CFM International CFM56-3C series
Service difficulty reports · 415
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 = 'CFM563C' 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 = 'CFM563C' 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 I5EA2023010600001Engine · stalledNR 1 ENGINE COMPRESSOR STALLED AND LOST POWER, ACFT UNABLE TO HOLD ALT LT ENG OUT ALT FL 220 PULL TO IDLE ACFT VIBRATION AND STALL STOPPED. PROBLEM CONTINUED AT FL280 FLOWING QRH. NR 1 ENGINE POWER RESTORED DIVERTED TO TPA. REMOVED AND REPLACED LT ENGINE ISDR AALA201702209009Engine · malfunctionedDURING ABORTED TAKEOFF, FULL TAKEOFF THRUST WAS NEVER APPLIED DUE TO NR 1 ENGINE LAGGING. SPEED AT TAKEOFF REJECTION LESS THAN 10 KNOTS. AIRCRAFT WAS GROUNDED. PERFORMED TSM 71-00-00-810-807-A. CHECK PERFORMED & FOUND WITHIN LIMITS IAW AMM 71-00-00-710-02 SDR KNNA2015031000042Fuel Line · leakingNR 2 ENGINE FUEL LINE FOUND TO BE LEAKING. APPEARED TO BE AT THE JUNCTION BETWEEN THE BRAIDED PORTION AND THE HARD LINE. THE DAMAGED LINE WAS RETURNED TO THE ENGINE LESSOR FOR INSPECTION. THE METAL BRAIDS WERE FOUND TO BE INTACT BUT THE INTERIOR WAS FRACTUREDSDR KNNA2013F00154Lamp · burned outEMERGENCY LIGHT AT L2 DOOR INOPERATIVE. REPLACED LAMPSDR KNNA2013081401Door Frame · corrodedCORROSION FOUND AROUND L-1 DOOR UPPER FORWARD CORNER FRAME.SDR KNNA20130422870Power Supply · failedEMERGENCY LIGHTS AT RT ABOVE OVERWING EXITS INOPERATIVE, LT FWD HATCH INOP, ROW 10 OVERHEAD BIN INOP. FOUND BATTERY NOT SECURED TO BATTERY POWER SUPPLYAT ROW 12 RT ABOVE OVERHEAD BIN, RESECURED BATTERY TO POWER PACK. R & R BATTERY POWER SUPPLY AT ROW 13, OPSDR KNNA201304220001Bulb · burned outEMERGENCY EXIT LIGHTS, LAST RED LIGHT AT AFT GALLEY INOPERATIVE. EMERGENCY EXIT LIGHTS ROW 8-11 INOPERATIVE.SDR 2013F00073Skin · crackedLT LOWER FUSELAGE SKIN BETWEEN FS 727C-727F WITH THREE NEW CRACKS ON SKIN.SDR XV6A2013022700005Skin · crackedDURING AN INSPECTION, FOUR CRACKS WERE FOUND IN FUSELAGE SKIN BS 727E & 727F AND BETWEEN STRINGERS 25-26L. INSTALLED REPAIR IAW SRM 53-00-00, REPAIR 31 DETAIL XXXIV.SDR BJNA20121201Actuator · inoperativeNR 2 THRUST REVERSER SLOW TO DEPLOY. NR 2 ENGINE OTBD THRUST REVERSER HALF MID ACTUATOR WAS IMPROPERLY SET FROM THE REPAIR FACILITY IN LENGTH CAUSING SLOW UNLOCK/DELOY AND SLOW STOW/LOCK OPERATION AND WORN UPPER THRUST REVERSER LOCKING ACTUATOR. REPLACED THRSDR I5EA20111001Bulb · burned outL1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R L1 DOOR EXTERIOR EMERGENCY LIGHT BULB IAW AMM 33-51-02/21.SDR 2011FA0000476Seal · missingENGINE DAMAGE WAS IDENTIFIED ON THE LLPT STAGE, 4 BLADES AND VANES, DURING AN ACFT DAILY INSP. 42 CYCLES WERE COMPLETED POST LAST SHOP VISIT. PRE-INPUT, ENGINE BOROSCOPE WAS CARRIED OUT AT REPAIR STATION AND IT WAS NOTED THAT THE STAGE 4 INNER STAGE HONEYCOMSDR 2011FA0000448Engine · misoverhauledDURING SHOP VISIT, INCORRECT CONFIGURATION BETWEEN THE OUTER NOZZLE SUPPORT PN 9999M78P10 - PRE SB 72-537, (51 MODULE) AND RETURNED TO SERVICE. ENGINE RECEIVED FROM NEW MAKE IN INCORRECT CONFIGURATION. NOT IDENTIFIED AT REPAIR STATION DURING SERVICE. ENGINE SDR MYWA100124Indicator · faultyETOPS SIGNIFICANT SYS: ON APPROACH CREW HAD A FLAP ASSEMETRY BETWEEN 2 AND 5. ACCOMPLISHED NON-NORMAL CHECKLIST. AFTER LANDING, REPLACED FLAP POSITION INDICATOR. SYS OPS NORMAL.SDR MYWA100015Mec · malfunctionedETOPS SIGNIFICANT SYSTEM - LEFT