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 USAA040318Frame · corrodedFRAME , 3.0 INCH X 1.5 INCH X .040 INCH AREA, CORROSION, LEVEL 2; FR66, Y1292, Z240. INSTALLED NEW FRAME IAW SRM.SDR 2004UALA00565Angle · crackedANGLE ON AFT OF INTERCOSTAL STA 294 STR 23L CRACKED. FABRICATED AND INSTALLED ANGLE.SDR USAA040319Frame · corrodedFRAME, .090 INCH X .090 INCH X .026 INCH AREA, CORROSION; LEVEL 2; FR16, Y81, Z240. NEW FRAME ASSY INSTALLED IAW SRM.SDR USA2004F00086Support · corrodedFOUND CORROSION ON SUPPORT PLATE, 6 INCH X 0.5 INCH X .020 INCH. INSTALLED NEW R2 DOOR FORWARD GIRT BAR FITTING SUPPORT PLATE.SDR USA2004F00088Seat Track · corrodedFOUND CORROSION ON SEAT TRACK, 1 INCH X 5 INCHES X .032 INCH. INSTALLED NEW SEAT TRACK SEGMENT AND SPLICES IAW SRM.SDR USAA040269Plate · corrodedPLATE ASSY, 6 INCHES X 4 INCHES X 0.060 INCH DEEP, CORROSION; LEVEL 2; FR68, Y1732, Z240. REPLACED WITH NEW PART IAW SRM.SDR USAA040284Floor Panel · delaminatedFLOOR PANEL, GREATER THAN 10 PERCENT OF AREA, DELAMINATION, MAIN DELAMINATION, MAIN DECK FLOOR PANEL, 221PF. FABRICATED NEW PANEL IAW SRM.SDR USAA040308Floor Panel · delaminatedFLOOR PANEL, 10 PERCENT OF TOTAL AREA, DELAMINATION, MAIN DECK, FLOOR PANEL 261DF. FABRICATED NEW FLOOR PANEL IAW SRM.SDR USAA040309Floor Panel · delaminatedFLOOR PANEL, 10 PERCENT OF TOTAL AREA, DELAMINATION, MAIN DECK, PANEL 262EF. FABRICATED NEW FLOOR PANEL 262 EF.SDR USAA040310Floor Panel · delaminatedFLOOR PANEL, 10 PERCENT OF TOTAL AREA, MAIN DECK FLOOR PANEL 262HG, DELAMINATION. FABRICATED NEW PANEL IAW SRM.SDR USAA040311Floor Panel · delaminatedFLOOR PANEL, EXCEEDS 10 PERCENT OF TOTAL AREA, DELAMINATION, MAIN DECK PANEL 221 PF. FABRICATED NEW FLOOR PANEL IAW SRM.SDR USAA040321Frame · corrodedFRAME, 1.0 INCH X 5 INCHES X 0.71 INCH AREA, CORROSION; LEVEL 2; FR 21 AT Y254. INSTALLED NEW FRAME IAW SRM. INSTALLED NEW FRAME IAW SRM.SDR USA2004F00090Floor Panel · corrodedFOUND CORROSION THROUGH MAIN FLOOR DECK PANEL, 2 INCH X 2 INCH X .040 INCH. REPLACED PANEL.SDR 2004UALA00553Actuator · failedRETURNED TO FIELD DUE TO NR 3 LEADING EDGE FLAP PROBLEM. REPLACEMENT OF THE LEADING EDGE FLAP ACTUATOR CORRECTED THE DISCREPANCY. THE LEADING EDGE FLAP ACTUATOR WAS FOUND WITH A SEVERELY DETERIORATED PISTON HEAD SEAL. THE CONDITION OF THIS SEAL SUPPORTS THE RESDR 2004UALA00558Skin · damagedSKIN DAMAGED AT STA 290 BETWEEN STR 20R AND 22R. REPLACED SKIN PANEL AND STR 21R AND 22R SEGMENTS.SDR USA2004F00075Power Supply · faultyTHE AFT EMERGENCY POWER SUPPLY UNIT FAILED TEST. MAINTENANCE REPLACED THE AFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK.SDR USA2004F00076Battery Pack · dischargedMAINTENANCE REPORTED THE EMERGENCY LIGHT BATTERY PACK, IN THE AFT POSITION, TO BE WEAK. MAINTENANCE REMOVED AND REPLACED THE AFT LEFT EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD.SDR MYW2004F00007Display · shortedDURING CRUISE, (ISFD) INTEGRATED STANDBY FLIGHT DISPLAY, DISPLAYED OUT OF ORDER MSG ONLY. AIRCRAFT DIVERTED. TROUBLESHOT SYSTEM. REMOVED AND REPLACED ISFD IAW 34-24-02. PERFORMED INSTALLATION TEST, TESTED NORMAL. RETURNED AIRCRAFT TO