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 = 'N752AX' 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 = 'N752AX' 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 ABXA20221026297Engine · hung startHUNG START AFTER STARTER CUTOUT. EGT CONTINUED TO RISE TWD THE LIMIT. N2 AND N1 NORMAL WITH NO INCREASE IN SPEED WITH THE INCREASING EGT. FOLLOWED QRH PROCEDURE FOR THE ABORTED START AND ELECTED TO RETURN TO BLOCK. AIRCRAFT GROUNDED BY MAINTENANCE. MAINTENANCESDR ABXA2020090283168Actuator · wornAFTER PUSHBACK AND ENGINES STARTED EICAS MESSAGE AILERON LOCKOUT DISPLAYED, AIRCRAFT RETURNED TO BLOCK. AIRCRAFT WAS GROUNDED. T/S IAW B767 FIM 27-11 FT 804 FAULT CONFIRMED BAD LT AILERON LOCKOUT ACTUATOR. REMOVED AND REPLACED LT AILERON LOCKOUT ACTUATOR, ISDR ABXA20200813163Aileron Sys · lack of lubeAILERON'S STIFF AND WILL NOT RETURN TO CENTER. AIRCRAFT WAS GROUNDED. CLEANED AND LUBE ROD BEARING. C/W INSPECTION FOR AILERON PULLEYS, ALL CHECKS NORMAL. LUBED AILERON PULLEYS AS PRECAUTIONARY. C/W OPS CHECK. AILERON ZERO OUT ON BOTH LH AND RH YOLK. REF AMM 2SDR ABXA202006296098Warning Light · illuminatedRUDDER RATIO LIGHT AND MESSAGE DISPLAYED ON PUSH BACK. THE AIRPLANE WAS GROUNDED.SDR ABXA20200720129Warning Message · illuminatedEICAS MESSAGE FOR THE LE SLAT ASSYM DURING APPROACH WHEN FLAPS 5 SELECTED. AIRCRAFT WAS GROUNDED.SDR ABXA201808043085Bulkhead Web · canningOIL CANNING ON APU BULKEAD WEB REPAIR AT BS 1832. THE WEB WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA201808043084Spar · corrodedCORROSION ON THE LEFT WING LOWER FRONT SPAR WEB AT OUTBOARD FRONT SPAR STATION 865. THE SPAR WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA201808043082Keelbeam · corrodedCORROSION ON THE KEEL BEAM AT BS 964. THE KEEL BEAM WAS REPAIRED. THE AIRPLANE WAS GROUNDED.SDR ABXA201808043081Support · corrodedCORROSION ON THE LEFT WING UPPER TRAILING EDGE PANEL SUPPORT AT WING STATION 318. THE PANEL SUPPORT RIB WAS REPLACED. THE AIRPLANE WAS GROUNDED.SDR ABXA201808043080Support · corrodedCORROSION FOUND ON THE LEFT WING FALSE SPAR, UPPER TRAILING EDGE PANEL SUPPORT, WING STATION 360. THE SUPPORT RIB WAS REPLACED. THE AIRPLANE WAS GROUNDED.SDR ABXA201808043079Intercostal · corrodedCORROSION FOUND ON THE LEFT WING TRAILING EDGE INTERCOSTAL ABOVE THE LEFT MAIN LANDING GEAR AFT TRUNNION. THE INTERCOSTAL WAS REPLACED. THE AIRPLANE WAS GROUNDED.SDR ABXA20150203010Skin · corrodedLEFT OTBD FLAP UPPER SURFACE AT APPROXIMATELY STATION 367 - 377, HAS CORROSION, BULGING SKIN & ALSO HAS CORRODED SHIMS AT ACCESS 566MT OPENING EDGE. FLAP REPLACED ON NON-ROUTINE 0037. SDR INFO, CORRODED, PN 113T3100-63, PART NAME LT OTBD FLAP, SN 000355, FS SDR ABXA20150203009Support · corrodedLEFT WING UPPER TE EDGE PANEL SUPPORT TEE CORRODED ALONG ENTIRE LENGTH. VIEWED THROUGH PANELS 561AB & 552HB. REMOVED LT WING UPPER TE PANELS FWD INBD AILERON. REMOVED TE PANEL SUPPORT. REINSTALLED SERVICEABLE SUPPORT TE PN 113T1510-33 & TE PANELS IAW SRM CH SDR ABXA20150130012Skin · crackedSKIN UNDER THE FWD ADF ANTENNA