N430MA

Service difficulty reports · 36

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 = 'N430MA' 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 DUFA20180529001Gear · strippedWHILE IN CRUISE DURING A PART 91 REPOSITION FLIGHT, THE NR 2 ENGINE FLAMED OUT AND SHUT DOWN. MAINTENANCE CREW WAS DISPATCHED TO THE LOCATION AND THE ENGINE GEARBOX OPENED UP FOR INVESTIGATION. FOUND ACCESSORY GEAR ASSEMBLY HAD FAILED LOSING CONTINUITY TO FUELMay 16, 2018 · N430MA · Swrngn SA227AC · Engine Fuel PumpSDR 2006F00039Indication Sys · malfunctionedLEFT LANDING GEAR INDICATION SHOWED GEAR NOT DOWN. CLEANED ANNUNCIATOR CONTACTS. OPS CHECK OK.Sep 13, 2006 · N430MA · Swrngn SA227AC · Landing Gear Position and WarningSDR 2006F00038Contactor · dirtyLEFT MAIN DOWN LIGHT FAILED TO ILLUMINATE. FLYOVER SHOWED GEAR DOWN. ANNUNCIATOR CONTACTS WERE CLEANED. GEAR WAS CYCLED AND DISCREPANCY WAS CLEARED.Sep 13, 2006 · N430MA · Swrngn SA227AC · Landing Gear Position and WarningSDR 2005FA0000041Acm · seizedON TOUCHDOWN, THE CREW NOTICED AN ACRID SMELL IN THE COCKPIT. THE CREW LANDED AND TAXIED IN WITH NO FURTHER INCIDENT. TROUBLESHOOTING FOUND THE SOURCE TO THE RT ACM. INITALLY DEFERRED ACM IAW MEL, LATER CHANGED THE ACM, MEL WAS CLEARED. (NM05200403534) (KDec 31, 2004 · N430MA · Swrngn SA227AC · Cabin Cooling SystemSDR 2005FA0000064Scavenge Pump · failedMRR-M04-23, NR 2 ENGINE OIL PRESSURE LIGHT CAME ON AS FLIGHT LEVELED OUT IN CRUISE, OIL PRESSURE GAUGE WAS CHECKED AND FOUND PRESSURE DROPPING. CREW DID A PRECAUTIONARY INFLIGHT SHUTDOWN, AND RETURNED TO STATION. LOSS OF OIL PRESSURE DUE TO LOSS OF OIL FRM RDec 6, 2004 · N430MA · Swrngn SA227* · Turbine Engine Oil SystemSDR 2005FA0000043Warning System · malfunctionedCARGO DOOR WARNING LIGHT CAME ON IN FLIGHT DURING THE START OF THE DESCENT TO THE NEXT STATION. ATC WAS NOTIFIED. THE LIGHTS STAYED ON FOR APPROXIMATELY 10 MINUTES. DOOR CLOSING PROCEDURES, DOOR HARD TO CLOSE, DOOR CLICK CLACK RIGGING/LUBRICATION, OR SWITCHMar 4, 2004 · N430MA · Swrngn SA227AC · Door Warning SystemSDR 2003F00624Line · leakingDURING CRUISE THE RT ENGINE OIL PRESS WARN LIGHT CAME ON, THIS VERIFIED WITH THE OIL PRESSURE GAUGE. CREW FOLLOWED CHECKLIST PROCEDURES AND SHUTDOWN THE ENGINE. OIL TEMPERATURE STAYED IN THE NORMAL RANGE THROUGH THE SHUTDOWN. CREW DIVERTED TO CLOSEST STATIOAug 9, 2003 · N430MA · Swrngn SA227AC · Engine Oil Distribution (Airframe Furnished)SDR 2003F00632Pump · malfunctionedRT ENGINE OIL PRESSURE LIGHT DIDN'T GO OUT AFTER 50 PERCENT RPM DURING START. OIL PRESSURE WAS ALSO LOW. MAINTENANCE FOUND OIL LEVEL LOW AND OIL IN THE TAIL PIPE. REPLACED REAR OIL SCAVENGE PUMP. OPS CHECK AND FLIGHT CHECK. (M)Jul 16, 2003 · N430MA · Swrngn SA227AC · Engine Oil System (Airframe Furnished)SDR 2003F00626Water Injection · failedCAWI DID NOT FIRE ON TAKEOFF ROLL. LIGHTS OPERATE NORMALLY BUT NO RISE IN PERCENT