# Service difficulty reports: N820US, cancelled Feb 12, 2003 A list on [N820US, cancelled Feb 12, 2003](https://openairdocs.org/deregistered/N820US-2003-02-12.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR USAAD01116](https://openairdocs.org/sdr/USAAD01116.md): Battery · discharged · May 27, 2001 · N820US · Doug DC982 · Emergency Lighting > PIT - THE FORWARD SECTION OF OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M) - [SDR USAAD010172](https://openairdocs.org/sdr/USAAD010172.md): Power Supply · failed · Mar 30, 2001 · N820US · Doug DC982 · Emergency Lighting > PIT - THE ENTRY WAY EMERGENCY LIGHTS WILL NOT STAY OFF WHEN ELECTICAL POWER IS REMOVED FROM THE AIRCRAFT. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY. (M) - [SDR USAA010413](https://openairdocs.org/sdr/USAA010413.md): Skin · cracked · Mar 23, 2001 · N820US · Doug DC982 · Fuselage Main, Plate/Skin > PIT - FOUND SKIN CRACKED.75 INCH AND PREVIOUS CRACK.25 INCH, STOP DRILLED AND PATCHED AT STATION 1437 L3L. CUT OUT DAMAGE, INSTALLED FILLER AND DOUBLER PER SRM 53-04, FIG 27. (M) - [SDR USAA010412](https://openairdocs.org/sdr/USAA010412.md): Skin · cracked · Mar 22, 2001 · N820US · Doug DC982 · Fuselage Main, Plate/Skin > BOS - FOUND SKIN CRACKED.375 INCH, ACCESS DOOR 6102A STATION 1474 AT LONGERON 23R. INSTALLED DOUBLER PER EA 57939A. (M) - [SDR USAAD01008](https://openairdocs.org/sdr/USAAD01008.md): Battery · discharged · Jan 11, 2001 · N820US · Doug DC982 · Emergency Lighting > CLT - THE EMERGENCY LIGHTS DID NOT COME ON WHEN EXTERNAL POWER FELL OFF LINE. MAINTENANCE REPLACED THE BATTERIES IN THE FORWARD ENTRY EMERGENCY LIGHT PACK. (M) - [SDR USAAD00101](https://openairdocs.org/sdr/USAAD00101.md): Switch · failed · Jun 23, 2000 · N820US · Doug DC982 · Visual Omnirange (VOR) System > PHL-MCO - FLT 1127 - DURING CLIMB-OUT, THE CAPTAINS NAV CDI NEEDLE WAS INOPERATIVE. SWITCHING THE RADIO SELECTOR TO BOTH ON 2 CDI DID NOT HELP. THE RMI NEEDLE POINTED CORRECTLY AND THE DME WORKED. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDE - [SDR USAA000830](https://openairdocs.org/sdr/USAA000830.md): Skin · cracked · Jun 9, 2000 · N820US · Doug DC982 · Fuselage Main, Plate/Skin > PIT - FOUND SKIN CRACKED.25 INCH AND.125 INCH FROM RIVET, STATION 76.5 LONG 2R. CUT OUT DAMAGE, INSTALLED INTERNAL DOUBLER AND FILLER PER SRM 53-04 FIG 38, VIEW L. (M) - [SDR USAA000829](https://openairdocs.org/sdr/USAA000829.md): Pan · cracked · Jun 8, 2000 · N820US · Doug DC982 · Emergency Exits > PIT - FOUND TWO 1 INCH LONG CRACKS, PAN BOTTOM LT NR 7 STOP AREA, LT TOP NR 12 STOP AREA. STOP DRILLED CRACK AND INSTALLED DOUBLER PER T/R 52-20-03 AND SRM 52-05 PAGE 299 FIG 5 (SHT 3). (M) - [SDR USAA000823](https://openairdocs.org/sdr/USAA000823.md): Skin · cracked · Jun 2, 2000 · N820US · Doug DC982 · Fuselage Main, Plate/Skin > PIT - FOUND TWO CRACKS.25 INCH AND.125 INCH FROM RIVET, ON SKIN AT STATION 76.5 LONGERON 2R. CUT OUT DAMAGE AND INSTALLED TITANIUM DOUBLER PER SRM 53-04 FIG 38 VIEW L. (M) - [SDR USAA000818](https://openairdocs.org/sdr/USAA000818.md): Doubler · cracked · Jun 2, 2000 · N820US · Doug DC982 · Fuselage Miscellaneous Structure > PIT - FOUND DOUBLER CRACKED 1 INCH, UPPER LT SIDE OF VENTRAL DOOR JAMB DOUBLER AFT RADIUS. REPLACED CRACKED SLIPS AND CRACKED ANGLE PER SRM 53-05 FIG 30. (M) - [SDR USAA990892](https://openairdocs.org/sdr/USAA990892.md): Pan · cracked · Aug 19, 