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 = '1900C' 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 = '1900C' 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 95ZZZX1969Skin · crackedON SCHEDULED MAINTENANCE A 1.5 INCH CRACK LOCATED OUTBOARD OF FIFTH RIB ON BOTTOM OF FLAP, FORWARD OF SPAR. REPAIRED WITH A 3.5 INCH BY 2.0 INCH PATCH.SDR 95ZZZX1994Line · crackedPRIMARY ENGINE FUEL LINE CRACKED AT FERRULE REINFORCEMENT RESULTNG IN LOSS OF SUFFICIENT FUEL PRESSURE TO MAKE REQUIRED POWER. TAKEOFF WAS ABORTED. SUSPECT CAUSED BY FATIGUE FROM ENVIRONMENT.SDR HERA9510Transmitter · defectiveANC - FLT 3423 - AIR TURN DUE TO THE NR 2 ENGINE OIL PRESSURE BEGAN FLUCTUATING BETWEEN 20 AND 120 PSI. THE ACFT LANDED ANC WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 OIL PRESSURE TRANSMITTER AND RETURNED THE ACFT TO SERVICE. (Z)SDR 95ZZZX2507Radome · crackedORD - WHILE AIRCRAFT WAS PARKED, A BAG CART IMPACTED THE RADOME. THE RADOME WAS REMOVED, THE MOUNTING STRUCTURE INSPECTED, AND REPLACED THE RADOME WITH SERVICEABLE.SDR 95ZZZX2506Switch · failedHON - AFTER TAKEOFF, THE CREW ELECTED AN AIR TURN-BACK DUE TO THE FLAPS BEING STUCK IN THE TAKEOFF POSITION. AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE REPLACED RT FLAP MICROSWITCH. THE FLAPS CYCLED SUCCESSFULLY.SDR 95ZZZX2508Aileron · dentedORD - WHILE PARKED WITHOUT PASSENGERS ON BOARD, THE LEFT WING TIP AND OUTBOARD TRAILING EDGE WERE DENTED BY A BAG CART TOW TRACTOR. MAINTENANCE REMOVED THE AILERON AND WING TIP AND INSPECTED THOSE AREAS FOR FURTHER DAMAGE. A SERVICEABLE AILERON AND WING TIP SDR 95ZZZX2509Engine Oil · lowDLH - INBOUND TO DLH, CREW EXPERIENCED THE RT ENGINE OIL PRESSURE FLUCTUATION BETWEEN 40-100 PSI ACCOMPANIED BY THE ILLUMINATION OF THE RT OIL PRESSURE ANNUNCIATOR. THE RT ENGINE WAS SECURED AFTER WHICH AN UNEVENTFUL LANDING WAS COMPLETED. MAINTENANCE INSPECSDR HERA9509Engine · failedFLT 1463 - AIR RETURN ANC, NR 2 ENGINE HAD TO BE SHUT DOWN DUE TO INTERNAL FAILURE. THE AIRCRAFT LANDED ANC WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE ENGINE AND RETURNED THE AIRCRAFT TO SERVICE. (W)SDR SW019505848Downlock Switch · failedPIT - UPON APPROACH, PILOT SELECTED GEAR DOWN AND DID NOT GET A NOSE DOWNLOCK INDICATION. REMOVED AND REPLACED DOWNLOCK SWITCH AND RETURNED TO SERVICE. (X)SDR 95ZZZX2020Aileron · dentedORD - WHILE PARKED WITHOUT PASSENGERS ON BOARD, A BAGGAGE TUG STRUCK THE LEFT AILERON. THE AILERON WAS REMOVED, THE SURROUNDING AREA INSPECTED, AND A SERVICEABLE AILERON INSTALLED. A TEST FLIGHT WAS SATISFACTORY.SDR 95ZZZX1967Truss · crackedRIGHT INBD FORWARD CRACK WAS FOUND DURING SCHEDULED MAINTENANCE AND REPAIRED BY WELDING PER TO 1900-71-20-0001, AND REPAIRED BY WELDING PER TO 1900-71-20-0001.SDR PLGA325951Connector · looseBOS - AFTER TAKEOFF THE LANDING GEAR FAILED TO RETRACT. THE AIRCRAFT RETURNED TO BOS LANDING WITHOUT INCIDENT. