N824US, cancelled Feb 6, 2002
Service difficulty reports · 42
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 = 'N824US' AND deregistration_id = 'N824US-2002-02-06' 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.
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 = 'N824US' AND deregistration_id = 'N824US-2002-02-06' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR USAAD01038Light · inoperativeTPA - THE FORWARD ENTRY ENTRY LIGHT WAS INOPERATIVE. REPLACED THE LIGHT ASSEMBLY. (M)SDR USAAD01052Handle · missingBWI - THE FORWARD GALLEY SERVICE DOOR EMERGENCY EVACUATION SLIDE MANUAL RELEASE WAS NOT ATTACHED TO THE LANYARD. MAINTENANCE SECURED THE MANUAL RELEASE. (M)SDR USAA002129Skin · crackedPIT - FOUND SKIN CRACKED .875 INCH AND HEAT DAMAGED 9.75 INCH BY 5 INCH, RIGHT SIDE AT STATION 27026-27526 STRINGER 46-49 RIGHT. CUT OUT DAMAGE AND INSTALLED FILLER AND DOUBLERS PER EA 547900 AND TYPICAL REPAIR 53-40-01. (M)SDR USAA002122Floorbeam · corrodedPIT - FOUND BEAM CORRODED 2 INCHES BY .75 INCHES, RIGHT LAVATORY FLOORBEAM STATION 1322. INSTALLED ANGLE PER SRM 53-05 FIG 20A. (M)SDR USAA002123Skin · crackedPIT - FOUND TWO SKIN CRACKS, .5 INCH LONG, EXIT SKIN AFT SERVICE DOOR, ABOVE/BELOW HOLD OPEN HOOK. INSTALLED DOUBLER PER EA 57045. (M)SDR USAA002125Longeron · crackedPIT - FOUND LONGERON CRACKED .5 INCH, STATION 927 LONGERON 5 RIGHT. REPLACED LONGERON SECTION PER SRM 53-02 FIG 18. (M)SDR USAA002124Longeron · crackedPIT - FOUND STRINGER CRACKED 2 INCHES, BETWEEN STATION 160 AND 180 LONGERON 4 LT. INSTALLED 10 INCH SPLICE IN LONGERON 4 LT PER MD80 SRM 53-02 FIG 18. (M)SDR USAA002128Skin · crackedPIT - FOUND SKIN CRACKED .75 INCH, STATION 1437 JUST BELOW LONGERON 3 RT. CUT OUT CRACK, INSTALLED FILLER AND EXTERNAL DOUBLER PER SRM 53-04 FIG 27. (M)SDR USAA002127Skin · crackedPIT - FOUND SKIN CRACKED .75 INCH, STATION 1437 JUST BELOW LONGERON 3 LEFT. CUT OUT CRACK 2.3 INCH. INSTALLED FILLER AND DOUBLER PER SRM 53-04 FIG 27. (M)SDR USAA002126Angle · crackedPIT - FOUND ANGLE CRACKED 4 INCHES, VERTICAL LEFT STAV ATTACH ANGLE AT STATINO 1437. INSTALLED EXTERNAL DOUBLER PER EA 57042. (M)SDR USAAD00162Battery · dischargedDFW - THE OVERWING EMERGENCY LIGHTS REMAINED ON AND SEAT MOUNTED LIGHT AT 11D WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK FOR THE OVERWING EXIT LIGHT AND LIGHT ASSEMBLY AT 11D. OPS CHECK OF THE EMERGENCY LIGHT SYSTEM WAS NORMAL. (M)SDR USAAD99188Slide · won't testPIT - THE TAILCONE EMERGENCY EVACUATION SLIDE FAILED TO AUTO DEPLOY, MANUAL DEPLOYMENT NORMAL. MAINTENANCE REPLACED THE TAILCONE EMERGENCY EVACUATION SLIDE. (M)SDR USAA991006Skin · crackedPIT - DURING RON, FOUND 2 CRACKS, ONE IS .625 INCH AT 5TH RIVET AND ONE IS .5 INCH AT 4TH RIVET ON SKIN AT STATION 58.750, 4TH AND 5TH RIVETS BELOW FLOOR LINE FORWARD SIDE LEFT SIDE. INSTALLED FILLER AND INTERNAL DOUBLER FLUSH REPAIR PER SRM 53-01 FIG 4. (M)SDR USAAD98137Engine · failedBUF - FLT 433 - AFTER TAKEOFF THE RIGHT ENGINE EXPERIENCED TWO COMPRESSOR STALLS, THE EGT INCREASED AND THE ENGINE WAS UNRESPONSIVE TO THROTTLE MOVEMENT. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. THERE WAS NO RESPONSE TO REVERSE THRUST SDR USAAD98093Fitting · looseCLT - FLT 306 - DURING CLIMB-OUT, AT 15,000 FT THE CABIN PRESSURE CONTINUED TO CLIMB. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TIGHTENED A LOOSE FITTING AT THE LEFT AIRCONDITIONING PACK FLOW CONTROL VALVE. (M)SDR USAAD98070Light · missingBWI - LOW LEVEL EMERGENCY LIGHT AT ROW 3 WAS MISSING. MAINTENANCE REPLACED THE MISSING LOW LEVEL EMERGENCY LIGHT. (X)SDR USAAD98045Cylinder · failedPBI - FLT 1753 - ON APPROACH INTO PBI, AS CREW ATTEMPTED TO EXTEND THE LANDING GEAR, DID NOT GET THREE GREENS. THE NOSE GEAR DID NOT APPEAR TO EXTEND NORMALLY. ON DOWNWIND THE TOWER ADVISED THE CAPTAIN THAT THE NOSE GEAR WAS NOT EXTENDED. CAPTAIN DID A MANUSDR USAAD98025Retract Mech · malfunctionedGSO - FLT 8001 - AFTER TAKEOFF AND GEAR RETRACTION THERE WAS A LOUD NOISE AND VIBRATION FROM THE FRONT OF THE AIRCRAFT. DURING RECYCLING OF THE GEAR, WHEN THE GEAR WAS DOWN THERE WAS NO VIBRATION, BUT WHEN THE WAS RETRACTED THE VIBRATION AND NOISE RETURNED. SDR USAAD98018Control Module · failedCLT - CABIN EMERGENCY LOW LEVEL LIGHTING FAILED TO EXTINGUISH AFTER TEST. MAINTENANCE REPLACED THE EMERGENCY LOW LEVEL LIGHTING CONTROL MODULE. (M)SDR USAAD98003Generator · failedCLT - FLT 1754 - CLIMBING THROUGH 12,000 FT, THE LEFT GENERATOR BECAME INOPERATIVE. THE APU WAS ON MEL. THE AIRCRAFT RETURNED TO THE FIELD WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT GENERATOR AND CSD. THE APU GENERATOR AND CONTROL UNIT WERE ALSO REPLASDR 98ZZZX378Gcu · failedCLT - FL 1754 - CLIMBING THROUGH 12,000 FEET, THE LEFT GENERATOR BECAME INOPERATIVE. THE APU WAS ON MEL. THE AIRCRAFT RETURNED TO THE FIELD WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT GENERATOR AND THE APU GENERATOR CONTROL UNIT. THE SYSTEMS THEN OPERASDR 98ZZZM202Control Unit · failedCLT - FLT 1754 - CLIMBING THROUGH 12,000 FT, THE LEFT GENERATOR BECAME INOPERATIVE. THE APU WAS ON MEL. THE AIRCRAFT RETURNED TO THE FIELD WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT GENERATOR AND CSD. THE APU GENERATOR AND CONTROL UNIT WERE ALSO REPLASDR 98ZZZM201Csd · failedCLT - FLT 1754 - CLIMBING THROUGH 12,000 FT, THE LEFT GENERATOR BECAME INOPERATIVE. THE APU WAS ON MEL. THE AIRCRAFT RETURNED TO THE FIELD WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT GENERATOR AND CSD. THE APU GENERATOR AND CONTROL UNIT WERE ALSO REPLASDR USAAD97219Battery · dischargedDCA - EMERGENCY FLOOR LIGHTING AND TAIL CONE LIGHT INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY FLOOR LIGHTING BATTERIES. (M)SDR USAAD97197Battery · dischargedPBI - FOUND FIRST CLASS EMERGENCY FLOOR LIGHTING INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. (M)SDR USAAD97195Battery · dischargedLGA - FL 528 - PRIOR TO DEPARTURE THE EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE SEAT MOUNTED LOW LEVEL LIGHTING BATTERIES. (M)SDR USAAD97175Batteries · dischargedPHL - EMERGENCY FLOOR PATH ESCAPE LIGHTING INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS. (M)SDR USAAD97158Battery Packs · dischargedPIT - EMERGENCY LIGHTS AT ROWS 1 AND 3 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS. (M)SDR 97ZZZX4182Relay · failedMCO - UNABLE TO SHUT OFF EMERGENCY LIGHTS ON THE GROUND. MAINTENANCE REPLACED THE DC EMERGENCY POWER TRANSFER RELAY (R2-326). (X)SDR USAAD97128Duct · disconnectedPHL - FL 445 - CREW COULD NOT GET CABIN TO PRESSURIZE. FLIGHT RETURNED TO PHL AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE FOUND THE FLEX DUCT DISCONNECTED FROM THE LEFT ACM. THE DUCT WAS RESECURED, AND THE AIRCRAFT GROUND PRESSURIZED USING LEFT, RIGHT SDR USAAD97101Duct · failedFLT 541 - PIT-RSW - CLIMBING THROUGH 9000 FEET, FLOW LIGHT CAME ON AND CABIN BEGAN CLIMBING. RETURNED TO FIELD. REPAIRED FLEXIBLE DUCT AT ACM. (M)SDR USAAD97069Check Valve · failedPBI/CLT - FLT 1722 - AFTER DEPARTURE FROM PBI UPON REACHING FL 330, RECEIVED STRONG OIL SMELL. SHUT DOWN LEFT PACK AND DESCENDED TO FL 250. CABIN CONTINUED TO CLIMB. FLIGHT DIVERTED TO CLT. FOUND RIGHT AIR CHECK VALVE JAMMED OPEN. REPLACED RIGHT AIR CHECKSDR USAAD97062Hyd System · leakingFLT 326 - PBI-PHL - WHILE HOLDING AT 12,000 FEET FOR PHL, RIGHT HYDRAULIC SYSTEM BEGAN TO LOSE QTY. DIVERTED TO BWI. SERVICED RIGHT HYDRAULIC RESERVOIR TO PROPER LEVEL. CHECKED RIGHT ENGINE DRIVEN AND AUX PUMPS AND LINES, POWER TRANSFER UNIT, SERVICE PANEL,SDR USAAD96160Power Supply · inoperativeFIRST CLASS OVERHEAD EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY. (M)SDR USAAD96142Regulator Vlv · failedFLT 693 - CLT-PHL - DURING CLIMB FLOW LIGHT ILLUMINATED. LEFT AIRCRAFT SUPPLY PRESSURE 0 PSI. RIGHT SUPPLY 30 PSI. OUTFLOW VALVE MANUALLY CLOSED DID NOT HELP. ON DESCENT LEFT PRESSURE INCREASED. CABIN WAS NEVER ABOVE 8000 FEET. MASKS DID NOT DEPLOY. FLISDR USAAD96141Line · looseFLT 1189 - LGA-PBI - AT FL 310 CABIN ALT BEGAN CLIMBING 300/400 FEET. CREW DESCENDED AND INCREASED POWER IN AN ATTEMPT TO MAINTAIN PRESS. NO HELP. FINALLY REGAINED PRESSURIZATION CONTROL AT 18,000 FEET AFTER TRYING STANDBY AND THEN MANUAL. CREW DECIDED TO SDR USAAD96134Battery Pack · dischargedAFT SERVICE DOOR CEILING EMERGENCY LIGHTS DID NOT TEST. REPLACED POWER SUPPLY B5-58. (M)SDR USAA960507Drag Angle · crackedPIT - DURING Q3/C5 CHECK, FOUND 1 INCH CRACK THROUGH RIVET AT LT VERTICAL STABILIZER DRAG ANGLE AFT SIDE CANTED STATION 1388. INSTALLED REPAIR STRAPS AND ANGLES PER SRM 55-02 FIG 26 CONFIG 7001. (M)SDR USAA960500Skin · corrodedPIT - DURING Q3/C5 CHECK, FOUND 3 INCH BY 4 INCH CORROSION IN SKIN AT NR 3 VHF ANTENNA FS 1174 AREA, LONGERON 30. TREATED AND INSTALLED DOUBLERS PER EO 32910 (10 INCH BY 20 INCH). CORROSION LEVEL 2, CORROSION TASK NR C50-53300. (M)SDR USAAD96043Engine · bird strikeFLT 730 - MSY-PHL - CLIMBING THROUGH APPROXIMATELY 12,000 FEET, CABIN AND COCKPIT STARTED TO FILL WITH NOXIOUS FUMES. PACKS WERE TURNED OFF, AND FUMES BEGAN TO CLEAR. RETURNED TO MSY. FOUND BIRD STRIKE AT INTAKE RIGHT ENGINE. INSPECTED INTAKE AND EXHAUST ASDR USAA950732Slide · malfunctionedBDL - THE TAIL CONE WAS INADVERTENTLY RELEASED. THE EVACUATION SLIDE FAILED TO DEPLOY. MAINTENANCE REINSTALLED THE TAIL CONE AND PERFORMED AN ADJUSTMENT TEST, NO DEFECTS NOTED. OPERATIONS CHECKED GOOD. (W)SDR USAA950106Retract Mech · malfunctionedMKE - FLT 293 - AFTER TAKEOFF, THE NOSE GEAR WOULD NOT RETRACT. FLIGHT RETURNED TO MKE WITHOUT INCIDENT. INSPECTED NOSE GEAR RETRACT AND EXTEND MECH. NO DEFECTS NOTED. SERVICED NOSE GEAR STRUT, IAW DOUGLAS MM 32-21-02. GEAR SWING CHECKS GOOD. (W)
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