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 USA2004F00038Power Supply · faultyPILOT REPORTED THE EMERGENCY EXIT LIGHTS FLASH ON AND OFF INDEPENDENT OF SWITCH POSITION. MAINTENANCE REMOVED AND REPLACED THE M1136 POWER SUPPLY AND BATTERY PACK IAW MM. OPERATIONAL CHECK GOOD.May 14, 2004 · N506AU · Boeing 7373B7 · Emergency LightingSDR USA2004F00042Power Supply · faultyTHE AFT EMERGENCY POWER SUPPLY UNIT TESTED BAD. MAINTENANCE REPLACED THE AFT CABIN EMERGENCY POWER SUPPLY UNIT. OPS CHECKED OK.May 14, 2004 · N707UW · Airbus A319112 · Emergency LightingSDR USA2004F00043Power Supply · faultyTHE LT SIDE EMERGENCY POWER SUPPLY UNIT TESTED BAD. MAINTENANCE REPLACED THE MID CABIN LT SIDE EMERGENCY POWER SUPPLY UNIT. OPS CHECKED, OK.May 14, 2004 · N707UW · Airbus A319112 · Emergency LightingSDR USA2004F00044Battery · dischargedTHE RT SIDE EMERGENCY POWER SUPPLY UNIT TESTED BAD. MAINTENANCE REPLACED THE MID CABIN RT SIDE EMERGENCY POWER SUPPLY UNIT BATTERY. OPS CHECKED OK.May 14, 2004 · N707UW · Airbus A319112 · Emergency LightingSDR UPS04842444Skin · dentedINSPECTION TYPE:C-2 JUST BELOW LOWER CUTOUT OF MAIN CARGO DOOR, FUSELAGE SKIN HAS TWO DENTS. REMOVED FASTENER IN SKIN FS 200-220, RMVD DAMAGE SECTION OF SKIN AT FS 210 MATERIAL ID FOR DOUBLER REPAIR EXTERNAL DOUBLER 7075-T6.080 PO 43557 21 FILLER 2024-T-3,071May 13, 2004 · N818UP · Doug DC873F · Fuselage Main, Plate/SkinSDR USAA040214Sill · corrodedSILL, 1.0 INCH X 1.0 INCH X .07 INCH AREA. CORROSION; LEVEL 2; TASK NR JA-260-53500, Z240, BTW FR 66 AND FR 68 BL-Y 1732. REMOVED AND REPLACED SILL IAW SRM.May 13, 2004 · N702UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040215Sill · crackedSILL, 1.0 INCH X 1.0 INCH X .08 INCH AREA, CORROSION; LEVEL 2 TASK NR JA-260-53500, Z240 BET FR 66,FR68J BL Y1732. REMOVED AND REPLACED SILL IAW SRM.May 13, 2004 · N702UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USA2004F00036Charger · failedMAINTENANCE REPORTED THE AFT SIX ROWS OF THE AISLE SEAT MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT BATTERY CHARGER ASSY. ALSO, REPLACED THE BATTERY PACK. OPS CHECK GOOD.May 13, 2004 · N300AU · Boeing 737301 · Emergency LightingSDR USA2004F00048Circuit Card · malfunctionedAFTER TAKEOFF, THE NOSE LANDING GEAR RED UNSAFE LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE CHECKED OPERATION OF NOSE LANDING GEAR DOWN LOCK SENSOR ANMay 13, 2004 · N591US · Boeing 737301 · Landing Gear Position and WarningSDR USAA040203Skin Panel · crackedPIT, Q5, INNER SKIN PANEL, .2500 INCH CRACKS, LIGHTENING HOLE NR 22. ROUTED OUT DAMAGE AND INSTALLED DOUBLER AND TRIPLER IAW EA 78419.May 13, 2004 · N433US · Boeing 7374B7 · Cargo/Baggage DoorsSDR UPS04842411Fitting · crackedINSPECTION TYPE:C1 LT WING FLAP LINK SUPPORT ASSY IS CRACKED AT FLAP HINGE 3. REMOVED AND REPLACED FITTING IAW DWG 5642342 AND SRM. 51-1-20D, 51-3-0.May 12, 2004 · N730UP · Doug DC871F · Wing, Control Surface Attach FittingsSDR 2004UALA00471Frame · corrodedSTA 380 FRAME HAS CORROSION FROM STR 28L TO 28R. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED REPAIR DOUBLER.May 12, 2004 · N906UA · Boeing 737522 · Fuselage Main, FrameSDR USAA040212Support · corrodedGIRT BAR FITTING SUPPORT, 1.5 INCHES X 1.0 INCH X .010 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, FR 68 BL-Y 1732. REMOVED AND REPLACED SUPPORT IAW SRM.May 12, 2004 · N702UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040213Support · corrodedGIRT BAR FITTING SUPPORT, 1.0 INCH X 1.0 INCH X .010 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, FR 66 BL, Y 1732, Z240. REMOVED AND REPLACED SUPPORT IAW SRM.May 12, 2004 · N702UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040216Floor Panel · crackedFLOOR PANEL, 1.2 INCH CRACK, MAIN CABIN FLOOR PANEL 261 HG. FABRICATED FLOOR PANEL IAW SRM.May 12, 2004 · N702UW · Airbus A319112 · Fuselage Floor PanelSDR USAA040217Floor Panel · crackedFLOOR PANEL, .9 INCH CRACK, MAIN CABIN, FLOOR PANEL 242 MF. FABRICATED FLOOR PANEL IAW SRM.May 12, 2004 · N702UW · Airbus A319112 · Fuselage Floor PanelSDR USAA040218Beam · corrodedBEAM, 1.0 INCH X 1.0 INCH X .020 INCH AREA. CORROSION; LEVEL 2; TASK NR JA-260-53500 FR 68, Y 1292, Z240. REMOVED AND REPLACED BEAM IAW SRM.May 12, 2004 · N702UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040219Beam · corrodedBEAM 1.0 INCH X 2.0 INCH X .020 INCH, CORROSION; LEVEL 2; TASK NR JA-160-53500. REMOVED AND REPLACED BEAM IAW SRM.May 12, 2004 · N702UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040220Beam · corrodedBEAM, 3.0 INCH X 3.0 INCH X .025 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, FR 68, BI-Y1292, Z240. DEFECTIVE PART REPLACED WITH IDENT PART NR IAW SRM.May 12, 2004 · N702UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040221Beam · corrodedBEAM, 1.5 INCH X 1.5 INCH X .030 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, FR 67, BL-Y1292, Z240. REMOVED AND REPLACED BEAM IAW SRM 53-00-14, FIG 102.May 12, 2004 · N702UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040222Beam · corrodedBEAM, 3.0 INCH X 1.0 INCH X 0.25 INCH CORROSION; LEVEL 2; TASK NR JA-260-53500, FR66, BL-Y1292, Z240. REMOVED AND REPLACED BEAM IAW SRM 53-00-14, FIG 102.May 12, 2004 · N702UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040223Beam · corrodedBEAM, 1.0 INCH X 1.0 INCH X 0.025 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500; Z240, FR66 BLY1292. REMOVED AND REPLACED IAW 53-00-14, FIG 102.May 12, 2004 · N702UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR UPS04842413Strap · brokenINSPECTION TYPE:C1 STATION 440 AT LBL 12 HAS STRAP BROKEN ON FLOOR WEB. REMOVED, FABRICATED AND REPLACED STRAP IAW DWG 5633853 AND SRM. 51-1-21.May 11, 2004 · N730UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS04842441Splice Plate · corrodedINSPECTION TYPE:C1 STATION 210 FINGER DOUBLER AND SPLICE PLATE ARE CORRODED BEYOND LIMITS BETWEEN LONG 21L TO 31L AND STATION 210 LONG 25R SPLICE FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER, SPLICE PLATE AND SPLICE FITTING IAW DWG 5779May 11, 2004 · N730UP · Doug DC871F · Fuselage Main, Plate/SkinSDR USA2004F00047Odor · detectedCREW ADVISED OF A BURNING RUBBER ODOR IN THE AFT GALLEY. THE MAIN GALLEY POWER SWITCH WAS SECURED AND THE ODOR DISSIPATED. MAINTENANCE INSPECTED THE AREA AND OPERATED THE GALLEY EQUIPEMENT. NOT PROBLEM WAS FOUND.May 11, 2004 · N446US · Boeing 7374B7 · Buffet/GalleysSDR USAA040198Beam · corrodedBEAM, 2.5 INCH X 1.5 INCH X .031 INCH AREA, CORROSION, LEVEL 2; TASK NR JA-260-53500 FLOOR SUPPORT, FRAME 66, Y1292, Z240. REMOVED