GE CF34-8C1

Service difficulty reports · 1,415

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 = 'CF348C1'
  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 CA030715002Servo · defective(CAN) PILOT YOKE BINDING DURING APPROACH. USING PITCH DISCONNECT HANDLE, COPILOT YOKE FELT NORMAL. FORCE FELT LIGHTER AS FLAPS EXTENDED. AUTOPILOT DISCONNECTED TO VERIFY A FLAP INDICATION AT A LOWER ALT & GREATER THAN NORM FORCE REQUIRED TO MOVE YOKE FORWARD. Jul 15, 2003 · Cndair CL6002C10 · Autopilot Main ServoSDR SW07200300006Turbine Blades · missingWHILE INVESTIGATING A HIGH PEAK VIBRATION WHICH WAS DISCOVERED BY ECTM, THE MAINTENANCE PERSONNEL PERFORMED A BOROSCOPE INSPECTION AND FOUND BLADES MISSING FROM THE 2ND STAGE HIGH PRESSURE TURBINE WHEEL.Jun 11, 2003 · N508MJ · Cndair CL6002C10 · Turbine SectionSDR SW07200300005Turbine Blades · missingTHE MAINTENANCE PERSONNEL DISCOVERED 2ND STAGE HIGH PRESSURE TURBINE BLADES MISSING FROM THE TURBINE WHEEL.Jun 6, 2003 · N504MJ · Cndair CL6002C10 · Turbine SectionSDR CA030530014Loop · failed(CAN) CREW EXPERIENCED A LT BLEED DUCT WARNING MSG ON CLIMB OUT THRU 23,000 FT. LT PACK WENT OFF LINE & APPROX. 30 SECONDS LATER, RT PACK WENT OFF LINE. CREW WERE UNABLE TO RESET THIS CONDITION IN AIR. AC DIVERTED. TROUBLESHOOTING, MAINT LT BLEED LOOP B HIGHMay 28, 2003 · Cndair CL6002C10 · Overheat DetectionSDR CA031001002Windshield · cracked(CAN) RT COCKPIT WINDOW CRACKED DURING DESCENT AT 18000 FT. AIRPLANE FERRIED FOR WINDOW REPLACEMENT.May 18, 2003 · Cndair CL6002C10 · Flight Compartment WindowsSDR SW07200300004Turbine Blades · damagedWHILE PERFORMING A BOROSCOPE INSPECTION AFTER A PEAK VIBRATION, THE MAINTENANCE PERSONNEL DISCOVERED 2ND STAGE HIGH PRESSURE TURBINE BLADES DAMAGE.May 16, 2003 · N508MJ · Cndair CL6002C10 · Turbine SectionSDR SW07200300003Turbine Blades · damagedBOROSCOPE INSPECTION WAS REQUIRED BECAUSE OF VIBRATION PEAK. THE INSPECTION REVEALED DAMAGE HIGH PRESSURE TURBINE FAILURE.May 8, 2003 · N503MJ · Cndair CL6002C10 · Turbine SectionSDR SW07200300002Turbine Blades · missingBOROSCOPE INSPECTION REVEALED THE LOSS OF HIGH PRESSURE TURBINE BLADES.Apr 16, 2003 · N504MJ · Cndair CL6002C10 · Turbine SectionSDR SW07200300001Turbine Blades · damagedTHE CREW REPORTED N2 VIBRATION AFTER WHICH THE MAINTENANCE PERSONNEL PERFORMED A BOROSCOPE INSPECTION WHERE THEY DISCOVERED THE HIGH PRESSURE TURBINE BLADE DAMAGE.Apr 16, 2003 · N506MJ · Cndair CL6002C10 · Turbine SectionSDR CA030406002Window · cracked(CAN) CREW REPORTED THAT CAPTAINS SIDE WINDOW CRACKED AT 30,000 FT. FOLLOWING THE WINDOW REPLACEMENT, THE AIRCRAFT RETURNED TO SERVICE.Apr 2, 2003 · Cndair CL6002C10 · Flight Compartment WindowsSDR CA030330001Circuit Breaker · shorted(CAN) IN CRUISE, THE FLIGHT CREW REPORTED A CROSSFLOW PUMP CAUTION MESSAGE ALONG WITH AUTO CROSSFLOW INHIBIT STATUS MESSAGE. SHORTLY AFTER, THE FUEL IMBALANCE CAUTION MESSAGE APPEARED. A 500 KG IMBALANCE DEVELOPED. THE TANKS READOUT WAS LT 2300, CTR 0, RT 1Mar 27, 2003 · Cndair CL6002C10 · Fuel System WiringSDR CA030314001Computer · failed(CAN) DIS-DURING CLIMB OUT CREW NOTED CAPT/FO ALT GO BLANK. CREW ELECTED TO RETURN TO AIRPORT. NOTE ON THEWAY TO AIRPORT SYSTEM CAME BACK ON LINE. CREW CONTINUED TO AIRPORT TO HAVE MTX CHECK OUT SYSTEM. A/C LANDED SAFELY NO FURTHER INCIDENTS WERE REPORTED. FOMar 13, 2003 · Cndair CL6002C10 · Air Data ComputerSDR ASOA03098Engine · malfunctionedDURING APPROACH INTO DAB FROM ATL, THE LT ENGINE COMPRESSOR STALLED THREE TIMES WITH AIR SPEED OF 180 KTS AT APPROX 4,000 FEET AND FLAPS SELECTED AT 8 DEGREES. THE CREW REDUCED THE POWER ON THE LEFT ENGINE TO IDEL AND THEN AN AMBER LEFT FULL AUTHORITY DIGITAL Mar 10, 2003 · N708EV · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR CA030314002Windshield · cracked(CAN) CREW NOTED THE CAPTAIN'S SIDE WINDOW HAD CRACKED. MAINTENANCE REMOVED AND REPLACED THE CAPTAIN'S SIDE WINDOW WITH SERVICEABLE UNIT.Mar 9, 2003 · Cndair CL6002C10 · Flight Compartment WindowsSDR CA030312006Window · cracked(CAN) AT FL340, CO-PILOTS WINDOW CRACKED. TWO CRACKS OF AROUND 30CM IN AFT PORTION OF WINDOW. DURING APPROACH, WINDOW CRACK FURTHER EXTEND TOTALLY FROM FRONT TO REAR. FOUND MIDDLE AND INNER PLY CRACKED. WINDOW REPLACED.Mar 7, 2003 · Cndair CL6002C10 · Flight Compartment WindowsSDR CA030312005Window · cracked(CAN) FLIGHTDECK LT SIDE WINDOW CRACKED. WINDOW ASSEMBLY REPLACED.Feb 28, 2003 · Cndair CL6002C10 · Flight Compartment WindowsSDR CA030313001Windshield · failed(CAN) RT WINDSHIELD SHATTERED ON TAXI OUT AT CINCINNATI. REMOVED P/N NP139321-10, S/N 02074H1855 (781.7 HOURS AND 576 CYCLES)INSTALLED S/N 99014H6982(SEE ALSO: US NR 2003030500013)Feb 27, 2003 · Cndair CL6002C10 · Flight Compartment WindowsSDR CA040204013Light · shorted(CAN) CREW REPORTED SMOKE/SPARKS FROM CO-PILOTS FLOOD LIGHTS ON SIDE PANEL BELOW BASE OF WINDSHIELD WITH BURN MARKS ON PLASTIC AREA AT BASE OF W/S AND SIDE WINDOW. REMOVED AND REPLACED F/OS MIDDLE FLOOD LIGHT ASSY IAW AMM 33-11-03 AND OPS CHECKED SERVICEABLE.Feb 26, 2003 · Cndair CL6002C10 · Flight Compartment LightingSDR QXEA0300293Blade · brokenENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND FOUR BLADES BROKEN. REPLACED ENGINE. AIRCRAFT OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. INVESTIGATION BY THE ENGINE MANUFACTURER (GE) HAS BEEN COMPLETED. ITFeb 18, 2003 · N607QX · Cndair CL6002C10 · Turbine Engine Compressor SectionSDR QXEA0300250Blade · missingPDX - NR1 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND FOUR MISSING BLADES AND SIX BLADES HAVE TRAILING EDGE DAMAGE. REPLACED ENGINE. AIRCRAFT OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. INVESTIGATION Feb 12, 2003 · N603QX · Cndair CL6002C10 · Turbine Engine Compressor SectionSDR QXEA0300251Blade · missingPDX - NR 2 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND ONE BLADE MISSING AND FOUR BLADES HAVE TRAILING EDGE DAMAGE. REPLACED ENGINE. AIRCRAFT OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. INVESTIGATION BYFeb 12, 2003 · N612QX · Cndair CL6002C10 · Turbine Engine Compressor SectionSDR QXEA0300252Blade · brokenPDX - NR 