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 aircraft_model_key = '7378AS' 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 aircraft_model_key = '7378AS' 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 3CEY2026100200001Manifold · chafedDURING THE INCOMING INSPECTION THE FOLLOWING FINDINGS WERE OBSERVED FUEL MANIFOLD TUBE CHAFED WITH HOLE AT 11 O'CLOCK POSITION AFT LOOKING FORWARD, WEAR TO THE LPT COOLING BRACKET, ABRASIONS ON COMBUSTION CASE LOCATED ON THE TOP OF THE MID-FLANGE - DAMAGE DIMESDR SCNA20260818366Battery · no discrepancyEMERGENCY LIGHTS LOW BATTERY. VERIFIED ACFT BATTERY POWER IS WITHIN NORMAL OPERATING LIMITS AND WAITED 90 MINUTES FOR CHARGE IAW AMM 33-51-06, AND AMM 33-51-00. ACFT OK FOR SERVICE.SDR SCNA20260702275Detection Sys · no testMAIN DECK CARGO FIRE SYSTEM TEST WILL NOT PASS. PERFORMED MAIN SYS CHECK OF CARGO FIRE REF FIM 26-23 TASK 805. NO DEFECTS NOTED.SDR SCNA20260522210Attach Fitting · corrodedMAIN CABIN L1 DOOR FWD GIRT BAR ATTACHMENT FITTINGS HOLES HAVE CORROSION.SDR K11A2024113000293Switch · out of positionMAIN CARGO DOOR LIGHT ILLUMINATED PASSING FL 33 EXTINGUISHED PASSING 9500 FT AND REMAINED OFF FOR THE DURATION OF THE FLIGHT. ADJUSTED FWD DOOR CLOSED SWITCH IAW B737 IAI SUP MANUAL 52-70-00, OPS CHECK GOOD NO DEFECTS NOTED. AIRCRAFT OK FOR SERVICE.SDR K11A2024092400287Fuel Filter · faultedON CLIMB OUT THE #1 ENGINE FUEL FILTER BYPASS LIGHT ILLUMINATED THEN WENT OUT CONTINUED TO CLIMB AND LIGHT ILLUMINATED AGAIN. REMOVED AND REPLACED #1 ENGINE FUEL FILTER IAW B737-800 AMM 73-11-02 FROM STEP A-G, PERFORMED LEAK IAW B737-800 AMM 73-11-02 STEP H. SDR K11A2024071800270Indicator · faultedON TAKEOFF CAPT. AIRSPEED READ 45 WHEN FO CALLED 80 KTS. THEN CAPT. AIRSPEED JUMPED TO 85 KTS. THE AUTO THROTTLES DISCONNECTED AT 85 KTS FO TRIED TO RECONNECT THE AUTO THROTTLES BUT COULD NOT GET THEM TO ENGAGE. CAPT. ABORTED TAKEOFF AT 110 KTS, 5500 FT OF RUSDR I5EA2023051100001Unknown · unknownCABIN ALT LIGHT ILLUMINATED AT FL390, PRESS CONTROLLER IN ALT MODE PER MEL 21-14-03, CABIN CONTINUED TO CLIMB TO 10,000, CONTINUED TO 11,000 CABIN CONTROLLER IN MAN MODE. EMERGENCY DECENT WITH OUTFLOW VALVE INDICATING CLOSEDSDR TX9220201228001Skin · corrodedDURING THE CONVERSION OF 737-800 PASSENGER AIRPLANE TO THE FREIGHTER TO DATUM AIRPLANE N239GE(MSN33717), TERRIBLE CORROSION DAMAGE WERE FOUND AT FUSELAGE SKIN AND STRINGERS OF E/E BAY AREA. SECTION 41 INNER SURFACE AT STA 294-STA 360, S-24L S-28L (P/N: 141A3SDR CA150106002Shaft · sheared(CAN) CREW NOTICED ENGINE NUMBER TWO N1 WAS 87.7% AND ENGINE NUMBER ONE N1 WAS 95% DURING TAKEOFF ROLL. AIRCRAFT WAS UNABLE TO CREATE ENOUGH POWER ON NR 2 FOR CONTINUED SAFE FLIGHT. FUEL PUMP PACK REPLACED. IAW AMM 73-11-01-400-801-F00.SDR CA140924005Tie Bolt · broken(CAN) AFTER A REMOVAL WHERE THE TIRE WAS NOTED TO BE DEFLATED, A WHEEL AND TIRE ASSY WAS SENT TO SHOP FOR INSPECTION. THE WHEEL WAS FOUND TO HAVE 5 TIE BOLTS, PN 2613109, WITH THE HEADS BROKEN OFF.SDR CA140818003Wire · chafed(CAN) ON DEPARTURE, FORWARD PANEL INDICATION LIGHTS BEGAN TO FLICKER THEN ALL STAYED ON PERMANENTLY. LIGHTS INCLUDED ANTI SKID INOP, LE FLAP TRANSIT/EXT, AUTOBRAKE DISARM, GREAN LDG GEAR, STAB OUT OF TRIM, SPEED BRAKE ARM/DO NOT ARM, LE DEVICE ON OVERHEAD, PARSDR CA130204011Connector · burned(CAN) TROUBLESHOOTING WAS BEING CONDUCTED ON THE SUBJECT ACFT DUE TO A DEFECT ON AN IFE DISPLAY. DURING TROUBLESHOOTING, THE J1 CONNECTOR AT LRU50-110 OF THE SVDU WAS FOUND TO BE BURNED. THE SVDU WAS REPLACED AND AN MEL APPLIED DUE TO THE BURNED PLUG. ALTHOSDR CA121220003Arm · sheared(CAN) DURING THE CREW`S PREFLIGHT CHECKS, IT WAS DISCOVERED THAT THE L1 FORWARD CABIN DOOR GUIDE ARM ROD END WAS SHEARED OFF. THE ACFT WAS TAKEN OUT OF SERVICE UNTIL THE ROD END WAS REPLACED.SDR CA130114003Rib · worn(CAN) THE RT DEFLECTION CONTROL RIB AT T/E WING STA 278, WHERE THE TURNBUCKLE ATTACHES TO THE RIB WAS FOUND WORN AND TORN OPEN.SDR CA120502002Wire · broken(CAN) REF CADORS REPORT NR: 2012O1034. FROM CREW INCIDENT/SAFETY REPORT: - "ON SELECTION OF FLAP 1, FLAP INDICATORS STOPPED PRIOR TO REACHING FLAP 1 AMBER FLAP TRANSIT LIGHT STAYED ILLUMINATED. ADVISED CENTER, WE WERE VECTORED NORTH WEST TO RUN CHECKLIST. Q
Back to Boeing 737-8AS