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 2005UALA01268Wire · disconnectedEMERGENCY EXIT FLOOR ESCAPE PATH LIGHTS INOP BACK THIRD OF CABIN. RECONNECTED POWER LEADS.SDR 2005UALA01269Lamp · inoperativeAFT EEL LIGHT INOP FRONT OF AFT GALLEY. RECONNECTED LAMP TO POWER CABLE.SDR 2005UALA01267Light · inoperativeRT OVERWING EMERGENCY LIGHT ON EXTERIOR OF FUSELAGE INOPERATIVE. REPLACED LAMP.SDR 2005UALA01264Skin · crackedAFT GALLEY DOOR LWR HINGE CUTOUT IN FUSELAGE LWR FWD EDGE CRACKED. DATA REMOVED CRACK FABRICATED DOUBLER AND TRIPLER PER SRM 53-60-01.SDR 2005UALA01265Frame · misdrilledFWD GALLEY DOOR AFT FRAME UPPER HOLE AT STOP FITTING HAS NO ED. SUPPLEMENTAL DATA UPDATE FABRICATED DOUBLER AND FILLER AND INSTALLED REF AAR EO 50267 AND SRM 51-40-02.SDR AU510002118Oven · failedSPARKS AND ELECTRICAL FUMES EMANATING FROM REAR GALLEY AREA. INSPECTION COULD FIND NO FAULTS BUT THE OVEN WAS REPLACED AS A PRECAUTION. INVESTIGATION CONTINUING.SDR AU510002125Clamp · fractured(AUS) APU BLEED AIR DUCT FRACTURED. BLEED AIR SUPPLY DUCT SEPARATED IN HORIZONTAL STABILISER COMPARTMENT. (CASA# 510002125)SDR CALA0500392Structure · corrodedINSPECTION FOUND R-2 DOOR CHORD CORRODED AT STA 967-986.5, RBL 45. THE R-2 DOOR CHORD WAS REMOVED AND REPLACED IAW SRM 51-40-02.SDR CALA0500393Intercostal · corrodedINSPECTION FOUND R-2 DOOR INTERCOSTAL CORRODED AT DRAIN HOLE, STA 947.5 TO 986.5, RBL 38. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02.SDR CALA0500394Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 986.5, RBL 24 TO RBL 38. THE FLOORBEAM WAS REPAIRED IAW ECRA 5321-01312.SDR CALA0500389Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 967, RBL 0 TO RBL 51. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51.SDR CALA0500388Frame · crackedINSPECTION FOUND A .5 INCH CRACK JUST BELOW UPPER HINGE, LOWER GUIDE PLATE AREA IN R-1 DOOR FUSELAGE CUTOUT FRAME, STA 294.5, S11 R TO S14R. THE DOOR FUSELAGE CUTOUT FRAME WAS REMOVED AND REPLACED IAW SRM 51-10-02 AND 51-40-02.SDR 2005UALA01234Relief Valve · failedEXPERIENCED A RAPID DECOMPRESSION. ACCOMPLISHED SAFETY RELIEF VALVE TEST PER MM 21-32-21 AND TEST FAILED. REPLACED VALVE AND PERFORMED CABIN DEPRESSURIZATION AND ALTITUDE WARNING CHECKS PER MM 05-51-81, SYSTEM OPS GOOD.SDR CALA0500387Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 947, RBL 4 TO LBL 15. THE CORRODED AREAS WERE TRIMMED OUT AND FILLERS AND DOUBLERS WERE INSTALLED IAW SRM 53-60-51, FIGURE 201.SDR ASMF200511004Apu · failedDURING ENGINES STARTING, THE PNEUMATIC AUXILIARY POWER UNIT FAILED. THE ENGINES WERE STARTED WITH EXTERNAL PNEUMATIC PLANT IAW MM 49-11-00, TESTED CORRECT. THE FIM PROCEDURE WAS PERFORMED IAW FIM 49-55 TASK 804, ALL CORRECT.SDR SCNA05009Slide · dislodgedR1 DOOR SLIDE FELL OUT OF SLIDE CASE, DOOR WAS DISARMED. INSTALLED R1 DOOR ESCAPE SLIDE PACK AND COVER TASK 25-66-01-400-801 RII ACCOMPLISHED 2083126.SDR 2005UALA01231Skin · crackedDOOR