TORQUE. DEFERRED CAWI SYSTEM. NO DEFECTS NOTED WHEN AIRCRAFT CAME IN FOR REPAIR. (M)Jul 2, 2003 · N430MA · Swrngn SA227AC · Water Injection SystemSDR 2003F00241Indicator · failedFLT 2579 - BIL - NR 1 VSI FAILED DURING DESCENT. CREW LANDED WITH NO FURTHER INCIDENT AFTER DECLARING EMERGENCY. TCAS/VSI INDICATOR WAS BAD. REPLACED VSI/TCAS INDICATOR, SYSTEM TEST GOOD. (M)Feb 5, 2003 · N430MA · Swrngn SA227AC · Air Collision Avoidance SystemSDR BSAA030231Indicator · failedNR 1 VSI FAILED DURING DESCENT. CREW LANDED WITH NO FURTHER INCIDENT AFTER DECLARING EMERGENCY. REPLACED VSI/TCAS INDICATOR, SYSTEM TEST GOOD.Feb 5, 2003 · N430MA · Swrngn SA227AC · Air Collision Avoidance SystemSDR MALA965240Rib · crackedDURING AN INSPECTION IN MSP, MAINTENANCE FOUND TWO CRACKS 1 INCH BY 1 INCH IN THE RADIUS OF THE LT WING RIB LOWER ATTACH FLANGE (P/N 27-31023). APPROXIMATE LOCATION IS WS 81 AND BETWEEN NS 130 AND 141. STOP DRILLED CRACK, FABRICATED AND INSTALLED AN APPROPRIDec 18, 1996 · N430MA · Swrngn SA227AC · Wing, Rib/BulkheadSDR MALA965241Rib · crackedDURING AN INSPECTION IN MSP, FOUND TWO CRACKS IN THE RADIUS OF THE RT WING RIB LOWER ATTACH FLANGE (P/N 27-31023). APPROXIMATE LOCATION IS WS 81 AND BETWEEN NS 130 AND 141. STOP DRILLED CRACK, FABRICATED AND INSTALLED AN APPROPRIATE SIZED 3 INCH BY 1 INCH BYDec 17, 1996 · N430MA · Swrngn SA227AC · Wing, Rib/BulkheadSDR MALA965215Rib · crackedDURING A BLOCK INSPECTION IN MSP, MAINTENANCE FOUND A CRACK APPROX .75 INCH LONG IN RIGHT INBOARD FLAP NOSE RIB. REMOVED AND REPLACED FLAP NOSE RIB P/N 27-36015-002 IAW FAIRCHILD STRUCTURAL REPAIR MANUAL 52-00-00 PAGE 4 AND 51-40-02. (M)Nov 21, 1996 · N430MA · Swrngn SA227AC · Trailing Edge FlapsSDR MALA965214Rib · crackedDURING A BLOCK INSPECTION IN MSP, MAINTENANCE FOUND TWO CRACKS IN LEFT FLAP SN C-134 OUTBOARD FLAP NOSE RIB. REMOVED AND REPLACED FLAP NOSE RIB P/N 27-36015-001 IAW FAIRCHILD STRUCTURAL REPAIR MANUAL 57-90-60 PAGES 43-46. (M)Nov 21, 1996 · N430MA · Swrngn SA227AC · Trailing Edge FlapsSDR MALA965213Angle · crackedDURING A BLOCK INSPECTION IN MSP, MAINTENANCE FOUND THE LEFT INBOARD UPPER NACELLE TO WING TRANSIT ANGLE CRACKED AT THE FORWARD EDGE. REPAIR WAS COMPLETED BY INSTALLING A REPAIR DOUBLER IAW ARP 54-20-9101 REV B AND FAIRCHILD SRM 51-30-02, 51-40 AND 51-30-03. Nov 20, 1996 · N430MA · Swrngn SA227AC · Nacelle/Pylon StructureSDR MALA965212Angle · crackedDURING A BLOCK INSPECTION IN MSP, MAINTENANCE FUOND LEFT INBOARD LOWER NACELLE TO WING TRANSIT ANGLE CRACKED AT FORWARD EDGE. COMPLETED REPAIR BY REMOVING EXISTING REPAIR, FABRICATING AND WET INSTALLING NEW DOUBLER IAW ARP 54-20-9101 REV B DATED MAY 12, 1993,Nov 20, 1996 · N430MA · Swrngn SA227AC · Nacelle/Pylon StructureSDR MALA965211Angle · crackedDURING A BLOCK INSPECTION IN MSP, MAINTENANCE FOUD THE RIGHT INBOARD LOWER NACELLE TO WING TRANSIT ANGLE CRACKED AT THE FORWARD