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 UPS04842888Longeron · crackedINSPECTION TYPE: C1, STATION 1770 LONG. 17L IS CRACKED REMOVED,FABRICATED AND REPLACED LONGERON IAW DWG. 5649327,AND SRM. 51-1-20D,51-1-21Jul 15, 2004 · N802UP · Doug DC873F · Fuselage Main, Longeron/StringerSDR 2004UALA00662Lamp · inoperativeEMERGENCY EXIT PATH LIGHTING IS INOP ON THE AFT SECTION. REPLACED DEFECTIVE RIBBON.Jul 14, 2004 · N936UA · Boeing 737522 · Emergency LightingSDR SCNA04011Slide · malfunctionedR-1 DOOR SLIDE DID NOT INFLATE AUTOMATICALLY DURING OPS CHECK SUN COUNTRY TASK CARD 25-220-00-02. ESCAPE SLIDE INFLATED MANUALLY AFTER PULLING THE MANUAL INFLATION HANDLE.Jul 13, 2004 · N804SY · Boeing 7378Q8 · Escape SlideSDR U30A200400008Odor · detectedAFTER PUSH BACK, THE AFT F/A'S REPORTED AN (ELECTRICAL) BURNING ODOR. THE FLIGHT CREW WAS NOTIFIED AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE AIRCRAFT IAW TSM 24-00-00-810-823 WITH NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.Jul 11, 2004 · N261AV · Airbus A320214 · Air Distribution SystemSDR DHL2004804518Fitting · crackedITEM REF. NR.2095: LT IB STUB WING ZEE PAN FITTING CRACK 4.000, STA XILD 43.188. REMOVED AND REPLACED CRACKED ZEE PAN FITTING, STA XILD 43.188 (LT IB STUB WING) IAW SRM 51-1-20D PG. 21, SRM 51-1-21 PG.1.Jul 10, 2004 · N804DH · Doug DC873F · Leading Edge DevicesSDR AWXA200400762Light · inoperativeDURING B2 CHECK THE EMERGENCY ESCAPE PATH LIGHTS AT SEAT ROWS 7 AND 11 LT WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT ASSEMBLIES AT SEAT ROWS 7 AND 11 LT, OPERATIONAL CHECK WAS GOOD.Jul 9, 2004 · N325AW · Boeing 737301 · Emergency LightingSDR AWXA200400755Flashlight · inoperativeEMERGENCY EQUIPMENT, DURING 4-DAY CHECK THE FORWARD FLIGHT ATTENDANT STATION EMERGENCY FLASHLIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD FLIGHT ATTENDANT STATION EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.Jul 8, 2004 · N309AW · Boeing 7373G7 · Emergency EquipmentSDR AWXA200400772Skin · crackedDURING 4-DAY CHECK A 3.5 INCH CRACK WAS FOUND IN LT FUSELAGE SKIN 4 INCHES ABOVE WING ROOT BETWEEN WINDOWS 11 AND 12, BETWEEN BS 500D+10 AND BS 520, STR 12 LT. MAINTENANCE CUTOUT DAMAGE IN LT FUSELAGE SKIN BETWEEN BS 500D+10 AND BS 520, STR 12 LT. PERFORMED AJul 8, 2004 · N175AW · Boeing 73733A · Fuselage Main, Plate/SkinSDR 2004UALA00645Window · crackedRETURNED TO DEN WITH CRACKED WINDSHIELD. CAUSE UNKNOWN. WINDOW REPLACED.Jul 7, 2004 · N908UA · Boeing 737522 · Flight Compartment WindowsSDR AWXA200400735Battery · dischargedEMERGENCY EQUIPMENT, FLIGHT CREW REPORTED THE AFT CABIN EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT CABIN EMERGENCY FLASHLIGHT BATTERIES, OPERATIONAL CHECK WAS GOOD.Jul 5, 2004 · N157AW · Boeing 7373G7 · Emergency EquipmentSDR AWXA200400800Stringer Clip · crackedDURING C-12 CHECK A .3750 INCH CRACK WAS FOUND IN AFT CARGO COMPARTMENT STRINGER TIE AT BS 927, STR 24 LT. MAINTENANCE REMOVED AND REPLACED CORRODED STRINGER TIE AT BS 927, STR 24 LT IAW B737-300 SRM 51-40-02.Jul 3, 2004 · N312AW · Boeing 7373S3 · Fuselage Main, Attach FittingsSDR 2004UALA00639Sensor · failedRETURNED TO DEN DUE TO OVERHEATED EXHAUST COOLING FAN. 