N708PS
Service difficulty reports · 108
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 = 'N708PS' AND registry_match = 'registration' 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 = 'N708PS' AND registry_match = 'registration' 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 VNAA0602009Warning Light · illuminatedDURING CLIMBOUT THE CREW REPORTED A -SMOKE AFT LAV- WARNING MESSAGE THAT DISAPPEARED AFTER 30 SECONDS. THE FLIGHT RETURNED TO SRQ AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AFT LAVATORY AND FOUND NO EVIDENCE OF SMOKE, OVERHEAT, OR FIRE. THE GALLSDR VNAA0601015Structure · ground damageWHILE PARKED AT THE GATE THE RIGHT WING TIP LEADING EDGE TRANSITION FAIRING AND OUTBOARD SLAT WERE HIT BY A VEHICLE. THE FAIRING WAS DENTED AND THE SLAT WAS DENTED & CRACKED. MAINTENANCE REMOVED AND REPLACED THE RIGHT WING TRANSITION FAIRING AND OUTBOARD SLASDR VNAA0512009Connector · dentedDURING CLIMB THE LT AND RT WING ANTI-ICE SYSTEMS CYCLED ON AND OFF. THE CREW FOLLOWED THE QRH AND RETURNED TO CLT. MAINTENANCE TROUBLESHOT THE SYSTEM AND FOUND THE NR 2 - NR 3 SLAT TRACK CONNECTOR FLEX TUBE DENTED CAUSING REDUCED BLEED AIR FLOW TO THE LT OUTSDR VNAA0512007Actuator · failedDURING CLIMB THE PITCH FEEL CAUTION LIGHT ILLUMINATED. THE CREW FOLLOWED THE QRH AND RETURNED TO CLT. MAINTENANCE REMOVED AND REPLACED THE RT PITCH FEEL LINEAR ACTUATOR. THE SYSTEM OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.SDR VNAA0508030Control Unit · malfunctionedON FINAL APPROACH, APPLICATION OF THE FLIGHT SPOILER LEVER RESULTED IN I/B SPOILERONS & I/B FLT SPLRS CAUTION MESSAGES. THE CREW FOLLOWED THE QRH AND LANDED SAFELY. MAINTENANCE RESET THE SSCU IAW CRJ700 SL-27-028. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFTSDR VNAA0507010Pump · leakingDURING CRUISE THE CREW REPORTED TOTAL LOSS OF THE NR 1 HYDRAULIC SYSTEM PRESSURE AND FLUID QUANTITY. MAINTENANCE FOUND THE LEFT ENGINE DRIVEN HYDRAULIC PUMP LEAKING. THE LEFT EDP WAS REMOVED & REPLACED IAW CRJ700 AMM 29-11-01-400-801-A01. ALL OPERATIONAL CHSDR VNAA0410012Pump · failedDURING CRUISE THE CREW REPORTED A NR 1 HYDRAULIC SYSTEM HIGH TEMP CAUTION MESSAGE. TWO SECONDS LATER O/B SPLRON, O/B FLT SPLRS, O/B GND SPLRS, & HYD 1 LOW PRESS CAUTION MESSAGES WERE RECEIVED. THE CREW ELECTED TO DIVERT FLIGHT 2219 TO DAY WHERE MAINTENANCE WSDR VNAA0409001Warning Light · illuminatedTHE CREW REPORTED RECEIVING A FIRE SYSTEM FAULT STATUS MESSAGE. MAINTENANCE CONTROL HAD THE CREW RESET THE CIRCUIT BREAKERS CBP-1, N1, AND N2, IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUAL 26-10-00 AND THE MESSAGE CLEARED. THE AIRCRAFT WAS THEN RELEASED F
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