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 29GA94232070611AUplock Switch · faultyAFTER RETRACTING THE LANDING GEAR THE RED GEAR HANDLE LIGHT REMAINED ILLUMINATED. RAN QRH AND THE LIGHT STILL REMAINED ILLUMINATED. EXTENDED THE LANDING GEAR AND RETURNED TO OUR DEPARTING STATION. A NORMAL LANDING WAS EXECUTED WITH NAY FURTHER INCIDENT. R SDR 29GA95757070511BStringer · corrodedDURING SCHEDULED X-RAY INSP, DISCOVERED .3750 INCH DIAMETER HOLE OF CORROSION ON THE LT WING "J" STRINGER AT WS 114.25. REMOVED CORROSION AND REPAIRED STRINGER.SDR 29GA95757070811AStringer · corrodedDURING SCHEDULED X-RAY INSP, DISCOVERED MINOR SPOT OF CORROSION ON THE LT WING "J" STRINGER JUST OTBD OF WS 114.25. REMOVED CORROSION AND REPAIRED STRINGER.SDR GLBA20110706HSupport · failedPILOT REPORTED THAT THE CABIN DOOR STRAP SUPPORT ON THE LT SIDE IS COMING APART. MX REINSTALLED A FASTENER ON THE LT CABIN DOOR STRAP SUPPORT IAW BMM 52-10-60, ALL CHECKS GOOD.SDR GLBA20110706FTire · failedPILOT REPORTED THAT THE LT INBD MAIN TIRE STRIPPED OF ITS CORD AFTER TOUCHDOWN, SHIMMY ON TOUCHDOWN. MX REPLACED THE NR 2 WHEEL ASSY IAW IAM TC 1900-3240-01.SDR GLBA20110706PSwitch · out of rigPILOT REPORTED THAT UPON RAISING THE LANDING GEAR WHILE FLAPS AT 17 DEGREES. TAKEOFF GEAR WARNING HORN SOUNDED AND COULD NOT BE SILENCED. IN TRANSIT LIGHT REMAINED ILLUMINATED UNTIL FLAPS 0 DEGREES WAS OBTAINED. MX RIGGED LANDING GEAR WARNING HORN FLAP POSITSDR GLBA20110706NGround Wire · brokenPILOT REPORTED THAT THE LT FIRE EXTINGUISHER DISCHARGE LIGHT ILLUMINATED IN FLT. MX FOUND BROKEN GROUND WIRE MAKING INTERMITTENT CONNECTION. R & R JACK KNIFE SPLICE IAW AIM 14.3.0 OPS CHECKED SYS.SDR GLBA20110706MCable · worn"SUP" - DURING A WALK-AROUND, THE PILOT FOUND THE FWD BOTTOM A/S DOOR CABLE ROD END BENT. MX R & R THE FWD BOTTOM A/S DOOR CABLE IAW BMM 52-10-02, PN: 1440-43GLA.SDR GLBA20110706LPanel · looseDURING AN INSPECTION, THE PILOT FOUND THE EMERGENCY EXIT INTERIOR PANEL LOOSE. MX RESECURED SPRINGS ON EMERGENCY EXIT INTERIOR PANEL BUTTON IAW BMM 52-20-00.SDR GLBA20110705HHandle · out of rigPILOT REPORTED THAT THE 6C EMERGENCY DOOR HANDLE WAS POPPED OUT. MX RIGGED THE DOOR HANDLE IAW BMM 52-20-00, OPS CK GOOD.SDR GLBA20110706KDoor · misinstalledPILOT REPORTED THAT DURING AN INSPECTION THE RT SIDE DOOR, 4C WAS NOT SEATED PROPERLY. MX REMOVED AND REINSTALLED THE EMERGENCY EXIT DOOR PROPERLY IAW BMM 52-20-00.SDR GLBA20110706JCable · failedDURING A ROUTINE INSP, MX FOUND THE FWD LWR A/S DOOR CABLE RUBBER TORN. MX REPLACED THE CABLE REF BMM 52-10-02, PN: 1440-43GLA.SDR 29GA93632070111AValve · inoperativeLANDING GEAR WOULD NOT EXTEND NORMALLY. PERFORMED MANUAL GEAR EXTENSION AND MADE NORMAL LANDING. R & R LANDING GEAR SERVICE VALVE.SDR GLBA20110705JPcb · inoperative"SUP" - SIG EVENT - PILOT REPORTED