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 2006UALA01976Door Frame · crackedFWD PIT DOORWAY AFT SIDE FRAME IS CRACKED AT INBD SIDE OF LOWER DOOR STOP FITTING. MAJOR REPAIR: REMOVED DAMAGE. INSTALLED A DOUBLER, TRIPLER AND FILLER PER AAR EAI060521 REV IR.SDR 2006UALA01977Landing Gear · malfunctionedRETURNED TO DEN DUE TO GEAR RETRACTION PROBLEM. FAULTY NOSE LANDING GEAR MODULAR PACKAGE. REPLACED THE MODULAR PACKAGE. ROOT CAUSE UNKNOWN.SDR 2006UALA01966Support Angle · crackedEMPENNAGE STAB CENTER BOX HAS A SUPPORT ANGLE CRACKED LBL 20, STA 1121. SUPPLEMENTAL DATA UPDATE, MAJOR REPAIR: REMOVED AND REPLACED ANGLE.SDR 2006UALA01975Slide · malfunctioned1L GIRT BAR DROPPED BACK INTO SLOT AS DOOR WAS OPENED CAUSING SLIDE TO PARTIALLY OPEN. THE CLAM SHELL GIRT BAR CLIP ON THE LEFT SIDE, WHEN FACING THE SLIDE, WAS STRETCHED OUT ALLOWING FOR A LOOSE FIT. SLIDE REPLACED ON AIRCRAFT. DEFECTIVE SLIDE OVERHAULED ATSDR 2006UALA01958Wire · inoperativeFLOOR MOUNTED EMERGENCY ESCAPE PATH LIGHTS INOP FROM ROW 16 THROUGH AFT GALLEY. SUPPLEMENTAL DATA UPDATE REPLACED AFT EEL STRIP CABLE.SDR 2006UALA01941O-Ring · pinchedB HYDRAULIC SYSTEM LOW PRESSURE LIGHT AND QUANITY LIGHT. FOUND LEAK AT PRESSURE SIDE OF EDP AT NIPPLE BY CASE. REPLACED PINCHED O-RING AND SERVICED HYDRAULICS TO FULL.SDR 2006UALA01942Light · inoperativeFLOOR STRIP LIGHTS INOP LEFT, AFT CABIN REPLACED 3 EEL LIGHT STRIPS.SDR 2006UALA01937Seal · wornWEAR FOUND RT SIDE AT BULB SEAL OF DORSAL FIN AT STA 998 STR 2R. MAJOR REPAIR: ACCOMPLISHED PERMANENT REPAIR PER UA-EVA-60612.SDR 2006UALA01927Skin · wornFUSELAGE SKIN AT CROWN AREA FROM BS 927-945 HAS .004" OF WEAR UNDER LT SIDE OF DORSAL FIN. INSTALLED WEAR STRIP REPAIR.SDR 2006UALA01928Duct · puncturedNR 1 ENGINE INLET DUCT HAS PUNCTURE AT 12 CLK POS FWD OF MOUNTING FLANGE. MAJOR REPAIR: FABRICATED AND INSTALLED A STAINLESS BONDED DOUBLER.SDR 2006UALA01929Skin · wornRUDDER LE ON RT SIDE HAS WEAR AND DAMAGE INTO FIBER, 8" FROM BOTTOM EDGE. MAJOR REPAIR: INSTALLED 2 PLY REPAIR.SDR 2006UALA01930Skin · wornEXTERNAL FUSELAGE SKIN UPPER CROWN HAS WEAR UNDER DORSAL FIN BLADE SEAL CONTACT POINT. DEEPEST WEAR NOTED .008" BY NDT. MAJOR REPAIR: FABRICATED AND INSTALLED DOUBLER AND TRIPLER REPAIR PER SRM 53-60-01 REPAIR NR 9.SDR 2006UALA01931Lug · corrodedLT HORIZ STAB, FWD UPPER LUG WAS FOUND CORRODED. MAJOR REPAIR: REPAIRED LUG AND BUSHING.SDR 2006UALA01932Skin · gougedLWR FUSELAGE STA 957 BTWN STR 18R AND STR 19R SKIN IS GOUGED. MAJOR REPAIR: REMOVED DAMAGE. ACCOMPLISHED A DOUBLER, TRIPLER AND FILLER REPAIR.SDR 2006UALA01933Tear Strap · undersizeLT AFT PIT REPLACMENT SKIN PANEL TEAR STRAP WAS FOUND TO BE SLIGHTLY SMALLER THAN THE ORIGINAL SKIN AT BS 727C +10" STR 20. MAJOR REPAIR: TRIMMED TEAR STRAP OF NEW REPLACEMENT SKIN TO