Raytheon 1900D
Service difficulty reports · 7,152
Newest first. General aviation reporting is voluntary.
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 20000510AP003Indicator · malfunctionedCAPTAINS ALTIMETER, ALTITUDE PRESELECT, TRANSPONDER, AND TCAS FAILED ON DEPARTURE. LANDED AND RETURNED TO GATE. MAINTENANCE PERSONNEL GROUND TESTED THE SYSTEM AND COULD NOT DUPLICATE THE PROBLEM. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)SDR 20000508SH028Gyro · failedPILOT WRITE-UP WAS ''HDG WON''T MOVE WITH AIRCRAFT MOVEMENT''. THIS GYRO IS LOCKED UP. (X)SDR 20000508SH015Altimeter · malfunctionedUNIT PULLED FROM AIRCRAFT FOR RE-CERTIFICATION. BENCH TEST REVEALED ALTITUDE READ OUT WAS CONSISTENLY LOW PF ABOUT 20 FEET TO 150 FEET IN THE RANGE OF -1000 FEET 4,000 FEET. A CHECK ABOVE 4,000 FEET WAS NOT COMPLETED DUE TO THE LARGE ERROR AT THE LOW END. SDR 20000516AP004Governor · failedLOUD NOISE ON TAKEOFF ROLL FROM LEFT ENGINE. MAXIMUM PROP RPM 1500 RPM. REMOVED AND REPLACED LEFT PROP GOVERNOR. SYSTEM GROUND AND FLIGHT CHECK SATISFACTORY. (M)SDR S2YA00005Switch · out of rigFLT 1630 - MKE-CMH - SHORTLY AFTER TAKEOFF, THE CABIN DOOR ANNUNCIATE ILLUMINATED AND THE CREW MADE AN AIRTURN BACK TO MKE. AFTER AN UNEVENTFUL LANDING THE CREW CONSULTED WITH MX AND PUT THE ANNUNCIATOR ON MEL. MAINTENANCE CLEARED THE MEL 3/21/00 BY CLEANINGSDR 20000505AP029Seal · leakingNR 1 ENGINE SHUTDOWN DUE TO LOSS OF OIL PRESSURE AND OIL PRESSURE ILLUMINATING. THE ENGINE WAS REPLACED AFTER IT WAS FOUND THAT THE ENGINE HAD EXCEEDED THE RUN TIME AT LOW OIL PRESSURE. ENGINE HAD HIGH OIL CONSUMPTION AT HIGH ALTITUDES. LABRYNTH SEAL WAS FOSDR S2YA00004Windshield · crackedFLT 1094 - FNT-MKE - THE CAPTAINS WINDSHIELD CRACKED. THE CREW DIVERTED TO MKG AD MADE AN UNEVENTFUL LANDING. MKE MAINTENANCE WAS CONTACTED AND THE AIRCRAFT WAS FERRIED BACK TO MKE. MAINTENANCE REPLACED THE WINDSHIELD AND RETURNED THE A/C TO SERVICE. (M)SDR CA000322007Governor · failed(CAN) OVERSPEED GOVERNOR FOUND TO BE CONTROLLING PROP SPEED GOVERNOR, REPLACED.SDR 20000425SH036Gyro · failedPILOT REPORTED THAT ''GYRO FREEZES UP''. NR 1 DIRECTIONAL GYRO REMOVED AND SENT TO TEST FACILITY.SDR CA000316006Cooler · cracked(CAN) WHILE PASSING THROUGH 13,000 FEET, THE PILOT NOTICED A BURNING SMELL. WHITE SMOKE WAS ALSO SEEN IN THE CABIN. INVESTIGATION FOUND BOTH THE ENGINE PRECOOLERS CRACKED ON THE COOLING FIN.SDR CA000314008Cooler · cracked(CAN) DURING CLIMB AT AROUND 17,000 FEET, THE PILOT COULD SMELL OIL FUMES AND SEE SMOKE IN THE CABIN. INVESTIGATION FOUND THE PRECOOLER COOLING FIN CRACKED ON THE SIDE OF THE INLET PORT LOCATED AT THE BOTTOM REAR. OIL HAD LEAKED IN CAUSING THE FUMES.SDR CA000314003Engine · failedENGINE FAILED ON TAKE OFF.SDR MASA00030Light · inoperativeFLT 6241 - MTJ-PHX - DURING PREFLIGHT CHECK, THE CREW REPORTED THAT ONE UNDER DASH EMERGENCY LIGHT WAS INOPERATIVE. MAINTENANCE INSPECTED AND THIS ITEM WAS DEFERRED PER MEL NR 3302. THE AIRCRAFT CONTINUED