GE CFM56 series

Service difficulty reports · 5,028

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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 USAA040193Beam · corrodedBEAM, 2.0 INCHES L X 1.5 INCHES W X .055 INCH DEEP, CORROSION; LEVEL 2; TASK NR JA-260-53500, BEAM, FR 68, Y1292, Z240. REPLACED BEAM.May 7, 2004 · N703UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040194Frame · corrodedFRAME, 1.5 INCHES L X 2.0 INCHES W AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, Y1292, C68, Z240. REMOVED AND REPLACED FRAME IAW SRM.May 7, 2004 · N703UW · Airbus A319112 · Fuselage Main, FrameSDR UPS04842414Shear Tie · crackedINSPECTION TYPE: C1 STATION 1766 AFT SIDE LONG 17R SHEAR TIE IS CRACKED. REMOVED, FABRICATED AND REPLACED SHEAR TIE IAW DWG 5773844 AND SRM. 51-3-0.May 6, 2004 · N730UP · Doug DC871F · Fuselage Main, StructureSDR UPS04842415Shear Tie · crackedINSPECTION TYPE: C1 AFT SIDE STATION 1766 J-FRAME TO LONGERON LONG 19R SHEAR TIE IS CRACKED. REMOVED, FABRICATED AND REPLACED SHEAR TIE IAW DWG 5773844 AND SRM 51-3-0.May 6, 2004 · N730UP · Doug DC871F · Fuselage Main, StructureSDR 2004UALA00446Structure · corrodedCORROSION AND MATERIAL LOSS ON STA 986.5 RBL 28 TO RBL 33. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED FILLER AND DOUBLER ANGLE REPAIR.May 6, 2004 · N399UA · Boeing 737322 · Fuselage Main, StructureSDR UPS04842445Doubler · gougedINSPECTION TYPE:C-2 LW OB FLAP UPPER SURFACE DOUBLER GOUGED AT I/B ICE BREAKER GUIDE TRACK STA XF219. REMOVED DAMAGED DOUBLER FAB NEW DOUBLER ALODINED AND PRIMED INSTALLED NEW DOUBLER.May 6, 2004 · N818UP · Doug DC873F · Trailing Edge FlapsSDR USAA040184Plate · corrodedPLATE, 2.00 INCH LONG X .05 INCH AREA, EXFOLIATED CORROSION; LEVEL 2; TACK NR JA-260-53500 R2 DOOR, AFT GIRT BAR PLATE ASSY, FR 68-Y1292. INSTALLED NEW PLATE IAW SRM.May 6, 2004 · N703UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040225Beam · corrodedBEAM, 1.0 INCH X 1.5 INCH X .040 INCH DEEP AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, FR-Y765, BETWEEN CROSSBEAM C66, C67, Z240. REMOVED AND REPLACED BEAM IAW SRM.May 6, 2004 · N702UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040226Beam · corrodedBEAM, 1.0 INCH X 1.50 INCH X .090 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, FRAME Y765 AND CROSSBEAM C66, Z240. REMOVED AND REPLACED BEAM IAW SRM.May 6, 2004 · N702UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040227Beam · corrodedBEAM, 1.0 INCH X 2.0 INCH X .025 INCH DEEP AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, FRAME Y765, CROSSBEAM C68 AND C70, Z240. REMOVED AND REPLACED BEAM IAW SRM.May 6, 2004 · N702UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040228Web · corrodedWEB, 7 INCH X 3 INCH X .010 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, WEB BETWEEN FRAME 69, 70, Y1292. REPLACED