N822US, cancelled Jul 31, 2006

Service difficulty reports · 41

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 = 'N822US' AND deregistration_id = 'N822US-2006-07-31'
  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 USAAD02013Battery · dischargedPIT - THE SEAT MOUNTED AND TAILCONE EMERGENCY LIGHT BATTERIES INDICATED LOW. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)Feb 18, 2002 · N822US · Doug DC982 · Emergency LightingSDR USAAF01086Battery · dischargedORF - THE FORWARD EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M)Dec 14, 2001 · N822US · Doug DC982 · Emergency LightingSDR 2002F00001Receiver · failedIND - THE SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS WERE DIM AND THE TAILCONE REMOTE RECEIVER WAS INOPERATIVE. MAINTENANCE REPLACED THE LOW LEVEL EMERGENCY LIGHT BATTERIES AND THE TAIL CONE REMOTE RECEIVER. (M)Dec 11, 2001 · N822US · Doug DC982 · Emergency LightingSDR USAAD01188Battery · dischargedIND - THE SEAT MOUNTED LOW LEVEL EMERGENCY LIGHTS WERE DIM AND THE TAIL CONE REMOTE RECEIVER WAS INOPERATIVE. MAINTENANCE REPLACED THE LOW LEVEL EMERGENCY LIGHT BATTERIES AND THE TAIL CONE REMOTE RECEIVER. (M)Dec 11, 2001 · N822US · Doug DC982 · Emergency LightingSDR 2001F00639Battery · dischargedIND - THE LOW LEVEL EMERGENCY LIGHTS AT SEAT ROWS 3 AND 25 AND THE CEILING EMERGENCY LIGHTS BETWEEN SEAT ROWS 5 AND 8 AND 27 AND 30 WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. REF USAAD01172. (M)Oct 18, 2001 · N822US · Doug DC982 · Emergency LightingSDR USAAD01172Battery · dischargedIND - THE LOW LEVEL EMERGENCY LIGHTS AT SEAT ROWS 3 AND 25 AND THE CEILING EMERGENCY LIGHTS BETWEEN SEAT ROWS 5 AND 8 AND 27 AND 30 WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)Oct 18, 2001 · N822US · Doug DC982 · Emergency LightingSDR USAAD01155Slide · failedPIT - THE AFT SERVICE DOOR EVACUATION SLIDE FAILED TO DEPLOY DURING A FUNCTIONAL TEST. MAINTENANCE REPLACED THE EVACUATION SLIDE. (M)Aug 31, 2001 · N822US · Doug DC982 · Escape SlideSDR USAAD01156Slide · failedPIT - THE TAIL CONE EVACUATION SLIDE FAILED TO DEPLOY DURING A FUNCTIONAL TEST. MAINTENANCE REPLACED THE EVACUATION SLIDE. (M)Aug 31, 2001 · N822US · Doug DC982 · Escape SlideSDR USAAD01059Power Supply · failedIND - THE CEILING EMERGENCY LIGHTS AT SEAT ROWS 15, 16 AND 17 WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT POWER SUPPLY. (M)Mar 21, 2001 · N822US · Doug DC982 · Emergency LightingSDR USAAD01004Coalescer Bag · dirtyEWR - PIT, FLT 1267 - DURING INITIAL CLIMB-OUT, THE AFT FLIGHT ATTENDANT REPORTED AN UNUSUAL ODOR IN THE REAR OF THE AIRCRAFT. THE FIRST OFFICER INVESTIGATED AND FOUND NO SMELL IN CRUISE. THE FLIGHT ATTENDANT REPORTED THE SAME SMELL AT TOUCHDOWN. BOTH FLIGHJan 8, 2001 · N822US · Doug DC982 · Humidity Control SystemSDR USAAD00173Battery · dischargedPIT - THE OVERHEAD EMERGENCY LIGHTS ABOVE SEAT ROW 18 WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERY. (M)Nov 12, 2000 · N822US · Doug DC982 · Emergency LightingSDR USAAD00158Apu · seizedORD-PIT - FLT 1674 - WHILE BOARDING THE FLIGHT, A LOUD BANG WAS HEARD AT THE REAR OF THE AIRCRAFT. AT THAT TIME, ALL APU POWER WAS LOST. PASSENGERS ON BOARD WERE DEPLANED AND THE FLIGHT WAS CANCELLED. MAINTENANCE FOUND THE APU, APU BOX, AND APU MOUNTING BRAOct 5, 2000 · N822US · Doug DC982 · APU Core EngineSDR USAA001330Clip · corrodedPIT - FOUND SKIN CLIP CORRODED 1 INCH BY 3 INCHES, STATION 1155 BETWEEN LONGERON 30 AND 29 RIGHT. REPLACED SKIN CLIP WITH MFG''S ONE. (M)Aug 13, 2000 · N822US · Doug DC982 · Fuselage Miscellaneous StructureSDR USAA001331Longeron · crackedPIT - FOUND LONGERON CRACKED .5 INCH IN TWO PLACES, STATION 160 LONGERON 4L AT FRAME TO LONG INTERSECTION. SPLICED IN NEW SECTION OF LONGERON PER SRM 53-04 FIG 18. (M)Aug 13, 2000 · N822US · Doug DC982 · Fuselage Main, Longeron/StringerSDR USAA001332Longeron · crackedPIT - FOUND LONGERON CRACKED .25 INCH TO .5 INCH IN FOUR PLACES, STATION 389 RIGHT AT LONGERON 17, STATION 237, 275, 408. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR. (M)Aug 13, 2000 · N822US · Doug DC982 · Fuselage Main, Longeron/StringerSDR USAA001333Clip · corrodedPIT - FOUND CLIP CORRODED 1 INCH BY .5 INCH AREA, ATTACH CLIP AT FORWARD END OF LT INBOARD OF SEAT TRACK. CLIP REPLACED WITH MFG CLIP PER DOUGLAS DWG NR 9936534. (M)Aug 13, 2000 · N822US · Doug DC982 · Fuselage Miscellaneous StructureSDR USAA001334Retainer · crackedPIT - FOUND INNER WINDOW RETAIN CRACKED .5 INCH, STATION 845 FORWARD UPPER CORNER AT FASTENER WIND RETAIN. FABRICATED AND INSTALLED REPAIR ANGLE PER TYPICAL REPAIR 53-30-06A. (M)Aug 13, 2000 · N822US · Doug DC982 · Passenger Compartment WindowsSDR USAA001335Spar · crackedPIT - FOUND REAR SPAR CRACKED .75 INCH, STATION 164 FLAP HINGE INBOARD LOWER STUD HOLE RIGHT REAR SPAR. INSTALLED TEMP REPAIR WITH REPEAT INSPECTIONS AT LOWER SPAR (REPUBLIC REPAIR) PER EA 2J06027-506, 55836. (M)Aug 13, 2000 · N822US · Doug DC982 · Wing SparSDR USAA001336Beltframe · crackedPIT - FOUND BELTFRAME CRACKED .25 INCH THREE PLACES, STATION 617, LONGERON 27R. STOP DRILLED 2 CRACKS AND ROUTED OUT 2. FABRICATED AND INSTALL REPAIR ANGLE PER EA 56203. (M)Aug 13, 2000 · N822US · Doug DC982 · Fuselage Main, StructureSDR USAA001428Beltframe · corrodedPIT - FOUND BELTFRAME CORRODED 1 INCH BY 7 INCH, STATION 1155 BETWEEN LONGERON 30 AND 29 RIGHT. BELTFRAME REPLACED WITH NEW. CORROSION LEVEL 1, TASK NR C57-53304. (M)Aug 6, 2000 · N822US · Doug DC982 · Fuselage Main, StructureSDR USAA001427Longeron · corrodedPIT - FOUND LONGERON CORRODED 1 INCH BY 2 INCH AREA, FRAME 218 AND LONGERON 17 LT. CORROSION LEVEL 1, TASK NR C46-5330. INSTALLED DOUBLER OF FABRICATED REPAIR ANGLE PER EA 55835. (M)Jul 29, 2000 · N822US · Doug DC982 · Fuselage Main, Longeron/StringerSDR USAA001431Pan · corrodedPIT - FOUND