GE CF34-8C5

Service difficulty reports · 772

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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 REXA2014121801220Structure · wornNR 1 ENGINE AFT CORE COWL SHOWS WEAR AT PYLON INTERFACE AREA. MECH REMOVED DAMAGE AT PYLON INTERFACE AREA, FABRICATED RUB STRIPS PERFORMED NDT AND INSTALLED RUB STRIPS IAW SRM 54-13-00-201-006-A01 AND NDTM PART 1 51-20-006-250-A01 AND SRM 51-42-06-001-001-A01Dec 18, 2014 · N904XJ · Cndair CL6002D24 · Nacelle/Pylon, Main FrameSDR REXA2014121801221Skin · damagedNR 2 ENGINE AFT CORE COWL SHOWS WEAR DAMAGE AT PYLON INTERFACE AREA. MECH REMOVED DAMAGE AT PYLON INTERFACE AREA, FABRICATED RUB STRIPS. PERFORMED NDT AND INSTALLED RUB STRIPS IAW SRM 54-13-00-201-006-A01 AND NDTM PART 1 51-20-006-25-A01, SRM 51-42-06-001-00Dec 18, 2014 · N904XJ · Cndair CL6002D24 · Nacelle/Pylon, Plate/SkinSDR REXA2014121701216Skin · damagedNR 1 ENGINE AFT CORE COWL STAND OF BLOCK AT 3 O'CLOCK POSITION HAS DAMAGE ALIGNMENT TAB. MECH R & R STANDOFF BLOCK AND INSULATION PAD AT NR 1 ENGINE AFT CORE COWL AT 3 O'CLOCK POSITION IAW SRM 54-13-00-201-002-A01.Dec 17, 2014 · N904XJ · Cndair CL6002D24 · Nacelle/Pylon, Plate/SkinSDR REXA2014121701217Pan · damagedNR 2 ENGINE AFT CORE COWL INSULATING PAD CRACKED AND STANDOFF BLOCK ALIGNMENT TAB DAMAGED AT 9 O'CLOCK POSITION. MECH R & R STAND OFF BLOCK AND INSULATING PAD AT NR 2 ENG AFT CORE COWL AT 9 O'CLOCK POSITION IAW SRM 54-13-00-201-002-A01.Dec 17, 2014 · N904XJ · Cndair CL6002D24 · Nacelle/Pylon Miscellaneous StructureSDR CA141217007Acm · failed(CAN) PILOTS REPORTED SMOKE IN THE CABIN DURING ACFT TAXI. ACFT RETURNED TO GATE. FOUND ACM FAILED.Dec 17, 2014 · Cndair CL600* · Cabin Cooling SystemSDR REXA2014121601211Structure · wornTASK CARD 900-71-440-100 RT ENG FWD UPPER CORE COWL BLOW OFF DOOR LATCH REST WORN. R & R RT ENG FWD UPPER CORE COWL BLOW OFF DOOR LATCH REST IAW SRM 51-42-06-001-001-A01 & 51-42-13-001-001-A01.Dec 16, 2014 · N904XJ · Cndair CL6002D24 · Engine Cowling SystemSDR REXA2014121601212Structure · wornTASK CARD 900-71-440-100 RT ENG FWD LOWER CORE COWL BLOW OFF DOOR LATCH REST WORN. R & R RT ENG FWD LOWER CORE COWL BLOW OFF DOOR LATCH REST SRM 51-42-06-001-001-A01 & 51-42-13-001-001-A01.Dec 16, 2014 · N904XJ · Cndair CL6002D24 · Engine Cowling SystemSDR CA141216002Crossmember · cracked(CAN) WHILE CARRYING OUT INSPECTION IAW SBA670BA-32-020 A CRACK WAS IDENTIFIED ON MLG DOOR . THE SPECIFIC AREA