PART IAW SRM.May 6, 2004 · N702UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040229Web · corrodedWEB, 1.5 INCH X 1.5 INCH X .015 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500. WEB BETWEEN FR69, 70, Y1292, Z240.May 6, 2004 · N702UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USAA040205Spar Cap · crackedSPAR CAP CRACKED (.2187 INCH CRACK) WBL 157 LT WING UPPER SKIN AT AFT SPAR.May 6, 2004 · N433US · Boeing 7374B7 · Wing SparSDR 2004UALA00443Coffeemaker · malfunctionedRETURNED TO YYZ DUE TO F-A REPORTED SPARKS AND POPPING COMING FROM FWD GALLEY CEILING ABOVE COFFEE MAKER. MECHANIC INSPECTING AIRCRAFT FOUND NO SIGNS OF ARCING OR MOISTURE ABOVE COFFEEMAKER. SUBJECT COFFEEMAKER FOUND TO FUNCTION PROPERLY. FURTHER ANALYSIS BYMay 5, 2004 · N944UA · Boeing 737522 · Buffet/GalleysSDR USAA040183Panel · crackedPANEL, 5 INCHES LONG, CRACKED, FR64, Y1732, Z240. FABRICATED NEW PANEL IAW SRM 53-02-00, FIG 209.May 5, 2004 · N703UW · Airbus A319112 · Fuselage Miscellaneous StructureSDR USA2004F00033Girt Bar · detachedTHE MAIN ENTRY DOOR SLIDE GIRT BAR WAS FOUND DETACHED. MAINTENANCE ATTACHED GIRT BAR. OK FOR SERVICE.May 5, 2004 · N764US · Airbus A319112 · Escape SlideSDR USA2004F00046Controller · malfunctionedENROUTE, CREW REPORTED VIA ACARS THEY ENCOUNTERED A SLOW LOSS OF CABIN PRESSURIZATION. PRESSURE LOSS WAS NOT EXPLOSIVE BUT CREW COULD NOT CONTROL PRESSURIZATION. FLIGHT DESCENDED TO 10,000 FEET AND CONTINUED. NO OXYGEN MASKS WERE DEPLOYED. FLIGHT LANDED WIMay 5, 2004 · N518AU · Boeing 7373B7 · Cabin Pressure ControllerSDR USA2004F00051Outflow Valve · failedENROUTE, CREW REPORTED CABIN ALTITUDE WARNING HORN SOUNDED AS THEY ENCOUNTERED A SLOW LOSS OF CABIN PRESSURIZATION. PRESSURE LOSS WAS NOT EXPLOSIVE BUT CREW COULD NOT CNTRL PRESS. FLIGHT DESCENDED TO 10,000 FT AND CONTINUED. NO OXYGEN MASKS WERE DEPLOYED. May 5, 2004 · N518AU · Boeing 7373B7 · Pressure Regulator/Outflow ValveSDR USAA040204Floor Support · corrodedPIT, Q5, FLOOR SUPPORT, 1 INCH DIA CORROSION; LEVEL 1 TASK NR C53-208-01, BS 727F PLUS 7 LBBL 12.50. REMOVED DAMAGED SECTION AND INSTALLED NESTED IAW TYPE REP 53-10-06B.May 5, 2004 · N433US · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR 2004UALA00436B-Nut · leakingCAPTAIN DECLARED AMBER ALERT, LOOSING A SYSTEM HYDRAULICS, UPON INSPECTION AT MSP, THE B-NUT ON THE SYSTEM A-EMDP ACOUSTIC FILTER WAS FOUND LOOSE AND LEAKING. THE B-NUT WAS TIGHTENED AND AN EXTERNAL HYDRAULIC LEAK CHECK WAS PERFORMED TO ENSURE THE LEAK WAS COMay 4, 2004 · N376UA · Boeing 737322 · Hydraulic System, MainSDR 2004UALA00440Lamp · inoperativeEMERGENCY EXIT LIGHT (EEL) INOP FROM SEAT 15 AFT. REPLACED LAST TWO SEGMENTS OF EEL LIGHTS. CLEANED WATER FROM EEL LIGHTS LAST THREE ROWS.May 4, 2004 · N331UA · Boeing 737322 · Emergency LightingSDR 2004UALA00441Skin · dentedFOUND DENT ON