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 AU000072Bearing · seized(AUS) RT OUTBOARD AILERON POWER CONTROL ACTUATOR INPUT LINK BEARING SEIZED.Feb 2, 2000 · Boeing 767277 · Aileron Control SystemSDR AU000193Spar · corroded(AUS) RT WING CENTRE SECTION REAR SPAR WEB CORRODED IN THE AREA LOCATED BEHIND THE REAR SPAR BULKHEAD FITTING PNO 145T2521. AREA OF CORROSION APPROXIMATELY 215.9MM (8.5IN) BY 38.1MM (2.5IN) BY2.54MM (0.100IN) DEEP.Jan 31, 2000 · Boeing 767277 · Wing SparSDR AU000079Skin · corroded(AUS) RT WING LOWER SKIN PANEL LOCATED AT WS391 CORRODED. AREA OF CORROSION 76.2MM BY 38.1MM (3IN BY 1.5IN). DEPTH OF CORROSION3.556MM (0.140IN).Jan 28, 2000 · Boeing 767277 · Wing, Plate/SkinSDR AALA20000148Nozzle Feeder · damagedORD - FLT 180 - DURING FLIGHT, AIRCRAFT YAWED AND CREW NOTED N1 EGT AND N2 WINDING DOWN. SHUTDOWN ENGINE. ATTEMPTED INFLIGHT START NO SUCCESS. DIVERTED AND LANDED ORD WITHOUT INCIDENT. REPLACED DAMAGED FUEL NOZZLE FEEDER MANIFOLDS AT POSITIONS 10:00 O'CLOCJan 27, 2000 · N302AA · Boeing 767223 · Fuel Controlling SystemSDR AU000066Wire Rope · frayed(AUS) RT AILERON CONTROL CABLE A4B-3 FOUND FRAYED AT WING STATION 531 FAIR LEAD. ALL STRANDS EXCEPT THE HEART STRAND WERE BROKEN. THE ADJACENT WIRE ROPE A4A-3 HAD BROKEN WIRES AND THE ENTIRE LENGTH OF BOTH WIRE ROPE RUNS WAS WORN AT THE FAIR LEAD LOCATIONS.Jan 25, 2000 · Boeing 767204 · Flight Control System WiringSDR AU000076Wedge · contaminated(AUS) LEADING EDGE SLAT TRAILING EDGE WEDGES CORRODED INTERNALLY & CONTAMINATED WITH MOISTURE.Jan 14, 2000 · Boeing 767277 · Leading Edge DevicesSDR AU000053Valve · fractured(AUS) LEFT HYDRAULIC SYSTEM HP FILTER MODULE PRESSURE RELIEF VALVE BODY FAILED AT O- RING GROOVE.Jan 9, 2000 · Boeing 767204 · Hydraulic Pressure Relief Valve, MainSDR AU991091Duct · burst(AUS) RIGHT ENGINE HP AIR DUCT ELBOW RUPTURED.Sep 12, 1999 · Boeing 767277 · Engine Bleed Air SystemSDR AU991092Bracket · broken(AUS) RIGHT ENGINE BLEED AIR DUCT SUPPORT BRACKET BROKEN. SUSPECT BROKEN BRACKET CAUSED BLEED AIR DUCT TO FAIL. SEE MDR AU991091.Sep 12, 1999 · Boeing 767277 · Engine Bleed Air SystemSDR AU990844Sensor · out of adjust(AUS) RIGHT ENGINE THRUST REVERSER LOCK PROXIMITY SENSOR OUT OF ADJUSTMENT.Jul 31, 1999 · Boeing 767277 · Engine Thrust ReverserSDR AU990681Sensor · faulty(AUS) LEFT ENGINE FAILED TO ACCELERATE ABOVE FLIGHT IDLE. NR 1 COMPRESSOR INLET TEMPERATURE SENSOR CHANGED.Jul 24, 1999 · Fuel Controlling SystemSDR AU990702Fcu · faulty(AUS) NR 2 ENGINE MAIN ENGINE CONTROL SUSPECT FAULTY.Jul 13, 1999 · Fuel Control/Reciprocating EnginesSDR DL76S991436Gcu · failedDURING CLIMBOUT AT APPROX FL 250 PILOTS NOTICED ODOR IN COCKPIT. THE ODOR BECAME STRONGER, SEVERAL MINUTES LATER THE RT GEN OFF LIGHT ILLUMINATED WITH ASSOCIATED EICAS LIGHTS. THE INTENSITY OF ODOR REQUIRED USE OF COCKPIT OXYGEN MASKS. A/C DIVERTED TO JAX. Jun 25, 1999 · N130DL · Boeing 767332 · AC RegulatorSDR AU991038Rod · out of adjust(AUS) OUTBOARD SLAT PDU INPUT ROD OUT OF ADJUSTMENT.Jun 22, 1999 · Boeing 767277 · Leading Edge Slat Control SystemSDR AU990494Cover · cracked(AUS) RT LATERAL CENTRAL CONTROL ACTUATOR FILTER COVER `O' RING SEAL DISPLACED. LOSS OF CENTER HYDRAULIC SYSTEM FLUID. INVESTIGATION FOUND THAT THE FILTER COVER CONTAINED A CIRCUMFERENTIAL CRACK INTHE THREADED PORTION EXPOSING THE SEAL TO HYDRAULIC PRESSURE May 24, 1999 · Boeing 767277 · Hydraulic System, MainSDR AU990471Valve · failed(AUS) RAM AIR TURBINE CHECKOUT MODULE CHECK VALVE FAILED. LOSS OF CENTER HYDRAULIC SYSTEM FLUID.May 9, 1999 · Boeing 767277 · Hydraulic System, AuxiliarySDR DL767990986Engine · failedIN DESCENT RT ENGINE FAILED, OIL PRESS WENT TO ZERO. REPLACED ENGINE.May 6, 1999 · N101DA · Boeing 767232 · Engine (Turbine/Turboprop)SDR AU990453Structure · damaged(AUS) AIRCRAFT SUFFERED HAIL DAMAGE TO THE FOLLOWING AREAS: 1. LT INBOARD AND OUTBOARD AILERONS. 2. LT AND RT LEADING EDGE SLAT WEDGES. 3. LT AND RT INBOARD AND OUTBOARD FLAP TRAILING EDGES. 4. NR 10 SPOILER. 5. VERTICAL STABILIZER RT SIDE LEAApr 15, 1999 · Boeing 767204 · Aircraft StructuresSDR AU990485Structure · damaged(AUS) AIRCRAFT SUFFERED HAIL DAMAGE TO THE FOLLOWING AREAS: 1. LT OUTBOARD AILERON, RT INBOARD AND OUTBOARD AILERONS. 2. LT AND RT ELEVATORS. 3. NR 1, NR 2, NR 3, NR 4, NR 5, NR 7, NR 8, NR 9, NR 10, NR 11, NR 12 LEADING EDGE SLATS. 4. NR 2, NR 3, NR 4Apr 15, 1999 · Boeing 767216 · Wing StructureSDR AU990293Pin · cracked(AUS) RIGHT INBOARD ENGINE PYLON MID-SPAR FUSE PIN CRACKED. CRACK LENGTH 11 MM (0.433 INCH). FOUND DURING EDDY CURRENT INSPECTION.Mar 24, 1999 · Boeing 767277 · Nacelle/Pylon, Attach FittingsSDR AU990407Wedge · disbonded(AUS) LEADING EDGE SLAT TRAILING EDGE WEDGES DISBONDED AND CORRODED ON THE FOLLOWING SLATS: SLAT NR 1. DISBOND 150 MM BY 40 MM (5.905 INCHES BY 1.574 INCH) AT INBOARD END, 30 MM (1.181 INCH) FORWARD OF TRAILING EDGE. DISBOND 180 MM BY 12 MM (7.086 INCHES BMar 12, 1999 · Boeing 767204 · Leading Edge DevicesSDR AU990430Wedge · disbonded(AUS) LEADING EDGE SLAT T/E WEDGES DISBONDED IN FOLLOWING AREAS: 1. NR 3 SLAT UPPER SURFACE DISBONDED AT OUTBOARD END 45 MM (1.771 INCH) FROM T/E . AREA OF DISBOND 50 MM BY 45 MM (1.968 INCH BY 1.771 INCH). 