GE CF6-80A

Service difficulty reports · 272

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 = 'CF680A'
  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 02FDEA00190Sensor · faultyDURING CLIMB NR 1 ENGINE FLUCTUATED. REMOVED AND REPLACED NR 1 CIT SENSOR & T2 SENSOR PER 73-21-02-4, 73-23-07-4. ALL OK.Mar 6, 2002 · N442FE · Airbus A310203 · Power Indicating SystemSDR AALA20020257Turbine Wheel · seizedLAX - FLT 76 - EN ROUTE LAX-DFW, ON ROTATION, LEFT ENGINE SHUTDOWN. ALL ENGINE INDICATIONS ZEROED AND FAN SEIZED. RETURNED LAX LANDED WITHOUT INCIDENT. FOUND 860 ROTOR SEIZED. ACCOMPLISHED PYLON INSPECTION AND CHANGED LEFT ENGINE. SYSTEM GROUND CHECKED NOMar 4, 2002 · N319AA · Boeing 767223 · Turbine SectionSDR AUS20020036Fitting · cracked(AUS) CENTER TANK LONGERON TO FORWARD FUSELAGE FITTINGS PNO 1114T4020-1 (LT) AND PN 1114T4020-3 (RT) CRACKED. FOUND DURING MAGNETIC PARTICLE INSPECTION.Jan 16, 2002 · Boeing 767277 · Fuselage Main, Attach FittingsSDR AUS20011223Strut · cracked(AUS) ENGINE FAN MODULE NR 9 FAN FRAME STRUT CRACKED PARALLEL TO THE WELD LINE AT THE INNER RADIAL END OF THE STRUT ADJACENT TO THE SUMP HOUSING.Nov 19, 2001 · Boeing 767277 · Turbine Engine Compressor SectionSDR AUS20010959Controller · malfunctioned(AUS) FLAP SYSTEM FAULTY. FLAP DRIVE SYSTEM INSPECTED AND NO FAULTS FOUND. FLAPS CYCLED AND FAULT DISAPPEARED. LIMITED INFORMATION PROVIDEDAug 31, 2001 · Boeing 767216 · Trailing Edge Flap Control SystemSDR ABXA010447Engine · vibrationCLIMB READING WAS 2.7, CRUISE READING WAS 1.3, ENGINE PARAMETERS NORMAL. OTHER INDICATION WAS AUDIBLE NOISE AND VIBRATION FOLLOWING THRUST CHANGE. CLEANED AND INSPECTED HOLD OPEN RODS FOR FAN COWL IAW B767 MM 77-11-10-2. VIBRATION LEVELS WERE FOUND TO BE WIAug 17, 2001 · N786AX · Boeing 767281 · Engine (Turbine/Turboprop)SDR AUS20010803Actuator · faulty(AUS) LH MAIN LANDING GEAR FORWARD DRAG BRACE DOWNLOCK ACTUATOR FAULTY. INVESTIGATION FOUND THE ACTUATOR PISTON ROD DETACHED FROM THE ACTUATOR BODY DUE TO FAILURE OF THE PISTON ROD IN THE THREADEDAREA WHICH ENGAGES THE PISTON RETAINING NUT.Jul 31, 2001 · Boeing 767204 · Landing Gear Retraction/Extension SystemSDR ABXA010419Engine · vibrationDURING CLIMB, RIGHT ENGINE VIBRATION 2.0 TO 2.2, SOME VIBRATION FELT. DURING ALL OTHER PHASES OF FLIGHT, NO VIBRATION FELT. OPENED COWLING AND CHECKED FOR LOOSE DUCTS, ETC. NO DEFECTS. PERFORMED BITE OF AVM AND EEC, NO DEFECTS NOTED AND NO MAINTENANCE MESSJul 30, 2001 · N785AX · Boeing 767200 · Engine (Turbine/Turboprop)SDR AUS20010747Generator · misinstalled(AUS) OXYGEN GENERATORS LOCATED AT SEATS 24AB, 25AB, 27AB AND 30FG HADTHE RELEASE PINS INCORRECTLY INSTALLED.Jul 17, 2001 · Boeing 767277 · Passenger Oxygen SystemSDR AUS20010672Pin · missing(AUS) FLAP BYPASS VALVE ROTARY ACTUATOR PIN MIGRATED OUT OF POSITIONLEVER.Jun 28, 2001 · Boeing 767204 · Trailing Edge FlapsSDR AUS20010607Valve · failed(AUS) FLAP/SLAT SHUTOFF VALVE FAILED.May 20, 2001 · Boeing 767277 · Trailing Edge Flap Control SystemSDR AUS20010707Support · cracked(AUS) ENGINE FIRST