OPENING AT 2R HAS A CRACK AT THE UPPER HINGE CUT-OUT. VERIFID LENGTH AND LOCATION OF CRACK. CUT OUT DAMAGED AREA AND MFG DOUBLER SKIN REPAIR PER SRM 53-60-01.SDR 2005UALA01232Relay · failedBOTH IRS ON DC LIGHTS ILLUM JUST AFTER LIFTOFF. SUA IRS POWER FAULT HAS NOT REOCCURRED.SDR 2005UALA01233Odor · detectedELEC ODOR DETECTED NEAR ROW 18. SUPPLEMENTAL DATA UPDATE, AIRCRAFT WAS CHECKED WITH NO DISCREPANCIES FOUND, AND NO FURTHER COMPLAINTS OF ELECTRICAL ODOR. AS A PRECAUTION, A CALLOUT HAS BEEN ENTERED TO LOWER THE PSUS BETWEEN ROWS 16 AND 20 TO CHECK FOR DAMAGESDR USAA051325Door Frame · crackedLOCATION: AFT DOOR CUTOUT AFT FRAME AT S25R. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-70-13. DEFECT SIZE: 1 INCHSDR USAA051324Clip · crackedNR 3 FLAP TRACK STRUCTURE IB SIDE, AFT END. FABRICATED AND INSTALLED NEW ANGLE IAW SRM 51-10-02 DEFECT SIZE: 1 INCH.SDR USAA051323Floorbeam · corrodedFLOORBEAM AT RT SERVICE DOOR ENTRY WAY. INSTALLED NEW REPAIR PART IAW SRM 51-40-02 DEFECT SIZE: 2 INCHES X 5 INCHES.SDR USAA051321Stringer · crackedS-5AR B.S. 1138 ACTION: INTERIM REPAIR WAS PREVIOUSLY INSTALLED IAW EA 73450B IAW EA 73450B. LENGTH UNKNOWN.SDR USAA051319Bracket · crackedLOWER FWD CORNER OF MAIN ENTRY DOOR. FABRICATED AND INSTALLED NEW BRACKET IAW SRM 51-10-02. DEFECT SIZE: .50 INCH.SDR USAA051318Stringer Clip · crackedLOCATION: BS360 AND S4R. DEFECTIVE PART REPLACED WITH IDENTICAL PART, IAW SRM 51-10-02 DEFECT SIZE: .50 IN.SDR USAA051317Skin · damagedRUDDER SKIN LT SISE STATION 233.9. DOUBLER INSTALLED ON LT UPPER SIDE OF RUDDER IAW SRM 51-60-05, DEFECT SIZE: 7 INCHES X 1INCH.SDR ASAA0691001Hmu · damagedYYC - AFTER START ON NR 2 ENGINE LEVER RAISED TO IDLE MASTER CAUTION ENGINE AND ENGINE CONTROL ON OVERHEAD PANEL ILLUMINATED. GROUND CREW AND OTHER ACFT REPORTED SMOKE AND TORCHING ON NR 2 ENGINE. NR 2 ENGINE LEVER PLACED TO CUT OUT PER TAIL PIPE FIRE CHECK SDR SB05139Sensor · faultyDURING CRUISE, EN ROUTE FROM ROC TO CLT AT FL340, THE NR 1 ENGINE EXPERIENCED MULTIPLE COMPRESSOR STALLS WHICH LASTED APPROXIMATELY 30 SECONDS EACH. PER QUICK REFERENCE HANDBOOK, CREW REDUCED THRUST AND OPERATED AT THAT POWER THE REMAINDER OF FLIGHT. EGT REMSDR ASMF200510014Pump · failedCAPTAIN REPORTED LOSS OF HYDRAULIC FLUID IN LT SIDE. DURING REVISION DETECTED A LEAK IN LT MAIN PUMP, SO IT WAS REPLACED IAW MM 29-11-11 AC WAS DISPATCHED. AC RETURNED TO PLATFORM, DURING TAXING PSEU AND LT HYDRAULIC SYS LIGHTS TURNED ON. BREAKERS D1 AND D2 WESDR CALA0500378Actuator · inoperativeWHEN THE GEAR HANDLE WAS PLACED DOWN ON FINAL APPROACH, THE NLG DID NOT EXTEND. THE CHECKLIST WAS RUN AND THE GEAR WAS EXTENDED MANUALLY WITH THREE GREEN LIGHTS RECEIVED. THE AIRCRAFT LANDED NORMALLY. MAINTENANCE REMOVED AND REPLACED THE NLG LOCK ACTUATOR ISDR SWAA053376Slide · out of adjustR2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE IAW MM.SDR SWAA053377Cover · looseEEPLS TRACK COVER LOOSE AT FWD