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 2005UALA00850Light · inoperativeLEFT AND RIGHT EMERGENCY EXIT LIGHTS INOP (EXTERIOR). REPLACED LIGHT ASSEMBLY.SDR 2005UALA00851Warning Light · illuminatedFLT SHOWED LE FLAPS IN TRANSIT LIGHT. AMBER ALERT CALLED IN. A FAILED LEADING EDGE (LE) FLAP AND SLAT CONTROL VALVE INHIBITED FULL EXTENTION OF THE LE FLAPS AND SLATS. SUBJECT FAILURE CONSIDERED AN ISOLATED INCIDENTCORRECTIVE ACTION: REPLACED AND TESTED SUBSDR 2005UALA00838Skin · crackedDENT FWD AND BELOW DOOR 2L.SDR ASAA0540394Frame · crackedCRACKED FRAME AT BIN RAIL STA 440. REPAIRED CRACKED FRAME AT BIN RAIL BSTA 440, STR 8L-9L IAW SRM. (K)SDR ASAA0540395Frame · crackedCRACKED FRAME AT BIN RAIL STA 400. REPAIRED CRACKED FRAME AT BIN RAIL BSTA 400, STR 8L- 9L IAW SRM. (K)SDR 2005UALA00834Structure · bird strikeBIRD STRIKE AROUND THE RADOME, VERY LOUD, ALSO, ODOR IN COCKPIT. ON CLIMB, THE AIRCRAFT ENCOUNTERD A BIRDSTRIKE. THE AIRCRAFT RETURNED TO FIELD AND MAINTENANCE PERFORMED A BID STRIKE INSPECTION PER AMM. THERE WAS EVIDENCE OF BIRD INGESTION IN THE NR 1 ENG HSDR DHL2005806503Doubler · damagedINTERIM REPAIR ON RT OB FLAP UPPER PLATING (STA XF 208.000-213.000) (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG. 1, SRM 57-7-1 FIG. 4, TR NR 57-94. REMOVED PLATING WITH INTERIM REPAIR ON IT IAW SRM 51-1-21 PG. 1, SRM 51-3-0 PG. 1. FABRICATED NEW PSDR 2005UALA00814Stringer Clip · bentAFT PIT STA 727D STR 20L STRINGER CLIP BENT AND CRACKED. REMOVED AND REPLACED STRINGER CLIP.SDR 2005UALA00815Stringer Clip · crackedAFT PIT STA 907 STR 24R STRINGER CLIP BENT AND CRACKED. REMOVED AND REPLACED STRINGER CLIP.SDR 2005UALA00817Switch · failedAIRCRAFT PRESSURIZATION PROBLEM. AFTER T/O, CREW REPORTED LOSS OF LNAV, VNAV, AUTOTHROTTLE, TCAS AND ENGINE LOW IDLE LIGHT WAS ON. THROUGH 25,000 FT, ALTITUDE WARNING HORN SOUNDED AND THE CABIN ALTITUDE MAXED OUT AT 11,000 FT. AFTER T/O, CREW REPORTED LOST LSDR AU510002039Connector · damagedHYDRAULIC PUMP CONNECTOR AND MATING RECEPTACLE CONTAMINATED WITH HYDRAULIC FLUID AND BADLY BURNT. ONE OF THE CONNECTOR SOCKETS WAS WELDED ONTO THE PUMP CONNECTOR PINS.SDR SWAA052373Engine · failedINFLIGHT SHUTDOWN/DECLARED EMERGENCY/DIVERSION, LOST NR 2 ENGINE OIL PRESSURE AND QUANTITY. REMOVED AND REPLACED NR 2 ENGINE PER MM.SDR AU510001835Latch · brokenENGINE CORE COWL NR 6 LATCH BROKEN. FURTHER INVESTIGATION FOUND NR 1, NR 3, NR 4 AND NR 5 LATCHES CRACKED.SDR SB05090Circuit Card · faultyAFTER TAKEOFF, ENROUTE, CAPTAIN REPORTED THE RT MLG RED UNSAFE LIGHT ILLUMINATED. CREW RECYCLED THE GEAR AND LIGHT EXTINGUISHED. CAPTAIN ELECTED TO RETURN TO FIELD WHERE THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. NORMAL GEAR INDICATION OF 3 GREEN LIGHTS WERESDR 2005UALA00789Battery · failedRETURNED TO THE FIELD DUE TO A BATTERY SYSTEM FAILURE. SHOP FINDINGS REVEALED BAD CELLS IN THE BATTERY. THE BATTERY HAS BEEN SCRAPPED.SDR AU510001689Seal · failedAPU BLEED VALVE AND DUCTS CONTAMINATED WITH