N830US, cancelled Oct 27, 2003

Service difficulty reports · 35

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 = 'N830US' AND deregistration_id = 'N830US-2003-10-27'
  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 USAAD02004Warning System · faultyFLL-CLT - FLT 482 - DURING CLIMB, THE RIGHT ENGINE OIL QUANTITY STARTED TO DROP. THE OIL PRESSURE WAS NORMAL WHEN THE CREW SHUT DOWN THE RIGHT ENGINE AND DIVERTED TO PB. THE FLIGHT LANDED WITHOUT INCIDENT. SINGLE ENGINE TIME WAS 10 MINUTES. MAINTENANCE CHEFeb 5, 2002 · N830US · Doug DC982 · Engine Oil QuantitySDR USAAD02002Landing Gear · lack of lubeCLT-MDT - FLT 910 - AFTER TAKEOFF, WHEN THE GEAR HANDLE WAS PLACED IN THE UP POSITION, THE RIGHT MAIN GEAR UNSAFE LIGHT REMAINED ILLUMINATED. WHEN PLACING THE GEAR HANDLE DOWN, THE UNSAFE LIGHT EXTINGUISHED AND 3 GREEN LIGHTS ILLUMINATED. MAINTENANCE FOUND TJan 19, 2002 · N830US · Doug DC982 · Landing Gear Retraction/Extension SystemSDR USAAD01190Light · inoperativeBOS - THE PASSENGER SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)Dec 16, 2001 · N830US · Doug DC982 · Emergency LightingSDR 2001F00598Battery · dischargedIND - THE RIGHT SIDE WALL EMERGENCY LIGHT AT SEAT ROW 19, THE LEFT AFT SERVICE DOOR EMERGENCY LIGHT, AND TWO LOW LEVEL SEAT MOUNTED EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. REF USAAD00168. (M)Oct 8, 2001 · N830US · Doug DC982 · Emergency LightingSDR USAAD01168Battery · dischargedIND - THE RIGHT SIDE WALL EMERGENCY LIGHT AT SEAT ROW 19, THE LEFT AFT SERVICE DOOR EMERGENCY LIGHT, AND TWO LOW LEVEL SEAT MOUNTED EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)Oct 8, 2001 · N830US · Doug DC982 · Emergency LightingSDR 2001F00413Light · inoperativeTHE LOW LEVEL EMERGENCY LIGHTS AND THE RIGHT AFT EMERGENCY EXIT LIGHT WERE INOPERATIVE. MAINTENANCE REPLACED THE LOW LEVEL EMERGENCY LIGHT BATTERIES AND THE RIGHT AFT EMERGENCY EXIT LIGHT ASSEMBLY. REF USAAD0160. (M)Sep 10, 2001 · N830US · Doug DC982 · Emergency LightingSDR USAAD01060Battery · dischargedTHE LOW LEVEL EMERGENCY LIGHTS AND THE RIGHT AFT EMERGENCY EXIT LIGHT WERE INOPERATIVE. MAINTENANCE REPLACED THE LOW LEVEL EMERGENCY LIGHT BATTERIES AND THE RIGHT AFT EMERGENCY EXIT LIGHT ASSEMBLY. (M)Sep 10, 2001 · N830US · Doug DC982 · Emergency LightingSDR USAA010800Skin · crackedPIT - FOUND SKIN CRACKED .5 INCH, STATION 1437 L3L. CUT OUT DAMAGE, INSTALLED DOUBLER AND FILLERS PER SRM 53-04 FIG 27. (M)Jul 3, 2001 · N830US · Doug DC982 · Fuselage Structure (General)SDR USAAD01045Battery · dischargedIND - THE LOW LEVEL EMERGENCY LIGHTS FAILED THE LIGHT TEST. MAINTENANCE REPLACED THE LOW LEVEL EMERGENCY LIGHT BATTERIES. (M)Mar 9, 2001 · N830US · Doug DC982 · Emergency LightingSDR 20010305SG002Battery · dischargedIND - THE LOW LEVEL EMERGENCY LIGHT AST SEAT ROW 11, AFT EMERGENCY CEILING LIGHTS, AND THE EXTERIOR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE LOW LEVEL LIGHT ASSEMBLY, AND THE BATTERIES FOR THE AFT CEILING EMERGENCY LIGHTS AND THE EXTERIOR EFeb 12, 2001 · N830US · Doug DC982 · Emergency LightingSDR 20010305SG001Battery · dischargedIND - THE LOW LEVEL EMERGENCY LIGHT AST SEAT ROW 11, AFT EMERGENCY CEILING LIGHTS, AND THE EXTERIOR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE LOW LEVEL LIGHT ASSEMBLY, AND THE BATTERIES FOR THE AFT CEILING EMERGENCY LIGHTS AND THE EXTERIOR EFeb 12, 2001 · N830US · Doug DC982 · Emergency LightingSDR