N428MA

Service difficulty reports · 42

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N428MA' AND registry_match = 'registration'
  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 JIKA2019072501Sending Unit · defectiveDURING DESCENT APPROXIMATELY 20 MILES INTO KSAT, THE PILOT NOTICED THE LEFT ENGINE OIL TEMPERATURE REGISTERED AT 90 DEGREE CREW THEN CONSULTED THE QRH. POWER LEVER WAS REDUCED TO FLIGHT IDLE AS INSTRUCTED BY QRH AND CONTINUED MONITORING THE OIL TEMPERATURE GAJul 25, 2019 · N428MA · Swrngn SA227AC · Engine Oil TemperatureSDR JIKA201812272301Indicator · failedTHIS FLIGHT WAS EN ROUTE FROM KDFW TO KPHX. AT CRUISE OVER THE AREA OF KMAF, THE PILOT NOTICES THE RIGHT FUEL QUALITY INDICATOR SLOWLY DECREASING FUEL QUANTITY FROM 1500 LBS. A SHORT TIME LATER IT STOPPED AT 500 LBS. APPROXIMATELY 30 MINUTES LATER THE FUEL Dec 23, 2018 · N428MA · Swrngn SA227AC · Fuel Quantity IndicatorSDR JIKA2013042701Engine · failedDURING CRUISE AT 16000 FT, THE PILOT GOT A R CHIP DETECT LIGHT. WHILE MONITORING THE ENGINE THE TORQUE INDICATION FLUCTUATED, AND THE ENGINE FAILED. DECLARED AN EMERGENCY AND DIVERTED. REVIEW OF THE ENGINE TEAR DOWN REPORT REVEALED THAT THE PROBABLE CAUSE Apr 27, 2013 · N428MA · Swrngn SA227AC · Engine (Turbine/Turboprop)SDR JIKA11092101Wire · shortedEN ROUTE TO IDA THE PILOT REPORTED THAT THE RIGHT ENGINE OIL TEMP WAS EXTREMELY HIGH READING AT THE RED LINE. THE PILOT PERFORMED A PRECAUTIONARY SHUT DOWN OF THE RIGHT ENGINE FOLLOWING THE EMERGENCY PROCEDURES CHECKLIST. THE PILOT DECLARED AN EMERGENCY AND Sep 16, 2011 · N428MA · Swrngn SA227AC · Engine Oil System WiringSDR MALA975336Skin · chafedRIGHT UPPER AFT FLAP SKIN S/N FAI-246 IS CHAFED BETWEEN WING STATION 27 AND 39 DETERMINED TO BE WITHIN LIMITS PER FAC SRM 51-00-00. PERMANENT REPAIR DUE WITHIN 100:00 FLIGHT HOURS. COMPLETED PERMANENT REPAIR TO UPPER AFT FLAP SKIN IAW FAIRCHILD SRM 57-90-60 Feb 27, 1997 · N428MA · Swrngn SA227AC · Trailing Edge FlapsSDR MALA965128Firewall · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND 0.500 INCH TRANSVERSE CRACK IN RT FIREWALL. APPROXIMATE LOCATION IS BL 6.00 AND WL 91.00. STOP DRILLED CRACK, FABRICATED AND INSTALLED A 0.020 INCH STAINLESS REPAIR DOUBLER (3.50 INCH BY 1.20 INCH) IAW Sep 13, 1996 · N428MA · Swrngn SA227AC · Nacelle/Pylon, Bulkhead/FirewallSDR MALA965127Corner · crackedMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND LOWER AFT CORNER OF CARGO DOOR FRAME DAMAGED. REMOVED LOWER AFT CARGO DOOR CORNER, PN 27-240082-003, AND INSTALLED NEW CORNER IAW FAIRCHILD SRM 51-00-00, PAGE 4 AND SEALED IAW FAIRCHILD SRM 51-30-03. (X)Sep 13, 1996 · N428MA · Swrngn SA227AC · Cargo/Baggage DoorsSDR MALA965126Skin · crackedMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND FUSELAGE SKIN AT FS 159.24 AND WL 75.13 CRACKED TRANSVERSELY. CRACK LENGTH APPROXIMATELY 0.450 INCH. FABRICATED AND INSTALLED A 0.032 INCH BY 