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 = '737809' 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 = '737809' 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 SAJF2014072203024Actuator · malfunctionedAIRCRAFT RTO DUE TO SPEED BRAKE DO NOT ARM LIGHT ILLUMINATED AFTER TAKEOFF THRUST SET. CREW INFO RTO IAS 70 GROSS WEIGHT 148000 LBS WITHOUT USING REVERSE. LIGHT EXTINGUISHED DURING DECELERATION. PFM AACU BITE TEST NO FAULT FOUND. BITE TEST SMYD 2 FOUND FAUSDR SAJF2014050903015Spar · corrodedDURING AV16C CHECK INPUT, CORROSION WAS FOUND ON THE LT HORIZONTAL STABILIZER REAR SPAR PN 182A1502-1. EVALUATED THE ISSUE & HAS DETERMINED THAT IT WAS ACCEPTABLE TO FERRY THE ACFT. PERFORMED THE TEMPORARY REPAIR IAW SR 3-2819481525 & THIS REPAIR IS STRUCTURSDR SAJF2014042803014Connector · defectiveDURING FLAP SET 1, FLAP ASYMMETRY, LT FALL BELOW 0 DEG, RT AT 0 DEG, CREW PERFORMED ALL FLAP UP LANDING PROCEDURE. IAW AMM 27-51-00 CHECK FCU RIGGING PIN NML. IAW AMM 27-51-00 CHECK FLAP TRACKS DIM Y WITHIN LIMIT. IAW AMM 27-59-00 PFM FLAP SKEW DETECTION SYSDR SAJF2013061702021Pressure Switch · malfunctioned(B-18607)REJECTED TAKEOFF DUE TO FLIGHT CONTROL SYS B LOW PRESSURE LIGHT ILLUMINATED JUST BELOW 80 KNOTS IAW FIM 27-21, TASK 814, FLT CONTROL HYD MODULE SYS B LOW PRESSURE SWITCH CLEANED UP. CHECK LOW PRESSURE LIGHT EXTINGUISHED AND THE RESULT IS NORMAL IAW ASDR SAJF2013061702020Control Panel · failed(B-18617) FLIGHT CREW INFORMED BOTH AUTOPILOT TRIPPED OFF IN FLIGHT AT FL260. DURING GROUND OPS CHECK, CONFIRMED THE STABILIZER ELECTRICAL TRIM FUNCTION OUT OF ORDER ALSO. PERFORMED DFCS BITE TEST AND STABILIZER ELECTRICAL TRIM OPS TEST, BOTH RESULTS FAILED.SDR SAJF2013042302014Electrical Box · malfunctioned(B-18606) PERFORMED A HIGH SPEED RTO DUE TO TAKEOFF CONFIG, WARNING SOUND CAME ON AND RTO SPEED AT ABOUT 140KTS IAW AMM05-51-07 PFM HIGH ENERGY STOP. FOUND MAINT MESSAGE 31-53010 (L/E FLAP NOT EXT) IAW FIM27-51 TASK 801 PFM FSEU BITE FOUND MSG 27-81218 (PROXSDR SAJFCALS102012Control Cable · broken(B-18608) WALK AROUND CHECK FOUND LT SPOILER NOT IN THE CORRECT POSITION. PERFORMED THE HYDRAULIC PRESSURE TEST, AND FOUND SPOILER CONTROL CABLE WSB-L2 WAS BROKEN. REPLACED THE CABLE AND CONDITION CHECKED NORMAL IAW AMM 20-10-91.SDR SAJFCALS102005Warning Light · false activation(B-18607) ABORTED TAKEOFF AT 40 KTS DUE TO THE AMBER LIGHT OF AFT CARGO DOOR ILLUMINATED. VERIFIED AFT CARGO DOOR CLOSED AND LOCKED.SDR SAJF2013102003Warning Light · false activation(B-18605) REJECTED TAKEOFF AT 90 KTS DUE TO AFT CARGO DOOR LIGHT ILLUMINATED. AFT CARGO DOOR OPS NORMAL, ITEM C/F TO D/D IAW MEL 52-3-1 FOR