N434MA, cancelled Nov 19, 2009

Service difficulty reports · 27

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 = 'N434MA' AND deregistration_id = 'N434MA-2009-11-19'
  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 2006F00054Fire Warning · activatedRT ENGINE FIRE WARNING ILLUMINATED, RETURNED TO FIELD.Nov 19, 2006 · N434MA · Frchld SA227CC · Fire DetectionSDR MALA965245Rib · crackedDURING AN INSPECTION IN MSP, MAINTENANCE FOUND TWO CRACKS 1INCH 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 A 6.5 INCH, Dec 18, 1996 · N434MA · Swrngn SA227AC · Wing, Rib/BulkheadSDR MALA965244Rib · crackedDURING AN INSPECTION IN MSP, MAINTENANCE FOUND TWO CRACKS 2 INCH BY 1 INCH IN THE RADIUS OF THE RIGHT WING RIB LOWR ATTACH FLANGE (P/N 27-31023). APPROXIMATE LOCATION IS WS 81 BETWEEN NS 130 AND 141. STOP DRILLED CRACK, FABRICATED AND INSTALLED A 6.5 INCH, Dec 18, 1996 · N434MA · Swrngn SA227AC · Wing, Rib/BulkheadSDR MALA965239Rib · crackedDURING AN INSPECTION IN MSP, MAINTENANCE FOUND A 5 INCH CRACK IN THE RADIUS OF THE 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 A 8.25 INCH BY 3 INCH BY 1 Dec 18, 1996 · N434MA · Swrngn SA227AC · Wing, Rib/BulkheadSDR MALA965230Skin · chafedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND SKIN CHAFE DAMAGE AT FS 241 AND ON BOTH SIDES OF BL 0.00. CHAF DAMAGE IS APPROX .025 INCH DEEP AND .125 INCH IN DIAMETER. FABRICATED AND INSTALLED EXTERNAL REPAIR DOUBLER (.050 BY 4 BY 5 INCH) IAW FAC SNov 28, 1996 · N434MA · Swrngn SA227AC · Fuselage Main, Plate/SkinSDR MALA965226Torque Tube · wornDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE RUDDER TORQUE TUBE WORN BEYOND ALLOWABLE LIMITS OF .003 FROM PHENOLIC SEAL. REPAIRED RUDDER TORQUE TUBE BY REMOVING AND REPLACING WITH A NEW RUDDER TORQUE TUBE, P/N 27-42051-8037, IAW FAIRCHILD MM 27Nov 28, 1996 · N434MA · Swrngn SA227AC · Rudder Control SystemSDR MALA965229Rib · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENACNE FOUND A CRACK IN THE LEFT FLAP S/N RPL10-88 OUTBOARD FLAP NOSE RIB. REMOVED AND REPLACED IAW FAC SRM 57-90-60. (M)Nov 27, 1996 · N434MA · Swrngn SA227AC · Trailing Edge FlapsSDR MALA965228Angle · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND A CRACK IN THE RIGHT FORWARD LOWER INBOARD WING TO NACELLE INTRANSIT ANGLE. (M)Nov 27, 1996 · N434MA · Swrngn SA227AC · Nacelle/Pylon StructureSDR MALA965227Intercostal · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND A .25 INCH CRACK IN LT INTERCOSTAL RELIEF RADIUS AT FUSELAGE STATION 377. REPAIRED PER FAC MM 53-90-20 REPAIR NR 20. (M)Nov 26, 1996 · N434MA · Swrngn SA227AC · Fuselage Miscellaneous StructureSDR MALA965192Rib · crackedDURING SCHEDULED MAINTENANCE IN MSP, THE LEFT FLAP NOSE RIB HAD A .5 INCH CRACK FROM THE RELIEF RADIUS. COMPLETED REPAIR TO LEFT FLAP BY REPLACING THE INBOARD NOSE RIB P/N 27-36004-007 IAW 51-00-00 PAGE 4 AND 51-40-02. (M)Nov 9, 1996 · N434MA · Swrngn SA227AC · Trailing Edge FlapsSDR