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT AND INSPECTED IT FOR FERRY FLIGHT PSM. PSM MAINTENANCE FOUND POWER WIRE G6D22 HAD PUSHED OUT OF THE SOCSDR 95ZZZX2021Rivet · looseSPW - DURING ROUTINE INSPECTION, MAINTENANCE FOUND 4 RIVETS IN RT FUEL TANK TOP SIDE BETWEEN THE NACELLE AND STALL FORCE LOOSE AND LEAKING FUEL. THE RIVETS WERE REPLACED, THE TANK SEALED, AND LEAK CHECK OKAY.SDR 95ZZZX1965Te Skin · crackedSPW - DURING ROUTINE MAINTENANCE, RUDDER TRAILING EDGE FAIRING WAS FOUND CRACKED AND HAD SEVERAL WORKING RIVETS. THE CRACK WAS REPAIRED AND RIVETS WERE REPLACED IAW DER APPROVED FROM 8110-3. RUDDER BALANCE CHECKED AND RESINSTALLED.SDR 95ZZZW549Beta System · out of rigAIRCRAFT LEFT PROP FEATHERED AT LIFT OFF AT DIA. RETURNED TO GATE WITHOUT INCIDENT FOUND BETA SYSTEM OUT TO RIG. FOUND BETA VALVE STICKING ALL THE WAY OUT. SUSPECT BETA CABLE WAS STRETCHED. RERIGGED BETA SYSTEM AND RETURNED TO SERVICE.SDR 95ZZZX1964Skin · crackedSPW - DURING ROUTINE INSPECTION, MAINTENANCE FOUND DORSAL FIN CRACKED ON LT SIDE AT REAR PRESSURE BULKHEAD ATTACH POINT. THE CRACK WAS BETWEEN TWO RIVET HOLES. INSTALLED REPAIR IAW BEECH 1900 SRM 51-70-00, PAGE 17.SDR 95ZZZX1963Truss · crackedSPW - DURING SCHEDULED VISUAL INSPECTION REQUIRED BY AD 95-02-18 IAW BEECH SB 2255R6, AREA OF THE RT ENGINE TRUSS WAS FOUND CRACKED. REPLACED TRUSS WITH SERVICEABLE.SDR 95ZZZX1941Flap · crackedREPAIRED A 1 INCH CRACK IN LOWER SKIN ALONG TRAILING EDGE APPROXIMATELY 38 INCHES OUTBOARD FROM INBOARD END OF THE RIGHT OUTBOARD FLAP. REPAIRED BY STOP DRILLING AND INSTALLING A DOUBLER IAW TECH ORDER NR 1900-27-00-0001.SDR SW019505853Bracket · bentPIT - UPON FINAL, PILOT SELECTED GEAR DOWN AND DID NOT GET A NOSE DOWNLOCK INDICATION. MAINTENANCE REPAIRED DOWNLOCK ADJUSTMENT BRACKET AND RETURNED TO SERVICE. (X)SDR 95ZZZX1862Air Distr · smokingBOS - WHILE ON THE GROUND WITH EXTERNAL POWER CONNECTED AND SELECTED ON, JUST PRIOR TO FIRST ENGINE START, THE CREW EXPERIENCED SMOKE IN THE COCKPIT. THE AIRCRAFT WAS SHUT DOWN, DEPLANED, AND MAINTENANCE NOTIFIED. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT. SDR 95ZZZX1506Bracket · failedAIRCRAFT EXPERIENCED ASYMMETRICAL FLAP CONDITION DURING APPROACH AFTER FLAPS WERE EXTENDED TO 35 DEGREES. REQUIRED FULL RIGHT AILERON USING EXTREME FORCE WITH BOTH HANDS TO REGAIN LEVEL FLIGHT. FOUND AFT FLAP BEARING OUTER RACE FLANGE OF THE LEFT OTUBOARD FLSDR 95ZZZW471Cable Lockplate · detachedDURING THE PREFLIGHT PROPELLER MANUAL FEATHER CHECK THE PROPELLERS WOULD NOT FEATHER, ALL OTHER PROPELLER FUNCTIONS OPERATED NORMALLY. THE PROPELLER CONTROL LEVER LINKAGES WERE INSPECTED. THE RIVETS SECURING THE PROPELLER CONTROL CABLE LOCKPLATE TO THE AIRFRSDR PLGA322951Washer · failedTHIS SDR (DATED 3-22-95) IS TO SUPPLEMENT AN SDR DATED 3-14-95. PRELIMINARY FINDINGS FROM THE OVERHAUL FACILITY VERIFIED A FAILURE OF WASHER, PN A3087. THE OVERHAUL FACILITY CONTACTED THE MANUFACTURER WHO CONFIRMED A POTENTIAL PROBLEM DUE TO A 'SOFT' BATCH OSDR 95ZZZX1940Flap · crackedDURING SCHEDULED MAINTENANCE, AN INSPECTION OF THE RIGHT INBOARD FLAP REVEALED A CRACK IN THE UPPER SKIN ALONG THE TRAILING EDGE APPROXIMATELY 26 INCHES OUTBOARD FROM THE INBOARD END. THE CRACK WAS REPAIRED BY STOP DRILLING AND INSTALLING A DOUBLER.SDR 95ZZZX1860Retainer · failedDURING A SCHEDULED OIL FILTER INSPECTION, FINE METAL DEBRIS WAS FOUND IN THE LEFT ENGINE OIL FILTER. DUE TO PRIOR OPERATING EXPERIENCE, AN INTERNAL BORESCOPE OF THE PROPELLER WAS PERFORMED. THE BORESCOPE INSPECTION REVEALED DISTRESS TO THE FEATHERING SPRING SDR 95ZZZW469Downlock Switch · out of adjustFLT 1412 - LANDING ANC COULD NOT GET A SAFE NOSE GEAR DOWN INDICATION (GREEN LIGHT) WHEN THE LANDING GEAR WAS LOWERED. A MANUAL GEAR EXTENSION WAS PERFORMED WITH THE NOSE GEAR STILL SHOWING UNSAFE. A LANDING WAS MADE AT ANC WITHOUT INCIDENT. MAINTENANCE RIGGSDR 95ZZZX1667Limit Switches · out of adjustLGA - FLT 4869 - AFTER TAKEOFF, FLAPS WOULD NOT RETRACT. AIRCRAFT RETURNED TO LGA AND LANDED WITHOUT INCIDENT. FLAPS WERE BROUGHT UP TO ZERO AND MEL'D. UPON ARRIVAL PSM RE-RIGGED FLAP UP AND DOWN LIMIT SWITCHES. ALL CHECKS WERE SATISFACTORY. ALL WORK WAS SDR PLGA321951Retract Mech · lack of lubeTHIS SDR (DATED 3-21-95) IS TO CLOSE OUT AN SDR DATED 3-8-95 WHERE THE FLAPS WERE MEL'D AFTER FAILING IN THE TAKEOFF POSITION. MAINTENANCE CLEANED AND LUBED THE FLAP ASYMMETRY SWITCHES AND PERFORMED SATISFACOTRY OPERATIONAL CHECK OF THE SYSTEM. (X)SDR 95ZZZX1966Computer · burnedAFTER TAKEOFF, CREW REPORTED SMOKE COMING INTO COCKPIT AND CIRCUIT BREAKER (YAW DAMPER SERVO) TRIPPED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED YAW DAMPER SYSTEM AND FOUND YAW DAMPER COMPUTER BURNED. SYSTEM WAS DISABLED DEFERRED.SDR 95ZZZX1944Computer · burnedAFTER TAKEOFF, CREW REPORTED SMOKE COMING INTO COCKPIT AND CIRCUIT BREAKER (YAW DAMPER SERVO) TRIPPED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED YAW DAMPER SYSTEM AND FOUND YAW DAMPER