GE CF6-50C2

Service difficulty reports · 719

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 = 'CF650C2'
  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 96UAL900880Control Cable · brokenON FLIGHT CHECK DURING TAXI OUT, LEFT HAND SPOILER INDICATED ONLY PARTIAL EXTENSION. *S/D* FOUND SPOILER CABLE 11B, LT SPOILER 1, 4 AND 5 UP BROKEN. REPLACED CABLE.Nov 19, 1996 · N1858U · Doug DC1030 · Drag Control SystemSDR 96UAL900884Warning Syst · inoperativeCENTER CARGO DOOR A-LOOP INDICATING SYSTEM INOPERATIVE. *S/D* CYCLED DOOR SEVERAL TIMES AND COULD NOT DUPLICATE.Nov 19, 1996 · N1859U · Doug DC1030 · Door Warning SystemSDR 96UAL900886Coalescer Bags · dirtyVERY STRONG ODOR IN CABIN AFTER TAKEOFF WITH PNEUMATIC AND RECIRCULATION FANS ON. REPLACED COALESCER BAGS, ACCOMPLISHED ENGINE RUN AND THERE WAS NO SMELL.Nov 19, 1996 · N1858U · Doug DC1030 · Humidity Control SystemSDR SCNA96378Engine · failedDURING CLIMB, EXPERIENCED EXTREME VIBRATION AND NUMBER 3 ENGINE OIL STRAINER CLOG LIGHT ILLUMINATED. RETARDED NUMBER 3 ENGINE THROTTLES AND LIGHT EXTINGUISHED. AFTER SEVERAL MINUTES, OIL PRESSURE DROPPED RAPIDLY, ENGINE FIRE LIGHT ILLUMINATED AND SMOKE ENTERNov 11, 1996 · N602GC · Doug DC1030F · Engine (Turbine/Turboprop)SDR 96UAL900845Light · inoperativeEMERGENCY EXIT LIGHTING TEST FAILED. FORWARD SECTION AT FAULT. FOUND FORWARD SECTION LIGHT ASSEMBLY INOPERATIVE AND BROKEN CABLE NEAR LIGHT CONNECTION. REPLACED LIGHT ASSEMBLY AND REPAIRED CABLE.Oct 30, 1996 · N1858U · Doug DC1030 · Emergency LightingSDR CA961104003Engine · fire(CAN) TAKE-OFF ABORTED AT 60 KNOTS. TOWER ADVISED FLAMES COMING FROM TAIL PIPE OF NR 1 ENGINE. FIRE EXTINGUISHER BOTTLES ACTIONED. MAINTENANCE INVESTIGATION REVEALED METAL IN TAILPIPE. BORESCOPE CHECK CONFIRMED ENGINE FAILURE.Oct 29, 1996 · Doug DC1030 · Engine (Turbine/Turboprop)SDR CA961025005Steering Collar · cracked(CAN) NOSE WHEEL LANDING GEAR STEERING COLLAR FOUND CRACKED AT RH STEERING CYLINDER UPPER ATTACHMENT LUG. COLLAR REPLACED.Oct 23, 1996 · Doug DC1030 · Landing Gear Steering SystemSDR CALA9601504Fuel So Vlv · out of rigTHE NR 2 ENG SPOOLED DOWN TO IDLE RPM SHORTLY AFTER TAKEOFF. FUEL WAS DUMPED AND THE AIRCRAFT WAS RETURNED. MAINTENANCE FOUND THE NR 2 ENG FUEL PUMP HAD FAILED. THE NR 2 ENG FUEL PUMP WAS REMOVED AND REPLACED. IN ADDITION, THE FUEL/OIL HEAT EXCHANGER AND EOct 23, 1996 · N14075 · Doug DC1030 · Fuel Selector/Shut-Off ValveSDR 96UAL900829Tq Link Bushing · brokenSLIGHT NOSE WHEEL SHIMMY ON ROLLOUT DURING LANDING. *S/D* REPLACED LOWER NOSE GEAR TORQUE LINK DUE TO BROKEN BUSHING AT DISCONNECT.Oct 22, 1996 · N1859U · Doug DC1030 · Nose/Tail Landing GearSDR 96UAL900814Bulkhead · failedDURING TIME CONTROLLED OVERHAUL, RAMP PORTION OF