N130G, cancelled Dec 10, 2003

Service difficulty reports · 55

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 = 'N130G' AND deregistration_id = 'N130G-2003-12-10'
  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 SWIA972584Computer · malfunctionedWHEN AUTOPILOT IS ENGAGED ON CAPTAINS SIDE, THE YOKE AND AIRCRAFT OSCILLATE ON ROLL AXIS CONTINUOUSLY. YOKE ROLLS ABOUT 2 INCHES TRAVEL. REMOVED AND REPLACED NR 1 AHC85 PER MM 34-21-01. OPS CHECK GOOD PER MM 34-21-00. AUTOPILOT OPS CHECK GOOD PER MM 22-10-May 17, 2001 · N130G · Emb EMB120RT · Integrated Flight SystemSDR SWIA972578Control Box · malfunctionedAFTER SELECTING GEAR UP, ALL RED AND GREEN INDICATING LIGHTS REMAINED ILLUMINATED. FOLLOWED QRH AND RECYCLED LANDING GEAR WITH SAME RESULTS. RETURNED FOR LANDING. REMOVED AND REPLACED LANDING GEAR SOLENOID VALVE. REMOVED AND REPLACED LANDING GEAR CONTROL BOMay 16, 2001 · N130G · Emb EMB120RT · Landing Gear SelectorSDR SWIA972571Servo · failedCO-PILOT''''S AUTOPILOT SERVO FAILURE, AMBER A ANNUNCIATED, VIBRATION ASSOCIATED WITH FAILURE PRIOR TO SERVO FAILURE. EXECUTED QRW PROCEDURES, VIBRATION REMAINED. REMOVED AND REPLACED AILERON SERVO, IAW MM 22-10-09, OPS CHECK GOOD. P/N 622-5734-002, S/N ON Apr 22, 2001 · N130G · Emb EMB120RT · Autopilot Main ServoSDR SWIA972479Flap · malfunctionedOUTBOARD FLAPS DO NOT EXTEND PAST 35 DEGREES WHEN SELECTED TO 45 DEGREES. INSPECTED OUTBOARD FLAPS AND TRACK SYSTEM. ALL FOUND GOOD. CLEANED CONNECTORS AT BOTH LEFT AND RIGHT ACTUATORS. PERFORMED SEVERAL FUNCTIONAL CHECKS WITH NO FAULTS FOUND.Mar 26, 2001 · N130G · Emb EMB120RT · Trailing Edge Flap Control SystemSDR SWIA972432Control Panel · malfunctionedWITH GEAR DOWN, FLAP 25 DEGREES, FLIGHT CONTROLS GET STUCK WHILE ATTEMPTING TO ROLL TO THE RIGHT. CHECKED AILERONS. COULD NOT DUPLICATE PROBLEM. SUSPECT AUTOPILOT DID NOT DISENGAGE. INSTALLED SERVICEABLE APP-65A. OPS CHECK GOOD AT THIS TIME. P/N: 622-66Mar 9, 2001 · N130G · Emb EMB120RT · Flight ControllerSDR SWIA972316Warning Light · illuminatedTRIM AURAL WARNING WITH TRIM IN GREEN BAND AT TAKEOFF. ABORTED TAKEOFF. RESET AURAL WARNING COMPUTER. RAN AIRCRAFT WITH TRIM SET TO TAKEOFF. COULD NOT DUPLICATE. CYCLED TRIM OUT OF GREEN BAND FORWARD AND AFT. TRIM AURAL WARNING CHECKS GOOD. RAN TRIM THRJan 28, 2001 · N130G · Emb EMB120RT · Data Recorders (Flight/Maintenance)SDR SWIA972286Display · failedJUST AFTER ROTATION FIRST OFFICERS EADI FAILED. RETURNED TO SEA. INSTALLED SERVICEABLE RIGHT EADI. OPS CHECKS GOOD 34-23-01. S/N ON: 893, S/N OFF: 2674.Jan 18, 2001 · N130G · Emb EMB120RT · Attitude Gyro and Indicating SystemSDR SWIA972009Light · illuminatedABORTED TAKEOFF AT 90 - 100 KNOTS DUE TO FUEL LIGHT ON MAIN ANNUNCIATOR PANEL. DUE TO ABORT COULDN''T TELL WHICH