STAGE HPT INNER NOZZLE SUPPORT CRACKED. TURBINEDAMAGE AND METAL IN TAILPIPE.May 9, 2001 · Boeing 767277 · Turbine SectionSDR AUS20010391Stringer · corroded(AUS) STRINGER 39L LOCATED BELOW THE FLOOR IN THE AFT CARGO AREACORRODED BETWEEN BS 1285 AND BS 1307.Apr 30, 2001 · Boeing 767277 · Fuselage Main, Longeron/StringerSDR AU010383Stringer · cracked(AUS) STRINGER 32L LOCATED AT STN 1085 CRACKED. CRACK LENGTH 114.3MM(4.5IN).Apr 24, 2001 · Boeing 767204 · Fuselage Main, Longeron/StringerSDR AUS20010580Oxygen Mask · faulty(AUS) PASSENGER OXYGEN MASKS (7OFF) SUSPECT FAULTY. FOUND DURINGINSPECTION IAW AD/B767/125.Apr 24, 2001 · Boeing 767204 · Passenger Oxygen SystemSDR AUS20010618Stringer · corroded(AUS) STRINGER 39L BADLY CORRODED IN THE AREA LOCATED BETWEEN BS1285AND BS1307. APPROXIMATELY 304.8MM (12IN) OF THE HAT SECTIONED STRINGER LOWER CHANNEL WAS SEVERELY CORRODED WITH PORTIONS OF THE CHANNEL TOTALLY DESTROYED.Apr 20, 2001 · Boeing 767277 · Fuselage Main, Longeron/StringerSDR AU010322Mount · cracked(AUS) LH WING FITTING OUTBOARD LUG CRACKED DIAGONALLY ACROSS THE UPPERFLANGE FACE THROUGH THE LUG FILLET RADIUS. THE CRACK WAS FOUNDVISUALLY AND CONFIRMED USING NDI. FOUND DURING INSPECTION IAW ERB76-57-40-19.Apr 10, 2001 · Boeing 767277 · Wing, Nacelle/Pylon Attach FittingsSDR AU010298Fitting · cracked(AUS) LT WING PYLON ATTACHMENT FITTING OUTBOARD LUG CRACKED. FOUND DURING VISUAL INSPECTION IAW ER B76-57-40-19.Apr 9, 2001 · Boeing 767277 · Wing, Nacelle/Pylon Attach FittingsSDR AU010323Fitting · cracked(AUS) RT WING FITTING OUTBOARD LUG CRACKED AROUND THE INBOARD AFT CORNER OF THE LUG APPROXIMATELY 10MM (0.393IN) FORWARDAND 5MM (0.196IN) OUTBOARD. CRACK CONFIRMED USING NDI. FOUND DURING INSPECTION IAW ER B76-57-40-18.Apr 9, 2001 · Boeing 767277 · Wing, Nacelle/Pylon Attach FittingsSDR AU010351Slide · misinstalled(AUS) ESCAPE SLIDE FITTED TO DOOR LT 1 INCORRECTLY FITTED FOLLOWINGHEAVY MAINTENANCE. INSPECTION FOUND THAT THE SLIDE BAR WAS IN THE STOWED (TRANSPORT) POSITION AND WAS NOT CONNECTED TO THE GIRT BAR. FURTHER INVESTIGATION FOUND THAT THE ESCAPE SLIDES ONTHE OTApr 9, 2001 · Boeing 767204 · Escape SlideSDR AU010297Fitting · cracked(AUS) RT WING PYLON ATTACHMENT FITTING OUTBOARD LUG CRACKED. CRACK PENETRATES THE FULL THICKNESS OF THE LUG AND EXTENDSAPPROXIMATELY 25.4MM (1IN) ALONG THE INBOARD FACE AND APPROXIMATELY 12.7MM (0.5IN) ALONG THE OUTBOARD FACE. FOUND USING EDDY CURRENT INSPECTIApr 6, 2001 · Boeing 767277 · Wing, Nacelle/Pylon Attach FittingsSDR AUS20010774Valve · cracked(AUS) RAM AIR TURBINE (RAT) MODULE LEAKING DUE TO CRACKED CHECK VALVE.Mar 23, 2001 · Boeing 767277 · Hydraulic System, AuxiliarySDR AUS20010865Valve · cracked(AUS) RAM AIR TURBINE (RAT) MODULE CHECK VALVE CRACKED. LOSS OF HYDRAULIC FLUID. INVESTIGATION FOUND THAT THE HEX HEAD SEPARATEDFROM THE CHECK VALVE BODY DUE TO A FRACTURE BETWEEN THE UPPER O' RING GROOVE AND THE INTERNAL BODY THREAD RELIEF.Mar 23, 2001 · Boeing 767277 · Hydraulic System, AuxiliarySDR AUS20010862Frame · cracked(AUS) RT BULKHEAD OUTER CHORD