COMPUTER BURNED. SYSTEM WAS DISABLED AND DEFERRED. OPERATOSDR 95ZZZW335Downlock Switch · intermittentDURING TAXI FROM GATE ON ORIGINATING FLIGHT FROM DSM, THE LANDING GEAR INTRANSIT LIGHT ILLUMINATED AND WARNING HORN SOUNDED INTERMTTENTLY. LOCAL FBO COULD NOT DUPLICATE PROBLEM. AIRCRAFT WAS FERRIED TO ICT WHERE MAINTENANCE FOUND THE NOSE GEAR DOWNLOCK SWITCSDR 95ZZZW334Downlock Switch · intermittentFLT NR 5682 - ON APPROACH TO MCI WITH THE LANDING GEAR DOWN, WHEN THE FLAPS WERE EXTENDED FULL, THE GEAR INTRANSIT LIGHT ILLUMINATED AND THE GEAR WARNING HORN SOUNDED INTERMITTENTLY. AIRCRAFT LANDED WITHOUT INCIDENT. INSPECTED AIRCRAFT AND FERRIED TO ICT. MSDR 95ZZZX1961Propeller · damagedMSP - DURING TAXI TO THE TERMINAL, THE RT PROPELLER CONTACTED A RAMP BAGGAGE CART. THE PROPELLER WAS CHANGED AND AS A PRECAUTION, ENGINE AND TRUSS WERE CHANGED. SMALL REPAIRS WERE ACCOMPLISHED TO THE FUSELAGE SKIN IAW THE BEECH SRM.SDR 95ZZZX1960Control Handle · shortedMSP - CREW REPORTED THE LANDING GEAR WOULD BLOW THE CIRCUIT BREAKER WHEN SELECTED TO EXTEND. GEAR LOWERED MANUALLY AND AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE REPLACED LANDING GEAR CONTROL HANDLE, THE CIRCUIT BREAKER, AND REPAIRED A BROKEN WIRE.SDR 95ZZZX1939Flap · crackedDURING SCHEDULED MAINTENANCE, AN INSPECTION OF THE RIGHT INBOARD FLAP REVEALED A 1 INCH CRACK IN THE UPPER SKIN DIRECTLY AFT OF THE AFT NACELLE FAIRING. THE CRACK WAS REPAIRED BY STOP DRILLING AND INSTALLING A DOUBLER.SDR 95ZZZX1968End Cap · crackedON SCHEDULED MAINTENANCE, A SMALL CRACK INBD END CAP, WAS FOUND 4 INCHES UP FROM T/E ON TOP OF FLAP. REPAIRED WITH PATCH.SDR 95ZZZX1938Flap · crackedDURING SCHEDULED MAINTENANCE, AN INSPECTION OF THE RIGHT INBOARD FLAP REVEALED A 2 INCH CRACK IN THE BOTTOM SKIN ALONG THE TRAILING EDGE BETWEEN THE THIRD AND FOURTH RIB OUTBOARD FROM THE INBOARD END. THE CRACK WAS REPAIRED BY STOP DRILLING AND INSTALLING A DSDR 95ZZZX1959Flap Motor · wornESC - CREW REPORTED THE FLAP MOTOR RAN SLOW AND THEY SMELLED ELECTRICAL SMOKE IN THE COCKPIT. REPLACED FLAP MOTOR WHICH CHECKED GOOD.SDR 95ZZZX1958Fuel Control · out of adjustSPI - CREW ELECTED AN AIR TURN-BACK AFTER TAKEOFF DUE TO LEFT ENGINE TORQUE SURGES OF PLUS OR MINUS 200 FEET/POUNDS. AFTER AN UNEVENTFUL LANDING, MAINTENANCE REPLACED THE FUEL CONTROL UNIT. POWER RUNS WERE SATISFACTORY.SDR 95ZZZX1728Skin · crackedDURING SCHEDULED MAINTENANCE, AN INSPECTION OF THE RIGHT OUTBOARD FLAP, PN 35165050259, REVEALED A CRACK IN THE UPPER SKIN APPROXIMATELY 3 INCHES OUTBOARD FROM THE INBOARD END. THE CRACK WAS REPAIRED BY STOP DRILLING AND INSTALLING A 1.5 INCH BY 