USAAD01028Light · inoperativeIND - THE LOW LEVEL EMERGENCY LIGHT AST SEAT ROW 11, AFT EMERGENCY CEILING LIGHTS, AND THE EXTERIOR EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE LOW LEVEL LIGHT ASSEMBLY, AND THE BATTERIES FOR THE AFT CEILING EMERGENCY LIGHTS AND THE EXTERIOR EFeb 12, 2001 · N830US · Doug DC982 · Emergency LightingSDR USAAD01017Flashlight · inoperativeBOS - THE EMERGENCY FLASHLIGHT MOUNTED AT THE MAIN ENTRY DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY FLASHLIGHT. (M)Jan 23, 2001 · N830US · Doug DC982 · Emergency EquipmentSDR USAAD01007Light · inoperativeCLT - THE LOW LEVEL EMERGENCY LIGHT AT SEAT ROW 11 STAYS ILLUMINATED. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY. (M)Jan 11, 2001 · N830US · Doug DC982 · Emergency LightingSDR USA001953Skin · corrodedPIT - FOUND LEADING EDGE SKIN PANEL CORRODED, .75 INCH BY 3 INCHES LONG, RT WING LEADING EDGE SKIN PANEL AT STATION X15 78.00. CORROSION LEVEL 1, TASK NR C10-57300. CLEANED CORROSION AS REQUIRED. (M)Nov 11, 2000 · N830US · Doug DC982 · Wing, Plate/SkinSDR USAA001954Longeron · corrodedPIT - FOUND LONGERON CORRODED 6 INCHES BY 2 INCHES, STATION 503 LONGERON 30. CORROSION LEVEL 1 TASK NR C51-53300. INSTALLED SPLICE PER SRM 53-02 FIG 18. (M)Nov 1, 2000 · N830US · Doug DC982 · Fuselage Main, Longeron/StringerSDR USAA001952Longeron · corrodedPIT - FOUND LONGERON HAS 2 FASTENERS PULLED, SKIN BULGING 2 INCH BY 1 INCH, STATION 332 LONGERON 29R. CORROSION LEVEL 1, TASK NR C50-53306. REPLACED INTERCOSTAL AND LONGERON SECTION PER 53-02 FIG 18 AND 51-60-0, 53-03. (M)Oct 25, 2000 · N830US · Doug DC982 · Fuselage Main, Longeron/StringerSDR USAAD00030Light · failedBOS - THE FORWARD SERVICE DOOR EXIT IDENTIFIER LIGHT HAD NO CHARGE INDICATION. MAINTENANCE REPLACED THE FORWARD SERVICE DOOR EXIT IDENTIFIER LIGHT. (M)Feb 17, 2000 · N830US · Doug DC982 · Emergency LightingSDR USAAD00022Battery · dischargedLGA - THE FORWARD ENTRY DOOR SLIDE ACTIVATED EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (X)Feb 2, 2000 · N830US · Doug DC982 · Emergency LightingSDR USAAD99122Battery · dischargedPIT - SEVERAL LOW LEVEL EMERGENCY LIGHT WERE INOPERATIVE. MAINTENANCE REPLACED THE LOW LEVEL EMERGENCY LIGHT BATTERIES. (M)Aug 31, 1999 · N830US · Doug DC982 · Emergency LightingSDR USAA990432Skin · crackedPIT - DURING C-4 CHECK, FOUND 1 INCH LONG CRACK IN SKIN AT LOWER AFT CORNER OF FORWARD AIRSTAIR DOOR CUTOUT. INSTALLED DOUBLER PER SRM 53-05 FIG 57A. (M)Apr 28, 1999 · N830US · Doug DC982 · Fuselage Main, Plate/SkinSDR USAAD99056Engine · failedRSW-PIT - FLT 352 - WHILE CLIMBING THROUGH 15,000 FEET THE RIGHT ENGINE EGT WAS 80 DEGREES HIGHER THAN THE LEFT AND THE FUEL FLOW WAS 1,000 LBS PER HOUR HIGHER. THE AIRCRAFT DIVERTED TO MCO AND LANDED WITHOUT INCIDENT. AN OVERWEIGHT LAND INSPECTION WAS PERFOApr 16, 1999 · N830US · Doug DC982 · Engine (Turbine/Turboprop)SDR USAAD99055Battery · dischargedIND - THE MAIN ENTRY DOOR SLIDE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE MAIN ENTRY DOOR SLIDE EMERGENCY LIGHT BATTERY. (M)Apr 15, 1999 · N830US · Doug DC982 · Emergency LightingSDR USAAD99047Compressor · damagedBDL-PIT - FLT 1147 - AFTER TAKEOFF AND CLIMBING THROUGH 26,000 FT, THE AIRCRAFT BEGAN TO VIBRATE. THE RIGHT ENGINE N1 INCREASED 6 PERCENT AND A SHUDDER WAS FELT IN THE COCKPIT. SHORTLY THEREAFTER ALL WAS NORMAL. WHEN THE AIRCRAFT LEVELED AT 28,000 FT THE SAMar 