# Service difficulty reports: N823US, cancelled Mar 18, 2004

A list on [N823US, cancelled Mar 18, 2004](https://openairdocs.org/deregistered/N823US-2004-03-18.md).

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

- [SDR USAAD02017](https://openairdocs.org/sdr/USAAD02017.md): Battery · discharged · Mar 29, 2002 · N823US · Doug DC982 · Emergency Lighting
  > IND - SEVERAL LOW LEVEL EMERGENCY LIGHTS FAILED TEST. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)
- [SDR USAAD02008](https://openairdocs.org/sdr/USAAD02008.md): Battery · discharged · Feb 9, 2002 · N823US · Doug DC982 · Emergency Lighting
  > IND - THE FORWARD CEILING AND OVERWING EXIT SIGN EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)
- [SDR USAAD01179](https://openairdocs.org/sdr/USAAD01179.md): Battery Pack · discharged · Nov 11, 2001 · N823US · Doug DC982 · Emergency Lighting
  > IND - THE INTERVALVE LOW LEVEL LIGHTS DO NOT TEST AT SEATS 1, 3, 6, 11, 16, 20, 25 AND 30. MAINTENANCE REPLACED THE BATTERY PACKS. SYSTEMS TESTS OK. (M)
- [SDR USAA010644](https://openairdocs.org/sdr/USAA010644.md): Beltframe · corroded · May 30, 2001 · N823US · Doug DC982 · Fuselage Main, Frame
  > PPIT - FOUND BELTFRAME CORRODED 24 INCHES BY 1 INCH, AFT SIDE OF BELTFRAME AT STATION 1309 FROM LONGERON 28 LEFT. CORROSION LEVEL 1, TASK NR C57-53300. REMOVED CORROSION, ACCOMPLISHED FORMER SPLICE REPAIR PER SRM 53-03 FIG 3 FIG 2A. (M)
- [SDR 20010427AP001](https://openairdocs.org/sdr/20010427AP001.md): Battery · discharged · Apr 3, 2001 · N823US · Doug DC982 · Emergency Lighting
  > IND - TWO LOW LEVEL EMERGENCY LIGHTS AND TWO SECTIONS OF CEILING EMERGENCY LIGHTS WERE INOPERATAIVE. THE LOW LEVEL EMERGENCY LIGHT FOR SEAT ROW 25 WAS LOCATED AT SEAT ROW 26. MAINTENANCE REPLACED THE LOW LEVEL AND CEILING EMERGENCY LIGHT BATTERIES AND RELOCA
- [SDR USAAD01075](https://openairdocs.org/sdr/USAAD01075.md): Battery · discharged · Apr 3, 2001 · N823US · Doug DC982 · Emergency Lighting
  > IND - TWO LOW LEVEL EMERGENCY LIGHTS AND TWO SECTIONS OF CEILING EMERGENCY LIGHTS WERE INOPERATAIVE. THE LOW LEVEL EMERGENCY LIGHT FOR SEAT ROW 25 WAS LOCATED AT SEAT ROW 26. MAINTENANCE REPLACED THE LOW LEVEL AND CEILING EMERGENCY LIGHT BATTERIES AND RELOCA
- [SDR USAAD01053](https://openairdocs.org/sdr/USAAD01053.md): Door · not closed · Mar 17, 2001 · N823US · Doug DC982 · Service Doors
  > CLT-MSY - FLT 1035 - AFTER TAKEOFF, THE PRESSURIZATION FLOW LIGHT ILLUMINATED. THE FLIGHT ATTENDANT REPORTED AN EXTREMELY LOUD AIR NOISE AT THE AFT SERVICE DOOR. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AFT SERVI
- [SDR USAA20010117](https://openairdocs.org/sdr/USAA20010117.md): O-Ring · damaged · Dec 31, 2000 · N823US · Doug DC982 · Landing Gear Retraction/Extension System
  > PIT-MCO FLT 1879 AFTER TAKEOFF, NOSE LANDING GEAR DID NOT RETRACT AND THE RED GEAR UNSAFE LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NOSE STRUT SCHRADER VALVE AND ORING. THE NOSE GEAR WAS SWUNG
