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 = '680A' 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 = '680A' 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 DXTA2020082003992Handle · bindingMAIN CABIN DOOR HANDLE IS JAMMED IN THE OPEN POSITION. UNABLE TO SECURE DOOR CLOSED. SIGN-OFF. FOUND SLIDING BOLTS HAD SLID INSIDE THE DOOR AND JAMMED THE ENTIRE DOOR MECHANISM. PERFORMED ALL RIGGING AND HEALTH CHECKS, AS PER CESSNA TEAM 680 REQUESTS. WORSDR 2020F00363Skin · corrodedAPU STINGER SKIN DAMAGE (CORROSION), REF ENGINEERING MEMO DQ26585M1 DATED AUGUST 13, 2020.SDR 2020F00362Cowling · overheatedRIGHT ENGINE UPPER COWL HEAT DAMAGE, REF ENGINEERING MEMO DQ26626 DATED AUGUST 16, 2020.SDR 2020F00361Strut · scratchedNOSE LANDING GEAR INNER BORE DAMAGE (SCRATCHES), REF ENGINEERING MEMO DQ26613M1 DATED AUGUST 14, 2020.SDR DXTA2020081703981Pin · bindingAFTER CLOSING THE MAIN CABIN DOOR THE DOOR LATCHING HANDLE WILL NOT MOVE TO THE CLOSED POSITION. RAN THE QRH WHILE PUSHING THE DOOL LIFT CANCEL BUTTON, WE NEVER GOT THE CHECK HANDLE/PUSH TO OVERRIDE LIGHT TO FLASH. PERFORMED ONE POWER UP ANOMALIES CHECK LISTSDR JGVR20200811002Frame · chafedREPLACE CHAFED FRAME JUST FWD OF E EXIT AT APPROXIMATELY F.S. 405.40 AND REPAIR SIX CHAFE MARKS ABOVE E-EXIT ON RH INTERNAL FUSELAGE STRUCTURE BETWEEN APPROX FS 404.26 AND 426.26 AND BETWEEN STRINGERS S-4R AND S-5R. REPLACED CHAFED FRAME JUST FORWARD OF E-EXITSDR JGVR20200811001Attach Bracket · corrodedCABIN DROP AISLE HAS 29 AREAS OF VERIFIED CORROSION ON SIDE ATTACHMENT BRACKETS BETWEEN FS 157.00 AND FS 199.95. MECHANICALLY BLENDED 29 AREAS OF CORROSION IN DROPPED AISLE BETWEEN BS 157 AND BS 199.95. REPAIRED THE CORROSION BLEND AREAS IN CABIN DROPPED AISSDR JGVR20200819001Spar · corrodedBLENDED AREA OF CORROSION ON RT SIDE OF VERTICAL STABILIZER AFT SPAR AT VFS 118.79. PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED AND TREATED BLENDED AREA THEN PRIMED, APPLIED TOP COAT, AND CORROSION INHIBITING COMPOUND PER TEXTRON FIELD REPAIR.SDR JGVR20200807001Spar · corrodedLH WING REAR SPAR HAS VERIFIED CORROSION AROUND LT SPOILER RETURN HYDRAULIC FITTING. MECHANICALLY BLENDED TWO SPOTS OF MILD/MODERATE CORROSION IN LT WHEEL WELL ON LT WING REAR SPAR AROUND LH SPOILER RETURN HYDRAULIC FITTING IAW SRM 51-10-01. FOUND BLENDED ARESDR DXTA2020080203932Door · malfunctionedMAIN CABIN DOOR IS "HANGING UP" OR BINDING INTERMITTENTLY WHEN THE HANDLE IS IN THE FULL UP POSITION WHEN ATTEMPTING TO PUSH DOWN TO CLOSE. THE DOOR FUNCTIONS NORMALLY FROM THE OUTSIDE. PERFORMED SERVERAL OPS CHECKS OF MAIN CABIN DOOR IAW CE-680A AMM 52-10-00SDR 2020F00351Doubler · crackedCRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW), FRAME, WEB, AND DOUBLERS, FS 75. ACCOMPLISHED TEXTRON AVIATION FIELD REPAIR SR-680A-ATA53-25890 REV- DATED JUNE 1, 2020 AND 8100-9 DATED 6/1/2020; STANDARD REPAIR - CRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NSDR DXTA2020072703908Light · inoperativeTHE EMERGENCY LIGHTS INOPERATIVE, WITH THE EMER LTS SWITCH IN THE ON POSITION, WHILE CONDUCTING THE POWER ON CHECKLIST.SDR DXTA2020072703895Connector · dirtyAPPROXIMATELY 90 MINUTES INTO THE FLIGHT WE STARTED OUR