N280AS, cancelled Sep 2, 2009

Service difficulty reports · 40

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 = 'N280AS' AND deregistration_id = 'N280AS-2009-09-02'
  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 GUUA05190801Relay · shortedFLIGHT: 9148, UPON STARTING, RT ENGINE, AFTER SELECTING THE START SWITCH TO START, A LOUD SIZZLE CAME FROM THE FIRST OFFICERS SIDE PANEL, ALONG WITH A SMALL FLAME AND SMOKE. DETERMINED THAT AIRBORNE AUXILIARY POWER UNIT RELAY BOX AT FIRST OFFICERS SIDE PANEL May 19, 2008 · N280AS · Emb EMB120ER · Electrical Power System WiringSDR GUUA05120801Light · inoperativeDURING SCHEDULED ROUTINE MAINTENANCE, DISCOVERED LT AFT EMERGENCY LIGHT INOPERATIVE. REPLACED LT AFT EMERGENCY LIGHT ASSY.May 12, 2008 · N280AS · Emb EMB120ER · Emergency LightingSDR GUUA04210802Proximity Sensor · inoperativeFLIGHT 9138, AFTER TAKEOFF, LANDING GEAR SELECTED UP RT MAIN GREEN (A) LIGHT ILLUMINATED. CONTINUED TO FLL. DURING APPROACH, LANDING GEAR DID NOT EXTEND IN NORMAL MODE, USED ELECTRICAL OVERRIDE. REPLACED RT MLG (A) DOWNLOCK PROXIMITY SENSOR.Apr 21, 2008 · N280AS · Emb EMB120ER · Landing Gear Position and WarningSDR GUUA01070801Sign · missingFLIGHT: 1601 MIA/FLL ILLUMINATED EXIT SIGN MISSING BY SEAT 8F. INSTALLED NEW EXIT SIGN.Jan 7, 2008 · N280AS · Emb EMB120ER · Emergency LightingSDR GUUA06280701Bulb · brokenAT SCHEDULED MAINTENANCE, DISCOVERED LT AFT EMERGENCY LIGHT BULB BROKEN OFF IN SOCKET. REPLACED LT AFT EMERGENCY LIGHT ASSEMBLY.Jun 28, 2007 · N280AS · Emb EMB120ER · Emergency LightingSDR GUUA06250702Wire Harness · damagedFLIGHT 9231, DURING FLIGHT BOTH (B) LANDING GEAR LIGHTS FOR NOSE WHEEL ILLUMINATED. REMOVED INSPECTED AND REINSTALLED LANDING GEAR PROXIMITY HARNESS.Jun 25, 2007 · N280AS · Emb EMB120ER · Landing Gear System WiringSDR GUUA06020702Unknown · odorSTRONG ODOR OF JET A WHEN APU FIRST STARTED. INSPECTED APU FOR LEAKS, NO LEAKS NOTED. INSPECTED BLEED CONNECTIONS, ALL ARE SECURE. OPS CHECK NORMAL. NO DEFECTS NOTED.Jun 2, 2007 · N280AS · Emb EMB120ER · Air Distribution SystemSDR GUUA05310701Unknown · odorDURING APU START WITH BOTH ENGINES RUNNING A STRONG ODOR OF JET A ENTERS THE CABIN AND COCKPIT. THIS HAPPENS AT THE END OF THE START SEQUENCE AFTER THE GEN TURNS ON. CHECKED ENGINE AND APU, NO LEAKS NOTED. STARTED APU. OPS CHECK NORMAL.May 31, 2007 · N280AS · Emb EMB120ER · Air Distribution SystemSDR GUUA04070701Unknown · unknownFLIGHT: 0253, DURING FINAL APPROACH FLIGHT CONTROLS WILL NOT PERMIT RT AILERON INPUT. INSPECTED LT AILERON CONTROL SURFACE REMOVED PANELS AND INSPECTED CABLES, PULLEYS, BEARING ATTACHMENTS ALSO INSPECTED AILERON CONTROL QUADRANTS UNDER THE FLOOR FOR LOOSE ITEApr 7, 2007 · N280AS · Emb EMB120ER · Aileron Control SystemSDR GUUA11020603Battery Pack · inoperativeFLIGHT:5202 FLL/FLL EMERGENCY LIGHTS LOWER LT SIDE INOPERATIVE. REPLACED MID BATTERY PACK OPERATIONAL CHECK NORMAL.Nov 2, 2006 · N280AS · Emb EMB120ER · Emergency LightingSDR GUUA11020602Battery Pack · inoperativeFLIGHT:5202 FLL/FLL EMERGENCY EXIT LIGHTS INOPERATIVE LOWER RT SIDE. REPLACED