MALA965069Door Frame · scuffedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE FORWARD CABIN DOOR FUSELAGE FRAME FS 133.87, P/N 27-22126, HAD SCUFF MARKS APPROX .016 INCH DEEP AT LOWER TEFLON GUIDE PAD CONTACT AREA. FABRICATED AND INSTALLED REPAIR PLATE, 'REPLACEABLE WEAR PLATJul 10, 1996 · N434MA · Swrngn SA227AC · Fuselage Miscellaneous StructureSDR MALA965063Mechanism · out of adjustFLT 3049 - EN ROUTE FROM LNK, THE CARGO DOOR WARNING LIGHT ILLUMINATED IN FLIGHT. THE AIRCRAFT RETURNED TO LNK. MAINTENANCE ADJUSTED THE CARGO DOOR ROD ENDS ON THE FORWARD BOTTOM BELLCRANK AND THE DOOR HANDLE POSITION SWITCH. ALL CHECKS SATISFACTORY. (M)Jul 6, 1996 · N434MA · Swrngn SA227AC · Cargo/Baggage DoorsSDR MALA964843Seal · out of adjustFLT NR 3354 - AFTER DEPARTURE FROM DTW, THE CREW NOTED A LOUD SQUEAL FROM THE PASSENGER DOOR. THE CREW ELECTED TO RETURN TO DTW AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL SHIMMED THE PASSENGER DOOR SEAL. ALL SYSTEMS OPERATED SATISFACTORJan 26, 1996 · N434MA · Swrngn SA227AC · Passenger/Crew DoorsSDR MALA954725Frame · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL NOTED A CRACK IN THE LOWER RIGHT BELT FRAME RELIEF RADIUS AT FS 242.27 AND WL 81.07 BELOW STRINGER NR 11. THE CRACK WAS REPAIRED BY STOP DRILLING IT AND FABRICATING AND INSTALLING A REPAIR DOUBLER IANov 24, 1995 · N434MA · Swrngn SA227AC · Fuselage Main, FrameSDR MALA954724Door · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND A CRACK IN THE LOWER AFT PASSENGER DOOR CORNER P/N 27-24044 AND WEAR IN THE LOWER AFT PASSENGER DOOR COVER, P/N 27-24150. THE COMPONENTS WERE REMOVED AND REPLACED WITH NEW IAW SRM 51-30-02, -04Nov 24, 1995 · N434MA · Swrngn SA227AC · Passenger/Crew DoorsSDR MALA954723Door · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND A CRACK IN THE LOWER FORWARD PASSENGER DOOR CORNER, P/N 27-24044 AND WEAR IN THE LOWER FORWARD PASSENGER DOOR COVER, P/N 27-24150. THE COMPONENTS WERE REMOVED AND REPLACED WITH NEW IN ACCORDANCNov 24, 1995 · N434MA · Swrngn SA227AC · Passenger/Crew DoorsSDR MALA954722Stiffener · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE PERSONNEL FOUND A CRACK IN THE CENTER CHANNEL AT BL 0.00 AND FS 254.52. THE CRACK WAS REPAIRED BY REPLACING THE CENTER STIFFENER (P/N 27-31110-031, 032) IAW SRM 157-90-30, REPAIRS NR 1 AND NR 2. (M)Nov 24, 1995 · N434MA · Swrngn SA227AC · Wing Miscellaneous StructureSDR MALA954705Cooling Turbine · seizedFLT NR 3434 - DURING TAXI AFTER LANDING, THE CREW NOTED SMOKE IN THE CABIN AND COCKPIT. THE CREW SHUT DOWN BOTH BLEEDS AND PROCEEDED TO THE GATE. MAINTENANCE PERSONNEL REPLACED THE LEFT COOLING TURBINE. ALL SYSTEMS OPERATED SATISFACTORILY. (M)Nov 9, 1995 · N434MA · Swrngn SA227AC · Cabin Temperature Control SystemSDR MALA954679Altimeter · failedFLT NR 3046 - ON CLIMB-OUT FROM DTW, THE CAPTAINS ALTIMETER BECAME INOPERATIVE. THE AIRCRAFT RETURNED TO DTW. MAINTENANCE REPLACED THE CAPTAINS ALTIMETER AND PURGED