- [SDR USAAD00186](https://openairdocs.org/sdr/USAAD00186.md): Door · open · Dec 3, 2000 · N823US · Doug DC982 · Service Doors
  > PIT-ORD - FLT 1640 - AFTER TAKEOFF, THE AIRCRAF WOULD NOT PRESSURIZE AND THERE WAS A LOUD NOISE AT THE AFT SERVICE DOOR. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE AFT SERVICE DOOR NOT CLOSED PROPERLY. THE DOOR WAS
- [SDR USAA001424](https://openairdocs.org/sdr/USAA001424.md): Attach Angle · cracked · Sep 3, 2000 · N823US · Doug DC982 · Fuselage Miscellaneous Structure
  > PIT - FOUND ATTACH BRACKET CRACKED 2 INCHES, STATION 937 AFT SIDE, RIGHT WHEEL WELL. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR. (M)
- [SDR USAA001425](https://openairdocs.org/sdr/USAA001425.md): Beam · cracked · Sep 3, 2000 · N823US · Doug DC982 · Fuselage Miscellaneous Structure
  > PIT - FOUND BEAM CRACKED 1 INCH CRACKED, STATION 1003 CTR VERTICAL BEAM AT BH AFT FLANGE. MFG TWO DOUBLERS OUT OF 2024-T3 032 AND 1 SHIM FROM 2024-T3 063, STOP DRILLED CRAC PER SRM 54-01 PAGE 7. (M)
- [SDR USAA001419](https://openairdocs.org/sdr/USAA001419.md): Skin · cracked · Aug 30, 2000 · N823US · Doug DC982 · Fuselage Main, Plate/Skin
  > PIT - FOUND SKIN CRACKED.25 INCH, FORWARD SERVICE DOOR, HOLD OPEN HOOK CUTOUT. INSTALLED EXTERNAL DOUBLER PER EA 56228. (M)
- [SDR USAA001420](https://openairdocs.org/sdr/USAA001420.md): Web · cracked · Aug 26, 2000 · N823US · Doug DC982 · Fuselage Miscellaneous Structure
  > PIT - FOUND RIGHT CUSP MEMBRANE CRACKED 1.5 INCHES, STATION 838. MANUFACTURED NEW AND INSTALLED PER SRM 53-05-97 AND DACO DWG 9910151. (M)
- [SDR USAA001421](https://openairdocs.org/sdr/USAA001421.md): Web · cracked · Aug 26, 2000 · N823US · Doug DC982 · Fuselage Miscellaneous Structure
  > PIT - FOUND RIGHT CUSP MEMBRANE CRACKED.75 INCH, STATION 905. MANUFACTURE NEW MEMBRANE AND INSTALLED PER SRM 53-05 FIG 97/DACO DWG 991051. (M)
- [SDR USAA001422](https://openairdocs.org/sdr/USAA001422.md): Web · cracked · Aug 26, 2000 · N823US · Doug DC982 · Fuselage Miscellaneous Structure
  > PIT - FOUND RIGHT CUSP MEMBRANE CRACKED TWO PLACES, 2 INCHES AND.75 INCH, STATION 886. MANUFACTURED NEW AND INSTALLED PER DACO DWG 9910151/SRM 53-05 FIG 97. (M)
- [SDR USAA001429](https://openairdocs.org/sdr/USAA001429.md): Web · corroded · Aug 25, 2000 · N823US · Doug DC982 · Fuselage Miscellaneous Structure
  > PIT - FOUND CUSP MEMBRANE 1 INCH BY 4 INCH AREA CORRODED, RIGHT CUSP SUBFLOOR AT FRAME FITTING, STATION 237. INSTALLED NEW SECTION OF MANUFACTURE CUSP MEMBRANE OUT OF 7075-T6.32 INCH PER EA 56223 AND SRM 53-05 FIG 96. (M)
- [SDR USAA001526](https://openairdocs.org/sdr/USAA001526.md): Beam · corroded · Aug 24, 2000 · N823US · Doug DC982 · Fuselage Miscellaneous Structure