AFT BATTERY PACK OPERATIONAL CHECK NORMAL.Nov 2, 2006 · N280AS · Emb EMB120ER · Emergency LightingSDR GUUA08250601Wire Harness · damagedFLIGHT: 9307 FPO/FLL DURING FLIGHT LT MAIN GEAR GREEN (A) ANNUNCIATOR ILLUMINATED. UPON ARRIVAL AT FLL LANDING GEAR SELECTED DOWN RED (A) AND (B) ANNUNCIATORS ILLUMINATED EXCEPT LT MAIN GEAR GREEN (A) ANNUNCIATOR. PERFORMED ALTERNATE LANDING GEAR EXTENSION. Aug 25, 2006 · N280AS · Emb EMB120ER · Landing Gear System WiringSDR GUUA07270601Actuator · out of adjustFLIGHT: 9143 FLL/GGT DURING APPROACH THE LT MAIN LANDING GEAR WOUILD NOT INDICATE DOWN AND LOCKED ELECTRICAL OVERIDE SWITCH GAVE A GREEN INDICATION. ADJUSTED THE LT MAIN LANDING GEAR ACTUATOR OPERATIONAL CHECK NORMAL. TEST FLIGHT SATISFACTORY.Jul 27, 2006 · N280AS · Emb EMB120ER · Landing Gear ActuatorSDR GUUA07250601Spring · unknownDURING APPROACH, LT MAIN LANDING GEAR WOULD NOT INDICATE DOWN AND LOCKED AFTER SEVERAL ATTEMPTS TO RECYCLE THE ELECTRICAL OVERRIDE SWITCH USED. REPLACED LT MAIN GEAR ACTUATOR SPRING LANDING GEAR OPERATIONAL CHECK GOOD. TEST FLIGHT SATISFACTORY.Jul 25, 2006 · N280AS · Emb EMB120ER · Landing Gear Position and WarningSDR GUUS07240601Proximity Sensor · out of adjustFLIGHT:9230 FLL/NAS DURING APPROACH LT LANDING GEAR WOULD NOT SHOW DOWN AND LOCKED AFTER SEVERAL ATTEMPTS OF RECYCLING THE LANDING GEAR HANDLE. THE ELECTRICAL OVERRIDE FINALLY WORKED LANDED WITHOUT INCIDENT, MAINTENANCE FERRY TO FLL. ADJUSTED THE LEFT GEAR Jul 24, 2006 · N280AS · Emb EMB120ER · Landing Gear Position and WarningSDR GUUA06080601Wire Harness · failedFLIGHT:9254 FLL/GHB AFTER TAKEOFF LEFT LANDING GEAR -B- LOOP LIGHT REMAINS ILLUMINATED AFTER LANDING GEAR IS RETRACTED. REPLACED LEFT DOWNLOCK PROXIMITY HARNESS.Jun 8, 2006 · N280AS · Emb EMB120ER · Landing Gear System WiringSDR GUUA03230601Hmu · shortedFLIGHT: 9202 FLL/ELH, AFTER TAKEOFF LOST TORQUE ON THE RIGHT ENGINE TORQUE WENT FROM 70 PERCENT TO 0 PERCENT. RETURNED TO FLL LANDED WITHOUT INCIDENT. REPLACED RIGHT HYDO MECHANICAL UNIT.Mar 23, 2006 · N280AS · Emb EMB120ER · Fuel Controlling SystemSDR GUUA03220601Connector · dirtyFLIGHT: 9126 FLL/NAS, AFTER TAKEOFF RIGHT ENGINE LOST TORQUE WENT FROM 80 PERCENT TO 20 PERCENT TORQUE. RETURNED TO FLL LANDED WITHOUT INCIDENT. CLEANED CONNECTORS AND CHARACTERIZATION PLUGS ON THE TORQUE SIGNAL CONDITION UNIT.Mar 22, 2006 · N280AS · Emb EMB120ER · Turbine Engine System WiringSDR GUUA03160601Arm · wornFLIGHT: 9230 FLL/NAS, AFTER TAKEOFF LEFT AIRCONDITION PACK FAIL ILLUMINATED CREW NOTICED AN OILY SMELL FROM PACKS RETURNED TO FLL LANDED WITHOUT INCIDENT. REPLACED LEFT RAM AIR DOOR ARM.Mar 16, 2006 · N280AS · Emb EMB120ER · Cabin Compressor SystemSDR GUUA03150601Fan · inoperativeAFTER TAKEOFF FLIGHT ATTENDANT NOTIFIED CAPTAIN OF SMOKE IN THE CABIN. A MOMENT LATER HAZE AND A SMELL OF SMOKE CAME INTO THE COCKPIT. DECLARED AN EMERGENCY, RETURNED TO MIA. OXYGEN MASK WERE NOT DEPLOYED, LANDED WITHOUT INCIDENT. INSPECTED THE AIR DISTRIBMar 15, 2006 · N280AS · Emb EMB120ER · Air Distribution FanSDR GUUA03100601Hose · looseAFTER TAKEOFF LEFT