2. NR 4 SLAT UPPER SURFACE DISBONDED 1440 MM (Feb 11, 1999 · Boeing 767216 · Leading Edge DevicesSDR AU990064Engine · making metal(AUS) LEFT ENGINE CHIP DETECTOR CONTAMINATED WITH M50 BEARING MATERIAL.Jan 24, 1999 · Engine (Turbine/Turboprop)SDR AU990063Heat Exchanger · cracked(AUS) LEFT ENGINE FUEL/OIL HEAT EXCHANGER HEADER RADIUS CONTAINED TWO CRACKS. FOUND DURING ULTRASONIC INSPECTION IAW GE6-79-00-2C AND GE SERVICE BULLETIN SB79-023. PART TC: 26,858.Jan 18, 1999 · Engine Fuel/Oil CoolerSDR AU990146Gear · corroded(AUS) NR 3 OUTBOARD AND NR 4 INBOARD LEADING EDGE SLAT ROTARY ACTUATORS CONTAINED INTERNAL CORROSION ON THE RING GEAR BEARING SURFACES AND THE PLANET GEAR P/N 256T2152. FOUND DURING VISUAL INSPECTION IAW ER B76-27-80-27 (AD/B767/095). PART TC: 51,949.Jan 15, 1999 · Boeing 767204 · Leading Edge Slat ActuatorSDR AU990037Wedge · disbonded(AUS) LEADING EDGE SLAT TRAILING EDGE WEDGES FOUND WITH DISBONDED AREAS ON A TOTAL OF SEVEN SLATS. FOUND DURING VISUAL AND ULTRASONIC INSPECTIONS IAW BOEING ALERT SB 767-57A0039.Jan 13, 1999 · Boeing 767204 · Leading Edge DevicesSDR AU990036Web · cracked(AUS) LEFT ENGINE PYLON TOP WEB CRACKED AT THE REAR OUTBOARD CORNER OF ONE WEB CUT-OUT. CRACK LENGTH 9.53 MM (0.375 INCH). FOUND DURING EDDY CURRENT INSPECTION.Jan 12, 1999 · Boeing 767204 · Nacelle/Pylon, Main FrameSDR AU981478Apu · failed(AUS) APU FAILED. REAR BEARING HOUSING AND OIL SCAVENGE PUMP FOUND ON THE RAMP. PART TC: 27,149.Nov 9, 1998 · Boeing 767204 · APU Core EngineSDR AU981703Tube · leaking(AUS) ENGINE REMOVED DUE TO HIGH OIL CONSUMPTION. THE COMPRESSOR REAR FRAME WAS DETACHED AND INVESTIGATION FOUND THE SUMP OIL SUPPLY TUBE HAD BEEN WORN THROUGH BY AN ATTACHMENT 'P' CLIP.Oct 22, 1998 · Turbine Engine Oil SystemSDR AU981310Compressor · damaged(AUS) LEFT ENGINE COMPRESSOR STAGE 10 TO STAGE 12 DAMAGED.Oct 10, 1998 · Turbine Engine Compressor SectionSDR AU981476Line · damaged(AUS) NOSE LANDING GEAR `DOWN' TITANIUM HYDRAULIC PIPE LOCATED AT FS 625 BETWEEN THE FORWARD CARGO HOLD LEFT SIDEWALL AND THE FUSELAGE SKIN DENTED AND CRACKED. LEAKING HYDRAULIC FLUID MIST IN CABIN. PIPE HAD BEEN DAMAGED DUE TO PREVIOUS MAINTENANCE. PART Oct 9, 1998 · Boeing 767277 · Hydraulic System, MainSDR AU981284Engine · fod(AUS) LEFT ENGINE VIBRATION. N2 VIBRATION INDICATED 5.1 UNITS AT 40 PERCENT N1. INVESTIGATION FOUND THAT THE VIBRATION WAS DUE TO BIRD STRIKE DAMAGE.Sep 30, 1998 · Engine (Turbine/Turboprop)SDR AU981261Nozzle · cracked(AUS) ENGINE HIGH PRESSURE TURBINE STAGE TWO NOZZLE SEGMENTS (2OFF) SEVERELY CRACKED.Sep 3, 1998 · Turbine SectionSDR AU981453Nozzle · cracked(AUS) HIGH PRESSURE TURBINE STAGE TWO NOZZLE SEGMENTS (3 OFF) CRACKED.Sep 3, 1998 · Turbine SectionSDR AU981222Slat · delaminated(AUS) NR 1 AND NR 3 LEADING EDGE SLAT TRAILING EDGES DELAMINATING.Aug 31, 1998 · Boeing 767204 · Leading Edge DevicesSDR AU981170Seat Belt · faulty(AUS) PASSENGER SEAT BELTS LOCATED AT 19D, 23E, 30C, 32E, 33E AND 34C AS WELL AS THE FIRST OFFICER'S SEAT BELT HAD MISSING ID LABELS. FOUND DURING INSPECTION IAW ER Z1-25-00-10J (AD/RES/29).Aug 12, 1998 · Boeing 767204 · Passenger Compartment EquipmentSDR AU981152Slat · delaminated(AUS) NR 2 LEADING EDGE SLAT TRAILING EDGE WEDGE DELAMINATED IN FOUR AREAS. FOUND DURING INSPECTION IAW AD/B767/73.Aug 11, 1998 · Boeing 767204 · Leading Edge DevicesSDR AU981049Actuator · failed(AUS) LEFT ELEVATOR POWER CONTROL ACTUATOR LEAKING FROM CHECK VALVE END CAP. LOSS OF RT HYDRAULIC SYSTEM FLUID. INVESTIGATION FOUND THE CHECK VALVE INNER AND BACKUP `O' RING SEALS MISSING FROM THREE CHECK VALVE END CAPS. PERSONNEL/MAINTENANCE ERROR. PART TC:Aug 3, 1998 · Boeing 767216 · Elevator Control SystemSDR AU981210Fitting · cracked(AUS) LEFT WING DEFLECTION CONTROL SUPPORT FITTING LOWER ATTACHMENT LUG FRACTURED THROUGH THE BEARING HOUSING. FITTING IS LOCATED AT WS 906.20. PART TC: 41,421.Jul 28, 1998 · Boeing 767277 · Wing, Control Surface Attach FittingsSDR AU981208Fitting · corroded(AUS) RIGHT PYLON CONTAINED EXFOLIATION CORROSION ON THE UPPER SURFACES OF THE UPPER WEB OF THE TORQUE BOX ADJACENT TO THE UPPER LINK ATTACHMENT BEAM EITHER SIDE OF AND RUNNING UNDER THE FORWARD UPPER STRUT FITTING. CORROSION HAD PENETRATED THROUGH THE WEB WIJul 20, 1998 · Boeing 767277 · Nacelle/Pylon, Main FrameSDR AU981209Fitting · corroded(AUS) LEFT PYLON CONTAINED EXFOLIATION CORROSION ON THE UPPER SURFACES OF THE UPPER WEB OF THE TORQUE BOX ADJACENT TO THE UPPER LINK ATTACHMENT BEAM OUTBOARD OF AND RUNNING UNDER THE STRUT FITTING. CORROSION HAD PENETRATED TO A DEPTH OF 1.778 MM (0.070 INCH) Jul 20, 1998 · Boeing 767277 · Nacelle/Pylon, Main FrameSDR CA980519014Engine · leaking(CAN) DURING FLIGHT ECAM INDICATION SHOWED LOW OIL QUANTITY