SLIDE SUFFERED INTERNAL BULKHEAD FAILURE. ALSO, LT RAMP RAIL, LOWER END SUFFERED INTERNAL BULKHEAD FAILURE. SCRAPPED RAMP PORTION OF SLIDE.Oct 15, 1996 · N1858U · Doug DC1030 · Escape SlideSDR 96UAL900770Press Ind · inoperativeNR 2 L-DOOR SLIDE TEST INOPERATIVE. REMOTE PRESSURE INDICATOR FOUND TO BE INOPERATIVE. REPLACED INDICATOR.Oct 2, 1996 · N1852U · Doug DC1030 · Emergency EquipmentSDR WRLA96041Fuel Filter · cloggedDURING TAXIING OUT, FLIGHT CREW NOTED NR 2 ENGINE FUEL FILTER PRESSURE DROP LIGHT ON, AIRCRAFT RETURNED TO GATE. MAINTENANCE PERSONNEL REPLACED FUEL FILTER, GROUND RUN THE AIRCRAFT, NO FAULT NOTED. AIRCRAFT RETURNED TO SERVICE. (M)Oct 2, 1996 · N107WA · Doug DC1030F · Engine Fuel DistributionSDR 96UAL900735Fire Loop · no testNR 3 ENGINE A FIRE DETECTION LOOP NO TEST.Sep 21, 1996 · N1858U · Doug DC1030 · Fire DetectionSDR 96UAL900736B-Fire Loop · no testNR 3 ENGINE B-LOOP NO TEST.Sep 21, 1996 · N1858U · Doug DC1030 · Fire DetectionSDR 96UAL900680Strip · defectiveDEFECTIVE EEL STRIP AT LAVATORY 2 RIGHT. *S/D* REPAIRED EEL STRIP, OPERATION NORMAL.Sep 4, 1996 · N1857U · Doug DC1030 · Emergency LightingSDR CA960826013Atach Bolt · sheared(CAN) MAIN LANDING GEAR RETRACT ACTUATOR SUPPORT FITTING ATTACHMENT BOLTS SHEARED AND ACTUATOR FELL OVER AND DOWN WHEN GEAR WAS EXTENDED. FREE FALL EXTENSION INITIATED, NO PROBLEMS. MAINTENANCE CHECK REVEALED ACTUATOR SUPPORT FITTING BOLTS SHEARED. BOLTS, NUTSAug 16, 1996 · Doug DC1030 · Landing Gear ActuatorSDR 96UAL900626Skin · corrodedTHE FUSELAGE SKIN AT BODY STATION 1133 HAD EXCESSIVE MATERIAL LOSS DUE TO CORROSION IN THE AREA OF STRINGER 46L. APPROXIMATELY 50 PERCENT OF THE ORIGINAL SKIN THICKNESS WAS REMOVED OVER A 2.5 DIAMETER AREA. THE DAMAGE WAS DETECTABLE FROM THE OUTSIDE OF THE AAug 14, 1996 · N1857U · Doug DC1030 · Fuselage Main, Plate/SkinSDR 96UAL900629Fuel Quantity · droppedRETURNED TO SFO DUE TO A SIGNIFICANT DROP IN FUEL QUANTITY.Aug 14, 1996 · N1855U · Doug DC1030 · Fuel Quantity IndicatorSDR 96UAL900610Cable Pin · brokenEEL LIGHTS INOPERATIVE IN B-ZONE LEFT SIDE STRIP. FOUND CABLE PIN BROKEN. REPLACED CABLE.Aug 9, 1996 · N1853U · Doug DC1030 · Emergency LightingSDR CA960826101Door · departed(CAN) ON DEPARTURE, LOWER TAIL CONE ACCESS DOOR AT STA 2184 SEPARATED FROM TAIL CONE OF AIRCRAFT. AS THE DOOR OPENED INTO THE SLIP STRESAM WIND, THE HINGE POINTS WERE TORN FROM THE STRUCTURE. THE SEPARATED DOOR STRUCK THE UNDERSIDE OF THE TAIL CONE RESULTING Aug 8, 1996 · Doug DC1030 · Tail Cone DoorsSDR 9617031229Fuel Filter · cloggedDURING TAKEOFF ROLLOUT, THE NR 1 ENGINE FUEL FILTER BYPASS LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE FUEL FILTER AND FOUND SLIGHTLY CLOGGED. REPLACED THE NR 1 FUEL FILTER AND