# Service difficulty reports: N829US, cancelled Sep 24, 2003

A list on [N829US, cancelled Sep 24, 2003](https://openairdocs.org/deregistered/N829US-2003-09-24.md).

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

- [SDR ASOA03307](https://openairdocs.org/sdr/ASOA03307.md): Cam · out of rig · Jul 13, 2003 · N829US · Doug DC982 · Passenger/Crew Doors
  > FLT 4140 - DURING GROUND INSPECTION IN DFW, THE MAIN PASSENGER DOOR WOULD NOT OPEN FROM THE OUTSIDE AND DIFFICULT TO OPEN FROM THE INSIDE. MAINTENANCE RIGGED THE MAIN PASSENGER DOOR UPPER CAM MECHANISM. OPERATIONAL AND WARNING CHECKS GOOD. AIRCRAFT OK FOR S
- [SDR USAAD01163](https://openairdocs.org/sdr/USAAD01163.md): Battery · discharged · Sep 22, 2001 · N829US · Doug DC982 · Emergency Lighting
  > PHL - THE LOW LEVEL EMERGENCY LIGHTS IN THE FIRST CLASS SECTION OF THE PASSENGER CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)
- [SDR USAAD01141](https://openairdocs.org/sdr/USAAD01141.md): Battery · inoperative · Jul 30, 2001 · N829US · Doug DC982 · Emergency Lighting
  > BOS - THE LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)
- [SDR USAAD01128](https://openairdocs.org/sdr/USAAD01128.md): Power Supply · discharged · Jun 14, 2001 · N829US · Doug DC982 · Emergency Lighting
  > CLT - THE CEILING EMERGENCY LIGHTS A SEAT ROWS 20 THROUGH 24 ILLUMINATE WITH THE POWER SHUTOFF. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY. (M)
- [SDR USAA010684](https://openairdocs.org/sdr/USAA010684.md): Attach Angle · cracked · Jun 5, 2001 · N829US · Doug DC982 · Fuselage Structure (General)
  > PIT - FOUND PYLON ATTACH ANGLE CRACKED.25 INCH, LOWER PYLON ATTACH ANGLE STATION 1463 CANTED. STOP DRILLED CRACK PER TYPICAL REPAIR 54-10-06A. (M)
- [SDR USAA010685](https://openairdocs.org/sdr/USAA010685.md): Attach Angle · cracked · Jun 5, 2001 · N829US · Doug DC982 · Fuselage Main, Attach Fittings
  > PIT - FOUND ATTACH ANGLE CRACKED.75 INCH, RIGHT UPPER PYLON ATTACH ANGLE CANTED STATION 1464. STOP DRILLED CRACK PER TYPICAL REPAIR 54-10-06A. (M)
- [SDR USAAD01118](https://openairdocs.org/sdr/USAAD01118.md): Battery · inoperative · May 30, 2001 · N829US · Doug DC982 · Emergency Lighting
  > MCO - THE LOW LEVEL LIGHT AT SEAT 25D DID NOT TEST. MAINTENANCE REPLACED THE BATTERY. (M)
- [SDR USAAD01111](https://openairdocs.org/sdr/USAAD01111.md): Water Heater · malfunctioned · May 20, 2001 · N829US · Doug DC982 · Wash Water System
  > PHL-IND - FLT 1787 - DURING DESCENT, AN ELECTRICAL BURNING SMELL WAS DETECTED IN THE LAVATORY AREA. THE AFT LAVATORY WATER HEATER CIRCUIT BREAKER WAS PULL BUT THE SMELL CONTINUED. THE AIRCRAFT CONTINUED TO ITS DESTINATION AND LANDED WITHOUT INCIDENT. MAINTE
- [SDR USAAD01018](https://openairdocs.org/sdr/USAAD01018.md): Battery · discharged · Feb 4, 2001 · N829US · Doug DC982 · Emergency Lighting
  > TPA - THE LOW LEVEL EMERGENCY LIGHT AS SEAT ROW 25 WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M)
- [SDR USAA001736](https://openairdocs.org/sdr/USAA001736.md): Longeron · cracked · Oct 13, 2000 · N829US · Doug DC982 · Fuselage Main, Longeron/Stringer
  > PIT - FOUND LONGERON CRACKED.5 INCH, LONGERON 4L AT INTERSECTION OF FRAME 160. SPLICED IN LONGERON SECTION PER SRM 53-02. (M)
- [SDR USAA001738](https://openairdocs.org/sdr/USAA001738.md): Longeron · cracked · Oct 13, 2000 · N829US · Doug DC982 · Fuselage Main, Longeron/Stringer
  > PIT - Q-3, LONGERON CRACKED.25 INCH AT LONGERON 2L INTERSECTION OF FRAME 160. SPLICED IN LONGERON SECTION PER SRM 53-02 FIG 18. (X)
