GE CFM56 series
Service difficulty reports · 5,028
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 = 'CFM56' 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.
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 = 'CFM56' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR AMTA200500316Overheat Sensor · malfunctionedAFTER GEAR RETRACTION, WHEEL WELL FIRE LIGHT ILLUMINATED WITH FIRE BELL. COMPLETED WHEEL WELL FIRE PROCEDURES, LIGHT WENT OUT ON SHORT FINAL, BRAKE TEMPS WERE (0) DEG AND HYD NORMAL. REMOVED AND REPLACED OVERHEAT DETECTION CONTROL UNIT IAW MM. OPS CHECK GOSDR 2005UALA00262Skin · dentedDENT ON FWD SIDE OF FWD CARGO DOOR, MEASURES 1.25 WIDE, .157 DEEP. MAJOR REPAIR ACCOMPLISHED. CAUSED BY CONTACT WITH LOADER. INSTALLED DOUBLER REPAIR.SDR 2005UALA00257Overheat Loop · malfunctionedRETURNED TO ORD DUE TO NR 2 ENGINE OVERHEATED AND SHUTDOWN. CREW REPORTED NR 2 ENGINE OVERHEAT INDICATION AT CLIMB. CREW SHUT DOWN NR 2 ENGINE PER QRC. PERFORMED TROUBLESHOOTING OF THE OVERHEAT DETECTION SYSTEM. FOUND NR 2 ENGINE CORE DETECTOR M1122, LOOPSSDR 2005UALA00251Fire Loop · malfunctionedDIVERTED TO LNK DUE TO NR 2 ENGINE OVERHEAT INDICATION. SHUTDOWN NR 2 ENGINE AND BLEW BOTH FIRE BOTTLES. THERE WERE NO EVIDENCE OF FIRE OR OVERHEAT ON POST FLT INSP. REPLACED UPPER FAN OVERHEAT DETECTOR LOOP M1120. ENGINE OVERHEAT DETECTION SYSTEM TESTED NSDR 2005UALA00244Generator · failedRETURNED TO FIELD DUE TO A LOST NR 1 ENGINE GENERATOR. FOUND THE CSD OVERSERVICED, AND THE DELTA P INDICATOR POPPED. METAL SHAVINGS WERE FOUND IN THE FILTER BOWL, SO CSD OIL SYSTEM WAS FLUSHED AND SERVICED. BOTH THE CSD AND GENERATOR WERE REPLACED.SDR 2005UALA00245Overheat Loop · malfunctionedSHUT DOWN NR 2 ENG DUE TO OVERHEAT INDICATION. CREW REPORTED NR 2 ENG OVERHEAT LIGHT CAME ON WITH NO ABNORMAL ENGINE INDICATION. OVERHEAT LIGHT STAYED ON AFTER THE CHECKLIST. CREW SHUT DOWN NR 2 ENGINE. OVERHEAT LIGHT WENT OUT. UPON ARRIVAL AT THE GATE BOTHSDR 2005UALA00246Frame · damagedUPPER FRAME LT SIDE STA 178 HAS LOW EDGE DISTANCE. FABRICATED AND INSTALLED A REPAIR CHORD SPLICE ANGLE, PICKING UP AN ADDITIONAL FASTENER LOCATION.SDR ASMF200503012Pneumatic System · malfunctionedAIRCRAFT RETURNED TO PLATFORM DURING PUSH BACK, THE PNEUMATIC WAS NOT ENOUGH TO START THE ENGINES. THE ENGINES WERE STARTED WITH EXTERNAL PNEUMATIC PLANT IAW MM 49-50-00, TESTED CORRECT AND THE PNEUMATIC AUXILIARY POWER UNIT WAS DEFERRED IAW MEL 49-7. DURING TSDR AMTA200500257Slide · failedWHILE COMPLYING WITH WORK CARD 382F2501 L1 SLIDE, SN NG4084, FAILED TO DEPLOY WITH