N815US, cancelled May 9, 2003

Service difficulty reports · 39

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 = 'N815US' AND deregistration_id = 'N815US-2003-05-09'
  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 COOSDR02219Web · corrodedIN THE PASSENGER CABIN AT THE MAIN ENTRY DOOR AT STA 160.0, LONGERON 18 LT LOWER CUSP WEB HAS CORROSION.Aug 1, 2002 · N815US · Doug DC982 · Fuselage Miscellaneous StructureSDR USAAD01182Link · brokenMDT-PIT - FLT 1532 - AFTER TAKEOFF AND LANDING GEAR RETRACTION, THE LEFT MAIN GEAR UNSAFE LIGHT REMAINED ILLUMINATED. THE LANDING GEAR WAS CYCLED. THE GEAR INDICATED ALL THREE GREEN WITH THE LANDING GEAR EXTENDED, BUT BOTH MAIN LANDING GEARS INDICATED UNSAFENov 22, 2001 · N815US · Doug DC982 · Landing Gear ActuatorSDR USAAD01177Battery · dischargedIND - THE SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS AND THE TAIL CONE REMOTE EMERGENCY LIGHT RECEIVER BATTERY WERE INOPERATIVE. MAINTENANCE REPLACED THE LOW LEVEL EMERGENCY LIGHT AND REMOTE RECEIVER BATTERIES. (M)Nov 1, 2001 · N815US · Doug DC982 · Emergency LightingSDR 2001F00379Battery · dischargedIND - THE TAILCONE EMERGENCY LIGHT RECEIVER, SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS, AND THE CEILING EMERGENCY LIGHTS FOR SEAT ROWS 1 THROUGH 8 WERE INOPERATIVE. MAINTENANCE REPLACED THE TAILCONE EMERGENCY LIGHT REMOTE RECEIVER, AND THE LOW LEVEL AND CEILINGAug 24, 2001 · N815US · Doug DC982 · Emergency LightingSDR 2001F00375Receiver · failedIND - THE TAILCONE EMERGENCY LIGHT RECEIVER, SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS, AND THE CEILING EMERGENCY LIGHTS FOR SEAT ROWS 1 THROUGH 8 WERE INOPERATIVE. MAINTENANCE REPLACED THE TAILCONE EMERGENCY LIGHT REMOTE RECEIVER, AND THE LOW LEVEL AND CEILINGAug 24, 2001 · N815US · Doug DC982 · Emergency LightingSDR USAAD01153Receiver · failedIND - THE TAILCONE EMERGENCY LIGHT RECEIVER, SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS, AND THE CEILING EMERGENCY LIGHTS FOR SEAT ROWS 1 THROUGH 8 WERE INOPERATIVE. MAINTENANCE REPLACED THE TAILCONE EMERGENCY LIGHT REMOTE RECEIVER, AND THE LOW LEVEL AND CEILINGAug 24, 2001 · N815US · Doug DC982 · Emergency LightingSDR USAAD01104Sign · burnedPIT - THE FORWARD RIGHT EMERGENCY WINDOW EXIT IDENTIFIER WAS BURNED AND MELTED. MAINTENANCE REPLACED THE EXIT IDENTIFIER. (M)May 15, 2001 · N815US · Doug DC982 · Emergency LightingSDR USAAD01080Warning System · activatedCLT-EWR - FLT 1744 - AFTER TAKEOFF AND LANING GEAR RETRACTION, THE LEFT GEAR RED UNSAFE LIGHT AND THE AMBER GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED. THE LANDING GEAR WAS CYCLED WITH NO CHANGE, BUT GEAR DOWN INDICATIONS WERE NORMAL. THE AIRCRAFT CONTINUED TApr 11, 2001 · N815US · Doug DC982 · Landing Gear Position and WarningSDR USAAD01055Battery · dischargedBOS - THE CENTER SECTION OF THE CEILING EMERGENCY LIGHTS AND THE OVERWING EXIT EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)Mar 17, 2001 · N815US · Doug DC982 · Emergency LightingSDR USAA001329Skin · crackedPIT - FOUND SKIN CRACKED 1.5 INCHES LONG, STATION 1474 LEFT SIDE 16 INCHES ABOVE AFT STAIR CUTOUT. STOP DRILLED CRACK AND INSTALLED EXT DOUBLER PER SRM 53-01 FIG 2 (SHT 3) AND EA 56070. (M)Aug 12, 2000 · N815US · Doug DC982 · Fuselage Main, Plate/SkinSDR USAA000644Longeron · corrodedCLT - FOUND LONGERON .5 INCH BY .2 INCH AREA, CORROSION LEVEL 1, LONGERON 30 BETWEEN STATION 579 AND 598. CLEANED, TREATED AND PRIMED. (M)Apr 28, 2000 · N815US · Doug DC982 · Fuselage Main, Longeron/StringerSDR USAA000667Flange · corrodedPIT - FOUND LOWER FLANGED CORRODED 2 INCHES BY 3 INCHES, STATION 1309 LONGERON 28L AND 28R LOWER FLANGE OF BELT FRAME. REPLACED FLANGE PER SRM 53-03 PAGE 4G FIG 2A. (M)Apr 8, 2000 · N815US · Doug DC982 · Fuselage Miscellaneous StructureSDR USAA000550Skin · corrodedPIT - FOUND SKIN CRACK AND RIVET PULLED FROM CORROSION, STATION 256 LONGERON 28 AND 29 LEFT. CUT SKIN, INSTALLED NEW SECTION AND SPLICED PER EA 54603. (M)Apr 8, 2000 · N815US · Doug DC982 · Fuselage Main, Plate/SkinSDR USAA000642Doubler · corrodedPIT - FOUND DOUBLER CORRODED, .5 INCH BY .5 INCH AREA, BETWEEN 579 AND 598, 28L AND 30. CORROSION LEVEL 1. CLEANED, TREATED AND PRIMED. (M)Apr 7, 2000 · N815US · Doug DC982 · Fuselage Main, StructureSDR USAA000544Longeron · crackedPIT - FOUND LONGERON CRACKED .75 INCHES, STATION 160 LONGERON 4L. SPLICED LONGERON PER SRM 53-02. (M)Apr 1, 2000 · N815US · Doug DC982 · Fuselage Main, Longeron/StringerSDR USAA000547Longeron · crackedPIT - FOUND LONGERON CRACKED .5 INCH, BS 160 LONGERON 2L. SPLICED IN LONGERON PER 53-02-18. (M)Apr 1, 2000 · N815US · Doug DC982 · Fuselage Main, Longeron/StringerSDR USAA000643Frame · corrodedPIT - FOUND FRAME CRACKED 1 INCH BY 2 INCH AREA, STATION 598 AT LONGERON 30L. CORROSION LEVEL 1. CLEANED, TREATED AND PRIMED. (M)Mar 31, 2000 · N815US · Doug DC982 · Fuselage Main, FrameSDR USAA000645Skin · corrodedPIT - FOUND SKIN CORRODED .5 INCH BY 1 INCH AREA, STATION 598 FRONT SIDE OF ANTENNA DOUBLER. CLEANED, TREATED AND PRIMED. (M)Mar 31, 2000 · N815US · Doug DC982 · Fuselage Main, Plate/SkinSDR USAAD99076Battery · dischargedPIT - FOUND FLOOR LEVEL EMERGNECY LIGHTS IN ROWS 1, 3, 11, 16 AND 19 INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES. (M)Jun 7, 1999 · N815US · Doug DC982 · Emergency LightingSDR USAA990266Frame · crackedPIT - DURING C-06 CHECK, FOUND 1.5 INCH CRACK AT CANTED FRAME 1416 AT LONGERON 6L. STOP