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.

SDR USAA040254Floorbeam · corrodedFLOORBEAM, 2.5 INCH X 1.5 INCH X .030 INCH DEEP, CORROSION. REMOVED AND REPLACED FLOORBEAM IAW SRM.May 28, 2004 · N102UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA040255Sill · corrodedDOOR SILL, 1.0 INCH X 1.5 INCH X 0.07 INCH DEEP, CORROSION; LEVEL 2; FR 66 TO 68, -Y 1524, Z-240. REPLACED DOOR SILL IWA SRM.May 28, 2004 · N102UW · Airbus A320214 · Fuselage Miscellaneous StructureSDR 2004UALA00510Shear Tie · crackedSTA 887 SHEAR TIE BETWEEN STR 24R AND 25R IS CRACKED. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGED SHEAR TIE WEB AND REPLACED.May 27, 2004 · N399UA · Boeing 737322 · Fuselage Main, FrameSDR USAA040252Plate · corrodedPLATE CORROSION, 4 INCH X 4 INCH X .70 INCH DEEP. REMOVED AND REPLACED PORT IAW SRM.May 27, 2004 · N102UW · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA040253Angle · corrodedANGLE CORROSION, 2.0 INCH X 2.0 INCH X .02 INCH DEEP. REMOVED AND REPLACED PART IAW SRM.May 27, 2004 · N102UW · Airbus A320214 · Fuselage Miscellaneous StructureSDR DL738040464Spar · damagedRT IB MAIN FLAP FRONT SPAR LOWER CHORD FOUND TO BE DAMAGED. DAMAGE WAS LOCATED BETWEEN 26 INCHES AND 34 INCHES FROM THE IB END OF SPAR. DAMAGE WAS REMOVED AND REPAIR INSTRUCTION ISSUED IAW ERA 090294-14.May 26, 2004 · N390DA · Boeing 737832 · Trailing Edge FlapsSDR DL78K040467Fseu · failedRETURN TO ATL, WITH LEADING EGDE SLAT NR 1 AND LEADING EDGE FLAPS NR 1 AND NR 4, REMAINING ILLUMINATED AMBER ON AFT OVERHEAD ANNUNCIATOR, LE FLAP TRANSIT REMAINED ILLUMINATED CREATING LE LOCKOUT NO ADVERSE ROLL. REPLACED FSEU FOR FAULT CODE 27-51105.May 26, 2004 · N399DA · Boeing 737832 · Leading Edge Slat Control SystemSDR AALA20040590Battery Pack · dischargedBDL SEAT EMERGENCY LIGHTS AT ROWS 5 THROUGH 8 INOPERATIVE. REPLACED BATTERY PACK FOR SEAT EMERGENCY LIGHTS AT ROWS 5 THROUGH 8. SYSTEM GROUND CHECKED NORMAL OPERATION.May 26, 2004 · N921AN · Boeing 737823 · Emergency LightingSDR 2004UALA00505Water Separator · contaminatedFLIGHT DIVERTED TO MRY DUE TO A BURNING ODOR IN COCKPIT. WATER SEPARATOR TEMPERATURE SENSOR FAILED. REPLACED TEMPERATURE SENSOR AND LH/RH COALESCER BAGS. PERFORMED OPERATIONAL TEST AND NO SMELL NOTED.May 26, 2004 · N919UA · Boeing 737522 · Humidity Control SystemSDR 2004UALA00506Frame · misinstalledSTA 178 LT UPPER FRAME HAS SHORT EDGE DISTANCE AT SPLICE. MAJOR REPAIR ACCOMPLISHED. INSTALLED ANGLE DOUBLER.May 26, 2004 · N399UA · Boeing 737322 · Fuselage Main, FrameSDR USAA040247Floorbeam · corrodedFLOORBEAM, 3.0 INCH X 1.5 INCH X .03 INCH AREA. CORROSION; LEVEL 2. REMOVED AND REPLACED FLOORBEAM IAW SRM.May 26, 2004 · N102UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA040248Floorbeam · corrodedFLOORBEAM, 2.0 INCH X 2.0 INCH X .035 INCH D, CORROSION BETWEEN FR 64 &66, +Y 1270, Z240. REMOVED AND REPLACED FLOORBEAM IAW SRM.May 26, 2004 · N102UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA040249Floorbeam · corrodedFLOORBEAM, 2.0 INCH X 2.0 INCH X .025 INCH D, BETWEEN FR 68-69, Y1270, Z240, CORROSION. REMOVED AND REPLACED FLOORBEAM IAW SRM.May 26, 2004 · N102UW · Airbus A320214 · Fuselage Main, Floor BeamSDR