# Service difficulty reports: N830US, cancelled Oct 27, 2003

A list on [N830US, cancelled Oct 27, 2003](https://openairdocs.org/deregistered/N830US-2003-10-27.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR USAAD02004](https://openairdocs.org/sdr/USAAD02004.md): Warning System · faulty · Feb 5, 2002 · N830US · Doug DC982 · Engine Oil Quantity
  > FLL-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 CHE
- [SDR USAAD02002](https://openairdocs.org/sdr/USAAD02002.md): Landing Gear · lack of lube · Jan 19, 2002 · N830US · Doug DC982 · Landing Gear Retraction/Extension System
  > CLT-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 T
- [SDR USAAD01190](https://openairdocs.org/sdr/USAAD01190.md): Light · inoperative · Dec 16, 2001 · N830US · Doug DC982 · Emergency Lighting
  > BOS - THE PASSENGER SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)
- [SDR 2001F00598](https://openairdocs.org/sdr/2001F00598.md): Battery · discharged · Oct 8, 2001 · N830US · Doug DC982 · Emergency Lighting
  > IND - 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)
- [SDR USAAD01168](https://openairdocs.org/sdr/USAAD01168.md): Battery · discharged · Oct 8, 2001 · N830US · Doug DC982 · Emergency Lighting
  > IND - 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)
- [SDR 2001F00413](https://openairdocs.org/sdr/2001F00413.md): Light · inoperative · Sep 10, 2001 · N830US · Doug DC982 · Emergency Lighting
  > THE 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)
- [SDR USAAD01060](https://openairdocs.org/sdr/USAAD01060.md): Battery · discharged · Sep 10, 2001 · N830US · Doug DC982 · Emergency Lighting
  > THE 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)
- [SDR USAA010800](https://openairdocs.org/sdr/USAA010800.md): Skin · cracked · Jul 3, 2001 · N830US · Doug DC982 · Fuselage Structure (General)
  > PIT - FOUND SKIN CRACKED.5 INCH, STATION 1437 L3L. CUT OUT DAMAGE, INSTALLED DOUBLER AND FILLERS PER SRM 53-04 FIG 27. (M)
- [SDR USAAD01045](https://openairdocs.org/sdr/USAAD01045.md): Battery · discharged · Mar 9, 2001 · N830US · Doug DC982 · Emergency Lighting
  > IND - THE LOW LEVEL EMERGENCY LIGHTS FAILED THE LIGHT TEST. MAINTENANCE REPLACED THE LOW LEVEL EMERGENCY LIGHT BATTERIES. (M)
- [SDR 20010305SG002](https://openairdocs.org/sdr/20010305SG002.md): Battery · discharged · Feb 12, 2001 · N830US · Doug DC982 · Emergency Lighting
  > IND - 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 E
- [SDR 20010305SG001](https://openairdocs.org/sdr/20010305SG001.md): Battery · discharged · Feb 12, 2001 · N830US · Doug DC982 · Emergency Lighting
  > IND - 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 E
- [SDR USAAD01028](https://openairdocs.org/sdr/USAAD01028.md): Light · inoperative · Feb 12, 2001 · N830US · Doug DC982 · Emergency Lighting
  > IND - 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 E
- [SDR USAAD01017](https://openairdocs.org/sdr/USAAD01017.md): Flashlight · inoperative · Jan 23, 2001 · N830US · Doug DC982 · Emergency Equipment
  > BOS - THE EMERGENCY FLASHLIGHT MOUNTED AT THE MAIN ENTRY DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY FLASHLIGHT. (M)
- [SDR USAAD01007](https://openairdocs.org/sdr/USAAD01007.md): Light · inoperative · Jan 11, 2001 · N830US · Doug DC982 · Emergency Lighting
  > CLT - THE LOW LEVEL EMERGENCY LIGHT AT SEAT ROW 11 STAYS ILLUMINATED. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY. (M)
- [SDR USA001953](https://openairdocs.org/sdr/USA001953.md): Skin · corroded · Nov 11, 2000 · N830US · Doug DC982 · Wing, Plate/Skin
  > PIT - 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)
- [SDR USAA001954](https://openairdocs.org/sdr/USAA001954.md): Longeron · corroded · Nov 1, 2000 · N830US · Doug DC982 · Fuselage Main, Longeron/Stringer
  > PIT - 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)
- [SDR USAA001952](https://openairdocs.org/sdr/USAA001952.md): Longeron · corroded · Oct 25, 2000 · N830US · Doug DC982 · Fuselage Main, Longeron/Stringer
  > PIT - 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)
- [SDR USAAD00030](https://openairdocs.org/sdr/USAAD00030.md): Light · failed · Feb 17, 2000 · N830US · Doug DC982 · Emergency Lighting
