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 DHL2003873581Splice · crackedITEM REF.: N/R 1212.: FWD. CARGO COMPT. SPLICE FITTING 9.000 CRACKED (STA.600.000 - 620.000, L-31L) (MAJOR REPAIR) PERFORMED MAJOR REPAIR IAW SRM 53-1-0 PG.1. REMOVED CRACKED FITTING IAW SRM 51-1-20D PG.21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSDR 2003UALA00543O-Ring · leakingUPON ARRIVAL FOUND BOTTLE PRESSURE ON SLIDE AT DOOR 1R BELOW THE GREEN BAND. LEAKING O-RING BETWEEN RESERVOIR AND VALVE/REGULATOR CAUSED REDUCED BOTTLE PRESSURE. REPLACED SLIDE BOTTLE, INSPECTED/TESTED REMOVED BOTTLE TO DETERMINE CAUSE, THEN OVERHAULED VALVSDR DHL2003873564Seat Track · wornITEM REF.: N/R 0827.: MAIN CARGO COMPT. NR 6 TRACK LUG WORN STA.1470.000-STA.1590.000. REMOVED DAMAGED TRACK IAW SRM 51-3-0 PG.1. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW TRACK IAW SRM 51-3-0 PG.1.SDR 2003UALA00527Controller · failedAIRCRAFT RETURNED TO THE FIELD WHEN IT WAS UNABLE TO PRESSURIZE AFTER TAKEOFF. THE CABIN PRESSURE CONTROLLER FAILED. REPLACED PRESSURE CONTROLLER, TESTED NORMAL.SDR 2003UALA00525Warning Light · false indicationAIRCRAFT DIVERTED EN ROUTE DUE TO A WING-BODY OVERHEAT INDICATION. AIRCRAFT EXPERIENCED LEFT WING-BODY OVERHEAT WARNING INDICATION IN CRUISE FLIGHT WITH APU SUPPLYING AIR. WING-BODY OVERHEAT INDICATION LIGHT EXTINGUISHED PER THE IRREGULAR PROCEDURE. AIRCRAFSDR DHL2003873541Intercostal · crackedFWD CARGO COMPT PRESSURE BULKHEAD INTERCOSTAL CRACKED (1.000), STA 640.000 LBL 11. REMOVED FASTENTERS IAW SRM 51-1-21 PG 1. STOP DRILLED CRACK AND FABRICATED DOUBLER IAW SRM 53-2-0 FIG 1B. CLEANED, TREATED AND PRIMED IAW SRM 51-1-8B. INSTALLED DOUBLER WITH NEWSDR 2003UALA00522Vane · unserviceableAIRCRAFT RETURNED TO FIELD AFTER ENGINE HAD A COMPRESSOR STALL JUST AFTER TAKEOFF. DISASSEMBLY OF THE ENGINE SHOWED TEARS AND MISSING MATERIAL ON COMPRESSOR BLADES AND VANES STAGES 6 THROUGH 9 DUE TO A STAGE 8 VANE SECTOR HONEYCOMB FAILURE. FAILURE OF THE HOSDR 2003UALA00523Module · looseAIRCRAFT ABORTED TAKEOFF WHEN FORWARD PANEL L/E FLAP INTRANSIT LIGHT AND OVERHEAD PANEL L/E FLAP INTRANSIT LIGHT ILLUMINATED. TROUBLESHOOTING REVEALED THAT PIN NR 14 ON CONNECTOR D728B OF THE M229 FLAP/SLAT POSITION INDICATION MODULE WAS PUSHED BACK AND NOT LSDR 2003UALA00524Charger · inoperativeAFT SECTION EMERGENCY EXITING LIGHTS (EEL) INOPERATIVE. REPLACED AFT BATTERY CHARGER, BATTERY PACK AND AFT EEL STRIP 24 FT CABLE. OPS OK.SDR CALA0300337Gate · crackedINSPECTION FOUND A 0.33 INCH CRACK IN LOWER GATE OF L-2 DOOR. THE CRACK WAS LOCATED AT AFT CORNER FROM AFT MOST RIVET TOWARDS HINGE. INSTALLED HINGE AND SEALED RETAINERS ON NEW GATE IAW SRM 51-40-02.SDR IXXA0300045OMechanism · brokenAFTER TAKEOFF AND GEAR RETRACTION, CREW EXPERIENCED A VIBRATION AND NOISE COMING FROM NOSE GEAR AREA. THE CREW ELECTED TO RETURN BASE. MAINTENANCE FOUND GROUND SHIFT ARM BROKEN. AS MORE INFORMATION BECOMES AVAILABLE IT WILL BE PROVIDED. MAINTENANCE REMOVED ANDSDR 2003UALA00520Wire · pulledUPON GEAR RETRACTION, NOSE GEAR