PRECAUTION.SDR SAJF20120105002Blade · damaged( B-18608) CREW REPORTED NR 1 ENGINE FAILED DURING CLIMBING, AND THEN SHUTDOWN THE ENGINE. METAL PARTICLES WERE FOUND IN TAILPIPE. THE ENGINE WAS REMOVED. BORESCOPE INSPECTION FOUND HPT BLADES AND ITS DOWNSTREAM PARTS DAMAGED. ALL HPT BLADES WERE FRACTUREDSDR SAJF2012121201049Warning Light · false activation(B18607) THE CREW INFORMED: "SPEED BRAKE DO NOT ARM LIGHT" ILLUMINATED DURING THE FIRST TAKEOFF, BUT RTO PERFORMED AND SECOND TAKEOFF WAS NORMAL. MX PERFORMED THE TEST OF THE "SPEED BRAKE DO NOT ARM LIGHT", AND THE RESULT IS NORMAL.SDR SAJF201211271044Spar · corroded(B-18610) RT HORIZ STABILIZER REAR SPAR UPPER CHORD CORROSION FOUND DURING AV14 MX CHECK. CORRODED REAR SPAR UPPER CHORD WAS REMOVED OTBD OF SPLICE LOCATION APPROX STAB STA 288. INSPECTION AND DAMAGE REMOVAL WAS PERFORMED IAW SRM 51-10-02 AND CONFIRMED NO CRASDR SAJF2012101700040Strap · corroded(B-18608) CORROSION WAS FOUND ON RT WING L/E FRONT SPAR LOWER ATTACH STRAP APPROXIMATE AT OSS 210. MFG TEAM PROVIDE ON-SITE TECH ASSISTANCE; SIMILAR CORROSIONS WERE ALSO REPORTED ON B-18605 AND B-18608 LT WING L/E LOWER ATTACH STRAP. ANALYSIS AND INVESTIGATISDR SAJF2012091701035Structure · corroded(B-18607) DURING THE MX CHECK, CORROSION WAS FOUND BETWEEN STRINGER S-21R AND S-22R AT BS 881 IN AFT CARGO COMPARTMENT. THE CORRODED AREA WAS REMOVED AND REPORTED TO MFG FOR REVIEW AND REPAIR INSTRUCTION. REPAIR IS IN PROCESS IAW MFG SERVICE REQUEST (SR 1-23SDR SAJF201206261022Warning Light · illuminated(B18617)TAKEOFF WARNING APPEARED & PSEU LIGHT ON DURING INITIAL ROLL RTO AT IAS 30-40 KTS. PERFORMED SPEED BRAKE HANDLE RESET, WARNING LIGHT DISAPPEARED, RAN ENGINE TO N1:60 PERCENT TO CONFIRM NO RELATED FAULT, CONTINUE FLT. AMM 05-51-07 HIGH ENERGY STOP INSSDR SAJFCALS100040Gate · worn(B-18606) ENROUTE, DURING CLIMB, PURSER REPORTED NOISE FROM 1L ENTRY DOOR (NEAR THE FORWARD LOWER SIDE AREA). AS THE NOISE BECAME LOUDER, CREW DECIDED TO TURN BACK FOR SAFETY REASON. CABIN WAS PRESSURIZED, AND CONFIRMED AIR LEAKING EVIDENCE IN THE FORWARD ENSDR SAJF20110930038Warning Light · illuminated(B-18612) DURING T/O ROLL SPEED BREAK DO NOT ARM LIGHT ILLUMINATED. IAW MEL 27-20 OPEN & COLLAR F/C AUTO SPEED BRAKE & AUTO STOW C/B. CW NOT OVERLIMIT IAW AMM 05-51-07 INSP NOT REQUIRED.SDR SAJF201109170036Oil System · underserviced(B-18606) ACFT, DURING DESCENT, CREW REPORTED NR 1 ENGINE LOW OIL PRESSURE/LOW OIL QUANTITY. ENGINE WAS THEN SHUTDOWN. AFTER LANDING, VISUAL INSP WAS PERFORMED AND FOUND OIL TANK EMPTY (OIL CAP CONFIRMED IN PLACE AND SECURED). CHECKED NORMAL, MAIN OIL FILTERSDR SAJF2011042600011Wire Harness · damaged(B-18605) DURING T/O ROLL, NR 1 ENGINE EGT RAISED TO AROUND 950 DEGREE C, ACFT ABORTED TAKEOFF. BITE TEST AND RESISTANCE CHECK FOUND LT BOTTOM EGT PROBE INDICATION WAS ABNORMAL. EGT PROBE (PN:TC296-02) AND HARNESS (PN: 325-025-401-0) WAS REPLACED. ENGINE RUNSDR SAJFCALS099034Lever · out of position(B-18610) RTO DUE TO TAKEOFF WARNING SOUND. TAKEOFF WARNING HORN SOUNDED AFTER PUSHING TO/GA SWITCH, ACFT REJECTED TAKEOFF. SPEED BRAKE LEVER WAS FOUND NOT IN DOWN POSITION PROPERLY. THE GROUND SPEED WAS 10 KNOTS WHEN RTO. SPEED BRAKE WAS THEN FULLY PUSHED DOWSDR SAJFCALS099028Shaft · sheared(B-18617) ENG 2 EDP LOW PRESSURE LIGHT ON. CK FOUND ENG-2 EDP SHAFT SHEARED AND EDP CASE DRAIN FILTER HAS METAL CONTAMINATION. IAW AMM 29-11-11, REPLACED ENG-2 EDP. IAW AMM 29-11-51 REPLACED CASE DRAIN FILTER ELEMENT; IAW AMM 29-11-61 REPLACE RETURN FILTER SDR SAJFCALS099026Control Valve · malfunctioned(B-18612) IN CLIMB FL350, CREW FOUND THE CABIN ALTITUDE RAISED TO 8,000 FT, CREW REQ ALTITUDE HOLD AND CHANGE CPC FROM AUTO TO MANUAL BUT CABIN ALTITUDE STILL INCREASED, QRH EMERGENCY DESCENDING PERFORMED BUT CABIN ALTITUDE STILL INCREASED TO 14,000 FT. DURISDR SAJ2010F00000Access Panel · cracked(B-18608) DAILY CHECK FOUND LT FUEL TANK ACCESS PANEL 532LB FUEL SEEPING TRACE. THE ACCESS PANEL WAS REMOVED AND FOUND A CRACKED DOME. THE ACCESS PANEL WAS REPLACED WITH NEW ONE. LEAK TEST WAS NORMAL. HAVE FOUND THAT A BUILDUP OF MOISTURE IN THE DOME OF TSDR SAJFCAL2010001Access Panel · crackedDURING DAILY CHECK, FUEL SEEPING TRACE WAS FOUND ON LT FUEL TANK ACCESS PANEL 532LB. THE ACCESS PANEL WAS REMOVED AND A CRACKED DOME WAS FOUND. MFG HAS FOUND THAT A BUILD-UP OF MOISTURE IN THE PANEL DOME CAN CAUSE A CRACK AFTER GOING THROUGH MUTIPLE FREEZE ANSDR SAJFCALS098037Sensor · failedAFTER AIRCRAFT LANDING, CREW FOUND BOTH SIDE FLAPS FAILED TO RETRACT. T/E FLAP ASYMMETRY. L IS 15, R IS 10. NR 8 FLAP SKEW SENSOR FAIL. EO 738-24-00-0017 WAS ISSUED TO INSP/PROTECT FLAP SKEW SENSOR. EO 738-27-51-0006 WAS ISSUED TO RECORD FAULT HISTORY FROMSDR SAJFCALS098031Transmitter · failedCREW VHF INFORM DURING APPROACH T/E FLAPS STUCK APPROX 10.5, IND L-15 R-10. FLAP POSITION TRANSMITTER FAIL. EO 738-24-00-0017 WAS ISSUED TO INSP/PROTECT FLAP POS TX TER. EO 738-27-51-0006 WAS ISSUED TO RECORD FAULT HISTORY FROM FSEU AT EVERY RE-CHK. (B-1860SDR SAJFCALS098003Bulkhead · corrodedFOUND CORROSION (3.8" X 2.7" X 0.060") AT BS 727 MAIN WHEEL WELL AFT BULKHEAD. REPAIR CORRODED AREA BY EO NR 738-53-00-0099. DO NOT HAVE FURTHER LEVEL 2 REPORT AT THIS CASE. WILL CONTIUE TO MONITOR THIS CASE. (B-18610)
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