PERFORMED ENGINEAug 5, 1996 · N229NW · Doug DC1030 · Engine Fuel DistributionSDR AU961147Seal · damaged(AUS) GREEN HYDRAULIC SYSTEM UNION SEAL LEAKING - SEAL WAS LOCATED AT RH KRUGER FLAP RETURN LINE UNION - LOSS OF HYDRAULIC FLUIDAug 2, 1996 · Airbus A300B4203 · Hydraulic System, MainSDR CA960808107Shear Pin · sheared(CAN) DURING DESCENT, AIRSPEED DECREASED TO 280 KNOTS, AUTO PILOT OUT OF TRIM LIGHT ILLUMINATED. AIRCRAFT LEVELED OUT AT 11,000 FEET AND AIRSPEED REDUCED TO 250 KNOTS, LIGHT REMAINED ON. AUTO PILOT #1 DISENGAGED AND AIRCRAFT NOTICEABLY NOSE HEAVY. ALL TRIMS TRJul 25, 1996 · Doug DC1030 · Stabilizer Control SystemSDR AU961024Torque Tube · sheared(AUS) LH FLAP TORQUE TUBE SHEARED IN AREA OF ATTACHMENT TO LH SHOCK ABSORBERJul 20, 1996 · Airbus A300B4203 · Trailing Edge Flap Control SystemSDR 96UAL900542Jumper Chord · failedEEL LIGHTING INOPERATIVE ON RT SIDE FROM FORWARD GALLEY THROUGH B-SECTION OF COACH. REPLACED JUMPER CHORD FOR RIGHT HAND SECTION B.Jul 15, 1996 · N1857U · Doug DC1030 · Emergency LightingSDR 96UAL900528Wire · looseEEL LEFT SIDE FIRST CLASS AT FWD END PULLED LOOSE AND PIN BROKEN. *S/D* REPLACED EEL POWER FEEDER STRIP AT DOOR ONE LEFT.Jul 12, 1996 · N1852U · Doug DC1030 · Light System WiringSDR CALA9600959Duct · separatedTHE 1 ENGINE FIRE WARNING LIGHT ILLUMINATED ON TAKEOFF ROLL AT APPROXIMATELY 120 KNOTS. THE ENGINE FAIL/FIRE CHECKLIST WAS ACCOMPLISHED. THE FIRE LIGHT WENT OUT APPROXIMATELY 10 SECONDS AFTER RETARDING THE NR 1 THROTTLE. THE NR 1 ENGINE B-LOOP LIGHT WAS STIJul 2, 1996 · N14063 · Doug DC1030 · Pneumatic Distribution SystemSDR 96UAL900482Connector · looseEEL FLOOR LIGHTING INOPERATIVE AT ROWS 9 TO 16. *S/D* SECURED EEL LIGHT CONNECTION AFT OF 2R LAVATORY.Jun 24, 1996 · N1855U · Doug DC1030 · Emergency LightingSDR 96UAL900449Slide · failedDURING SHOP OVERHAUL OF SLIDE/RAFT FROM DOOR 3L, REMOVED FOR OVERHAUL TIME EXPIRATION, RAMP PORTION OF SLIDE EXPERIENCED INTERNAL BULKHEAD SEPARATION DURING INFLATION. SUPPLEMENTAL DATA UPDATE: SUBMITTER STATES CAUSE UNDETERMINED. SCRAPPED RAMP.Jun 14, 1996 · N1856U · Doug DC1030 · Escape SlideSDR AU960877Slide · faulty(AUS) DOOR 3R SLIDE FAILED TO DROP OUT OF CONTAINERJun 10, 1996 · Airbus A300B4203 · Escape SlideSDR CALA9600646Y-Duct · rupturedTHE NR 3 ENGINE FIRE WARNING ACTIVATED MOMENTARILY WHILE EN ROUTE. THE FIRE WARNING SYSTEM OF ALL ENGINES WAS TESTED AND ALL SYSTEMS CHECKED GOOD. THE FLIGHT WAS CONTINUED TO LGW WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 3 ENGINE 8TH STAGE May 24, 1996 · N68065 · Doug DC1030 · Pneumatic Distribution SystemSDR 96UAL900313Slide Raft · damagedDOOR 3 LEFT OFFWING SLIDE/RAFT REMOVED FOR TIME LIMIT. SHOP FOUND RAMP PORTION OF SLIDE DAMAGED DUE TO