N159A, cancelled Oct 24, 2007

Service difficulty reports · 54

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 = 'N159A' AND deregistration_id = 'N159A-2007-10-24'
  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 COMA0010042Actuator · failedFLAP ANNUNCIATOR CONTROL FAULT APPEARED ON TAKEOFF ROLL. REMOVED LEFT INBOARD FLAP ACTUATOR AND INSTALLED A SERVICEABLE ONE.Mar 27, 2000 · N159A · Emb EMB120RT · Trailing Edge Flap ActuatorSDR COMA0010041Actuator · leakingFOUND RIGHT INBOARD FLAP ACTUATOR LEAKING. REMOVED AND REPLACED RIGHT INBOARD FLAP ACTUATOR. AIRCRAFT RETURNED TO SERVICE.Mar 27, 2000 · N159A · Emb EMB120RT · Trailing Edge Flap ActuatorSDR COMA0010046Actuator · malfunctionedFLAP CONTROL FAULT DURING T/O. REPLACED THE LEFT HAND INBOARD FLAP ACTUATOR.Mar 26, 2000 · N159A · Emb EMB120RT · Trailing Edge Flap ActuatorSDR COMA0010038Annunciator · malfunctionedFLAP CONTROL FAULT WARNING DURING TAKEOFF. REPLACED THE FLAP ANNUNCIATOR PANEL.Mar 15, 2000 · N159A · Emb EMB120RT · Trailing Edge Flap Control SystemSDR COMA0010029Control Unit · malfunctionedFLAP CONTROL FAULT. REPLACED THE FLAP CONTROL UNIT.Feb 22, 2000 · N159A · Emb EMB120RT · Trailing Edge Flap Control SystemSDR COMA0010012Switch · failedMASTER WARNING LIGHT ON. WILL NOT CANCEL. ADJUSTED THE FUEL SERVICE DOOR SWITCHES.Jan 24, 2000 · N159A · Emb EMB120RT · Door Warning SystemSDR COMA0010002Flap · malfunctionedFLAP CONTROL FAULT DURING TAKEOFF. COULD NOT DUPLICATE, NO FAULTS FOUND IN FLAP SYSTEM.Jan 3, 2000 · N159A · Emb EMB120RT · Trailing Edge Flap Control SystemSDR COMA9910146Annunciator · failedTAKEOFF WAS ABORTED DUE TO MULTIPLE ERRATIC WARNINGS ON ANNUNCIATOR. REPLACED THE ANNUNCIATOR PANEL ASSEMBLY.Sep 10, 1999 · N159A · Emb EMB120RT · Central DisplaySDR COMA9910145Warning · activatedFLAP CONTROL FAULT WARNING. COULD NOT DUPLICATE. SYSTEM TEST WAS NORMAL.Sep 7, 1999 · N159A · Emb EMB120RT · Trailing Flap Position Indicating SystemSDR COMA9910096Battery · dischargedEMERGENCY LIGHTS ARE INOPERABLE. REPLACED EMERGENCY BATTERIES.Jun 21, 1999 · N159A · Emb EMB120RT · Emergency LightingSDR COMA9910083Indicator · malfunctionCOPILOTS AIR SPEED INDICATOR STUCK AT 100 KTS. REPLACED AIRSPEED INDICATOR.May 23, 1999 · N159A · Emb EMB120RT · Airspeed/Mach IndicatorSDR COMA9910029Warning · malfunctionedFLAP CONTROL FAULT WARNING DURING TAKEOFF. COULD NOT DUPLICATE, OPERATIONAL CHECK OF FLAP SYSTEM WAS NORMAL.Feb 2, 1999 · N159A · Emb EMB120RT · Trailing Edge Flap Control SystemSDR COMA9910018Guide · corrodedDURING ROUTINE MAINTENANCE, THE UPPER CABLE GUIDE FITTING ON THE CARGO DOOR WAS FOUND TO HAVE SEVERE EXFOLIATION CORROSION. CORROSION WAS APPROX .1875 IN DEPTH OVER AN AREA OF 1X .50. THE FITTING WAS REPLACED WITH A SERVICEABLE FITTING AS PER EMB MAINTENANCEJan 19, 1999 · N159A · Emb EMB120RT · Cargo/Baggage DoorsSDR COMA9810286Relay · malfunctionEMERGENCY LIGHTS WILL NOT TURN OFF. REPLACED RELAY KO201.Dec 20, 1998 · N159A · Emb EMB120RT · Emergency LightingSDR COMA9810275Control · malfunctionedFLAP CONTROL FAULT DURING TAKEOFF. CANNOT DUPLICATE DISCREPANCY. C/W SERVICE BULLETIN 120-027-0067 FOR TROUBLESHOOTING.Nov 28, 1998 · N159A · Emb EMB120RT · Trailing Edge Flap Control SystemSDR COMA9810263Lamp · failedONE EMERGENCY LIGHT IS INOPERABLE. REPLACED LIGHT BULB.Nov 14, 1998 · N159A · Emb EMB120RT · Emergency LightingSDR COMA9810036Fan · failedAT CRUISE FLIGHT THE COCKPIT AND CABIN STARTED FILLING UP WITH SMOKE. CREW DESCENDED FROM 17,000 FT AND MADE UNSCHEDULED LANDING. FOUND RIGHT RECIRCULATION FAN TO BE FAULTY. REMOVED AND REPLACED FAN.Feb 2, 1998 · N159A · Emb EMB120RT · Air Distribution FanSDR COMA9710413Stator · crackedDURING TEARDOWN OF BRAKE ASSY P/N 2-1585, THE ACCESSORY SHOP FOUND THE NUMBER ONE STATOR CRACKED. OVERHAULED BRAKE.Sep 23, 1997 · N159A · Emb EMB120RT · BrakeSDR COMA9710412Stator · crackedDURING TEAR DOWN OF BRAKE ASSY P/N 2-1585, THE ACCESSORY SHOP FOUND THE NUMBER ONE STATOR CRACKED. OVERHAULED BRAKE.Sep 23, 1997 · N159A · Emb EMB120RT · BrakeSDR COMA9710319Propeller · damagedRT PROPELLER STRUCK GROUND EQUIPMENT DURING TAXI OPERATION. REPLACED THE RT PROPELLER AND ENGINE.Jun 24, 1997 · N159A · Emb EMB120RT · Propeller AssemblySDR COMA9710307Control Module · failedLANDING GEAR DID NOT RETRACT WHEN SELECTED UP. REPLACED THE LANDING GEAR CONTROL MODULE.Jun 9, 1997 · N159A · Emb EMB120RT · Landing Gear SelectorSDR COMA9710165Skin · dentedDURING INSPECTION, FOUND A DENT IN THE RIGHT WING LOWER SKIN BETWEEN RIBS 24 AND 25 AFT OF THE AUXILIARY SPAR. CUT OUT DENT AND INSTALLED A FILLER OF THE SAME THICKNESS, INSTALLED AN INTERNAL DOUBLER MADE OF 0.040 INCH 2024-T3 AND AN EXTERNAL DOUBLER MADE OF Mar 3, 1997 · N159A · Emb EMB120RT · Wing, Plate/SkinSDR COMA9710151Relay · inoperativeRIGHT HAND PROPELLER AUTO FEATHER SYSTEM DOES NOT TEST. REPLACED RELAY K0039, SYSTEM TEST NORMAL.Feb 15, 1997 · N159A · Emb EMB120RT · Propeller Feathering/ReversingSDR COMA9710149Skin · corrodedON 2C INSPECTION, THE LOWER FUSELAGE SKIN WAS FOUND CORRODED UNDER THE TITANIUM STRAP AT FRAME 21, BETWEEN STRINGERS 19L AND 20L. THE SKIN WAS REPAIRED PER SRM 53-00-01, FIGURE 202.Feb 12, 1997 · N159A · Emb EMB120RT · Fuselage Main, Plate/SkinSDR COMA9710148Skin · corrodedON 2C INSPECTION, THE LOWER FUSELAGE SKIN WAS FOUND CORRODED UNDER TITANIUM STRAP AT FRAME 23, BETWEEN STRINGERS 20R AND 21R. THE SKIN WAS REPAIRED PER AERODESIGN REPORT NR 1896-1, REV A, DATED 2-7-97.Feb 12, 1997 · N159A · Emb EMB120RT · Fuselage Main, Plate/SkinSDR COMA9710147Sill · corrodedON 2C INSPECTION, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT SILL WAS FOUND CORRODED. REPLACED WITH A NEW PART PER SRM 51 STANDARD PRACTICES.Feb 12, 1997 · N159A · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710146Crossbeam · corrodedON 2C INSPECTION, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT CROSSBEAM WAS FOUND CORRODED. REPLACED WITH A NEW PART PER SRM 51 