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 2005UALA00056Floorbeam · corrodedSTA 947 FLOORBEAM HAS MATERIAL LOSS FROM CORROSION AT LBL 4. REMOVED CORROSION INTALLED REPAIR STRAP.SDR 2005UALA00057Keelbeam · crackedKEEL BEAM LOWER CHORD BS 685-695 IS CRACKED. TRIMMED OUT CRACKED LOWER CHORD. INSTALLED REPAIR ANGLE AND STRIP.SDR AU510002206Tire · failedNR 2 MAIN WHEEL TIRE TREAD SEPARATED. TIRE WAS RETREAD LEVEL R2. DAMAGE WAS CAUSED TO THE LT INBOARD TRAILING EDGE FLAP AND LT INBOARD LOWER WING FIXED TRAILING EDGE PANEL.SDR 2005UALA00047Stringer · crackedSTATION 482 STRINGER 16R IS CRACKED. INSTALLED SPLICED REPAIR.SDR 2005UALA00049Csd · overservicedDIVERTED TO SLC DUE TO ELECTRICAL PROBLEMS. FOUND CSD OVERSERVICED WITH OIL. CHECKED CSD CHIP DETECTOR, ALL DIFF. PRESSURE INDICATORS, ALL OK. SERVICED OIL TO PROPER LEVEL. RAN ENGINE AT IDLE. RESIDUAL VOLTS=19, FREQS 400, 119 VOLTS ALL NORMAL. GENERATOR OPS.SDR 2005UALA00046Stringer Clip · crackedSTRINGER CLIP IS CRACKED AT STA 685 STR 3L. REPLACED STRINGER CLIP.SDR 2005UALA00048Shear Web · crackedLEFT SHEAR WEB AT STA 194 IS CRACKED AT WL 207. REPLACED SHEAR WEB.SDR AU510001685Actuator · failedNR 2 ENGINE SPAR VALVE ACTUATOR FAILED. NR 2 ENGINE FAILED TO START.SDR 2005UALA00040Fire Detector · malfunctionedAPU FIRE LIGHT ILLUMINATED WITH THE APU SHUTDOWN. CREW REPORTED THAT AFTER TAKEOFF THEY HAD APU FIRE WARNING INDICATION WITH THE APU SHUTDOWN. CREW DISCHARGED APU FIRE BOTTLE. APU FIRE WARNING INDICATION WENT OUT THEN BEGAN TO FLASH AND CAME BACK ON STEADY. SDR 2005UALA00025Seal · leakingAIRCRAFT RETURNED WITH CABIN PRESSURE PROBLEM. SEAL REPLACED AND RIGGED THE FORWARD CARGO DOOR.SDR MAMA040915Door · leakingAIRCRAFT RETURNED WITH CABIN PRESSURE PROBLEM.SDR 2005UALA00008Warning System · activatedABORTED TAKEOFF AT 100 KNOTS DUE TO WINDSHEAR WARNING INDICATION. OPS CHECK OF WEATHER RADAR TRANSCEIVER PERFORMED, AND NO FAULT FOUND.SDR 2005UALA01298Warning System · activatedABORTED TAKEOFF AT 100 KNOTS DUE TO WINDSHEAR WARNING INDICATION. REPLACED EMERGENCY LIGHT ON SEAT 42R.SDR 2005UALA00026Sensing Element · damagedCREW REPORT NR 1 ENG -A- OVERHEAT LIGHT ILLUMINATED. *S/D* CREW REPORTED NR 1 ENGINE -A- LOOP OVERHEAT LIGHT ILLUMINATED. SHUTDOWN ENGINE AND DISCHARGED BOTH FIRE EXTINGUISHER BOTTLES. OVERHEAT DETECTION LOOP -B- WAS INOPERATIVE AND DEFERRED, ELIMINATING RSDR 2004UALA01256Skin · dentedVERTICAL FIN L/E SKIN HAS A DENT AT LES 132. DENT IS 1.55 BY 0.046 INCH DEEP. DENT IS A ZONE 3 DENT. INSTALLED FLUSH REPAIR.SDR 2004UALA01251Windshield · crackedDIVERTED DUE TO FIRST OFFICER'S WINDSHIELD CRACKED. WINDOW HEATING ELEMENT ARCED. REPLACED WINDOW.SDR 2004UALA01249Smoke · detectedFLIGHT ATTENDANT SAW SMOKE COMING FROM AFT GALLEY TRASH COMPACTOR AREA. LINE MAINTENANCE ACCOMPLISHED A DETAILED INSPECTION AND OPERATIONAL CHECK ON THE SUSPECT TRASH COMPACTOR. NO EVIDENCE OF SMOKE WAS FOUND ON THE DETAILED INSPECTION, AND A SUBSEQUENT OPERASDR 2004UALA01244Switch · malfunctionedGEAR WOULD NOT RETRACT AFTER TAKEOFF. FLIGHT DIVERTED. A FAILED S106 LANDING GEAR SAFETY SWITCH CAUSED THE AIRCRAFT TO REMAIN IN THE GROUND MODE, RESULTING IN THE GEAR FAILING TO RETRACT. THE