ENGINE PMC CAUSING ENGINE SURGE DURING FLIGHT. ENGINES STABILIZES WHEN PMC IS DISENGAGED. REPLACED MEC.SDR UPS08854080Engine · flamed outINSPECTION TYPE:N/A NR 3 ENGINE FLAMED OUT. ENGINE RELIT ON IT'S OWN. PERFORMED FIRST FOUR STEPS OF DC-8 M/M 71-00-00-1 FIG 139 UP TO INSPECT FUEL FILTER. FILTER KIT ON ORDER. REPLACED NR 3 FUEL FILTER PER AMM 73-10-02-4. LEAK CHECK OK. ACCOMPLISHED STEPSDR 2008UALA05427Lamp · inoperativeEMERGENCY LIGHT LAMP INOP ROW 12. REPLACED LAMP.SDR 2008UALA04358Frame · damagedDAMAGE AT FRAME 277 AND STR 24R. *S/D* MAJOR REPAIR ACCOMPLISHED: MFG & INSTALLED REPAIR FILLERS, DOUBLER & TRIPLER.SDR 2008FA0000513Spar · corrodedDURING SCHEDULED INSPECTION, FOUND CORROSION ON LT IB MID FLAP, MID SPAR UPPER CHORD. (K)SDR 2008FA0000514Spar · corrodedDURING SCHEDULED INSP, FOUND CORROSION ON LT IB MID FLAP, MID SPAR UPPER CHORD. (K)SDR 2008FA0000538Spar · corrodedDURING SCHEDULED INSP, FOUND CORROSION ON LT IB MID FLAP, MID SPAR UPPER CHORD. (K)SDR 2008UALA03923Oxygen Bottle · reads low700 PSI ON COCKPIT O2 GAUGE. PLS CHECK DIRECT GAUGE ON BOTTLE AND CONTACT SAM.SDR 2008FA0000474Skin · dentedDURING SCHEDULED INSPECTION, FOUND NUMEROUS DENT ON AFT CARGO EXT DOOR SKIN. S/O 312001, OPS 24422. (K)SDR UALA2008111303630Indicator · faultyFLAPS WOULD NOT RETRACT AFTER TAKEOFF. CYCLED INDICATOR CB, NO HELP. RTFL. SUSPECT FAULTY INDICATOR. CYCLED FLAP INDICATOR CB AND FLAPS BEGAN TO OPERATE. REPLACED INDICATOR, OP CHECKS OK. ACMP FCC INTERFERENCE TEST OF FLAP TRANSMITTERS. ALL VALUES NORMASDR 2008FA0000475Floorbeam · corrodedDURING SCHEDULED INSPECTION, FOUND CORROSION ON UNDERSIDE OF "T" CAP REPLACEMENT 986.5 AROUND ATTACH HOLES BL 29R TO BL 29L, NUMEROUS HOLES. (K)SDR DU4R2008193Skin · dentedS/O 312001 OPS NR 24422 - AFT CARGO EXT DOOR SKIN HAS OUT OF LIMIT DENTS BETWEEN 2 EA EXISTING REPAIRS.SDR DU4R2008195Frame · crackedS/O 312001 OPS NR 24727 - CRACK AT MAIN FRAME OB CHORD STA. 188 RT SIDE FLOOR LEVEL (CRACK IN RADIUS).SDR DU4R2008196Shear Web · crackedS/O 312001 OPS NR24728, FLIGHT COMPARTMENT CRACK AT SHEAR WEB BETWEEN SBS 188 - 196 RT FLOOR LEVEL (CRACK EMANATING AT EDGE CUT OUT).SDR 2008UALA01383Elevator · crackedFOUND A CRACK ON THE LT ELEV FWD OF TRIM TAB (DMG) APPROX 8" TO 10" LONG.SDR 2008UALA01413Frame · crackedCABIN FRAME BS 303.9 IS CRACKED ON AFT SIDE DOUBLER AT FEED THROUGH FOR STR 16L. MAJOR REPAIR ACCOMPLISHED: FABRICATED & INSTALLED FRAME REPAIR ANGLE REPAIR. REPAIR OF INTERCOSTAL - FABRICATED AND INSTALLED 2 CLIPS & 2 ANGLES, 1 H-STRAP & 1 FRAME DOUBLER.SDR DHL2008805509Skin · wornNR 1 ENG NACELLE INLET COWL UPPER EXTERNAL SKIN WORN, STA YN 147.534 AT 12 O'CLOCK POS (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2 SHEET 1, 2. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SECTION AND FABRICATED SKIN (AL2024T3 0.080") ASDR DHL2008805510Skin · wornNR 2 ENG NACELLE INLET COWL UPPER SKIN WORN, STA YN 147.334 AT 12 O'CLOCK POS. (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 71-5-2 FIG 2 SHEET 1, 2. REMOVED FASTENERS IAW SRM 51-1-21. CUT OUT DAMAGED SECTION AND FABRICATED SKIN (AL2024T3 0.080") AND SPLICSDR 2008UALA00997Bracket · looseDOOR 1R BRACKET THAT HOLDS GIRT BAR ON DOOR LOOSE. GIRT BAR COMES OUT TOO EASILY. ADJUSTED BRACKET.SDR 2008UALA00418Attach Angle · crackedINTERCOSTAL ATTACH ANGLE IS CRACKED AT BS 294.5 AT STRINGER 11L. MAJOR REPAIR: REPLACED ATTACH ANGLE.