CLEAR THE ORIGINAL FASTENERS AND ADDED 2 NEW FASTENERS.SDR BJNA061001Brake Assy · seizedAT INITIAL TAXI, AFTER TURN, AIRCRAFT DRAGGED TO A STOP AS RESISTANCE FELT IN LANDING GEAR. INSPECTION FOUND NR 2 BRAKE SEIZURE. REPLACED BROKEN AND DAMAGED PARTS AND OVERHAULED BRAKE ASSEMBLY. (K)SDR PIDR2006022Floorbeam · corrodedFLOORBEAM AT BS 312 CORRODED AT NUTPLATE HOLES FROM RBL8 TO RBL32. REPLACED FLOORBEAM T-CAP IAW SRM 53-10-51.SDR PIDR2006021Skin · wornFUSELAGE SKIN WORN UNDER DORSAL FIN. REPAIRED AREA IAW SB 737-55-1057.SDR PIDR2006020Skin · dentedEXISTING DOUBLER ON FUSELAGE AT BS 400 AND S23RT HAS A DENT. REMOVED EXISTING DOUBLER AND INSTALLED NEW IAW SRM 53-00-01 FIG. 201.SDR PIDR2006019Floorbeam · corrodedUNDERSIDE OF BS 727D+5 FLOORBEAM IN AFT CARGO BIN IS CORRODED FROM LBL17 TO RBL8. REPAIRED AREA IAW SRM 53-00-53 FIG. 201.SDR 2007FA0000126Frame · crackedFRAME IS CRACKED AT BODY STAION 727, STRINGER 14L. (K)SDR 2007FA0000128Skin · dentedBODY STATION 915 ABOVE STRINGER 25L LAP JOINT FUSELAGE SKIN HAS DENT. (K)SDR 2007FA0000135Frame · crackedFRAME IS CRACKED AT BODY STATION 727, STRINGER 14L. (K)SDR 2007FA0000124Skin · gougedUPPER FUSELAGE, STA 860 THRU 885, LBL 8 THRU RBL 8, UNDER DORSAL FIN BLADE SEAL, SKIN IS GOUGED. (K)SDR 2007FA0000125Frame · crackedUPPER FUSELAGE, BS 500A, BETWEEN STR 8R AND STR 9R, FRAME IS CRACKED AT PSU MOUNT. (K)SDR 2007FA0000129Floorbeam · gougedCABIN FLOORBEAM, STA 827, WL 203.6, RBL 10, LOWER T-CAP, AFT FLANGE, GOUGED. (K)SDR 2007FA0000133Frame · crackedCABIN, BS 787, FRAME AT STR 8R, CRACKED AT STOW BIN ATTACH BRACKET. (K)SDR 2007FA0000134Pressure Panel · crackedMID CABIN BS 663, LBL 31, WHEEL WELL PRESSURE DECK WEB, CRACKED. (K)SDR 2007FA0000136Fitting · corrodedDOOR 1R, BS 306-312, WL 248-249, LBL 57-63, SERPENTINE PLATE CASTING CORRODED AROUND FASTENER HOLES. (K)SDR 2006UALA01827Skin · crackedON WALK AROUND, FOUND 3-8 INCH CRACK ON RIGHT HORIZ STAB LEADING EDGE APPROX 6FT FROM INBD SIDE. MAJOR REPAIR: REPAIRED RIGHT HORIZONTAL STAB LEADING EDGE PER SRM 55-10-01.SDR 2006UALA01828Skin · damagedBIRD STRIKE DISCOVERED ON PREFLIGHT WALKAROUND. RIGHT SIDE OF NOSECONE. PEELED METAL BACK. MAJOR REPAIR: REMOVED DAMAGE. FABRICATED AND INSTALLED DOUBLER AND FILLER PER SRM 53-10-01 AND UA-EVA 60585.SDR 2006UALA01811Wire · damagedAFT 20' OF EEL LIGHT INOP. REPLACED THE FEEDER CABLE AND AFT GALLEY EEL LAMP.SDR 2006UALA01816Bottle · lowLOW BOTTLE PRESSURE. UNDETERMINABLE, LEAK TEST ON VALVE PRODUCED NO FINDINGS. REPLACED VALVE.SDR 2006UALA01820Bottle · lowLOW BOTTLE PRESSURE CAUSE: UNDETERMINED, FOUND NO DEFECTS DURING TROUBLESHOOTING. REPLACED THE SLIDE ON A/C. SLIDE VALVE OVERHAULED AS PRECAUTION.SDR 2007FA0000123Intercostal · crackedCABIN STA 303.9 JUST ABOVE STRINGER 10L. INTERCOSTAL OUTER