HAS A 0.50 IN CRACK AT FS 1125, STRINGER 1L. FABRICATED & INSTALLED REPAIR TRIPLER & DOUBLER FOR SKIN UNDER FWD ADF ANTENNA AT FS 1125, STRINGER IL IAW DWG 146T3110 & SRM 53-00-01. SDR INFO, CRACKED 0.5 INCHES, PN 146T3110, SN SDR ABXA20150116007Beam · corrodedRIGHT WING LE OSS 1007.5 NOSE BEAM EXFOLIATED AT NUTPLATE AREA. R & R NOSE BEAM SECTION ON RT WING LE OSS 1007.5 IAW SRM 51-40-02. ACCOMPLISHED SB-60 351084. SDR INFO, CORRODED, PN 114T2330, PART NAME NOSE BEAM, SN NSN, STRINGER & WS LOCATION FROM OSS 1007.SDR ABXA20150115011Rib · crackedNUMBER 2 INBD CORE COWL NR 3 RIB FROM AFT CRACKED. REMOVED NR 3 RIB & LOWER DOUBLER. WELDED RIB IAW PSM 900-7-2-1 NR 1 REV 50. REINSTALLED IAW SRM 51-40-02. SDR INFO, CRACKED LENGTH 2.5 INCHES, PN 314T1210-17, SN NSN, PART NAME RIB. ACFT WAS GNDED.SDR ABXA20150109008Beam · corrodedRIGHT WING LE OSS 695 NOSE BEAM EXFOLIATED AT LE PANEL ATTACH FLANGE. REPLACED RT WING LE 055 695 NOSE BEAM PART 114T2300-292 & NR 10 INBD SLAT CURTAIN. RE-FINISHED NOSE BEAM IAW SRM 51-40-02, SRM 51-20-01 & AMM 27-81-31. SDR INFO, CORRODED, PN 114T2300-292SDR ABXA20141201345Switch · failedINTERMITTENT BURNING RUBBER SMELL DURING FLIGHT. AFTER LANDING, THE RUNWAY TURNOFF LIGHT SWITCH WAS CYCLED & VISIBLE SMOKE & FIRE APPEARED AT OVERHEAD PANEL. RT RUNWAY TURNOFF LIGHT REMAINED ILLUMINATED WITH THE SWITCH IN THE OFF POSITION. PERFORMED VISUAL SDR IXXA2013110100039Lever · fodL1 DOOR EVACUATION SLIDE DIFFICULT TO MOVE TO DISARMED POSITION. REMOVED FOREIGN OBJECT FROM L1 DOOR MODE SELECTOR LEVER MECHANISM. OPS CHECKED OK IAW AMM 52-11-00. ACFT WAS GROUNDED.SDR ABXA20131008576Gpu · malfunctionedLEFT ENGINE VERY SLOW TO RESPOND WITH THROTTLE ADVANCEMENT. ON BLOCK IN, LT ENGINE ADVANCED UNCOMMANDED, THROTTLE IN IDLE POSITION, TO APPROXIMATELY 80 PERCENT, N2. PERFORMED ENGINE RUN IAW 74-00-00-2, NO DEFECTS NOTED. AS FAR AS ENGINE GOING TO FLIGHT IDLESDR ABXA20130423426Tee Fitting · corrodedCORROSION ON UPPER RIGHT WING TRAILING EDGE PANEL ATTACH TEE-CAP FROM WING REAR SPAR TO TRAILING EDGE AT WING STA 434. INSTALLED NEW WING CHORD IAW B767 SRM 51-40-02 PARA 4, 7 AND 9. AIRCRAFT WAS GROUNDED.SDR ABXA20121203309Battery · defectiveEMERGENCY LIGHT SPARE BATTERY M736 WILL NOT HOLD A CHARGE. REPLACED EMERGENCY LIGHT SPARE BATTERY (M736) IAW B767 AMM 33-51-07-2, ACFT WAS GROUNDED.SDR ABXA20121203308Battery · dischargedEMERGENCY LIGHT SPARE BATTERY M735 WILL NOT HOLD A CHARGE. REPLACED SPARE EMERGENCY LIGHT BATTERY. REPLACED EMERGENCY LIGHT SPARE BATTERY (M735) IAW B767 AMM 33-51-07-2, ACFT WAS GROUNDED.SDR ABXA20111019129Bracket · crackedT-BRACKET CRACKED AT LOWER SUPPORT BRACE FWD OF RT INBD AILERON UNDERNEATH PANEL 661BB. REMOVED AND REPLACED T-BRACKET IN LWR SUPPORT BRACE BELOW PANEL 661BB IAW B767 DWG 113T1944, AWG.SDR ABXA20111019128Plate · corrodedCORROSION ON BULK CARGO DOOR FLOOR PLATE BY AFT DOUBLER UNDER SCUFF PLATE. REMOVED & REPLACED CORRODED FLOOR PLATE IAW B767-200 SRM 51-40-02, AWG.SDR ABXA20111019127Fitting · corrodedCORROSION ON FITTING AT FORWARD LOWER END OF