STANDARD PRACTICES.Feb 12, 1997 · N159A · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710145Butt Strap · corrodedON 2C INSPECTION, THE FUSELAGE FLOOR SUPPORT STRUCTURE LT BUTT-STRAP WAS FOUND CORRODED. REPLACED WITH A NEW PART PER SRM 51 STANDARD PRACTICES.Feb 12, 1997 · N159A · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710144Butt Strap · corrodedON 2C INSPECTION, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT BUTT-STRAP WAS FOUND CORRODED. REPLACED WITH A NEW PART PER SRM 51 STANDARD PRACTICES.Feb 12, 1997 · N159A · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710143Butt Strap · corrodedON 2C INSPECTION, THE FUSELAGE FLOOR SUPPORT STRUCTURE RT BUTT STRAP WAS FOUND CORRODED. REPLACED WITH A NEW PART PER SRM 51 STANDARD PRACTICES.Feb 12, 1997 · N159A · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710142Omega Beam · corrodedON 2C INSPECTION, THE FUSELAGE FLOOR SUPPORT STRUCTURE LT OMEGA BEAM WAS FOUND CORRODED. REPLACED WITH A NEW PART PER SRM 51 STANDARD PRACTICES.Feb 12, 1997 · N159A · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710141Supporting Sect · corrodedON 2C INSPECTION, THE FWD SECTION RT SIDEWALL SEAT TRACK SUPPORTING SECTION WAS FOUND CORRODED. REPLACED WITH A NEW PART PER SRM CHAPT 51 STANDARD PRACTICES.Feb 12, 1997 · N159A · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710140Supporting Sect · corrodedON 2C INSPECTION, THE AFT SECTION RT SIDEWALL SEAT TRACK SUPPORTING SECTION WAS FOUND CORRODED. REPLACED WITH A NEW PART PER SRM CHAPT 51 STANDARD PRACTICES.Feb 12, 1997 · N159A · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710139Butt Strap · corrodedON 2C INSPECTION, THE FUSLEAGE FLOOR SUPPORT STRUCTURE CENTER BUTT STRAP WAS FOUND CORRODED. REPLACED WITH A NEW PART PER SRM 51 STANDARD PRACTICES AND AERODESIGN REPORT NR 1671-1, REV IR, DATED 10-22-95.Feb 12, 1997 · N159A · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710138Angle · corrodedON 2C INSPECTION, THE FUSELAGE FLOOR SUPPORT STRUCTURE Z-ANGLE WAS FOUND CORRODED. REPLACED WITH A NEW PART PER SRM 51 STANDARD PRACTICES.Feb 12, 1997 · N159A · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710137Angle · corrodedON 2C INSPECTION, THE AFT RIGHT EMERGENCY EXIT LOWER GUIDE PIN RECEPTACLES ON FUSELAGE AND THE LOWER ANGLE THEY'RE ATTACHED TO WERE FOUND CORRODED. THE LOWER ANGLE AND BOTH RECEPTACLES WERE REPLACED PER SRM CHAPT 51 STANDARD PRACTICES.Feb 12, 1997 · N159A · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710136Skin · corrodedON 2C INSPECTION, THE FUSELAGE PASSENGER DOOR SURROUND STRUCTURE INNER SKIN WAS FOUND CORRODED BETWEEN FRAMES 15 AND 15A, JUST ABOVE STRINGER 17L. AN EXTERNAL DOUBLER REPAIR WAS INSTALLED PER AERODESIGN REPORT NR 2118-2, REV IR, DATED 2-8-97.Feb 12, 1997 · N159A · Emb EMB120RT · Fuselage Main, Plate/SkinSDR COMA9710135Skin · gougedON 2C CHECK, THE CARGO DOOR OUTER SKIN WAS FOUND GOUGED ALONG THE TOP EDGE BY CONTACTING THE FUSELAGE FIXED STOPS