4.00 INCH BY 4.00 INCH SURFACE REPAIR DOUBLER TO AFFECTED ARESep 13, 1996 · N428MA · Swrngn SA227AC · Fuselage Main, Plate/SkinSDR MALA965125Torque Tube · chafedMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND RUDDER TORQUE TUBE CHAFED AT PRESSURE SEAL MOUNT AREA. REMOVED RUDDER TORQUE TUBE, PN 27-42051-037, AND INSTALLED NEW TORQUE TUBE IAW FAIRCHILD MM 27-20-20, PAGES 201-202. (X)Sep 13, 1996 · N428MA · Swrngn SA227AC · Rudder Control SystemSDR MALA965124Rib · crackedMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND AT WS 27.03 RT AFT WING RIB TRAILING EDGE (PN 27-31523), A 0.375 INCH CRACK. COMPLETED REPAIR PER FAC SRM 57-90-10, PAGES 3-6, REV. NOVEMBER 1, 1994, BY FABRICATING AND INSTALLING A 0.050 INCH BY 4.00 INCSep 13, 1996 · N428MA · Swrngn SA227AC · Wing, Rib/BulkheadSDR MALA965123Skin · chafedMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND CHAFE DAMAGE AT FS 241.00 AND ON BOTH SIDES OF BL 0.00. CHAFE DAMAGE IS APPROXIMATELY 0.025 INCH DEEP. (SUSTAINED DAMAGE ON RT SIDE WAS TO A FASTENER, AND ON LT SIDE, DAMAGE WAS TO FUSELAGE SKIN). REMOVSep 13, 1996 · N428MA · Swrngn SA227AC · Fuselage Main, Plate/SkinSDR MALA965122Actuator Mount · elongated holesMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND RIGHT FLAP ACTUATOR LINK UPPER SUPPORTING MOUNT HOLES ELONGATED. REPAIRED FLAP ACTUATOR UPPER SUPPORTING MOUNT HOLES BY REAMING HOLES AND INSTALLING INTERFERENCE FIT BUSHINGS IAW AERO TECH DESIGNS EA 01-9Sep 13, 1996 · N428MA · Swrngn SA227AC · Trailing Edge Flap ActuatorSDR MALA965121Angle · crackedMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND REPAIR ANGLE ON LEFT NACELLE INBOARD LOWER 'WING TO NACELLE' ATTACH ANGLE CRACKED. REMOVED PREVIOUS REPAIR ANGLE, FABRICATED AND INSTALLED NEW REPAIR ANGLE IAW ARP 54-20-9101, REV. B. (X)Sep 13, 1996 · N428MA · Swrngn SA227AC · Nacelle/Pylon StructureSDR MALA965120Intercostal · crackedMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND LOWER LT BELT FRAME INTERCOSTAL CRACKED IN TWO LOCATIONS AT CORNER RELIEF RADIUS CUT-OUTS. ONE CRACK IS 0.250 INCH AND THE OTHER IS 0.400 INCH. FABRICATED AND INSTALLED REPAIR DOUBLER IAW AEROTECH DESIGNSep 13, 1996 · N428MA · Swrngn SA227AC · Fuselage Miscellaneous StructureSDR MALA965119Skin · chafedMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE UPPER PASSENGER DOOR HINGE TO SKIN FASTENERS (ON PASSENGER DOOR) 'WORKING' AND CHAFING SKIN. REMOVED AFFECTED SKIN, FABRICATED AND INSTALLED A 10.50 INCH REPAIR SKIN SPLICE ONTO UPPER PASSENGER DOOR HSep 13, 1996 · N428MA · Swrngn SA227AC · Passenger/Crew DoorsSDR MALA965065Oil Temp Sensor · malfunctionedFLT 3048 - AFTER TAKEOFF FROM DTW, THE RIGHT OIL TEMPERATURE DROPPED TO 40 DEGREES CELSIUS. ALL OTHER ENGINE INDICATIONS WERE NORMAL. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. AS A PRECAUTION, THE RIGHT OIL TEMP BULJul 6, 1996 · N428MA · Swrngn SA227AC · Engine Oil TemperatureSDR MALA964986Switch · dirtyFLT NR 3182 - ON APPROACH TO DTW, THE RIGHT GEAR INTRANSIT LIGHT FAILED TO ILLUMINATE DURING GEAR EXTENSION. ALL OTHER INDICATIONS WERE NORMAL. MX CLEANED AND LUBED THE RIGHT OUTBOARD UPPER POSITION SWITCH. SYSTEM OPERATED SATISFACTORILY. (M)May 8, 1996 · N428MA · Swrngn SA227AC · Landing Gear Position and WarningSDR MALA964948Bus Light · flickersYNG - FLT 3367 - ON APPROACH THE RIGHT NON-ESSENTIAL BUS LIGHTS BEGAN TO FLICKER AND THE CREW NOTED AN ELECTRICAL SMELL. MAINTENANCE DEFERRED THE SYSTEM PER MEL 33-1C. (X)Apr 11, 1996 · N428MA · Swrngn SA227AC · DC Indicating SystemSDR MALA964902Frame · chafedDURING A SCHEDULED INSPECTION IN MSP, THE PASSENGER DOOR FORWARD SIDE FRAME WAS CHAFED THROUGH AT THE CENTER BAYONET AREA. REPAIRS WERE COMPLETED BY INSTALLING AN ELEVEN INCH DOUBLER IAW FAC SRM 52-90-10 PAGES 5-7 AS PER FAC LAR 96-MALA-043. (M)Mar 7, 1996 · N428MA · Swrngn SA227AC · Passenger/Crew DoorsSDR MALA964901Corner · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE LOWER FORWARD DOOR CORNER TO BE CRACKED. REPAIRS WERE COMPLETED BY REPLACING THE CORNER IAW FAC SRM 51-00-00. (M)Mar 6, 1996 · N428MA · Swrngn SA227AC · Passenger/Crew DoorsSDR MALA964895Switches · failedSTC - FLT 3491 - DURING APPROACH, CREW NOTED NOSE GEAR GREEN DOWN AND LOCKED LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION. THE CREW ELECTED TO RETURN TO MSP, AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE LT AND RT NOSE DOWN AND LOMar 2, 1996 · N428MA · Swrngn SA227AC · Landing Gear Position and WarningSDR MALA964853Tq Tube Arm · failedFLT 3017 - ON APPROACH TO DTW, THE NOSE GEAR DOWN AND LOCKED LIGHT FAILED TO ILLUMINATE. THE CREW CYCLED THE GEAR UNTIL A DOWN AND LOCKED INDICATION WAS RECEIVED. MAINTENANCE REPLACED THE NLG TORQUE TUBE ARM ASSY. SYSTEM OPERATED SATISFACTORILY. (X)Jan 31, 1996 · N428MA · Swrngn SA227AC · Landing Gear Retraction/Extension SystemSDR MALA964828Door Frame · crackedDURING A SCHEDULED INSPECTION IN MSP, THE CARGO DOOR FRAME, AT FS 438.060, WAS FOUND TO BE CRACKED. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR ANGLE, PLATE AND FILLER IAW FAC ARM 53-20-9503. (M)Jan 19, 1996 · N428MA · Swrngn SA227AC · Fuselage Miscellaneous StructureSDR MALA954711Inverter · failedFLT NR 3237 - EN ROUTE FROM MSP TO BJI, THE NR 2 INVERTER DROPPED OFF LINE. THE AIRCRAFT RETURNED TO MSP WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE NR 2 INVERTER. ALL SYSTEMS OPERATED SATISFACTORILY. (M)Nov 14, 1995 · N428MA · Swrngn SA227AC · AC InverterSDR MALA954576Door Frame · crackedMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND AFT CARGO DOOR FUSELAGE FRAME CRACKED AT THE ACTUATOR ATTACH POINT HOLE. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING A REPAIR ANGLE, DOUBLER, AND FILLER IAW FAC ARP 53-20-9503. (X)Aug 7, 1995 · N428MA · Swrngn SA227AC · Fuselage Miscellaneous StructureSDR MALA954566Angle · crackedMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE PERSONNEL FOUND THE LT NACELLE INBOARD LOWER WING SKIN TO NACELLE ATTACH ANGLE CRACKED AT SEVERAL RIVET HOLES ON THE FORWARD END. THEY REPLACED THE FORWARD 20 INCHES OF THE ANGLE AND INSTALLED A DOUBLER OVER THAug 1, 1995 · N428MA · Swrngn SA227AC · Nacelle/Pylon StructureSDR MALA954565Doubler · wornMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE PERSONNEL FOUND WEAR ON THE LT FLAP WALKING BEAM ROLLER DOUBLER. THEY REPLACED THE DOUBLER WITH A SERVICEABLE DOUBLER IAW FAIRCHILD SRM 57-90-10. (X)Aug 1, 1995 · N428MA · Swrngn SA227AC · Trailing Edge FlapsSDR MALA954564Flange · crackedMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE PERSONNEL FOUND A .125 INCH CRACK AT THE RT CONSTANT SECTION INNER FLANGE RADIUS FS 159.24 AND APPROXIMATELY WL 70.65. THEY STOP DRILLED THE CRACK AND FABRICATED, PREPPED, AND INSTALLED A DOUBLER AND STIFFENER Aug 1, 1995 · N428MA · Swrngn SA227AC · Fuselage Miscellaneous StructureSDR MALA954563Flange · crackedMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE PERSONNEL FOUND A .5 INCH CRACK AT RT CONSTANT SECTION INNER FLANGE RADIUS FS 145.95 AND APPROXIMATELY WL 70.65. THEY STOP DRILLED THE CRACK AND FABRICATED, PREPPED, AND INSTALLED A DOUBLER AND STIFFENER IAW FAAug 1, 1995 · N428MA · Swrngn SA227AC · Fuselage Miscellaneous StructureSDR MALA954562Flange · crackedMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE PERSONNEL FOUND A .125 INCH CRACK AT THE RT CONSTANT SECTION INNER FLANGE RADIUS, FS 254.52 AND APPROXIMATELY WL 70.65. THEY REPAIRED THE CRACK BY STOP DRILLING IT AND FABRICATING, PREPPING, AND INSTALLING A DOAug 1, 1995 · N428MA · Swrngn SA227AC · Fuselage Miscellaneous StructureSDR MALA954561Doubler · wornMSP - DURING SCHEDULED INSPECTION, MAINTENANCE PERSONNEL FOUND WEAR ON THE RT FLAP WALKING BEAM ROLLER DOUBLER. THEY REPLACED THE DOUBLER WITH A SERVICEABLE DOUBLER IAW FAIRCHILD SRM 57-90-10. (X)Aug 1, 1995 · N428MA · Swrngn SA227AC · Trailing Edge FlapsSDR MALA954455Hook Assy · stickingFLT 3298 - ON CLIMB-OUT FROM BJI, THE NOSE GEAR CONTINUED TO CYCLE IN THE GEARWELL AFTER IT WAS RETRACTED. THE CREW RECYCLED THE GEAR UNTIL THE GEAR REMAINED UP AND LOCKED. THE AIRCRAFT CONTINUED TO MSP. MAINTENANCE REPLACED THE UPLOCK HOOK ASSY, P/N 27-520May 15, 1995 · N428MA · Swrngn SA227AC · Landing Gear Retraction/Extension SystemSDR MALA954410Uplock Roller · failedDTW - FLT 3014 - AFTER TAKEOFF, NOSE GEAR CONTINUED TO CYCLE AFTER GEAR RETRACTION. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE NOSE GEAR DOOR UPLOCK ROLLER. SYSTEM OPERATED SATISFACTORILY. (X)Apr 11, 1995 · N428MA · Swrngn SA227AC · Landing Gear Retraction/Extension SystemSDR MALA954367Switch · out of adjustFLT 3355 - ON CLIMB-OUT FROM YXU, THE NOSE GEAR CONTINUED TO CYCLE AFTER GEAR RETRACTION. THE AIRCRAFT RETURNED TO YXU. MAINTENANCE ADJUSTED THE NOSE GEAR UPLOCK SWITCH. SYSTEM OPERATED SATISFACTORILY. (W)Mar 9, 1995 · N428MA · Swrngn SA227AC · Landing Gear Position and WarningSDR MALA954354Switch · out of adjustTOL - FLT 3393 - ON CLIMB-OUT, LEFT GEAR CONTINUED TO CYCLE AFTER GEAR RETRACTION. THE CREW CYCLED GEAR AND THE PROBLEM RECURRED. THE AIRCRAFT CONTINUED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE LEFT GEAR 'UP' POSITION SWITCH. SYSTEM OPEMar 2, 1995 · N428MA · Swrngn SA227AC · Landing Gear Retraction/Extension SystemSDR MALA954301Attitude · failedFLT 3467 - UPON DEPARTURE FROM DTW, THE ARTIFICIAL HORIZON TUMBLED DURING ROTATION. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE NR 1 ATTITUDE GYRO. SYSTEM OPERATED SATISFACTORILY. (Z)Feb 9, 1995 · N428MA · Swrngn SA227AC · Attitude Gyro and Indicating SystemSDR MALA954272Engine · failedFLT 3185 - ON CLIMB-OUT FROM DTW, THE CREW RECEIVED A LEFT ENGINE FIRE WARNING LIGHT AND THE LEFT SUB PANEL FIRE LIGHT. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE LEFT ENGINE. SYSTEM OPERATED SATISFACTORILY. (W)Jan 22, 1995 · N428MA · Swrngn SA227AC · Engine (Turbine/Turboprop)SDR MALA954268Tadpole Seal · wornYNG - FLT 3055 - ON CLIMB-OUT, LT ENGINE FIRE ANNUNCIATOR PANEL LIGHT, AND LT ENGINE SUB-PANEL FIRE LIGHT ILLUMINATED. THE CREW SHUT DOWN THE LT ENGINE AND DIVERTED TO CLE. MAINTENANCE REPLACED TADPOLE SEAL. SYSTEM OPERATED SATISFACTORILY. (X)Jan 18, 1995 · N428MA · Swrngn SA227AC · Fire DetectionSDR MALA954244Dnlock Switch · failedFLT 3240 - ON APPROACH TO MSP, THE RIGHT GEAR DID NOT INDICATE DOWN AND LOCKED AFTER GEAR EXTENSION. THE CREW CYCLED THE GEAR AND THE INDICATION LIGHT WAS SLOW TO ILLUMINATE. THE AIRCRAFT LANDED WITHOUT INCIDENT IN MSP. MAINTENANCE REPLACED THE INBOARD DOWNJan 16, 1995 · N428MA · Swrngn SA227AC · Landing Gear Position and WarningSDR MALA954227Fire Detector · intermittentDTW - FLT 3341 - DURING CLIMBOUT, THE LT ENGINE FIRE LIGHT ILLUMINATED FOR 10 TO 15 SECONDS. ALL ENGINE PARAMETERS NORMAL. THE ACFT RETURNED TO DTW. MAINTENANCE REPLACED THE 450 DEGREES FIRE DETECTOR. SYSTEM OPERATED SATISFACTORILY. (W)Jan 3, 1995 · N428MA · Swrngn SA227AC · Fire DetectionSDR MALA954222Air Distr · smokingDTW - DURING A MAINTENANCE TEST FLIGHT, THE CREW NOTED SMOKE IN THE COCKPIT AND CABIN ON SHORT FINAL. THE CREW SHUT OFF THE BLEEDS AND RETURNED TO DTW. MAINTENANCE GROUND RAN THE ACFT. ALL SYSTEMS OPERATED SATISFACTORILY. NO SMOKE NOTED. (W)Jan 2, 1995 · N428MA · Swrngn SA227AC · Air Distribution SystemSDR MALA954221Wire · chafedFLT 3014 - IN CRUISE FLIGHT FROM DTW, THE LEFT ENGINE FIRE LIGHT FLASHED MOMENTARILY IN FLIGHT. THE AIRCRAFT RETURNED DTW. MAINTENANCE REPAIRED CHAFED WIRES 393005B-22 AND 393005E-22. SYSTEM OPERATED SATISFACTORILY. THE FIRE EXTINGUISHER LOGIC MODULE WAS AJan 1, 1995 · N428MA · Swrngn SA227AC · Fire Protection System Wiring
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