THAT THE LANDING GEAR HORN WAS INOPERATIVE. MX REPLACED PCB A119 PN: 112-3CY, OPS CK GOOD.SDR 29GA91279070111ATransducer · failedDURING CLIMB, NOTICED THE RT ENGINE OIL PRESSURE WAS BELOW 90 PSI, ALL OTHER ENGINE INDICATIONS WERE NORMAL. ADVISED ATC OF THE DIVERSION AND DECLARED AN EMERGENCY. LANDED WITHOUT FURTHER INCIDENT. R & R RT ENGINE OIL PRESSURE TRANSDUCER.SDR GLBA20110630OSwitch · false activationPILOT REPORTED THAT WHILE CLIMBING THROUGH 8,000 FT HAD A CABIN DOOR ANNUNCIATOR ILLUMINATE, NO EMERGENCY DECLARED, RETURN TO BASE. MX CHECKED CABIN DOOR SWITCHES FOR LOOSE CONNECTIONS, LUBRICATED. SWITCHES OPS CHECKED GOOD REF AIM 12-10-0, CHAP 12. REMOVEDSDR CA110704001Bearing · failedEIR PT6A 2011-075, IN CRUISE AT FL 190, A LARGE BANG FOR THE L/T ENGINE FOLLOWED BY A RAPID RISE IT ITT WAS EXPERIENCED. AS THE ITT WAS RISING TO APPROX 860, THE CREW REDUCED TORQUE TO MAINTAIN ITT WITHIN LIMITS. THE TORQUE WAS REDUCED TO 2000 FT/LBS WHERE SDR 29GA94671062911ATruss · crackedDURING MAGNETIC PARTICLE INSPECTION DISCOVERED ENGINE TRUSS COWLING ATTACH BRACKETS WELD AREA CRACKS AND RIGHT FORWARD LOWER ENGINE MOUNT ATTACH POINT WELD AREA CRACK. PERFORMED WELD REPAIR TO ENGINE TRUSS ATTACH BRACKETS WELD AREAS AND RIGHT FORWARD LOWER ENSDR GLBA201106291Latch · unsecureDURING AN INSP THE PILOT FOUND EMERGENCY EXIT 4C LATCH NOT SECURE. MX INSPECTED EMERGENCY DOOR 4C FOUND LATCH ON OUTSIDE DOOR. NOT SECURE REINSTALLED SECURE EMERGENCY DOOR 4C DOOR. SECURED REF MM 52-20-00 1(B).SDR GLBA20110629FSkin · debondedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP, MX FOUND THE AIRSTAIR DOOR EXTERIOR SKIN DEBONDING IN A 7" X 7" AREA AROUND THE PRESSURE LOCK. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-52-003. MATERIALS UTILIZED SDR 29GA94971062811ATruss · crackedDURING MAGNETIC PARTICLE INSPECTION DISCOVERED ENGINE TRUSS COWLING ATTACH BRACKETS WELD AREA CRACKS AND RIGHT FORWARD LOWER ENGINE MOUNT ATTACH POINT WELD AREA CRACK. PERFORMED WELD REPAIR TO ENGINE TRUSS ATTACH BRACKETS WELD AREAS AND RIGHT FORWARD LOWER ENSDR 29GA93761062811APressure Switch · malfunctionedPILOT REPORTS, ON APPROACH, RT PROPELLER CYCLES IN AND OUT OF AUTOFEATHER. REPLACED RT AUTOFEATHER LOW PRESSURE SWITCH.SDR GLBA20110630NCover · torn"SUP" - SIG EVENT - DURING ROUTINE MX INSP FOUND THE LWR AFT AS DOOR HANDRAIL CABLE COVER TORN. MX R & R LOWER AFT AS DOOR CABLE WITH REF TO D1900MM 52-10-02.SDR GLBA20110630MCover · torn"SUP" - SIG EVENT - DURING ROUTINE MX INSP, FOUND THE UPPER AFT AS DOOR CABLE COVER CUT. MX R & R UPPER AFT AS DOOR CABLE IN REF WITH MM 52-10-02.SDR GLBA20110630GCover · torn"SUP" - DURING A ROUTINE INSPECTION, MX FOUND THE UPPER FWD AIR STAIR DOOR CABLE COVER TORN. MX R & R THE UPPER FWD AS DOOR CABLE REF BMM 52-10-02.SDR GLBA20110630FSwitch · inoperativePILOT