EDGE. REPAIR WAS COMPLETED BY INSTALLING A REPAIR DOUBLER IAW ARP 54-20-9101 REV B AND FAIRCHILD SRM 51-30-02, 51-40 AND 51-30-03. Nov 20, 1996 · N430MA · Swrngn SA227AC · Nacelle/Pylon StructureSDR MALA964977Engine · failedTOL/DTW - FLT 3328 - IN CRUISE FLIGHT, THE LEFT ENGINE CHIP DETECTOR LIGHT ILLUMINATED. THE CREW PERFORMED QUICK REFERENCE PROCEDURES. (X)Apr 30, 1996 · N430MA · Swrngn SA227AC · Engine (Turbine/Turboprop)SDR MALA964970Switch · out of adjustFLIGHT 3234 - ON CLIMB-OUT FROM BJI, THE NOSE GEAR CONTINUED TO CYCLE IN THE WHEEL WELL AFTER THE GEAR WAS RETRACTED. MAINTENANCE ADJUSTED THE UPLIMIT SWITCH. ALL SYSTEMS OPERATED SATISFACTORILY. (M)Apr 19, 1996 · N430MA · Swrngn SA227AC · Landing Gear Retraction/Extension SystemSDR MALA954774Shear Bolt · shearedFLT NR 3250 - DURING LANDING AT GFK, THE RIGHT GEAR DOOR POSITION LIGHT ILLUMINATED. THE AIRCRAFT CONTINUED THE LANDING WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE RIGHT GEAR DOOR ROLLER SHEAR BOLT. ALL SYSTEMS OPERATED SATISFACTORILY. (M)Dec 26, 1995 · N430MA · Swrngn SA227AC · Landing Gear Door Retract SectionSDR MALA954689Skin Patch · damagedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE RIGHT OUTBOARD GEAR DOOR FLUSH PATCH DOOR SKIN REPAIR DAMAGED. REPAIRS WERE COMPLETED BY REPLACING THE FILLER IAW FAC SRM 52-90-30. (M)Oct 29, 1995 · N430MA · Swrngn SA227AC · Landing Gear DoorsSDR MALA954688Seat Track · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE PILOTS SEAT TRACK ATTACH POINTS AT FS 107 TO BE CRACKED. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING A REPAIR FLAGNE IAW ARP 53-10-8913. (M)Oct 29, 1995 · N430MA · Swrngn SA227AC · Fuselage, Seat/Cargo Attach FittingsSDR MALA954687Seat Track · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND A CRACK AT THE NUT PLATES FOR THE PILOTS OUTBOARD SEAT TRACK ATTACHMENT JUST AFT OF FS 107. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR DOUBLER IAW ARP 53-10-9322. (M)Oct 29, 1995 · N430MA · Swrngn SA227AC · Fuselage, Seat/Cargo Attach FittingsSDR MALA954686Torque Tube · corrosionDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE RIGHT ELEVATOR TORQUE TUBE WELDMENT TO HAVE SIGNS OF CORROSION. REPAIRS WERE COMPLETED BY REPLACING THE RIGHT ELEVATOR ASSEMBLY. (M)Oct 29, 1995 · N430MA · Swrngn SA227AC · Elevator StructureSDR MALA954685Door Corner · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE UPPER PASSENGER DOOR CORNER CRACKED. REPAIRS WERE COMPLETED BY REPLACING THE CORNER, P/N 27-24044-010, IAW FAC SRM 51-00-00 PAGE 4. (M)Oct 29, 1995 · N430MA · Swrngn SA227AC · Passenger/Crew DoorsSDR MALA954684Door Corner · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE AFT UPPER PASSENGER DOOR CORNER CRACKED. REPAIRS WERE COMPLETED BY REPLACING THE CORNER, P/N 27-24044-009, IAW FAC SRM 51-00-00 PAGE 4. (M)Oct 29, 1995 · N430MA · Swrngn SA227AC · Passenger/Crew DoorsSDR