AWXA200400576Socket · burnedPRIOR TO DEPARTURE, FLIGHT CREW OBSERVED SMOKE IN CABIN BETWEEN SEAT ROWS 13 AND 18. MAINTENANCE DEACTIVATED THE RECIRCULATION FAN AND PLACED SYSTEM ON MEL 21-31, COND. 1 (RECIRC FAN INOP). AIRCRAFT WAS MAINTENANCE FERRIED BACK TO PHX WHERE MAINTENANCE DISCOVEMay 25, 2004 · N309AW · Boeing 7373G7 · Passenger Compartment LightingSDR USAA040250Seat Track · corrodedSEAT TRACK, 5.45 INCH X 0.813 INCH X .047 INCH D, CORROSION, FR17 AT Y 1270, Z240. REMOVED AND REPLACED SEAT TRACK IAW SRM.May 25, 2004 · N102UW · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR USA2004F00055Charger · failedMAINTENANCE REPORTED NUMEROUS EMERGENCY LIGHTS, THROUGHOUT THE INTERIOR CABIN, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY AND BATTERY PACK. OPERATIONAL CHECK GOOD.May 25, 2004 · N425US · Boeing 737401 · Emergency LightingSDR USA2004F00060Lanyard · missingTHE ESCAPE SLIDE RELEASE LANYARD WAS FOUND NOT INSTALLED WHEN SLIDE WAS REMOVED FOR ACESS DURING THE HEAVY MAINTENANCE VISIT. MAINTENANCE ACTION PENDING.May 25, 2004 · N710UW · Airbus A319112 · Escape SlideSDR 2004UALA00496Skin · damagedLEFT EXTERNAL FUSELAGE AFT OF L2 DOOR IS DAMAGED. REPAIR ACCOMPLISHED. INSTALLED DOUBLER/TRIPLER.May 24, 2004 · N906UA · Boeing 737522 · Fuselage Main, Plate/SkinSDR 2004UALA00499Skin · dentedLEFT FUSE SKIN AND SIDE FRAME DENTED AT BS 178 WL 195. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER.May 24, 2004 · N906UA · Boeing 737522 · Fuselage Main, Plate/SkinSDR USAA040260Pad · corrodedADAPTER PAD, 11 INCH X 2 INCH X 0.050 INCH, CORROSION; LEVEL 2; AFT GIRT BAR FITTING, R1 DOOR, FR 19-20, Z240, Y1293. REPLACED PORT GIRT BAR FITTING ADAPTER IAW SRM.May 24, 2004 · N102UW · Airbus A320214 · Escape SlideSDR USA2004F00095Check Valve · contaminatedON APPROACH, CAPTAIN REPORTED THE RT MLG RED UNSAFE LIGHT ILLUMINATED AND THAT THE RT MLG WOULD NOT EXTEND. TOWER CONFIRMED THAT THE RT MLG WAS NOT DOWN. CAPTAIN EXTENDED THE RT MLG MANUALLY USING THE ALTERNATE GEAR EXTENSION PROCEDURES. GEAR FELL AND LOCKEMay 24, 2004 · N352US · Boeing 737301 · Landing Gear Retraction/Extension SystemSDR USAA040240Sill · corrodedDOOR SILL, 1.0 INCH L X 1.2 INCH W X .08 INCH D. REMOVED AND REPLACED DOOR SILL IAW SRM.May 22, 2004 · N701UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040256Floorbeam · corrodedFLOORBEAM, 1.0 INCH X 1.0 INCH X .03 INCH D, CORROSION; LEVEL 2; FR64-66, Y787, Z240. REMOVED AND REPLACED FLOORBEAM IAW SRM.May 22, 2004 · N102UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA040259Floorbeam · corrodedFLOORBEAM, 1.5 INCH X 1.0 INCH X .02 INCH DEEP, CORROSION; LEVEL 2; FR 66-68, Y787, Z240. REMOVED AND REPLACED FLOORBEAM IAW SRM.May 22, 2004 · N102UW · Airbus A320214 · Fuselage Main, Floor BeamSDR AWXA200400562Battery · dischargedLCQ - EMERGENCY EQUIPMENT - DURING C-19 CHECK FOUND THE AFT GALLEY EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AFT GALLEY EMERGENCY FLASHLIGHT BATTERY, OPERATIONAL CHECK WAS GOOD.May 21, 2004 · N175AW · Boeing 73733A · Emergency EquipmentSDR 2004UALA00497Frame · misinstalledSTATION 178 LT UPPER FRAME WL 243 NO EDGE DISTANCE. MAJOR REPAIR ACCOMPLISHED. FABRICATED & INSTALLED