RIGHT STABILIZER LEADING EDGE. DENT IS LOCATED ELEVEN BAYS O/B OF STA 86.66 IN CENTER OF BAY. DIMENSIONS ARE 1.00 VERT LENGTH X 0.41 HORIZONTAL WIDTH X 0.047 DEEP. MAJOR REPAIR ACCOMPLISHED. INSTALLED INTERNAL DOUBLER AND FLUSH FILLER.May 4, 2004 · N399UA · Boeing 737322 · Horizontal Stabilizer StructureSDR UPS04842422Rib · crackedINSPECTION TYPE: C1 LT WING LE UPPER RIB IS CRACKED AT XFS 641. NDT VERIFIED CRACK TERMINATES AT FASTENER HOLE, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-2-0 FIG 2May 4, 2004 · N730UP · Doug DC871F · Wing, Rib/BulkheadSDR UPS04842443Skin · corrodedINSPECTION TYPE: C-2 FUSELAGE SKIN CORRODED ALONG LONGERON 21R AT FS 8 AND FS55 EO DC8-5330-19540-A INSTALLED TEMP REPAIR, INSTALL PERMANENT REPAIR AT NEXT C- CHECK. GEN AND RECEIVED RFTS N818UP-1-20760. REMOVED FASTENERS STA-9 TO STA-70 L2OR -L24 RMVD TEMPMay 4, 2004 · N818UP · Doug DC873F · Fuselage Main, Plate/SkinSDR USAA040201Intercostal · corrodedBULKHEAD, INTERCOSTAL (5 INCH WIDE X 7 INCHES TALL) CORROSION; NO LEVEL OR TASK NR STA 1016 AFT PRESS BULKHEAD AT LOWER AREA, BL 0 . REPAIRED IAW EO5302V112A, DOUBLER INSTALLATION.May 4, 2004 · N375US · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA040200Stringer · crackedSTRINGER (.2500 INCH X .1250 INCH CRACKS) CRACKED STA 908 AND STR 4R. REPLACED STRINGER SPLICE IAW SRM 51-20-02.May 3, 2004 · N585US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR IXXA0400072SVane · elongatedROUTINE C-CHECK INSP FOUND RT IB VANE SLOT ELONGATED HOLES AT STA XS. 250.089. REPAIR WAS ACCOMPLISHED. REMOVED ALL FASTENERS WITHIN REPAIR AREAS IAW SRM 51-1-21 PG 1, SRM 51-1-20D PG 21. REMOVED DAMAGED AREA IAW DWG V82-R07. PERFORMED NDT INSP IAW NDT SPM PARMay 3, 2004 · N830BX · Doug DC871F · Trailing Edge FlapsSDR IXXA0400074SSkin · damagedDURING A ROUTINE C-CHECK INSPECTION, FOUND RT HORIZONTAL STAB LE HAS AN INTERIM REPAIR. STA XFS. 109.750. REPAIR WAS ACCOMPLISHED. REMOVED INTERIM REPAIR IAW SRM 51-1-21 PG1. FABRICATED DOUBLER. CLEANED, TREATED AND PRIMED AREA AND DOUBLER INTERNAL PART IAW SMay 3, 2004 · N830BX · Doug DC871F · Horizontal Stabilizer, Plate/SkinSDR USAA040232Frame · crackedFRAME CRCKED, 1 INCH LONG CRACK, STA 616 JUST BELOW STRINGER 17L. FABRICATED FILLER IAW T/R 53-62-01, 53-60-01 AND J NR 58-53503-004.May 3, 2004 · N585US · Boeing 737301 · Fuselage Main, FrameSDR 2004UALA00435O-Ring · leakingAIRCRAFT DIVERTED TO AMA DUE TO HIGH OIL CONSUMPTION IN NR 1 ENGINE. FOUND STARTER SHAFT O-RING MISSING. STARTER WAS REPLACED PREVIOUS DAY. REPLACED STARTER SHAFT O-RING AND SERVICED ENGINE OIL .May 2, 2004 · N390UA · Boeing 737322 · Turbine Engine Oil SystemSDR IXXA0400067SSkin · crackedDURING A ROUTINE C-CHECK INSPECTION, FOUND LT WING OB LE LOWER SKIN CRACKED .5000 INCH. REPAIR ACCOMPLISHED. REMOVED FASTENERS WITHIN REPAIR AREA IAW SRM 51-1-21 AND 51-1-20D