DECENT FOR LANDING. FIRST WE GOT A ENG CNTRL FAULT R MESSAGE THEN WE WOULD GET A GEA FAIL 3 MESSAGE (THAT WOULD CYCLE ON AND OFF FOR THE DURATION OF THE PROBLEM). WITH THE GEA FAIL 3 MESSAGE WE WOULD ALSDR 2020FA0000340Battery Pack · dischargedEMERGENCY EXIT LIGHTS WOULD NOT ILLUMINATE DUE TO EMERGENCY EXIT LIGHT BATTERY PACK NOT HOLDING A CHARGE. THE BATTERY PACK CONTAINS A BUILT IN CHARGER. THIS BATTERY PACK WAS INSTALLED NEW BY AIRCRAFT MANUFACTURE WITH A TOTAL OF 4 BATTERY PACKS INSTALLED FOR HESDR 2020FA0000337Support Web · crackedSTANDARD REPAIR - CRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW), FRAME, WEB, AND DOUBLERS, FS 75. FIELD REPAIR SR-680A-ATA53-25890 REV- DATED 6/1/2020 WITH FAA FORM 8100-9.SDR 2020F00336Frame · crackedCRACK DAMAGE REPAIR OF NOSE LANDING GEAR WHEEL WELL (NWW), FRAME WEB, AND DOUBLERS, FS 75. TEXTRON AVIATION STANDARD REPAIR SR-680A-ATA53-25890 DATED 06/01/2020 WITH FAA FORM 8100-9 DATED 06/01/2020.SDR DXTA2020072133861Line · shearedRECEIVED HYDR PRESS LOW L/R AND HYDRAULIC VOL LOW AMBER CAS MESSAGE IN ROUTE AT FL 350. DECLARED AN EMERGENCY AND DIVERTED TO CMH. RAN QRH CHECKLIST AND BLEW THE GEAR DOWN WITH 3 GREEN. LANDED UNEVENTFULLY IN CMH. RECEIVED FIRE DETECTION FAIL R CAS MESSAGE AT SDR DXTA2020071733861Line · failedRECEIVED HYD PRESSURE LOW, LT & RT AND HYDRAULIC VOLUME LOW, AMBER CAS MESSAGE AT FL 350. DECLARED AN EMERGENCY AND DIVERTED. RAN QRH CHECKLIST AND BLEW THE GEAR DOWN WITH 3 GREEN. LANDED UNEVENTFULLY. RECEIVED FIRE DETECTION FAIL RT CAS MESSAGE AT FL 3SDR DXTA2020071703861Pipe · shearedRECEIVED HYDR PRESS LOW L/R AND HYDRAULIC VOL LOW AMBER CAS MESSAGE IN ROUTE AT FL 350. DECLARED AN EMERGENCY AND DIVERTED TO CMH. RAN QRH CHECKLIST AND BLEW THE GEAR DOWN WITH 3 GREEN. LANDED UNEVENTFULLY IN CMH. RECEIVED FIRE DETECTION FAIL R CAS MESSAGESDR DXTA2020071433861Warning Message · activatedRECEIVED HYDR PRESS LOW L/R AND HYDRAULIC VOLUME LOW AMBER CAS MESSAGE IN ROUTE AT FL 350. DECLARED AN EMERGENCY AND DIVERTED TO CMH. RAN QRH CHECKLIST AND BLEW THE GEAR DOWN WITH 3 GREEN. LANDED UNEVENTFULLY IN CMH. RECEIVED FIRE DETECTION FAIL R CAS MESSAGE SDR DXTA2020071003849Wire Harness · defectiveNOSE GEAR SHOWED UP, LEFT MAIN GEAR SHOWED UP, RIGHT MAIN GEAR SHOWED YELLOW HASH. GEAR DISAGREEMENT LIGHT ILLUMINATED. FOLLOWED CHECKLIST AND RETURNED TO KSLC. REPLACED RIGHT MLG HARNESS AND RIGHT MLG UPLOCK SWITCH P/N 6948101-3.SDR 2020F00327Doubler · crackedCRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW), FRAME, WEB, AND DOUBLERS, FS 75. ACCOMPLISHED FIELD REPAIR SR-680A-ATA53-25890 REV- DATED JUNE 1, 2020 AND 8100-9 DATED 6/1/2020; STANDARD REPAIR - CRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW), FRAME, WEB,SDR DXTA2020070603833Squat Switch · faultyAFTER TAKEOFF WHEN GEAR UP WAS SELECTED THE GEAR RETRACTED NORMALLY FOLLOWED BY AN AMBER LEFT GEAR DN INDICATION, AN AMBER GEAR DISAGREE L, AND AMBER ADC SSEC MISCOMPARE. CLIMB WAS CONTINUED TO 10,000' WITH IAS REMAINING BELOW 200KTS. WHEREUPON THE QRH AMBER MSDR 2020F00310Doubler · crackedCRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW), FRAME, WEB, AND DOUBLERS, FS 75. ACCOMPLISHED TEXTRON AVIATION FIELD