DURING DOOR OPENING AND CLOSING. THE SKIN WAS REPAIRED PER SRM 52-30-01, PG 201 TO 203.Feb 12, 1997 · N159A · Emb EMB120RT · Cargo/Baggage DoorsSDR COMA9610268Actuator · malfunctionFLAP ASYMMETRY WARNING WHEN FLAPS SELECTED TO 25 DEGREES. REPLACED THE RT INBD FLAP ACTUATOR.Aug 29, 1996 · N159A · Emb EMB120RT · Trailing Edge Flap ActuatorSDR COMA9610255Fuel Hose · leakingRT ENGINE IS LEAKING FUEL. REPLACED LEAKING PRIMARY FLOW HOSE ASSY.Aug 21, 1996 · N159A · Emb EMB120RT · Engine Fuel DistributionSDR COMA9610254Prop Blade · crackedRT PROPELLER, NR 1 BLADE IS CRACKED NEAR THE TIP AT TWO PLACES. REMOVED AND REPLACED THE NR 1 BLADE ASSY.Aug 20, 1996 · N159A · Emb EMB120RT · Propeller Blade SectionSDR COMA9610185Hyd Pump · failedLEFT ENGINE DRIVEN HYDRAULIC PUMP FAILED. REPLACED HYDRAULIC PUMP.Jun 19, 1996 · N159A · Emb EMB120RT · Hydraulic Pump (Electric/Engine), MainSDR COMA9610183Connector · defectiveLEFT ENGINE LOW HYDRAULIC PRESSURE WARNING DURING CLIMB. REPAIRED WIRING CONNECTOR JO807 IN LT ENGINE NACELLE.Jun 17, 1996 · N159A · Emb EMB120RT · Hydraulic Pressure IndicatorSDR COMA9610176Wow Sensor · failedLANDING GEAR HANDLE COULD NOT BE SELECTED TO UP POSITION. REPLACED THE RT MLG, WEIGHT ON WHEELS PROXIMITY SENSOR.Jun 11, 1996 · N159A · Emb EMB120RT · Landing Gear Position and WarningSDR COMA9610153Skin · corrodedSEVERE CORROSION WAS FOUND DURING INSPECTION ON THE LOWER FUSELAGE SKIN AT FRAME 22 BETWEEN STRINGERS 21R AND 20R. THE CORROSION IS WHERE THE SKIN CONTACTS THE TITANIUM REINFORCING STRAP P/N 120-22409-001. THE DAMAGED AREA WAS REMOVED AND A REPAIR INSTALLED May 24, 1996 · N159A · Emb EMB120RT · Fuselage Main, Plate/SkinSDR COMA9610122Actuator · malfunctionFLAP DISAGREEMENT WARNING. INBD FLAPS INDICATE 5 DEGREES DOWN WHEN SELECTED UP. REPLACED THE LT INBD FLAP ACTUATOR. PART TOTAL CYCLES, 7,272.Mar 31, 1996 · N159A · Emb EMB120RT · Trailing Edge Flap ActuatorSDR COMA9610111Brake · wornLEFT ANTI-SKID INOP WARNING DURING LANDING. LT MLG OUTBD TIRE FOUND FLAT DURING POST FLIGHT. REPLACED THE LT MLG OUTBD BRAKE ASSY.Mar 22, 1996 · N159A · Emb EMB120RT · BrakeSDR COMA9511985Battery · dischargedBACKUP BATTERY DOES NOT TEST. REPLACED THE EMERGENCY POWER SUPPLY BATTERY.Oct 9, 1995 · N159A · Emb EMB120RT · Battery/Charger SystemSDR COMA9511962Bracket · crackedTHE CARGO DOOR LIFTING MECHANISM TORSION BAR FORWARD SUPPORT ATTACH BRACKET WAS FOUND CRACKED. THE BRACKET WAS REPLACED WITH SUBSTITUTE PART OF THICKER MATERIAL (P/N 120-20235-005), PER AERODESIGN REPORT NR 1397-1, DATED 2-15-95.Sep 11, 1995 · N159A · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA1956Valve · stuckDURING FLIGHT, THE NR 1 ENGINE OIL PRESSURE DECREASED TO 52 PSI, ALONG WITH SOUND OF RELAYS CLICKING IN PILOTS SIDE PANEL. WHILE THE PROPELLER WAS IN FEATHER OIL PRESSURE RETURNED TO 60 PSI. REMOVED AND REPLACED THE P2.5 SWITCHING VALVE.Sep 1, 1995 · N159A · Emb EMB120RT · Engine Oil Pressure
Back to N159A, cancelled Oct 24, 2007