OF THE CRACK WAS ON CROSSMEMBER. MLG DOOR HAS BEEN REPLACED IAW AMM WITH SERVICEABLE PART.Dec 16, 2014 · Cndair CL6002D24 · Landing Gear DoorsSDR REXA2014121401207Hinge Bracket · wornTASK CARD 900-71-440-100 RT ENG FWD LOWER CORE COWL BLOW OFF DOOR HINGE BRACKET WORN. R & R RT ENG BLOW OFF DOOR HINGE BRACKET & HINGE LEVER IAW SRM 51-42-20-001-001-A01, AMM 71-12-05-05-400-801-A01 & SRM 51-41-02-001-001-A01.Dec 14, 2014 · N904XJ · Cndair CL6002D24 · Engine Cowling SystemSDR CA141215001Bolt · sheared(CAN) DURING THE ACCOMPLISHMENT OF TASK RJ9-52-830-500 - DETAILED INSPECTION OF THE PASSENGER DOOR INTERNAL STRUCTURE - IT WAS REPORTED THAT ON THE UPPER LATCH AFT FITTING, THE ATTACHMENT BOLT HEAD WAS FOUND SHEARED FROM CORROSION.Dec 9, 2014 · Cndair CL600* · Passenger/Crew DoorsSDR SWIA201440169Pin · unserviceableRT ENGINE VIBRATION REACHED 5.2 AT FL 360. REPLACED FAN BLADE PINS WITH SERVICEABLE UNITS. LUBED FAN BLADE TANGS AND REINSTALLED ORIGINAL SET OF FAN BLADES IAW ENGINE MANUAL.Nov 26, 2014 · N802SK · Cndair CL6002D24 · Turbine Engine Compressor SectionSDR CA141126004Windscreen · failed(CAN) WHILE IN CRUISE THE LEFT HAND WINDSHIELD SHATTERED (OUTER LAYER). THE CREW CARRIED OUT THE QRH AND DESCENDED TO FL100. FLIGHT LANDED AT DESTINATION WITHOUT FURTHER ISSUE.Nov 25, 2014 · Cndair CL600* · Flight Compartment WindowsSDR CA141126005Roller · missing(CAN) IN THE CLIMB AT 4000 FEET THE CREW RECEIVED A FLAP FAIL CAUTION MESSAGE. THE FLAPS INDICATED ZERO HOWEVER VISUAL INSPECTION SHOWED THEM SLIGHTLY EXTENDED. CREW CONTINUED TO DESTINATION AT A LOWER ALTITUDE AND SLOWER AIRSPEED. MAINTENANCE INVESTIGATION FONov 25, 2014 · Cndair CL600* · Trailing Edge FlapsSDR REXA2014111101135Tab · damagedTASK CARD 900-26-440-100 NR 2 ENG AFT CORE COWL STANDOFF BLOCK AT 9 O'CLOCK POSITION SHOWS DAMAGE TO ALIGNMENT TAB. R & R IAW SRM 54-13-00-201-002-A01 & SRM 51-42-06-001-001-A01.Nov 11, 2014 · N902XJ · Cndair CL6002D24 · Engine Cowling SystemSDR REXA2014111001131Tab · damagedTASK CARD 900-26-430-100 NR 1 ENG AFT CORE COWL SHOWS DAMAGE TO STANDOFF BLOCK ALIGNMENT TAB AT 3 O'CLOCK POSITION. R & R IAW SRM 54-13-00-201-002-A01.Nov 10, 2014 · N902XJ · Cndair CL6002D24 · Engine Cowling SystemSDR MASA2014110202715Fadec · warning messageRT FADEC CAUTION IN FLIGHT, RETURNED TO DEPARTURE AND A EMERGENCY WAS DECLARED. REPLACED RT FADEC.Nov 2, 2014 · N932LR · Cndair CL6002D24 · Fuel Controlling SystemSDR CA141030009Actuator · failed(CAN) SLATS