REPAIR SR-680A-ATA53-25890 REV- DATED JUNE 1, 2020 AND 8100-9 DATED 6/1/2020; STANDARD REPAIR - CRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NSDR 2020F00326Doubler · crackedCRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW), FRAME, WEB, AND DOUBLERS, FS 75. ACCOMPLISHED A FIELD REPAIR SR-680A-ATA53-25890 REV- DATED JUNE 1, 2020 AND 8100-9. STANDARD REPAIR - CRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW), FRAME, WEB, AND DOUBLERSSDR 2020F00323Frame · crackedNLG WHEEL WELL WEB AND UPPER MID FRAME CRACKED. STANDARD REPAIR SR-680A-ATA53-25890, CRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW), FRAME WEB AND DOUBLERS FS 75 WITH FAA FORM 8100-9 DATED: 6/1/2020.SDR DXTA2020062603814Control Handle · defectiveTHE AUTO THROTTLES WOULD NOT ENGAGE DURING TAKEOFF ROLL, AT POSITIVE RATE, CALLED GEAR UP. MLG WOULD NOT RETRACT. GEAR HANDLE CAME OUT OF DETENT AND RAISED HANDLE SOUNDED LIKE A JACKHAMMER AND THE GEAR WOULDNT RETRACT. GEAR HANDLE RETUNED TO DETENT AND POWER RSDR 2020F00309Skin · corrodedREPAIR OF HORIZONTAL STABILIZER SKIN DAMAGE (CORROSION). ENGINEERING REPAIR LETTER DQ26103M1 DATED: 06/24/2020.SDR 2020F00322Skin · gougedREPAIR GOUGES IN LT ELEVATOR. ERL DQ26099M1.SDR 2020F00321Skin · corrodedFIELD REPAIR FR-680A-0037-8080. CORROSION, HORIZONTAL STABILIZER, UPPER AND LOWER SKINS, LBL 16.5 TO RBL 16.5. WITH FAA FORM 8100-9SDR 2020F00320Frame · crackedCRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW), FRAME, WEB, AND DOUBLERS, BS 75. ACCOMPLISHED FIELD REPAIR SR-680A-ATA53-25890 REV-, AND 8100-9. STANDARD REPAIR CRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW), FRAME, WEB, AND DOUBLERS.SDR 2020F00317Frame · crackedNLG WHEEL WELL WEB AND UPPER MID FRAME CRACKED. STANDARD REPAIR SR-680A-ATA53-25890 , CRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW),SDR DXTA2020063013793Unknown · odorDURING TAXI AFTER FLIGHT, APU WAS STARTED, AND AND ONCE THE APU BLEED WAS SELECTED ON, NOTICED SMOKE FILLING THE COCKPIT AND CABIN. APU BLEED SELECTED OFF AND AIRCRAFT WAS SHUT DOWN. EVACUATION CHECKLIST FOLLOWED, SMOKE DISSIPATED. STARTED APU AND TURNED OSDR DXTA2020062203793Unknown · smokeDURING TAXI AFTER FLIGHT, APU WAS STARTED, AND AND ONCE THE APU BLEED WAS SELECTED ON WE NOTICED SMOKE FILLING THE COCKPIT AND CABIN. APU BLEED SELECTED OFF AND AIRCRAFT WAS SHUT DOWN. EVACUATION CHECKLIST FOLLOWED, SMOKE DISSIPATED.SDR 2020F00316Skin · corrodedREPAIR OF CORROSION ON TAILCONE STINGER INNER RIGHTHAND SKIN. TEXTRON AVIATION ENGINEERING REPAIR LETTER DQ26060M1 DATED 06/16/2020.SDR 2020F00315Doubler · crackedCRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW), FRAME, WEB, AND DOUBLERS, FS 75. ACCOMPLISHED FIELD REPAIR SR-680A-ATA53-25890 REV- DATED JUNE 1, 2020 AND 8100-9 DATED 6/1/2020; STANDARD REPAIR.SDR JGVR20200616002Stiffener · gougedFOUND UPPER RT BOLT HOLE ON THE VERTICAL STABILIZER AFT SPAR STIFFENER GOUGED, BLENDED DAMAGED. REPLACED THE STIFFENER.SDR 2020F00304Doubler · crackedCRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW), FRAME, WEB, AND DOUBLERS, FS 75. ACCOMPLISHED FIELD REPAIR SR-680A-ATA53-25890 REV- DATED JUNE 1, 2020 AND 8100-9 DATED 6/1/2020; STANDARD