UNSAFE LIGHT (RED) CAME ON. FOUND WIRE 328-201-24R PULLED OUT OF SPLICE SP374. REPLACED SPLICE SP374, SP376 AND LATCHING RELAY R374.SDR DHL2003873544Cargo Track · wornMAIN CARGO COMPT NR 2 TRACK LUG WORN,( STA.1570.000-STA.1590.000) REMOVED NR 2 TRACK DAMAGED SECTION IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT WITH NEW FASTENERS IAW SRM 51-3-0 PG 1.SDR DHL2003873536Cargo Track · wornMAING CARGO COMPT NR 2 TRACK LUG WORN, STA 1590.000 - 1680.000. REMOVED NR 2 TRACK DAMAGED SEGMENT IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW TRACK SEGMENT WITH NEW FASTENERS IAW SRM 51-3-0 PG 1.SDR CALA0300328Skin · crackedINSPECTION FOUND A 2.5 INCH CRACK IN FUSELAGE SKIN OUTBOARD OF EE ACCESS DOOR AT STA 338 BETWEEN STRINGER 24R AND 25R. THE CRACK WAS STOP DRILLED AND A REPAIR WAS INSTALLED IAW ECRA 5330-03260.SDR UPS03840928Skin · crackedINSPECTION TYPE: C, C-PIT DOOR LOWER AFT CORNER, REMOVED EXISTING REPAIR TO ACCOMPLISH AND SATISFY REPAIR REQUIREMENTS OF SRM, FOR DOOR CORNER REPAIRS AT STATION 1220 LONG 33R. NDT VERIFIED NO CRACKS AT EXISTING CUTOUTS, FABRICATED AND INSTALLED DOUBLER, TRISDR UPS03840885Skin · crackedINSPECTION TYPE:C3 LEFT WING CENTER LE. LOWER SKIN IS CRACKED AT FASTENER HOLES AT XOLDI 6.225 STOP DRILLED CRACKS, NDT VERIFIED STOPDRILLS TERMINATES CRACKS, FABRICATED AND INSTALLED DOUBLER IAW DC8-5720-4087-B APPX. CSDR DHL2003873527Doubler · corrodedFWD CARGO COMPT FRAME DOUBLER CORRODED STA 160.000 L26R. REMOVED FASTENERS AND DOUBLER IAW SRM 51-1-20D PG 21. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 53-2-0 PG 2P. FABRICATED DOUBLER IAW SRM 53-2-0 FIG 1F. HEAT TREATED IAW SRM 5SDR DHL2003873530Skin · damagedLT WING INBD FLAP LOWER FWD PLATING HAS INERIM REPAIR AT STA XW.86.50 TO XW.115.250. PERFORMED MAJOR REPAIR IAW EODHL-030602, ED-3428. REMOVED FASTENERS IAW SRM 51-1-21 PG.1. TRIMMED OUT THE DAMAGED SKIN SEGMENT IAW EODHL-030602, ED-3428. FABRICATED A NEW SKINSDR 2003UALA00517Charger · failedFLIGHT CREW REPORTED THAT THE EMERGENCY ASILE LIGHTS ABOVE ROW 19 AND 20, AND THE DOOR 2R FLOOR LEVEL LIGHT ARE INOPERATIVE. *SUPPLEMENTAL DATA UPDATE* REPLACED M1137 BATTERY CHARGER ASSY.SDR DHL2003873519Seat Track · wornITEM REF.: N/R 0843.: MAIN CARGO COMPT NR 5 TRACK LUG WORN BETWEEN STA.1680.000 AND STA.1695.000. CUT OUT NR 5 TRACK DAMAGED SEGMENT IAW SRM 53-2-3 PG.49-50. FABRICATED SPLICES (7075-T6 0.160) IAW SRM 53-2-3 PG.49-50. CLEANED, TREATED AND PRIMED IAW SRM 51-1-SDR 2003UALA00514Lamp · inoperativeAFT FLOOR EMERGENCY EXIT LIGHTING (EEL) INOPERATIVE AT THE GATE. REPLACED EEL LAMP STRIP. GROUND TEST EMERENCY LIGHT SYSTEM, CHECKS NORMAL.SDR AWXA200300745Bulkhead · crackedDURING C-13 CHECK 3 EACH 1 INCH CRACKS WERE FOUND ON BS 178 BULKHEAD WEB AT RBL 5, WL 197.75 - 198.75, WL 201 - 201.75, AND RBL 6.25, WL 200.75 - 201.5. MAINTENANCE STOP DRILLED CRACKS ON BS 178 BULKHEAD WEB AT RBL 5, WL 197.75 - 198.75, WL 201 - 201.75, AND RSDR UPS03840925Shear Tie · brokenINSPECTION TYPE: C, EXTERIOR FUSELAGE FRAME TO SKIN SHEAR TIE IS BROKEN,STATION 