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 BJNA110402Battery · inoperativeAFT LT INBD EMERGENCY FLASHLIGHT CHARGE WEAK. R & R AFT F/A FLASHLIGHT BATTERY IAW AMM 33-51-02.SDR F3LA2011040500623Plate · corrodedC-CHECK: NON ROUTINE NR 36902; FRAME 70 RT INTERNAL SHEAR PLATE HAS CORROSION. R & R SHEAR PLATE IAW SRM 51-42-11, FIG 8, 51-44-11 PARA 6A (1), 7A(1) AND PARA 7, FIG 12, 51-21-11 PARA 4 (A)-(D), 51-75-12 AND 51-23-11.SDR DU4R2011002Skin · dentedDURING SCHEDULED INSP, FOUND RT OTBD FLAP, OTBD UPPER SKIN DENTED, CREASED DENTS.SDR DU4R2011001Threshold · corrodedDURING SCHEDULED INSP, FOUND R-2 DOOR THRESHOLD FLOOR ATTACH ANGLE HAS SURFACE CORROSION.SDR F3LA2011022100605Engine · overtempAIR TURN BACK DUE TO BIRDSTRIKE ON NR 1 ENGINE. ENGINE SHUTDOWN, INVESTIGATION FOR ENGINE SHUTDOWN SHOWS THE EGT WAS EXCEEDED AT 1015 DEGREES CELCIUS FOR 21 SECONDS. PERFORMED AN AIRFRAME AND ENG NR 1 BIRDSTRIKE INSP. REF TASK CARDS MP05510-02 AND MP72400-0SDR F3LA2011021700601Shear Plate · corrodedC-CHECK: NON ROUTINE N0284; RT AFT FUSELAGE SHEAR PLATE BETWEEN FRAMES 69R AND 70R HAS 4 SQUARE INCHES OF CORROSION. EO AO-53EO-31434 SHEAR PLATE NEEDS TO BE REPLACED WITH NEW CONFIGURATION. REPLACED RT SHEAR PLATE BETWEEN FRAMES 69R AND 70R WITH NEW CONFIGUSDR IXXA110019OConnector · dirtyDURING TAKEOFF, NR 1 ENG OIL PRESSURE LIGHT CAME ON INTERMITTENTLY, OIL TEMP AND PRESSURE GOOD ON FLIGHT ENGINEER PANEL. THE CREW ABORTED TAKEOFF AND RETURNED TO BLOCKS WITHOUT FURTHER INCIDENT. MX CLEANED THE CONNECTOR PLUG ON DIFFERENTIAL PRESSURE WITH. OSDR IXXA110018OTarget · looseDURING CLIMBOUT, AFTER GEARS WAS RETRACTED THE DOOR NOT LATCH LIGHT REMAINED ON. THE CREW CYCLED THE GEARS, DOOR NOT LATCH LIGHT STILL REMAINED ON, AFTER ACCOMPLISHING UPLATCH CHECK LIGHT WENT OUT. THEY LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED BOTH LT ASDR IXXA11SMN023SSkin · wornDURING ROUTINE C-CHECK INSP FOUND RT WING OTBD FLAP SKIN WORN AT STA XRS 162.263. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED, PAINTED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS ANDSDR DHLA201100001Battery Pack · inoperativeEMERGENCY EXIT LIGHTS ARE VERY DIM. ACFT WAS GROUNDED. R & R EMER EXIT LIGHTS POWER SUPPLY, OPS CHECK GOOD IAW AMM 33-50-1. EMERGENCY LIGHT CB WILL NOT RESET. R & R EMERGENCY LIGHT BATTERY PACK. SYS OPS CHECK GOOD IAW 33-50-00.SDR DALA1100573257Power Supply · faultedDURING NON-ROUTINE CHECK, FOUND THE EMERGENCY POWER SUPPLY UNIT FAULTED AT 10WL. MX REPLACED POWER SUPPLY UNIT AND FUNCTIONAL CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.SDR DALA1053713226Light · missingFLIGHT CREW REPORTED EMERGENCY PATH FLOOR LIGHT SEAT 5C MISSING AND WIRES ARE EXPOSED, INSTALLED COVER AND TESTS OK.SDR DALA1053133258Connector · unsecureDURING A NON ROUTINE, THE EMERGENCY LIGHT INTEROR LOAD TEST OF EPSU FAULTS THE FWD LT. MX RESEATED THE CONNECTOR PLUG AND FUNCTIONAL CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.SDR