AND REPLACED BEAM IAW SRM.May 10, 2004 · N703UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR UPS04842407Fitting · crackedINSPECTION TYPE:C1 NR 1 ALT. TANK AT XRS 440 APPROX. STRINGER 59 FITTINGS ARE CRACKED. REMOVED AND REPLACED FITTINGS IAW DWG.5644972, 3645612 AND SRM. 51-1-20D.May 8, 2004 · N730UP · Doug DC871F · Wing Miscellaneous StructureSDR UPS04842408Fitting · corrodedINSPECTION TYPE:C1 STATION 300 BATHTUB FITTING IS CORRODED BEYOND LIMITS BETWEEN LONG. 33R-34R. REMOVED AND REPLACED FITTING IAW DWG. 3755824 AND SRM. 53-2-0 FIG. 2D.May 8, 2004 · N730UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS04842412Longeron · crackedINSPECTION TYPE: C1 STATION 1730 LONGERON 14R IS CRACKED. REMOVED, FABRICATED AND REPLACED LONGERON SECTION BETWEEN STATION 1720 TO 1740 AND INSTALLED SPLICES AND STRAPS IAW SRM. 53-2-2 FIG. 10.May 8, 2004 · N730UP · Doug DC871F · Fuselage Main, Longeron/StringerSDR UPS04842416Fitting · corrodedINSPECTION TYPE: C1 BATHTUB FITTING IS CORRODED BEYOND LIMITS AT STATION 300 BETWEEN LONG 34L-35L. REMOVED AND REPLACED FITTING IAW DWG 3755822 AND SRM 53-2-0 FIG. 2D.May 8, 2004 · N730UP · Doug DC871F · Fuselage Miscellaneous StructureSDR 2004UALA00448Skin · damagedHFEC INSPECTION FOUND INDICATIONS OF DEFECTS PER NDT 51-00-01 AT SEVERAL LOCATIONS. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND EXTERNAL FUSELAGE SKIN DOUBLER.May 8, 2004 · N395UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR USAA040195Sill · corrodedSILL, 1 INCH X .75 INCH X .052 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, L-2 DOOR SILL PLATE FRAME 66-68, Z240. REMOVED AND REPLACED SILL IAW SRM.May 8, 2004 · N703UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040196Beam · corrodedBEAM, 2.5 INCH X 1.5 INCH X .028 INCH, CORROSION; LEVEL 2, TASK NR JA-260-53500, BL Y1292, FR 66, Z240. DEFECTIVE PART REPLACED WITH IDENT PN IAW EA 95469 AND SRM.May 8, 2004 · N703UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040197Plate · corrodedDOOR SEAL PLATE, 1 INCH X .8 INCH X .50 INCH DEEP, CORROSION; LEVEL 2; TASK NR JA-260-53500, BEAM C66, Y1732, Z240. REMOVED AND REPLACED SCUFF PLATE.May 8, 2004 · N703UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USA2004F00034Odor · detectedENROUTE, DURING DESCENT, THE CABIN CREW REPORTED A PUNGENT ODOR IN THE CABIN. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE CABIN, CARGO, AND AVIONICS COMPARTMENTS. NO ABNORMALITIES FOUND. OK FOR SERVICE.May 8, 2004 · N710UW · Airbus A319112 · Air Distribution SystemSDR USA2004F00037Battery Pack · dischargedMAINTENANCE REPORTED THE FORWARD EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BOTH FORWARD BATTERY PACKS. OPERATIONAL CHECK GOOD.May 8, 2004 · N300AU · Boeing 737301 · Emergency LightingSDR USA2004F00052Shutoff Valve · failedRT PACK TRIP OFF LIGHT ILLUMINATED, WOULD NOT RESET. LT PACK TRIP OFF LIGHT ILLUMINATED DURING TEMP ADJMT. IMMEDIATE DESCENT WAS INITIATED TO 10,000 FT BUT CABIN ALTITUDE CLIMBED ABOVE 14,000 FT DEPLOYING OXYGEN MASKS. LT PACK RESET, PRESS WAS REGAINED. FMay 8, 2004 · N376US · Boeing 7373B7 · Cabin Cooling SystemSDR UPS04842409Angle · crackedINSPECTION TYPE:C1 STATION 781 LOWER HORIZONTAL ANGLE AT LBL 60 APPROX IS CRACKED OVER WING BOX. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG.3643111 AND SRM. 51-1-20D.May 7, 2004 · N730UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS04842410Fitting · crackedINSPECTION TYPE:C1 NR 4 ALT TANK HAS STRINGER 59 FITTING CRACKED AT XRS 428 AND XRS 440 REMOVED, FABRICATED AND REPLACED FITTING IAW DWG. 5644973 AND SRM. 51-1-20D.May 7, 2004 · N730UP · Doug DC871F · Wing Miscellaneous StructureSDR UPS04842417Fitting · crackedINSPECTION TYPE:C1 STATION 1160 BATHTUB FITTING IS CRACKED BETWEEN LONG 34R-35R. REMOVED AND REPLACED FITTING IAW DWG 3755843 AND SRM 53-2-0 FIG 2D.May 7, 2004 · N730UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS04842418Fitting · crackedINSPECTION TYPE: C1 STATION 1152 OB OF LONG 35R BATHTUB FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755843 AND SRM 53-2-0 FIG 2D.May 7, 2004 · N730UP · Doug DC871F · Fuselage Miscellaneous StructureSDR 2004UALA00449Frame · crackedCABIN BELOW FLOOR LEVEL, BS 616R I/B FRAME CHORD CRACKED AT OVERWING EXIT. MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND ANGLE.May 7, 2004 · N906UA · Boeing 737522 · Fuselage Main, FrameSDR 2004UALA00450Splice · crackedSTRINGER SPLICE CRACKED AT STA 907 STR 4L. MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED STRINGER SPLICE.May 7, 2004 · N399UA · Boeing 737322 · Fuselage Miscellaneous StructureSDR 2004UALA00451Splice · crackedSTRINGER SPLICE CRACKED AT STA 907 STR 4R. MAJOR REPAIR ACCOMPLISHED. REMOVED AND REPLACED STRINGER SPLICE.May 7, 2004 · N399UA · Boeing 737322 · Fuselage Miscellaneous StructureSDR UPS04842423Fitting · crackedINSPECTION TYPE:C1 AFT TORQUE BOX UPPER FRAME IS CRACKED AT STATION 1220 LONGERON 34L TO 35L. REMOVED AND REPLACED FRAME GUIDE FITTING IAW DWG 9754055 AND SRM 51-3-0May 7, 2004 · N730UP · Doug DC871F · Fuselage Miscellaneous StructureSDR UPS04842424Frame · corrodedINSPECTION TYPE: C1 STATION 1120 FRAME CAP IS CORRODED BEYOND LIMITS AT LONG 36. REMOVED AND REPLACED FRAME CAP IAW DWG 5764343 AND REPAIRED FRAME IAW DWG DC8-53A-010, EO DC8-5310-11728-A, SRM 51-1-20D, 51-1-21May 7, 2004 · N730UP · Doug DC871F · Fuselage Main, FrameSDR UPS04842447Clip · corrodedINSPECTION TYPE:C-2 MAIN CABIN RT CUSP AT LWR FWD CORNER OF R2 DOOR (FS 1620) EXFOLIATION CORROSION. REMOVED CORROSION ON CLIP IAW DC8-SRM 51-1-8, OUT OF LIMITS. MAT ID AND FAB CUSP CLIP IAW DAC DWG 4773150 PERFORMED DYE PEN TEST. ALODINE AND PRIME CUSP CLIMay 7, 2004 · N818UP · Doug DC873F · Fuselage Miscellaneous StructureSDR USAA040185Beam · corrodedBEAM, 3 INCH X 1.5 INCHES X .032 INCH DEEP AREA, CORROSION; LEVEL 2; TASK JA-260-53500 BETWEEN FR 68, 69, Y1292, Z240. REMOVED AND REPLACED BEAM IAW SRM.May 7, 2004 · N703UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040186Seat Track · corrodedSEAT TRACK, 2 INCHES X 1.6 INCHES X .038 INCHES DEEP AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, FR68, Y1292, Z240. REMOVED AND REPLACED SEAT TRACK IAW SRM.May 7, 2004 · N703UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR USAA040192Track · corrodedTRACK, 2.5 INCHES X 1.5 INCHES X .090 INCHES DEEP AREA, CORROSION; LEVEL 2; TASK NR JA-220-53500, FR14, Y503.2, Z240. REMOVED AND REPLACED TRACK IAW SRM.May 7, 2004 · N703UW · Airbus A319112 · Fuselage, Seat/Cargo Attach Fittings
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