6 INCH DOUBLESDR 95ZZZW336Mount Truss · crackedDURING A SCHEDULED ENGINE CHANGE AN INSPECTION OF THE LEFT ENGINE MOUNT TRUSS REVEALED A .500 INCH CRACK IN THE UPPER INBOARD FORWARD TUBE AT THE UPPER INBOARD FORWARD TUBE INTERSECTION WELD. THE CRACK WAS REPAIRED BY WELDING.SDR 95ZZZW332Mount Truss · crackedDURING A SCHEDULED AD92-06-09 AREA 'A' INSPECTION OF THE LEFT ENGINE MOUNT TRUSS ASSEMBLY REVEALED A .300 INCH CRACK IN THE TOP OF THE OUTBOARD FORWARD UPPER COWL ATTACH BRACKET. THE CRACK WAS REPAIRED BY WELDING.SDR 95ZZZX1956Bleed Valve · faultyMSP - ON APPROACH THE RT ENGINE STALLED, AFTER WHICH THE CREW SHUT DOWN AND SECURED THE ENGINE. AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE REPLACED THE COMPRESSOR BLEED VALVE. AFTER A SUCCESSFUL TEST FLIGHT, THE AIRCRAFT WAS RELEASED FROM MAINTENASDR 95ZZZX1955Downlock Wire · brokenMSP - CREW REPORTED THE RT MAIN GEAR UNSAFE INDICATION ILLUMINATED WHEN GEAR SELECTED DOWN. AFTER AN UNEVENTFUL LANDING, MAINTENANCE REPAIRED A BROKEN WIRE AT THE DOWNLOCK SWITCH ON THE DRAG LEG. A GEAR SWING WAS SATISFACTORY.SDR 95ZZZW783Seal · failedPBI-TPA - FLT NR 2283 WAS LEVEL AT 16,000 FEET AND READY TO BEGIN DESCENT TO 10,000 FEET WHEN A LOUD EXPLOSION FOLLOWED BY CABIN PRESSURIZATION WAS EXPERIENCED. AIRCRAFT WAS LANDED SAFELY IN TPA WHERE GP EXPRESS MAINTENANCE FOUND THE CABIN DOOR SEAL BLWON OUTSDR 95ZZZX1816Bearing · spalledPRELIMINARY FINDINGS ARE FOCUSING ON THE ARCING AND MAGNETISM FOUND THROUGHOUT THE ENTIRE GEAR TRAIN.SDR 95ZZZZ139Hsi · failedFLT NR 2099 - AFTER DEPARTURE FROM DEN, THE CAPTAINS HSI WENT INOP. AIRCRAFT RETURNED TO DEN WHERE GP EXPRESS MAINTENANCE REPLACED THIS HSI WITH A SERVICEABLE UNIT. SYSTEM GROUND CHECKED SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (Z)SDR 95ZZZW470Engine · failedON DEPARTURE OUT OF CSP RIGHT ENGINE TORQUE SURGED. CREW NOTICED RT OIL PRESSURE DROPPED AND SECURED ENGINE AT WHICH TIME A SEVERE VIBRATION WAS NOTICED. RETURNED TO CSP WITHOUT FURTHER INCIDENT. UPON ARRIVAL NO OIL WAS PRESENT IN RT ENGINE, OR WAS A LEAK NSDR 95ZZZX1954Eva Tubing · crackedSPW - AFTER TAKEOFF, CREW ELECTED AN AIR TURN-BACK WHEN THE LEFT BLEED AIR FAIL ANNUNCIATOR ILLUMINATED. AFTER AN UNEVENTFUL LANDING, MAINTENANCE REPAIRED AND LEAK CHECKED THE EVA TUBING.SDR 95ZZZX871Relay · failedPSP/LAX - EN ROUTE, CREW SMELLED SMOKE AND NOTICED LIGHT HAZE IN COCKPIT AREA. THEY CLEARED SMOKE WITH VENT AND MADE PRECAUTIONARY LANDING AT ONT. BEECH DEALER RAN SYSTEMS CHECKS AND FOUND NO MALFUNCTION. AIRCRAFT FERRIED TO HOMEBASE AND FURTHER INSPECTION
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