SERVICE.SDR USA2004F00081Pcu · inoperativePILOT REPORTED A SLIGHT UNCOMMANDED RUDDER INPUT WHICH WAS DESCRIBED AS AN UNCONTROLLED RUDDER JERK. JERK WAS NOT ADVERSE OR SEVERE. CREW REPORTED NO RUDDER PEDAL MOVEMENT WAS DETECTED. (A) CHANNEL AUTOPILOT WAS ENGAGED AT TIME IN BOTH LNAV AND VNAV, FLT WASDR USA2004F00078Control System · malfunctionedENROUTE, CREW REPORTED THE ELEVATOR FEEL WAS VERY HARD IN FLIGHT. ON APPROACH, VERY HEAVY NOSE DOWN PRESSURE IS REQUIRED TO GET A MINIMAL NOSE DOWN RESPONSE. ON LANDING, NOT AS MUCH EFFORT WAS REQUIRED. AIRCRAFT WAS FOUND IN SAFE CONDITION FOR MAINTENANCE FSDR USA2004F00080Shuttle Valve · faultyENROUTE, CREW REPORTED THE ELEVATOR FEEL WAS VERY HARD IN FLIGHT. ON APPROACH, VERY HEAVY NOSE DOWN PRESSURE IS REQUIRED TO GET A MINIMAL NOSE DOWN RESPONSE. ON LANDING NOT AS MUCH EFFORT WAS REQUIRED. AC WAS FOUND IN SAFE CONDITION FOR MAINT FERRY FLIGHT. SDR USAA040251Sill · corrodedSILL, 2.0 INCH X 1.0 INCH X 0.06 INCH AREA, CORRODED. BETWEEN FR 66 & 68, BL Y11371, WL Z240. INSTALLED NEW SILL IAW SRM.SDR USAA040317Floor Support · corrodedFLOOR SUPPORT, 2.0 INCH X 1.0 INCH X .026 INCH D, CORROSION; LEVEL 2 BETWEEN FR 21-22, Y1292, Z240. REMOVED AND REPLACED PART IAW SRM.SDR USA2004F00065Strap · misroutedTHE EMERGENCY ESCAPE SLIDE/RAFT GIRT BAR RELEASE STRAP ON THE LT REAR ENTRANCE DOOR WAS FOUND ROUTED INCORRECTLY DURING INSPECTION. MAINTENANCE CORRECTLY ROUTED THE STRAP.SDR IXXA0400084SFitting · crackedDURING A ROUTINE A-CHECK INSPECTION, FOUND ALT. CARGO COMPT FITTING CRACKED AT STA 1260.000. REPAIRS WERE ACCOMPLISHED BY PERFORMING MAJOR REPAIRS IAW SRM 53-1-0 PAGE, PAIR SPECIFICATION NR 2003-05M DWG NR 3350223, REMOVED FASTENERS IAW SRM 51-1-21 PAGE 1, TRSDR USA2004F00059Power Supply · faultyTHE AFT LEFT EMERGENCY POWER SUPPLY UNIT FAILED TESTING. MAINTENANCE REMOVED AND REPLACED THE AFT LEFT EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK.SDR USA2004F00061Release Mech · misroutedTHE EMERGENCY ESCAPE SLIDE/ RAFT GIRT BAR RELEASE STRAP ON THE RT REAR SERVICE DOOR WAS FOUND ROUTED INCORRECTLY DURING INSPECTION. MAINTENANCE CORRECTLY ROUTED THE STRAP.SDR USA2004F00062Release Mech · misroutedTHE EMERGENCY ESCAPE SLIDE/ RAFT GIRT BAR RELEASE STRAP ON THE RT FORWARD SERVICE DOOR WAS FOUND ROUTED INCORRECTLY DURING INSPECTION. MAINTENANCE CORRECTLY ROUTED THE STRAP.SDR USA2004F00064Strap · misroutedTHE EMERGENCY ESCAPE SLIDE/ RAFT GIRT BAR RELEASE STRAP ON THE LT FORWARD ENTRANCE DOOR WAS FOUND ROUTED INCORRECTLY DURING INSPECTION. MAINTENANCE CORRECTLY ROUTED THE STRAP.SDR 2004UALA00527Bear Strap · cutAFT CARGO DOOR CUTOUT AFT EDGE BEAR STRAP REPAIR DOUBLER IS INSUFFICIENT. REPLACED BEAR STRAP DOUBLER.SDR 2004UALA00528Skin · misinstalledBOTTOM BELLY SKIN HAS INSUFFICIENT ED ON THE LT SKIN LAP FASTENER HOLES FROM STA 727-907. REPLACED LOWER BELLY SKIN.SDR 2004UALA00532Splice · misinstalledTWO EA STRINGER SPLICES WERE FOUND WITH INADEQUATE EDGE DISTANCE AT FASTENER LOCATIONS STA 907 STR 26R AND 25R. REPLACED STRINGER SPLICES.SDR 2004UALA00533Beam · corrodedAFT PIT SILL BEAM HAD CORROSION. REPLACED LOWER SILL BEAM