Raytheon 1900D
Service difficulty reports · 7,152
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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 S2YA00031Wheel · vibrationAFTER TAKE OFF OF FLIGHT THE CAPTAIN REPORTED AN UNUSUAL VIBRATION THE AIRCRAFT. THE CREW MADE AN AIRTURNBACK TO MKE. MAINTENANCE REMOVED AND REPLACED THE NOSE WHEEL AND RETURNED THE AIRCRAFT TO SERVICE.SDR 20010123CW004Bearing · failedRT ENGINE FAILURE IN FLIGHT. ENGINE FAILED DUE TO NR1 BEARING FAILURE.SDR 20010111SG033Control Handle · inoperativeAIRCRAFT RETURNED TO STATION AFTER CREW ATTEMPTED TO RETRACT THE LANDING GEAR. THE FLIGHT CREW WAS UNABLE TO MOVE THE LANDING GEAR HANDLE TO THE RETRACTED POSITION. THE LANDING GEAR CONTROL HANDLE WAS CLEANED AND LUBRICATED. THE LANDING GEAR RETRACTION TESTSDR 20010111SG032Motor · inoperativeWHEN ATTEMPTING TO EXTEND THE LANDING GEAR THE CIRCUIT BREAKERPOPPED. THE LANDING GEAR WAS MANUALLY EXTENDED. FOUND LANDING GEAR MOTOR SHORTED. REPLACED THE MOTOR. LANDING GEAR RETRACTION/EXTENSION TEST WAS GOOD. (M)SDR 20001229AP019Engine · seizedUPON ENGINE START IN SHR, FOUND IT TO BE IMPOSSIBLE TO ROTATE THE LEFT PROPELLER. FOUND THE ENGINE POWER SECTION SEIZED. REPLACED THE POWER SECTION. THE AIRCRAFT WAS RELEASED TO SERVICE. (M)SDR CA001020003Line · failed(CAN) RT BLEED AIR FAIL WARNING LIGHT COME ON DURING FLIGHT. AFTER INVESTIGATION WE FOUND THAT THE BLEED AIR TUBE WAS CRACKED AROUND THE FITTING WELDING JOINT.SDR S2YA00030Display · failedAFTER TAKE OFF OF FLIGHT THE F.O. EHSI SCREEN WENT BLANK. THE CREW MADE AN AIR TURN BACK TO MKE. MAINTENANCE REMOVED AND REPLACED THE NR 2 DPU84, PERFORMED OPERATION CHECK AND RETURNED THE AIRCRAFT TO SERVICE.SDR 20001229AP015Circuit Board · failedLANDING GEAR WOULD NOT EXTEND AND HAD TO BE MANUALLY EXTENDED. FOUND LOOSE PIN ON THE LANDING GEAR PRITED CIRCUIT BOARD A316. RESECURED PIN, LANDING GEAR EXTENSION, RETRACTION TEST GOOD. (M)SDR 20001229AP014Motor · inoperativeTHE CREW HAD TO PUMP THE LANDING GEAR TO EXTEND. REPLACED THE LANDING GEAR HYDRAULIC POWER PACK MOTOR. RETRACTION/EXTENSION CHECK GOOD. (M)SDR 20001229AP013Cam · wornLEFT UPPER COWLING CAME UNLATCHED SHORTLY AFTER TAKEOFF. THE AIRCRAFT RETURNED TO GRI. MAINTENANCE INSPECTED AND DETERMINED THE HOOK AND CAM ASSY WAS AFFECTED BY VIBRATION. REPLACED THE HOOK AND CAM ASSY. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR 20001229AP012Connector · unsecureLANDING GEAR WOULD NOT EXTEND UNTIL THE 4TH ATTEMPT. RESECURED ELECTRICAL CONNECTOR TO PCB A316. OPERATIONAL CHECK GOOD. (M)SDR 20010111SG023Pressure Switch · failedCLE - FLT 3170 - THE CREW REPORTED THE RIGHT AUTO FEATHER TEST WAS NOT FEATHERING THE PROPELLER. THE AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 AUTO FEATHER LOW PRESSURE SWITCH (P/N 50-389121-29)IAW 