SIDE HAD LOW FUEL PRESSURE. FOUND THE LEFT FUEL FILTER LIGHT WAS ILLUMINATING. REMOVED AND REPLACED LEFT LOW PRESS FUEL FILTER IAW MM 73-00-00.Oct 1, 2000 · N130G · Emb EMB120RT · Fuel Pressure IndicatingSDR SWIA971990Fcu · failedOUTBOARD PAIR OF FLAPS DID NOT EXTEND BEYOND 25 DEGREES TO 45 DEGREES (LAST 2 SEGMENTS) WHEN COMMANDED. DIVERTED TO RDD FROM CEC. RERACKED FLAP CONTROL UNIT. OPS CHECKS GOOD.Sep 22, 2000 · N130G · Emb EMB120RT · Trailing Edge Flap Control SystemSDR SWIA971964Altimeter · malfunctionedAT 2000 FT ON CAPTAINS ALTIMETER, FIRST OFFICERS ALTIMETER READS 2100 FT. AT 5000 FT ON CAPTAINS ALTIMETER FIRST OFFICERS READS 5200 FT, AT 8000 FT ON CAPTAINS ALTIMETER FIRST OFFICERS ALTIMETER READS 8250 FT AND AT 14000 FT FIRST OFFICERS READS 14300 FT. TRSep 7, 2000 · N130G · Emb EMB120RT · Altimeter, Barometric/EncoderSDR SWIA971925Sequence Valve · out of adjAFTER TAKEOFF, RIGHT MAIN GEAR WOULD NOT RETRACT. RETURNED TO PDX. FOUND RIGHT GEAR DOOR SEQUENCE VALVE OUT OF ADJUSTMENT. ADJUSTED PER MM 32-32-04. PERFORMED MULTIPLE GEAR SWINGS. OPS CHECKS GOOD.Aug 7, 2000 · N130G · Emb EMB120RT · Landing Gear Door Retract SectionSDR SWIA971710Dpu · failedCO-PILOT EHSI WENT BLANK IN FLIGHT. COULD NOT TRANSFER ANY NAVIGATION INFORMATION TO SCREEN. RETURN TO LAX, INSTALLED SERVICEABLE DPU 864 ON NR 2 SIDE. OPS CK GOOD, SN: 7059, SN OFF: 4381.Feb 25, 2000 · N130G · Emb EMB120RT · Integrated Flight SystemSDR SWIA971646Control Unit · malfunctionedON CLIMB-OUT, CONTROL FAULT APPEARED WITH FLAP HANDLE UP, OVERHEAD FLAP CONTROL PANEL INDICATED NAC WAS FULLY EXTENDED. CONTROL FAULT INITIALLY WOULD NOT RESET, RESET SUCCESSFUL PER QRH 3RD TRY. RETURNED TO PDX. REPLACED FLAP CONTROL UNIT IAW 270000 AND CLEJan 4, 2000 · N130G · Emb EMB120RT · Trailing Edge Flap Control SystemSDR SWIA971643Controller · malfunctionedCONTROL FAULT ILLUMINATED IN FLIGHT AND WOULD NOT CANCEL. FAULT CORRECTED ITSELF AFTER 5 MINUTES. RETURNED TO SEA. PERFORMED FUNCTIONAL TEST PER MM 275000. FUNCTIONAL TEST GOOD, NO DISCREPENCIES NOTED. UNABLE TO DUPLICATE PROBLEM.Jan 3, 2000 · N130G · Emb EMB120RT · Trailing Edge Flap Control SystemSDR SWIA971278Oil Syst · reqd serviceOIL PRESSURE 1 WARNING AT V1 AND INTERMITTENT PRESSURE DROPS DURING CLIMBOUT. RETURNED TO AIRPORT. VISUALLY INSPECTED LEFT ENGINE AND NO OIL LEAKS EVIDENT. INSPECTED FILTER BY PASS AND CHIP DETECTOR LIGHTS, CHECKS NORMAL. SERVICED ENGINE WITH 2 QUARTS EXXOOct 8, 1998 · N130G · Emb EMB120RT · Turbine Engine Oil SystemSDR SWIA971235Ahrs · out of adjustRECEIVED HEADING FLAG, RMI FLAG BOTH SIDES WITH GYRO PRECESSING ALL THE TIME INFLIGHT. RETURNED TO LAX. RE-ORIENTED NR 1 AND NR 2 AHRS IAW MM 34-00-00. OPERATED SYSTEM ON GROUND AND ALL CHECKS OK.Aug 3, 1998 · N130G · Emb