1 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND ONE BLADE BROKEN OFF. REPLACED ENGINE. AIRCRAFT OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. NVESTIGATION BY THE ENGINE MANUFACTURER (GE) HAS BEEN CFeb 12, 2003 · N614QX · Cndair CL6002C10 · Turbine Engine Compressor SectionSDR QXEA0300247Blade · missingNR 2 ENGINE FAILED SCHEDULED BORESCOPE. FOUND ONE BLADE MISSING FROM HP TURBINE. REPLACED ENGINE. AIRCRAFT OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. INVESTIGATION BY THE ENGINE MANUFACTURER(GE) HAS BEEN COMPLEFeb 10, 2003 · N611QX · Cndair CL6002C10 · Turbine Engine Compressor SectionSDR QXEA0300246Blade · missingNR 1 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND FOUR BLADES MISSING FROM HP TURBINE. REPLACED ENGINE. AIRCRAFT OPERATION CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. INVESTIGATION BY THE ENGINE MANUFACTURER (GE) HFeb 10, 2003 · N611QX · Cndair CL6002C10 · Turbine Engine Compressor SectionSDR QXEA0300244Blade · brokenNR 1 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND TWO BLADES BROKEN, ANOTHER WITH POSSIBLE CRACK. REPLACED ENGINE. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE.Feb 8, 2003 · N610QX · Cndair CL6002C10 · Turbine Engine Compressor SectionSDR QXEA0300245Blade · brokenNR 2 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND THREE BROKEN BLADES, ANOTHER WITH MATERIAL MISSING AND SEVERAL OTHERS WITH SMALL NICKS IN TIPS. REPLACED ENGINE. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION ATFeb 8, 2003 · N610QX · Cndair CL6002C10 · Turbine Engine Compressor SectionSDR QXEA0300248Blade · missingNR 2 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND ONE BLADE MISSING. REPLACED ENGINE. AIRCRAFT OPERATIONAL CHECKED GOOD. AIRCRAFT OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. INVESTIGATION BY THE ENGINE MANUFeb 6, 2003 · N608QX · Cndair CL6002C10 · Turbine Engine Compressor SectionSDR QXEA0300230Blade · missingNR 1 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND TWO BLADES MISSING. REPLACED ENGINE. AIRCRAFT OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. INVESTIGATION BY THE ENGINE MANUFACTURER (GE) HAS BEEN COMPLETEFeb 3, 2003 · N605QX · Cndair CL6002C10 · Turbine Engine Compressor SectionSDR QXEA0300217Blade · crackedPDX - NR 2 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND TWO HPT 1 BLADES BROKEN, TWO BLADES CRACKED AND SOME WITH COLLATERAL DAMAGE. REPLACED ENGINE. AIRCRAFT OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE.Jan 30, 2003 · N603QX · Cndair CL6002C10 · Turbine Engine Compressor SectionSDR QXEA0300129Turbine Blades · damagedPDX - NR 1 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND TWO HPT 1 BLADES 2/3 MISSING. REPLACED ENGINE. AIRCRAFT OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. INVESTIGATION BY THE ENGINE MANUFACTURER (GEJan 28, 2003 · N609QX · Cndair CL6002C10 · Turbine SectionSDR QXEA0300103Turbine Blades · damagedPDX - NR 1 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND TWO HPT BLADES 1/3 MISSING. REPLACED ENGINE. AIRCRAFT OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. INVESTIGATION BY THE ENGINE MANUFACTURER (GE) Jan 20, 2003 · N604QX · Cndair CL6002C10 · Turbine SectionSDR QXEA0300082Turbine Blades · damagedPDX - NR 1 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND ONE HPT 1 BLADE 2/3 MISSING AND TWO BLADES CRACKED. REPLACED ENGINE. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. INVESTIGATION BY THE ENGINE MANJan 14, 2003 · N601QX · Cndair CL6002C10 · Turbine SectionSDR CA030119001Line · cracked(CAN) WHEN A/C WAS BEING FUELED, CENTER TANK WAS FILLED TO 2000 LBS AND WINGS FILLED TO 5500 LBS. ALSO CREW GOT A FUEL IMB CAUTION ON CLIMB OUT ABOUT 5 MIN AFTER TAKE OFF. USED PUMPS AND GRAVITY TO REMOVE FUEL FROM CENTER TANK ASSY. INSPECTED LT CENTER TANK Jan 11, 2003 · Cndair CL6002C10 · Aircraft Fuel Distribution SystemSDR QXEA0300015Turbine Blades · damagedCKB - NR 2 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND ONE BLADE WITH MISSING MATERIAL. REPLACED ENGINE. AIRCRAFT OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVETIGATION AT GE.INVESTIGATION BY THE ENGINE MANUFACTURER (GE) HAJan 6, 2003 · N602QX · Cndair CL6002C10 · Turbine SectionSDR CA030104001Line · cracked(CAN) IN CRUISE, CREW RECEIVED SEVERAL FUEL IMBALANCE MESSAGES THAT THE CREW WAS ABLE TO CORRECT, CENTER TANK FILED WITH FUEL VERY RAPIDLY. DISPATCH AND MOC CONCURRED WITH THE CREW TO LAND AT THE NEAREST AIRPORT. NO EMERGENCY WAS DECLARED BUT CFR DID ROLL DO Jan 4, 2003 · Cndair CL6002C10 · Aircraft Fuel Distribution SystemSDR QXEA0300014Turbine Blades · damagedPDX - NR 2 ENGINE FAILED SCHEDULED BORESCOPE INSPECTION. FOUND ONE HPT 1 BLADE MISSING 20 PERCENT SPAN. REPLACED ENGINE. OPERATIONAL CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. INVESTIGATION BY THE ENGINE MANUFACTURER (GDec 30, 2002 · N606QX · Cndair CL6002C10 · Turbine SectionSDR CA021222001Tube · cracked(CAN) DURING MAINT. IT WAS OBSERVED THAT FUEL WAS GETTING INTO THE CENTER TANK (CTR. TANK QUANTITY INCREASE OVER TIME) WHEN EVER THE BOOST PUMPS WERE SELECTED ON. INVESTIGATION BY MAINT. IDENTIFIED A CRACK ON TUBE CC670621042 LOCATED IN THE RT SIDE OF THE CENDec 19, 2002 · Cndair CL6002C10 · Aircraft Fuel Distribution SystemSDR CA021228001Fitting · leaking(CAN) ON APPROACH, AFTER GEAR DOWN SELECTION AND GEAR DOWN INDICATION, MESSAGE HYD 3 LOW PRESS (C) WITH LOSS OF HYDRAULIC 3 QUANTITY. HYDRAULIC PUMP 3A AND 3B SHUT DOWN AND AIRCRAFT LANDED SAFELY. MECHANICS FOUND THAT THE LEAK WAS COMING FROM ONE OF THE FLEXIDec 19, 2002 · Cndair CL6002C10 · Landing Gear Retraction/Extension SystemSDR CA021222002Windshield · cracked(CAN) LT WINDSHIELD CRACKED DURING APPROACH AT FL80, IAS 220 KNOTS. WINDSHIELD WAS REMOVED AND REPLACED PER AMM.Dec 18, 2002 · Cndair CL6002C10 · Flight Compartment WindowsSDR CA021218003Window · cracked(CAN) CO-PILOT SIDE WINDOW CRACKED IN FLIGHT. CAUSE UNKNOWN. UNEVENTFUL LANDING MADE AT CYMX. WINDSHIELD REMOVED AND NEW WINDSHIELD INSTALLED. NO MORE PROBLEM FOUND.Dec 16, 2002 · Cndair CL6002C10 · Flight