702 BETWEEN LONG. 33L TO 35L. REMOVED DAMAGED SHEAR TIE SECTION, FABRICATED AND REPLACED SHEARTIE SECTION IAW DWG. 5750365 AND SRM. 53-2-0 FIG. 2SDR UPS03840929Seat Track · corrodedINSPECTION TYPE: C, AFT ACCESSORY COMPT. STA. 1600-1620 AT RBL 45 SEAT TRACK REPAIR IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED SEAT TRACK SECTION STATION 1590-1610 AT RBL 45, AND REPLACED SEAT TRACK SPLICE STATION 1600-1620 IAW SRM 53-2-3 SDR DHL2003873619Cargo Track · wornMAIN CARGO COMPT NR 5 TRACK PLUG LUG WORN AT STA 1315.000. REMOVED DAMAGED PLUG AND CHANNEL IAW SRM 51-3-0 PG 1. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW PLUG CHANNEL TO TRACK NR 5 AT STA 1315.000 IAW SRM 51-3-0 PG 1.SDR UPS03840892Skin · damagedINSPECTION TYPE: C3, RIGHT WING LEADING EDGE INBOARD END OF OUTBBOARD. SLOT HAS SCREWS PULLING THRU SKIN AT XFS XOLDI 6.225. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM. 57-2-0 FIG. 2ASDR UPS03840894Angle · crackedINSPECTION TYPE: C3, RIGHT WING LEADING EDGE ABOVE NR 3 PYLON, RIB TO WEB ATTACH ANGLE IS CRACKED AT LOWER END AT XS 256.339 APPROX. REMOVED ATTACH ANGLE, FABRICATED AND REPLACED ANGLE IAW DWG. 9753294, AND SRM. 51-1-20DSDR 2003UALA00511Wire · damagedEMERGENCY ELECTRICAL LIGHTING (EEL) INOPERATIVE BETWEEN ROWS 14 AND 19. REPLACED FEEDER CABLE.SDR 2003UALA00510Gasket · leakingAIRCRAFT ABORTED TAKEOFF WHEN THE NR 1 CSD LOW OIL PRESSURE LIGHT ILLUMINATED. FOUND CSD LEAKING FROM SIGHT GLASS. REINSTALLED GASKET. SERVICED THE CSD, RAN ENGINE WITH NO LEAKS NOTED.SDR UPS03840856Rib · crackedINSPECTION TYPE: C3, LT WING LE LOWER RIB IS CRACKED AT XFS 385, STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK,FABRICATED AND INSTALLED REPAIR DOUBLERS I.A.W. SRM. 57-2-0 FIG.2SDR 2003UALA00504Skin · crackedSHEET METAL AT EXT POWER DOOR LOWER LATCH STOP CRACKED BETWEEN RIVET HOLES. MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED INTERNAL DOUBLER.SDR UPS03840884Rib · crackedINSPECTION TYPE:C3 LEFT WING LE UPPER RIB IS CRACKED AT XFS 741.25. STOPDRILLED CRACK,NDT VERIFIED STOPDRILL TERMINATES CRACK,FABRICATED AND INSTALLED REPAIR DOUBLER I.A.W. SRM. 57-2-0 FIG. 2SDR 2003UALA00506Switch · intermittentAIRCRAFT LANDED UNDER AMBER ALERT DUE TO LEADING EDGE FLAP DISAGREE INDICATION. TROUBLESHOOTING IDENTIFIED A FAILED NR 4 FLAT EXTEND SWITCH. THE SWITCH WAS REPLACED AND THE SYSTEM WAS TESTED TO ENSURE PROPER OPERATION.SDR UPS03840927Skin · damagedINSPECTION TYPE: C, 8 PREVIOUS BLENDOUTS BELOW C-PIT DOOR BETWEEN LONG. 34R TO 30R FROM STA. 1220 TO 1260 CUT AND REMOVED SKIN SECTION FROM STATION 1190-1230 BETWEEN LONG 29R TO 34R,NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED SKIN SECTION ANSDR 2003UALA00493Skin · dentedEXTERNAL FUSELAGE SKIN AT B.S. 928 BETWEEN STR. 17L AND 18L IS DENTED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR AWXA200300735Floorbeam · corrodedDURING C-14 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF FLOORBEAM AT BS 994, LBL 13-44, WL 208. MAINTENANCE REMOVED FLOORBEAM BS 994, LBL 13-44, WL 