DID NOT EXTEND WHEN SELECTED FOR LANDING. MDC INDICATED "SLAT ACTUATOR SYSTEM FAILED MECHANICAL JAM." DURING SUBSEQUENT MAINTENANCE ACTION, SERVICE LETTER 27-074 REV. A WAS CARRIED OUT. THIS ACTUATOR FAILED TORQUE TEST AND WAS REPLACED.Oct 30, 2014 · Cndair CL600* · Leading Edge Slat ActuatorSDR CA141028008Bleed Valve · malfunctioned(CAN) RT BLEED CAUTION, RT VALVE WILL NOT CLOSE WHEN SELECTED FOR DEICING. RIGHT BLEED VALVE REPLACED IAW AMM 36-12-01. ENGINE RUN UP COMPLETED BLEED VALVES OPERATE NORMALLY.Oct 28, 2014 · Cndair CL600* · Compressor Bleed ValveSDR CA141027003Windshield · fractured(CAN) IN CRUISE, FLIGHT CREW REPORTED A SHATTERED RT WINDSHIELD. DECISION WAS TAKEN TO DESCEND TO A LOWER FLIGHT LEVEL AND CONTINUE TO DESTINATION. UPON ARRIVAL, ACFT WAS REMOVED FROM SERVICE AND MAINTENANCE CONFIRMED THE OUTER PLY WAS FRACTURED. THE RT WINOct 27, 2014 · Bombdr CL6002D15 · Flight Compartment WindowsSDR CA141204017Shroud · failed(CAN) HP DUCTS HAVE BEEN INSPECTED FOR THE FIRST TIME (10 000 FH) BY AIR NOSTRUM IN OCTOBER AND ROUGHLY 80% OF THE DUCTS ARE FAILING THE AMM CHECK BECAUSE OF EXCESSIVE LEAKAGE OF THE EXTERNAL SHROUD. SSP EVALUATION CONFIRMED THAT THE DUCTS ARE LEAKING EXCESSIVOct 24, 2014 · Cndair CL600* · Pneumatic Distribution SystemSDR REXA2014102301098Plate · chafedTASK CARD 900-71-430-100 1 ENG LOWER & UPPER FWD CORE COWL SHOWS CHAFE DAMAGE TO LOWER & UPPER DOUBLER PLATE WHERE THE BLOW OFF DOORS LATCH CATCHES. DOOR MUST BE OPEN TO SEE. REPAIRED NR 1 ENG LOWER & UPPER FWD CORE COWL BLOW OFF DOOR CATCH REINFORCING PADS Oct 23, 2014 · N901XJ · Cndair CL6002D24 · Engine Cowling SystemSDR REXA2014101101049Fireshield · peelingTASK CARD 900-54-440-301 RIGHT ENG LOWER FWD CORE COWL FIRE SHIELD PEELING UP, TYPICAL LOCATION. REPAIRED RT ENG LOWER FWD CORE COWL IAW EO R54090.Oct 11, 2014 · N937XJ · Cndair CL6002D24 · Engine FiresealsSDR CA141015004Clamp · torn(CAN) AFTER DEPARTURE AND GEAR UP THE NO 2A HYD PUMP CAUTION LIGHT CAME ON AND SYSTEM QTY WENT TO 0% MAINTENANCE FOUND LEAK AT FLEXIBLE LINE (REF IPC 29-17-06, FIG. 1C, ITEM 128) FROM IB AFT NR 2 PYLON DOWN TO THE HYDRAULIC DAMPENER. THE SADDLE CLAMP P/N BBDREOct 10, 2014 · Cndair CL600* · Nacelle/Pylon, Main FrameSDR REXA2014100801043Block · wornTASK CARD CRJ900 C1 NR 1 ENG AFT CORE COWL ALIGNMENT STANDOFF BLOCK AT 3 O'CLOCK POSITION SHOWS WEAR DAMAGE TO ALIGNMENT TAB. R & R NR 1 ENG AFT COWL ALIGNMENT BLOCK IAW SRM 54-13-00-201-002-A01.Oct 