DALA1053163258Connector · disconnectedDURING A NON ROUTINE CHECK, FOUND THE EMERGENCY PATH LIGHT AT SEAT ROW 11L INOPERATIVE. MX RECONNECTED HARNESS TO CONNECTOR AND FUNCTIONAL CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.SDR SWAA107960Fuel Sys · leakingENGINE SUTDOWN, DIVERSION, DECLARED EMERGENCY. SURGE/VIBRATION ON NR 2 ENGINE FIRE WARN LIGHT INDICATION. SHUTDOWN ENGINE. FIRE INDICATION WENT OUT AFTER FIRE HANDLE PULLED. REMOVED AND REPLACED NR 2 ENGINE PER MT.SDR CALA2010122000625Channel · corrodedSTA 787, S24-25L CORRODED, REMOVED CORROSION, ORIGINAL THICKNESS .050 MAT REMAINING .033. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101. REMOVED CHANNEL IAW SRM 51-40-02. INSTALLED NEW CHANNEL IAW SRM 51-40-02. NEW CHANNEL FABRICATED ON N/R 6603371/10 SDR MYWA100131Warning Light · illuminatedETOPS SIGNIFICANT SYS: LT ENGINE BLEED TRIP OFF LIGHT ILLUMINATES AND WILL NOT RESET FOR MORE THAN 2 MINUTES. RESET LT ENGINE BLEED LIGHT. PERFORMED ENGINE BLEED OPS CHECK. SYS CHECKED NORMAL.SDR DALA1051913259Battery Pack · inoperativeDURING A NON ROUTINE CHECK, FOUND THE EMERGENCY LIGHT AT 10WL INOPERATIVE. MX REPLACED THE BATTERY PACK AND FUNCTIONAL CHECK WAS NORMAL. ACFT RETURN TO SERVICE.SDR IXXA100060OConnector · looseDURING CRUISE NR 1 ENGINE FIRE WARNING AND BELL FLICKERED MOMENTARILY AT 410, SAT -50, TAT -21, MANIFOLD PRESSURE 32, MANIFOLD AIR TEP 150. THE CREW TESTED FIRE WARNING AND SHORT CIRCUIT WERE NORMAL CONDITION, REMAINED NORMAL REST OF FLIGHT. THEY LANDED IN KSJSDR MYWA100130Valve · inoperativeETOPS SIGNIFICANT SYS: DURING CLIMB, THROUGH FL240, LT DUCT PRESSURE INDICATED 22 PSI AND RT DUCT PRESSURE INDICATED 42 PSI. REPLACED NR1 ENGINE HIGH STAGE VALVE.SDR DALA1036033213Floor Panel · delaminatedDURING L-CHECK, FOUND FWD CARGO COMPARTMENT, ZONE 130 FLOOR PANEL 131EF HAS DELAMINATION. REMOVED FLOOR PANEL 131EF IAW AMM 53-22-14-000-001. FABRICATED NEW PANEL IAW SRM 53-02-00, FIG 209. INSTALLED PANEL IAW AM, M 53-22-14-000-001.SDR DALA1036043213Floor Panel · crackedDURING L-CHECK, FOUND AFT CARGO COMPARTMENT FLOOR PANEL 151PF CRACKED. REMOVED FLOOR PANEL IAW AMM 53-42-14-000-001. FABRICATED NEW PANEL IAW SRM 53-02-00, FIG 209. INSTALLED NEW FLOOR PANEL IAW AMM 53-42-14 -000-0.SDR DALA1036053213Floor Panel · delaminatedDURING L-CHECK FOUND FWD CARGO COMPARTMENT, ZONE 130 - FLOOR PANEL 131AF DELAMINATED. REMOVED FLOOR PANEL 131AF IAW AMM 53-22-14-000-001. FABRICATED NEW PANEL IAW SRM 53-02-00, FIG 209. INSTALLED PANEL IAW AMM 53-22-14-000-001.SDR DALA1051893269Connector · unsecureDURING A NON ROUTINE CHECK, FOUND THE EMERGENCY PATH LIGHT AT SEAT 5C AND 8C INOPERATIVE. MX RESECURED WIRING CONNECTORS AND FUNCTIONAL CHECK WAS NORMAL. ACFT RETURNED SERVICE.SDR DALA1052013748Windshield · crackedCLIMBING OUT OF 8000 FT THE LT OUTER PANE CRACKED. FLIGHT RETURNED TO MSP, LANDING UNEVENTFULLY. MX REPLACED THE L1 WINDOW IAW THE AMM. OPS TESTED WINDOW HEAT IAW THE AMM.SDR DHLA201000150Skin · damagedINSPECTED EXISTING REPAIR LOCATED AT FS 1890.000, L36 FOR CONDITION, SECURITY AND CONFORMITY. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, DATED 12-09-10 AND EVA D853-00384 REV "IR" DATED 11-18-10. REMOVED EXISTING REPAIR IAW SRM 51-1-21. TRIMMED OUT DAMAGED ASDR DHLA201000152Access Door · corrodedACCESS DOOR HAS CORROSION AT FUSELAGE STA FS 650.000 L32R - L36. PERFORMED MAJOR REPAIR IAW ASTAR EC-02354-001 AND DWG 5800471 AND WO 9735. REMOVED CORRODED ACCESS DOOR IAW DPS 3.67 AND SRM 51-3-0. REMOVED CORROSION IAW SRM 51-1-8. FOUND OUT OF LIMITS IAWSDR DALA1035333228Stringer · corrodedDURING LINE CHECK FOUND STR 31 AT FR 65 AND FR 66 RT HAS CORROSION JUST BELOW OUTFLOW VALVE. REMOVED DAMAGED SECTION OF STR REMOVED ENTIRE STR DRILLED UP NEW STRINGER. INSTALLED ENTIRE STR 31RT. COMPLIED WITH RII REQUIREMENTS FOR THE INSTALLATION AND SECURITY SDR DALA1035143133Shear Tie · bentDURING L-CHECK, FOUND THS COMPARTMENT FR 74 BETWEEN S 32L- S33L SHEAR TIE IS BENT. REMOVED SHEAR TIES IAW SRM 51-42-11. FABRICATED SHEAR TIE IAW SRM 53-51-12, FIG 4. LOCATED AND DRILLED NEW SHEAR TIES IAW SRM 51-44-11. TREATED AND PRIMED IAW SRM 51-21-11. SDR DALA1035153133Shear Tie · crackedDURING L-CHECK, FOUND THS COMPARTMENT FR 74 BETWEEN S 31R- S 32R SHEAR TIE IS CRACKED. REMOVED SHEAR TIE IAW SRM 51-42-11. FABRICATED SHEAR TIE IAW SRM 53-51-12 FIG 4. LOCATED AND DRILLED NEW SHEAR TIE IAW SRM. TREATED AND PRIMED IAW SRM 51-21-11. APPLIEDSDR DALA1035163133Shear Tie · bentDURING L-CHECK, FOUND THS COMPARTMENT FR 73 BETWEEN S 32L-S 32R, SHEAR TIE IS BENT IN 2 PLACES. REMOVED SHEAR TIE IAW SRM 51-42-11. FABRICATED NEW SHEAR TIE IAW SRM 53-51-12. LOCATED AND DRILLED NEW SHEAR TIE IAW SRM 51-44-11. TREATED AND PRIMED IAW SRM 5SDR DALA1035173133Shear Tie · crackedDURING L-CHECK, FOUND THS COMPARTMENT FR 74 BETWEEN S 31L-S 32L SHEAR TIE IS CRACKED. REMOVED SHEAR TIE IAW SRM 51-42-11. FABRICATED SHEAR TIE IAW SRM 53-51-12 FIG 4. LOCATED AND DRILLED NEW SHEAR TIE IAW SRM 51-44-11. TREATED AND PRIMED IAW SRM -51-21-11.SDR DALA1035183133Shear Tie · bentDURING L-CHECK, FOUND THS COMPARTMENT FR 73 BETWEEN S 32L-S 32R, SHEAR TIE BENT IN 2 PLACES. REMOVED SHEAR TIE IAW SRM 51-42-11. FABRICATED NEW SHEAR TIE ON IAW SRM 53-51-12. LOCATED AND DRILLED NEW SHEAR TIE IAW SRM 51-42-11. TREATED AND PRIMED IAW 51-21-11. SDR DALA1035193133Shear Tie · crackedDURING L-CHECK, FOUND THS COMPARTMENT FR 74 BETWEEN S 32R-S 33R SHEAR TIE IS CRACKED. REMOVED SHEAR TIE IAW SRM 51-42-11. FABRICATED NEW SHEAR TIE IAW SRM 53-51-12. LOCATED AND DRILLED NEW SHEAR TIE IAW SRM 51-44-11. TREATED AND PRIMED IAW SRM 51-21-11. ASDR DALA1050943218Light · inoperativePILOT REPORTED SEAT 24C EMERGENCY PATH LIGHT OUT, REPLACED LIGHT ASSY AND TESTS OK.SDR DALA1050743217Power Supply · inoperativeAFTER PUSH BACK THE F/A REPORTED THAT THE EMERGENCY EXIT LIGHTS WERE NOT ILLUMINATED, RETURNED TO GATE AND THE FLIGHT CANCELLED. THE