CARGO DOOR CUTOUT BEHIND SEAL DEPRESSOR. REPAIRED IAW REA B653-595330-MR, AWG.SDR ABXA2011031809Pbe · unserviceableCREW REPORTED VACUUM SEAL ON PBE BROKEN. DEFERRED 68232 IAW B767 SERVICE CHECK AND GMM 07.04 FOR TRACKING MUST BE CLEARED BY 36 HOURS. PLACARD INSTALLED. CODE 15. AIRCRAFT WAS NOT GROUNDED.SDR ABXA201011290166Warning System · false activationEICAS MESSAGE "L/E SLAT ASYMMETRY" AND L/E DISCRETE LIGHT ILLUMINATED ON APPROACH TO LANDING. EMERGENCY DECLARED. PERFORMED FIM PROCEDURE IAW 27-81-00-1 FIG 107 SYSTEM CHECK'S OK.SDR ABXA201003260020Skin · crackedLEFT OUTBOARD FLAP AFT SKIN IS CRACKED AT INBOARD END CAP. REPAIRED DAMAGED AREA IAW 767 SRM 51-70-03.SDR ABXA201003260019Support Beam · crackedNR 1 ENGINE PYLON SUPPORT BEAM IS CRACKED AND HAS LOOSE / MISSING NUT PLATES CON TO PANEL 437ERX. REPAIRED SUPPORT BEAM IAW REA B654-58641-MR.SDR ABXA200911170063Mec · malfunctionedLEFT ENGINE FLAMED OUT AT APPROXIMATELY 1,000 AGL AFTER VNAV SELECTED. RE-LIGHT OF LEFT ENGINE SUCCESSFUL. (WHEN VNAV IS SELECTED THIS CHANGES THE THRUST PROFILE. FLAME OUT OCCURRED AS THROTTLES CAME BACK.) INSPECTED SUMPS AND FOUND NO WATER. FUEL FILTERSSDR ABXA080131Strap · crackedSTRAP ON UPPER CAP OF FRONT SPAR WAS CRACKED LES 485. REMOVED AND REPLACED UPPER SPAR CAP STRAP SECTIONS IAW B767 SRM.SDR ABXA080130Keelbeam · corrodedLOWER RIGHT KEEL BEAM APPROXIMATELY STA 970 CORRODED. BLENDED CORROSION ON LOWER RIGHT KEEL BEAM STA 970 IAW B767 SRM.SDR ABXA080129Keelbeam · corrodedLOWER RIGHT KEEL BEAM CORD APPROXIMATELY STA 1030 - CORRODED. BLENDED CORROSION ON LOWER RIGHT KEEL BEAM STA 1030 IAW B767 SRM.SDR ABXA080137Skin · crackedL1 DOOR CUTOUT LOWER AFT CORNER INTERIOR DOUBLER HAD 2 EACH .25 INCH CRACKS AT THE FASTENER HOLE AND THE EXTERIOR SKIN HAD A .125 INCH CRACK AT SAME HOLE. REPAIRED L1 DOOR CUTOUT LOWER AFT CORNER IAW REA B653-57165-MR.SDR ABXA080128Skin · crackedCRACK IN SKIN APPROXIMATELY 1.375" LONG AT FASTENER FS 1654 AT STRINGER 6 LEFT. REPAIRED AREA IAW B767 SRM 53-80-01.SDR ABXA080127Skin · crackedL1 DOOR CUTOUT LOWER AFT CORNER INTERIOR DOUBLER HAD 2 EACH .25 INCH CRACKS AT THE FASTENER HOLE AND THE EXTERIOR SKIN HAD A .125 INCH CRACK AT THE SAME HOLE. REPAIRED L1 DOOR CUTOUT LOWER AFT CORNER IAW REA B653-57165-MR.SDR ABXA080126Door Frame · crackedR1 DOOR CUTOUT LOWER AFT CORNER INTERIOR DOUBLER HAD A .125 INCH CRACK AT THE FASTENER HOLE. REPLACED R1 DOOR CUTOUT LOWER AFT CORNER IAW REA 13653-57164-MA.SDR ABXA070266Actuator · failedDURING MAINTENANCE, REF JOB CARD 12-003-C1, STABILIZER TRIM BALL NUT UPPER SEAL APPEARED TO HAVE FAILED - STEP (23) (B) NOTE 2 (BEAVER UNIT). REMOVED AND REPLACED TRIM BALL SCREW ACTUATOR IAW B767 MM 27-41-10.SDR ABXA070048Control Unit · malfunctionedAS CREW WAS ON FINAL AT ILN, GOING THROUGH 27K, NR 2 ENGINE HAD AN UNCOMMANDED SHUTDOWN. CREW RESTARTED ENGINE WITHOUT ANY FURTHER ISSUES. NO EMERGENCY DECLARED. NO EN ROUTE DELAY. REMOVED AND REPLACED NR 2 ENGINE MAIN ENGINE CONTROL IAW B767 AMM 73-21-01-
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