N820US, cancelled Feb 12, 2003

Service difficulty reports · 30

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 = 'N820US' AND deregistration_id = 'N820US-2003-02-12'
  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 USAAD01116Battery · dischargedPIT - THE FORWARD SECTION OF OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)May 27, 2001 · N820US · Doug DC982 · Emergency LightingSDR USAAD010172Power Supply · failedPIT - 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)Mar 30, 2001 · N820US · Doug DC982 · Emergency LightingSDR USAA010413Skin · crackedPIT - 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)Mar 23, 2001 · N820US · Doug DC982 · Fuselage Main, Plate/SkinSDR USAA010412Skin · crackedBOS - FOUND SKIN CRACKED .375 INCH, ACCESS DOOR 6102A STATION 1474 AT LONGERON 23R. INSTALLED DOUBLER PER EA 57939A. (M)Mar 22, 2001 · N820US · Doug DC982 · Fuselage Main, Plate/SkinSDR USAAD01008Battery · dischargedCLT - 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)Jan 11, 2001 · N820US · Doug DC982 · Emergency LightingSDR USAAD00101Switch · failedPHL-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 INCIDEJun 23, 2000 · N820US · Doug DC982 · Visual Omnirange (VOR) SystemSDR USAA000830Skin · crackedPIT - 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)Jun 9, 2000 · N820US · Doug DC982 · Fuselage Main, Plate/SkinSDR USAA000829Pan · crackedPIT - 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)Jun 8, 2000 · N820US · Doug DC982 · Emergency ExitsSDR USAA000823Skin · crackedPIT - 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)Jun 2, 2000 · N820US · Doug DC982 · Fuselage Main, Plate/SkinSDR USAA000818Doubler · crackedPIT - 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)Jun 2, 2000 · N820US · Doug DC982 · Fuselage Miscellaneous StructureSDR USAA990892Pan · crackedPIT - 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)Aug 19, 1999 · N820US · Doug DC982 · Landing Gear DoorsSDR USAA990891Rib · crackedPIT - 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)Aug 19, 1999 · N820US · Doug DC982 · Landing Gear DoorsSDR USAA990890Hinge · brokenPIT - DURING C2 CHECK, FOUND HINGE LUG BROKEN, RIGHT MLG DOOR. REPLACED WITH IDENTICAL PART PER DOUGLAS DRAWING SR09520022. (M)Aug 19, 1999 · N820US · Doug DC982 · Landing Gear DoorsSDR USAAD99035Indicator · fluctuationPIT-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 OPMar 3, 1999 · N820US · Doug DC982 · Engine EGT/TIT Indicating SystemSDR USAAD98171Engine · failedATL/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)Oct 2, 1998 · N820US · Doug DC982 · Engine (Turbine/Turboprop)SDR USAA980410Skin · crackedPIT - 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)Sep 11, 1998 · N820US · Doug DC982 · Fuselage Main, Plate/SkinSDR USAA980394Longeron · crackedPIT - 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)Sep 10, 1998 · N820US · Doug DC982 · Fuselage Main, Longeron/StringerSDR USAAD98150Battery · dischargedIND - THE FORWARD CABIN CEILING EMERGENCY LIGHTS WERE DIM. MAINTENANCE REPLACED THE BATTERIES. (M)Aug 22, 1998 · N820US · Doug DC982 · Emergency LightingSDR USAAD98122Battery · dischargedPIT - 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)Jul 10, 1998 · N820US · Doug DC982 · Emergency LightingSDR 98ZZZM554Light · inoperativePIT - 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)Jul 10, 1998 · N820US · Doug DC982 · Emergency LightingSDR USAAD98096Battery · dischargedLGA - 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 May 26, 1998 · N820US · Doug DC982 · Emergency LightingSDR 98ZZZM492Battery · failedLGA - 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 May 26, 1998 · N820US · Doug DC982 · Emergency LightingSDR USAAD98067Engine · failedMCO - 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.Apr 13, 1998 · N820US · Doug DC982 · Engine (Turbine/Turboprop)SDR USAAD98065Battery · dischargedDCA - FOUR LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE LOW LEVEL EMERGENCY LIGHT BATTERIES. (X)Apr 7, 1998 · N820US · Doug DC982 · Emergency LightingSDR USAAD97042Engine · failedFLT 821 - SRQ-PHL - IN CRUISE AT FL 330, THE RIGHT ENGINE FAILED. SHUT ENGINE DOWN AND DIVERTED TO CLT. REPLACED RIGHT ENGINE. (M)Feb 21, 1997 · N820US · Doug DC982 · Engine (Turbine/Turboprop)SDR USAA960058Bulkhead · chaffedPIT - 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)Jan 19, 1996 · N820US · Doug DC982 · Fuselage Main, BulkheadSDR USAA960057Bulkhead · chaffedPIT - 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)Jan 19, 1996 · N820US · Doug DC982 · Fuselage Main, BulkheadSDR USAA960056Skin · crackedPIT - 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)Jan 19, 1996 · N820US · Doug DC982 · Fuselage Main, Plate/SkinSDR USAA960004Skin · crackedPIT - 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)Jan 19, 1996 · N820US · Doug DC982 · Fuselage Main, Plate/SkinSDR USAA950525Eel Power Supply · inoperativeCAE - THE EMERGENCY LIGHTS WOULD NOT SHUT OFF. MAINTENANCE REPLACED THE POWER SUPPLY. (W)May 12, 1995 · N820US · Doug DC982 · Emergency Lighting
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