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 = '1900D' 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 = '1900D' 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 GUUA95453080607ASkin · corrodedDURING SCHEDULED ROUTINE MX DISCOVERED EXFOLIATION AT LOWER FUSELAGE SKIN AT FS 273.25 AND FS 285.25. REMOVED DAMAGE SKIN FABRICATED AND INSTALLED AN EXTERNAL DOUBLER REPAIR.SDR GUUA08040701Actuator · leakingFLIGHT: 9179, DURING FLIGHT RT MAIN LANDING GEAR EXTENDED ON ITS OWN WITH NOSE AND LT STILL RETRACTED. ATTEMPTED TO EXTEND LANDING GEAR, AND WAS UNABLE. PERFORMED MANUAL GEAR EXTENSION,GEAR EXTENDED AND LOCKED WITH (3) GREEN LIGHTS. RETURNED TO FLL LANDED WSDR CA071016006Turbine Blades · damaged(CAN) ON TAKEOFF ROLL THE ENGINE EMITTED A LOUD NOISE AND THE TAKEOFF WAS ABORTED. SUBSEQUENT INSPECTION REVEALED DAMAGED POWER TURBINE BLADES. (TC NR 20071016006)SDR N843E12007Hed · faultedCREW LEFT STATION. TWENTY MINUTES IN FLIGHT "BATT TIE OPEN" ANNUNCIATOR ILLUMINATED. CREW RETURNED TO STATION WITHOUT ISSUE. REMOVED AND REPLACED BATTERY HED. OPS CHECK GOOD.SDR BSAASRD0723Terminal · shortedPUFF OF WHITE SMOKE FROM THE BOTTOM OF THE FIRST OFFICER'S FRONT WINDSHIELD. FOUND -S- TERMINAL THAT WAS CURRENTLY BEING USED BURNED (SHORTED). SWAPPED THE WIRE TO OTHER -S- TERMINAL, WINDSHIELD OP CHECK GOOD.SDR GUUA08010701Uplock Switch · out of adjustFLIGHT: 5404, DURING FLIGHT LANDING GEAR HANDLE LIGHT ILLUMINATED. INSPECTED LANDING GEAR SYSTEM RIGGED LT LANDING GEAR UPLOCK SWITCH. LANDING GEAR OPERATIONAL CHECK GOOD.SDR NSVA20070198Gas Generator · leakingSMALL AMOUNT OF SMOKE IN THE COCKPIT, ODOR. LANDED SAFELY. FOUND GAS GENERATOR LEAKING OIL INTO COMPRESSOR SECTION (UNDETERMINED INTERNAL LEAK) LT ENGINE, REQUIRES ENGINE CHANGE.SDR GLBA20060968Skin · crackedBELLY SKIN CRACKED ON RT SIDE 8 INCHES AFT OF FWD WING SPAR AT APPROXIMATELY FS 298.00 TO 300.25. CRACK APPROXIMATELY 2.375 INCHES IN LENGTH. MAINTENANCE INSTALLED A PRESSURIZED COVER PATCH IAW SRM 51-70. RII PROCEDURES COMPLIED IAW TASKCARD 8.2.1. AIRCRAFT WSDR NSVA20070197Autofeather Sys · malfunctionedRT ENGINE WILL NOT AUTOFEATHER. RESET CB9 AND OPS CHECK NORMAL IAW BMM 61-21-00.SDR GUUA07260704Spar Cap · crackedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LT WING REAR SPAR LOWER CAP CRACKED FROM RIVET HOLE TO REAR EDGE AT LWS 117.50. REMOVED DAMAGED SECTION OF LT LOWER AFT SPAR FROM LWS 73 TO LWS 129.86 SPLICED IN NEW SECTION OF SPAR IAW FIELD REPAIR FR-CO-01583 SDR GUUA07260703Switch · out of adjustFLIGHT: 9234, AFTER TAKEOFF, LANDING GEAR HANDLE LIGHT REMAINS ILLUMINATED IN THE UP POSITION. ADJUSTED RT MAIN LANDING GEAR UP POSITION SWITCH OPERATIONAL CHECK NORMAL.SDR GUUA07260701Pcb · shortedFLIGHT: 9162 FLL/FPO DURING APPROACH NO GREEN LANDING GEAR INDICATION WHEN GEAR HANDLE DOWN. RETURNED, LANDED WITHOUT INCIDENT. REPLACED ANNUNCIATOR PCB A125 LANDING GEAR OPERATIONAL CHECK NORMAL.SDR AMWA06032EFrame · chafedFUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.SDR AMWA06032DFrame · chafedFUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.SDR AMWA06032CFrame · chafedFUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.SDR AMWA06032UFrame · chafedFUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.SDR AMWA06032HFrame · chafedFUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.SDR AMWA06032GFrame · chafedFUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING INC. REPORT 6799-1 REV 1R.SDR AMWA06032BStructure · chafedFRICTION CHAFING DURING OPERATION HAS CREATED WORN SEGMENTS ON THE RT ENGINE NACELLE. DAMAGE WAS ALONG THE ENTIRE LENGTH OF THE NACELLE SHAPE: DEPTH VARIED AS INDICATED ON THE REPAIR AUTHENTICATION. REPAIRED IAW ACFT ENGINEERING REPORT 6799-2 REV 1R.SDR AMWA06032AStructure · chafedFRICTION CHAFING DURING OPERATION HAS CREATED WORN SEGMENTS ON THE LT ENGINE NACELLE. DAMAGE WAS ALONG THE ENTIRE LENGTH OF THE NACELLE SHAPE: DEPTH VARIED AS INDICATED ON THE REPAIR AUTHENTICATION. REPAIRED IAW ACFT ENGINEERING REPORT 6799-2 REV 1R.SDR AMWA06032VFrame · chafedFUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.SDR AMWA06032TFrame · chafedFUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.SDR AMWA06032SFrame · chafedFUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.SDR AMWA06032RFrame · chafedFUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.SDR AMWA06032MFrame · chafedFUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.SDR AMWA06032QFrame · chafedFUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.SDR AMWA06032PFrame · chafedFUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.SDR AMWA06032OFrame · chafedFUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.SDR AMWA06032NFrame · chafedFUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.SDR AMWA06032LFrame · chafedFUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.SDR AMWA06032KFrame · chafedFUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.SDR AMWA06032JFrame · chafedFUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.SDR AMWA06032FFrame · chafedFUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.SDR AMWA06032IFrame · chafedFUSELAGE FRAME DAMAGED BY FRICTION CHAFING. REPAIRED IAW AIRCRAFT ENGINEERING REPORT 6799-1 REV 1R.SDR AMWA06002Spar Cap · corrodedBIO CORROSION LT SPAR, ALT SPAR FLANGE ATTACHMENT OF THE RIB TO THE MAIN SPAR. REPAIRED IAW ENGINEERING REPORT 6799-3 REV 1R.SDR NSVA20070195Limit Switch · malfunctionedOUT OF AUG AS GEAR WAS BEING RETRACTED INTRANSIT LIGHT STAYED ILLUMINATED. RECYCLED GEAR INTRANSIT LIGHT, STAYED ILLUMINATED, CONTINUED FLIGHT WITH GEAR DOWN. AS HANDLE WAS IN UP POSITION INTRANSIT LIGHT STAYED ILLUMINATED. REPLACED LT MLG UPLIMIT SWITCH ANSDR BSAASDR0722Engine · surgesDURING CLIMB AND CRUISE THE RT ENGINE SURGED SEVERAL TIMES. ENGINE SHUT DOWN ON FINAL. INSPECTED PROP GOV, AND OVERSPEED GOV DUMP VALVE WIRING AND CONNECTOR. REINSTALLED CONNECTORS IN RESPECTIVE POSITIONS. GROUND CHECK NORMAL, WITH NO FURTHER DISCREPANCIESSDR GLBA230060965Unknown · odorAIR RETURN, FLIGHT 5069, PILOTS REPORTED A STRONG BURNING ODOR DURING FLIGHT. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF BOTH ENGINES ON THE GROUND WITH NO FAULTS FOUND. SUBSEQUENT OPERATIONAL CHECK FLIGHT WAS CONDUCTED WITH NO FURTHER REPORTS.SDR NSVA20070192Flap System · malfunctionedFLAP INOP, WHEN FLAPS WERE SELECTED 35* THEY DID NOT RESPOND. FLAP DID COME UP, HOWEVER THEY DID NOT RESPOND THEREAFTER. RESET C/B PERFORMED OPERATIONAL TEST OF FLAP SYSTEM, IAW BEECH MANUAL 27-00-00, NO FAULTS FOUND.SDR GLBA20060966Rib · crackedLT WING RIB OB OF POWER PACK CRACKED AT (L) BRACKET APPROX. 1 INCH BY 1 INCH IN LENGTH ORIGINATING FROM RIVET HEAD. MAINTENANCE REPAIRED THE LT WING RIB OB OF HYDRAULIC POWER PACK ONE INCH CRACK AT W.S. 79.65 IAW SRM 51-70. REPAIR DIMENSION 4 INCH BY 2.7500 ISDR GLBA20060963Acm · contaminatedPILOTS REPORTED A STRONG EXHAUST ODOR IN CABIN WITH HEAT TURNED ON. MAINTENANCE REMOVED EXCESS WATER IN ACM AND CLEANED OBSTRUCTION IN WATER NOZZLE ASSEMBLY. OPERATIONAL CHECK OF THE SYSTEM IAW 21-40-00 AND 21-50-00 WAS GOOD.SDR GUUA07140702Unknown · odorFLIGHT: 9131- DURING FLIGHT, STRONG ODOR COMING FROM THE OVERHEAD BLOWERS. PERFORMED OPERATIONAL CHECK OF VCM COULD NOT DUPLICATE ODOR. OPERATIONAL CHECK GOOD.SDR GUUA07140701Unknown · unknownDURING APPROACH LANDING GEAR WOULD NOT EXTEND WITH THE GEAR HANDLE DOWN, CYCLED LANDING GEAR AND THE RT GEAR EXTENDED PARTIALLY THEN 10 SECONDS LATER ALL GEARS EXTENDED. INSPECTED LANDING GEAR SYSTEM NO DEFECTS NOTED. LANDING GEAR OPERATIONAL TEST NORMAL. TESSDR NSVA20070183Ovrspeed Limiter · malfunctionedON TAKEOFF, LT PROP FEATHERED. REMOVED AND REPLACED OVERSPEED GOVERNOR, AND REMOVED AND REPLACED PROP GOVERNOR ON LT SIDE REF 61-20-02, PN:8210-410 SN: 11536603.SDR AMWA86034Switch · malfunctionedDURING FLT LT PROPS WENT INTO AUTOFEATHER. LANDED WITH NO FURTHER INCIDENT. PERFORMED CHECK FLT AND WAS UNSATISFACTORY. REMOVED AND REPLACED LOW AND HIGH TQ SWITCH, A123PCB. TEST FLT SATISFACTORYSDR NSVA20070180Uplock Switch · malfunctionedGEAR IN TRANSIT LIGHT ANNUNCIATOR ILLUMINATED NORMALLY DURING POWER REDUCTION, HOWEVER IT WOULD NOT EXTINGUISH AFTER ADVANCING POWER AND REMAINED ILLUMINATED UNTIL GEAR WAS EXTENDED FOR LANDING. REMOVED AND REPLACED NOSE GEAR UP LOCK SWITCH, PERFORMED GEAR EXSDR AMWA15036AFrame · chafedFUSELAGE FRAME AT FS 438.25 LT HAD CHAFFING. REPAIRED IAW ACFT ENGINEERING REPORT NR 6772-2 REV 1R.SDR AMWA15036CSkin · chafedFRICTION CHAFFING CREATED WORN SEGMENTS ON THE RT ENGINE NACELLES. DAMAGE WAS ALONG THE ENTIRE LENGTH OF THE NACELLE SHAPE. DEPTH VARIED AS INDICATED ON THE REPAIR AUTHORIZATION. REPAIRED IAW ENGINEERING REPORT NR 6772-1 REV 1R.SDR AMWA15036BSkin · chafedFRICTION CHAFFING CREATED WORN SEGMENTS ON THE LT AND RT ENGINE NACELLES. DAMAGE WAS ALONG THE ENTIRE LENGTH OF THE NACELLE SHAPE. DEPTH VARIED AS INDICATED ON THE REPAIR AUTHORIZATION. REPAIRED IAW ENGINEERING REPORT NR 677201 REV 1R.SDR NSVA20070181Handle · lack of lubeJUST AFTER BRAKE RELEASE, CARGO DOOR LIGHT ILLUMINATED. LUBED DOOR HANDLE, OP CHECKS GOOD.
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