SERVICE. (M)SDR 20000331SH012Altimeter · malfunctionedPILOT WRITE UP WAS ''STICKS SEVERAL THOUSAND FEET'', CALIBRATION WAS OUT AT -1,000 AND ZERO FEET AND 500 FEET, ENCODER FUNCTIONS PROPERLY, COULD NOT VERIFY OR DUPLICATE STICKING. ALTIMETER WAS 40 FEET LOW AT -1,000 FEET AND PROGRESSIVELY GOT BETER. AT +1,000SDR CA000301033Pump · worn(CAN) THERMOSTATIC VALVE FOUND TO BE MALFUNCTIONING WHICH CAUSED EXCESS HEAT IN OIL. THIS CAUSED POOR SCAVENGE FROM AGB AND INITIATED A STATIC LEAK THROUGH NR 1 BEARING LAB SEAL. PWC TERMED BLACK OIL SYNDROME .SDR S2YA00003Altimeter · failedFLT 1071 - EN ROUTE MKE-CWA - THE CAPTAINS ALTIMETER FLAGGED AND ALERTER WENT BLANK. AFTER TALKING WITH MAINTENANCE AND OPERATIONS THE DECISION WAS MADE TO RETURN TO MKE WHERE MAINTENANCE COULD WORK THE PROBLEM. MAINTENANCE REPLACED THE CAPTAINS ALTIMETER. SDR 20000424SH002Gyro · inoperativeNR 1 GYRO SLOW TO SPOOL AND STUCK ON ZERO DEGREES (NORTH). (X)SDR C2XA00CL027Engine · failedLAN - FLT 3126 - THE CREW REPORTED DURING TAKEOFF ROLL, THE LEFT ENGINE LOST TORQUE AND EXCEEDED 900 DEGREES ITT. THE AIRCRAFT ABORTED THE TAKEOFF AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE IAW CONTINESDR 20000331SH013Gyro · inoperativeCAPTAIN''S DIRECTIONAL GYRO INOPERATIVE. NR 1 GYRO LOCKED UP. (X)SDR S2YA00002Actuator · inoperativeFLT 1123 - YYZ-GRR - CREW SELECTED GEAR DOWN BUT DID NOT GET THE NOSE DOWN AND LOCK INDICATION. THE CREW MADE SEVERAL ATTEMPTS TO GET THE NOSE DOWN AND LOCKED INDICATION. THE CREW NOT GET THREE GREEN SO EMERGENCY WAS DECLARED AND LANDED WITHOUT INCIDENT. OUSDR 20000405AP006Governor · will not testRIGHT OVERSPEED GOV WILL NOT GROUND TEST. REPLACED DEFECTIVE GOVERNOR, SYSTEM AND UNIT. CHECKS SATISFACTORY IAW CHAPTER 61. (M)SDR C2XA00IA041Handle · inoperativeTYR-IAH - FLT 3741 - THE CREW REPORTED THAT THE LANDING GEAR WOULD NOT RETRACT WITHOUT CYCLING THE CONTROL HANDLE. THE AIRCRAFT LANDED AT IAH WITHOUT INCIDENT WHERE MAINTENANCE INSPECTED THE AIRCRAFT AND PERFORMED OPERATIONAL CHECKS OF THE GEAR SYSTEM IAW B19SDR CA000306029Switch · stuck(CAN) DURING UNSCHED MAINT ON FLAP RIGGING, LT INBOARD FLAP ACTUATOR DRIVE WAS DISCONNECTED AT FLAP ATTACH. FLAPS WERE FULLY DOWN (35 DEGREES). FLAP SELECTED FROM DOWN TO 17 DEGREES AND FLAPS TRAVELLED TO 17 DEGREES. THE LT SPLIT FLAP SWITCH ACTUATOR HAD MOSDR MASA00024Cable · out of adjFLT 5299 - IAD-SYR - DURING STANDARD PREFLIGHT INSPECTION, THE CREW NOTED THEY HAD A BINDING AT THE PAX DOOR. THE AIRCRAFT WAS FERRIED TO RDG AND MAINTENANCE FOUND THE COUNTER CABLE TO BE SHORT. MAINTENANCE THEN ADJUSTED THE COUNTER BALANCE CABLE, OPS CHECKESDR CA000306001Control Cable · frayed(CAN) DURING ROUTINE INSPECTION MAINTENANCE FOUND THE AILERON CABLE WAS FRAYED BEYOND LIMITS. LOCATION WAS ON FIRST PULLEY BELOW CONTROL YOKE IN COCKPIT PEDESTAL. ACCESS IS FROM BELLY PANEL IMMEDIATELY BEHIND NLG WHEELWELL.SDR C2XA00CL025Altimeter · failedCLE - FLT 3094 - AFTER TAKEOFF FROM CLEVELAND, THE CREW REPORTED THE CAPTAINS ALTIMETER FAILED IN FLIGHT. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE CAPTAINS ALTIMETER IAW BEECHCRAFT MM 34-12-04, AND OPESDR GLBA2001036Engine · out of rigUNSCHEDULED LANDING - RIGHT ENGINE POWER LEVER LIMITED ON TORQUE. RIGGED RIGHT ENGINE, OPS CHECKED GOOD.SDR MASA00016Control Cable · out of adjFLT 6540 - PHX-CLD - AFTER TAKEOFF, THE CREW NOTED THE NR 1 ENGINE FAILED AND THE TORQUE WENT TO ZERO. THE PROP AUTOFEATHERED AND THE CREW COMPLIED WITH THE CHECKLIST AND MANUALLY SHUTDOWN THE ENGINE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO PHSDR 2000ZZZX613Altimeter · reads highENCODER READS 200 FEET HIGH. PROBLEM VERIFIED ON BENCH. (X)SDR 2000ZZZX612Altimeter · inoperativeALTIMETER FLAGGED AT 4,200 FEET AND REMAINED INOPERABLE. VERIFIED ON BENCH. (X)SDR 2000ZZZX611Altimeter · inoperativeENCODER INOPERATIVE. (X)SDR 20000329SH008Seal · deterioratedNEW STYLE SEAL APPEARS TO HAVE DETERIORATED AFTER 672.4 HOURS OF SERVICE. RETURNED PARTS TO FACTORY FOR EVALUATION. (X)SDR C2XA00CL015Trim Tab · malfunctionedCLE - FLT 3036 - AFTER TAKEOFF FROM CLEVELAND, THE CREW REPORTED THEIR ELEVATOR PITCH TRIM WHEEL WAS DIFFICULT TO OPERATE. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPOSITIONED ELEVATOR TRIM TAB CONTROL WHEEL ANDSDR C2XA00CL013Connector · looseCLE - FLT 3009 - THE CREW REPORTED CAPTAINS ALTIMETER FAILED IN FLIGHT. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE RESET CANNON PLUG ON BACK OF CAPTAINS ALTIMETER. PERFORMED OPERATIONAL CHECKS IAW BEECH MM 34-12-04. THE AIRCRASDR 2000ZZZM222Indicator · shortedSMOKE SMELL IN COCKPIT, NOTICED DURING LANDING. TERMINALS ON PROP AMP GAUGE ARCED. REPLACED PROP AMP GAUGE, OPERATIONAL CHECKED GOOD. (M)SDR CA000209069Bearing · disintegrated(CAN) UNKNOWN TO THE AIRCREW, THE AIRCRAFT LOST ITS RT INBOARD WHEEL FOLLOWING TAKEOFF. PILOT DISCOVERED AT DESTINATION WHEEL MISSING WITH THE INNER BEARING, TANG WASHER, NUT AND COTTER PIN REMAINING.THE AXLE SHOWED MINOR SCORING MARKS AND THE BRAKE UNIT WAS ISDR CA000209068Switch · stuck(CAN) THE AIRCRAFT LOST ALL COMMUNICATIONS FOR A PERIOD OF 20 MINUTES. A PUSH-TO-TALK SWITCH ON THE RT CONTROL COLUMN WAS FOUND STUCK IN THE TRANSMIT POSITION BLOCKING ALL TRANSMIT & RECIEVE COMMUNICATIONS. SWITCH REPLACED. SUBMITTER STATES THIS HAS BEEN A RECSDR 047254Elevator · roughWHILE ON FLIGHT 2629 DEPARTING, THE CREW PERFORMED AN ELEVATOR CHECK. THEY FELT ROUGHNESS IN THE ELEVATOR SYSTEM. THE CREW RETURNED TO THE GATE. MAINTENANCE PERFORMED AN INSPECTION AND NO DEFECTS WERE NOTICED. NO PARTS WERE USED. TEARDOWN REPORT WILL BE NOT BESDR C2XA00CL011Switch · failedAZO - FLT 3010 - AFTER TAKEOFF FROM AZO, LANDING GEAR WOULD NOT RETRACT. RETURNED TO AZO AND LANDED WITHOUT INCIDENT. MAINTENANCE ACCOMPLISHED SEVERAL UP AND DOWN CYCLES WITHOUT FAILURE. APPLIED REFRIGERANT TO RIGHT LANDING GEAR SQUAT SWITCH AND THE GEAR DIDSDR C2XA00CL010Mlg · malfunctionedAZO - FLT 3010 - AFTER TAKEOFF FROM AZO, LANDING