING FROM THE OUTSIDE. ALSO RECEIVED A STALL FAIL CAUTION MESSAGE FOR A FEW SECONDS, THEN IT CLEARED ITSELF. WITH INCREASED SPEED, THE NOISE GOT LOUDER AND FELT SLIGHT VIBRATION. RETURNED TO DEN FOR LANDING. FOUND THE FFeb 16, 2003 · N917SW · Cndair CL6002B19 · Landing Gear DoorsSDR CA030225008Drag Brace · cracked(CAN) THE AIRCRAFT LANDED NORMALLY AND SHORTLY AFTER, THE NLG TOUCH DOWN, THE CREW REPORTED AN IMPACT FOLLOWED BY A NOISE AND THE NLG COLLAPSED. THE NLG COLLAPSE DUE TO THE DRAG BRACE CRACKED. THE CREW MENTIONNED ALSO A PROBABLE IMPACT WITH A SNOW BANK FOR SFeb 15, 2003 · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA200311787Bulb · burned outFORWARD CEILING EMERGENCY LIGHT INOP. RELAMPED FORWARD EMERGENCY LIGHT BULB. OPS CHECK GOOD.Feb 14, 2003 · N917SW · Cndair CL6002B19 · Emergency Lighting
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