61-21-01. MAINTENANSDR C2XA00CL075Circuit Board · failedCLE - FLT 3170 - THE CREW REPORTED THE RIGHT AUTO FEATHER TEST WAS NOT FEATHERING THE PROPELLER. THE AIRCRAFT RETURNED TO GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 AUTO FEATHER LOW PRESSURE SWITCH (P/N 50-389121-29)IAW 61-21-01. MAINTENANSDR C2XA00CL071Wire · chafedCLE - FLT 3264 - DURING APPROACH, THE GEAR INDICATOR CIRCUIT BREAKER POPPED. THE CREW RESET AND THE BREAKER POPPED AGAIN. THERE WERE NO GEAR INDICATION LIGHTS BUT THE PILOTS WERE ABLE TO VERIFY THE GEAR WAS DOWN. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENTSDR C2XA00CL066Governor · malfunctionedTHE CREW REPORTED ON LANDING APPROACH (FLARE) RIGHT PROPELLER FEATHERED CAUSING THE A/C TO YAW SEVERELY TO RIGHT. A/C LANDED SAFELY WITHOUT FURTHER INCIDENT. MX REMOVED/REPLACED RIGHT PROPELLER GOVERNOR IAW BEECHCRAFT MM 61-20-00. THE OPS WERE GOOD AND A/C WASSDR 20001229AP010Gyro · failedHEADING FLAG ILLUMINATES IN FLIGHT. NR 1 AND NR 2 DIRECTIONAL GYROS INDICATE PLUS OR MINUS 40 DEGREES. PROBLEM ISOLATED TO NR 1 DIRECTIONAL GYRO. REMOVED AND REPLACED NR 1 GYRO. (M)SDR CA000928016Indicator · failed(CAN) MAINT CREW REPLACED LANDING GEAR INDICATOR LIGHT ASSY ON PREVIOUS NIGHT SHIFT DUE TO SCHED MAINT DISCREPANCY RELATING TO MALFING BULB HOLDER SPRING & CAM SUB-ASSEMBLESON IND. LIGHT ASSY. CORRECTIVE ACTION INC LUDED GEAR RETRACTIN & EXTENSIONS IAW MM. 1STSDR 20001208AP008Indicator · inoperativeCAPTAINS ALTIMETER FLAGGED, ALTITUDE PRESELECTOR INOPERATIVE, AND NR 1 MODE C INOPERATIVE. REMOVED AND REPLACED CAPTAINS ALTIMETER. SYSTEM TESTS GOOD. (M)SDR CA000928018Bearing · failed(CAN) DURING DESCENT, CREW NOTICED FOLLOWING INDICATORS ON RT ENGINE INSTRUMENTS. TORQUE HAD DROPPED TO ZERO, NG HAD FALLEN TO 66 PERCENT & ITT APPROX. 800 DEGS. ALL OTHER ENGINE PARAMETERS WERE NORMAL. AS POWER LEVER ADVANCED IN ORDER TO INCREASE NG ITT WOULDSDR C2XA00CL062Switch · looseON APPROACH TO CLE CREW REPORTED RIGHT SIDE OF FIRST OFFICER''S CONTROL WHEEL (YOKE) WAS EMITTING SMOKE. A EMERGENCY WAS DECLARED AND A/C LANDED AND TAXIED TO GATE WITHOUT FURTHER INCIDENT. MX INSPECTED AND REASSEMBLED THE FIRT OFFICER''S FLIGHT DIRECTOR SYNC,SDR EY2R57207Erosion Shield · crackedTHREE EROSION SHIELDS HAD CRACKS IN VARIOUS PLACES. REPLACED WITH NEW S/N C2082, C2071, C2075. (X)SDR C2XA00CL060Duct · disconnectedFLT 3130 - AFTER TAKEOFF, THE CREW REPORTED A BURNING SMELL IN COCKPIT (ELECTRICAL). THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. AFTER LANDING THE SMELL DISSIPATED. MAINTENANCE INSPECTED AND FOUND THE NR 2 ENGINE BLEED DUCT ON THE PRECOOLERSDR 20001204AP012Connector · shortedWHILE CLIMBING THROUGH 9000 FEET, SMOKE STARTED COMING OUT OF THE OVERHEAD PANEL. ALL OVERHEAD PANEL SWITCHES WERE SHUTOFF AND AIRCRAFT RETURNED TO POINT