GEAR WOULD NOT RETRACT. RETURNED TO AZO AND LANDED WITHOUT INCIDENT. MAINTENANCE ACCOMPLISHED SEVERAL UP AND DOWN CYCLES WITHOUT FAILURE, SIMULATING AIRLOAD AND VIBRATION ON WIRING. SYSTEM OPS CHECKED GOOD IAWSDR MASA00006Gas Generator · overtempFMN - DURING FLIGHT OUT OF FARMINGTON, THE CREW NOTED THE LEFT ENGINE INDICATION ITT WENT TO FULL HOT. THE ENGINE SHUT DOWN AND THE AIRCRAFT RETURNED TO FARMINGTON. MAINTENANCE INSPECTED AND REMOVED AND REPLACED THE LEFT ENGINE GAS GENERATOR. OPS CHECKED GOSDR C2XA00CL009Mlg · malfunctionedCLE - FLT 3027 - AFTER TAKEOFF FROM PIT, LANDING GEAR FAILED TO RETRACT INITIALLY. AFTER 30-60 SECONDS, GEAR CAME UP. CONTINUED ON TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE CYCLED GEAR SEVERAL TIMES IAW BEECH 1900D MM CHAP 32-30-00. SYSTEM OPS CHECKEDSDR CA000120019Motor · shorted(CAN) DURING GEAR DOWN SELECTION THE FLIGHT CREW DID NOT OBSERVE THE LANDING GEAR ATTEMPT TO REPOSITION AND OPEN THE C/B. NORMAL RESET PROCEDURES FOLLOWED WITHOUT SUCCESSFUL EXTENSION OF THE LANDING GEAR. THE LANDING GEAR WAS MANUALLY SELECTED DOWN. MAINTENANSDR CA000201025Switch · frozen(CAN) ON APPROACH THE CREW SELECTED LANDING FLAPS. THE FLAPS EXTENDED TO LANDING POSITION (35 DEGREES), BUT THE RIGHT INBOARD FLAP PANEL STAYED RETRACTED. MAINTENANCE FOUND THE RIGHT INBOARD FLEX DRIVE CABLE SWAGED END HAD SLIPPED ON THE CABLE END, ALLOWING THSDR CA000128028Wire · worn(CAN) ALL 3 LANDING LIGHTS FAILED TO ILLUMINATE WITH GEAR DOWN. MAINTENANCE FOUND LANDING GEAR WIRE HARNESS CHAFFED THROUGH BY STIFFENER. STIFFENER IS PART OF UPPER AFT SKIN OF LT NACELLE. THERE WAS NO PROTECTION ON THE STIFFENER.SDR AU000128028Wire · worn(AU) ALL 3 LANDING LIGHTS FAILED TO ILLUMINATE WITH GEAR DOWN. MAINTENANCE FOUND LANDING GEAR WIRE HARNESS CHAFED THROUGH BY STIFFENER (P/N 980033-21). STIFFENER IS PART OF UPPER AFT SKIN OF LT NACELLE. THERE WAS NO PROTECTION ON THE STIFFENER.SDR CA000128061Drive Shaft · corroded(CAN) THE PILOT FOUND THE FLAP DOWN TO 17 DEGREES BUT THEY JAMMED AT 8 DEGREES. WE FOUND THE LT INBOARD FLAP FLEX DRIVE BROKEN APPROXIMATELY 4 FROM THE END. SHAFT REPLACED.SDR CA000128013Actuator · failed(CAN) ON APPROACH THE CREW SELECTED GEAR DOWN.THE NOSE LANDING ACTUATOR ANNUNCIATOR DID NOT ILLUMINATE. THE INTRANSIT LIGHT WAS NOT ILLUMINATED. DURING TOWING TO THE HANGAR THE LIGHT CAME ON. THE GEAR WAS SWUNG NUMEROUS TIMES WITHOUT FAULT. THE ACTUATOR COSDR AU000128061Flex Drive · broken(AU) THE PILOT FOUND THE FLAP DOWN TO 17 DEGREES, BUT THEY JAMMED AT 8 DEGREES. FOUND THE LT INBOARD FLAP FLEX DRIVE BROKEN APPROXIMATELY 4 INCHES FROM THE END. SHAFT REPLACED.SDR AU000128013Actuator · failed(AU) ON APPROACH, THE CREW SELECTED GEAR DOWN.THE NOSE LANDING ACTUATOR ANNUNCIATOR DID NOT ILLUMINATE. THE INTRANSIT LIGHT WAS NOT ILLUMINATED. DURING TOWING TO THE HANGAR THE LIGHT CAME ON. THE GEAR WAS SWUNG NUMEROUS TIMES WITHOUT FAULT. THE ACTUATOR C
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