REPAIR - CRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW), FRAME, WEB, SDR 2020FA0000293Warning Message · illuminatedAT THE START OF TAKE OFF OUT OF BTR ON 6/10/20 THE CREW RECEIVED A "CONTROL LOCK ON" CASS MESSAGE AND DECIDED TO ABORT TAKE OFF. THEY WERE BELOW 40KNTS AND ESSENTIALLY JUST TAXIED OFF RUN WAY. THE CREW STATED THEY REPORTED TO ATC THAT EVERYTHING WAS OK AND THESDR DXTA2020060903743Guard · dentedAIRCRAFT LEFT AIRPORT AND RETURNED BACK, AFTER TAKEOFF LANDING GEAR HANDLE WAS RAISED ON SCHEDULED BUT AFTER THE MAIN MOUNTS INDICATED UP AND LOCKED THE NOSE GEAR INDICATED A AMBER HASH PATTERN INDICATING ACCORDING TO THE EMERGENCY/ABNORMAL CHECKLIST N-2 THAT SDR 3EJA20200625201Spar · corrodedDURING DOC 1,3,5,5,15 AND MC INSPECTIONS LEFT HORIZONTAL STAB HAS CORROSION ON AFT UPPER SPAR (3 PLACES) STA 5.75-7.75 AND STA 135.8. AIRCRAFT FERRIED TO HOME STATION ON FERRY PERMIT DATED 06/10/2020. AIRCRAFT IS AWAITING MAINTENANCE AT THIS TIME.SDR 3EJA2020062500001Spar · corrodedRIGHT WHEEL WELL AFT SPAR WEB AT CENTER WING ATTACHMENT TUBS HAS CORROSION. REMOVED 4EA HI LOK FASTENERS. REMOVED SURFACE CORROSION TO LIMIT OF SRM 57-10-03. NDT ACCOMPLISHED ON WO 20TR612281, FURTHER CORROSION DETECTED. INSTALLED NEW HI LOKS P/N HL30-6-10SDR JGVR20200605001Rib · corrodedCORROSION AROUND 2 HI-LOKS ON UPPER OUTBOARD RIB ABOVE LT MLG AT APPROXIMATELY MIDLINE. REMOVED 2 HI-LOK FASTENERS AND MECHANICALLY BLENDED CORROSION IN AREA AROUND HOLES ON UPPER OUTBOARD RIB ABOVE LT MLG AT APPROXIMATELY MIDLINE, IAW SRM 51-10-01. PERFORMED SDR 2020F00300Frame · crackedCRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW), FRAME, WEB, AND DOUBLERS, FS 75. ACCOMPLISHED STANDARD REPAIR SR-680A-ATA53-25890 REV DATED JUNE 01, 2020 AND FAA FORM 8100-9 DATED 6/1/2020. STANDARD REPAIR CRACK DAMAGE, NOSE LANDING GEAR WHEEL WELL (NWW), FSDR DXTA2020053103729Circuit Card · defectiveDURING CLIMBOUT THROUGH FL330 "RIGHT ENGINE FIRE" AURAL ALONG WITH RIGHT SIDE MASTER WARNING. ONLY ONE AURAL WARNING, LASTED ONLY ABOUT ONE SECOND. NO SECONDARY INDICATIONS. HIT EVENT MARKER AFTERWARDS. PERFORNNED ENGINE FIRE SELF-TEST. SELF-TEST PASSED. INSPSDR 2020FA0000274Rib · crackedLEFT HORIZONTAL STAB O/B RIB COMMON TO PANEL 351AC LOWER FLANGE IS CRACKED. REFERENCE ENGINEERING MEMO DQ25863M1. HORIZONTAL STABILIZER TRAILING EDGE REPAIR DATED MAY 27, 2020.SDR 2020F00294Frame · crackedCRACK DAMAGE NOSE LANDING GEAR WHEEL WELL, FRAME, WEB, AND DOUBLERS AT FS 75.SDR 2020F00288Rib · crackedHORIZONTAL TRAILING EDGE RIB REPAIR (LEFT SIDE). ENGINEERING REPAIR LETTER DQ25863M1 DATED 5/27/2020.SDR DXTA2020052803715Manifold · defectiveAT FL 430 HEAVY BANGING / VIBRATION COMING FROM NOSE WHEEL AREA WITH RAPID CONCESSION. NO CASS MESSAGES. NO GEAR ERROR INDICATION OTHER THAN UP. BELOW 16000 AND 210 KNOTS BANGING / VIBRATION WENT AWAY. NORMAL GEAR EXTENSION WITH DOWN LOCKED INDICATIONS. HAD AISDR 2020F00295Frame · crackedCRACKS, NWW, DOUBLER, FRAME AND WEB, FS 75. ACCOMPLISHED FIELD REPAIR FR-680A-0063-7977 REV - DATED MAY 21, 2020 AND FAA FORM 8100-9 DATED 5/21/2020; FIELD REPAIR - CRACKS, NWW, DOUBLER, FRAME AND WEB, FS 75.
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