SEPARATION OF THE INTERNAL BULKHEADS. SCRAPPED RAMP PORTION OF SLIDE/RAFT.May 3, 1996 · N1854U · Doug DC1030 · Life RaftSDR WRLA96021Compressor · stalledDURING TAKEOFF AT ROTATION, FLIGHT CREW EXPERIENCED COMPRESSOR STALL ON NR 2 ENGINE. FLIGHT ENGINEER NOTED A 6 PERCENT DROP IN N-1 SPEED. DURING INITIAL CLIMB-OUT, CREW NOTED SECOND COMPRESSOR STALL. AIRCRAFT RETURNED TO POINT OF DEPARTURE, LANDING WITHOUT May 3, 1996 · N117WA · Doug DC1030 · Turbine Engine Compressor SectionSDR 96UAL900287Reverser Cowl · delaminatedLARGE AREA OF HEAT AND DELAMINATION DAMAGE ON THE NR 2 ENGINE RIGHT REVERSER COWL. THERE IS ALSO INSULATION DAMAGE. THERE WAS NO FIRE WARNING INDICATION ON THE FLIGHT DECK. UNDER INVESTIGATION. SUPPLEMENTAL DATA UPDATE: DAMAGE CAUSED BY NR 2 PNEUMATIC DUCApr 25, 1996 · N1855U · Doug DC1030 · Engine Thrust ReverserSDR 9609101229Engine · failedDURING TAXI TO RAMP, THE NR 3 ENGINE WAS SHUTDOWN DUE TO FUEL LEAKING OUT OF FRONT OF COMPRESSOR. REPLACED NR 3 ENGINE AFTER REPLACING THE FUEL/OIL EXCHANGER AND INDUCTOR VALVE. CHECK WAS NORMAL AND AIRCRAFT RETURNED TO SERVICE.Apr 17, 1996 · N229NW · Doug DC1030 · Engine (Turbine/Turboprop)SDR 96UAL900257Skin · corrodedWHEN REMOVING NR 2 ADF ANTENNA FOUND CORROSION ON FUSELAGE MOUNTING SURFACE STATION 1069 AT LONGERON L52. REMOVED AFFECTED SKIN SECTION AND PERFORMED EXTERNAL DOUBLER/TRIPLER REPAIR.Apr 15, 1996 · N1854U · Doug DC1030 · Fuselage Main, Plate/SkinSDR CA960515101Smoke Detector · alarm activated(CAN)TAKEOFF REJECTED AFTER SMOKE DETECTOR SOUNDED IN LAV. E. SMOKE DETECTOR RESET. THERE WERE NO FURTHER INDICATIONS. BRAKE TEMP PEAKED AT 400 DEGREES "C". INVESTIGATION REVEALED ALARM ACTIVATED DUE TO PASSENGER SMOKING IN ADJACENT LAV. SMOKE DETECTORS OF LAVApr 7, 1996 · Doug DC1030 · Smoke DetectionSDR CA960514101Control Cable · broken(CAN)WHILE CYCLING AILERON CONTROLS FOR INVESTIGATION OF A HYDRAULIC LEAK, THE CAPTAINS CONTROL WHEEL WOULD NOT RETURN TO THE CENTRE POSITION. FURTHER INVESTIGATION REVEALED THE AILERON DOWN CABLE RUN #7 BROKE INSIDE THE CONTROL COLUMN. AL SO THE AILERON "UPMar 28, 1996 · Doug DC1030 · Aileron Control SystemSDR 96UAL900210Spar Web · crackedNR 3 PYLON UPPER SPAR WEB HAD A CRACK INDICATION IN A FASTENER HOLE COMMON TO THE SPAR CHORD. REPAIRED PER DC-10 SRM 54-20-00 FIGURE 27.Mar 22, 1996 · N1857U · Doug DC1030 · Nacelle/Pylon StructureSDR 96UAL900197Battery Pack · dischargedEMERGENCY LIGHT BATTERY TEST FAILED. AFT POWER SUPPLY LIGHT ILLUMINATED BELOW SECOND OFFICER'S DESK. REPLACED BATTERY PACK AND POWER SUPPLY.Mar 19, 1996 · N1856U · Doug DC1030 · Emergency LightingSDR 96UAL900193Apu · malfunctionedPUNGENT ODOR OF SMOKE IN AIRCRAFT ON ENGINE PNEUMATICS AT HIGH ENGINE POWER. ODOR ISOLATED TO