EMB120RT · Integrated Flight SystemSDR COMA9810050Wheel · crackedMECHANIC REMOVED WHEEL ASSEMBLY FROM A/C DUE TO TIRE WAS FOUND FLAT. WHEEL SHOP INFLATED TIRE AND FOUND INBOARD HALF CRACKED AT BOTTOM OF KEY INSERT BOSS. WHEEL HALF (P/N 300-604-1) HAS BEEN REMOVED FROM SERVICE.Feb 26, 1998 · N130G · Emb EMB120RT · Wheel/Ski/FloatSDR COMA9710500Acm · failedLAV SMOKE DETECTOR ACTIVATED. CABIN FILLED WITH SMOKE. REPLACED THE LEFT AIR CYCLE MACHINE.Dec 19, 1997 · N130G · Emb EMB120RT · Cabin Cooling SystemSDR COMA9710499Sign · looseEMERGENCY EXIT SIGN AT ROW 5C IS LOOSE. REPLACED SIGN ASSY.Dec 17, 1997 · N130G · Emb EMB120RT · Emergency LightingSDR COMA9710476Sign · brokenEMERGENCY EXIT SIGN AT 5C BROKEN. REPLACED EXIT SIGN.Nov 16, 1997 · N130G · Emb EMB120RT · Emergency LightingSDR COMA9710244Safety Pin · not removedTHE RT MLG WOULD NOT RETRACT. REMOVED DOWN LOCK SAFETY PIN FROM LANDING GEAR.May 6, 1997 · N130G · Emb EMB120RT · Landing Gear Retraction/Extension SystemSDR COMA9710240Flap Warning · illuminatedFLAPS FAIL WARNING DURING TAKEOFF ROLL. INSPECTED FLAP SYSTEM, FOUND NO DEFECTS. COULD NOT DUPLICATE DISCREPANCY.May 3, 1997 · N130G · Emb EMB120RT · Trailing Flap Position Indicating SystemSDR COMA9710174Lead · brokenRT PROPELLER DE-ICE SYSTEM INOP. REPLACED DEFECTIVE ELECTRICAL LEAD ON RT PROPELLER.Mar 13, 1997 · N130G · Emb EMB120RT · Propeller/Rotor Anti-Ice/De-Ice SystemSDR COMA9710159Door · not latchedSERVICE DOOR WARNING DURING TAKEOFF. FOUND THE FUEL SINGLE POINT SERVICE DOOR UNLATCHED. SECURED DOOR LATCHES AND AIRCRAFT CONTINUED SERVICE.Feb 25, 1997 · N130G · Emb EMB120RT · Fluid Service DoorsSDR COMA9710155Control · malfunctionedNLG GREEN LIGHTS ARE INTERMITTENT. COULD NOT DUPLICATE DISCREPANCY. REPLACED THE LANDING GEAR CONTROL FOR TROUBLESHOOTING.Feb 19, 1997 · N130G · Emb EMB120RT · Landing Gear Position and WarningSDR COMA9710095Pitchlock Screw · bentACTUATOR ASSEMBLY REMOVED ORIGINALLY FOR PROPELLER FEATHERING PROBLEMS. UPON INITIAL RECEIVING INSPECTION THE FEATHER STOP TAB S/N S0159 WAS FOUND TO BE BENT APPROXIMATELY 0.25 INCH. PITCHLOCK SCREW WAS REMOVED FROM ASSEMBLY AND RETURNED TO MANUFACTURER. PAJan 28, 1997 · N130G · Emb EMB120RT · Propeller Controlling SystemSDR COMA9710017Test Switch · sticksCOPILOTS STALL WARNING SYSTEM ACTIVATES PERIODICALLY. TEST BUTTON IS STICKING. REPLACED THE STALL WARNING TEST PANEL.Jan 2, 1997 · N130G · Emb EMB120RT · Stall Warning SystemSDR COMA9610406Control Unit · malfunctionAFTER TAKEOFF, WHEN LANDING GEAR SELECTED UP, THE LT MLG INDICATED DOWN. CYCLED GEAR CONTROL WITH SAME RESULTS. ELECTRICAL OVERRIDE PROCEDURE WAS USED TO EXTEND LANDING GEAR FOR LANDING. REPLACED THE LANDING GEAR CONTROL ASSY.Dec 17, 1996 · N130G · Emb EMB120RT · Landing Gear