GE CF34-8C5

Service difficulty reports · 772

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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 = 'CF348C5'
  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 ASOA201701161065Engine · vibrationON T/O LEFT ENGINE VIBE AT 2.1 - RETURN TO ATL. REMOVED BLADES, PINS AND BUMPERS. PERFORMED GENERAL VISUAL INSPECTION OF FAN BLADES. RE-MAPPED FAN BLADES, LUBRICATED RETAINING PINS, INSTALLED FAN BLADES, PERFORMED CHECK OF THE ENGINE N1 VIBRATION LEVEL IAW TASJan 16, 2017 · N176PQ · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR MASA2017011412809Engine · unknownNR 1 ENGINE VIBRATION AT 2.5, RETARDED THROTTLE TO IDLE, DECLARED AN EMERGENCY & LANDED WITH THE NR 1 ENGINE AT IDLE. PERFORMED BLADE SHAKE & APPLIED R.O., PERFORMED ENGINE RUNS WITH CREW, VIBRATION NEVER WENT ABOVE .8, WITHIN LIMITS.Jan 14, 2017 · N910FJ · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR VNAA2016121500030Warning Message · illuminatedRIGHT FADEC CAUTION MESSAGE. CYCLED SYSTEM CIRCUIT BREAKERS.Dec 15, 2016 · N564NN · Cndair CL6002D24 · Fuel Controlling SystemSDR REXA2016121002471Engine · failedLEFT ENGINE FAILED IN FLIGHT, N1 DROPPED, ITT RED LINE, N2 DROPPED, VIBRATION REDLINE, PHYSICAL VIBRATION OF AIRFRAME PRECEDED BY A BANG. R & R THE LEFT ENGINE IAW JC 900-72-430-902. OPS CHECKED GOOD IAW JC 900-72-430-906 "Dec 10, 2016 · N902XJ · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR VNAA20162400029Engine · bird ingestionBIRD STRIKE DAMAGE TO LEFT ENGINE.Oct 24, 2016 · N557NN · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR VNAA2016102400029Blade · damagedBIRD STRIKE DAMAGE TO LEFT ENGINE. REMOVED AND REPLACED FAN BLADES NUMBERS 6 AND 20. OPS CHECK GOOD IAW AMM. RELEASED FOR SERVICE.Oct 24, 2016 · N557NN · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR VNAA2016060400003Sensor · inoperativeRIGHT ENGINE OIL PRESSURE INTERMITTENT IN FLIGHT. THE CREW DECLARED AN EMERGENCY, CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE RT OIL LEVEL, OIL TEMP SENSOR, AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOJun 4, 2016 · N547NN · Cndair CL6002D24 · Engine Oil Indicating SystemSDR MASA2016052612710Engine · flamed outLEFT ENGINE FLAMEOUT CAUTION. MAINTENANCE TROUBLESHOOTING.May 26, 2016 · N910FJ · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR REXA2016031600412Carbon Seal · damagedEN-ROUTE, LT OIL PRESS WENT FROM GREEN TO AMBER TO RED. LT ENG OIL PRESS EICAS WARNING MSG CAME ON. FOLLOWED NON-NORMAL PROCEDURES, SHUTDOWN ENG & LANDED. REMOVED STARTER FOUND AXIS D CARBON SEAL TO BE BAD. R & R AXIS D CARBON SEAL IAW AMM 72-64-01. LEAMar 16, 2016 · N314PQ · Cndair CL6002D24 · Turbine Engine Oil SystemSDR VNAA2016030800013Pressure Sensor · dirtyCREW REPORTED RECEIVING A LT MAIN EJECTOR CAUTION MESSAGE, ALONG WITH THE FUEL BOOST PUMPS CYCLING DURING CRUISE AT FL220. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, CLEANED THE LT PRIMARY EJECTOR’S PRESSURE SENSOR CONNEMar 8, 2016 · N569NN · Cndair CL6002D24 · Fuel Boost PumpSDR ASOA2016030314549Engine · shutdownRIGHT ENGINE AUTO SHUTDOWN DUE TO LIGHTNING STRIKE. R & R RT ENGINE ACFT RETURN TO SERVICE.Mar 3, 2016 · N132EV · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR CA160224005Duct · ruptured(CAN) FLIGHT CREW REPORTED, LEFT HAND BLEED DUCT WARNING, THEN CHANGED TO LT BLEED DUCT CAUTION MESSAGE, LEFT PACK OFF. QRH ACTIONED. LT BLEED SELECTED OFF, LT BLEED DUCT WARNING RETURNED AGAIN WHEN POWER APPLIED TO CLIMB, RT BLEED SHUTDOWN & STARTED LOSING PRFeb 23, 2016 · Cndair CL600* · Air Distribution SystemSDR MASA2016021612772Fadec · warning lightRT FADEC CAUTION, RETURNED TO FIELD, EMERGENCY DECLARED. OPENFeb 16, 2016 · N243LR · Cndair CL6002D24 · Fuel Controlling SystemSDR VNAA2016010400006Idg · failedCREW REPORTED GENERATOR 2 FAIL. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R NR 2 INTEGRATED DRIVE GENERATOR AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.Jan 4, 2016 · N564NN · Cndair CL6002D24 · AC Generator-AlternatorSDR CA151231004Skin · corroded(CAN) FOUND 2 CORROSION AREAS AT LT WING T/E BETWEEN WS370.25-398.93. DUE TO EXTENSIVE CORROSION DAMAGE, THE PART, PN:CC690-15116-3 NEEDS TO BE REPLACED.Dec 29, 2015 · Cndair CL6002D24 · Wing, Plate/SkinSDR CA151223009Bleed Valve · failed(CAN) CREW REPORTED A RIGHT HAND BLEED CAUTION MESSAGE AFTER TAKE OFF. QRH FOLLOWED AIRCRAFT RETURNED TO DEPARTURE AIRPORT . MAINTENANCE TROUBLESHOOTING CARRIED OUT AND 10TH STAGE BLEED VALVE REPLACED. FUNCTION CHECKS CARRIED OUT WITH NO FURTHER FAULTS TO REPODec 22, 2015 · Cndair CL600* · Compressor Bleed ValveSDR CA151119010Acm · failed(CAN) AFTER PUSHBACK THE COCKPIT FILLED WITH SMOKE AND ASH, LEFT PACK AUTO FAIL MSG CAME ON. THE PACK WAS SHUT OFF AND THE SMOKE CLEARED. THE A/C RETURNED TO GATE.Nov 18, 2015 · Cndair CL6002D24 · Cabin Cooling SystemSDR CA151111006Fitting · cracked(CAN) NLG ALTERNATE-RELEASE ACTUATOR FWD FITTING CRACKED.Nov 11, 2015 · Cndair CL6002D24 · Fuselage, Landing Gear Attach FittingsSDR CA151104003Frame · cracked(CAN) CRACK FOUND ON RT SIDE OF UPPER FRAME FS235, WL 110.Nov 3, 2015 · Cndair CL6002D24 · Fuselage Main, FrameSDR CA151028003Fadec · malfunctioned(CAN) LEFT ENGINE DEGRADED, MESSAGE FOLLOWED BY A FLAMEOUT. THEY WERE ON CONTINUOUS IGNITION DUE TO LIGHT TURBULENCE. AFTER FLAMEOUT THEY HAD LT ENGINE HIGH ITT MESSAGE AND THE MDC SHOWS A PEAK OF 968 DEGREES AND A DURATION OF 9.1 SECS. AFTER RECEIVING LT EOct 26, 2015 · Cndair CL6002C10 · Fuel Control/Turbine EnginesSDR N6WA2015100101Fmu · malfunctionedRIGHT FADEC CAUTION ILLUMINATED INFLIGHT. B1 CODE 006794 FIM TASK 73-21-03-810-826, R & R NR 2 ENG FMU IAW