PG1. REMOVED DAMAGED AREA IAW DWG V82-R01. PERFORMED NDT INSPECTION IAW NDT SPM PMay 1, 2004 · N830BX · Doug DC871F · Wing, Plate/SkinSDR IXXA0400068SSkin · corrodedDURING A ROUTINE C-CHECK INSPECTION, FOUND LT OB WING LE OB SECTION CORRODED AT STA XFS 710.000. THIS REPAIR WAS ACCOMPLISHED IAW DWG V82-R02 AND N/R 0652. REMOVED FASTENERS IAW SRM 51-1-21 PG1. REMOVED CORROSION IAW SRM 51-1-8 PGS. 17-18. FOUND OUT OF LIMITS.May 1, 2004 · N830BX · Doug DC871F · Wing, Plate/SkinSDR IXXA0400069SSkin · damagedDURING A ROUTINE C-CHECK INSPECTION, FOUND LT WING CENTER LE HAS REPAIR ON UPPER SURFACE, STATION XFS 304.000. THIS REPAIR WAS ACCOMPLISHED IAW SRM 57-2-1 FIG 38 TR NR 57-85, 51-1-21, 51-1-20D. REMOVED DOUBLER AND FABRICATED FILLER AND DOUBLER. CLEANED TREATEMay 1, 2004 · N830BX · Doug DC871F · Wing, Plate/SkinSDR IXXA0400070SPanel · corrodedDURING A ROUTINE C-CHECK INSPECTION, FOUND LT WIND IB LE SLANT PANEL UPPER CAP CORRODED AT SEVERAL AREAS. STA XW.0 - XFS 164.000. REPAIR WAS ACCOMPLISHED. PERFORMED MAJOR REPAIR IAW SRM 57-1-0 PG 1. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITMay 1, 2004 · N830BX · Doug DC871F · Wing, Plate/SkinSDR IXXA0400071SSkin Panel · corrodedDURING A ROUTINE C-CHECK INSPECTION, FOUND LT WING CTR LE UPPER SURFACE CORRODED AT STA XFS 341.500. REPAIR WAS ACCOMPLISHED, REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 51-1-8 PG 17-18 AND 57-2-1 PG 11. TOOK OUT DAMAGED SECTION IAW SRM 57-2-1 FIG. 38, May 1, 2004 · N830BX · Doug DC871F · Wing, Plate/SkinSDR 2004UALA00416Hydraulic System · malfunctionedFLIGHT RETURNED TO THE FIELD WITH A LOSS OF THE A SYSTEM HYDRAULIC PRESSURE. REPLACED THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP.Apr 29, 2004 · N924UA · Boeing 737522 · Hydraulic System, MainSDR USAA040174Sill · corrodedSILL, 4.25 INCHES X 2.5 INCHES X .042 INCH DEEP AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500, FR 66, Z240, Y1972. REMOVED AND REPLACED SILL IAW SRM 51-74-00, 53-41-14, 51-42-11.Apr 29, 2004 · N101UW · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA040175Floor Support · corrodedFLOOR SUPPORT, 1.9 INCHES X .6 INCH X .040 INCH DEEP AREA, CORROSION; LEVEL 2, TASK NR JA-220-53500, FR 22, Y254, Z240. INSTALLED REPAIR ANGLE AND FILLER, REMOVED DAMAGE IAW SRM 51-74-00, 51-21-11, 51-75-12.Apr 29, 2004 · N101UW · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA040176Floor Support · corrodedFLOOR SUPPORT, .8 INCH X .6 INCH X .030 INCH DEEP, CORROSION; LEVEL 2; TASK NR JA-220-53500, FR 16, Y254, Z240. INSTALLED REPAIR ANGLE AND FILLER IAW SRM 51-74-00, 53-11-14, 51-21-11, 51-75-12.Apr 29, 2004 · N101UW · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA040177Web · corrodedWEB, 3 INCHES L X 2INCHES W X .020 INCHES D, CORROSION, LEVEL 2; TASK NR JA-260-53500 BETWEEN FR 69-70 + Y1244.6, Z240. REMOVED AND REPLACED WEB IAW SRM 51-74-00, 53-00-14, 51-42-11.Apr 29, 2004 · N101UW · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA040178Seat Track · corrodedSEAT TRACK, 1.5 INCH X 1.3 INCH X .032 INCH DEEP. CORROSION; LEVEL 2; TASK NR JA-220-53500, FR 16, Y765, Z240. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-11-14, 51-42-11.Apr 29, 2004 · N101UW · Airbus A320214 · Fuselage, Seat/Cargo Attach FittingsSDR IXXA0400066SSkin · dentedDURING A ROUTINE C-CHECK INSPECTION, FOUND DENTS ON RT WING STATION 660. REPAIR WAS ACCOMPLISHED. REMOVED FASTENERS IAW SRM 51-1-21 PG. 1 ALSO REMOVED DAMAGED AREA AND FABRICATED REPAIR DOUBLER 57-2-1 FIG 24 PG 15. CLEANED, TREATED AND PRIMED AREA IAW SRM 51Apr 29, 2004 · N830BX · Doug DC871F · Wing, Plate/SkinSDR 2004UALA00409Light · damagedEMERGENCY EXIT LIGHTING STRIP DAMAGED ON LT SIDE OF AFT GALLEY. REPLACED LIGHT ASSY AND SECTION OF PLASTIC COVER.Apr 28, 2004 · N350UA · Boeing 737322 · Emergency LightingSDR 2004UALA00413Light · inoperativeFLOOR PROX EMERGENCY EXIT LIGHTING INOPERATIVE FROM ROW 14 AFT. REPLACED LIGHT CABLE AND AFT GALLEY FLOOR LIGHT.Apr 28, 2004 · N939UA · Boeing 737522 · Emergency LightingSDR USAA040164Floor Support · corrodedFLOOR SUPPORT, 1.8 INCH X .70 INCH X .037 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-220-53500 LONGERON-FR 20, Y-254. INSTALLED FILLER AND REPAIR ANGLE IAW SRM 53-00-14, FIG 204.Apr 28, 2004 · N101UW · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA040165Floor Support · corrodedFLOOR SUPPORT, 1.3 INCHES X .90 INCH X .021 INCH AREA, CORROSION; LEVEL 2; TASK NR JA-220-53500 LONGERON - FR 16, Y-254. INSTALLED FILLER AND REPAIR ANGLES IAW SRM 53-11-14, FIG 201.Apr 28, 2004 · N101UW · Airbus A320214 · Fuselage Miscellaneous StructureSDR USAA040170Floor Panel · delaminatedFLOOR PANEL, 4.5 INCH X 5.5 INCH OB AFT CORNER, DELAMINATION FR 66, Y1182, FLOOR PANEL 261 HG. NEW PANEL FABRICATED IAW SRM 53-02-00, FIG 309.Apr 28, 2004 · N101UW · Airbus A320214 · Fuselage Floor PanelSDR USAA040171Floor Panel · delaminatedFLOOR PANEL 4 INCH X 4 INCH AREA, DELAMINATION, 31.25 CM FWD OF FR 68, Y 756.25. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.Apr 28, 2004 · N101UW · Airbus A320214 · Fuselage Floor PanelSDR USAA040172Floor Panel · delaminatedFLOOR PANEL, 6 INCHES X .2500 INCH W, DELAMINATION, FLOOR PANEL NR 241 AF, FR 34 AND 35 AT Y24, Z240. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.Apr 28, 2004 · N101UW · Airbus A320214 · Fuselage Floor PanelSDR USAA040166Track · corrodedTRACK, 3.5 INCHES X 3.5 INCHES X .170 INCHES DEEP AREA, CORROSION; LEVEL 2; TASK NR JA-260-53500 BETWEEN FR 64 TO 70, Y736.6, Z240. REMOVED AND REPLACED SEAT TRACK IAW SRM 53-00-14, 51-42-11, 51-71-12.Apr 27, 2004 · N101UW · Airbus A320214 · Fuselage Miscellaneous Structure
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