REPORTED THAT WHILE REDUCING POWER FROM 1200 LBS TORQUE TO IDLE NR1 ENGINE TRIED TO AUTOFEATHER. MX R & R LT & RT LOW PRESSURE AUTOFEATHER SWITCHES & RIGGED LT & RT ENGINE TORQUE IAW AIM CH 7, SECTION 7.5 & BMM 61-21-01, OPS CK GOOD.SDR GLBA20110627JFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP MX FOUND A CRACK IN THE AIR STAIR DOOR LOWER FRAME AT THE LOWER AFT CORNER, .75" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-53-043 MATERIALS UTISDR GLBA20110627HFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP, MX FOUND A CRACK IN THE FUSELAGE FRAME AT FS 456 AND STRINGER 10R, .2" IN LENGTH. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-042 MATERIALS UTILIZED ARE INCLUDED ISDR GLBA20110630LCable · warpedDURING ROUTINE MX INSP, FOUND THE LWR FWD AS DOOR CABLE WARPED. MX R & R LWR FWD AS DOOR CABLE IAW B1900MM REF 52-10-00 PN 1440-43GLA.SDR GLBA20110630KCable · out of adjustDURING ROUTINE MX INSP, FOUND THE A/S DOOR INTERNAL CABLE TENSIONS LOW. MX ADJUSTED CABLE TENSION AS REQURIED IAW MM REF 52-10-00.SDR GLBA20110630JSpring · broken"SUP" - SIG EVENT - DURING ROUTINE MX INSP, FOUND THE AS DOOR EXTERIOR HANDLE LOOSE. MX R & R AS DOOR SPRING REF 52-10-02, PN 129-5814093-1.SDR GLBA20110630HHandle · worn"SUP" - SIG EVENT - DURING ROUTINE MX INSP, FOUND THE AS DOOR EXTERIOR HANDLE LOOSE. MX R & R AS DOOR HANDLE REF 52-10-05, PN: 101-514176-17 AND SPRING REF 52-10-02, PN 129-5814093-1.SDR GUUA93632062711ASwitch · failedDURING APPROACH, LANDING GEAR WOULD NOT EXTEND ON APPROACH. NO GEAR UNSAFE GREEN LIGHTS WARNING HORN, DIVERTED, NORMAL LANDING WITH MANUAL EXTENSION. REPLACED LANDING GEAR SWITCH. OPS CHECKED GOOD.SDR GLBA20110628GConnector · loosePILOT REPORTED THAT WHEN THEY REDUCED POWER FROM 1200 TO IDLE THE LT ENGINE TRIED TO AUTOFEATHER, DISENGAGED AUTOFEATHER AND LANDED. MX RESECURED THE CONNECTOR PLUG ON THE LT LOW PRESSURE AFX SWITCH, OPS CK GOOD.SDR GLBA20110627GSkin · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP, MX FOUND A CRACK IN THE INNER SKIN OF THE EMERGENCY EXIT AT 6A, VERT LENGTH 3.25"M ABD HORZ 3". MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-52-007. MATERIALS UTILIZESDR GLBA20110628FBattery · dischargedPILOT REPORTED THAT THE FLIGHT DECK FLASHLIGHT NEEDS NEW BATTERIES. MX INSTALLED NEW BATTERIES, OPS CK GOOD.SDR GLBA20110627FSelector Valve · inoperativePILOT REPORTED THAT THE LANDING GEAR CIRCUIT BREAKER TRIPPED ON GEAR RETRACTION, GEAR DID NOT RETRACT. MX TROUBLESHOT MLG, REMOVED & INSTALLED SERVICABLE MLG SELECTOR VALVE IAW AMM 52-30-03-201, PERFORMED OPS CHECK IAW AIM MIC 32-01. OPS & LEAK CHECKED GOOD.SDR GLBA201106241Bulb · inoperativeINSTRUMENT EMERGENCY LIGHT ON F/O SIDE INOPERATIVE. MX REPLACED THE BULBS PN 1864 IAW BMM 33-10-00, OPS CHECKED GOOD.SDR V0DR2011012Bearing · failedUPON