EITHER NORMAL OR MANUAL DEPLOY PROCEDURES. SLIDE WAS REPLACED AND OPS CHECK NORMAL. (K)SDR AU510002216A/C Pack · contaminatedSTRONG OIL SMELL IN COCKPIT AND CABIN. INVESTIGATION FOUND OIL CONTAMINATION OF THE AIR CONDITIONING AND PNEUMATIC SYSTEMS.SDR 2005UALA00235Skin · dentedDENT WITH SHARP BOTTOM ON RT SIDE OF FUSELAGE 36 INCHES BEHIND DOOR 1R AND 30 INCHES BELOW WINDOWS. DENT IS 1 INCH X 1 INCH WITH A 0.25 INCH CREASE, 0.65 INCH DEEP. CUT AND REMOVED DAMAGED, AND INSTALLED DOUBLER AND FILLER REPAIR.SDR 2005UALA00236Skin · dentedFOUND DENT IN HORIZONTAL STAB RT SIDE ABOUT 2 FEET IN FROM TIP. CUT OUT DAMAGED AREA AND INSTALLED DOUBLER REPAIR.SDR 2005FA0000417Light · misinstalledWHILE CLEANING LENS, IT APPEARED TO BE LOOSE IN THE HOUSING. A VERY GENTLE PULL RELEASED THE LENS FROM ITS HOUSING. THE LENS IS THICK GLASS THAT COULD BE A RUNWAY HAZARD IF IT FELL FROM THE AC AND BROKE. PROBABLE CAUSE IS SKYDROL WHICH LEAKED FROM RUDDER PCSDR 2005UALA00200Bear Strap · damagedAFT CARGO DOOR AFT LOWER CORNER BEAR STRAP DAMAGED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER AND TRIPLER REPAIR.SDR 2005UALA00192Seal · tornUNABLE TO PRESSURIZE THE AIRCRAFT. DOOR 1L LEAKING. SEAL TORN BY LOWER HINGE AREA. REPLACED LOWER HINGE SEAL. REPLACED L1 DOOR SNUBBER. ADJUSTED DOOR STOPS.SDR 2005UALA00186Sill · corrodedAFT PIT SIL BEAM UPPER STRAP HAS CORROSION FROM STA 847-787. REPLACED STRAP.SDR 2005UALA00183Floorbeam · corrodedCORROSION ON FWD LT CABIN FLOORBEAM AT STA 294.5 LBL 37-53. ACCOMPLISHED. BLENDED OUT DAMAGE AND INSTALLED ANGLE/STRAP REPAIR.SDR 2005UALA00184Pressure Panel · crackedSTA 664 PRESSURE DECK IS CRACKED AT APPROXIMATELY LBL 30. ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 2005UALA00172Frame · damaged178 BULKHEAD UPPER FRAME ANGLE LT SIDE AT SPLICE HAS 2 EACH HOLES WITH NO EDGE DISTANCE. TRIMMED THE DISCREPANT FRAME, FABRICATED AND INSTALLED REPAIR FRAME SPLICE ANGLE.SDR 2005UALA00158Connector · disconnectedEEL STRIP AT AFT GALLEY INOPERATIVE. FOUND POWER SOCKET DISCONNECTED. CONNECTED SOCKET.SDR AU510001950Probe · blockedAIRCRAFT SUFFERED MOTH STRIKES DURING TAKEOFF. CAPTAIN`S PITOT PROBE BLOCKED BY MOTH FOD.SDR AU510001951Bolt · looseNR 2 ENGINE THRUST REVERSER BLOCKER DOOR DRAG LINK/DOOR ATTACHMENT BOLT NUT AND WASHER MISSING ALLOWING BOLT TO DROP DOWN AND GOUGE AND DAMAGE DOOR BEYOND LIMITS.SDR AU510001842Regulator · faultyLT BLEED AIR FAILURE. BLEED AIR REGULATOR AND PRECOOLER CONTROL VALVE REPLACED. INVESTIGATION FOUND PRECOOLER CONTROL VALVE FAULTY. POPPET SET AND ADAPTER PLATE WORN. SIGNIFICANT