Retraction/Extension SystemSDR COMA9610394Annunciator · malfunctionedREPEATED FLAP CONTROL FAULT WARNINGS DURING FLIGHT. REPLACED THE FLAP ANNUCIATOR UNIT.Dec 11, 1996 · N130G · Emb EMB120RT · Trailing Flap Position Indicating SystemSDR COMA9610289Seals · wornLEFT PROPELLER IS SLOW TO FEATHER OR UNFEATHER. REPLACED PROPELLER TRANSFER TUBE SEALS.Sep 26, 1996 · N130G · Emb EMB120RT · Propeller Controlling SystemSDR COMA9610216Floor Beam · corrodedDURING 2C INSPECTION, THE FLOOR BEAM NEXT TO THE ELEVATOR CONTROL COLUMN LEFT WAS FOUND WITH SURFACE CORROSION. CLEANED, TREATED AND PAINTED AREA PER M/M 51-21-04.Jun 15, 1996 · N130G · Emb EMB120RT · Fuselage Main, Floor BeamSDR COMA9610215Floor Beam · corrodedDURING 2C INSPECTION, THE FLOOR BEAM NEXT TO THE ELEVATOR CONTROL COLUMN RIGHT WAS FOUND WITH SURFACE CORROSION. CLEANED, TREATED AND PAINTED AREA PER M/M 51-21-04.Jun 15, 1996 · N130G · Emb EMB120RT · Fuselage Main, Floor BeamSDR COMA9610214Butt Strap · corrodedDURING 2C INSPECTION, SEVERAL RIVETS WERE FOUND LOOSE OR WITH CORROSION AT ENTRY FLOOR, LT BUTT STRAP. REMOVED AND REPLACED WITH ORIGINAL TYPE AND SIZE RIVETS, 19 TOTAL PER EMB 120 SRM CHAPTER 51.Jun 15, 1996 · N130G · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610213Cross Beam · corrodedDURING 2C INSPECTION, FOUND PASSENGER FLOOR SUPPORT CROSSBEAM T-SECTION CORRODED AT FUSELAGE FRAME 16. REMOVED CORRODED T-SECTION, LOCATED, DRILLED AND INSTALLED NEW PART PER EMB 120 SRM STANDARD PRACTICES.Jun 15, 1996 · N130G · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610212Support Section · corrodedDURING 2C INSPECTION, FOUND PASSENGER SEAT LEFT HAND SIDE WALL SEAT TRACK SUPPORT SECTION CORRODED ON SURFACE. CLEANED, TREATED, PAINTED CORRODED AREA PER EMB 120 M/M 51-21-04, OK FOR SERVICE.Jun 15, 1996 · N130G · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610211Support Section · corrodedDURING 2C INSPECTION, FOUND PASSENGER SEAT RIGHT HAND SIDE WALL SEAT TRACK SUPPORT SECTION CORRODED ON SURFACE. CLEANED, TREATED, PAINTED CORRODED AREA PER EMB 120 M/M 51-21-04, OK FOR SERVICE.Jun 15, 1996 · N130G · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610210Seat Track · corrodedDURING 2C INSPECTION, FOUND SEAT TRACKS FOR RIGHT HAND SIDE PASSENGERS SEATS TO BE CORRODED. REMOVED CORRODED SEAT TRACKS AND REPLACED WITH SERVICEABLE TRACKS.Jun 15, 1996 · N130G · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR COMA9610209Stringer · corrodedDURING 2C INSPECTION, FOUND STRINGERS IN LOWER FUSELAGE AREA BELOW LAV TO HAVE SURFACE CORROSION. CLEANED LIGHT CORROSION, TREATED AND PAINTED PER M/M 51-20-04.Jun 15, 1996 · N130G · Emb EMB120RT · Fuselage Main, Longeron/StringerSDR COMA9610208Butt Strap · corrodedDURING 2C INSPECTION, FOUND BUTT