FRONT LT EPSU (10WL) WAS REPLACED AND TESTS OK.SDR DALA1050753250Connector · unsecureDURING EMERGENCY LIGHT TEST EPSU FWD LT SHOWED LOAD FAULT, SECURED CONNECTOR AND TEST OK.SDR DALA1050763170Light · inoperativeDURING NON ROUTINE CHECK, FOUND 5C EMERGENCY EXIT LIGHT INOPERATIVE. MX REPLACED LIGHT ASSY AND FUNCTIONAL CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.SDR DHLA201000142Skin · corrodedFUSELAGE SKIN BULGING AND CRACKED BETWEEN 2 FASTENERS AT FS 1447.0, BETWEEN LONGERONS 30R AND 29R. ACCOMPLISHED FUSELAGE SKIN DOUBLER AND FILLER REPAIR IAW EVA D853-00386 REV IR, DWG NR D85300386-001-D, REV IR, AND SRM CHAPTERS 51 & 53. HFEC OF REPAIR PARTS SDR DALA1035033218Light · no testDURING EMERGENCY LIGHT TEST, AFT LT SHOWED LOAD FAULT, REPLACED SLIDE 2R AND CHECKED OK. (2010-00905)SDR DALA1034643270Wire · damagedDURING A NON ROUTINE CHECK, FOUND THE EMERGENCY PATH LIGHT AT ROW 1 INOPERATIVE. REPAIRED PULLED WIRE AT CONNECTOR UNDER SEAT AND FUNCTIONAL CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.SDR DALA1034623241Floorboard · damagedDURING LINE CHECK FOUND AFT CARGO FLOORBOARD 151GF DAMAGED. R & R AFT CARGO FLOORBOARD 151GF IAW MM. OK FOR SERVICE.SDR DALA1034633266Hinge Fitting · chafedDURING M-CHECK FOUND CHAFE DAMAGE ON RT & LT MLG FWD DOOR HINGE FITTINGS, FWD LUG, FWD FACE. IAW ERA 482533-14AD, FOLLOW UP INSP IS REQUIRED ON THE LT & RT MLG DOOR FWD HINGE FITTING. ACCOMPLISH SECTION II INSP NTE 3500 CYCLE INTERVALS FROM 03JUN10.SDR DALA1050113765Light · intermittentDURING TEST, THE EMERGENCY EGRESS AISLE LIGHTING FROM ROW 25AFT WARD TO THE L2 DOOR, EXTINGUISH AFTER 15-20 SECONDS. REPLACED EMERGENCY LIGHT BATTERY PACK M1673, OPS CHECK NORMAL.SDR DALA1034473757Unknown · fumesFOLLOWING 2 PASSENGERS WITH MEDICAL SITUATIONS IN CABIN (PASSED OUT & RECOVERED), AFT CABIN F/A AND PASSENGERS MENTIONED BURNING NOSE/SORE THROATS. CREW ELECTEDTO DIVERT AND LANDED UNEVENTFULLY. MX INSPECTED ENGINES, BAG BINS, E&E COMPARTMENTS, ACCOMPLISHED ESDR MYWA100123Warning Light · illuminatedETOPS SIGNIFICANT SYS: DURING PREFLIGHT, A SYS ELEC/HYD LIGHT REMAINED ILLUMINATED WITH THE PUMP ON AND 3030 PSI SYS PRESSURE.SDR DHLA201000137Control Valve · shearedLT BRAKE INOP, BRAKE PRESSURE NORMAL. ACFT WAS GROUNDED. REPLACED WHEEL BRAKE CONTROL VALVE ASSY IAW MM 32-42-2. SYS OPS NORMAL, OK FOR SERVICE.SDR DALA1050143705Intercostal · corrodedFWD GALLEY/ LAV INTERCOSTAL CORRODED AT FS 309, LBL13. REPLACED INTERCOSTAL IAW SRM 51-40-02.SDR DALA1050223705Floorbeam · corrodedFLOORBEAM HAS SCRIBE MARKS AND CORRODED. REPLACED T CAP IAW SRM 53-70-51, REPAIR 4.SDR 2010FA0001178Filter · deteriorated(C7GR) ON 2 HMU’S RETURNED FOR FUNCTIONAL ISSUES, FOUND THE EHSV NOZZLE CLOGGED, PREVENTING PROPER OPERATION OF THE EHSV. THE FIRST CONFIRMED FIELD EVENT WAS BECW7260 (2731 HRS TSN), REMOVED ON OR ABOUT JUNE 28, 2010 FOR AN IN-FLIGHT SHUTDOWN AS A RESULT OF A
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