PACK FAILED, NOTICED A BAD ODOR. RESECURED LOOSE HOSE ON AIR CYCLE MACHINE.Mar 10, 2006 · N280AS · Emb EMB120ER · Cabin Cooling SystemSDR GUUA02230601Odor · detectedDURING DESCENT BURNED ODOR FROM AIR CONDITIONING CAUSED SMOKE ALARM IN TOILET TO SOUND. RAN LEFT AND RIGHT PACKS WITH ENGINES RUNNING, COULD NOT DUPLICATE.Feb 23, 2006 · N280AS · Emb EMB120ER · Cabin Cooling SystemSDR GUUA02080603Pressure Switch · leakingDURING CLIMB RIGHT AIR CONDITION PACK STUCK IN THE HEAT SETTING. CREW NOTICED OVERHEAT ODOR. RETURNED TO NAS. REPLACED APU OIL PRESSURE SWITCH.Feb 8, 2006 · N280AS · Emb EMB120ER · Airborne Auxiliary Power Unit (APU) SystemSDR GUU2005F00046Socket · inoperativeON POST FLIGHT, EMERGENCY FLOOR TRACK LIGHT AT TROW 9A WAS INOPERATIVE. REPOSITIONED BULB IN SOCKET. (K)Aug 30, 2005 · N280AS · Emb EMB120ER · Emergency LightingSDR GUU2005F00029Engine · overservicedAFTER TAKEOFF, MAIN HYDRAULIC PUMP PRESSURE LIGHT ILLUMINATED. NOTICED A SMELL AND SMOKE ENTERED THE COCKPIT AND CABIN. RETURNED AND LANDED WITHOUT INCIDENT. DETERMINED RT ENGINE TO BE OVERSERVICED. SERVICED TO PROPER LEVEL. OPERATIONAL CHECKS OF BOTH COOJul 4, 2005 · N280AS · Emb EMB120ER · Turbine Engine Oil SystemSDR GUU2005F00027Fuse · failedEMERGENCY FLOOR LIGHTING IN FRONT OF THE GALLEY, INOPERATIVE. REMOVED AND REPLACED EMERGENCY FLOOR LIGHT FUSE. (K)Jun 9, 2005 · N280AS · Emb EMB120ER · Emergency LightingSDR GUU2005F00025Odor · detectedDURING FLIGHT, OIL SMELL ODOR WITH A FOG APPEARANCE IN COCKPIT WITH ENGINE BLEEDS ON. RETURNED TO DEPARTURE. INSPECTED AIRCRAFT, DO DISCREPANCIES FOUND. RAN ENGINE. OPERATIONAL CHECKS NORMAL. (K)Jun 4, 2005 · N280AS · Emb EMB120ER · Air Distribution SystemSDR ASOA03055Window Post · crackedDURING A HANGAR CHECK IN TXK, THE LT DIRECT VISUAL WINDOW POST SKIN AT THE LOWER TRAILING EDGE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CRACKED SKIN IAW ASA EO 120-53-0119A. (M)Feb 12, 2003 · N280AS · Emb EMB120RT · Fuselage Main, StructureSDR ASOA02440Seat · out of positionDURING HANGAR INSPECTION IN MCN, THE EMERGENCY EXIT DOORS AT ROWS 5 AND 8 WERE INHIBITED FROM OPENING. MAINTENANCE FOUND THE EXIT AT ROW 5 WAS OPENING AGAINST THE SEAT BACK AT ROW 4A. MAINTENANCE REPOSITIONED THE SEAT FOR SUFFICIENT CLEARANCE OF THE EXIT DOOAug 4, 2002 · N280AS · Emb EMB120RT · Passenger Compartment EquipmentSDR ASOA02139Bulb · burned outFLT 4903 - DURING GROUND INSPECTION IN DFW, THE CREW REPORTED THAT THE RED FLOOR EMERGENCY LIGHT NEAR THE AIRSTAIR DOOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT FLOOR EMERGENCY LIGHT BULB. OPERATIONAL CHECKS NORMAL. AIRCRAFT OK FOR SMar 6, 2002 · N280AS · Emb EMB120RT · Emergency LightingSDR ASOA01239Stringer · corrodedDURING C-CHECK INSPECTION IN BNA, CORROSION WAS DISCOVERED ON STRINGER 20 RIGHT BETWEEN FRAMES 14 AND 15. MAINTENANCE REMOVED CORROSION IAW CPM 51-14-00. THE DAMAGED SECTION OF THE STRINGER WAS REMOVED. A NEW SECTION OF STRINGER WAS CUT AND DRILLED IAW SRM Nov 11, 2001 · N280AS · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR ASOA01240Stringer · corrodedDURING