OIL. INVESTIGATION FOUND THE APU LOAD COMPRESSOR SEAL FAILED.SDR 2005UALA00779Battery Pack · inoperativeEMERGENCY EXIT LIGHTS INOPERATIVE FROM ROW 13 TO AFT CABIN. REPLACED BATTERY AND AFT GALLEY STRIP.SDR 2005UALA00756Light · inoperativeEEL LIGHTS INOPERATIVE ON FLOOR AT AFT CABIN. CLEANED AND DRIED RACEWAY, PWR CABLE AND LIGHTS.SDR 2005UALA00748Frame · gougedAFT CARGO DOOR LOWER AFT FRAME HAS .035 GOUGE WITH 15" LONG CRACK. REMOVED LOWER AFT FRAME. REMOVED INNER SUPPORT ANGLE. REINSTALLED ANGLE AND NEW FRAME. REF SRM 51-40-02. FRAME PN 65-47952-136.SDR 2005UALA00749Light · inoperativeEEL FLOOR LIGHTING ROWS 15-21 INOPERATIVE. REPLACED CABLE AND SECURED TRACKS. REPLACED CABLE AND SECURED TRACKS.SDR 2005UALA00754Skin · crackedAFT CARGO DOOR HAS A VERTICAL CRACK APPROX 2 INCHES LONG, 6 T0 8 INCHES DOWN FROM DOOR HANDLE. REMOVED EXISTING DOUBLERS AND INSTALLED NEW DOUBLER APPROX 48" BY 48" PER SRM 52-30-01 AND SRM 52-00-01.SDR 2005UALA00755Attach Fitting · corrodedVERTICAL STABILIZER LT AND RT AFT PRIMARY ATTACH LUG FITTINGS ON FUSELAGE HAD CORROSION REMOVAL BEYOND LIMITS. REPLACED LT AND RT AFT PRIMARY ATTACH LUGS AND INSTALLED NEW BUSHINGS PER BACO DRAWING 65-52274.SDR 2005UALA00745Skin · dentedSTA 837 IS DENTED BETWEEN STR 25L AND 26L. CUT OUT DAMAGE AND INSTALLED DOUBLER AND TRIPLER REPAIR PER SRM 53-00-01 FIG 229.SDR 2005UALA00734Stringer Clip · crackedCABIN UPPER LOBE STRINGER CLIP IS CRACKED AT STA 685, STR 4 LT. REMOVED AND REPLACED STRINGER CLIP.SDR 2005UALA00735Stringer Clip · crackedCABIN UPPER LOBE STRINGER CLIP IS CRACKED AT STA 639 STR 4 LT. REPLACED STRINGER CLIP.SDR 2005UALA00736Web · corrodedCABIN FLOOR WEB CORRODED AT STATION 749 JUST INBD OF STR 17R CREASE BEAM. REMOVED AND REPLACED WEB.SDR 2005UALA00744Web · corrodedAFT CARGO DOOR SILL WEB HAS NUMEROUS AREAS OF CORROSION WL 141 STATION 800 TO 847 RBL 20" TO RBL 24". REMOVED AND INSTALLED NEW WEB REPAIR.SDR 2005UALA00719Skin · crackedAPPROXIMATE 1.5 INCH CRACK IN FUSELAGE AT LOWER AFT RADIUS OF DOOR 1R. REPAIRED DOOR 1R LOWER AFT CORNER REF SRM 53-10-01 PAGE 207.SDR 2005UALA00769Light · unknownMACH TRIM FAIL LIGHT ON RECALL, VERY CHRONIC. AFTER TROUBLESHOOTING & PARTS REPLACEMENT, REVIEW OF BITE DATA REVEALED INTERMITTENT MOMENTARY LOSS OF POWER TO MACH TRIM SYS. CIRCUIT BREAKER C1064, B-MACH TRIM DC, REPLACED & TEST FLT PERFORMED. INTERMITTENT NASDR 2005UALA00712Skin · dentedSTATION 807 IS DENTED AT STR 28R. CUT OUT DAMAGE AND INSTALLED A TRIPLER REPAIR REF SRM 53-00-01 FIG 229.SDR 2005UALA00707Odor · detectedFLIGHT DIVERTED DUE TO ODOR IN CABIN. TOOK OFF AND RETURNED A SECOND TIME WITH SAME ODOR.SDR 2005UALA00708Skin · dentedAFT CARGO DOOR EXT SKIN HAS 8 EA DENTS. REPAIR ACP'D PER SRM 52-00-01, 41" BY 23" DOUBLER INSTALLED.SDR 2005UALA00709Frame · crackedFUSELAGE FRAME STA 663 IS CRACKED AT STR 1 CUTOUT. MAJOR REPAIR ACP'D PER SRM 53-00-07 AND BACO DRAW 65-73740.SDR 2005UALA00710Wire · inoperativeALL EEL LIGHTS AFT OF ROW 12 INOPERATIVE. REPAIRED