DISASSEMBLY, VENT BLOWER FOR O/H, TECH NOTICED 1 BEARING HAD FAILED. THE BEARING IS A SEALED UNIT. 1 SIDE OF THE BEARING SEAL HAD FALLEN OUT ALONG WITH PIECES OF THE BEARING'S ROLLER CAGE DURING REMOVAL FROM THE END BELL.SDR GUUA95152062211ALinkage · bindingDURING SCHEDULED ROUTINE STRUCTURAL INSP, DISCOVERED LT EMERGENCY DOOR LINKAGE OPEN AND CLOSE STIFF AND NOT WORKING CORRECTLY. CLEANED AND LUBRICATED LT EMERGENCY DOOR LOCKING MECHANISM, OPS CHECK GOOD.SDR CA110810009Connector · faultyELT BEGAN SOUNDING ON THE GROUND FOR NO APPARENT REASON. FAULTY "D" SUB CONNECTOR AT REMOTE SWITCH OF ELT SYS CAUSES ELT TO TRANSMIT INTERMITTENTLY. REPLACED CONNECTOR WITH MIL CRIMP TYPE. NO FURTHER FAILURES REPORTED.SDR GLBA20110621FUplock Switch · failed"SUP" - SIG EVENT - PILOT REPORTED THAT WHEN THE RETRACTED THE GEAR, THE INTRANSIT LIGHT WOULD NOT EXTINGUISH, LANDING GEAR EXTENDED WITH 3 GREENS WITH NO INTRANSIT LIGHT. MX REPLACED THE NLG UPLOCK SWITCH, OPS CHECK GOOD.SDR GUUA95652062011AControl Cable · brokenPILOT REPORTED PASSENGER AIRSTAIR DOOR WOULD NOT OPEN. REPLACED AIRSTAIR DOOR AFT LOWER CONTROL CABLE, OPS CHECK GOOD.SDR GUUA94253061711CAngle · crackedDURING SCHEDULED STRUCTURAL INSP, DISCOVERED RT HEAVY ANGLE CRACKED AT FORWARD END, APPROX 2.0 INCHES. STOP DRILLED CRACK AND INSTALLED REPAIR ANGLE.SDR GUUA94253061711BAngle · crackedDURING SCHEDULED STRUCTURAL INSP, DISCOVERED LT HEAVY ANGLE CRACKED AT FWD END APPROX 1.7 INCHES. STOP DRILLED CRACK AND INSTALLED REPAIR ANGLE.SDR GUUA94253061711ADoor Frame · crackedDURING SCHEDULED STRUCTURAL INSP, DISCOVERED AIRSTAIR DOOR FRAME CRACKED AT LOWER COUNTER BALANCE MOUNT. REMOVED DAMAGED PORTION OF ANGLE AND INSTALLED FRAME REPAIR SECTION.SDR GLBA20110614FDoor Frame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, MX FOUND A CRACK IN THE CARGO DOOR FUSELAGE FRAME AT FS 509.5 BETWEEN STRINGERS 3L AND 4L INNER FACE OF FRAME AT 2 FASTNER HOLES, 2" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSSDR GLBA20110615FSkin · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND A CRACK IN THE LT EMERGENCY EXIT INNER SKIN, LOWER FWD CORNER, 1.8" IN LENGTH. REPAIRED AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-52-006 MATERIALS UTILIZED ARESDR CA110614016Line · damagedCREW HAD RT BL FAIL ANNUNCIATOR ILLUMINATE IN FLIGHT. WHEN COMPLETING THE REQUIRED CHECK LIST TURNING THE BLEED OFF THERE WAS NO CORRESPONDING DECREASE IN ENGINE ITT. MX FOUND THAT THE FLARE ON PN 129-550084-X WAS CRACKED.SDR GLBA20110613JSkin · corrodedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION, MX FOUND A CORROSION IN THE BELLY SKIN AT FS 243.25 BETWEEN STRINGER 16 AND 15R. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-040 MATERIALS UTILIZED ARE INCLUDED
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