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 2003UALA00436Light · inoperativeFLIGHT DECK EMERGENCY LIGHT INOPERATIVE.SDR 2003UALA00421Skin · damagedEXTERNAL FUSELAGE SKIN DAMAGED AT STA 1050 ALONG CENTERLINE 36 INCHES FWD OF APU ACCESS DOOR. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND SKIN DOUBLER REPAIR.SDR 2003UALA00422Light · inoperativeFLOOR EEL LIGHTS AFT THIRD OF CABIN INOPERATIVE. CLEANED CONNECTOR AT AFT GALLEY POWER STRIP.SDR 2003UALA00425Warning Light · illuminatedAIRCRAFT HAD AN UNSAFE GEAR INDICATION ON APPROACH. FLEW A MISSED APPROACH AND USED ALTERNATE GEAR EXTENSION PROCEDURE.SDR S03853022Skin · damagedB-18611 FUSELAGE SKIN FLUSH REPAIR LOCATED BETWEEN STA. 360 TO 380 / S-20R TO S-21R. REPAIR IAW EO 738-53-00-0021. TO MEET REQUIREMENT OF CCAA AD 2003-03-020.SDR AWXA200300518Valve · openSTL - DIVERSION - FLT 0126 - EN ROUTE FROM PHX TO MKE, NR 2 ENGINE COWL ANTI-ICE VALVE FAILED TO OPEN, DUE TO ICING CONDITIONS DIVERTED TO STL. MAINTENANCE AT STL COMPLIED WITH MEL PROCEDURE 30-3, COND 4, OPENING OF THE NR 2 ENGINE COWL ANTI-ICE VALVE. WHEN SDR 2003UALA00413Light · inoperativeEEL FLOOR LIGHTING INOPERATIVE FROM ROW 15 THROUGH AFT GALLEY. REPLACED 4 EEL LIGHTS AND ONE EEL CABLE. OPS CHECK OK.SDR 2003UALA00411Light · inoperativeEEL FLOOR LIGHTING INOPERATIVE FROM ROW 15ABC THROUGH AFT GALLEY. *S/D* REPLACED EEL 4 EACH LIGHTS AND EEL CABLE. OPS CHECK OK.SDR 2003UALA00408Skin · gougedBELLY SKIN AREA OF THE AFT FUSELAGE DRAIN MAST IS GOUGED. MAJOR REPAIR ACCOMPLISHED. STRINGER SPLICE, FILLER & DOUBLER REPAIR.SDR 2003UALA00410Apu · fireAPU CAUGHT ON FIRE AT GATE. AFTER REMOVAL THE APU DISPLAYED VERY LITTLE EVIDENCE OF FIRE. THE FADEC CONTROL UNIT WAS CAPTURED FOR THE DOWN LOAD OF THE NON-VOLITILE MEMORY. DATA INDICATED NO UNUSUAL OCCURENCES DURING THE OPERATION OF THE ENGINE AT THE TIME DOSDR 2003UALA00404Controller · malfunctionedAIRCRAFT DIVERTED ENROUTE BECAUSE THE CABIN PRESSURE BECAME UNCONTROLLABLE. CABIN PRESSURE CONTROLER (CPC) FAILED DUE TO INTERNAL FAULT. REPLACED THE CABIN PRESSURE CONTROLER, THAN PRESSURIZED AIRCRAFT USING APU IN AUTO, STANDBY AND MANUAL TO ENSURE CORRECT SDR AUS20030452Brake · failed(AUS) NR 2 MAIN BRAKE FAILED. INSPECTION FOUND SMALL METAL CHIPS AROUND BRAKE AND IN WHEEL HUB.SDR 2003UALA00394Wire · defectiveEMERGENCY EXIT LIGHTING (EEL) AFT OF ROW 16 WAS INOPERATIVE. *S/D* REPLACED 18 FT SECTION OF EEL CABLE.SDR AUS20030434Filter · faulty(AUS) HYDRAULIC RESERVOIR PRESSURE MODULE FILTER SUSPECT FAULTY.SDR 2003UALA00430Wedge · damagedHAIL DAMAGE OCCURRED TO T/E WEDGE, NR 2 SLAT. REPAIRED T/E WEDGE, SLAT NR 2.SDR 2003UALA00431Wedge · damagedHAIL DAMAGE OCCURRED TO T/E WEDGE, NR 3 SLAT. REPAIRED T/E WEDGE, SLAT NR 3.SDR 2003UALA00433Wedge · damagedHAIL DAMAGE OCCURRED TO T/E WEDGE, NR 5 SLAT. REPAIRED T/E WEDGE, SLAT NR 5.SDR 2003UALA00434Wedge · damagedHAIL DAMAGE OCCURRED TO T/E WEDGE, NR 6 SLAT. REPAIRED T/E WEDGE, SLAT NR 6.SDR 2003UALA00388Line · leakingAIRCRAFT RETURNED