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.Jul 3, 2004 · N311UA · Boeing 737322 · Cabin Cooling SystemSDR TSAA0436052Precooler · failedETOPS FLIGHT 352, CLIMBING THROUGH 15,000 FT THE BLEED TRIP OFF LIGHT FOR THE NR 2 ENGINE ILLUMINATED. PERFORMED QRH CHECKLIST, RETURNED. OVER-WEIGHT LANDING AT 131.2 K, LOW TO MEDIUM SINK RATE. VERIFIED NR 2 ENGINE BLEED TRIP ON THE GROUND. REMOVED AND REPLAJul 2, 2004 · N742AL · Boeing 73776N · Pneumatic Distribution SystemSDR TSAA0436053Precooler · failedCLIMBING THROUGH 15,000 FT THE BLEED TRIP OFF LIGHT FOR THE NR 2 ENGINE ILLUMINATED. PERFORMED QRH CHECKLIST, RETURNED TO KWA. OVER-WEIGHT LANDING AT 131.2 K, LOW TO MEDIUM SINK RATE. VERIFIED NR 2 ENGINE BLEED TRIP ON THE GROUND. REMOVED AND REPLACED PRE-COOJul 2, 2004 · N742AL · Boeing 73776N · Pneumatic Distribution SystemSDR AWXA200400799Splice · corrodedDURING C-12 CHECK CORROSION WAS FOUND ON AFT CARGO COMPARTMENT STRINGER SPLICE AT BS 907, STR 25 LT. MAINTENANCE REMOVED CORRODED STRINGER SPLICE AT BS 907, STR 25 LT; FABRICATED A NEW REPLACEMENT STRINGER SPLICE; INSTALLED REPAIR PART IAW DWG 65-51698.Jul 2, 2004 · N312AW · Boeing 7373S3 · Fuselage Miscellaneous StructureSDR F3LA200400069Odor · detectedBLOCK TURN BACK. FLIGHT CREW REPORTED ODOR OF SMOKE IN THE CABIN NEAR ROW 20. INVESTIGATED CABIN FOR SMOKE ODOR, OPERATED BOTH ENGINES AND AIR CONDITIONING SYSTEM. INSPECTED ALL LAVATORIES AND CARGO BAYS. NO SMOKE ODOR NOTED, NO FAULTS NOTED. INSPECTED AVJul 1, 2004 · N906FR · Airbus A319111 · Air Distribution SystemSDR USA2004F00094Charger · inoperativeFOUND SEVERAL AFT CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANE REPLACED THE AFT BATTERY AND CHARGER.Jun 30, 2004 · N512AU · Boeing 7373B7 · Emergency LightingSDR AWXA200400804Skin · corrodedMAJOR REPAIR, DURING C-12 CHECK EXFOLIATION CORROSION WAS FOUND ON EXTERIOR FUSELAGE SKIN BELOW CENTER FUEL TANK AT BS 590, LBL 57. MAINTENANCE BLENDED OUT CORROSION ON SKIN BELOW CENTER FUEL TANK AT BS 590, LBL 57, MATERIAL LOSS OUT OF LIMITS; FABRICATED WASHJun 30, 2004 · N312AW · Boeing 7373S3 · Fuselage Main, Plate/SkinSDR AWXA200400708Skin · crackedMAJOR REPAIR-DURING C-04 CHECK HFEC INSPECTION OF LOG ITEM DENT, CRACK INDICATION NOTED ON FUSELAGE SKIN AT BS 937,3 INCH ABOVE S24R, APPROX 0.75 INCH LONG. MAINTENANCE INSTALLED A DOUBLER/TRIPLER REPAIR IAW SRM 53-00-01-3 FIG 229.Jun 28, 2004 · N312AW · Boeing 7373S3 · Fuselage Main, Plate/SkinSDR 2004UALA00626Warning Light · illuminatedABORTED TAKEOFF AT 80 KNOTS DUE TO ELECTRICAL SIX PACK ALERT. COULD NOT DUPLICATE. REPLACED WORN LAMPS IN SIX PACK, CHECKS NORMAL.Jun 28, 2004 · N365UA · Boeing 737322 · Central WarningSDR DHL2004805006Warning Light · false indicationDURING UPLATCH CHECK RT GEAR UNSAFE LIGHT ILLUMINATED. PERFORMED ABNORMAL PROCEDURE CYCLED GEAR TWICE UPLATCH CHECKED, OK. DEFER