THE NR 1 AND NR 2 STATIC SYSTEMS. ALL SYSTEMS OPERATED SATISFACTORILY. (M)Oct 27, 1995 · N434MA · Swrngn SA227AC · Altimeter, Barometric/EncoderSDR MALA954677Position Sw · failedFLT NR 3087 - ON APPROACH IN MSP, THE LEFT GEAR INTRANSIT LIGHT REMAINED ILLUMINATED AFTER THE GEAR INDICATOR SHOWED IT TO BE DOWN AND LOCKED. THE CREW CYCLED THE GEAR AND ALL INDICATIONS WERE NORMAL. MAINTENANCE REPLACED THE LEFT INBOARD POSITION SWITCH, P/Oct 21, 1995 · N434MA · Swrngn SA227AC · Landing Gear Position and WarningSDR MALA954595Former · crackedMSP - DURING A SCHEDULED INSPECTION, THE LT INBD FORMER, PN 27-35025-067, AND STR, PN 27-35041-012, WERE FOUND CRACKED AT NACELLE STA 120.00. REPAIRS WERE COMPLETED BY FABRICATING AND INSTALLING REPAIR DOUBLERS IAW FAC LAR NR 95-MALA-225. (X)Aug 20, 1995 · N434MA · Swrngn SA227AC · Nacelle/Pylon StructureSDR MALA954579Switch · failedMSP - FLT 3027 - ON APPROACH, LT GEAR INTRANSIT LIGHT WAS VERY DIM WHEN ILLUMINATED DURING GEAR EXTENSION. THE INDICATION LIGHT ILLUMINATED NORMALLY WHEN TESTED. MAINTENANCE REPLACED THE LEFT INBOARD UPPER GEAR POSITION SWITCH. SYSTEM OPERATED SATISFACTORILAug 9, 1995 · N434MA · Swrngn SA227AC · Landing Gear Position and WarningSDR MALA954469Skin · birdstrikeDURING POSTFLIGHT INSPECTION IN FFM, THE CREW FOUND A DENT IN THE LEFT LEADING EDGE DUE TO A BIRDSTRIKE JUST INBOARD OF WS 131.899. THE AIRCRAFT WAS FERRIED TO MSP FOR REPAIR. MAINTENANCE REPAIRED THE LEADING EDGE BY INSTALLING A FILLER AND REPAIR DOUBLER IAMay 19, 1995 · N434MA · Swrngn SA227AC · Wing, Plate/SkinSDR MALA954436Doubler · wornDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE LEFT FLAP DOUBLER WORN. REPAIRS WERE COMPLETED BY REPLACING THE ROLLER DOUBLER, P/N 27-31141-001, IAW FAC SRM 51-00-00 PAGE 4. (W)Apr 30, 1995 · N434MA · Swrngn SA227AC · Trailing Edge FlapsSDR MALA954287Door Frame · crackedDURING A SCHEDULED INSPECTION IN MSP, MAINTENANCE FOUND THE FUSELAGE CARGO DOOR FRAME CRACKED AT THE GAS SPRING BOLT MOUNTING HOLE. REPAIRS WERE COMPLETED THROUGH INSTALLATION OF A REPAIR DOUBLER IAW FAC LAR 95-MALA-042 AND FAC 51-00-00 STANDARD PRACTICES. (Feb 5, 1995 · N434MA · Swrngn SA227AC · Fuselage Miscellaneous StructureSDR MALA954270Compressor Seal · leakingMSP - FLT 3306 - IN CRUISE FLIGHT, CREW NOTED AN UNPLEASANT SMELL WHILE THE AIRCRAFT WAS PRESSURIZED. THE AIRCRAFT CONTINUED TO MSP WITHOUT INCIDENT. MAINTENANCE REPLACED LT ENGINE COMPRESSOR SEAL. SYSTEM OPERATED SATISFACTORILY. (X)Jan 21, 1995 · N434MA · Swrngn SA227AC · Turbine Engine Compressor SectionSDR MALA954232Pitot System · req'd serviceFLT NR 3094 - ON CLIMB-OUT FROM DTW, THE CAPTAINS AIRSPEED INDICATOR BEGAN TO DROP. DURING THE CLIMB THE FIRST OFFICERS AIRSPEED INDICATOR ALSO BEGAN TO DROP. THE CREW SELECTED PITOT HEAT ONLY ON BOTH SIDES AND BOTH AIRSPEEDS CAME BACK TO NORMAL. THE AIRCRAJan 6, 1995 · N434MA · Swrngn SA227AC · Pitot/Static System
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