8, 2014 · N937XJ · Cndair CL6002D24 · Engine Cowling SystemSDR REXA2014100801044Block · wornTASK CARD NR 2 ENG AFT CORE COWL ALIGNMENT STANDOFF BLOCK AT 9 O'CLOCK POSITION SHOWS WEAR DAMAGE TO ALIGNMENT TAB. R & R STANDOFF BLOCK IAW SRM 54-13-00-201-0025-A01.Oct 8, 2014 · N937XJ · Cndair CL6002D24 · Engine Cowling SystemSDR REXA2014100801045Cowling · wornTASK CARD CRJ900 C1 NR 1 ENG AFT CORE COWL SHOWS WEAR DAMAGE AT PYLON INTERFACE AREA. REPAIRED NR 1 ENG AFT CORE COWL AT PYLON INTERFACE IAW SRM 54-13-00-201-006-A01.Oct 8, 2014 · N937XJ · Cndair CL6002D24 · Engine Cowling SystemSDR REXA2014100801046Cowling · wornTASK CARD CRJ900 C1 NR 2 ENG AFT CORE COWL SHOWS WEAR DAMAGE AT PYLON INTERFACE AREA. REPAIRED NR 2 ENG AFT CORE COWL AT PYLON INTERFACE IAW SRM 54-13-00-201-006-A01 BY INSTALLATION OF RUB STRIPS.Oct 8, 2014 · N937XJ · Cndair CL6002D24 · Engine Cowling SystemSDR CA140919002Wire · failed(CAN) DURING TROUBLESHOOTING OF AN INOPERATIVE AUXILIARY POWER UNIT (APU) ASSOCIATED WITH AN APU FAULT CAUTION MESSAGE, SIGN OF OVERHEATING CONDITION WAS NOTICED AT THE APU STARTER POSITIVE ELECTRICAL LUG. AIRCRAFT DEFERRED IN ACCORDANCE WITH MEL 49-10-01-1.Sep 19, 2014 · Cndair CL600* · APU System WiringSDR REXA2014091300975Nozzle · gougedTASK CARD 900-26-440-100 NR 2 ENG EXHAUST NOZZLE PYLON INTERFACE GOUGED & NEEDS TYPICAL REPAIR. REPAIRED NR 2 ENG EXHAUST NOZZLE IAW SRM 54-13-00-201-006-A01.Sep 13, 2014 · N935XJ · Cndair CL6002D24 · Engine Collector/Tailpipe/NozzleSDR CA140912010Wire Harness · damaged(CAN) DURING TAXI OUT, SMOKE IN THE CABIN WAS DETECTED. THE CREW DECIDED TO RETURN TO GATE FOR PROBLEM RESOLUTION. MAINTENANCE FOUND THE ORIGIN OF THE SMOKE WAS A PROBLEM WITH AN ELECTRICAL WIRE ASSEMBLY BEHIND THE NR 2 GALLEY. ROOT CAUSE UNDER INVESTIGATISep 9, 2014 · Cndair CL6002D24 · Equipment/Furnishings WiringSDR CA140917010Pressure Switch · failed(CAN) DURING TAXI-OUT THE LH ENGINE EICAS MESSAGE "PRESS L ENG" REMAINED. THE FLIGHT CREW RETURNED TO GATE. MAINTENANCE REPLACED THE LOW OIL PRESSURE SWITCH WITH NO FURTHER ISSUES.Sep 7, 2014 · Cndair CL6002D24 · Engine Oil Indicating SystemSDR WVER2014090590601Skin · crackedTHE TRANSCOWL SKIN UNDER THE EXTRUSION NEAR LATCH IS CRACKED AROUND 2 FASTENER HOLES.Sep 5, 2014 · N906F · Cndair CL6002D24 · Nacelle/Pylon, Plate/SkinSDR REXA2014082700869Fireshield · damagedLEFT ENG LOWER CORE COWL INNER SKIN FIRE SHIELD SHOWS WEAR & CHAFFING AROUND FWD CUT OUT APPROX 6 