N807US, cancelled Jun 18, 2004
Service difficulty reports · 33
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 = 'N807US' AND deregistration_id = 'N807US-2004-06-18' 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.
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 = 'N807US' AND deregistration_id = 'N807US-2004-06-18' 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 LCQPad · crackedCRACK INDICATIONS AROUND JACK PAD ON BOTTOM OF LOWER SEGMENT OF RT MAIN LANDING GEAR.SDR USAAD01148Control Valve · out of rigPIT-BOS - FLT 564 - DURING APPROACH, RECEIVED LANDING GEAR UNSAFE INDICATIONS WHEN THE LANDING GEAR WAS SELECTED DOWN. RECYCLED THE LANDING GEAR AND RECEIVED NORMAL GEAR DOWN INDICATIONS. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE CHECKED AND ASDR USAAD01147Battery · inoperativeIND - THE SEAT MOUNTED EMERGENCY LIGHT AT ROW 30 WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY AT ROW 30. OPS CHECKED OK. (M)SDR USAAD01144Battery · inoperativeTPA - THE EMERGENCY PACK WILL NOT TEST ROW 11. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONALLY CHECKED OK. (M)SDR USAAD01125Battery · dischargedIND - THE LOW LEVEL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)SDR USAAD01112Battery · dischargedBOS - THE LOW LEVEL LIGHTS FAILED TO TEST AT SEAT ROWS 1, 11, 25 AND 30. MAINTENANCE REPLACED THE EMERGENCY LIGHT BATTERIES. (M)SDR USAAD01049Coalescer Bag · contaminatedCLT-EWR - FLT 554 - AFTER TAKEOFF, SMOKE APPEARED IN THE REAR CABIN. THE LEFT AIR CONDITIONING PACK WAS TURNED OFF AND THE SMOKE DISSIPATED. THE AIRCRAFT CONTINUED TO ITS DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE RELEASED THE AIRCRAFT WITH THE LESDR USAAD01032Light · out of positionMCO - THE EMERGENCY LIGHTS AT ROWS 30, 25, AND 20 WERE FOUND TO BE OUT OF POSITION. THE LIGHTS WERE PLACED INTO THEIR CORRECT POSITIONS. (M)SDR USAAD01021Light · shortedMHT-PIT - FLT 395 - DURING CRUISE, THE EMERGENCY LIGHTS ILLUMINATED WITH THE EMERGENCY LIGHT SWITCH IN THE ARM POSITION. WITH THE EMERGENCY LIGHT SWITCH IN THE OFF POSITION ALL LIGHTS EXTINGUISHED EXCEPT THE EMERGENCY LIGHTS AT THE EMERGENCY EXIT ROWS. THE ESDR USAA010163Fitting · crackedPIT - FOUND FITTING CRACKED .75 INCH, LEFT SPOILER ACTUATOR FITTING AT BOLT BOSS. REPLACED PART PER EO 5788M381. (M)SDR USAAD00171Battery · dischargedMCO - THE OVERHEAD EMERGENCY LIGHTS FOR ROWS 17-24 WERE FOUND TO BE INOPERTIVE. MAINTENANCE REPLACED THE BATTERIES IN TWO BATTERY PACKS. OPS CHECKED OK. (M)SDR USAAD00045Battery · dischargedTPA - THE FLOOR LEVEL EMERGENCY LIGHTS WERE INOPERATIVE AT ROWS 9 AND 11, AND THE REMAINING LIGHTS WERE DIM. MAINTENANCE REPLACED THE FLOOR LEVEL EMERGENCY LIGHT BATTERIES. (M)SDR USAAD00044Hydraulic System · overservicedBTV-PIT - FLT 1221 - NOTICED BURNING RUBBER SMELL IN COCKPIT AND CABIN BETWEEN 800 AND 3000 FEET DURING TAKEOFF. USED FULL POWER AND BOTH PACKS ON, SMELL WAS NOT OVERPOWERING, BUT NOTICEABLE. DISSIPATED ABOVE 3000 FEET. MAINTENANCE FOUND RIGHT HYDRAULIC SYSSDR USAAD99149Battery · dischargedCLT - THE EMERGENCY LIGHTS IN THE FIRST CLASS SECTION OF THE PASSENGER CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES FOR THE EMERGENCY LIGHTS. (M)SDR USAA991069Skin · crackedPIT - DURING RON VISIT, FOUND 1 INCH CRACK IN SKIN AT RIGHT STATION 69.5 LONGERON 20 RT. INSTALLED DOUBLER PER SRM 53-01 FIG 4. (M)SDR USAAD98209Drag Link · out of adjustPIT-EWR - FLT 1642 - ON TAKEOFF, THERE WAS SEVERE NOSE WHEEL VIBRATION. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE SHIMMED THE NOSE LANDING GEAR DRAG LINK ASSEMBLY TO REMOVE EXCESSIVE CLEARANCE AND REPLACED BOTH NOSE WHEEL ASSDR USAAD98164Pump · failedPIT-MDT - FLT 710 - AFTER TAKEOFF THE PRESSURE WENT TO ZERO FOR THE LEFT ENGINE HYDRAULIC PUMP. FOR MAINTENANCE CONVENIENCE THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE DRIVEN HYDRAULIC PUMP. (M)SDR USAAD98133Door · openBOS - FLT 1924 - AIRCRAFT EXPERIENCED HEAVY VIBRATION FROM NOSE WHEEL AREA AFTER GEAR RETRACTION. MAINTENANCE FOUND THE RIGHT NOSE GEAR DOOR OPEN. THE DOOR WAS SECURED CLOSED AND THE AIRCRAFT DISPATCHED. (M)SDR USAA980157Skin · crackedPIT - DURNIG C-2 CHECK, FOUND .5 INCH CRACK AT STATION 984 LONGERON 20 LEFT. INSTALLED DOUBLER PER TYPICAL REPAIR 53-10-28. (M)SDR USAA980156Skin · crackedPIT - DURING C-2 CHECK, FOUND .5 INCH CRACK IN SKIN AT STATION 984 LONGERON 20 RIGHT. INSTALLED DOUBLER PER TYPICAL REPAIR 53-10-28. (M)SDR USAAD97205Temp Bulb · failedPIT - FLT 1108 - AIRCRAFT DIVERTED FROM BDL DUE TO ICING CONDITIONS. CREW EXPERIENCED RIGHT ICE PROTECTION TEMP HIGH LIGHT ON AND OFF AT CRUISE ALTITUDE WITH THE AIRFOIL HEAT SWITCH POSITIONED OFF. MAINTENANCE REPLACED THE RIGHT ICE PROTECTION HIGH TEMP BULBSDR USAAD97191Line · failedPIT - FL 8001 - CREW REPORTED LOSS OF LEFT HYDRAULIC QUANTITY AND PRESSURE EN ROUTE. MAINTENANCE REPLACED A BROKEN HYDRAULIC LINE AT THE PRESSURE FILTER IN THE TAIL SECTION OF THE AIRCRAFT. ALSO, REPLACED THE LEFT ENGINE DRIVEN HYDRAULIC PUMP AND SERVICED THSDR USAAD97119Ducts · looseDFW/PIT - FLT 335 - 0N CLIMB-OUT, AIRCRAFT WOULD NOT PRESSURIZE. RETURNED TO FIELD. FOUND RT AND LT ACM EXHAUST DUCTS OFF. RECONNECTED, CHECKED GOOD. (X)SDR USAAD97035Switch · failedBOS/CLT - FLT 1071 - AT FL 350, RIGHT PACK TRIPPED OFF, DESCENDED TO FL 250. THE LEFT PACK THEN TRIPPED OFF. BEGAN EMERGENCY DESCENT. AT FL 180, THE CABIN ALTITUDE WAS 12,000 FEET. THE CAPTAIN MANUALLY DEPLOYED THE OXYGEN MASKS. JUST BELOW FL 180, BOTH PASDR USAAD96012AGenerator · failedCLT - CREW RECEIVED FAULT LIGHT ON LEFT ELECTRIC BUS. RESET WOULD NOT CURE PROBLEM. APU STARTED, BUT IT WOULD NOT POWER THE BUS. FLIGHT DIVERTED TO CLT AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT GENERATOR. (M)SDR USAAD96011AFire Loops · malfunctionedTYS - FL 285 - EN ROUTE BNA-BWI, CREW RECEIVED RIGHT ENGINE 'B' LOOP FIRE WARNING. CREW FOLLOWED PILOT HANDBOOK PROCEDURES. SHORTLY THEREAFTER, THE CREW RECEIVED THE RIGHT AND LEFT 'A' LOOP AND LEFT 'B' LOOP WARNINGS. FLIGHT DIVERTED TO TYS AND LANDED WITHOSDR USAA950071Clips · corrodedPIT - DURING Q-3 CHECK INSPECTION ACCOMPLISHED CORROSION CONTROL TASK ITEM NR C51-53300 AND FOUND LEVEL II CORROSION AT THE FORWARD CARGO DOOR HINGE ATTACH FLANGE CLIPS. MANU NEW CLIPS AND INSTALLED PER SRM 53-11-2. (Z)SDR USAA950070Cusp Membrane · crackedPIT - DURING Q-3 CHECK INSPECTION, FOUND 1.25 INCH CRACK AT STATION 906 RT CUSP MEMBRANE. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 2. (Z)SDR USAA950069Cusp Membrane · crackedPIT - DURING Q-3 CHECK INSPECTION, FOUND A 3 INCH CRACK AT STATION 885 RT CUSP MEMBRANE. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER SRM 53-01 FIG 1 AND 2. (Z)SDR USAA950067Angle · crackedPIT - DURING Q-3 CHECK INSPECTION, FOUND .25 INCH CRACK AT STRINGER 1388 AFT SIDE OF CANTED BELT FRAME RT SIDE ATTACH ANGLE. INSTALLED ATTACH ANGLE STRAP REPAIR PER SRM 55-02 FIG 26. (Z)SDR USAA950066Longerons · crackedPIT - DURING Q-3 CHECK INSPECTION, FOUND .5 INCH AND .75 INCH CRACK IN STATION 1452 LONGERONS 3R AND 3L. MANUAL NEW CLIP AND REPAIRED PER SRM 53-03. (Z)SDR USAA950065Longeron · crackedPIT - DURING Q-3 CHECK INSPECTION, FOUND SEVERAL CRACKS IN LONGERON 17L AT STATION 280. REPLACED LONGERON AND SPLICED PER SRM 53-02 FIG 2 AND USAIR EA NR 2893. (Z)SDR USAA950064Angle · crackedPIT - DURING Q-3 CHECK INSPECTION, FOUND .75 INCH CRACK AT STATION 1388 RT SIDE OF VERTICAL STAB ATTACH ANGLE. STOP DRILLED AND INSTALLED REPAIR ANGLES PER SRM 53-05 FIG 84 AND USAIR EA NR 29735. (Z)
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