  > PIT - FOUND BEAM CORRODED IN TWO AREAS, 11 INCH BY 4 INCH AND 1 INCH BY 6 INCHES, MID AND AFT CARGO BEAM BELOW DOOR. REPLACED BOTH BEAMS PER EO 5390M251 AND EA 51567. (M)
- [SDR USAA001423](https://openairdocs.org/sdr/USAA001423.md): Intercostal · corroded · Aug 24, 2000 · N823US · Doug DC982 · Fuselage Miscellaneous Structure
  > PIT - FOUND INTERCOSTAL CORRODED 1 INCH BY 6 INCHES, STATION 1309-1322 L28R. REPLACED INTERCOSTAL PER SRM 51-30. (M)
- [SDR USAA001426](https://openairdocs.org/sdr/USAA001426.md): Skin · cracked · Aug 22, 2000 · N823US · Doug DC982 · Fuselage Main, Plate/Skin
  > PIT - FOUND SKIN CRACKED 1 INCH, STATION 1437 AT 3 RT. INSTALLED DOUBLER 9 INCHES BY 12 INCHES PER SRM 53-04 PAGE 143, FIG 27. (M)
- [SDR USAA001430](https://openairdocs.org/sdr/USAA001430.md): Beam · corroded · Aug 22, 2000 · N823US · Doug DC982 · Fuselage Miscellaneous Structure
  > PIT - FOUND BEAM CORRODED 1 INCH BY 2 INCH AREA, FS 1135, 1165 AND 1185 AT 29 RIGHT. INSTALLED STRAP.125 INCH THICK. CORROSION LEVEL 1. TASK NR C57-5330. (M)
- [SDR USAAD00106](https://openairdocs.org/sdr/USAAD00106.md): Door · not closed · Jul 1, 2000 · N823US · Doug DC982 · Service Doors
  > BUF-CLT - FLT 489 - AFTER TAKEOFF, THE CABIN WOULD NOT PRESSURIZE. THE AIRCRAFT DIVERTED TO PIT AND LANDED WITHOUT INCIDENT. MAINTENANCE SECURED THE L2 SERVICE DOOR. AN OVERWEIGHT LANDING INSPECTION WAS PERFORMED. (M)
- [SDR USAAD00066](https://openairdocs.org/sdr/USAAD00066.md): Cylinder · failed · May 4, 2000 · N823US · Doug DC982 · Landing Gear Retraction/Extension System
  > CLT-IND - FLT 429 - DURING APPROACH, WHEN THEN LANDING GEAR WAS LOWERED, THE NOSE GEAR UNSAFE LIGHT ILLUMINATED. THE NOSE GEAR WAS EXTENDED USING THE EMERGENCY GEAR EXTENSION LEVER AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NOSE GEAR
- [SDR USAAD00023](https://openairdocs.org/sdr/USAAD00023.md): Battery · discharged · Feb 2, 2000 · N823US · Doug DC982 · Emergency Lighting
  > PHL - DURING SHUT DOWN OF THE AIRCRAFT ELECTRICAL SYSTEM, THE FLOOR LEVEL EMERGENCY LIGHTS DID NOT EXTINGUISH. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES FOR SEAT ROWS 16, 20, 25, AND 30. (X)
- [SDR USAAD00020](https://openairdocs.org/sdr/USAAD00020.md): Connector · failed · Jan 31, 2000 · N823US · Doug DC982 · Pressure Regulator/Outflow Valve
  > MSY/CLT - FLT 2310 - AFTER TAKEOFF, CABIN WOULD NOT PRESSURIZE. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS FERRIED TO CLT FOR MAINTENANCE WHERE THE ELECTRICAL CONNECTOR TO THE LEFT AIR CONDITIONING PRESSURE REGULATOR VAL
- [SDR USAAD99172](https://openairdocs.org/sdr/USAAD99172.md): Engine · failed · Dec 3, 1999 · N823US · Doug DC982 · Turbine Section
  > PIT - BUF - FLT 1648 - AFTER TAKEOFF, THE CREW HEARD A LOUD NOISE AND VIBRATION. THE CREW SUSPECTED A NOSE GEAR DOOR NOT FULLY CLOSED AS THER WERE NO ABNORMAL ENGINE INDICATIONS. HALF WAY THROUGH THE FLIGHT THE LEFT ENGINE REVERSE THRUST LIGHT ILLUMINATED.