LOCATED AT BS1809.5 CRACKED IN AREA OFLOWER TWO FASTENERS IN INSPECTION AREA 1.Feb 1, 2001 · Boeing 767277 · Fuselage Main, FrameSDR AU010109Fitting · corroded(AUS) LT AND RT MAIN LANDING GEAR SIDE STRUT SWIVEL ASSEMBLY FITTINGS COORODED IN AREA BENEATH BUSHING FLANGE.Jan 23, 2001 · Boeing 767277 · Landing Gear Retraction/Extension SystemSDR AU001331Seat Back · cracked(AUS) CAPTAINS SEAT BACK VERTICAL ADJUSTMENT TRACKS PNO 812072-7 ANDPNO 812072-8 CRACKED FROM THE UPPER EDGE OF THE AFT TRACK FLANGE. CRACK LENGTH 30MM (1.18IN).Dec 7, 2000 · Boeing 767204 · Flight Compartment EquipmentSDR AU001150Pump · cracked(AUS) RT ENGINE DRIVEN HYDRAULIC PUMP CASING CRACKED. PUMP DRIVESHAFT FAILED AT SHEAR POINT. SEVERE INTERNAL DAMAGE TO PUMP. SUSPECTPISTON AND SHOE SUBASSEMBLY FAILED FIRST. LOSS OF HYDRAULIC FLUID.Nov 15, 2000 · Boeing 767216 · Hydraulic Pump (Electric/Engine), MainSDR AU001023Warning System · faulty(AUS) LT ENGINE FIRE WARNING. A THOROUGH INVESTIGATION OF THE FIRE WARNING SYSTEM COULD FIND NO FAULTS AND THE SYSTEM HAS OPERATED CORRECTLY SINCE. DEFECT NOT CONFIRMED.Sep 20, 2000 · Boeing 767277 · Fire DetectionSDR AU001073Bearing · collapsed(AUS) NR 7 MAIN WHEEL INNER BEARING COLLAPSED. INVESTIGATION FOUND THAT DURING THE LAST WHEEL CHANGE, THE INBOARD WHEEL SPACER WAS NOTREFITTED TO THE AXLE DUE TO THE SPACER COMING OFF WITH THE WHEEL. PERSONNEL/MAINTENANCE ERROR.Sep 16, 2000 · Boeing 767277 · Wheel/Ski/FloatSDR AU001066Pin · cracked(AUS) LT ENGINE PYLON MIDSPAR INBOARD FUSE PIN CRACKED. CRACK LENGTH APPROXIMATELY 14MM (0.55IN). FOUND DURING EDDY CURRENT INSPECTION.Sep 7, 2000 · Boeing 767277 · Nacelle/Pylon, Attach FittingsSDR AU000734Skin · corroded(AUS) AIRCRAFT SKIN CORRODED BENEATH PAINT LOCATED AFT OF STN 287 AND BELOW STRINGER NR 24. AREA OF CORROSION 50MM BY 50MM (1.968IN BY 1.968IN) AND 2.032MM (0.080IN) DEEP.Sep 1, 2000 · Boeing 767277 · Fuselage Main, Plate/SkinSDR AU000735Housing · corroded(AUS) RT MAIN LANDING GEAR SIDE STRUT SWIVEL HOUSING CORRODED IN THEAREA OF THE BUSHING FLANGE. DEPTH OF CORROSION 0.127MM (0.005IN).Sep 1, 2000 · Boeing 767277 · Landing Gear Retraction/Extension SystemSDR AU000803Actuator · failed(AUS) RT MAIN LANDING GEAR DRAG BRACE ACTUATOR PISTON ROD PN 273T6034-1 FRACTURED IN THREADED END.Jul 31, 2000 · Boeing 767277 · Landing Gear ActuatorSDR AU000890Actuator · faulty(AUS) RUDDER TRIM ACTUATOR FAULTY. WORKSHOP INVESTIGATION COULD FIND NO FAULTS.Jul 24, 2000 · Boeing 767277 · Rudder Tab Control SystemSDR AU000801Actuator · corroded(AUS) NR 11 LEADING EDGE SLAT INBOARD ROTARY ACTUATOR INTERNALLY CORRODED. RING GEAR SEAL MISSING.Jul 15, 2000 · Boeing 767277 · Leading Edge Slat ActuatorSDR AU000579Pin · sheared(AUS) NOSE LANDING GEAR STEERING SYSTEM RT METERING VALVE INDEXING PINSHEARED. WORKSHOP FOUND EVIDENCE OF HEAVY CORROSION AROUND THEPIN LOCATION HOLE.Jul 7, 2000 · Boeing 767277 · Steering UnitSDR AU000804Fuse · cracked(AUS) OUTBOARD HYDRAULIC FUSE ON BRAKE MODULE CRACKED IN VALVE BODY. VALVE IS LOCATED AT THE WING TRAILING EDGE OUTBOARD OF THE