O'CLOCK POSITION TYPICAL. REPAIRED IAW EO R54090.Aug 27, 2014 · N934XJ · Cndair CL6002D24 · Engine FiresealsSDR REXA2014082700870Fireshield · damagedLEFT ENG LOWER CORE COWL FIRE SHIELD HAS A PEELED & BENT CORNER MIDDLE OF COWLING. REPAIRED IAW EA CRJ954-02862.Aug 27, 2014 · N934XJ · Cndair CL6002D24 · Engine FiresealsSDR CA140818007Gasket · failed(CAN) ENROUTE, CREW ADVISED DISPATCH THEY HAD HYDRAULIC ENGINE DRIVEN PUMP 2A CAUTION MESSAGE AND NEEDED TO DESCEND TO FL 260. HALF HOUR LATER THEY ADVISED THEY HAD LOST NUMBER TWO HYDRAULIC SYSTEM. CREW DECLARED AN EMERGENCY WITH ATC. FLIGHT SUCCESSFULLY LANDAug 15, 2014 · Cndair CL600* · Hydraulic Pump (Electric/Engine), MainSDR REXA2014081200826Cowling · chafedLEFT ENG AFT CORE COWL HAS CHAFE DAMAGE BETWEEN COWL & PYLON INTERFACE. REPAIRED LT ENG AFT CORE COWL IAW SRM 54-13-00-201-006-A01. NO FURTHER DAMAGE.Aug 12, 2014 · N933XJ · Cndair CL6002D24 · Engine Cowling SystemSDR REXA2014081200828Fireshield · chafedRIGHT ENG LOWER CORE COWL HAS CHAFE DAMAGE ON FIRE SHIELDS IN THE DRAIN STARTER ACCESS PANEL, WITHIN REPAIR LIMITS OF R54090. REPAIRED DAMAGE TO RT LOWER CORE COWL FIRE SHIELD IAW EO R54090.Aug 12, 2014 · N933XJ · Cndair CL6002D24 · Engine FiresealsSDR CA140812004Engine · shutdown(CAN) DURING TAXI THE RT ENGINE DID AN AUTO SHUTDOWN. THE ITT BRIEFLY REACHED 1049. NEITHER ENGINE WAS AT POWER (9 KNOTS AT THE TIME OF THE EVENT) THE ENGINE HAD BEEN INSTALLED THE NIGHT BEFORE ROOT CAUSE UNDER INVESTIGATION.Aug 7, 2014 · Cndair CL6002D24 · Engine (Turbine/Turboprop)SDR CA140805005Pulley · seized(CAN) THE FLIGHT CREW REPORTED THAT THE ROLL CONTROL WAS STIFF IN FLIGHT FOR BOTH LT AND RT TURNS. MAINTENANCE INVESTIGATION FOUND A SEIZED PULLEY IN THE AILERON CIRCUIT AT THE LT WING ROOT. THE PULLEY WAS REPLACED AND SYSTEM TESTED SERVICEABLE.Aug 1, 2014 · Cndair CL600* · Aileron Control SystemSDR REXA2014071500719Fireshield · damagedTASK CARD 90-26-440-100 NR 2 ENG LOWER CORE COWL FIRE SHIELD BETWEEN DRAIN PAN & ACOC VENT. REPAIRED NR 2 ENG LOWER CORE COWL FIRE SHIELD CHAFE IAW EO R54090.Jul 15, 2014 · N931XJ · Cndair CL6002D24 · Engine FiresealsSDR CA140729004Selector Valve · malfunctioned(CAN) GEAR DISAGREE ON GEAR DOWN SELECTION., WHITE LIGHTS ON INITIAL , RE-SELECT HAD NO LIGHTS , THEN ALTERNATE EXTENSION THEY GOT ALL GREEN. REPLACED GEAR SELECTOR VALVE IAW AMM 32-32-10 GEAR SWING C/O NFF. ACFT RETURNED TO SERVICE.Jul 10, 2014 · Cndair CL600* · Landing Gear