ON NR 1 ENGINE. THRUST REVERSERS REDUCED AND AIRCRAFT DIVERTED. SEVERE OIL LEAK FOUND ON AFT CENTER SECTION OF THE ENGINE. ENGINE REPLACED AND SENT FOR INVESTIGATION. INITIAL TEST COULD NOT DUPLICMay 5, 1998 · Engine (Turbine/Turboprop)SDR AU980787Collar · cracked(AUS) LEFT INBOARD FLAP INBOARD TORQUE TUBE COLLAR CRACKED AND TORQUE TUBE HEAVILY CORRODED. RIGHT SIDE FLAP COLLARS AND TORQUE TUBE ALSO CORRODED. PART TOTAL CYCLES: 39,633.Apr 22, 1998 · Boeing 767277 · Trailing Edge Flap Control SystemSDR AU980821Pin · cracked(AUS) LT ENGINE MID SPAR INBOARD FUSE PIN INNER BORE CONTAINED TWO LONGITUDINAL CRACKS. TOTAL CRACK LENGTH 8.89 MM (0.35 INCHES). FOUND DURING EDDY CURRENT INSPECTION IAW ER B76-54-40-4I.Mar 6, 1998 · Boeing 767277 · Nacelle/Pylon, Attach FittingsSDR AU980612Nozzle · cracked(AUS) NR 1 ENGINE FUEL NOZZLE ELBOW CRACKED AND LEAKING FUEL. THE NOZZLE WAS LOCATED AT APPROXIMATELY THE 1 O'CLOCK POSITION. THE ELBOW WAS IDENTIFIED AS AN OLD TYPE CAST ELBOW WHICH HAD BEEN FOUND TO BE PRONE TO POROSITY.Jan 30, 1998 · Fuel Injector NozzleSDR AU980063Skin · damaged(AUS) FUSELAGE SKIN AND STRINGER 31R LOCATED AT STN 485 DAMAGED BY FORK LIFT DURING LOADING OF FORWARD CARGO HOLD.Jan 12, 1998 · Boeing 767204 · Fuselage Main, Plate/SkinSDR AU971644Actuator · failed(AUS) LH MAIN LANDING GEAR LEFT HAND DRAG BRACE ACTUATOR PISTON ROD SHEARED IN THREADED AREA.Dec 26, 1997 · Boeing 767277 · Landing Gear Retraction/Extension SystemSDR 97FDEA00828Compressor · stalledNR 1 ENG CLIMBING THROUGH FL230 NR 1 ENGINE HAD VIBRATION AND COMPRESSOR STALLS. ANY POWER SETTINGS ABOVE IDLE WOULD CAUSE COMPRESSOR STALLS. EGT READING 720 DEG, LANDED WITH PWR AT IDLE.Nov 12, 1997 · N404FE · Airbus A310203 · Turbine Engine Compressor SectionSDR 97FDEA00744Compressor · stalled97-0203, DURING CLIMB-OUT THROUGH FL 180 A LOUD BANG WAS HEARD, AND THE A/C BEGAN TO SHUTTER. THE MAIN DECK SMOKE DETECTION CAME ON, ENGINE WAS SHUTDOWN. EMERGENCY RETURN TO MEMPHIS, OVERWEIGHT LANDING.Oct 16, 1997 · N430FE · Airbus A310203 · Engine (Turbine/Turboprop)SDR 97FDEA00660Compressor Line · looseAT APPROX 10,000 FT IN CLIMB, THE LEFT FUEL FLOW STARTED FLUCTUATING. FUEL PRESSURE FLUCTUATED FROM 130 TO 115 PSI, FF FLUCTUATED BETWEEN 6000 AND 14000 AND NR 1 N2 SHOWED A 3 PERCENT SURGE. RESECURED AND SAFTIED COMPRESSOR DISCHARGE LINE. C/W ADJUST TEST OSep 17, 1997 · N401FE · Airbus A310203 · Turbine Engine Compressor Section
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