DOOR JAMB PAN CORRODED 38 INCHES, FORWARD CARGO DOOR JAMB, STATION 389-427. REPLACED PAN PER SRM 53-05 FIG 44. CORROSION LEVEL 1, TASK NR C51-53300. (M)Jul 27, 2000 · N822US · Doug DC982 · Fuselage Miscellaneous StructureSDR USAAD00102Battery · dischargedPHL - THREE LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)Jun 28, 2000 · N822US · Doug DC982 · Emergency LightingSDR USAAD000072Sensor · out of adjPIT/SDF - FLT 1805 - AFTER TAKEOFF AND GEAR RETRACTION,THE NOSE GEAR RED LIGHT REMAINED ILLUMINATED, NO ABNORMAL VIBRATION WAS NOTED. THE LANDING GEAR WAS CYCLED, BUT THE LIGHT REMAINED ON. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAIMay 13, 2000 · N822US · Doug DC982 · Landing Gear Position and WarningSDR USAAD99119Battery · dischargedBOS - THE EXIT IDENTIFIERS AND ONE SEAT MOUNTED EMERGENCY LIGHT WERE IOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)Aug 22, 1999 · N822US · Doug DC982 · Emergency LightingSDR USAAD99065Wire Harness · damagedLGA-MCO - FLT 259 - EN ROUTE THE AFT LEFT FUEL BOOST PUMP, 'A' PHASE AND THE FORWARD LEFT FUEL BOOST PUMP, 'A' PHASE CIRCUIT BREAKERS TRIPPED. SHORTLY AFTERWARDS BOTH BOOST PUMPS FAILED ON THE LEFT SIDE AS WELL AT THE RIGHT AFT BOOST PUMP. ALL THREE PHASES OMay 16, 1999 · N822US · Doug DC982 · Fuel System WiringSDR USAAD98014Engine · vibrationCLT-BUF - FLT 825 - DURING CRUISE THE FLIGHT CREW NOTICED VIBRATION FROM THE LEFT ENGINE. THE CREW REDUCED THE POWER TO IDLE, AND THE ENGINE STAYED WITHIN NORMAL PARAMETERS. THE AIRCRAFT THEN DIVERTED TO PIT AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED Jan 22, 1998 · N822US · Doug DC982 · Engine (Turbine/Turboprop)SDR USAAD97093Ballast · failedCLT/BOS - FLT 2391 - AFTER DEPARTURE, FLIGHT ATTENDANT REPORTED A STRONG SMOKE SMELL IN CABIN. RETURNED TO FIELD. REPLACED LIGHTING BALLAST OVER SEAT ROW 23AC. (X)Jun 1, 1997 · N822US · Doug DC982 · Passenger Compartment LightingSDR USAAD97029Battery · dischargedROC - FOUND SECTION OF FLOOR TRACK LIGHTING INOPERATIVE AT ROWS 12-18. REPLACED BATTERIES IN BATTERY PACK AT OVERHEAD BIN 14 DEF. (M)Jan 31, 1997 · N822US · Doug DC982 · Emergency LightingSDR USAAD96151Relief Valve · failedFLT 2285 - PBI-DCA - AT CRUISE THE CREW NOTICED HIGH OIL PRESSURE ON NR 1 ENGINE. FLIGHT DIVERTED TO MCO. NO EMEGENCY WAS DECLARED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LEFT OIL PRESSURE RELIEF VALVE. OPERATIONAL CHECK WAS GOOD. (Oct 20, 1996 · N822US · Doug DC982 · Engine Oil PressureSDR USAA960390Door Pan · corrodedPIT - DURING A SCHEDULED Q-1/C-1 CHECK INSPECTION, FOUND APPROXIMATELY 38 INCHES OF CORROSION IN FWD CARGO DOOR STATION 389 THROUGH STATION 427 DOOR PAN. INSTALLED NEW SECTION OF PAN PER SRM 53-05 FIG 44. (M)Apr 13, 1996 · N822US · Doug DC982 · Fuselage Miscellaneous StructureSDR USAA960389Longeron · corrodedPIT - DURING A SCHEDULED Q-1/C-1 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED SECTION OF LONGERON 28L STATION 1211-1250. CORROSION TASK NR C57-53300. SPLICED IN NEW SECTION OF LONGERON PER USAIR EA 32559. (M)Apr 13, 1996 · N822US · Doug DC982 · Fuselage Main, Longeron/StringerSDR USAA960388Longeron · corrodedPIT - DURING A SCHEDULED Q-1/C-1 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED ON LONGERON 29R STATION 1211-1250. CORROSION TASK NR C57-53300. INSTALLED NEW SECTION OF LONGERON PER USAIR EA 32559. (M)Apr 13, 1996 · N822US · Doug DC982 · Fuselage Main, Longeron/StringerSDR USAA960387Panel · crackedPIT - DURING A SCHEDULED Q-1/C-1 CHECK INSPECTION, FOUND A 1.75 INCH CRACK IN SKIN PANEL JUST OUTBOARD OF REAR SPAR STATION XH=7.234 RIGHT SIDE HORIZONTAL STAB. REMOVED DAMAGE AND INSTALLED FILLER REPAIR PER SR09550010-3 AND USAIR EO NR 5592X156. (M)Apr 13, 1996 · N822US · Doug DC982 · Horizontal Stabilizer, Plate/SkinSDR USAA960386Support · corrodedPIT - DURING A SCHEDULED Q-1/C-1 CHECK INSPECTION, FOUND LEVEL 1 CORROSION PREVIOUSLY REWORKED IN CARGO FLOOR SUPPORT STATION 541, BETWEEN LONGERON 28L AND 28R. MANU SUPPORT USING 7075-T6 PER DACO DRAWING NR 5936592. (M)Apr 13, 1996 · N822US · Doug DC982 · Fuselage Miscellaneous StructureSDR USAA960385Angle · crackedPIT - DURING A SCHEDULED Q-1/C-1 CHECK INSPECTION, FOUND 3.5 INCH CRACK LEFT SIDE AFT DRAG ANGLE AT LOWER VERT STAB. INSTALLED DOUBLER REPAIR PER USAIR EA 32425. (M)Apr 13, 1996 · N822US · Doug DC982 · Vertical StabilizerSDR USAA960384Angle · crackedPIT - DURING A SCHEDULED Q-1/C-1 CHECK INSPECTION, FOUND 3.5 INCH CRACK RIGHT SIDE DRAG ANGLE LOWER VERT STABILIZER. INSTALLED DOUBLER REPAIR PER USAIR EA 32426. (M)Apr 13, 1996 · N822US · Doug DC982 · Vertical StabilizerSDR USAA960383Frame · chafedPIT - DURING A SCHEDULED Q-1/C-1 CHECK INSPECTION, FOUND STATION 1380 FORWARD SIDE FRAME CHAFED BETWEEN LONGERON 4L AND 5L. ROUTED OUT CHAFED AREA AND INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 2 SHEET 3 AND SRM 53-14-1. (M)Apr 13, 1996 · N822US · Doug DC982 · Fuselage Main, FrameSDR USAAD96026ASlide · malfunctionedFLT NR 307 - LGA - LEFT AFT CABIN DOOR CHUTE DEPLOYED WHEN IT FELL FROM THE DOOR AFTER UTILITY ENTERED. GIRT BAR WAS STOWED AND CAUGHT ON DOOR WHEN SLIDE PACK FELL. MAINTENANCE REPLACED THE AFT DOOR EMERGENCY SLIDE. NO PROBLEM EXISTED WITH THE SLIDES AS IT Feb 29, 1996 · N822US · Doug DC982 · Escape SlideSDR USAAD96026Slide · fell outFLT NR 307 - LGA - LEFT AFT CABIN DOOR CHUTE DEPLOYED WHEN IT FELL FROM THE DOOR AFTER UTILITY ENTERED. GIRT BAR WAS STOWED AND CAUGHT ON DOOR WHEN SLIDE PACK FELL. (M)Feb 29, 1996 · N822US · Doug DC982 · Emergency EquipmentSDR USAA950020Eel Wire · brokenLGA - FLT 2236 - THE CABIN FLOOR EMERGENCY EXIT LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE. OPERATIONS CHECKED NORMAL. (Z)Jan 11, 1995 · N822US · Doug DC982 · Emergency Lighting
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