- [SDR USAAD99170](https://openairdocs.org/sdr/USAAD99170.md): Battery · discharged · Dec 2, 1999 · N823US · Doug DC982 · Emergency Lighting
  > CLT - THE CABIN OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES FROM OVERHEAD BINS FIVE RIGHT AND TEN RIGHT. OPS CHECKED OK. (M)
- [SDR USAA991038](https://openairdocs.org/sdr/USAA991038.md): Skin · cracked · Sep 20, 1999 · N823US · Doug DC982 · Fuselage Main, Plate/Skin
  > PIT - DURING RON VISIT, FOUND TWO CRACKS.5 INCH LENGTH IN SKIN AT STATION 58.750 LEFT, 5TH AND 6TH RIVETS BELOW FLOOR LINE. INSTALLED DOUBLER PER SRM 53-01, FIG 4. (M)
- [SDR USAA990123](https://openairdocs.org/sdr/USAA990123.md): Rivet · broken · Feb 22, 1999 · N823US · Doug DC982 · Service Doors
  > PIT - DURING C-3 CHECK, FOUND TWO RIVET HEADS POPPED AT NR 1 HORIZ BEAM FORWARD END ON OUTER SKIN OF SERVICE DOOR. REPAIRED AND REPLACED RIVETS PER SRM 52-01 PAGE 1. (M)
- [SDR USAA990122](https://openairdocs.org/sdr/USAA990122.md): Skin · cracked · Feb 22, 1999 · N823US · Doug DC982 · Fuselage Main, Plate/Skin
  > PIT - DURING C-3 CHECK, FOUND.25 INCH CRACK ON SKIN AT STATION 1380 BETWEEN LONGERONS 13L AND 14L. INSTALLED DOUBLER, STOP DRILLED PER SRM 53-01 FIG 2 SHEET. (M)
- [SDR USAA990121](https://openairdocs.org/sdr/USAA990121.md): Skin · cracked · Feb 22, 1999 · N823US · Doug DC982 · Fuselage Main, Plate/Skin
  > PIT - DURING C-3 CHECK, FOUND.75 INCH CRACK ON SKIN AT STATION 1380 BETWEEN LONGERON 13R AND 14R. INSTALLED DOUBLER, STOP DRILLED PER SRM 53-01 FIG2, SHT 3. (M)
- [SDR USAAD98079](https://openairdocs.org/sdr/USAAD98079.md): Panel · cracked · May 3, 1998 · N823US · Doug DC982 · Flight Compartment Windows
  > CLT - FLT 467 - DURING CLIMB-OUT, THE FIRST OFFICER'S WINDSHIELD GLASS CRACKED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE WINDSHIELD ASSEMBLY AND THE WINDSHIELD HEAT CONTROLLER. REF: OPERATOR CONTROL NR 98ZZZX2
- [SDR 98ZZZX2256](https://openairdocs.org/sdr/98ZZZX2256.md): Control · malfunctioned · May 3, 1998 · N823US · Doug DC982 · Windshield/Door Rain/Ice Removal
  > CLT - FLT 467 - DURING CLIMB-OUT, THE FIRST OFFICER'S WINDSHIELD GLASS CRACKED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE WINDSHIELD ASSEMBLY AND THE WINDSHIELD HEAT CONTROLLER. REF: OPERATOR CONTROL NR USAAD98
- [SDR USAAD97178](https://openairdocs.org/sdr/USAAD97178.md): Engine · failed · Oct 10, 1997 · N823US · Doug DC982 · Engine (Turbine/Turboprop)
  > BDL - FLT 628 - EN ROUTE BOS/CLT, CREW RECEIVED NR 1 OIL STRAINER CLOG LIGHT. CREW REDUCED POWER TO NR 1 ENGINE AND IT BEGAN TO VIBRATE. ENGINE WAS SHUT DOWN. FLIGHT DIVERTED TO BDL AND LANDED WITH NO FURTHER INCIDENT. (SET 20 MINUTES). MAINTENANCE REPLAC
- [SDR USAAD96125](https://openairdocs.org/sdr/USAAD96125.md): Bushing · failed · Sep 7, 1996 · N823US · Doug DC982 · Passenger/Crew Doors