LT MAIN LANDING GEAR. LOSS OF RT HYDRAULIC SYSTEM FLUID.Jun 21, 2000 · Boeing 767277 · Hydraulic System, MainSDR AU000516Controller · faulty(AUS) LT WING NR 3 SPOILER VIBRATING UP TO 52.8MM (2IN) FROM THE SELECTED POSITION. WORKSHOP INVESTIGATION FOUND THE SPOILER CONTROL MODULE FAULTY.Jun 4, 2000 · Boeing 767277 · Drag Control SystemSDR AU000517Web · cracked(AUS) PARK BRAKE INPUT CRANK ASSEMBLY SUPPORT WEB CRACKED. SUSPECTPARKING BRAKE MECHANISM INCORRECTLY RIGGED CAUSING FLEXING OF THE WEB.May 27, 2000 · Boeing 767277 · Fuselage Miscellaneous StructureSDR AU000450Housing · eroded(AUS) MAIN FORWARD FUEL TANK LEFT BOOST PUMP FAILED. INVESTIGATION FOUND PIECES OF METAL SEPARATED FROM THE HOUSING INLET STRUTS JAMMING THE CHECK VALVE PARTIALLY OPEN.May 20, 2000 · Boeing 767277 · Fuel Boost PumpSDR AU000442Structure · damaged(AUS) NOSE LANDING GEAR INADVERTANTLY RETRACTED DURING OVERNIGHT MAINTENANCE. EXTENSIVE DAMAGE WAS CAUSED TO THE FUSELAGESTRUCTURE IN THE NOSEMay 19, 2000 · Boeing 767204 · Fuselage Main, StructureSDR AU000398Hose · leaking(AUS) HORIZONTAL STABILISER TRIM CONTROL MODULE HYDRAULIC HOSE LEAKING. LOSS OF HYDRAULIC FLUID. HOSE IS ORIGINAL FITMENT ITEM FROM AUGUST 1987.May 12, 2000 · Boeing 767204 · Hydraulic System, MainSDR AALA20000687Nozzle · separatedBOS- FLT 0012 - DURING FLIGHT, ENGINE EXHAUST NOZZLE DEPARTED AIRCRAFT. DAMAGED FLAP, AILERON AND HORIZONTAL STABILIZER. REPLACED ENGINE. SYSTEM GROUND CHECKED, NORMAL OPERATION. ENGINE FAILURE UNDER INVESTIGATION. (X)Apr 24, 2000 · N334AA · Boeing 767223 · Engine Collector/Tailpipe/NozzleSDR AU000386Gear · stripped(AUS) TRAILING EDGE FLAP DRIVE GEARBOX INPUT GEAR STRIPPED.Apr 20, 2000 · Boeing 767277 · Trailing Edge Flap ActuatorSDR AU000116Pin · cracked(AUS) RT ENGINE PYLON MIDSPAR FITTING INBOARD FUSE PIN CRACKEDINTERNALLY. CRACK LENGTH 19.050MM (0.75IN). FOUND DURING EDDY CURRENT INSPECTION.Apr 7, 2000 · Boeing 767204 · Nacelle/Pylon, Attach FittingsSDR AU000350Frame · cracked(AUS) LT ENGINE PYLON TOP WEB CRACKED AT THE FORWARD INBOARD CORNER OFTHE POWER FEEDER CABLE CUTOUT. CRACK LENGTH 9.525MM (0.375IN).Mar 31, 2000 · Boeing 767204 · Nacelle/Pylon, Frame/Spar/RibSDR AU000891Inverter · faulty(AUS) STANDBY STATIC INVERTER FAULTY. WORKSHOP INVESTIGATION FOUND THAT TRANSISTORS Q3 TO Q10 WERE SHORT CIRCUITED OR OPEN CIRCUITED WITH THE BASE BIAS RESISTORS BLOWN OPEN.Mar 16, 2000 · Boeing 767277 · AC InverterSDR AU000887Cvr · faulty(AUS) COCKPIT VOICE RECORDER (CVR) FAULTY. WORKSHOP INVESTIGATION FOUND INTERMITTENT FAILURE DUE TO TAPE DEPOSIT ON RECORDING HEADS CAUSING LOW AUDIO ON TRACK 2.Mar 11, 2000 · Boeing 767204 · Audio/Video MonitoringSDR AU000987Circuit Board · burned(AUS) MASTER DIM AND TEST PRINTED CIRCUIT BOARD M2 IN PANEL P29 BURNED.Mar 10, 2000 · Boeing 767277 · Passenger Compartment LightingSDR AU000177Arm · corroded(AUS) DO 11 LEADING EDGE SLAT INBOARD ROTARY ACTUATOR CORRODED INTERNALLY BENEATH BEARING.Feb 23, 2000 · Boeing 767277 · Leading Edge Slat Actuator
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