DRILLED WITH .25 INCH DRILL (TEMP REPAIR) PER EA 51797. (M)Mar 26, 1999 · N815US · Doug DC982 · Fuselage Main, FrameSDR USAA990265Frame · crackedPIT - DURING C-06 CHECK, FOUND 1.5 INCH CRACK AT CANTED FRAME 1416 AT LONGERON 6R. STOP DRILLED WITH .25 INCH DRILL (TEMP REPAIR) PER EA 51797. (M)Mar 26, 1999 · N815US · Doug DC982 · Fuselage Main, FrameSDR USAA990264Frame · crackedPIT - DURING C-06 CHECK, FOUND 4 INCH CRACK AT CANTED FRAME WEB STATION 1463 BETWEEN LONGERON 8 AND 9R. SPLICED IN SECTION. REPAIRED PER EA TYPICAL REPAIR 53-10-25. (M)Mar 26, 1999 · N815US · Doug DC982 · Fuselage Main, FrameSDR USAAD98210Retract Mech · lack of lubeDFW-PIT - FLT 1220 - DURING GEAR EXTENSION PRIOR TO LANDING, THE CREW RECEIVED A LEFT MAIN GEAR UNSAFE INDICATION. THE GEAR WAS CYCLED WITH THE SAME RESULT. THE EMERGENCY EXTENSION HANDLE WAS PULLED BUT STILL HAD THE UNSAFE LIGHT. THE EMERGENCY GEAR EXTENSINov 21, 1998 · N815US · Doug DC982 · Landing Gear Retraction/Extension SystemSDR USAAD98180Latch · looseBOS-CLT - FLT 1524 - ON ROTATION, THE ARICRAFT WOULD NOT PRESSURIZE. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE FORWARD 2 ACCESSORY HATCH LOCK ARMS UNSNAPPED. THE LOCKS WERE SECURED AND ALL CHECKED NORMAL. (M)Oct 11, 1998 · N815US · Doug DC982 · Service DoorsSDR USAAD97157Power Supply · inoperativeLGA - EXTERIOR EMERGENCY LIGHTS STAY ON WITH SWITCH IN ARMED POSITION. MAINTENANCE REPLACED THE BATTERY AND POWER SUPPLY. (X)Sep 15, 1997 · N815US · Doug DC982 · Emergency LightingSDR USAAD97067Bungee Cylinder · failedFLT 1745 - BNA-DCA - NOSE GEAR DID NOT EXTEND ON APPROACH. RECYCLED GEAR, NO CHANGE. USED EMERGENCY EXTENSION, LANDED NORMALLY. REPLACED NOSE GEAR BUNGEE CYLINDER. OPS CHECK GOOD. (M)Apr 9, 1997 · N815US · Doug DC982 · Landing Gear Retraction/Extension SystemSDR USAAD96114Manifold · failedFLT NR 1085 - PIT-TPA - AFTER TAKEOFF, RIGHT AIR CONDITIONING SUPPLY TEMP HI LIGHT ILLUMINATED, FOLLOWED BY RIGHT ENGINE FIRE LIGHT. EXTINGUISHED WHEN THROTTLE WAS RETARDED. RETURNED TO FIELD. REPLACED RIGHT ENGINE 8TH STAGE BLEED MANIFOLD DUE TO LEAK. (M)Aug 11, 1996 · N815US · Doug DC982 · Pneumatic Distribution SystemSDR USAA951112Seat Track · corrodedPIT - DURING Q-6/C-2 INSPECTION, FOUND LEVEL 1 CORROSION AT STATION 1297, LEFT INBOARD SEAT TRACK. REPLACED SECTION OF SEAT TRACK PER SRM 53-05 FIG 4. (M)Oct 4, 1995 · N815US · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR USAA951111Pan · crackedPIT - DURING Q-6/C-2 INSPECTION, FOUND .25 INCH CRACK, LEFT AFT EMERGENCY EXIT DOOR TOP PAN LEFT STOP. SID REF 52-21-003. REMOVED AND REPLACED EXIT DOOR. (M)Oct 4, 1995 · N815US · Doug DC982 · Emergency ExitsSDR USAA951110Jamb · crackedPIT - DURING Q-6/C-2 INSPECTION, FOUND .25 INCH CRACK AFT JAMB BETWEEN 2ND AND 3RD STOPS FOR BOTTOM (FORWARD CARGO). INSTALLED PERMANENT REPAIR PER 53-05 FIG 4 AND USAIR EA NR 27454. (M)Oct 4, 1995 · N815US · Doug DC982 · Fuselage Miscellaneous StructureSDR USAA951109Seat Track · corrodedPIT - DURING Q-6/C-2 INSPECTION, FOUND LEVEL 1 CORROSION AT STATION 256 LEFT INBOARD SEAT TRACK. CORROSION TASK NR C58-53302. REPLACED SEAT TRACK SECTION PER SRM 53-05 FIG 4. (M)Oct 4, 1995 · N815US · Doug DC982 · Fuselage, Seat/Cargo Attach FittingsSDR USAA951108Skin · damagedPIT - DURING Q-6/C-2 INSPECTION, FOUND PREVIOUS REPAIR CLASS 3, UPPER AFT AREA OF MED SKIN. REMOVED PREVIOUS REPAIR AND INSTALLED CLASS 1 REPAIR PER SRM 53-04 FIG 38. (M)Oct 4, 1995 · N815US · Doug DC982 · Passenger/Crew DoorsSDR USAA951107Doubler · crackedPIT - DURING Q-6/C-2 INSPECTION, FOUND 2 INCH CRACK LONGERON 30 SPLICE DOUBLER BETWEEN STATION 484 AND 503. REPLACED SPLICE DOUBLER PER SRM 53-02. (M)Oct 4, 1995 · N815US · Doug DC982 · Fuselage Miscellaneous StructureSDR USAA951105Intercostal · crackedPIT - DURING Q-6/C-2 INSPECTION, FOUND .25 INCH CRACK AT STATION 1510 LONGERON 20 LEFT. INSTALLED DOUBLER REPAIR PER SRM 51-01. (M)Oct 4, 1995 · N815US · Doug DC982 · Fuselage Miscellaneous StructureSDR USAA951103Frame · crackedPIT - DURING Q-6/C-2 INSPECTION, FOUND 1.5 INCH CRACK STATION 1437, LONGERON 12L IN FRAME WEB. REPLACED CRACKED FRAME AND INSTALLED DOUBLER 7075 T-6 .050 PER SRM 53-01 FIG 2. (M)Oct 4, 1995 · N815US · Doug DC982 · Fuselage Main, FrameSDR USAA951104Pan · crackedPIT - DURING Q-6/C-2 INSPECTION, FOUND 1.5 INCH CRACK LEFT FORWARD EMERGENCY EXIT DOOR (OVER WING EXIT). STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 52-20-03 FIG 1. (M)Oct 2, 1995 · N815US · Doug DC982 · Emergency ExitsSDR USAA951091Skin · corrodedPIT - DURING Q-6/C-2 INSPECTION, FOUND LEVEL 2 SKIN CORROSION .063 DEEP AROUND FILLET SCREW HOLE STATION 807, LONGERON 29R AREA. CORROSION TASK NR C22-57301. REMOVED CORROSION AND ACCOMPLISHED DOUBLER REPAIR PER SRM 53-14 FIG 53. (M)Sep 20, 1995 · N815US · Doug DC982 · Fuselage Main, Plate/SkinSDR USAA951102Jamb · crackedPIT - DURING Q-6/C-2 INSPECTION, FOUND .025 INCH CRACK ROUTED OUT TO A . 375 INCH HOLE IN AFT DOOR JAMB, FORWARD CARGO BETWEEN 2ND AND 3RD STOP. INSTALLED DOUBLER REPAIR PER USAIR EA NR 27454 REV A. (M)Sep 18, 1995 · N815US · Doug DC982 · Fuselage Miscellaneous StructureSDR USAA951106Skin · damagedPIT - DURING Q-6/C-2 INSPECTION, FOUND SKIN DAMAGE 2 INCH BY .5 INCH ON DOOR FRAME AREA STATION 1211, AFT CARGO DOOR. INSTALLED FILLER AND DOUBLER REPAIR (EXTERNAL) PER SRM 53-05 FIG 80. (M)Sep 11, 1995 · N815US · Doug DC982 · Fuselage Main, Plate/Skin
Back to N815US, cancelled May 9, 2003