NR 2 PNEUMATICS WHEN USING APU BLEED. REPLACED APU.Mar 15, 1996 · N1858U · Doug DC1030 · Airborne Auxiliary Power Unit (APU) SystemSDR 96UAL900144Spar Web · crackedDURING ENGINE CHANGE THE NR 3 PYLON CENTER SPAR WEB WAS FOUND TO BE CRACKED. THE CRACK IS AT STATION 416 AND PROPAGATES 2 INCHES FROM LIGHTENING HOLE TO EDGE OF WEB. A PERMANENT REPAIR WAS MADE PER DC-10-30 STRUCTURAL REPAIR MANUAL.Feb 22, 1996 · N1858U · Doug DC1030 · Nacelle/Pylon StructureSDR 96UAL900104Battery Pack · dischargedAFT EMERGENCY LIGHT FAILED BATTERY TEST. REPLACED AFT EMERGENCY LIGHT BATTERY (P/N EMSE299A).Feb 12, 1996 · N1854U · Doug DC1030 · Emergency LightingSDR CA960208101Apu · smoking(CAN)PRIOR TO DEPARTURE, APU AUTO SHUT DOWN, EMITTING CLOUDS OF SMOKE. APU WAS MEL'D AND AIRCRAFT DEPARTED. ON CLIMB, CABIN AIR CONDITIONING SYSTEM DISCHARGED OIL VAPOURS. AIRCRAFT RETURNED TO BLOCKS AND C OMPLETED AN OVERWEIGHT LANDING. OVERWEIGHT LANDING CHEJan 26, 1996 · Doug DC1030 · Airborne Auxiliary Power Unit (APU) SystemSDR 95UAL900328Ac Power Syst · malfunctionedDURING INITIAL CLIMB AC BUS NR 3 AND ASSOCIATED LIGHTS RT EMERGENCY, AC AND RT EMERGENCY DC BUS LIGHTS CAME ON. COULD NOT RESTORE THE RT EMERGENCY BUS. FLIGHT RETURNED TO ORD. REPLACED THE GENERATOR CONTROL UNIT AND THE BUS POWER CONTROL AND RECONNECTED THEDec 19, 1995 · N1859U · Doug DC1030 · AC Power Distribution SystemSDR 95UAL900293Pneu Manifold · fail indicationNR 2 MANIFOLD INDICATION FAILURE. THE TRIP WAS CANCELED.Dec 5, 1995 · N1859U · Doug DC1030F · Pneumatic Indicating SystemSDR 95UAL900241Skin · crackedSHEET METAL CRACKED AROUND RIVET, LEFT SIDE OF FUSELAGE, FORWARD OF OUTFLOW VALVE ALONG CIRCULAR FRAME LINE. THE SKIN CRACKING WAS ACTUALLY SKIN CORROSION DAMAGE COMMON TO FRAME LOCATIONS AND WAS REPAIRED PER SRM 53-20-00 FIGURE 6 SHEET 13 CLASS III REPAIR. Nov 1, 1995 · N1859U · Doug DC1030 · Fuselage Main, Plate/SkinSDR 95UAL900175Fitting · crackedNR 3 ENGINE PYLON FWD MOUNT TRUSS FITTING ASSY, PRIOR TO FURTHER FLIGHT, REPLACE AT LEAST ONE TRUSS FITTING ACCT RT FITTING PREVIOUSLY CRACKED AND REPAIRED. LT FITTING CRACKED AT HORIZ FLANGE INBD BOLT HOLE.Oct 5, 1995 · N1858U · Doug DC1030 · Nacelle/Pylon, Attach FittingsSDR 95UAL900163Fillet · missingON ARRIVAL AT NRT, FOUND LEFT SLAT NR 1 DAMAGED AND FILLET MISSING. REPLACED FILLET. INSPECTED AREA AND REPAIRED MINOR DAMAGE TO SLAT. RELEASED COAT 3-8065 TO PERFORM A ONE TIME FLEET INSPECTION OF SLAT FILLET ATTACHMENTS.Oct 2, 1995 · N1855U · Doug DC1030 · Leading Edge DevicesSDR 95UAL900149Eel Battery Pack · dischargedOVERWING EMERGENCY LIGHTS FAILED TEST. REPLACED BATTERY PACK.Sep 22, 1995 · N1854U · Doug DC1030 · Emergency Lighting
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