IAW MEL32-16-1 CAT A ITEM DMI NR 17038, COMPLIED WITH S/P 32-16,MAIN LANDING GEAR UPLATCH SYS. PLACARD INSTALLED.Jun 27, 2004 · N805DH · Doug DC873F · Landing Gear Position and WarningSDR AWXA200400737Syncronizer · faultyFLIGHT CONTROL, ON APPROACH, ENROUTE FLAPS FAILED TO EXTEND BEYOND FLAPS 5, USED ALTERNATE FLAP PROCEDURES TO EXTEND FLAPS TO 15. MAINTENANCE REMOVED AND REPLACED FLAP POSITION INDICATOR IAW T/C 1B27001, OPERATIONAL CHECK WAS GOOD. FUNCTIONAL TEST OF FLAP POSJun 27, 2004 · N173AW · Boeing 73733A · Trailing Edge Flap Control SystemSDR DHL2004804504Rib · crackedITEM REF. NR. 1514: RT WING CTR. LE UPPER FORMER CRACKED 0.500 AT XFS 354.000. REMOVED FASTENER IAW SRM 51-1-21 PG.1. PERFORMED STOP HOLE ON CRACK END AND FABRICATED ANGLE DOUBLER (AL 2024-T3 0.040) IAW SRM 57-2-0 PG.9-10. CLEANED TREATED AND PRIMED ANGLE DOJun 27, 2004 · N804DH · Doug DC873F · Wing, Rib/BulkheadSDR DHL2004804505Rib · crackedRT WING CTR. LE UPPER FORMER CRACKED 0.500, XFS 347.750. CORR.: REMOVED FASTENER IAW SRM 51-1-21 PG.1. PERFORMED STOP HOLE ON CRACK END AND FABRICATED ANGLE DOUBLER (AL2024-T3 0.040) IAW SRM 57-2-0 PG.9-10. CLEANED, TREATED AND PRIMED ANGLE DOUBLER IAW SRM 51-Jun 27, 2004 · N804DH · Doug DC873F · Wing, Rib/BulkheadSDR USA2004F00093Circuit Breaker · trippedON APPROACH, CREW DID NOT RECEIVE ANY LANDING GEAR INDICATION LIGHTS AFTER GEAR EXTENSION. A MISSED APPROACH WAS EXECUTED. CREW TESTED THE LIGHTS BUT HAD NO ILLUMINATION OF THE GEAR LIGHTS. BULBS CHECKED OK ALONG WITH CIRCUIT BREAKERS. MAINTENANCE FOUND THJun 26, 2004 · N522AU · Boeing 7373B7 · Landing Gear SystemSDR 04FDEA01692Engine · overtempNR 1 ENG EGT INDICATION EXCEEDED TAKEOFF LIMIT MAX OF 948 DEGS FOR 20 SECONDS. REMOVED AND REPLACED NR 1 ENG PER MM.Jun 24, 2004 · N366SW · Boeing 7373H4 · Engine (Turbine/Turboprop)SDR SWAA041780Engine · overtempNR 1 ENG EGT INDICATION EXCEEDED TAKEOFF LIMIT MAX OF 948 DEGS FOR 20 SECONDS. REMOVED AND REPLACED NR 1 ENG PER MM.Jun 24, 2004 · N366SW · Boeing 7373H4 · Engine (Turbine/Turboprop)SDR MYW2004F00005Fmc · failedDURING DECENT INTO AIRPORT, AIRCRAFT EXPERIENCED DUAL FMC FAILURE. RECYCLED FMS CIRCUIT BREAKER. ACCOMPLISHED OPERATION TEST IAW MM. OPERATION NORMAL. RETURNED AIRCRAFT TO SERVICE.Jun 24, 2004 · N734MA · Boeing 7378Q8 · Flight Management Computing Software SystemSDR SWAA041779Turbine · failedIN FLIGHT SHUTDOWN / AIR TURNBACK, DURING CLIMB NR 1 ENGINE MADE A LOUD BANG. EGT INDICATION INCREASED TO 1060 DEGS. REMOVED AND REPLACED NR 1 ENG PER MM.Jun 23, 2004 · N346SW · Boeing 7373H4 · Turbine SectionSDR 2004UALA00600Frame · crackedSTA 663 FRAME HAS 4 CRACKS, 2 EACH AT THE STR 3 RT LIGHTENING HOLE, AND 1 EACH AT THE STR 1 AND 2 RT LIGHTENING HOLE. MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND REMOVED STRINGER SPLICES FOR ACCESS, INSTALLED REPAIR ANGLE DOUBLER AND STRINGER SPLICES.Jun 21, 2004 · N391UA · Boeing 737322 · Fuselage Main, FrameSDR AWXA200400805Support Angle · crackedDURING C-12 CHECK A 1.5 INCH CRACK WAS FOUND IN