AMM 73-21-03. OPERATIONS & LEAK CHECKED GOOD IAW 71-00-00.Oct 1, 2015 · N184GJ · Cndair CL6002D24 · Fuel Control/Turbine EnginesSDR CA151001008Ahrs · failed(CAN) AIRCRAFT TURNED BACK DUE TO FAILED NR 1 AHRS FAILED, RED MAG FLAG, ATC REPORTED NAVIGATION WAS INNACURATE, HEADING OFF.Sep 28, 2015 · Cndair CL6002D24 · Integrated Flight SystemSDR CA150928004Link · broken(CAN) DURING REPLACEMENT OF RT INBD GROUND SPOILER ACTUATOR OUTPUT LINK (SCHED MAINTENANCE), FOUND THE CENTRAL FITTING WITH ONE BORE BROKEN.Sep 25, 2015 · Cndair CL6002D24 · Drag Control ActuatorSDR N6WA2015092201Warning System · false activationRIGHT FADEC CAUTION MSG IN FLIGHT. RAN NR 2 ENG MULTIPLE TIMES IAW AMM 71-00-00, COULD NOT DUPLICATE FAULT AT THIS TIME.Sep 22, 2015 · N184GJ · Cndair CL6002D24 · Engine Fuel Indicating SystemSDR CA150916013Skin Panel · corroded(CAN) CORROSION FOUND ON RT WINGLET LOWER SKIN PANEL.Sep 15, 2015 · Cndair CL6002D24 · Wing, Plate/SkinSDR CA150916010Skin · corroded(CAN) CORROSION ON BOTH LT AND RT LOWER WING SKIN PANELS CC690-15116-3/4.Sep 9, 2015 · Cndair CL6002D24 · Wing, Plate/SkinSDR CA150916011Drag Angle · cracked(CAN) WE HAVE CRACK ON OUR VERTICAL STAB TO FUSELAGE ATTACHMENT DRAG ANGLE ON AFT LHS . THE CRACK IS .750 INCH LONG.Sep 9, 2015 · Cndair CL6002D24 · Vertical Stabilizer Miscellaneous StructureSDR CA150909005Sensor · malfunctioned(CAN) LEFT HAND BRAKE OVERHEAD WARNING MESSAGE DURING CLIMB OUT FROM DEPARTURE POINT. BTMS TEMP INDICATORS INITIALLY INDICATED MAX TEMP BUT THEN DISPLAY WENT BLANK. AN EMERGENCY WAS DECLARED AND CREW ELECTED RETURNED TO DEPARTURE POINT. ON LANDING AND BRAKE TESep 8, 2015 · Cndair CL600* · Landing Gear Brake SystemSDR CA150901011Ecu · burned(CAN) DURING REGULAR MAINTENANCE, SMELL OF SMOKE WAS NOTICED IN THE AVIONICS BAY AND SLAT CB ON ACPC FOUND TRIPPED. SFECU NR 1 FOUND TO BE BURNT.Aug 26, 2015 · Cndair CL6002D24 · Leading Edge Slat Control SystemSDR CA150817017Probe · malfunctioned(CAN) REJECTED TAKEOFF DUE TO NR 3 BRAKE OVERHEAT INDICATION. MAINTENANCE DOCUMENTED THAT THE MDC CODE SHOWED B1-006938. THE FIM PROCEDURE WAS CARRIED OUT NO FAULT FOUND. NR 3 BRAKE TEMPERATURE PROBE WAS REPLACED IAW AMM. ALL FAULTS CLEARED FROM MDC AND AIRAug 17, 2015 · Cndair CL600* · Landing Gear Brake SystemSDR REXA2015081200783Plate · chafedTASK CARD 900-71-430-100, LEFT ENG LOWER CORE COWL BLOW OUT DOOR HINGE & LATCH PLATE CHAFED. R & R LATCH PLATE IAW SRM 51-42-06 & SRM 51-42-13. BLENDED HINGE BODY IAW EA 954-03625. R & R HINGE LEVER IAW SRM 51-42-02 0.003 MATERIAL REMOVED.Aug 12, 2015 · N918XJ · Cndair CL6002D24 · Engine Cowling SystemSDR REXA2015081200790Plate · chafedTASK CARD 900-71-430-100, LEFT ENG LOWER CORE COWL BLOW OUT DOOR HINGE & LATCH PLATE CHAFED. R & R LATCH PLATE IAW SRM 51-42-06 & SRM 51-42-13. BLENDED HINGE BODY IAW EA 954-03625. R & R HINGE