1999 · N820US · Doug DC982 · Landing Gear Doors > PIT - DURING C2 CHECK, FOUND CRACK 1.5 INCH LONG AT RT MAIN LANDING GEAR DOOR FORWARD INBOARD CORNER OF PAN. INSTALLED FACTORY DOUBLER J06020038 PER SRM 52-05 FIG 28. (M) - [SDR USAA990891](https://openairdocs.org/sdr/USAA990891.md): Rib · cracked · Aug 19, 1999 · N820US · Doug DC982 · Landing Gear Doors > PIT - DURING C2 CHECK, FOUND 3.5 CRACK IN RT MLG DOOR OUTER SKIN AT GROUND SKID RIB FRAME 4/5, NR 4 RIB CRACKED. INSTALLED TYPICAL REPAIR TO FRAME RIB NR 4 PER EA 52695. (M) - [SDR USAA990890](https://openairdocs.org/sdr/USAA990890.md): Hinge · broken · Aug 19, 1999 · N820US · Doug DC982 · Landing Gear Doors > PIT - DURING C2 CHECK, FOUND HINGE LUG BROKEN, RIGHT MLG DOOR. REPLACED WITH IDENTICAL PART PER DOUGLAS DRAWING SR09520022. (M) - [SDR USAAD99035](https://openairdocs.org/sdr/USAAD99035.md): Indicator · fluctuation · Mar 3, 1999 · N820US · Doug DC982 · Engine EGT/TIT Indicating System > PIT-PBI - FLT 1807 - THE RIGHT ENGINE STARTED TOWARDS EXCEEDING MCP (580) WHEN APPLYING CLIMB POWER WHEN CLEARED TO CLIMB TO 14,000 FT. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT ENGINE EGT INDICATOR AND OP - [SDR USAAD98171](https://openairdocs.org/sdr/USAAD98171.md): Engine · failed · Oct 2, 1998 · N820US · Doug DC982 · Engine (Turbine/Turboprop) > ATL/PIT - FLT 592 - EN ROUTE, LT ENGINE BEGAN TO VIBRATE SEVERELY. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT CONTINUED TO THE DISTINATION AND LANDED WITHOUT INCIDENT. 12 MINUTES SINGLE ENGINE TIME. MAINTENANCE REPLACED THE LEFT ENGINE. (X) - [SDR USAA980410](https://openairdocs.org/sdr/USAA980410.md): Skin · cracked · Sep 11, 1998 · N820US · Doug DC982 · Fuselage Main, Plate/Skin > PIT - DURING C-1 CHECK, FOUND 2 INCH CRACK AT DOUBLER STATION 1429 BETWEEN LONGERON 2-3 RIGHT. CUT OUT CRACK SECTION, INSTALLED DOUBLER PER EA 50498. (M) - [SDR USAA980394](https://openairdocs.org/sdr/USAA980394.md): Longeron · cracked · Sep 10, 1998 · N820US · Doug DC982 · Fuselage Main, Longeron/Stringer > PIT - DURING C-1 CHECK, FOUND TWO CRACKS 2 INCHES LONG AT STATION 1437, LONGERON 2-3 AND 3-4 RIGHT. INSTALLED DOUBLERS PER SRM 53-04 FIG 27. (M) - [SDR USAAD98150](https://openairdocs.org/sdr/USAAD98150.md): Battery · discharged · Aug 22, 1998 · N820US · Doug DC982 · Emergency Lighting > IND - THE FORWARD CABIN CEILING EMERGENCY LIGHTS WERE DIM. MAINTENANCE REPLACED THE BATTERIES. (M) - [SDR USAAD98122](https://openairdocs.org/sdr/USAAD98122.md): Battery · discharged · Jul 10, 1998 · N820US · Doug DC982 · Emergency Lighting > PIT - THE LOW LEVEL EMERGENCY LIGHTS WERE DIM AND THE LIGHT AT ROW 16 WAS INOPERATIVE. MAINTENANCE REPLACED ALL THE LOW LEVEL EMERGENCY LIGHT BATTERIES AND THE LIGHT ASSEMBLY AT ROW 16. (M) - [SDR 98ZZZM554](https://openairdocs.org/sdr/98ZZZM554.md): Light · inoperative · Jul 10, 1998 · N820US · Doug DC982 · Emergency Lighting > PIT - THE LOW LEVEL EMERGENCY LIGHTS WERE DIM AND THE LIGHT AT ROW 16 WAS INOPERATIVE. MAINTENANCE REPLACED ALL THE LOW LEVEL EMERGENCY LIGHT BATTERIES AND THE LIGHT ASSEMBLY AT ROW 16. (M) - [SDR USAAD98096](https://openairdocs.org/sdr/USAAD98096.md): Battery · discharged · May 26, 1998 · N820US · Doug DC982 · Emergency Lighting > LGA - THE LEFT AND RIGHT FORWARD OVERWING EMERGENCY LIGHTS WERE INOPERATIVE AND THE REMOTE TAILCONE LOW LEVEL LIGHT RECEIVER GREEN LIGHT DID NOT ILLUMINATE DURING