CHORD ANGLE, CRACKED. (K)SDR 2007FA0000127Frame · crackedMID CABIN, STA 500A FRAME, BETWEEN STRINGER 8 AND 9L, CRACKED AT PSU MOUNT RAIL ATTACH POINT. (K)SDR 2007FA0000130Frame · crackedMID CABIN, STATION 400 FRAME AT STRINGER 8R, CRACKED AT PSU RAIL OUNT ATTACH POINT. (K)SDR 2007FA0000131Crease Beam · corrodedAFT GALLEY DOOR CREASE BEAM INNER CHORD ANGLE, BS 947 TO 992, STRINGER 17R, WL 208, CORROSION OUT OF LIMITS. (K)SDR 2007FA0000137Stringer Clip · crackedPASSENGER CABIN, STATION 639 AT STRINGER 4L, STRINGER CLIP, CRACKED. (K)SDR 2007FA0000138Frame · crackedMID CABIN, STATION 480 FRAME, AT STRINGER 8L, CRACKED AT PSU MOUNT RAIL ATTACH POINT. (K)SDR 2007FA0000139Frame · crackedMID CABIN, STATION 500A FRAME, BETWEEN STRINGER 8 AND 9L, CRACKED AT PSU MOUNT RAIL ATTACH POINT. (K)SDR 2007FA0000140Support · crackedAT FWD CABIN STA 328+6, DOOR 2R AFT STOP FTG INTERCOSTAL TEE SUPPORT, CRACKED. (K)SDR 2006UALA01775Skin · scratchedFOUND DEEP SCRATCH ON SKIN ABOUT 1" LONG AT STR 3L, STA 277. MAJOR REPAIR ACCOMPLISHED PER SRM 53-00-01 REPAIR 31.SDR 2006FA0000922Amplifier · fireWHILE MAINTENANCE PERSONNEL WERE PERFORMING A ROUTINE POST FLIGHT INSPECTION, A TECHNICIAN DISCOVERED A PROBLEM. ACFT POWERED BY EXTERNAL POWER, AND CABIN ENTERTAINMENT SYS OPERATING (PLAYING A DVD MOVIE) WITH THE AUDIO SYSTEM VOLUME AT A LOW LEVEL. AFTER A SDR SA06072Engine · shutdownFLT1408 - DURING CRUISE, EN ROUTE FROM SFO TO CLT, CREW RECEIVED ECAM MESSAGE "ENG 2 HI TEMP FADEC OVHT" AND "ENG 2 FADEC B FAULT" ALONG WITH OTHER ASSOCIATED FAULT MESSAGES. CIRCUIT BREAKER FOR ENG 2 FADEC TRIPPED, AND MOMENTS LATER, THE NR 2 ENGINE AUTOMATISDR 2006FA0001198Rudder · damagedRUDDER DAMAGED DUE TO LIGHTENING STRIKE WHILE AIRCRAFT WAS ON GROUND. DETAILED INFORMATION CONCERNING THIS REPAIR CAN BE FOUND ON (NR 10981-3600-0001). (K)SDR SB06088Unknown · unknownDURING CRUISE, EN ROUTE FROM CLT TO ROC, CREW REPORTED THE NR 2 ENGINE FLAMED OUT (AND THE CROSSFEED LIGHT EXTINGUISHED) WHILE CROSSFEEDING FUEL AT FL370. CREW DECLARED AN EMERGENCY TO CLEAR TRAFFIC AND DESCEND TO LOWER ALTITUDE AND WAS ABLE TO RESTART NR 2 ESDR 2006UALA01752Bulkhead · corrodedAFT EQUIPMENT BAY FWD SIDE OF 1016 BULKHEAD, STA 1016 - 1022 RBL 6-LBL 6 STR 27R AND 27L IS CORRODED. REMOVED CORRODED SECTION. FABRICATED AND INSTALLED RADIAL DOUBLER AND STIFFENER SPLICES.SDR 2006UALA01747Doubler · damagedCHAFING ON PREVIOUS FUSELAGE SKIN REPAIR DOUBLER UNDER DORSAL FIN BLADE-BULB SEALS BS 886-897. MAJOR REPAIR; REMOVED DAMAGE. FABRICATED AND INSTALLED DOUBLER AND TRIPLER REPAIR.SDR 2006UALA01748Keelbeam · corrodedFWD PIT BILGE KEEL BEAM CHORD IS CORRODED AT BS 523 STR 28L WL 149. REMOVED CORROSION. FABRICATED AND INSTALLED ANGLE AND 2 FILLERS.
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