- [SDR USAA001737](https://openairdocs.org/sdr/USAA001737.md): Longeron · cracked · Oct 13, 2000 · N829US · Doug DC982 · Fuselage Main, Longeron/Stringer
  > PIT - Q-3, LONGERON CRACKED.25 INCH AT LONGERON 3L AT INTERSECTION OF FRAME 160. SPLICED IN LONGERON SECTION PER SRM 53-02. (X)
- [SDR USAA001735](https://openairdocs.org/sdr/USAA001735.md): Angle · cracked · Oct 13, 2000 · N829US · Doug DC982 · Fuselage Miscellaneous Structure
  > PIT - Q-3, REPAIR ANGLE CRACKED, 1.75 INCHES IN RADIUS OF REPAIR ANGLE AT BS 1474, RIGHT VERTICAL STABILIZER. SPLICED IN NEW SECTION AND INSTALLED REPAIR ANGLES (DOUBLERS) PER EA 15895 AND SRM 53-05 FIG 23A. (X)
- [SDR USAAD00093](https://openairdocs.org/sdr/USAAD00093.md): Battery · discharged · Jun 14, 2000 · N829US · Doug DC982 · Emergency Lighting
  > PHL - THE LOW LEVEL EMERGENCY LIGHT AT SEAT ROW 24 ILLUMINATED AND COULD NOT BE EXTINGUISHED. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M)
- [SDR USAAD00029](https://openairdocs.org/sdr/USAAD00029.md): Strut · lack of lube · Feb 16, 2000 · N829US · Doug DC982 · Nose/Tail Landing Gear Strut/Axle
  > LGA - BUF - FLT 2240 - AFTER TAKEOFF, THE NOSE GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE SERVICED THE NOSE STRUT, JACKED THE NOSE OF THE AIRCRAFT AND PERFORMED A NOSE GEAR RETRACTION AND EXTENSION CHE
- [SDR USAAD99099](https://openairdocs.org/sdr/USAAD99099.md): Relay · failed · Jul 19, 1999 · N829US · Doug DC982 · AC Power Distribution System
  > PIT/MSY - FLT 474 - AFTER TAKEOFF IT WAS NOTED THERE WERE NO CABIN LIGHTS OR LAVATORY LIGHTS. THE TOILETS DID NOT FLUSH, THE NR 4 TR INDICATED ZERO, AND THE BATTERY CHARGER WAS INOPERATIVE. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAI
- [SDR USAAD99050](https://openairdocs.org/sdr/USAAD99050.md): Hose · ruptured · Apr 2, 1999 · N829US · Doug DC982 · Air Distribution System
  > DCA-BUF - FLT 8005 - DURING CLIMB POWER SETTINGS THE TAIL COMPARTMENT HIGH TEMP LIGHT ILLUMINATED BUT WOULD EXTINGUISH DURING CRUISE POWER. THE AIRCRAFT DIVERTED TO PIT AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FLEX COUPLING DOWNSTREAM OF THE RIG
- [SDR USAA990084](https://openairdocs.org/sdr/USAA990084.md): Web · cracked · Feb 12, 1999 · N829US · Doug DC982 · Passenger/Crew Doors
  > PIT - DURING C2 CHECK, FOUND 1 INCH CRACK ON VERTICAL WEB AT CENTER OF DOOR ADJACENT TO DOOR OPERATING MECHANISM BETWEEN BEAM 4 AND 5 INNER DOOR HINGE, BOX AFT INTERCOSTAL. INSTALLED DOUBLER P/N SR09520001-3 PER SRM 52-05 FIG 4-5. (M)
- [SDR USAAD98168](https://openairdocs.org/sdr/USAAD98168.md): Generator · failed · Oct 1, 1998 · N829US · Doug DC982 · AC Generator-Alternator
  > MCO-PIT - FLT 843 - EN ROUTE THE LEFT ENGINE GENERATOR POWER DROPPED OFF LINE, AND THE APU WAS ON MEL. THE AIRCRAFT DIVERTED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE GENERATOR. (M)
- [SDR USAAD98130](https://openairdocs.org/sdr/USAAD98130.md): Fuse · broken · Jul 31, 1998 · N829US · Doug DC982 · Hydraulic System, Main
  > TPA - FLT 1622 - DURING CRUISE, THE LEFT HYDRAULIC PRESSURE LOW LIGHT ILLUMINATED WITH THE QTY INDICATING 4 QTS. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. THE LANDING WEIGHT WAS 132,000 LBS. MAINTENANCE REPLACED THE UPPER HYDRAULIC FUS
- [SDR USAAD98091](https://openairdocs.org/sdr/USAAD98091.md): Battery · discharged · May 15, 1998 · N829US · Doug DC982 · Emergency Lighting
  > THE PASSENGER CABIN CEILING EMERGENCY LIGHTS WERE DIM. MAINTENANCE REPLACED THE BATTERIES. (M)
