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 AWXA200300346Structure · delaminatedYVR - MAJOR REPAIR - DURING C-16 CHECK THE UPPER SURFACE, INBOARD CORNER OF THE NR 4 SLAT WAS FOUND DELAMINATED. MAINTENANCE REMOVED NR 4 SLAT, REPAIRED DAMAGE IAW SRM 51-70-10, FIG. 32, PG. 88I, RE-INSTALLED SLAT AND RIGGED SYSTEM IAW BMM 27-81-21, PG. 414-41SDR AWXA200300347Structure · delaminatedYVR - MAJOR REPAIR - DURING C-16 CHECK THE UPPER SURFACE OUTBOARD TRAILING EDGE OF THE NR 2 SLAT WAS FOUND DELAMINATED. MAINTENANCE REMOVED AND REPLACED NR 2 SLAT IAW BMM 27-81-21, PG. 401-419.SDR 2003UALA00267Actuator · malfunctionedAIRCRAFT PREPARED FOR DIVERSION WHEN LEADING EDGE FLAP DID NOT DEPLOY. LEADING EDGE FLAP DEPLOYED ON FINAL APPROACH, AND AIRCRAFT LANDED AT PLANNED DESTINATION. THE NR 1 FLAP ACTUATOR WAS REPLACED. ACTUATOR WAS REMOVED AND SENT TO SHOP FOR REWORK.SDR 2003UALA00250Floorbeam · corrodedAFT CABIN FLOOR BEAM CORRODED AT STA 986 RBL 7 TO RBL 44. MAJOR REPAIR ACCOMPLISHED. T-CAP REPAIR AND SPLICE REPAIR.SDR 2003UALA00249Frame · corrodedFWD PIT STATION 482 TO 482B STRINGER 25R TO STRINGER 26R IS CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED EXTERNAL SKIN DOUBLER.SDR 2003UALA00231Frame · crackedSTATION 188 FRAME CRACKED RT SIDE WL 207. SUPPLEMENTAL DATA UPDATE, MAJOR REPAIR ACCOMPLISHED. FRAME REPAIRED. SIDE DOUBLER INSTALLED.SDR 2003UALA00247Bulkhead · crackedFUSELAGE BULKHEAD WEB HAS 2EA CRACKS BS178 RBL6 WL200. ACCOMPLISHED MAJOR REPAIR ACCOMPLISHED. SPLICED WEB REPAIR.SDR 2003UALA00248Frame · crackedBS 188 RT FUSELAGE FRAME CRACKED IN RADIUS ON AFT SIDE AT WL208. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 373PA0009Battery · inoperativeEMERGENCY LIGHT INOPERATIVE AT SEAT 21D. REPLACED BATTERY.SDR 2003UALA00230Skin · crackedE AND E COOLING OUTFLOW CUTOUT SKIN IS CRACKED. MAJOR REPAIR ACCOMPLISHED. SKIN REPAIRED.SDR 2003UALA00226Crease Beam · corrodedSTATION 293 THRU 351, RBL 59, FORWARD CABIN RIGHT CREASE BEAM CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW SECTION.SDR 2003UALA00227Skin · dentedEXTERNAL FUSELAGE HAS 3 EA DENTS BELOW AND ABOVE DOUBLER STA 384 - 390 S17L. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW DOUBLER.SDR 2003UALA00228Frame · crackedLEFT STATION 188 FRAME CRACKED IN RAD ON AFT SIDE JUST ABOVE FLOOR LINE. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE REPAIR AND EXTERNAL SKIN DOUBLER.SDR 2003UALA00232Light · shortedEMERGENCY EXIT FLOOR LIGHTING (EEL) NOT VISIBLE FROM ROW 15 AFT. FOUND AFT GALLEY SHORTING THAT PORTION OUT. REPLACE AND GROUND CHECKS OKAY.SDR 2003UALA00222Frame · crackedSTATION 188 FRAME CRACKED AT WL 207 LEFT HAND SIDE. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER.SDR 2003UALA00223Crease Beam · damagedAFT ENTRY DOOR THRESHOLD CREASE BEAM OUTER CHORD ROUTED OUT BEYOND LIMITS STATION 968 STRINGER 17L. MAJOR REPAIR ACCOMPLISHED. INSTALLED STRAP REPAIR.SDR 2003UALA00213Door Frame · crackedFORWARD GALLEY DOOR FRAME IS CRACKED AT FLOOR STATION 294.5. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED AND INSTALLED REPAIR DOUBLER.SDR USAASB03030Engine · surgesAFTER LIFTOFF, CAPTAIN REPORTED THE NR 2 ENGINE RAPIDLY SURGED BACK AND FORTH. APPROXIMATE N1 WAS FROM 77 PERCENT TO 85 PERCENT WITH FUEL FLOW INCREASING TO 8,000 POUNDS AND EGT INCREASING TO 800 DEGREES. CREW PULLED THE NR 2 ENGINE THROTTLE BACK TO IDLE ANDSDR 2003UALA00201Crease Beam · corrodedAFT CABIN FLOOR STRUCTURE, INNER CREASE BEAM AT STRINGER 17R BETWEEN STA. 947.5 TO 990 IS CORRODED. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW CREASEBEAM PART.SDR 2003UALA00210Bulkhead · crackedSTATION 178 BULKHEAD UPPER RIGHT ANTENNA MOUNT UPPER OUTBOARD ATTACH POINT HAS CRACK INDICATION. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED AND INSTALLED REPAIR DOUBLER.SDR 2003UALA00198Turbine Wheel · failedAPU HAD AUTO SHUTDOWN EVENT AT DEPARTURE GATE AS THE RESULT OF THE APU TURBINE FAILURE. THERMAL FATIGUE BLADE FAILURE. MINIMAL DUE TO RATE OF INCIDENTS: MTBF IS 2,414,347 HOURS AND 3,380,158 CYCLES. TRENDING WHEEL PERFORMANCE. CONSIDER DEVELOPMENT OF ON-WINGSDR 2003UALA00193Frame · damagedSKIN IS CREASED NEAR THE FORWARD LAV SERVICE PANEL. 2 CREASES ARE WITHIN LIMITS OF SRM, BUT DAMAGE TO FRAME IS BEYOND LIMITS. MANUFACTURED AND INSTALLED DOUBLER REPAIR.SDR 2003UALA00292Frame · crackedSTATION 188 LT FUSELAGE FRAME CRACKED IN RADIUS ON AFT SIDE AT WL 208. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED & INSTALLED REPAIR ANGLES.SDR 2003UALA00293Frame · crackedSTATION 178 BULKHEAD LT SIDE FRAME CRACKED ABOVE AND BELOW WL 207. MAJOR REPAIR ACCOMPLISHED. SPLICED SIDE FRAME.SDR 2003UALA00294Frame · crackedSTATION 178 BULKHEAD RH SIDE FRAME CRACKED ABOVE AND BELOW WL 207. MAJOR REPAIR ACCOMPLISHED. SPLICED SIDE FRAME.SDR 2003UALA00178Skin · damagedFUSELAGE SKIN DAMAGED AT STATION 815 STRINGER 18R. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR 2003UALA00184Bulkhead · wornFWD SURFACE OF AFT PRESSURE BULKHEAD BS 1016, SKIN IS WORN AT EDGE APPROXIMATELY THREE THIRTY POSITION OF CUTOUT FOR APU PNEUMATIC BLEED AIR DUCT. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR INSTALLED.SDR 2003UALA00183Flap · malfunctionedAIRCRAFT MADE A LANDING UNDER AMBER ALERT BECAUSE OF A FLAP SYMMETRY PROBLEM.SDR 2003UALA00176Skin · damagedRIGHT LOWER FUSELAGE SKIN HAS EXCESSIVE MATERIAL LOSS 25 PERCENT, .036 ORIG . 027 AT DEEPEST AREA. STA 450 S25R AND STATION 435 4 IN BELOW LOWER AFT CORNER OF FORWARD CARGO DOOR CUTOUT. MAJOR REPAIR ACCOMPLISHMENT. INSTALLED REPAIR DOUBLER AND FILLER.SDR 2003UALA00166Stringer · dentedAFT CABIN FUSELAGE STRINGER OUTBOARD SURFACE DENTED APPROXIMATELY BODY STATION 1004 STRINGER 14L. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER.SDR 2003UALA00167Frame · crackedLT STATION 188 FRAME IS CRACKED AT WL 207. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED MODIFIED FRAME.SDR 2003UALA00168Frame · crackedSTATION 188 RT SIDE FRAME CRACKED IN RADIUS AT WL 207. MAJOR REPAIR ACCOMPLISHED. MANUFACTURED AND INSTALLED RT SIDE FRAME.SDR 2003UALA00164Crease Beam · corrodedCABIN RT CREASE BEAM WEB CORRODED BETWEEN BODY STATION 727B AND BODY STATION 727C. MAJOR REPAIR ACCOMPLISHED. REPLACED RT CREASE BEAM WEB.SDR AWXA200300113Wire · brokenDURING INSPECTION ROW 13 LT ESCAPE PATH LIGHTING WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHTING HARNESS AT SEAT ROW 13 LT, OPERATIONAL CHECK WAS GOOD.SDR 2003UALA00149Bulkhead · crackedSTATION 178 BULKHEAD WEB CRACKED AT WL 199 LBL 5.7. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR.SDR 2003UALA00150Frame · crackedSTATION 616 WL 208 LT BODY FRAME CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE REPAIR.SDR 2003UALA00153Floorbeam · crackedCABIN FLOOR INTERCOSTAL UPPER FLANGE CRACKED AT FASTENER HOLES, STA 927-947 AT CENTERLINE. MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR ANGLE.SDR 2003UALA00154Frame · crackedLEFT FUSELAGE WING ROOT FRAME CRACKED AT STATION 540 S22L. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR.SDR 2003UALA00146Bulkhead · crackedSTATION 178 BULKHEAD WEB CRACKED AT WL 199 RBL 5.7 MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR.SDR 2003UALA00147Frame · crackedCABIN BODY STUB FRAME IS CRACKED BS 296 RT WL 257-277. MAJOR REPAIR ACCOMPLISHED. REPLACED STUB FRAME.SDR 2003UALA00148Frame · crackedCABIN FRAME WEB CRACKED AT STATION 616 LT, WL 205. MAJOR REPAIR ACCOMPLISHED. FABRICATED AND INSTALLED NEW WEB SECTION AND SPLICE DOUBLER.SDR 2003UALA00142SwitchEMERGENCY EXIT "NOT ARMED" LIGHT DOES NOT ILLUMINATE WHEN SYSTEM IS OFF SUPPLEMENTAL DATA UPDATE REPLACED EMER EXIT LIGHT SWITCH S7. OPS CKECKED NORMAL.SDR 2003UALA00127Floorbeam · corrodedCABIN FLOORBEAM UPPER FLANGE HAD EXCESSIVE CORROSION AT STATION 360 RBL 5 IN TO LBL 18IN STRINGER 17L-17R. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW SECTION OF T-CAP MOUNTED ON AFT SIDE OF VERTICAL WEB WITH 9.5 IN, L-ANGLE SPLICES FWD AND AFT OF EACH CUT, FOURSDR 2003UALA00138Intercostal · corrodedCABIN FLOOR INTERCOSTAL AT STATION 1009 TO 1016 LBL 5 TO 9, STRINGER 17L HAD UPPER FLANGE CORRODED TO EXCESS. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW VENDER PART [I-CHANNEL ].SDR 2003UALA00139Floor Support · corrodedCABIN FLOOR SUPPORT AT STATION 335 RBL 52 TO 60, STRINGER 17R HAD EXCESSIVE CORROSION. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW VENDOR T -ANGLE SUPPORT.SDR 2003UALA00140Channel · corrodedCABIN FLOOR INTERCOSTAL AT STATION 328 TO 344 RBL 51 STRINGER 17R CORRODED. MAJOR REPAIR ACCOMPLISHED. REMOVED INTERCOSTAL EXTRUSION CHANNEL AND REPLACED WITH NEW VENDER PART.SDR 0300153243Controller · malfunctionedDURING CLIMB RECEIVED CABIN PRRESSURE EXCESS CABIN ALTITUDE MESSAGE AT 10,000 FT. LEVELED OFF AT 11,000 FT AND MESSAGE WENT AWAY. CLIMBED TO 12,800 FT AND MESSAGE RETURNED. LEVELED OFF AT 12,000 FT AND MESSAGE CLEARED FOLLOWED SHORTLY BY THE SAFETY VALVE OPENISDR 2003UALA00129Girt Bar · inoperativeGIRT BAR AT DOOR 2L WILL NOT STAY ENGAGED DURING TAKEOFF AND LANDING. REPLACED SLIDE. SLIDE AND GIRT BAR HAVE BEEN EXAMINED BY THE SHOP. NO DEFECTS FOUND.SDR 2003UALA00120Frame · crackedSTATION 188 RT FRAME CRACKED AT WL 207. MAJOR REPAIR ACCOMPLISHED. DOUBLER INSTALLED.SDR 2003UALA00121Pressure Panel · crackedMLG WHEEL WELL PRESSURE PANEL CRACKED AT STA 670 LBL33, OUTBOARD AND AFT OF AILERON TOWER SHAFT. SUPPLEMENTAL DATA UPDATE MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER.
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