SDR 2008UALA00351Floorbeam · corrodedAFT CABIN FLOORBEAM TEE CAP UPPER SURFACE CORRODED BS 986 LBL 46 - 48, 2 EA MISDRILL MARKS ON BOTH SIDES OF REPAIR FILLER. MAJOR REPAIR: REMOVED DAMAGE. FABRICATED AND INSTALLED NESTED ANGLE STRAP AND FILLER REPAIR.
SDR 2008UALA00187Light · inoperativeAFT SECTION OF EEL LIGHTS INOP. CLEANED AND REPLACED SHORTED POWER STRIP.SDR 2008UALA00081Structure · dentedLEFT HAND SIDE HORIZONTAL STAB HAS DENT LEFT OF A PATCH. DENT MEASURES 6" X 2.5" AND IS .125" DEEP. LOCATED MIDSPAN ON LOWER SURFACE OF LEADING EDGE. A-Y RATIO IS 48. INSTALLED DOUBLER REPAIR.SDR 2008UALA0034Skin · crackedFUSELAGE SKIN CRACKED AT FASTENER HOLE AFT OF E&E COOLING EXHAUST DUCT CUTOUT LBL 2 STA 378.SDR 2007UALA05348Angle · crackedFWD ENTRY DOOR AFT CUTOUT AT BS 360 WEB AT STR 11L CRACKED AT ANGLE. INSTALLED NEW ANGLE.SDR 2007UALA05355Skin · wornUPPER FUSELAGE CROWN SKIN HAS WEAR DAMAGE AT RT DORSAL FIN LANDING AREA FROM STA 907 TO 1006. FABRICATED AND INSTALLED SINGLE EXTERNAL FUSELAGE DOUBLER REPAIR.SDR 2007UALA04580Jumper · inoperativeEMERGENCY ESCAPE PATH LIGHTS INOP FROM ROW 12 TO ROW 16. REPLACED POWER CABLE JUMPERSDR 2007UALA03719None · noneRTFL DUE TO A MASTER CAUTION APU FIRE INDICATION. CLEANED AND TESTED. NO DEFECTS NOTED.SDR 2007UALA03685Steering Sys · malfunctionedNWS PROBLEMS: WHEN CENTERED IT DRIFTS TO THE LEFT OCCASIONALLY. ALSO SEEMS TO BIND. FOUND STEERING METERING VALVE FAULTY. REPLACED THE STEERING METERING VALVE AND PERFORMED A VISUAL INSPECTION OF STEERING CABLES. PERFORMED SEVERAL TAXI TESTS WITH NO BINSDR 2007UALA03601Door Frame · crackedFWD PIT DOORWAY AFT SIDE FRAME IS CRACKED AT LOWER DOOR STOP FITTING.SDR 2007UALA03359Crease Beam · damagedCREASE BEAM INNER CHORD AND WEB CRACKED AT BS 616R RBL 64. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED SECTION OF INBOARD CHORD. FABRICATED & INSTALLED ANGLE REPAIR. REMOVED DAMAGED WEB. FABRICATED & INSTALLED REPLACEMENT WEB.SDR 2007UALA03132Slide · out of positionDOOR 1L SLIDE PACK FELL OUT OF HOLDER WHEN DOOR WAS OPENED. SLIDE DID NOT DEPLOY.SDR 2007UALA02750Inverter · faultyFLOOR EEL LIGHTS INOP FROM SEAT 14C AFT TO GALLEY. REPLACED INVERTER AND CORRECTED WIRING.SDR SWAA073521Engine · failedINFLIGHT SHUTDOWN / DECLARED EMERGENCY. NR 2 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED INTERMITTENTLY. NR 2 ENGINE OIL QUANTITY WENT TO ZERO. PER QRH SHUTDOWN NR 2 ENGINE. REMOVED AND REPLACED NR 2 ENGINE PER MT.SDR 2007UALA01839Light · meltedCREW REPORT: OVERHEAD LIGHT AT SEAT 5B OVERHEATED AND PRODUCED A BURNING SMELL.SDR 2007UALA00917Frame · dentedAFT CARGO COMPARTMENT FRAME DENTED IN FWD RADIUS AT BS 727B BETWEEN STR S25R & STR S26R. *S/D* MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED EXTERNAL DOUBLER REPAIR.
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