N14889, cancelled Jul 23, 2003

Service difficulty reports · 23

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 = 'N14889' AND deregistration_id = 'N14889-2003-07-23'
  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 CALA0100828Duct · blownTHE CREW RECEIVED A FIRE WARNING INDICATION FROM THE RT ENGINE DURING CLIMBOUT OF IAH. THE THROTTLE WAS RETARDED AND THE FIRE WARNING INDICATION WENT OUT. THE AIRCRAFT WAS RETURNED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 ENGINE 8Aug 31, 2001 · N14889 · Doug DC982 · Engine Anti-Icing SystemSDR CALA0100580Fuse · blownINSPECTION FOUND L-2 DOOR AND AFT STAIRWAY DOOR EXIT IDENTIFIER LIGHTS INOPERATIVE. THE FUSE FOR BATTERY PACK IN AFT CABIN DROP CEILING WAS REPLACED AND OPERATION CHECKED GOOD IAW MM 33-53-00.Jun 22, 2001 · N14889 · Doug DC982 · Emergency LightingSDR CALA0100225Beam · corrodedINSPECTION FOUND MID CARGO DOOR JAMB BEAM CORRODED. A DOUBLER, SPACER, AND FASTENERS WERE INSTALLED.Mar 13, 2001 · N14889 · Doug DC982 · Fuselage Main, StructureSDR CALA0100213Web · corrodedINSPECTION FOUND FORWARD SIDE OF AFT CARGO TORQUE BOX WEB CORRODED. THE TORQUE BOX WEB AND ATTACHMENTS WERE REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-5, 51-10-4, 51-10-3, AND 51-30-2.Mar 8, 2001 · N14889 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA0100198Door Frame · corrodedINSPECTION FOUND FORWARD CARGO DOOR JAMB PAN CORRODED AROUND RIVNUTS. THE CORRODED AREA OF DOOR PAN WAS CUT OUT AND A REPAIR ANGLE AND SPLICE ANGLES WERE INSTALLED IAW SRM 53-05, FIGURE 44, 51-10-3, 51-30-2, AND 51-30-5.Mar 3, 2001 · N14889 · Doug DC982 · Fuselage Main, StructureSDR CALA0001837Cable · out of rigTHE TAILCONE PULL FROM THE INTERIOR AND AFT DOOR HANDLES EXCEEDED LIMITS TO DROP TAIL CONE. THE TAILCONE CABLES WERE RIGGED IAW MM 53-53-00 AND OPERATION CHECKED GOOD.Nov 25, 2000 · N14889 · Doug DC982 · Aerodynamic FairingsSDR CALA0000940Proximity Switch · out of adjTHE RED NOSE GEAR WARNING LIGHT REMAINED ILLUMINATED WHEN GEAR WAS RETRACTED AFTER TAKEOFF FROM BWI. WHEN THE GEAR WAS EXTENDED FOR RETURN TO BWI THREE GREEN DOWN AND LOCKED LIGHTS WERE INDICATED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE Jun 20, 2000 · N14889 · Doug DC982 · Landing Gear Position and WarningSDR CALA9802044Handle · out of adjustTHE FORCE REQUIRED TO RELEASE TAIL CONE USING THE EXTERIOR, INTERIOR, AND AFT ENTRY DOOR HANDLES WAS OUT OF LIMITS. THE HANDLES WERE ADJUSTED AND TESTED IAW MM 53-53-00.Nov 5, 1998 · N14889 · Doug DC982 · Aerodynamic FairingsSDR CALA9802035Frame · corrodedINSPECTION FOUND CORROSION ON CUSP MEMBRANE AND AFT SIDE OF FRAME AT STA 200 TO 204 JUST AFT OF MAIN CABIN DOOR AFT LOWER CORNER INSIDE LIGHTENING HOLE. A REPAIR WAS INSTALLED IAW ECRA 5310-03778.Nov 4, 1998 · N14889 · Doug DC982 · Fuselage Main, FrameSDR CALA9802006Fitting · crackedINSPECTION FOUND A .75 INCH CRACK IN LT WHEEL WELL FITTING AT FLAP ACTUATOR MOUNTS STA 980. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-5.Nov 1, 1998 · N14889 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9801995Seat Track · corrodedINSPECTION FOUND L/H INBOARD SEAT TRACK CORRODED AT STA 1212-1309. THE SEAT TRACK SECTION WAS REMOVED AND REPLACED IAW SRM 51-30-1.Oct 27, 1998 · N14889 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9802003Seat Track · corrodedINSPECTION FOUND L/H INBOARD SEAT TRACK CORRODED AT STA 221. THE CORRODED SECTION OF SEAT TRACK WAS REMOVED AND A NEW SECTION WAS INSTALLED IAW SRM 53-05, FIGURE 4.Oct 23, 