WEB.SDR 2004UALA00540Warning Light · illuminatedEQUIPMENT COOLING EXHAUST OFF LIGHT ILLUMINATED IN BOTH NORMAL AND ALTERNATE MODES. THE EQUIPMENT COOLING LOW FLOW SENSOR FAILED. REPLACED THE LOW FLOW SENSOR WITH A NEW AND IMPROVED ONE. PERFORMED EQUIPMENT COOLING EXHAUST SYSTEM TEST. NO FAULTS NOTED.SDR 2004UALA00541Fan Blade · incorrectNUMBER 1 ENGINE VIBRATION AT 5.0. INCORRECT REPLACEMENT OF 2 FAN BLADE PAIRS RESULTED IN UN-BALANCED FAN SYSTEM. REPLACED FAN BLADES.SDR 2004UALA00538Shear Tie · damagedSHEAR TIES WERE FOUND DAMAGED OR HAD EXCESSIVE GAP BETWEEN SKIN AND SHEAR TIE AT STA 727 S24L-S25L, 727D S24L-S25L, 727C S25R-S26R, 727D S25R-S26R, 727E S24L-S25L AND 767 S24L-S25L. *S/D* MAJOR REPAIR ACCOMPLISHED. REPAIRED SHEAR TIES.SDR USA2004F00063Release Mech · misroutedTHE EMERGENCY ESCAPE SLIDE/ RAFT GIRT BAR RELEASE STRAP ON THE RT FORWARD SERVICE DOOR WAS FOUND ROUTED INCORRECTLY DURING INSPECTION. MAINTENANCE CORRECTLY ROUTED THE STRAP.SDR 2004UALA00517Wire · failedFLIGHT DIVERTED DUE TO A STUCK FUEL CROSS-FEED VALVE CAUSING A FUEL IMBALANCE. CREW REPORTED FUEL CROSSFEED LIGHT REMAINS BRIGHT (INDICATING VALVE IS IN TRANSIT) NO MATTER WHAT POSITION THE CROSSFEED SWITCH IS IN. AND FUEL CROSS FEED VALVE POSITION LIGHT DOES SDR 2004UALA00518Stringer Clip · crackedSTATION 277 STRINGER 15R STRINGER CLIP IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED STRINGER CLIP.SDR 2004UALA00519Shear Tie · damagedSTATION 727A INBOARD OF STRINGER 27L SHEAR TIE HAD EXCESSIVE MATERIAL LOSS. REPLACED SHEAR TIE.SDR 2004UALA00520Splice · damagedSTATION 727A STRINGER SPLICE HAS ELONGATED HOLE. REPLACED STRINGER SPLICE.SDR 2004UALA00521Shear Tie · misrepairedSTATION 787 SHEAR TIE BETWEEN STR 2L AND 27R HAS NO EDGE DISTANCE ON PREVIOUS REPAIR. REPAIRED SHEAR TIE.SDR 2004UALA00523Doubler · cutSTRAP DOUBLERS ARE CUT AT STR 26R, BETWEEN STA 727C AND 727D. REPLACED STRAP DOUBLERS.SDR 2004UALA00525Wire · inoperativeEMERGENCY ESCAPE LIGHTING INOP FROM ROWS 15-21. REPLACED FEEDER CABLE ROWS 14-21.SDR USAA040243Skin · crackedSKIN CRACKED (1 INCH X Q.22 INCH) LOWER AFT CORNER FORWARD SERV CUTOUT STA 322, 4 INCH/ 14 INCH. INSTALLED DOUBLERS IAW SRM.SDR AWXA200400582Wire Harness · brokenDURING THRU-FLIGHT INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 16 LT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT WIRE HARNESS AT SEAT ROW 16 LT, OPERATIONAL CHECK WAS GOOD.SDR 2004UALA00516Stringer Clip · crackedSTA 706 STR 4 RT, STRINGER CLIP IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED STR CLIP.SDR AWXA200400581Flashlight · inoperativeEMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE CABIN FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED CABIN EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.SDR USA2004F00058Power Supply · inoperativeTHE EMERGENCY LIGHTS FAILED THE TEST. MAINTENANCE REPLACED THE EMERGENCY LIGHTS POWER SUPPLY. SYSTEM CHECKS OK.SDR 2004UALA00511Light · shortedEMERGENCY EQUIPMENT LIGHT (EEL) IS SHORTING OUT AT THE AFT SECTION OF THE EEL SYSTEM. REPLACE LIGHT ASSEMBLY.
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