LEVER IAW SRM 51-42-02 0.003 MATERIAL REMOVED.Aug 12, 2015 · N918XJ · Cndair CL6002D24 · Engine Cowling SystemSDR REXA2015080800778Engine · malfunctionedAFTER TAKEOFF IN CLIMB, THRUST ACCELERATING FROM 200KTS - 250KTS 6000 FT, RT ENG LOUD NOISE, YAW RT, LOSS OF OIL PRESS, ITT SPIKED, ENG FLAMED OUT N1 & N2 DECELERATION. PERFORMED EAC ENG FIRE OR SEVERE ENG DAMAGE & ALL QRH PROCEDURES. REPLACED RT ENG PN ON &Aug 8, 2015 · N909XJ · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR CA150814002Engine · malfunctioned(CAN) NORMAL TAKE OFF, HDG 100, CLIMBING TO 7000 FT. DURING SECOND STAGE CLIMB, WITH CLIMB THRUST SET, PASSING 6000 FT, THE CAPTAIN REPORTED A LOUD BANG ACCOMPANIED BY A YAW TO THE RIGHT. THIS WAS FOLLOWED BY A TRIPLE CHIME, ENG OIL PRESSURE WARNING, AND ITT SAug 8, 2015 · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR ASOA2015080713457Light · missingEMERGENCY LIGHTN MISSING IN FRONT OF FORWARD LAVATORY. REPLACED EMERGENCY LIGHT IAW AMM 33=51=01. ACFT OK FOR SERVICE.Aug 7, 2015 · N197PQ · Cndair CL6002D24 · Emergency LightingSDR CA150804002Brake Assy · seized(CAN) NR 2 BRAKE ASSY REPLACED DUE TO NORMAL WEAR. PERFORMED NORMAL SCHEDULED FLIGHTS, ON THE 4TH LANDING THE NR 2 BRAKE ASSY FAILED IN THE LOCKED POSITION CAUSING NR 2 TIRE TO NOT ROTATE. THE AIRCRAFT ROLLED OUT ONTO THE TAXIWAY AND THE TIRE DEFLATED. MAIAug 2, 2015 · Cndair CL6002D24 · Landing Gear Brake SystemSDR CA150801001Motor · failed(CAN) DURING APU START SEQUENCE ON RAMP IN PREPARATION FOR SCHEDULED FLIGHT, THE APU ACCELERATED TO 9% AND HUNG WITH RAPIDLY INCREASING ITT. THE START ATTEMPT WAS INTERRUPTED PRIOR TO ITT EXCEEDANCE BY THE PILOT STARTING THE APU. TROUBLESHOOTING BY MAINTENANCEJul 31, 2015 · Cndair CL6002D24 · Engine StarterSDR CA150727028Window · cracked(CAN) ON CLIMB AT FL 150, RT SIDE WINDOW CRACKED. ATB.Jul 21, 2015 · Cndair CL6002D24 · Flight Compartment WindowsSDR CA150721006Anti-Ice Valve · failed(CAN) FLIGHT CREW ADVISED ON CLIMBOUT OF DEPARTURE POINT, THE LT COWL ANTI-ICE VALVE FAILED TO OPEN. AFTER SEVERAL ATTEMPTS TO GET VALVE TO OPEN, FLIGHT RETURNED TO THE DEPARTURE POINT. MAINTENANCE ACTION HAD THE ANTI-ICE VALVE REPLACED AND THE ACFT RETURNEDJul 18, 2015 · Bombdr CL6002D15 · Air Intake Anti/De-Ice SystemSDR REXA2015071700725Engine · failedCLIMBING TO FL 220, RT ENGINE VIBRATION BEGAN TO CLIMB, SHORTLY AFTER THE RT ENGINE ITT ALSO BEGAN TO RISE. THE VIBRATION WAS PEAKING, REDUCED THE THRUST LEVER. AT THE SAME TIME RECEIVED A FWD LAV SMOKE WARNING, SHORTLY AFTER RECEIVED A AFT LAV SMOKE WARNINGJul 17, 2015 · N604LR · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR CA150720012Actuator · damaged(CAN) AS PER FLIGHT CREW, THE LHS ENGINE WAS STARTING HOT WITH ALL OTHER ENGINE INDICATIONS NORMAL. A RAPID INCREASE IN ITT WAS OBSERVED WITH ITT REACHING AS HIGH AS 940 