S106 LANDING GEAR SAFETY SWITCH WAS REPLACED AND THE LANDING GEAR SDR 2004UALA01231Fan · failedLANDED UNDER AMBER ALERT DUE TO REPORTED SMOKE IN CABIN. FOUND EQUIPMENT COOLING NORMAL FAN FAILED. REPLACED NORMAL FAN.SDR 2004UALA01232Gcu · malfunctionedDIVERTED TO TWF (TWIN FALLS, ID) DUE TO LEFT GENERATOR BUSS FAILURE. AIRCRAFT EXPERIENCED ELECTRICAL FAILURE WHILE CLIMBING. NR 1 GEN OFF BUS LIGHT WITH ASSOCIATED "BUSS OFF" LIGHT ILLUMINATED. TRANSFER BUS LIGHT DID NOT ILLUMINATE BUT HAD BOTH LT TANK FUELSDR 2004UALA01214Light · looseEMERGENCY EXIT FLOOR LIGHTS AT ROW 12 HAVE BEEN PULLED UP. REPLACED DAMAGED EEL STRIP.SDR 2004UALA01216Light · inoperativeAFT EMERGENCY FLOOR EEL LIGHTS INOP FROM MID TO AFT OF AIRCRAFT. REPLACED EEL LIGHTS MID TO AFT GALLEY.SDR SWAA043602Blade · tornDURING SCHEDULED HC2 CHECK, FOUND NR 2 ENGINE 8TH STAGE HPC ROTOR HAS 1 EACH BLADE TORN. REMOVED AND REPLACED NR 2 ENGINE PER MT 771-00-01.SDR 2004UALA01213Switch · failedDIVERTED TO LAS DUE TO A CABIN PRESSURE PROBLEM OUT OF LAX. WHEN TROUBLE SHOOTING INTERFACING SYSTEM ON E11 "LANDING GEAR LOGIC SHELF", M1110 "NOSE GEAR GROUND SENSING PROXIMITY SWITCH" FAILED. IN ADDITION, MAIN LANDING GEAR GROUND SAFETY SENSOR FOUND OUT OFSDR 2004UALA01203Slide · deployedDURING SERVICING, CATERERS REPORTED THAT THE DOOR 1R WAS OPEN AND HAD THE SLIDE PARTIALLY DEPLOYED. THE DOOR WAS NOT DISARMED. CAUSE IS UNKNOWN. A SLIDE COMPARTMENT (CLAMSHELL) LATCH WAS FOUND OPENED DURING INSPECTION. WHETHER THE LATCH WAS OPENED WHILE ISDR 2004UALA01202Transmitter · malfunctionedRETURNED TO GATE AFTER 90 KNOT ABORTED TAKEOFF DUE TO OIL PRESSURE INDICATION. ENG 2 OIL PRESSURE WENT TO ZERO. REPLACED NR 2 OIL PRESSURE INDICATOR, OIL TEMPERATURE INDICATOR AND OIL PRESSURE TRANSMITTER. RAN ENGINE AND OPS CHECKED OK. THEN ON DEC 15, OILSDR 2004UALA01191Pump · failedB-ELECTRIC PUMP OVERHEAT LIGHT ILLUMINATED. FUNCTIONAL BENCH TEST FAILED IN THE SHOP. NUMEROUS PARTS REPLACED DURING OVERHAUL OF UNIT (BEARINGS, CYLINDER BLOCK, MATING RING, ETC.).SDR 2004UALA01184Warning Light · activatedFLIGHT RETURNED TO DEN DUE TO B-SYSTEM HYDRAULIC PRESSURE LIGHT. PROBLEM COULD NOT BE REPEATED ON GROUND. OPS CHECKED OK. NO UNITS REPLACED.SDR 2004UALA01173Overheat Loop · failedDIVERTED TO SLC DUE TO WING BODY OVERHEAT INDICATION. DISCREPANCY FOUND TO BE NR 2 ENGINE, STRUT CAVITY OVERHEAT DETECTOR ELEMENT FAULT. REPLACED OVERHEAT DETECTOR SENSING ELEMENT OF NR 2 ENGINE STRUT CAVITY .SDR 2004UALA01164Proximity Sensor · malfunctionedRETURNED TO DEN, DUE TO A GEAR IN TRANSIT LIGHT PROBLEM. INDICATION WAS CAUSED BY FAULTY GEAR DOWN LOCK PROXIMITY SWITCH. REPLACED GEAR DOWN LOCK SWITCH. PERFORMED OPERATIONAL AND FUNCTIONAL CHECK OF THE SYSTEM. GEAR OPEARTION AND INDICATION FOUND NORMAL.SDR 2004UALA01149Overheat Loop · failedDIVERTED TO PIT DUE TO WING BODY OVERHEAT INDICATION. DISCREPANCY FOUND TO BE NR 2 ENGINE, STRUT CAVITY OVERHEAT DETECTOR ELEMENT FAULT. REPLACED OVERHEAT DETECTOR SENSING ELEMENT OF NR 2 ENGINE STRUT CAVITY .SDR 2004UALA01172Cylinder · damagedSQUIB FIRED A HOLE STRAIGHT THROUGH THE CYLINDER. FIRE EXTINGUISHER BOTTLE AND CARTRIDGE WERE SUBJECTED TO AN ABNORMALLY HIGH AMBIENT TEMP, NOT