208; FABRICATED A NEW REPLACEMENT FLOORBEAM IAW DWG 65-46812; INSTALLED REPAIR PART IAW B737-300 SRMSDR AUS20030564Skin · cracked(AUS) FORWARD GALLEY DOOR CUTOUT SKIN FORWARD AND AFT UPPER CORNERS CRACKED. THE AFT UPPER CORNER OF THE CUTOUT WAS CRACKED FROM ONEHOLE IN THE BEARSTRAP ONLY. TWO HOLES AT THE FORWARD UPPER CORNER OF THE CUTOUT WERE CRACKED IN THE STUBFRAME ONLY AND ATHIRD HOSDR SWAA031303Engine · failedIN-FLIGHT SHUTDOWN, DECLARED EMERGENCY, AIR TURNBACK, NR 1 ENGINE FAILURE, AUTO SHUTDOWN IN-FLIGHT. REMOVED AND REPLACED NR 1 ENGINE PER MM.SDR AWXA200300709Floorbeam · corrodedDURING C-14 CHECK EXFOLIATION CORROSION WAS FOUND ON LOWER SURFACE OF FLOORBEAM AT BS 996, LBL 38, WL 208. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED CORRODED FLOORBEAM BS 996, LBL 38, WL 208; FABRICATED A NEW REPLACEMENSDR AWXA200300734Floorbeam · corrodedDURING C-14 CHECK CORROSION WAS FOUND ON LOWER SURFACE OF FLOORBEAM AT BS 992, RBL 23-47, WL 208. MAINTENANCE FOUND PRE-WORK MEASUREMENT OF MATERIAL LOSS TO BE OUT OF LIMITS; REMOVED FLOORBEAM BS 992, RBL 23-47, WL 208; FABRICATED A NEW REPLACEMENT FLOORBEAM ISDR UPS03840926Skin · damagedINSPECTION TYPE: C, COMPLY WITH MPI P 14035: IAW M REPAIR TO AIRSTART DOOR CUTOUT AT 100Y CYCLES OR 3 MONTHS WHICHEVER COMES FIRST IAW EO DC8-5330-0793, STATION 25 TO 55 LONG. 28L-30L AT DOOR CUTOUT REMOVED EXISTING FILLERS,NDT VERIFIED NO CRACKS AT EXISDR AWXA200300749Web · crackedDURING C-14 CHECK 2 EACH CRACKS WERE FOUND LT WHEEL WELL PRESSURE WEB AT OUTBOARD SIDE OF FORMED CHANNEL BS 664, LBL 32. MAINTENANCE CUTOUT DAMAGE ON LT W/W PRESSURE WEB BS 664, LBL 32; PERFORMED HFEC INSPECTION OF CUTOUT TO VERIFY NO CRACKS EXIST; FABRICATED SDR AUS20030569Fmc · faulty(AUS) BOTH FLIGHT MANAGEMENT COMPUTERS (FMC) FAILED. INVESTIGATION ANDTESTING COULD FIND NO FAULT.SDR 2003UALA00455Socket · damagedNR 1 RIGHT HAND DOOR EXTERNAL FUSELAGE EMERGENCY SLIDE LIGHT INOPERATIVE. REPLACED SLIDE LIGHT SOCKET ASSY.SDR 2003UALA00456Skin · dentedLT FUSELAGE EXTERNAL SKIN DENTED AT STA 445 BETWEEN STRINGERS 18L & 19L. MAJOR REPAIR ACCOMPLISHED. DOUBLER REPAIR.SDR SWAA031183Pin · looseDURING SCHEDULED A1 CHECK, SWA SI 11165-72, NR 2 ENGINE RETAINING RING PINS AND MID FLANGE FAN DISK PINS FAILED TORQUE PIN CHECK. REMOVED AND REPLACED NR 2 ENGINE PER MM.SDR 2003UALA00449Fitting · leakingB-HYDRAULIC SYSTEM QUANTITY AND PUMP LOW PRESSURE LIGHTS ILLUMINATED. INSPECTION FOUND THAT THE RETURN LINE CHECK VALVE FITTING ON THE HYDRAULIC FLAP DRIVE MOTOR SHEARED OFF AT THE BOSS. THE FITTING WAS REPLACED. THE HYDRAULIC SYSTEM WAS SERVICED AND THE FSDR 2003UALA00444Light · inoperativeEEL LIGHTING IN FIRST CLASS CABIN INOPERATIVESDR 2003UALA00443Indicator · malfunctionedAIRCRAFT ABORTED TAKEOFF, AIRCRAFT SWERVED DURING THE TAKEOFF ROLL. CAUSE IS STILL TO BE DETERMINED. CREW ABORTED TAKEOFF DUE TO NR 1 ENGINE GAUGE INDICATING FUEL FLOW ROLLBACK TO ZERO. NO FLAMEOUT REPORTED AND ALL OTHER ENGINE INDICATIONS WERE NORMAL. THE
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