C-CHECK INSPECTION IN BNA, STRINGER 18 RIGHT WAS FOUND TO BE CORRODED BETWEEN FRAMES 14 AND 16. MAINTENANCE REMOVED CORROSION IAW CPM 51-14-00. THE DAMAGED SECTION OF THE STRINGER WAS REMOVED. A NEW SECTION OF STRINGER WAS CUT AND DRILLED IAW SRM 51-Nov 10, 2001 · N280AS · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR ASOA01233Skin · corrodedDURING C-CHECK INSPECTION IN BNA, THE LOWER FUSELAGE WAS FOUND CORRODED ON THE EXTERNAL SKIN BETWEEN FRAMES 7 AND 8 WHERE THE DME ANTENNA MOUNTS BETWEEN STRINGERS 21 LEFT AND 21 RIGHT. MAINTENANCE REMOVED CORROSION IAW CPM 51-14-00. A NEW INSIDE DOUBLER WAS Nov 10, 2001 · N280AS · Emb EMB120RT · Fuselage Main, Plate/SkinSDR ASOA01232Seat Track · corrodedDURING C-CHECK INSPECTION IN BNA, THE RIGHT FLOOR SEAT TRACK, CENTER SECTION, WAS FOUND CORRODED BETWEEN FRAMES 24 AND 32. MAINTENANCE REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW CPM 51-14-00. THE SEAT TRACK WAS REMOVED IAW SRM 51-40-02. A NEW SEAT TRACNov 10, 2001 · N280AS · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR ASOA01231Seat Track · corrodedDURING C-CHECK INSPECTION IN BNA, THE LEFT FLOOR SEAT TRACK, CENTER SECTION, WAS FOUND CORRODED BETWEEN FRAMES 22 AND 32. MAINTENANCE REMOVED THE SEAT TRACK IAW SRM 51-40-2. A NEW SEAT TRACK WAS LOCATED AND DRILLED IAW SRM 51-25-00 AND 51-40-6. AIRCRAFT WINov 10, 2001 · N280AS · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR ASOA01054Unknown · odorFLT 4327 - IN CRUISE FROM ATL TO EVV, CAPTAIN REPORTED SMELL OF BURNING MATCHES, TWICE AT 18,000 FT AND ONCE AFTER LEFT ENGINE WAS SECURED ON TAXI INTO EVV. EACH TIME THE SMELL LASTED BETWEEN 5-10 SECONDS AND LOCATION COULD NOT BE ISOLATED. MX PERFORMED VISUMay 13, 2001 · N280AS · Emb EMB120 · Air Distribution SystemSDR ASOA00039Stringer · corrodedDURING INSPECTION, FOUND A STRINGER ON THE BELLY OF THE AIRCRAFT CORRODED. ATL MAINTENANCE REPLACED CORRODED STRINGER IAW EMB120 SRM 53-20-03. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)Apr 26, 2000 · N280AS · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR 20000424SH005Frame · crackedFLUORESCENT PENETRANT INSPECTION INDICATED CRACKS IN LT NACELLE FORWARD NR 1 FRAME. POSSIBLE CAUSE IS STILL UNDETERMINED. SUBMITTER SUSPECTED ENGINE TORQUE AND VIBRATION TO BE POSSIBLE CONTRIBUTING FACTORS. (X)Mar 20, 2000 · N280AS · Emb EMB120RT · Nacelle/Pylon, Main FrameSDR 20000424SH004Frame · crackedFLUORESCENT PENETRANT INSPECTION INDICATED CRACKS IN RT NACELLE FORWARD NR 1 FRAME. POSSIBLE CAUSE IS STILL UNDETERMINED. WOULD SUSPECT ENGINE TORQUE AND VIBRATION TO BE POSSIBLE CONTRIBUTING FACTORS. (X)Mar 20, 2000 · N280AS · Emb EMB120RT · Nacelle/Pylon, Main FrameSDR ASOA99027Controller · defectiveEN ROUTE ATL-FLO, AT 19,000 FEET, CABIN STARTED TO CLIMB AT 2,000 FPM. CREW PERFORMED DECOMPRESSION CHECKLIST AND DESCENDED TO 10,000 FEET. OXYGEN MASKS WERE NOT DEPLOYED AS CABIN NEVER EXCEEDED 10,500 FEET. FLIGHT CONTINUED TO FLO, PRESSURE WAS CONTROLLED INFeb 19, 1999 · N280AS · Emb EMB120RT · Cabin Pressure Controller
Back to N280AS, cancelled Sep 2, 2009