6, 1999 · N830US · Doug DC982 · Turbine SectionSDR USAAD98044Duct · failedRSW - FLT 932 - EN ROUTE AT 31,000 FEET THE FLOW LIGH TILLUMINATED ON THE PRESSURE CONTROLLER AND THE CABIN STARTED TO CLIMB AT 1000 FT/MIN. THE CREW SWITCHED TO THE STANDBY PRESSURIZATION SYSTEM BUT THE CABIN CONTINUED TO CLIMB AT THE MAX RATE, THE OUTFLOW VMar 18, 1998 · N830US · Doug DC982 · Cabin Pressure Control SystemSDR USAAD97208Battery · dischargedPIT - MAIN ENTRANCE DOOR ESCAPE SLIDE EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M)Nov 20, 1997 · N830US · Doug DC982 · Emergency LightingSDR USAAD97053Smoke Detector · malfunctionedFLT 251 - CLT-SRQ - AFTER TAKEOFF, F/A NOTED SMOKE ODOR IN AFT LAV AREA, ACCOMPANIED BY INTERMITTENT CHIRPING OF SMOKE DETECTOR. RETURNED TO FIELD. CHANGED LEFT PACK ACM OUTLET AND INLET SENSORS AND BOTH RIGHT AND LEFT COALESCER BAGS. RAN ENGINES AT VARIOUSMar 9, 1997 · N830US · Doug DC982 · Smoke DetectionSDR USAAD96157Wire · brokenFORWARD OVERWING EXIT FLOOR LEVEL EMERGENCY LIGHT (RED) INOPERATIVE. REPAIRED BROKEN WIRE TO LIGHT. (M)Oct 27, 1996 · N830US · Doug DC982 · Light System WiringSDR USAAD96146Controller · failedFLT 417 - PIT-MDT - CLIMBING THROUGH 17,000 FEET, CABIN ALTITUDE CONTROL WHEEL WENT FULL CLOSED AND STARTED TO CHATTER AND VIBRATE. SELECTED STANDBY WITH NO CHANGE. WENT TO MANUAL AND REGAINED CONTROL OF CABIN PRESSURE. RETURNED TO PIT. FOUND NR 1 PRESSURIOct 16, 1996 · N830US · Doug DC982 · Cabin Pressure ControllerSDR USAAA960640Seat Track · corrodedPIT - DURING Q-2 CHECK, FOUND SEAT TRACK CORRODD AT LEFT INBOARD SEAT TRACK STATION 1125 TO 1168. SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05 FIG 4F. CORROSION TASK NR C58-53302, CORROSION LEVEL 1. (M)Sep 27, 1996 · N830US · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR USAA960662Seat Track · corrodedPIT - DURING Q-2 CHECK, FOUND LEVEL ONE SUSPECT, LEVEL TWO CORROSION AT RIGHT INBOARD SEAT TRACK AT STATION 339 TO STATION 360. SPLICED IN NEW SECTION OF SEAT TRCK PER SRM 53-05 FIG 4F. CORROSION TASK NR C58-53302, CORROSION LEVEL 1. (M)Sep 27, 1996 · N830US · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR USAA960661Seat Track · corrodedPIT - DURING Q-2 CHECK, FOUND SEAT TRACK CORROSION AT RIGHT INBOARD STATION 321 TO STATION 398. SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05 FIG 4. CORROSION TASK NR C58-53302, CORROSION LEVEL 1. (M)Sep 27, 1996 · N830US · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR USAA960637Belt Frame · corrodedPIT - DURING Q2 CHECK, FOUND SEVERAL CORRODED AREAS .5 INCH BY 1 INCH AROUND FASTENERS AT STATION 1322 BELTFRAME L28L TO L28R. INSTALLED BELTFRAME SPLICE PER SRM 53-03 FIG 2A. CORROSION TASK NR C57-55300, CORROSION LEVEL 1. (M)Sep 27, 1996 · N830US · Doug DC982 · Fuselage Main, FrameSDR USAA960636Seat Track · corrodedPIT - DURING Q-2 CHECK, FOUND CORRODED AREA .75 INCH BY 4 INCH AT STATION 373 SEAT TRACK RIGHT OUTBOARD. SPLICED IN NEW SECTION OF SEAT TRACK PER SRM 53-05 FIG 4F. CORROSION TASK NR C58-53302, CORROSION LEVEL 1. (M)Sep 27, 1996 · N830US · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR USAA960626Angle · crackedPIT - DURING Q-2 CHECK, FOUND RIGHT AFT RIGHT VERT STAB ATTACH ANGLE CRACKED AT STATION 1474. INSTALLED DOUBLER PER SRM 53-05 FIG 23A. (M)Sep 27, 1996 · N830US · Doug DC982 · Fuselage Miscellaneous Structure
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