TEST. MAINTENANCE REPLACED THE FORWARD OVERWING EMERGENCY LIGHT BATTERY AND THE REMOTE TAILCONE - [SDR 98ZZZM492](https://openairdocs.org/sdr/98ZZZM492.md): Battery · failed · May 26, 1998 · N820US · Doug DC982 · Emergency Lighting > LGA - THE LEFT AND RIGHT FORWARD OVERWING EMERGENCY LIGHTS WERE INOPERATIVE AND THE REMOTE TAILCONE LOW LEVEL LIGHT RECEIVER GREEN LIGHT DID NOT ILLUMINATE DURING TEST. MAINTENANCE REPLACED THE FORWARD OVERWING EMERGENCY LIGHT BATTERY AND THE REMOTE TAILCONE - [SDR USAAD98067](https://openairdocs.org/sdr/USAAD98067.md): Engine · failed · Apr 13, 1998 · N820US · Doug DC982 · Engine (Turbine/Turboprop) > MCO - FLT 1554 - DURING CLIMB A VIBRATION WAS FELT COMING FROM NUMBER 2 ENGINE, FOLLOWED BY AN OIL CLOG LIGHT ILLUMINATING. THE ENGINE THRUST WAS REDUCED IDLE AND THE AIRCRAFT DIVERTED TO MCO AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 ENGINE. - [SDR USAAD98065](https://openairdocs.org/sdr/USAAD98065.md): Battery · discharged · Apr 7, 1998 · N820US · Doug DC982 · Emergency Lighting > DCA - FOUR LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE LOW LEVEL EMERGENCY LIGHT BATTERIES. (X) - [SDR USAAD97042](https://openairdocs.org/sdr/USAAD97042.md): Engine · failed · Feb 21, 1997 · N820US · Doug DC982 · Engine (Turbine/Turboprop) > FLT 821 - SRQ-PHL - IN CRUISE AT FL 330, THE RIGHT ENGINE FAILED. SHUT ENGINE DOWN AND DIVERTED TO CLT. REPLACED RIGHT ENGINE. (M) - [SDR USAA960058](https://openairdocs.org/sdr/USAA960058.md): Bulkhead · chaffed · Jan 19, 1996 · N820US · Doug DC982 · Fuselage Main, Bulkhead > PIT - DURING Q-6 INSPECTION, FOUND TWO CHAFFED 4 INCH RADIUS AREAS FROM RIGHT ENGINE THRUST REVERSER CABLE DRUM SHAFT BOLT HEADS IN STATION 1338 AFT PRESSURE BULKHEAD AFT SIDE. INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 78-30-14. (M) - [SDR USAA960057](https://openairdocs.org/sdr/USAA960057.md): Bulkhead · chaffed · Jan 19, 1996 · N820US · Doug DC982 · Fuselage Main, Bulkhead > PIT - DURING Q-6 INSPECTION, FOUND TWO CHAFFED 4 INCH RADIUS AREAS FROM LEFT ENGINE THRUST REVERSER CABLE DRUM SHAFT BOLT HEADS IN STATION 1338 AFT PRESSURE BULKHEAD AFT SIDE. INSTALLED DOUBLER REPAIR PER USAIR TYPICAL REPAIR 78-30-14. (M) - [SDR USAA960056](https://openairdocs.org/sdr/USAA960056.md): Skin · cracked · Jan 19, 1996 · N820US · Doug DC982 · Fuselage Main, Plate/Skin > PIT - DURING Q-6 INSPECTION, FOUND A.5 INCH CRACK STATION 101 RIGHT SIDE LEADING EDGE OF STROBE IN SKIN. REMOVED DAMAGED AREA AND INSTALLED FILLER AND DOUBLER REPAIR PER USAIR TYPICAL REPAIR 53-30-11. (M) - [SDR USAA960004](https://openairdocs.org/sdr/USAA960004.md): Skin · cracked · Jan 19, 1996 · N820US · Doug DC982 · Fuselage Main, Plate/Skin > PIT - DURING Q-6 CHECK INSPECTION, FOUND A.25 INCH CRACK COMING FROM RIVET AT STA 101, LEFT AFT OF STRAKE IN SKIN. REMOVED DAMAGED AREA AND INSTALLED DOUBLER AND FILLER REPAIR PER USAIR TYPICAL REPAIR 53-30-11. (X) - [SDR USAA950525](https://openairdocs.org/sdr/USAA950525.md): Eel Power Supply · inoperative · May 12, 1995 · N820US · Doug DC982 · Emergency Lighting > CAE - THE EMERGENCY LIGHTS WOULD NOT SHUT OFF. MAINTENANCE REPLACED THE POWER SUPPLY. (W) ## 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 = 'N820US' AND deregistration_id = 'N820US-2003-02-12' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N820US-2003-02-12/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.