Retraction/Extension SystemSDR SWIA201438654Bushing · galledRIGHT ENGINE FWD YOKE MOUNT LINK AND CLAMP-UP BUSHING GALLED AND SCORED AND BUSHING IS MIGRATED. REMOVED RT ENGINE FWD YOKE MOUNT LINK AND CLAMP-UP BUSHING AND REPLACED WITH A SERVICEABLE LINK AND CLAMP-UP BUSHING IAW AMM.Jul 9, 2014 · N822SK · Cndair CL6002D24 · Engine Mount SectionSDR CA140709003Windshield · arced(CAN) ARCING ON THE ELECTRICAL HEATING SYSTEM ON LT WINDSHIELD.Jul 7, 2014 · Cndair CL6002D24 · Flight Compartment WindowsSDR CA140710001Seal · failed(CAN) AFTER TAKEOFF, DURING THE CLIMB PHASE OF FLIGHT, THE MAIN CABIN DOOR BEGAN SQUEALING. THE FLIGHT CREW DECIDED TO RETURN TO THE POINT OF DEPARTURE. AFTER ARRIVING, MAINTENANCE ACTION FOUND THAT THE MCD SEAL WAS RIPPED AT THE LOWER, FORWARD CORNER OF THE DJul 2, 2014 · Cndair CL600* · Passenger/Crew DoorsSDR REXA2014063000660Fireshield · gougedTASK CARD 900-54-430-301 LT ENG LOWER COWL HEAT AROUND VENT PANEL HAS MINOR GOUGES. REPAIRED LT ENG COWL FIRE SHIELD IAW EO R54090.Jun 30, 2014 · N930XJ · Cndair CL6002D24 · Engine FiresealsSDR REXA2014063000661Fireseal · wornTASK CARD 900-54-440-301 RT ENG LOWER COWL METAL FIRE SEAL ABOVE DRAIN MAST IS WORN THROUGH. REPAIRED RT COWL FIRE SEAL IAW EO 54090.Jun 30, 2014 · N930XJ · Cndair CL6002D24 · Engine FiresealsSDR REXA2014062800659Heat Shield · bentTASK CARD 900-54-430-301 LT ENG LOWER COWL HEAT SHIELD AFT OF BLOW OUT DOOR HAS A TAB THAT IS BENT UP. REPAIRED HEAT SHIELD ON AFT SECTION OF LOWER CORE COWL IAW EA CRJ954-02711.Jun 28, 2014 · N930XJ · Cndair CL6002D24 · Engine FiresealsSDR REXA2014062700657Structure · wornTASK CARD 900-26-430-100 NR 1 ENG AFT CORE COWL HAS WEAR MARKS AT PYLON INTERFACE AREA. REPAIRED NR 1 ENG AFT CORE COWL PYLON INTERFACE AREA IAW SRMM 54-13-00-101-001-A01 & 54-13-00-201-006-A01.Jun 27, 2014 · N930XJ · Cndair CL6002D24 · Engine Cowling SystemSDR REXA2014062700658Cowling · wornTASK CARD 900-26-440-100 NR 2 ENG AFT CORE COWL HAS WEAR MARKS AT PYLON INTERFACE AREA. REPAIRED NR 2 ENG AFT CORE COWL PYLON INTERFACE AREA IAW SRM 54-13-00-101-001-A01 & 54-13-00-201-006-A01.Jun 27, 2014 · N930XJ · Cndair CL6002D24 · Engine Cowling SystemSDR REXA2014062600651Plate · damagedTASK CARD 900-71-430-100 LT ENG LOWER BLOW OFF DOOR LATCH DIGGING INTO METAL. REPAIRED LT ENG LOWER BLOW OFF DOOR STRIKE PLATE IAW EA CRJ954-02716.Jun 26, 2014 · N930XJ · Cndair CL6002D24 · Engine Cowling System
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