CONSISTENT WITH THE DESIGN PARAMETERS OF BOTH UNITS, AND THEY FUNCTIONED AS EXPECTED. THE ELEVATED AMBIENT TEMPERATUSDR 2004UALA01138Light · inoperativeLAST 6 ROWS OF EMERGENCY FLOOR LIGHTING INOP. REPLACED POWER STRIP FOR AFT SET OF FLOOR LIGHTS. CHECKS GOOD.SDR 2004UALA01128Wire · failedEEL LIGHTS INOPERATIVE FROM SEATS 17 TO AFT GALLEY. REPLACED FLOOR FEEDER CABLE FOR EEL LTS FROM ROW 17 BACK.SDR 2004UALA01124Frame · damagedSTA 986 FRAME I/B FLANGE HAS AN ELONGATED FASTENER HOLE AT WL 206. INSTALLED ANGLE DOUBLER REPAIR.SDR 2004UALA01112Skin · crackedFWD GALLEY DOOR EXT SKIN IS CRACKED AT THE LWR HINGE CUTOUT. TRIMMED OUT DAMAGE AND INSTALL REPAIR DOUBLER.SDR 2004UALA01123Beam · corrodedAFT CARGO DOOR LWR SILL BEAM UPPER WEB HAS CORROSION. *S/D* MAJOR REPAIR ACCOMPLISHED. REPLACED WEB.SDR 2004UALA01111Floorbeam · corrodedSTA 986 FLOOR BEAM UPR CAP HAS CORROSION AT RBL 16 . SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. SPLICED UPR T-CAP SECTION AT STA 986 FROM RBL 24 TO LBL 65.SDR 2004UALA01122Structure · damagedFWD CARGO PIT HAS DAMAGE JUST AFT OF EXISTING REPAIR. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. REMOVED EXISTING REPAIR TO INCLUDE NEW REPAIR. REMOVED DAMAGE AS NEEDED. INSTALLED DOUBLER REPAIR.SDR 2004UALA01134Bulkhead · damagedSTATION 178 FWD BULKHEAD IS DAMAGED. ACCOMPLISHED ULTRASONIC INSPECTION ALONG THE STIFFENER AT WATER LINE 195 FROM THE AFT SIDE OF THE WEB. REPLACED BS 178 BULKHEAD WEB.SDR 2004UALA01120Bear Strap · damagedREPAIR AT AFT CARGO DOOR BEAR STRAP BS 807 ABOVE STR 25 RT AT CARGO DOOR OPENING IS INSUFFICIENT. FABRICATED EXTERNAL DOUBLER,TRIPLER AND FILLER AND INSTALLED,SDR 2004UALA01121Bear Strap · damagedAFT CARGO DOOR BEAR STRAP REPAIR NEEDS TO BE REPLACED AT BS 847 STR. 23R. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED REPAIR DOUBLER.SDR 2004UALA01043Lamp · burned outEMERGENCY EXIT EXTERIOR LIGHT AT DOOR 1R INOP. LAMP HAD REPORTEDLY "BURNED OUT" AND WAS REPLACED BY MAINTENANCE.SDR 2004UALA01044Oxygen Gen · activatedPSU LT NR 10 OXYGEN GENERATOR HEAT SENSITIVE BAND IS BLACK. RELEASE PIN INADVERTENTLY PULLED. REPLACED AND INSTALLED NEW OXYGEN GENERATOR.SDR 2004UALA01133Slide · dislodgedDOOR 1L SLIDE HAS SLID DOWN FROM ITS MOUNT. UNIT WAS INSPECTED AND FOUND TO BE OK. SLIDE WAS REINSTALLED.SDR 2004UALA01041Overheat Loop · malfunctionedDIVERTED TO COS DUE TO WING BODY OVERHEAT INDICATION. EXPERIENCED RIGHT WING BODY OVERHEAT WARNING IN FLIGHT WITH ENGINE SUPPLYING AIR. ISOLATED TO RIGHT WING LEADING EDGE OVERHEAT DETECTOR LOOP M1204. REPLACED OVERHEAT DETECTOR LOOP M1204. SYSTEM OPERATIOSDR 2004UALA01126Wire · failedEMERGENCY EEL LIGHTS ROWS 15ABC TO 21ABC ARE INOPERATIVE. REPLACED LOWER FEEDER WIRE.SDR 2004UALA01132Skin · crackedAFT SERVICE DOOR OPENING HAS CRACK AT FWD LOWER CORNER. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED SCUFF PLATE AND TAPERED SHIM.SDR 2004UALA01035Shear Web · crackedSTA 194 SHEAR WEB IS CRACKED AT WL 208 RBL 16. REPLACED SHEAR WEB.SDR 2004UALA01036Shear Web · crackedSTA 194 SHEAR WEB IS CRACKED AT WL 208 LBL 16. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR WEB.
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