  > BOS - THE FORWARD SERVICE DOOR EXIT IDENTIFIER LIGHT HAD NO CHARGE INDICATION. MAINTENANCE REPLACED THE FORWARD SERVICE DOOR EXIT IDENTIFIER LIGHT. (M)
- [SDR USAAD00022](https://openairdocs.org/sdr/USAAD00022.md): Battery · discharged · Feb 2, 2000 · N830US · Doug DC982 · Emergency Lighting
  > LGA - THE FORWARD ENTRY DOOR SLIDE ACTIVATED EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (X)
- [SDR USAAD99122](https://openairdocs.org/sdr/USAAD99122.md): Battery · discharged · Aug 31, 1999 · N830US · Doug DC982 · Emergency Lighting
  > PIT - SEVERAL LOW LEVEL EMERGENCY LIGHT WERE INOPERATIVE. MAINTENANCE REPLACED THE LOW LEVEL EMERGENCY LIGHT BATTERIES. (M)
- [SDR USAA990432](https://openairdocs.org/sdr/USAA990432.md): Skin · cracked · Apr 28, 1999 · N830US · Doug DC982 · Fuselage Main, Plate/Skin
  > PIT - 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)
- [SDR USAAD99056](https://openairdocs.org/sdr/USAAD99056.md): Engine · failed · Apr 16, 1999 · N830US · Doug DC982 · Engine (Turbine/Turboprop)
  > RSW-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 PERFO
- [SDR USAAD99055](https://openairdocs.org/sdr/USAAD99055.md): Battery · discharged · Apr 15, 1999 · N830US · Doug DC982 · Emergency Lighting
  > IND - THE MAIN ENTRY DOOR SLIDE EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE MAIN ENTRY DOOR SLIDE EMERGENCY LIGHT BATTERY. (M)
- [SDR USAAD99047](https://openairdocs.org/sdr/USAAD99047.md): Compressor · damaged · Mar 6, 1999 · N830US · Doug DC982 · Turbine Section
  > BDL-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 SA
- [SDR USAAD98044](https://openairdocs.org/sdr/USAAD98044.md): Duct · failed · Mar 18, 1998 · N830US · Doug DC982 · Cabin Pressure Control System
  > RSW - 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 V
- [SDR USAAD97208](https://openairdocs.org/sdr/USAAD97208.md): Battery · discharged · Nov 20, 1997 · N830US · Doug DC982 · Emergency Lighting
  > PIT - MAIN ENTRANCE DOOR ESCAPE SLIDE EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M)
- [SDR USAAD97053](https://openairdocs.org/sdr/USAAD97053.md): Smoke Detector · malfunctioned · Mar 9, 1997 · N830US · Doug DC982 · Smoke Detection
  > FLT 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 VARIOUS
- [SDR USAAD96157](https://openairdocs.org/sdr/USAAD96157.md): Wire · broken · Oct 27, 1996 · N830US · Doug DC982 · Light System Wiring
  > FORWARD OVERWING EXIT FLOOR LEVEL EMERGENCY LIGHT (RED) INOPERATIVE. REPAIRED BROKEN WIRE TO LIGHT. (M)
- [SDR USAAD96146](https://openairdocs.org/sdr/USAAD96146.md): Controller · failed · Oct 16, 1996 · N830US · Doug DC982 · Cabin Pressure Controller
  > FLT 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 PRESSURI
- [SDR USAAA960640](https://openairdocs.org/sdr/USAAA960640.md): Seat Track · corroded · Sep 27, 1996 · N830US · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > PIT - 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)
- [SDR USAA960662](https://openairdocs.org/sdr/USAA960662.md): Seat Track · corroded · Sep 27, 1996 · N830US · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > PIT - 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)
- [SDR USAA960661](https://openairdocs.org/sdr/USAA960661.md): Seat Track · corroded · Sep 27, 1996 · N830US · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > PIT - 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)
- [SDR USAA960637](https://openairdocs.org/sdr/USAA960637.md): Belt Frame · corroded · Sep 27, 1996 · N830US · Doug DC982 · Fuselage Main, Frame
  > PIT - 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)
- [SDR USAA960636](https://openairdocs.org/sdr/USAA960636.md): Seat Track · corroded · Sep 27, 1996 · N830US · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings
  > PIT - 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)
- [SDR USAA960626](https://openairdocs.org/sdr/USAA960626.md): Angle · cracked · Sep 27, 1996 · N830US · Doug DC982 · Fuselage Miscellaneous Structure
  > PIT - 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)

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/deregistered/N830US-2003-10-27/reports

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