ANGLE SPLICE REPAIR.May 21, 2004 · N906UA · Boeing 737522 · Fuselage Main, FrameSDR MYW2004F00002Duct · contaminatedON TAKEOFF THRUST, SMOKE IN COCKPIT AND CABIN. ABORTED TAKEOFF AND RETURNED TO HANGER. TROUBLE SHOT SYSTEM. ACCOMPLISHED AIR CONDITIONING PACK BITE CHECK. CHECK WAS NORMAL. REMOVED APU SUPPLY DUCT CONNECTOR TO CHECK FOR CONTAMINATION IAW 49-11-02. NONE FMay 21, 2004 · N733MA · Boeing 737800* · Air Distribution SystemSDR USAA040233Girt Bar · corrodedPLATE (GIRT BAR) 1.30 INCHES X .50 INCH AREA. CORROSION; LEVEL 2; TASK NR JA-26053500, FR 68, Z240, Y1230. EXFOLIATED ON OB EDGE, REMOVED AND REPLACED PLATE IAW SRM.May 21, 2004 · N701UW · Airbus A319112 · Escape SlideSDR USAA040237Support Angle · corrodedSUPPORT ANGLE ASSY, .95 INCH X .50 INCH AREA, CORROSION; LEVEL 2 Z240,Y1732, X=843. REMOVED AND REPLACED SUPPORT ANGLE ASSY IAW SRM.May 21, 2004 · N701UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040238Floorbeam · corrodedFLOORBEAM, 1.3 INCH X 1.9 INCH X .35 INCH DEEP, CORROSION; LEVEL 2; TASK NR JA26053500, FR68, Y1300MM, Z240. REMOVED AND REPLACED FLOORBEAM IAW SRM.May 21, 2004 · N701UW · Airbus A319112 · Fuselage Main, Floor BeamSDR USAA040239Floor Support · corrodedFLOOR SUPPORT, 1.5 INCH X 1.2 INCH X .055 INCH DEEP, CORROSION; LEVEL 2. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM.May 21, 2004 · N701UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040257Floorbeam · corrodedFLOORBEAM, 1.0 INCH X 1.0 INCH X .025 INCH DEEP, CORROSION, LEVEL 2; BETWEEN FRAME 64 & 66, +Y787, Z240.May 21, 2004 · N102UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA040258Floorbeam · corrodedFLOORBEAM, 3.0 INCH X 2.0 INCH X .025 INCH DEEP, CORROSION, LEVEL 2; BETWEEN FR66-68, +Y762,Z240. REPLACED FLOORBEAM IAW SRM.May 21, 2004 · N102UW · Airbus A320214 · Fuselage Main, Floor BeamSDR USAA040246Web · crackedPIT, Q5, WEB .5000 INCH CRACK, 2ND LIGHTENING HOLE FROM FWD EDGE OF DOOR 12 INCHES UP FROM LOWER EDGE OF DOOR. CUT OUT DAMAGE AND INSTALLED REPAIR PLATE IAW SRM.May 21, 2004 · N433US · Boeing 7374B7 · Emergency ExitsSDR USAA040234Shear Web · corrodedSHEAR WEB, 8 INCHES X 3 INCHES X .040 INCH DEEP. CORROSION THRU WEB FR 69-70, Y200, Z240. REMOVED AND REPLACED SHEAR WEB IAW SRM.May 20, 2004 · N701UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040235Floorbeam · corrodedFLOORBEAM, 1.0 INCH X 0.950 INCH X 0.055 INCH DEEP, CORROSION; LEVEL 2; TASK NR JA260535, FR 66-68, Y1200, Z240. REPLACED WITH NEW FRAME IAW SRM.May 20, 2004 · N701UW · Airbus A319112 · Fuselage Main, Floor BeamSDR 304AW0007Skin · lightning strikeSEVERAL LIGHTENING STRIKES IN THE CROWN OF THE FUSELAGE SKIN NEAR STATION 259 BETWEEN STR 2 AND 3 LEFT. REPAIRED IAW SRM 53-00-01 AND EA NR 53-171.May 19, 2004 · N304AW · Boeing 7373G7 · Fuselage Main, Plate/SkinSDR TSAA0436040Bleed Valve · failedNR 1 ENGINE BLEED VALVE DOES NOT CLOSE. RETURN TO HNL, NO EMERGENCY DECLARED; REQUESTED PRECAUTIONARY FOR OVERWEIGHT LANDING AND POSSIBLE HOT BRAKES. OVERWEIGHT LANDING (147,000 LBS) WITH MINIMUM SINK RATE. WITH ENGINE NR 1 AT IDLE, VERIFIED NR 1 ENGINE BLEMay 18, 2004 · N740AL · Boeing 73776N · Compressor Bleed ValveSDR 2004UALA00481Shear Web · crackedSTA 194 SHEAR WEB AT STR 17 LT IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR WEB.May 18, 2004 · N906UA · Boeing 737522 · Fuselage Main, StructureSDR 2004UALA00482Shear Web · crackedSTA 194 SHEAR WEB AT STR 17 RT IS CRACKED. MAJOR REPAIR ACCOMPLISHED. REPLACED SHEAR WEB.May 18, 2004 · N906UA · Boeing 737522 · Fuselage Main, StructureSDR IXXA0400080SSkin · damagedDURING A ROUTINE A-CHECK INSPECTION, FOUND AFT SERVICE DOOR HAS INTERIM REPAIR ON UPPER AFT CORNER, STA 1660.000 L-11R TD L-98. REPAIRS WERE ACCOMPLISHED BY PERFORMING MAJOR REPAIR IAW SRM 53-2-0, FIG 76, TR NR 53-197 MAR 26/04 REMOVED INTERIM REPAIR IAW SRM 5May 18, 2004 · N830BX · Doug DC871F · Service DoorsSDR USAA040236Frame · corrodedFRAME, 1.100 INCH X 1.00 INCH X 0.62 INCH, CORROSION. REPLACED NEW FRAME IAW SRM.May 18, 2004 · N701UW · Airbus A319112 · Fuselage Main, FrameSDR 374PA0008Angle · corrodedCORROSION ON LT TRANSITION ANGLE IN AFT CARGO BIN FROM BS 727E TO AFT END. FABRICATED AND INSTALLED REPLACEMENT TRANSITION ANGLE IAW SRM 53-60-53.May 17, 2004 · N374PA · Boeing 73736M · Fuselage Miscellaneous StructureSDR USA2004F00050Flap · malfunctionedON APPROACH, CREW RECEIVED A LEADING EDGE FLAPS TRANSIT LIGHT ASSOCIATED WITH A YELLOW TRANSIT LIGHT ON THE NR 3 LEADING EDGE SLAT. CAPTAIN REPORTED THE FLAPS WOULD NOT EXTEND PAST 15 UNITS. FLIGHT LANDED WITHOUT FURTHER INCIDENT AND TAXIED TO THE GATE. AN May 17, 2004 · N385US · Boeing 7373B7 · Leading Edge Slat Control SystemSDR USAA040231Stiffener · corrodedSTIFFENER (1 INCH X 1 INCH AREA) CORROSION; NO LEVEL/TASK NO LEVEL/TASK STA 1016 AT BL 0. CLEANED CORROSION AND TREATED AND PRIMED IAW SRM 53-00-01 FIG 101.May 16, 2004 · N352US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA040230Lap Joint · corroded.2500 INCH DIA. AREA OF CORROSION ON LAP JOINT AT STA 1016 BL 0. REMOVED RIVET AND CLEANED CORROSION AROUND RIVET HOLE AND REINSTALLED RIVET IAW SRM, FIG 1.May 16, 2004 · N352US · Boeing 737301 · Fuselage Main, StructureSDR USA2004F00039Charger · failedMAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEAT ROWS 24 AND 25 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSY IN THE AFT GALLEY CEILING. OPERATIONAL CHECK GOOD.May 16, 2004 · N784UA · Boeing 777222 · Emergency LightingSDR USA2004F00040Battery Pack · dischargedMAINTENANCE REPORTED THE EMERGENCY LIGHTS AT SEAT ROW 21DEF INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK ABOVE SEAT ROW 21DEF. OPS CHECK GOOD.May 16, 2004 · N784AU · Boeing 7374B7 · Emergency LightingSDR 2004UALA00478Landing Gear · malfunctionedRETURNED TO DEN, DUE TO GEAR WOULD NOT RETRACT. TARGET FOR SWITCH S106 OF GROUND TO AIR SAFETY SENSOR IS OUT OF LIMIT. ADJUSTED SWITCH AND PERFORMED GEAR SWING. NO HISTORY BEFORE OR AFTER.May 15, 2004 · N367UA · Boeing 737322 · Main Landing GearSDR USA2004F00035Apu · shutdownENROUTE, WITH THE NR 2 ENGINE INTEGRATED DRIVE GEN (IDG) ON MINIMUM EQUIPMENT LIST (MEL), THE AUXILARY POWER UNIT (APU) SHUT DOWN DURING FLIGHT. FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACE THE NR 2 ENGINE IDG AND REMOVED MMay 14, 2004 · N101UW · Airbus A320214 · APU Oil System
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