STRAPS TO HAVE SURFACE CORROSION. CLEANED, TREATED AND PAINTED AREA PER EMB M/M 51-21-04.Jun 15, 1996 · N130G · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610207Bolt · rustedDURING 2C INSPECTION, FOUND FORWARD INBOARD CORNER OF BATTERY COMPARTMENT AT FRAME 4 TO HAVE SIGNS OF CORROSION. FURTHER INSPECTION FOUND NOSE GEAR FORWARD DOOR, AFT HINGE, HARDWARE TO BE CORRODED. REPLACED HARDWARE AND CLEANED BATTERY COMPARTMENT.Jun 15, 1996 · N130G · Emb EMB120RT · Battery Box StructureSDR COMA9610206Track · corrodedDURING 2C INSPECTION, FOUND GALLEY FLOOR ATTACHMENT TRACK TO BE CORRODED. REMOVED CORRODED TRACK AND REPLACED WITH A SERVICEABLE TRACK.Jun 15, 1996 · N130G · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR COMA9610205Floor Beam · corrodedDURING 2C INSPECTION, FOUND SURFACE CORROSION ON FLOOR BEAM THAT GALLEY FLOOR ATTACHMENT TRACK MOUNTS TO. REMOVED SURFACE CORROSION TREATED AREA AND PAINTED TO SERVICEABLE CONDITION.Jun 15, 1996 · N130G · Emb EMB120RT · Fuselage Main, Floor BeamSDR COMA9610204Seat Track · corrodedDURING 2C INSPECTION, FOUND SEAT TRACKS FOR LEFT HAND SIDE PASSENGER SEATS TO BE CORRODED. REMOVED CORRODED SEAT TRACKS AND REPLACED WITH SERVICEABLE TRACKS.Jun 15, 1996 · N130G · Emb EMB120RT · Fuselage, Seat/Cargo Attach FittingsSDR COMA9610177Bolt · brokenON PREFLIGHT INSPECTION, MECHANIC NOTICED TWO BOLTS MISSING FROM THE RIGHT MAIN INBOARD WHEEL ASSEMBLY. BOLTS ARE PRESUMED TO HAVE BROKEN AND FALLEN OUT. WHEEL/TIRE ASSEMBLY WAS REMOVED AND REPLACED.Jun 11, 1996 · N130G · Emb EMB120RT · Wheel/Ski/FloatSDR COMA9610106Roller · wornCARGO DOOR WILL NOT OPEN. FORWARD LOWER ROLLER CAME OUT OF THE TRACK. REPLACED DOOR ROLLER, OPERATES NORMAL.Mar 18, 1996 · N130G · Emb EMB120RT · Cargo/Baggage DoorsSDR COMA9610050Bolt · missingLEFT MLG INTRANSIT INDICATOR REMAINED ON AFTER LANDING GEAR RETRACTED. REPLACED MISSING BOLT ON INBOARD FORWARD GEAR DOOR LATCH HANDLE. ACFT RETURNED TO SERVICE.Jan 31, 1996 · N130G · Emb EMB120RT · Landing Gear DoorsSDR COMA9511998Fcu · defectiveLEFT ENGINE WILL NOT START. REPLACED THE LEFT ENGINE FUEL CONTROL UNIT.Nov 9, 1995 · N130G · Emb EMB120RT · Fuel Control/Turbine EnginesSDR COMA9511988Latch Assy · brokenTHE LEFT MAIN LANDING GEAR DID NOT RETRACT. REPLACED A BROKEN LANDING GEAR DOOR LATCH ASSEMBLY.Oct 23, 1995 · N130G · Emb EMB120RT · Landing Gear Door Retract SectionSDR COMA9511989Antenna · defectiveRADAR CIRCUIT BREAKER TRIPPED AND WOULD NOT RESET. REPLACED THE RADAR ANTENNA.Oct 19, 1995 · N130G · Emb EMB120RT · Weather Radar SystemSDR COMA9511983Transponder · defectiveNR 2 TRANSPONDER INOPERATIVE. REPLACED THE NR 2 TRANSPONDER.Oct 16, 1995 · N130G · Emb EMB120RT · ATC Transponder System
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