1998 · N14889 · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR CALA9802002Intercostal · crackedINSPECTION FOUND A 2.5 CRACK IN INTERCOSTAL AT #1 VHF ANTENNA, STA 474. A NEW INTERCOSTAL WAS INSTALLED IAW EA 5330-01823.Oct 23, 1998 · N14889 · Doug DC982 · Fuselage Miscellaneous StructureSDR CALA9801980Skin · scratchedINSPECTION FOUND LT FUSELAGE SKIN SCRATCHED AT STA 237, LONGERON 17L. THE EXISTING DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-5 AND ECRA 5330-02445.Oct 20, 1998 · N14889 · Doug DC982 · Fuselage Main, Plate/SkinSDR CALA9800019Batteries · dischargedINSPECTION FOUND EMERGENCY LIGHTS ON CEILING ABOVE ROW 1 TO 4 AND ROW 22 TO 30 INOPERATIVE. THE BATTERIES IN FORWARD CABIN CEILING AND ABOVE ROW 24 WERE REMOVED AND REPLACED.Jan 13, 1998 · N14889 · Doug DC982 · Emergency LightingSDR CALA9701159Uplock Sensor · out of adjustTHE NOSE GEAR UNSAFE LIGHT ILLUMINATED DURING CLIMBOUT. ABNORMAL PROCEDURES WERE COMPLIED WITH AND THE NOSE GEAR UNSAFE LIGHT EXTINGUISHED. THE FLIGHT WAS COMPLETED WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND THE UP/DOWN LOCK SENSOR OUT OF LIMITS. THE SENSOAug 2, 1997 · N14889 · Doug DC982 · Landing Gear Position and WarningSDR CALA9700313Actuator · leakingTHE HYDRAULIC QUANTITY DROPPED TO TWO QUARTS ON FINAL APPROACH, WHEN THE LANDING GEAR WAS LOWERED. THE NOSE GEAR CAME DOWN AND LOCKED ABOUT 30 SECONDS AFTER GEAR EXTENSION WAS INITIATED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RT MLG RETMar 6, 1997 · N14889 · Doug DC982 · Landing Gear ActuatorSDR CALA9601605Frame · crackedINSPECTION FOUND .50 INCH CRACKS IN CANTED BELTFRAME AT STA 1446, LONGERONS 3, 4, AND 5R. THE FRAME WAS REPAIRED IAW SRM 53-03.Oct 29, 1996 · N14889 · Doug DC982 · Fuselage Main, FrameSDR CALA9601297Engine · failedTHE TOWER REPORTED FIRE FROM THE NR 2 ENGINE TAILCONE AREA DURING TAXI OUT. THE CAPTAIN DISCHARGED BOTH ENGINE FIRE BOTTLES AND THE FIRE DEPARTMENT WAS SUMMONED. AN EMERGENCY EVACUATION WAS PERFORMED. THE FORWARD SERVICE DOOR AND AFT SERVICE DOOR ESCAPE SLISep 5, 1996 · N14889 · Doug DC982 · Engine (Turbine/Turboprop)SDR CALA9601206Bearing · failedTHE WHEEL NOT TURNING LIGHT ILLUMINATED DURING TAKEOFF ROLL. THE TAKEOFF WAS ABORTED AT LOW SPEED AND THE AIRCRAFT WAS RETURNED TO GATE. MAINTENANCE FOUND THE NR 3 TIRE FLAT WHEN THE NR 3 TIRE WAS REMOVED THE BEARING WAS FOUND FROZEN TO AXLE AND THE ANTI-SKIAug 21, 1996 · N14889 · Doug DC982 · Wheel/Ski/FloatSDR CAL950487Eel Wiring · brokenEWR - FLT 0346 - INSPECTION FOUND OVERHEAD EMERGENCY EXIT LIGHTS AT ROWS 19-31 INOPERATIVE. MAINTENANCE FOUND WIRING TO LIGHTS BROKEN. THE WIRES WERE SPLICED AND OPERATION OF THE LIGHTS CHECKED GOOD. (X)Jun 14, 1995 · N14889 · Doug DC982 · Emergency LightingSDR CAL950430Eel Batt Charger · inoperativeFLT NR 1421 - EWR - WHEN EXTERNAL POWER WAS DISCONNECTED AT THE GATE, NONE OF THE OVERHEAD EMERGENCY LIGHTS BEHIND ROW 28 CAME ON. SOME BURNT OUT BULBS HAD TO BE REPLACED AND THE AFT BATTERY CHARGER WAS REMOVED AND REPLACED. OPERATION OF THE OVERHEAD EMERGENMay 30, 1995 · N14889 · Doug DC982 · Emergency LightingSDR CAL950416Separator · frozen shutIAH - FLT 0108 - THE AIRCRAFT STARTED LOSING PRESSURE AT 37,000 FEET WITH DE-ICING ON, AND OXYGEN MASKS WERE DROPPED MANUALLY. CREW ATTEMPTED SECONDARY WHICH INDICATED FAILURE, SO SWITCHED BACK TO PRIMARY. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE OBSERMay 24, 1995 · N14889 · Doug DC982 · Humidity Control System
Back to N14889, cancelled Jul 23, 2003