OF DEPARTURE (RIW). FOUND RECOGNITION LIGHT SWITCH LOOSE AND WIRE INSULATION BURNED. MAINTENANCE REPLACSDR EY2R57102Bearing · corrodedTHREE SPLIT BEARING HAD CORROSION ON SURFACE. REPLACED. (X)SDR EY2R57100AErosion Shield · crackedEROSION SHIELD HAD CRACKS IN VARIOUS AREAS ON BLADE NR 2. REPLACED WITH NEW S/N C2074. (X)SDR EY2R57100Bracket · crackedDEICE BRACKET CRACKED IN RADIUS. REPLACED. (X)SDR C2XA00CL058Actuator · failedPIT - FLT 3030 - ON APPROACH TO PIT, THE LEFT MLG FAILED TO EXTEND. THE CREW RECYCLED THE GEAR AND THE GEAR CAME DOWN WITH NORMAL INDICATION. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT MLG ACTUATOR IAW BEECHCRAFTSDR EY2R57007AErosion Shield · crackedEROSION SHIELD CRACKED IN VARIOUS PLACES ON THREE BLADES. REPLACED EROSION SHIELD ON THREE BLADES. REPLACEMENT S/N'S C2083, C2081, C1512SDR EY2R57007Hub · corrodedHUB CORRODED IN CYLINDER THREADS. REPLACED HUB.SDR S2YA00023Block · wornFLT 1354 - MKE-TVC - SHORTLY AFTER TAKEOFF, THE LEFT ENGINE TORQUE STARTED FLUCTUATED 100-200 LB. THE CREW MADE AN AIR-TURN-BACK AND AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE ENGINE AND REPLACED THE BETA BLOCK. MAINTENANCE OPS CHECKED THE A/C AND RETSDR AU000584Fork · out of rig(AUS) RT PROPELLER REVERSE STOP INCORRECTLY SET. PITCH CHANGE FORK CRACKED.SDR C2XA00CL054Skin · failedAZO - DURING A 3RD 200 HOUR INSPECTION, A 1.5 INCH CRACK WAS FOUND ON THE EXTERIOR SKIN ON THE RIGHT WING ROOT INBOARD JUST FORWARD OF WING SPAR. MAINTENANCE REMOVED THE INTERIOR FOR INSPECTION OF THE SPAR AND SURROUNDING AREAS AND FOUND NO OTHER DAMAGE. THESDR S2YA00022Outflow Valve · inoperativeFLT 1001 - MKE-STL - THE CABIN ALT HI ILLUMINATED AND THE CABIN OXYGEN MASKS WERE DEPLOYED. THE CREW MADE AN UNEVENTFUL LANDING IN STL AND CONTACTED MX. OUTSTATION MAINTENANCE PERFORM THE MX FUNCTIONS AND MEL THE PRESSURIZATION. THE AIRCRAFT WAS RETURNED TOSDR 20001018AP006Indicator · reads highRIGHT ENGINE OIL TEMPERATURE ALMOST AT RED LINE. PROBLEM FOUND TO BE A DEFECTIVE OIL TEMPERATIVE INDICATOR. INDICATOR REPLACED AND A/C RETURNED TO SERVICE. (M)SDR EY2R56924AErosion Shield · crackedTHREE AREAS OF EROSION SHIELD ON THREE BLADES CRACKED ON BOTH FACE AND CAMBER SIDES. REPLACED ALL EROSION SHIELDS. S/N''S INSTALLED C1951, C1623, C1610, AND C2084.SDR EY2R56924Rod · corrodedBETA RODS CORRODED IN THREAD AREA. (X)SDR 0001024AP005Strap · chafedAVIONICS ANNUNCIATOR CIRCUIT BREAKER POPPED CONCURRENT WITH SMOKE SMELL IN COCKPIT. AVIONICS ANNUNCIATOR WOULD NOT ILUMINATE AND PA AND CO-PILOTS PHONE CIRCUIT BREAKER WOULD NOT RESET. FOUND BONDING STRAP CHAFING ON GPWS WIRING. REPAIRED WIRING AND BONDING SDR CA000724014Relay · failed(CAN) AFTER TAKEOFF THE PILOT SELECTED THE GEAR UP BUT THEY DIDN'T MOVE. THEY DIVERTED THE FLIGHT TO YQB. AFTER INVESTIGATION WE FOUND RELAY LANDING GEAR MOTOR P/N MS24171D1 IN LT NACELLE COMPLETELY BURNED.SDR 20001018AP005Tach Generator · bindingRIGHT PROP RPM FLUCTUATING. FOUND PROBLEMS TO BE A DEFECTIVE TACH GENERATOR. UNIT REPLACED AND A/C RETURNED TO SERVICE. (M)SDR C2XA00CL050Actuator · failedCLE - FLT 3042 - ON APPROACH, THE CREW SELECTED THE GEAR DOWN AND DID NOT GET THE GREEN INDICATION FOR A DOWN AND LOCKED ON THE RIGHT GEAR. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT MAIN LANDING GEAR DOWNLOCK POSITION SSDR CA000731022Cooler · cracked(CAN) AIRCRAFT ARRIVED WITH SMALL OIL LEAK ON RT LOWER ENGINE NACELLE. PRECOOLER HAD CRACKED ALLOWING HOT P3 AIR TO BLOW ONTO OIL COOLER. OIL COOLER FINS MELTED ALLOWING OIL LEAK. OIL COOLER P/N 114-389000-5.THIS IS SECOND INSTANCE FOR THIS DEFECT FOR OUR FLEESDR S2YA00021Windshield · crackedFLT 1198 - MKE-IND - AT FL210, THE CO-PILOTS WINDSHIELD CRACKED. THE CREW MADE AN AIR-TURN-BACK AND AN UNEVENTFUL LANDING AT MKE. MAINTENANCE REMOVED AND REPLACED THE WINDSHIELD AND RETURNED THE AIRCRAFT TO SERVICE. (M)SDR 20001018AP004Gyro · bindingCAPTAINS EADI PITCH COMPARATOR INOPERATIVE. TROUBLESHOOTING FOUND NR 1 VERTICAL GYRO DEFECTIVE. REPLACED UNIT AND RETURNED A/C TO SERVICE. (M)SDR 20001018AP003Cooler · leakingOIL LEAK LEFT ENGINE LOWER AFT COWL AREA. INSPECTION FOUND OIL COOLER LEAKING. REPLACED OIL COOLER, AIRCRAFT RETURNED TO SERVICE. (M)SDR CA000731024Fuel Control · jammed(CAN) AFTER ROUTINE MAINTENANCE THE AIRCRAFT WAS STARTED FOR GROUND RUN. ENGINE STARTED NORMALLY BUT HAD LOWER THAN NORMAL GAS GENERATOR SPEED. POWER LEVER INPUTS MADE LITTLE OR NO EFFECT TO ENGINE AND MAX POWER INPUT ONLY INCREASE ENGINE TO HIGH IDLE SPEED. PSDR S2YA00019Circuit Breaker · inoperativeMKE-IND - FLT 1052 - SHORTLY AFTER TAKEOFF, THE CREW WAS GOING TO SELECT GEAR UP BUT NOTED THE J HOOK WAS ENGAGED. THE CREW MOVED THE J HOOK AND ATTEMPTED TO RETRACT THE GEAR BUT IT STILL INDICATING DOWN AND LOCKED. THE CREW MADE AN AIR-TURN-ACK AND AN UNEVESDR S2YA00018Radar · inoperativeFLT 1026 - MKE-CVG - DURING FLIGHT, THE RADAR DISPLAYED FAULT THREE TIMES AND IT WOULD NOT PAINT UNLESS THE GAIN WAS TURNED ALL THE WAY UP. THE CREW DIVERTED TO FWA BECAUSE THERE WAS KNOW WEATHER ON ROUTE TO CVG. MAINTENANCE WAS CONTACTED FROM FWA AND THE RASDR EY2R56728Bearing · crackedOUTBOARD BEARING HALF CRACKED NR 2 BLADE. REPLACED.SDR 20001115SH017Door Frame · fracturedENTRANCE DOOR, FORWARD SUPPORT CABLE ANCHOR BROKEN. ANCHOR IS MADE FROM WRONG TYPE MATERIAL AND BREAKS WHEN ANY SIDE LOAD IS APPLIED TO CABLE; THUS, CREATING A SAFETY HAZARD. (X)SDR MASA00054Strut · damagedFLT 610 - FMN-ABQ - EXPERIENCED THE PASSENGER DOOR DIFFICULT TO OPEN OR CLOSE. MAINTENANCE REMOVED AND REPLACED STRUT. OPS CHECKED GOOD. (M)
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