Raytheon 1900D

Service difficulty reports · 7,152

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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.

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)Mar 25, 2000 · N249GL · Beech 1900D · Altimeter, Barometric/EncoderSDR 20000508SH028Gyro · failedPILOT WRITE-UP WAS ''HDG WON''T MOVE WITH AIRCRAFT MOVEMENT''. THIS GYRO IS LOCKED UP. (X)Mar 24, 2000 · N184UX · Beech 1900D · Directional Gyro and Indicating SystemSDR 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. Mar 24, 2000 · N122UX · Beech 1900D · Altimeter, Barometric/EncoderSDR 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)Mar 23, 2000 · N831CA · Beech 1900D · Propeller GovernorSDR 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 CLEANINGMar 18, 2000 · N891SK · Beech 1900D · Door Warning SystemSDR 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 FOMar 17, 2000 · N153GL · Beech 1900D · Turbine Engine Oil SystemSDR 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)Mar 15, 2000 · N79SK · Beech 1900D · Flight Compartment WindowsSDR CA000322007Governor · failed(CAN) OVERSPEED GOVERNOR FOUND TO BE CONTROLLING PROP SPEED GOVERNOR, REPLACED.Mar 13, 2000 · Beech 1900D · Propeller GovernorSDR 20000425SH036Gyro · failedPILOT REPORTED THAT ''GYRO FREEZES UP''. NR 1 DIRECTIONAL GYRO REMOVED AND SENT TO TEST FACILITY.Mar 10, 2000 · N179GL · Beech 1900D · Directional Gyro and Indicating SystemSDR 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.Mar 9, 2000 · Beech 1900D · Pneumatic Distribution SystemSDR 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.Mar 7, 2000 · Beech 1900D · Pneumatic Distribution SystemSDR CA000314003Engine · failedENGINE FAILED ON TAKE OFF.Mar 3, 2000 · Beech 1900D · Engine (Turbine/Turboprop)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)Mar 1, 2000 · N105YV · Beech 1900D · Emergency LightingSDR 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 +1,000Mar 1, 2000 · N220GL · Beech 1900D · Altimeter, Barometric/EncoderSDR 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 .Feb 29, 2000 · Beech 1900D · Turbine Engine Oil SystemSDR 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. Feb 28, 2000 · N91SK · Beech 1900D · Altimeter, Barometric/EncoderSDR 20000424SH002Gyro · inoperativeNR 1 GYRO SLOW TO SPOOL AND STUCK ON ZERO DEGREES (NORTH). (X)Feb 28, 2000 · N260GL · Beech 1900D · Directional Gyro and Indicating SystemSDR 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 CONTINEFeb 24, 2000 · N69548 · Beech 1900D · Engine (Turbine/Turboprop)SDR 20000331SH013Gyro · inoperativeCAPTAIN''S DIRECTIONAL GYRO INOPERATIVE. NR 1 GYRO LOCKED UP. (X)Feb 23, 2000 · N245GL · Beech 1900D · Directional Gyro and Indicating SystemSDR 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. OUFeb 22, 2000 · N92SK · Beech 1900D · Landing Gear ActuatorSDR 20000405AP006Governor · will not testRIGHT OVERSPEED GOV WILL NOT GROUND TEST. REPLACED DEFECTIVE GOVERNOR, SYSTEM AND UNIT. CHECKS SATISFACTORY IAW CHAPTER 61. (M)Feb 22, 2000 · N841CA · Beech 1900D · Propeller GovernorSDR 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 B19Feb 20, 2000 · N81538 · Beech 1900D · Landing Gear SelectorSDR 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 MOFeb 19, 2000 · Beech 1900D · Trailing Edge Flap Control SystemSDR 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 CHECKEFeb 18, 2000 · N133YV · Beech 1900D · Entrance StairsSDR 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.Feb 17, 2000 · Beech 1900D · Aileron Control SystemSDR 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 OPEFeb 15, 2000 · N48544 · Beech 1900D · Altimeter, Barometric/EncoderSDR GLBA2001036Engine · out of rigUNSCHEDULED LANDING - RIGHT ENGINE POWER LEVER LIMITED ON TORQUE. RIGGED RIGHT ENGINE, OPS CHECKED GOOD.Feb 13, 2000 · N150UX · Beech 1900D · Power LeverSDR 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 PHFeb 10, 2000 · N3YV · Beech 1900D · Propeller Feathering/ReversingSDR 2000ZZZX613Altimeter · reads highENCODER READS 200 FEET HIGH. PROBLEM VERIFIED ON BENCH. (X)Feb 8, 2000 · N257GL · Beech 1900D · Altimeter, Barometric/EncoderSDR 2000ZZZX612Altimeter · inoperativeALTIMETER FLAGGED AT 4,200 FEET AND REMAINED INOPERABLE. VERIFIED ON BENCH. (X)Feb 8, 2000 · N201YQ · Beech 1900D · Altimeter, Barometric/EncoderSDR 2000ZZZX611Altimeter · inoperativeENCODER INOPERATIVE. (X)Feb 8, 2000 · N254GL · Beech 1900D · Altimeter, Barometric/EncoderSDR 20000329SH008Seal · deterioratedNEW STYLE SEAL APPEARS TO HAVE DETERIORATED AFTER 672.4 HOURS OF SERVICE. RETURNED PARTS TO FACTORY FOR EVALUATION. (X)Feb 7, 2000 · Beech 1900D · Propeller Blade SectionSDR 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 ANDFeb 6, 2000 · N81533 · Beech 1900D · Elevator Tab Control SystemSDR 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 AIRCRAFeb 1, 2000 · N87550 · Beech 1900D · Outside Air Temperature Indicator/SensorSDR 2000ZZZM222Indicator · shortedSMOKE SMELL IN COCKPIT, NOTICED DURING LANDING. TERMINALS ON PROP AMP GAUGE ARCED. REPLACED PROP AMP GAUGE, OPERATIONAL CHECKED GOOD. (M)Jan 31, 2000 · N210UX · Beech 1900D · Instrument PanelSDR 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 IJan 28, 2000 · Beech 1900D · Wheel/Ski/FloatSDR 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 RECJan 28, 2000 · Beech 1900D · Communications SystemSDR 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 BEJan 26, 2000 · N127ZV · Beech 1900D · Elevator Control SystemSDR 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 DIDJan 26, 2000 · N38537 · Beech 1900D · Landing Gear Retraction/Extension SystemSDR 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 IAWJan 26, 2000 · N38537 · Beech 1900D · Main Landing GearSDR 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 GOJan 25, 2000 · N107YV · Beech 1900D · Turbine SectionSDR 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 CHECKEDJan 25, 2000 · N38537 · Beech 1900D · Main Landing GearSDR 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. MAINTENANJan 19, 2000 · Beech 1900D · Hydraulic Pump (Electric/Engine), MainSDR 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 THJan 18, 2000 · Beech 1900D · Trailing Edge Flap Control SystemSDR 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.Jan 17, 2000 · Beech 1900D · Landing Gear System WiringSDR 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.Jan 17, 2000 · Beech 1900D · Landing Gear System WiringSDR 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.Jan 14, 2000 · Beech 1900D · Trailing Edge Flap ActuatorSDR 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 COJan 14, 2000 · Beech 1900D · Landing Gear ActuatorSDR 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.Jan 14, 2000 · Beech 1900D · Trailing Edge Flap Control SystemSDR 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 CJan 14, 2000 · Beech 1900D · Landing Gear Door Actuator
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