- [SDR USAAD97103](https://openairdocs.org/sdr/USAAD97103.md): Clamp · loose · Jun 17, 1997 · N829US · Doug DC982 · Pneumatic Distribution System
  > BDL/CLT - FLT 1053 - AT 1,000 FEET AFTER TAKEOFF, 'TAIL COMPARTMENT TEMP HI' LIGHT ILLUMINATED. LIGHT EXTINGUISHED WITH HP BLEED SELECTED OFF AND POWER REDUCED. REPEATED FROM PREVIOUS WRITE-UP. RETURNED TO FIELD. REPOSITIONED AND SECURED LOOSE CLAMP AT LEFT
- [SDR USAAD97102](https://openairdocs.org/sdr/USAAD97102.md): Gasket · failed · Jun 17, 1997 · N829US · Doug DC982 · Pneumatic Distribution System
  > BDL/CLT - FLT 1053 - AFTER TAKEOFF AT 600 FEET, 'TAIL COMPARTMENT TEMP HI' LIGHT ILLUMINATED. LIGHT WENT OUT WITH HP BLEEDS SELECTED OFF AND POWER REDUCED. RETURNED TO FIELD. REPLACED HI TEMP SENSOR GASKET, RAN ENGINES, NO OBVIOUS LEAKS NOTED. (X)
- [SDR USAAD97086](https://openairdocs.org/sdr/USAAD97086.md): Engine · failed · May 18, 1997 · N829US · Doug DC982 · Engine (Turbine/Turboprop)
  > FLT 463 - CLT-IAH - AFTER CLIMB THROUGH 19,000 FEET, CREW HEARD A LOUD BANG, AND LEFT ENGINE PARAMETERS BEGAN TO DROP. RETURNED TO CLT. REPLACED LEFT ENGINE. (M)
- [SDR USAAD97064](https://openairdocs.org/sdr/USAAD97064.md): Transmitter · failed · Apr 2, 1997 · N829US · Doug DC982 · Engine Oil Pressure
  > FLIGHT 1438 - BOS-FLL - LEFT OIL PRESSURE LOW LIGHT CAME ON IN FLIGHT. OIL PRESSURE GAUGE INDICATED 34 PSI. OIL TEMP, QTY, AND ALL OTHER ENGINE INDICATIONS NORMAL. DIVERTED TO CLT. REPLACED OIL PRESSURE RELIEF VALVE AND OIL PRESSURE TRANSMITTER. (M)
- [SDR USAAD97054](https://openairdocs.org/sdr/USAAD97054.md): Mechanism · not latched · Mar 10, 1997 · N829US · Doug DC982 · Passenger/Crew Doors
  > FLT 2198 - ROC-PHL - AIRCRAFT FAILED TO PRESSURIZE ON TAKEOFF. RETURNED TO FIELD. L2 DOOR BAYONET WAS NOT IN PROPER POSITION. OPENED AND CLOSED DOOR. NO DEFECTS NOTED. RETURNED AIRCRAFT TO SERVICE. (M)
- [SDR USAAD96173](https://openairdocs.org/sdr/USAAD96173.md): Batteries · discharged · Nov 28, 1996 · N829US · Doug DC982 · Emergency Lighting
  > FORWARD SECTION OF EMERGENCY FLOOR TRACK LIGHTING INOPERATIVE. REPLACED BATTERIES IN BATTERY PACK. (M)
- [SDR USAA960508](https://openairdocs.org/sdr/USAA960508.md): Beltframe · corroded · Jul 16, 1996 · N829US · Doug DC982 · Fuselage Main, Frame
  > PIT - DURING Q-2/C-5 CHECK, FOUND.5 INCH BY 4 INCH CORRODED AREA,STATION 1322 LONGERON 30 BELTFRAME. SPLICED IN NEW BELTFRAME PER SRM53-14-3, CORROSION TASK NR C57-53300. CORROSION LEVEL 1.(M)
- [SDR USAAD96068](https://openairdocs.org/sdr/USAAD96068.md): Pressurization · malfunctioned · Jun 1, 1996 · N829US · Doug DC982 · Cabin Pressure Control System
  > RIC/CLT - FLT 761 - CABIN ALTITUDE CONTROLLER FAILED TO MAINTAIN ALTITUDE AND CLIMBED AT A HIGH RATE ABOVE 10,000 FEET. DESCENDED TO 8,000 FEET. PERFORMED BITE CHECK ON NR 1 AND NR 2 PRESSURIZATION CONTROLLERS. NO FAULTS FOUND. RAN NR 1 AND NR 2 PACKS, OPS
- [SDR USAA950526](https://openairdocs.org/sdr/USAA950526.md): Cargo Net · out of position · May 23, 1995 · N829US · Doug DC982 · Cargo Compartments
  > BOS - FLIGHT 0120 - WHILE ON ROTATION, THE CREW FELT A BUMP THEN NOTICED THE FORWARD CARGO DOOR LIGHT ILLUMINATED. THE CAPTAIN DECIDED TO RETURN TO BOS. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE PRESSURIZED THE AIRCRAFT AND CHECKED FOR LEAKS. NONE WERE F

## 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 = 'N829US' AND deregistration_id = 'N829US-2003-09-24'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N829US-2003-09-24/reports

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