CONTAMINATION INSIDE VALVE. BLEED AIR REGULATOR ALSO FAILED SHOP TEST. RELISDR 2005UALA00136Relay · failedAFTER TAKEOFF GEAR HANDLE WOULD NOT GO UP AND TAKEOFF WARNING HORN SOUNDING. REPLACED R276 RELAY AND ADJUSTED SAFETY SENSOR TARGET. PERFORMED EXTENSION AND RETRACTION CHECK OF THE LANDING GEAR. OPERATIONS CHECK GOOD.SDR 2005UALA00128Frame · crackedFWD CARGO DOOR CUTOUT FRAME CRACKED AT FWD LOWER STOP. MANUFACTURED AND INSTALLED REPAIR ANGLE DOUBLER.SDR AU510001546Radio · failedNR 2 HF RADIO NOT TRANSMITTING.SDR 2005UALA00114Skin · dentedRT HORIZ LEADING EDGE DENT APPROX 7 FT FROM INBOARD EDGE. DENT IS APPROX 5 INCHES IN LENGTH, 1.5 INCH WIDE AND .125 IN DEPTH. REPAIR ACCOMPLISHED. INTERIM DOUBLER REPAIR REPLACED WITH PERMANENT FLUSH REPAIR.SDR 2005UALA00113Relief Valve · out of adjustFLIGHT DIVERTED TO CMH DUE TO LOSS OF CABIN PRESSURE. THE INBOARD SAFETY RELIEF VALVE FAILED OPERATIONAL TEST AND WAS REPLACED. THE CABIN PRESSURE CONTROLLER WAS ALSO REPLACED PRECAUTIONARY.SDR 2005UALA00105Overheat Loop · damagedDIVERTED TO SFO DUE TO WING BODY OVERHEAT INDICATION. CREW REPORTED RIGHT WING BODY OVERHEAT LIGHT ILLUMINATED DURING CLIMB. PERFORMED TROUBLESHOOTING OF THE OVERHEAT DETECTION SYSTEM AND CONFIRMED A SHORT WITH RIGHT WING LEADING EDGE OVERHEAT DETECTOR LOOP MSDR 2005UALA00106Floorbeam · corrodedCABIN FLOORBEAM HAS CORROSION REMOVAL BEYOND LIMITS AT STA 967 LBL 18. INSTALLED STRAP REPAIR.SDR 2005UALA00107Skin · dentedVERTICAL STAB LEADING EDGE IS DENTED AT L/E STA 104. REMOVED DENT DAMAGE AND INSTALLED DOUBLER REPAIR.SDR 2005UALA00103Controller · failedAT 32,000 FEET CABIN, FLIGHT MADE EMERGENCY DESCENT FROM 32,000 TO 15,000 DUE TO CABIN PRESSURE PROBLEM. CABIN PRESSURE CONTROLLER FAILED. REPLACED CONTROLLER.SDR 2005UALA00104Unknown · unknownRETURNED TO SFO DUE TO PRESSURIZATION PROBLEM. FOUND EXCESSIVE LEAK AROUND E&E COMPARTMENT DOOR. REPLACED E&E COMPARTMENT DOOR SEAL.SDR 2005UALA00097Skin · dentedLEFT HORIZONTAL STABILIZER HAS A DENT IN THE LEADING EDGE, FOUND DENT APPROX 4 FT OUTBD ON L/E HORZ STAB. DIMENSIONS ARE 3 INCH BY 2 INCH BY .25 INCH DEEP WITHIN 1 INCH OF FASTENERS. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INTERIM DOUBLER REPAIRSDR 2005UALA00098Skin · dentedLT HORIZ STAB LEADING EDGE IS DENTED APROX 4' FROM FUSE. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REMOVED DENT DAMAGE AND INSTALLED DOUBLER REPAIR.SDR 2005UALA00090Light · inoperativeAFT CABIN EEL LIGHTS INOP FROM ROWS 15 TO AFT GALLEY. REPLACED EEL CABLE AND MISSING END CAP.SDR 2005UALA00084Indicator · malfunctionedABORTED TAKEOFF DUE TO F/O AIR SPEED INDICATOR. REPLACED FIRST OFFICERS AIR SPEED INDICATOR.SDR 2005UALA00083Frame · damagedBS 178 BULKHEAD ON THE UPPER LT CHORD WAS FOUND TO HAVE INSUFFECENT EDGE DISTANCE AT WL 230 FOR REQUIRED OVERSIZING OF FASTENER HOLES. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND INSTALLED SPLICE REPAIR.SDR 2005UALA00075Floorbeam · corrodedSTA 294 FLOORBEAM UPPER CAP HAS MATERIAL LOSS FROM CORROSION REMOVAL AT RBL 39 TO RBL 52. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. CUTOUT DAMAGED SECTION AND INSTALLED DOUBLE FLANGE REPAIR.SDR 2005UALA00076Pressure Panel · crackedSTA 664 PRESSURE DECK HAS 2 CRACKS AT LBL 30. CUT-OUT WEB AND INSTALLED SPLICE REPAIR.SDR 2005UALA00077Skin · dentedLT FUSE SKIN IS DENTED AT STA 897 BETWEEN STR 24L AND 25L. SUPPLEMENTAL DATA UPDATE, MAJOR REPAIR ACCOMPLISHED. CUT-OUT DAMAGE AND INSTALLED REPAIR DOUBLER, TRIPLER AND FILLER.SDR 2005UALA00078Skin · dentedSTA 341-359 HAS 3 DENTS ABOVE STR 21R. CUT OUT DAMAGE AND INSTALLED DOUBLER AND TRIPLER REPAIR.SDR 2005UALA00069Stringer · crackedSTR 16 RT HAS A CRACK AT STA 498B JUST AFT OF LIGHT ASSY. SUPPLEMENTAL DATA UPDATE, MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SECTION FROM STRINGER AND INSTALLED SPLICE REPAIR.SDR 2005UALA00073Floorbeam · corrodedSTA 986 FLOORBEAM FWD FLANGE HAS CORROSION FROM RBL 16 TO RBL 41. DATA MAJOR CUT-OUT DAMAGE AND INSTALLED REPAIR ANGLE AND FILLER.SDR 2005UALA00062Drain Valve · not closedAT FL250 UNABLE TO HOLD CABIN ALTITUDE. CABIN CLIMBING AT 1000 FPM. DRAIN VALVE IN BOTH THE AFT CARGO PIT AND E/E DOOR NOT CLOSING. LUBED FWD ONE AND CLEANED DEBRIS FROM AFT PIT DOOR VALVE.SDR 2005UALA00063Floorbeam · corrodedFLOORBEAM CORRODED ON AFT FLANGE STA 986 FROM RBL 10 TO LBL 6. SUPPLEMENTAL DATA UPDATE, MAJOR REPAIR ACCOMPLISHED. CUT-OUT DAMAGE AND INSTALLED REPAIR ANGLE AND FILLER.SDR 2005UALA00072Floorbeam · corrodedFLOORBEAM AT STATION 947 HAS CORROSION FROM LBL 14 TO RBL 53. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. SPLICED IN NEW SECTION OF FLOOR BEAM.SDR 2005UALA00074Skin · dentedDENT FOUND AT LT SIDE OF FUSELAGE 3 FT AFT OF DOOR 1L SILL. CUT-OUT DAMAGE AND INSTALLED DOUBLER AND TRIPLER REPAIR.SDR A6WA200440204Keelbeam · crackedKEEL BEAM LOWER CHORD BS 685-695 IS CRACKED. TRIMMED OUT CRACKED LOWER CHORD. INSTALLED REPAIR ANGLE AND STRIP.SDR 2005UALA00055Frame · crackedSTA 616 FRAME INNER CHORD IS CRACKED FROM BOTTOM FASTENER BELOW STR 17 LT. CUT-OUT DAMAGE AND INSTALLED ANGLE DOUBLER.
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