Compartment WindowsSDR QXEA0202149Turbine Blades · damagedPDX - DURING SCHEDULED BORESCOPE INSPECTION FOUND TOP ONE THIRD OF THREE TURBINE BLADES IN THE HPT DISK MISSING. REPLACED ENGINE. REPLACED ENGINE. OPERATIONAL OF AIRCRAFT CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. ENGINE UNDER INVESTIGATION AT GE. INVESTIGATIDec 8, 2002 · N607QX · Cndair CL6002C10 · Turbine SectionSDR CA021129005Fitting · cracked(CAN) DURING A SCHEDULE DOWN TIME FOR EICAS 5 MOD PROGRAM FOUND CRACKED FITTING HINGE AT RT INBOARD WS 185.11, THE PART WAS REPLACED BY A NEW ONE AND THE CRACKED FITTING WAS SHIPPED FOR ANALYSIS.Nov 29, 2002 · Cndair CL6002C10 · Drag Control SystemSDR CA021112006Windshield · failed(CAN) COPILOT SIDE WINDOW MIDDLE LAYER SHATTERED (CRACKED) WHILE AIRCRAFT WAS ON APPROACH . UNEVENTFUL LANDING COMPLETED AFTER USUAL QRH PROCEDURES FOLLOWED. NO GAP FOUND AROUND CONTOUR AT REMOVAL OF WINDSHIELD. PART REPLACED BY NEW ONE. CONDITIONS: 1700Z, VMCNov 8, 2002 · Cndair CL6002C10 · Flight Compartment WindowsSDR CA021025003Window · cracked(CAN) FIRST OFFICER'S SIDE WINDOW CRACKED (INNER PANE) DURING CRUISE ENROUTE . WINDOW WAS REMOVED AND REPLACED WITH SERVICABLE COMPONENT.Oct 24, 2002 · Cndair CL6002C10 · Flight Compartment WindowsSDR CA021025004Window · cracked(CAN) FIRST OFFICER'S SIDE WINDOW CRACKED (INNER PANE) DURING DESCENT . WINDOW WAS REMOVED AND REPLACED WITH SERVICABLE COMPONENT.Oct 17, 2002 · Cndair CL6002C10 · Flight Compartment WindowsSDR CA021025005Window · cracked(CAN) CAPTAIN SIDE WINDOW CRACKED DURING DESCENT . WINDOW WAS REMOVED AND REPLACED WITH SERVICABLE COMPONENT.Oct 16, 2002 · Cndair CL6002C10 · Flight Compartment WindowsSDR QXEA0201678Pump · obstructedBOI - ABORTED TAKEOFF. TAKEOFF RPM (N1) ON NR 1 ENGINE APPROXIMATELY 10 PERCENT BELOW REQUIRED INDICATION, FADEC CALLED FOR 88.2 PERCENT, N1 INDICATOR SHOWED APPROXIMATELY 76.3 PERCENT. REMOVED OBSTRUCTION FROM MAIN FUEL PUMP INLET AND REINSTALLED. GROUND RAN,Oct 14, 2002 · N612QX · Cndair CL6002C10 · Engine Fuel PumpSDR CA021015003Bulkhead · cracked(CAN) THE NR 2 HYDRAULIC EDP PRESSURE LINE WAS LOOSE FROM THE BACK OF THE PRESSURE BULKHEAD, DECIDED TO OPEN THE CARGO AREA TO SEE IF IT COULD BE RETORQUED. HOLE ON THE PRESSURE BULKHEAD WAS ELONGATED AND THREAD OF THE HYDRAULIC FITTING WERE WORN NDT INSPECTOct 13, 2002 · Cndair CL6002C10 · Fuselage Main, BulkheadSDR QXEA0201682Intake · gougedPDX - TWO GOUGES IN FORWARD AIR FLOW PATH AROUND 713C LOOKING AFT OF NR 2 ENGINE. REPAIRED IAW TASK 70-42-00-350-002, SECTION 2, CHAPTER 70-42-00, PAGE 2 OF GE STANDARD PRACTICES.Oct 12, 2002 · N613QX · Cndair CL6002C10 · Engine Air Intake SystemSDR CA021017001Bulkhead · cracked(CAN) DURING INCORPORATION OF THE SB 670BA3-003 FOUND FOUR (4) CRACKS IN THE AFT PRESURE BULKHEAD WEB FS=1098.2, STR 8-9 LT AND RT. THE CRACKS ARE CONCENTRATED AROUND THE HOLES IN THE WEB FOR THE HYDRAULIC LINES (SEE ATTACHED DIGITAL PHOTOS). LHS-TWO CRACKS, Oct 11, 2002 · Cndair CL6002C10 · Fuselage Main, Bulkhead
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