TO FIELD WHEN A LEAK IN THE PITOT STATIC SYSTEM RESULTED IN UNRELIABLE AIR DATA. FLEX LINE WAS FOUND TO BE LEAKING FROM UPPER RT PITOT TUBE TO FIRST ELBOW .SDR AUS20030428Filter · contaminated(AUS) HYDRAULIC RESERVOIR PRESSURISATION MODULE AIR FILTER CONTAMINATED.SDR 2003UALA00384Skin · gougedA GOUGE WAS FOUND ON THE FWD LOWER CORNER OF THE FUSELAGE SKIN AT APPROXIMATELY BS 300-S17R.SDR 2003UALA00381Skin · dentedFUSELAGE SKIN DENT 15 INCHES BELOW AND 18 INCHES AFT OF FWD LAV SERVICE PANEL. MANUFACTURED AND INSTALLED REPAIR STRAP AND DOUBLER.SDR 2003UALA00383Indicator · inoperativeAIRCRAFT REPORTED ASYMMETRIC FLAP CONDITION AND LANDED UNDER AMBER ALERT WITH FLAP POSITION 1. GROUND TEST DETERMINED THAT FLAP SYSTEM WAS FUNCTIONING PROPERLY. THE FAILURE WAS ISOLATED TO THE INDICATOR IN THE FLAP POSITION INDICATION SYSTEM. THE INDICATOR SDR TX22003F00000Starter · failedNPRM STATES TO REMOVE PART NUMBERS AND SERIES NUMBER AND REPLACE THESE ITEMS WITH A SERIES 7 OR GREATER. THE SERIES 7 UNIT WHEN INSTALLED FAILED. WHEN AN APU START WAS ATTEMPTED USING A SERIES 7 START CONVERTER UNIT. THE NEW UNIT EXPERIENCED A COMPLETE ELECSDR 2003UALA00377Floorbeam · corrodedCABIN STATION 942 FLOORBEAM CAP IS CORRODED. MAJOR REPAIR ACCOMPLISHED. REPLACED FLOORBEAM CAP.SDR 2003UALA00378Floorbeam · damagedCABIN FLOORBEAM STA 947 UPPER CAP HAS FREEZE PLUG DRILLED INTO EDGE AT APPROXIMATE LBL 20. REMOVED, MANUFACTURED AND INSTALLED UPPER "T" CAP.SDR 2003UALA00376Stringer · corrodedFWD NOSE COMPARTMENT STATION 284 STR 23R IS CORRODED ON TOP OUTBOARD SIDE. INSTALLED NEW STRINGER SECTION A CLIPS.SDR 2003UALA00373Threshold · corrodedAFT PIT DOOR THRESHOLD WEB BS 749 TO 847 HAS LEVEL 1 CORROSION. MAJOR REPAIR ACCOMPLISHED. REPLACED THE WEB.SDR 2003UALA00374Frame · crackedRT FUSELAGE FRAME CRACKED AT BS 360 SKIN ATTACH FLANGE BELOW STRINGER 14R. MAJOR REPAIR ACCOMPLISHED. INSTALLED NEW REPAIR FLANGE.SDR UPS03840423Compressor · stalledNR 3 ENGINE COMPRESSOR STALL IFSD AT FL350 WHEN POWER WAS REDUCED FROM 85 TO 77 N & CONTINUED TO STALL IN DESCENT WHEN POWER WAS REDUCED BELOW 72N NR 3 ENG SHUTDOWN IN FLIGHT DUE TO CONTINUED COMPRESSOR STALLS IN LEVEL FLIGHT WITHOUT MOVING THROTTLE. REMOVED SDR 2003UALA00369Warning Light · illuminatedAIRCRAFT ABORTED TAKEOFF DUE TO DOOR 1L INDICATION LIGHT ON. CAUSE UNKNOWN. INSPECTED AND SECURED TARGET AND PLATE. DOOR INDICATION SYSTEM FUNCTIONED NORMALLY.SDR DHL2003801079Cargo Track · wornMAIN CARGO COMPT. NR 6 TRACK LUGS WORN (STA. 280.000 - STA. 321.000) REMOVED NR 6 TRACK DAMAGED SEGMENT IAW SRM 53-2-3 PG.49-50. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT IAW SRM 53-2-3 PG. 49-50.SDR DHL2003801078Cargo Track · wornMAIN CARGO COMPT. NR 2 CARGO TRACK LUGS BETWEEN STA. 1553 AND STA. 1620, WORN, CORRODED. REMOVED NR 2 WORN TRACK SEGMENT IAW SRM 53-2-3 PG. 49-50. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED 3 SPLICES IAW SRM 53-2-3 PG.49-50. INSTALLED NEW SDR DHL2003801080Cargo Track · wornMAIN CARGO COMPT. NR 2 TRACK PLUG LUGS AT STA. 219.000 WORN. REMOVED WORN PLUG AT STA. 219.000 IAW SRM 51-3-0 PG.1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PLUG AND CHANNEL IAW SRM 53-2-3 PG.17-19.SDR CALA0300175Angle · crackedINSPECTION FOUND A 1 INCH CRACK IN SUPPORT ANGLE ON RT WING TRAILING EDGE PANEL JUST OUTBOARD OF NR 5 SPOILER PANEL. THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 57-53-71.SDR CALA0300176Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED THROUGH FASTENERS AND SHIM AT STA 986.5, RBL 48. THE CORRODED SECTION WAS REMOVED AND A REPAIR WAS INSTALLED IAW ECRA 5310-03851.SDR CALA0300177Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 344, LBL 20 TO RBL 4. REPAIRED IAW SRM 53-10-51.SDR CALA0300178Seat Track · corrodedINSPECTION FOUND SEAT TRACK CORRODED AT STA 277-294.5, RBL 40. A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-10-2.SDR CALA0300179Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED ON UPPER FLANGE AT STA 294.5, RBL 35-50. REPAIRED FLOORBEAM IAW SRM 53-10-51.SDR CALA0300180Skin · crackedINSPECTION FOUND A 2 INCH CRACK IN SKIN OF PILOT'S LT WINDOW POST. REPAIRED IAW SRM 53-10-01.SDR 373PA0011Battery Pack · inoperativeEMERGENCY EXIT LIGHTS NOT WORKING ROWS 1,16,26. REMOVED AND REPLACED BATTERY PACKS IAW MM 33-51-51. OPS CHECK GOOD IAW MAINTENANCE ALERT NR 7.SDR CALA0300170Skin · crackedINSPECTION FOUND A 4 INCH CRACK IN FUSELAGE SKIN AT STA 837-867, STRINGER 1. A REPAIR WAS INSTALLED IAW SRM 53-00-01, FIGURE 201.SDR CALA0300171Angle · corrodedINSPECTION FOUND SUPPORT ANGLE FOR FORWARD LAV AFT WALL CORRODED AT STA 307. THE SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-2.SDR CALA0300172Floor Support · crackedINSPECTION FOUND A 1INCH CRACK IN FLOOR SUPPORT AT STA 312-328, LBL 10. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-2.SDR CALA0300173Crease Beam · crackedINSPECTION FOUND A .2500 INCH CRACK IN WEB AT STA 386 INBOARD OF CREASE BEAM. THE CREASE BEAM WEB WAS REMOVED AND REPLACED IAW SRM 51-10-2 AND 51-70-13.SDR CALA0300174Floor Support · corrodedINSPECTION FOUND FLOOR SUPPORT CORRODED ON UPPER SURFACE AT STA 328-344, LBL 11. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-2.SDR 2003UALA00370Fuse · failedDURING PREFLIGHT INSPECTION CREW REPORTED EEL (AISLE) LIGHTS INOP ROW 15 TO REAR OF CABIN. REPLACED FUSES ON AFT BATTREY PACKSDR 2003UALA00371Power Supply · inoperativeFLIGHT CREW REPORTED THAT AFT SECTION OF FLOOR EEL INOPERATIVE. REPLACED AFT EEL POWER STRIP.SDR DHL2003873593Fitting · crackedITEM REF: N/R 1684: FWD CARGO COMPT FLOOR BEAM CUSP EXTRUSION FITTING SHOWS 1 CRACK IN IT (STA.340.000 RBL-49) (MAJOR REPAIR). CORR: PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG 1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG 21, SRM 51-3-0 PG 1. CLEANED, TREATED SDR 377PA0013Light · inoperativeEMERGENCY FLOOR LIGHTING INOPERATIVE, ROW 20 AFT. REPLACED ROW 17-29 LIGHT STRIP IAW MM 25-60-01. OPS CHECK OK.
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