POWER CABLE AND FEEDER CABLE.SDR 2005UALA00694Skin · dentedSTATION 203 HAS A SCRATCH BETWEEN STR 24 AND 25 LT. CUT-OUT DAMAGED AREAS AND INSTALLED TRIPLER REPAIR REF SRM 53-10-01 FIG 211 DETAIL XII AND XIII.SDR 2005UALA00703Guide Arm · damagedDOOR 2L EXTERIOR DOOR HANDLE RAISES IN SLIPSTREAM AND PARTIALLY ROTATES NO SPRING IN DOOR HANDLE, HANDLE HAS NO RESISTANCE WHEN PULLING OUT OR PUTTING BACK. SECURED EXTERNAL HANDLE, REPLACED GUIDE ARM, ADJUSTED STOP PIN.SDR 2005UALA00704Wire · damagedEMERGENCY EXIT PATH LIGHTS STRIP INOP FROM ROW NR 15 AFT. REPLACED CABLE.SDR 2005UALA00691Angle · corrodedAFT CABIN FLOOR ANGLE CAP IS CORRODED AT STA 996 RPL 53, WL208. REPLACED ZEE ANGLE ASSY AT HMV3.SDR 2005UALA00692Frame · crackedFWD GALLEY DOOR, AFT SIDE LOWER END FRAME CRACKED 1 EA FASTENER HOLE. MAJOR REPAIR ACP'D, AFT FRAME REPLACED PER SRM 51-40-02 AND BACO DRAW 65-45871.SDR 2005UALA00693Frame · crackedFWD GALLEY DOOR, FWD SIDE LOWER END FRAME CRACKED 1 EA FASTENER HOLE. MAJOR REPAIR ACP'D, REPLACED FRAME REF SRM 51-40-02 AND BACO DRAW 69-69430.SDR 2005UALA00696Lamp · burned outAISLE ILLUMINATION EMERGENCY LIGHT INOP AT ROW 10 BULLNOSE. REPLACED BURNED OUT LAMP.SDR AU510002222Heat Exchanger · crackedRT AIR CONDITIONING PACK HEAT EXCHANGER CRACKED AND LEAKING.SDR AU510001573Switch · faultyCENTER FUEL TANK RT BOOST PUMP RUNNING WHEN SWITCH `OFF`. SUSPECT FUEL PANEL CONTROL SWITCH.SDR IXXA05SMN155SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, MID ACCESSORY COMPARTMENT L-31R CORRODED, STA 665.000. PERFORMED MAJOR REPAIR IAW SRM 53-2-2 FIG. 11, EO SEMAN NR 20051003 DATE 06-27-05. REMOVED FASTENERS IAW SRM 51-1-20D PAGE 21. REMOVED CORROSION IAW SRM 51-1-8 PAGES 17-SDR IXXA05SMN156SSkin · corrodedDURING ROUTINE C CHECK INSPECTION, RT WING IB L/E UPPER PART EXTERNAL SKIN CORRODED XS 250.089. PERFORMED MAJOR REPAIR IAW SRM, TR NR 57-85, EO SEMAN NR 2005984 DATE 06-18-05. REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1, SRM. REMOVED CORROSION IAW SRM. FOUND SDR IXXA05SMN157SSkin · crackedDURING ROUTINE C CHECK INSPECTION, LT WING. STUB WING UPPER SURFACE STA XS 250.000 XS 240.000 HAS TWO CRACKS OF .5 INCH. PERFORMED MAJOR REPAIR IAW SRM 57-2-1 FIG. 38, TR NR 57-85, EO SEMAN NR 2005983 DATE 06-18-05. REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1.SDR DU4R0507001Skin · dentedLT WING IB FWD FLAP LWR SIDE HAS 8 DENTS AT STA. WBL 85 TO 95 AT VARIOUS LOCATIONS.SDR 138Skin · gougedRT WING OB FORE FLAP GOUGED ON OB END. S/O 269008, OPS NR 24931.SDR DU4R0507002Skin · chafedLT WING NR 3 SLAT HAS SKIN CHAFED THRU AT T/E LOWER IB SKIN SURFACE. S/O 269008, OPS NR 24936SDR CALA0500212Engine · malfunctionedLOUD THUMP HEARD AFTER T/O. ALL ENG IND`S NORMAL THROUGH CLIMB-OUT TO 10,000 FT. PASSING 10,000 FT SEVERAL SUCCESSIVE THUMPS WITH NO ABNORMAL ENG IND`S. A/C RETURNED WITH NORMAL LANDING. ENG SHUTDOWN AFTER LANDING. L-1 AND L-2 DOOR SLIDES DEPLOYED & PAX`S EV
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