MALA954683Stairs · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE PASSENGER DOOR STAIR ASSEMBLY CRACKED. REPAIRS WERE COMPLETED BY REPLACING THE STAIR ASSEMBLY, P/N 27-24150-297. (M)Oct 29, 1995 · N430MA · Swrngn SA227AC · Passenger/Crew DoorsSDR MALA954682Skin · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE PASSENGER DOOR AFT LOWER SKIN CRACKED NEAR THE HINGE. REPAIRS WERE COMPLETED BY REPLACING THE SKIN SEGMENT IAW FAC SRM 51-90-10, PAGES 12-14. (M)Oct 29, 1995 · N430MA · Swrngn SA227AC · Passenger/Crew DoorsSDR MALA954615Door Frame · crackedMSP - DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND THE CARGO DOOR FUSELAGE FRAME AT FS 438 CRACKED AT THE GAS STRUT MOUNT POST HOLE. REPAIRS WERE COMPLETED BY INSTALLING A REPAIR ANGLE, PLATE AND FILLER IAW FAC ARP 53-20-9503. (X)Aug 31, 1995 · N430MA · Swrngn SA227AC · Fuselage Miscellaneous StructureSDR MALA954614Frame · crackedMSP - DURING A SCHEDULED INSPECTION, FOUND THE CARGO DOOR FUSELAGE FRAME AT FS 491 CRACKED AT THE GAS STRUT MOUNT POST HOLE. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING A REPAIR ANGLE, PLATE, AND FILLER IAW ARP 53-20-9503. (X)Aug 31, 1995 · N430MA · Swrngn SA227AC · Fuselage Miscellaneous StructureSDR MALA954585Doubler · wornDURING SCHEDULED MAINTENANCE IN MSP, THE RIGHT FLAP ROLLER DOUBLER WAS WORN. REPAIRS WERE COMPLETED BY REPLACING THE DOUBLER IAW FAC 57-10-9207 AND ARP 57-20-9024. (M)Aug 16, 1995 · N430MA · Swrngn SA227AC · Trailing Edge FlapsSDR MALA954541Switch · failedFLT 3027 - ON APPROACH TO MSP, THE CREW DIDN'T RECEIVE A DOWN AND LOCKED INDICATION FROM THE NOSE GEAR POSITION AFTER GEAR EXTENSION. THE CREW CYCLED THE GEAR TWICE BEFORE A DOWN AND LOCKED INDICATION WAS RECEIVED. THE AIRCRAFT CONTINUED TO MSP AND LANDED WIJul 15, 1995 · N430MA · Swrngn SA227AC · Landing Gear Position and WarningSDR MALA954533Position Ind · malfunctionedFLT 3253 - ON APPROACH TO MSP, THE NOSE GEAR GREEN LIGHT FAILED TO ILLUMINATE UPON GEAR EXTENSION. THE CREW CYCLED THE GEAR UNTIL THE LIGHT ILLUMINATED. MAINTENANCE WAS UNABLE TO DUPLICATE THE DISCREPANCY. THE GEAR POSITION INDICATOR WAS REPLACED AS A PRECAJul 10, 1995 · N430MA · Swrngn SA227AC · Landing Gear Position and WarningSDR MALA954496Eel Bulbs · failedMSP - DURING WALKAROUND, THE FORWARD EMERGENCY EXIT ESCAPE FLOOR PATH LIGHTS HAD TWO BULBS INOPERATIVE. MAINTENANCE REPLACED THE LT AFT BATTERY PACK. SYSTEM OPERATED SATISFACTORILY. (W)Jun 7, 1995 · N430MA · Swrngn SA227AC · Emergency LightingSDR MALA954497Feed Back Pot · failedDTW - FLT 3186 - DURING LANDING AT DTW, AIRCRAFT PROCEEDED LEFT UNCOMMANDED WHEN NOSE WHEEL STEERING WAS ENGAGED. MAINTENANCE REPLACED THE NOSE WHEEL STEERING FEEDBACK POT MOUNT ASSEMBLY. THE SYSTEM OPERATED SATISFACTORILY. (X)Jun 6, 1995 · N430MA · Swrngn SA227AC · Landing Gear Steering System
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