N823US, cancelled Mar 18, 2004

Service difficulty reports · 40

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 = 'N823US' AND deregistration_id = 'N823US-2004-03-18'
  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 USAAD02017Battery · dischargedIND - SEVERAL LOW LEVEL EMERGENCY LIGHTS FAILED TEST. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)Mar 29, 2002 · N823US · Doug DC982 · Emergency LightingSDR USAAD02008Battery · dischargedIND - THE FORWARD CEILING AND OVERWING EXIT SIGN EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)Feb 9, 2002 · N823US · Doug DC982 · Emergency LightingSDR USAAD01179Battery Pack · dischargedIND - 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)Nov 11, 2001 · N823US · Doug DC982 · Emergency LightingSDR USAA010644Beltframe · corrodedPPIT - 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)May 30, 2001 · N823US · Doug DC982 · Fuselage Main, FrameSDR 20010427AP001Battery · dischargedIND - 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 RELOCAApr 3, 2001 · N823US · Doug DC982 · Emergency LightingSDR USAAD01075Battery · dischargedIND - 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 RELOCAApr 3, 2001 · N823US · Doug DC982 · Emergency LightingSDR USAAD01053Door · not closedCLT-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 SERVIMar 17, 2001 · N823US · Doug DC982 · Service DoorsSDR USAA20010117O-Ring · damagedPIT-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 SWUNGDec 31, 2000 · N823US · Doug DC982 · Landing Gear Retraction/Extension SystemSDR USAAD00186Door · openPIT-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 WASDec 3, 2000 · N823US · Doug DC982 · Service DoorsSDR USAA001424Attach Angle · crackedPIT - FOUND ATTACH BRACKET CRACKED 2 INCHES, STATION 937 AFT SIDE, RIGHT WHEEL WELL. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR. (M)Sep 3, 2000 · N823US · Doug DC982 · Fuselage Miscellaneous StructureSDR USAA001425Beam · crackedPIT - 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)Sep 3, 2000 · N823US · Doug DC982 · Fuselage Miscellaneous StructureSDR USAA001419Skin · crackedPIT - FOUND SKIN CRACKED .25 INCH, FORWARD SERVICE DOOR, HOLD OPEN HOOK CUTOUT. INSTALLED EXTERNAL DOUBLER PER EA 56228. (M)Aug 30, 2000 · N823US · Doug DC982 · Fuselage Main, Plate/SkinSDR USAA001420Web · crackedPIT - FOUND RIGHT CUSP MEMBRANE CRACKED 1.5 INCHES, STATION 838. MANUFACTURED NEW AND INSTALLED PER SRM 53-05-97 AND DACO DWG 9910151. (M)Aug 26, 2000 · N823US · Doug DC982 · Fuselage Miscellaneous StructureSDR USAA001421Web · crackedPIT - FOUND RIGHT CUSP MEMBRANE CRACKED .75 INCH, STATION 905. MANUFACTURE NEW MEMBRANE AND INSTALLED PER SRM 53-05 FIG 97/DACO DWG 991051. (M)Aug 26, 2000 · N823US · Doug DC982 · Fuselage Miscellaneous StructureSDR USAA001422Web · crackedPIT - 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)Aug 26, 2000 · N823US · Doug DC982 · Fuselage Miscellaneous StructureSDR USAA001429Web · corrodedPIT - 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)Aug 25, 2000 · N823US · Doug DC982 · Fuselage Miscellaneous StructureSDR USAA001526Beam · corrodedPIT - 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)Aug 24, 2000 · N823US · Doug DC982 · Fuselage Miscellaneous StructureSDR USAA001423Intercostal · corrodedPIT - FOUND INTERCOSTAL CORRODED 1 INCH BY 6 INCHES, STATION 1309-1322 L28R. REPLACED INTERCOSTAL PER SRM 51-30. (M)Aug 24, 2000 · N823US · Doug DC982 · Fuselage Miscellaneous StructureSDR USAA001426Skin · crackedPIT - 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)Aug 22, 2000 · N823US · Doug DC982 · Fuselage Main, Plate/SkinSDR USAA001430Beam · corrodedPIT - 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)Aug 22, 2000 · N823US · Doug DC982 · Fuselage Miscellaneous StructureSDR USAAD00106Door · not closedBUF-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)Jul 1, 2000 · N823US · Doug DC982 · Service DoorsSDR USAAD00066Cylinder · failedCLT-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 May 4, 2000 · N823US · Doug DC982 · Landing Gear Retraction/Extension SystemSDR USAAD00023Battery · dischargedPHL - 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)Feb 2, 2000 · N823US · Doug DC982 · Emergency LightingSDR USAAD00020Connector · failedMSY/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 VALJan 31, 2000 · N823US · Doug DC982 · Pressure Regulator/Outflow ValveSDR USAAD99172Engine · failedPIT - 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. Dec 3, 1999 · N823US · Doug DC982 · Turbine SectionSDR USAAD99170Battery · dischargedCLT - THE CABIN OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES FROM OVERHEAD BINS FIVE RIGHT AND TEN RIGHT. OPS CHECKED OK. (M)Dec 2, 1999 · N823US · Doug DC982 · Emergency LightingSDR USAA991038Skin · crackedPIT - 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)Sep 20, 1999 · N823US · Doug DC982 · Fuselage Main, Plate/SkinSDR USAA990123Rivet · brokenPIT - 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)Feb 22, 1999 · N823US · Doug DC982 · Service DoorsSDR USAA990122Skin · crackedPIT - 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)Feb 22, 1999 · N823US · Doug DC982 · Fuselage Main, Plate/SkinSDR USAA990121Skin · crackedPIT - 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)Feb 22, 1999 · N823US · Doug DC982 · Fuselage Main, Plate/SkinSDR USAAD98079Panel · crackedCLT - 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 98ZZZX2May 3, 1998 · N823US · Doug DC982 · Flight Compartment WindowsSDR 98ZZZX2256Control · malfunctionedCLT - 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 USAAD98May 3, 1998 · N823US · Doug DC982 · Windshield/Door Rain/Ice RemovalSDR USAAD97178Engine · failedBDL - 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 REPLACOct 10, 1997 · N823US · Doug DC982 · Engine (Turbine/Turboprop)SDR USAAD96125Bushing · failedFLT 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)Sep 7, 1996 · N823US · Doug DC982 · Passenger/Crew DoorsSDR USAA960464Fitting · crackedPIT - 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)May 23, 1996 · N823US · Doug DC982 · Fuselage Miscellaneous StructureSDR USAA960440Longeron · crackedPIT - 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)May 23, 1996 · N823US · Doug DC982 · Fuselage Main, Longeron/StringerSDR USAAD96005Retract Mech · malfunctionedMCO - AFTER TAKEOFF FROM MCO, NOSE GEAR WOULD NOT RETRACT. FLIGHT RETURNED TO MCO AND LANDED WITH NO FURTHER INCIDENT. (M)Jan 20, 1996 · N823US · Doug DC982 · Landing Gear Retraction/Extension SystemSDR USAAD96005ABolts · missingMCO - 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)Jan 10, 1996 · N823US · Doug DC982 · Landing Gear Retraction/Extension SystemSDR USAA950550Cylinder · leakingPHL - 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 Jun 7, 1995 · N823US · Doug DC982 · Landing Gear ActuatorSDR USAA950155Harness · misalignedPIT - 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, THFeb 16, 1995 · N823US · Doug DC982 · Landing Gear Position and Warning
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