  > FLT 2382 - MCO-DCA - AIRCRAFT WOULD NOT PRESSURIZE ON TAKEOFF, 2L DOOR APPEARED NOT TO SEAL PROPERLY. REPLACED 2L DOOR MECHANISM BUSHING AND SPRING FROM BAYONET. (M)
- [SDR USAA960464](https://openairdocs.org/sdr/USAA960464.md): Fitting · cracked · May 23, 1996 · N823US · Doug DC982 · Fuselage Miscellaneous Structure
  > PIT - DURING A SCHEDULED Q-2/C-6 CHECK INSPECTION, FOUND VENTRAL DOOR JAMB RIGHT OUTBOARD FITTING CRACKED BETWEEN NR 5 AND NR 6 RADIAL. FITTING WAS REPLACED PER 53-14-3, FIGURE 2, AND DACO DRAWING 5917579. (X)
- [SDR USAA960440](https://openairdocs.org/sdr/USAA960440.md): Longeron · cracked · May 23, 1996 · N823US · Doug DC982 · Fuselage Main, Longeron/Stringer
  > PIT - DURING A SCHEDULED Q-2/C-6 CHECK INSPECTION, FOUND A.50 INCH CRACK IN LONGERON 17L LOWER FASTENER TO FRAME AT STA 256, VISUALLY. SPLICED IN NEW SECTION OF LONGERON STA 230 TO STA 273 PER SRM 53-02, FIGURE 2. (X)
- [SDR USAAD96005](https://openairdocs.org/sdr/USAAD96005.md): Retract Mech · malfunctioned · Jan 20, 1996 · N823US · Doug DC982 · Landing Gear Retraction/Extension System
  > MCO - AFTER TAKEOFF FROM MCO, NOSE GEAR WOULD NOT RETRACT. FLIGHT RETURNED TO MCO AND LANDED WITH NO FURTHER INCIDENT. (M)
- [SDR USAAD96005A](https://openairdocs.org/sdr/USAAD96005A.md): Bolts · missing · Jan 10, 1996 · N823US · Doug DC982 · Landing Gear Retraction/Extension System
  > MCO - AFTER TAKEOFF FROM MCO, NOSE GEAR WOULD NOT RETRACT. CREW TRIED TO CYCLE THE GEAR TO NO AVAIL. FLIGHT RETURNED TO MCO AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED BOLTS IN THE NOSE GEAR SPRAY DEFLECTOR AND LUBED THE GEAR. (M)
- [SDR USAA950550](https://openairdocs.org/sdr/USAA950550.md): Cylinder · leaking · Jun 7, 1995 · N823US · Doug DC982 · Landing Gear Actuator
  > PHL - FLT NR 1468 - PRIOR TO FLAP EXTENSION, THE RIGHT HYDRAULIC QUANTITY DROPPED TO TWO QUARTS. EMERGENCY WAS DECLARED. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE RIGHT MAIN LANDING GEAR RETRACT ACTUATOR LEAKING AT THE CYLINDER AND REPLACED
- [SDR USAA950155](https://openairdocs.org/sdr/USAA950155.md): Harness · misaligned · Feb 16, 1995 · N823US · Doug DC982 · Landing Gear Position and Warning
  > PIT - FLIGHT 1181 - AFTER TAKEOFF, THE RIGHT MAIN GEAR UNSAFE LIGHT ILLUMINATED. THE CREW RECYCLED THE GEAR AND GOT THREE GREEN LIGHTS. AFTER THE SECOND RETRACTION THE UNSAFE LIGHT STILL REMAINED ILLUMINATED. ON FINAL APPROACH JUST BEFORE GEAR EXTENSION, TH

## 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 = 'N823US' AND deregistration_id = 'N823US-2004-03-18'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N823US-2004-03-18/reports

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