SUPPORT ANGLE UNDER KEELBEAM PANEL 3402 AT BS 616. MAINTENANCE REMOVED CRACKED SUPPORT ANGLE UNDER KEEL BEAM PANEL 3402 AT BS 616; FABRICATED A NEW REPLACEMENT SUPPORT ANGLE; INSTALLED REPAIR PART IAW DWG 69-3725Jun 21, 2004 · N312AW · Boeing 7373S3 · Fuselage Miscellaneous StructureSDR AWXA200400757Floorbeam · crackedMAJOR REPAIR, DURING C-15 CHECK, A .5000 INCH CRACK WAS FOUND IN FLOORBEAM AT FASTENER HEAD IN WEB BS 700, LBL 24.5, WL 204. MAINTENANCE CUTOUT DAMAGED SECTION OF FLOOR BEAM WEB AT BS 700, LBL 24.5, WL 204; FABRICATED A NEW REPLACEMENT SECTION OF WEB AND A REIJun 20, 2004 · N306AW · Boeing 7373G7 · Fuselage Main, Floor BeamSDR USA2004F00085Slide · unserviceableTHE RT SIDE REAR SERVICE DOOR HAS A SLIDE PACK STRAP EXTENDING OUT OF THE DOOR. MAINTENANCE REPLACED THE RT SIDE REAR SERVICE DOOR SLIDE ASSY. OK FOR SERVICE.Jun 20, 2004 · N119US · Airbus A320214 · Escape SlideSDR AWXA200400759Skin Panel · damagedMAJOR REPAIR, DURING C-17 CHECK FOUND 103 LOOSE RIVETS ON BOTH SIDES OF LOWER KEEL BEAM SKIN PANEL BETWEEN BS 663 AND BS 727. MAINTENANCE REMOVED DAMAGED LOWER KEEL BEAM SKIN PANEL FROM BS 661.75 TO BS 727; FABRICATED A NEW REPLACEMENT KEEL BEAM SKIN PANEL; Jun 19, 2004 · N315AW · Boeing 7373S3 · Fuselage Main, Plate/SkinSDR 2004UALA00695Skin · dentedDENT IN FUSELAGE JUST FWD AND ABOVE AFT LAV SERVICE PANEL. DENT MEASURES 6 INCH LONG X 5 INCH VERTICAL AT 0.250 INCH DEEP. FRAME HAS DISTORTION. *S/D* MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER/TRIPLER REPAIR.Jun 18, 2004 · N330UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR 2004UALA00593Indicator · inaccurateDIVERTED TO COS DUE TO INOP FUEL GAUGE. CREW REPORTED UNEVEN FUEL LOAD WITH EQUAL FUEL FLOW. FOUND 340 LBS DIFFERENCE BETWEEN THE DRIP STICK VALUE AND THE LEFT MAIN FUEL QUANTITY INDICATION SYSTEM. CALIBRATED NR 1 AND NR 2 FUEL QUANTITY INDICATION SYSTEMS.Jun 17, 2004 · N399UA · Boeing 737322 · Fuel Quantity IndicatorSDR USA2004F00087Skin · dentedFOUND DENT IN FUSELAGE SKIN, 2.5 INCH DIAMETER BY .050 INCH DEEP. CUT OUT DAMAGE AND INSTALLED DOUBLER IAW SRM.Jun 17, 2004 · N709UW · Airbus A319112 · Fuselage Main, Plate/SkinSDR USA2004F00089Skin · dentedFOUND DENT IN FUSELAGE SKIN, 1 INCH DIAMETER BY .050 INCH DEEP. CUT OUT DAMAGE AND INSTALLED DOUBLER IAW SRM.Jun 17, 2004 · N709UW · Airbus A319112 · Fuselage Main, Plate/SkinSDR USAA040320Seat Track · corrodedSEAT TRACK, 27 INCHES X .85 INCH X .047 INCH AREA, CORROSION; LEVEL 2; MAIN DECK FLOOR SUPPORT, FRAME 14-16, Y+503. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM.Jun 16, 2004 · N709UW · Airbus A319112 · Fuselage, Seat/Cargo Attach FittingsSDR 2004UALA00588Circuit Breaker · trippedDIVERTED TO IAD DUE TO CIRCUIT BREAKER PROBLEMS. GROUND SERVICE CB P6-11 D8 POPPED 2 TIMES ON TAXI. CYCLED BATTERY CHARGER C-B'S AFTER 20 MINUTES. RESET GROUND C-B WITH NORMAL FAN SELECTED FOR 5 MINUTES AND ALT EXHAUST FOR 20 MINUTES, GROUND C-B HELD AND STJun 16, 2004 · N306UA · Boeing 737322 · External Power SystemSDR 2004UALA00589Skin · dentedFOUND A 3.5 X 1.5 X 0.1875 DEEP DENT ON RIGHT HORIZONTAL STABILIZER LEADING EDGE APPROX 15 FEET FROM THE FUSELAGE. *S/D* MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND INSTALLED FLUSH REPAIR.Jun 16, 2004 · N391UA · Boeing 737322 · Horizontal Stabilizer, Plate/SkinSDR 2004UALA00584Light · contaminatedEMERGENCY EXIT PATH LIGHTS ARE INOP FROM ROW 15 AFT. REMOVED COFFEE AND CLEANED EEL TRACKS. OPS CHECKED NORMAL.Jun 15, 2004 · N347UA · Boeing 737322 · Emergency LightingSDR AWXA200400760Splice · crackedDURING C-17 CHECK A .5000 INCH CRACK WAS FOUND IN STRINGER SPLICE AT BS 907, STR 4 LT MAINTENANCE REMOVED CRACKED STRINGER SPLICE AT BS 907, STR 4 LT; FABRICATED A NEW REPLACEMENT SPLICE IAW DWG 65-51698-9; INSTALLED REPAIR PART IAW B737-300 SRM 51-40-02, PARAJun 15, 2004 · N315AW · Boeing 7373S3 · Fuselage Miscellaneous StructureSDR 2004UALA00583Lap Joint · damagedREPLACEMENT OF REPAIRS AT STA 887 STR 20R LAP JOINT AND AT STA 907 SKIN SPLICE DURING THE REPLACEMENT OF RIGHT AFT LOWER SKIN. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER, TRIPLER AND QUADRUPLER RUNNING FROM STA 874 TO STA 921, AND FROM STR 19R TO 21R.Jun 14, 2004 · N391UA · Boeing 737322 · Fuselage Main, Plate/SkinSDR 2004UALA00578Sensing Element · failedDIVERTED TO DENVER WITH NR 1 ENGINE OVERHEAT LIGHT ON. LANDED ON AMBER ALERT WITH ENGINE SHUTDOWN. CREW REPORTED CRUISING AT FL350, NR 1 ENGINE OVERHEAT LIGHT FLICKERED TWICE AND THEN CAME ON STEADY. ACCOMPLISHED ENGINE OVERHEAT CHECK LIST, LIGHT STAYED ON.Jun 13, 2004 · N368UA · Boeing 737322 · Overheat DetectionSDR 2004UALA00582Rib · dentedRT HORIZONTAL O/B LEADING EDGE SKIN IS DENTED AT THE 7TH RIB. *S/D* MAJOR REPAIR ACCOMPLISHED. CUT OUT DAMAGE AND INSTALLED INTERNAL DOUBLER AND FILLER.Jun 13, 2004 · N391UA · Boeing 737322 · Horizontal Stabilizer, Spar/RibSDR IXXA060164SSkin · gougedDURING ROUTINE C CHECK FOUND LT WING NR 1 MAIN-TANK-VENT FLOAT VALVE JUST OB OF XRS-358 HAS GOUGED UPPER SKIN. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTS, NEW FASTENERS AND SEALED REPAIJun 12, 2004 · N605AL · Doug DC873F · Wing, Plate/SkinSDR IXXA060162SRib · gougedDURING ROUTINE C-CHECK, FOUND LT WING TRAILING EDGE NR 4 SPOILER BAY THIRD RIB FROM FLAP HINGE FORWARD OB SIDE GOUGED. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND NEW FASTENERS IAW SJun 11, 2004 · N605AL · Doug DC873F · Wing, Rib/BulkheadSDR IXXA060163SDoubler · crackedDURING ROUTINE C-CHECK FOUND LT WING TRAILING EDGE NR 4 SPOILER BAY THIRD RIB FROM FLAP HINGE FORWARD OB SIDE DOUBLER CRACKED AND MISSING FASTENERS. REMOVED DOUBLER. FABRICATED REPAIR PART, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, PRIMED, INSTALLED REPAIRJun 11, 2004 · N605AL · Doug DC873F · Wing Miscellaneous StructureSDR USAA040316Frame · corrodedFRAME, 4.5 INCH X 1.75 INCH X .064 INCH AREA, CORROSION; LEVEL 2; FR68, Y1292, Z240. INSTALLED NEW FRAME IAW SRM.Jun 10, 2004 · N709UW · Airbus A319112 · Fuselage Main, Frame
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