DEGREES AT WHICH TIME THE FADEC WOULD ABORT THE START. HOT ICON WAS ON ON THE ASSOCIATED IJul 16, 2015 · Cndair CL600* · Engine (Turbine/Turboprop)SDR REXA2015071400685Cowling · chafedTASK CARD 900-54-440-301 RT ENG LOWER CORE COWL CHAFED NEAR DRAIN. REPAIRED DAMAGE TO RT ENG LOWER CORE COWL FIRE SHIELD IAW EO R54090 SEE RC 60012 FOR EO.Jul 14, 2015 · N915XJ · Cndair CL6002D24 · Engine Cowling SystemSDR REXA2015071400689Guide · wornTASK CARD 900-54-430-300 LT CORE COWL ALIGNMENT GUIDE WORN. R & R LT AFT CORE COWL ALIGNMENT GUIDE IAW REO 690-54-13-097.Jul 14, 2015 · N915XJ · Cndair CL6002D24 · Engine Cowling SystemSDR CA150707007Acm · failed(CAN) R PACK AUTOFAIL CAUTION MESSAGE POSTED ON THE EICAS AND CABIN CREW REPORTED SMOKE IN THE CABIN. FLIGHT CREW DECIDED TO RETURN TO GATE. T/S REVEALED RT ACM SEIZED (NOT ROTATING).Jul 6, 2015 · Cndair CL600* · Cabin Cooling SystemSDR REXA2015062900645Rub Strip · chafedTASK CARD 900-54-430-301 LEFT ENG AFT CORE COWL RUB STRIP CHAFED. REMOVED DAMAGE ON LT ENG AFT CORE COWL RUB STRIP TO A REMAINING THICKNESS OF .083, MINIMUM ALLOWABLE THICKNESS. .100 OUT OF LIMITS IAW SRM 54-13-00-201-005-A01. RECEIVED NEW LT ENG AFT CORE CJun 29, 2015 · N604LR · Cndair CL6002D24 · Engine Cowling SystemSDR REXA2015062900648Rub Strip · chafedTASK CARD 900-54-430-301 LT ENG UPPER & LOWER CORE COWLS RUB STRIP CHAFED. REPAIR DAMAGED SEGMENTS IAW SRM 54-23-00.Jun 29, 2015 · N604LR · Cndair CL6002D24 · Engine Cowling SystemSDR CA150626004Pump · leaking(CAN) DURING APPROACH A TOTAL LOSS OF FLUID FROM NR 3 HYD SYS WAS OBSERVED. AN EMER DECLARED. MX FOUND 3A HYD PUMP LEAKING FROM CASE DRAIN DURING PUMP OPERATION. REPLACED 3A PUMP IAW AMM 29-12-03. HYD SYS 3 BLED IAW AMM 29-10-00, GEAR SWINGS CARRIED OUT WIJun 25, 2015 · Bombdr CL6002D15 · Hydraulic Pump (Electric/Engine), MainSDR CA150622006Ballast · burned(CAN) ON GND, PRIOR TO FIRST FLIGHT OF THE DAY, STRONG ELEC SMELL IN THE FWD AREA OF CABIN WHEN ELEC POWER WAS APPLIED TO THE ACFT. REMOVED THE CEILING PANELS & SIDE WALL PANELS TO ACCESS OVERHEAD & SIDEWALL LIGHTING IN THE FWD AREA OF THE CABIN. SMELL FOUNDJun 17, 2015 · Bombdr CL6002D15 · Passenger Compartment LightingSDR CA150615004Regulator · failed(CAN) DURING TAKEOFF ROLL, FLIGHT ATTENDANT WITNESSED A LOUD SCREECHING & POPPING SOUND FROM THE GALLEY COFFEE MAKER & WATER SPILLING ONTO THE FLOOR. THE FLIGHT ATTENDANT PUSHED EMER CALL BUTTON & CREW REJECTED TAKEOFF. MX TROUBLESHOOTING DETERMINED THAT THEJun 13, 2015 · Cndair CL600* · Potable Water SystemSDR REXA2015061200580Plate · gougedTASK CARD 900-71-440-901 RT ENG LOWER THRUST REVERSER COWL OUTER LATCH COVER STRICKER PLATES GOUGED. R & R STRIKER PLATES ON RT LOWER TRANSCOWL IAW SRM 51-42-06.Jun 12, 2015 · N914XJ · Cndair CL6002D24 · Engine Thrust Reverser
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