END. SECURED COVER IAW MM.SDR SWAA053378Stringer · damagedDURING SCHEDULED MAINTENANCE, FOUND FUSELAGE STRINGER DAMAGED AT BS 482, STR 3R. REPAIRED STRINGER IAW SRM.SDR SWAA053379Frame · crackedDURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 304, STR 16L. REPAIRED FRAME IAW MFG ER.SDR SWAA053380Floorbeam · corrodedDURING SCHEDULED D CHECK, FOUND COCKPIT FLOOR Z-CHORD CORRODED AT BS 270, BETWEEN RBL 11 TO LBL 11, WL 208. REMOVED AND REPLACED Z-CHORD IAW SRM.SDR SWAA053381Crease Beam · corrodedDURING SCHEDULED D CHECK, FOUND LT CREASE BEAM CORRODED BETWEEN BS 294.5 TO BS 360, WL 208. REPAIRED CREASE BEAM IAW SRM.SDR SWAA053384Skin · crackedFUSELAGE SKIN CRACKED AT BS 235.8, EXTERNAL GROUND POWER DOOR CUTOUT. REPAIRED SKIN IAW EA.SDR SWAA053387Relay · faultyAIR TURNBACK, SMOKE AND BURNING ELECTRICAL SMELL IN COCKPIT AND CABIN. REMOVED AND REPLACED R3 RELAY IAW MM.SDR SWAA053372Skin · crackedDURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727D, STR 19R. REPAIRED SKIN IAW EA.SDR SWAA053373Skin · crackedDURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727E, STR 18L. REPAIRED SKIN IAW SRM.SDR SWAA053374Skin · crackedDURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 760, STR 18L. REPAIRED SKIN IAW SRM.SDR SWAA053382Bearing · bindingSHUDDERING AND BINDING FELT IN AILERONS DURING FLIGHT CONTROL CHECK. REMOVED AND REPLACED AILERON CENTERING MECHANISM ROLLER BEARING IAW MM.SDR SWAA053383Cable Assy · misroutedDURING SCHEDULED C1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE LATCH CABLE ASSY MISROUTED. REROUTED CABLE ASSY IAW MM.SDR SWAA053385Skin · crackedDURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 910, STR 4L. REPAIRED SKIN IAW EA.SDR SWAA053386Skin · crackedDURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 520, STR 12R. REPAIRED SKIN IAW EA.SDR 2005FA0001479Wire · crossedDURING TROUBLESHOOTING FOLLOWING PTU TEST FIRE, THE PTU CONTROL VALUE AS FOUND FAILED IN CLOSED POSITION WITH 28 VDC ON PIN: 2 OF VALVE CONNECTOR. AN INVESTIGATION REVEALED WIRES WERE CROSSED AT MFG. WIRING REMADE IAW WDM2911 AND NEW VALVE FIT. (SW152006063SDR SWAA053334Seal · leakingELECTRICAL ODOR IN CABIN FOR APROX 5 MINUTES DURING CLIMB. FOUND NR 2 ENGINE OIL LEAK AT NR 3 OIL BEARING SEAL. MX FERRY TO MDW AND REMOVED AND REPLACED NR 2 ENGINE PER MM.SDR SWAA053375Window · arcedR1 COCKPIT WINDOW ARCED AND CRACKED. REMOVED AND REPLACED R1 WINDOW AND HEAT CONTROLLER IAW MM.SDR UPS05845648Fitting · crackedNA FRAME SUPPORT ATTACH FITTING BELOW L21L AT FS 216 IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D, AND SRM 51-3-2 AT FS 216 L21L.SDR 2005UALA01137Landing Gear · malfunctionedUNABLE TO RAISE GEAR AFTER DEPARTURE. SAFETY SENSORS (AIR & GROUND) FOUND OUT OF ADJUSTMENT . (SENSORS STUCK IN GROUND MODE). REPLACED S106 SENSOR AND ADJUSTED THE CLEARANCE PER MM 32-09-01 AND PERFORMED OPS CHECK GOOD.
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