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 2000ZZZX157Altimeter · malfunctionedCAPTAIN'S ALTIMETER HAS INTERMITTENT INVALID ENCODER IN-FLIGHT. REMOVED AND REPLACED ALTIMETER. SUBSEQUENT BENCH TEST VERIFIED THAT ENCODER WAS INTERMITTENTLY INOPERABLE. P/N KEA-346/066-0362-0008. (X)SDR 2000ZZZX158Alimeter · malfunctionedCAPTAIN'S ALTIMETER REPORTED AS INOPERATIVE IN-FLIGHT. REMOVED AND REPLACED ALTIMETER. SUBSEQUENT BENCH TEST RESULTED IN 'NO FAULT FOUND'. P/N KEA-346/066-0362-0008.SDR 2000ZZZX160Directional Gyro · failedCAPTAIN'S RMI FLAGS AND CARD DO NOT TURN. (CAPTAIN'S DG FROZE). REMOVED AND REPLACED NR 1DGS-65. P/N DGS-65/622-6136-002.SDR 99ZZZX4610Actuator · failedPOWER PACK SCREWS BROKE OFF IN-FLIGHT. PILOT COULD NOT LOCK NOSE GEAR. PILOT THEN PROCEEDED TO EXTEND MANUALLY, BUT NOSE GEAR DID NOT LOCK. PROCEEDED TO MAKE A VERY SOFT LANDING AND AIRCRAFT HAD BOTH PROPS CUT OFF. NOSE WHEELWELL DAMAGED, AND ENGINE REMOVSDR MASA99170Gyro · failedFLT 5415 - PHL-LEB - AFTER TAKEOFF FROM BOS, THE CREW NOTED THAT BOTH DIRECTIONAL GYROS WERE DRIFTING AT AN EXTREME RATE. THE CREW NOTIFIED THE TOWER THEY WERE RETURNING TO BOS AND THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REMOVSDR 99ZZZM789Prop Governor · fluctuatingRIGHT PROP RPM AND TORQUE FLUCTUATING. REPLACED RIGHT ENGINE PROP GOVERNOR, REVERSING ARM AND BETA BLOCK. AIRCRAFT TEST FLOWN AND RETURNED TO SERVICE. (M)SDR C2XA99CL119Harness · failedTHE PILOT REPORTED THE RIGHT GEAR NEEDED TO BE CYCLED ONCE TO GET A DOWN AND LOCKED INDICATION LIGHT ON APPROACH. THE AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT DOWN AND LOCKED SQUAT SWITCHES AND HARNESSSDR 2000ZZZX161Directional Gyro · inoperableCAPTAIN'S DIRECTIONAL GYRO INOPERABLE. REMOVED AND REPLACED NR 1 DGS-65 GYRO. P/N DGS-65/622-6136-002. (X)SDR CA991112023Relay · failed(CAN) AFTER THE ENGINE SHUTDOWN , THE RE-FUELER SAW SMOKE COMING OUT FROM ONE OF THE DE-ICER BOOTS ON THE NR TWO PROPELLER. HE ADVISED THE CREW ABOUT THE SITUATION. THE CAPTAIN EXTINGUISHED THE FLAME WHILE THE COPILOT INITIATED THE EMERGENCY PROCEDURE. MAISDR C2XA99IA540Uplock Switch · inoperativeIAH - DURING FLIGHT 3449, THE CREW REPORTED A GEAR UNSAFE LIGHT DURING EXTENSION AND RETRACTION. THE CREW MANUALLY EXTENDED THE LANDING GEAR AND RETURNED TO IAH WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RIGHT MLG UPLOCK SWITCH IAW B1900-D MM 32-SDR 99ZZZM806Turbine · failedRIGHT ENGINE POWER LOSS ON TAKEOFF ROLL PRIOR TO FULL POWER. TAKEOFF ABORTED WITHOUT INCIDENT. LOUD 'BANG' HEARD BY CREW PRIOR TO POWER LOSS. ENGINE WAS REMOVED AND REPLACED AND AIRCRAFT RETURNED TO SERVICE. (M)SDR CA991112022Actuator · failed(CAN) AFTER SELECTING THE GEAR DOWN, THE NOSE GREEN LIGHT INDICATION DID NOT ILLUMINATE AND THE RED GEAR HANDLE INTRANSIT LIGHT ILLUMINATED. THE CREW COMPLETED AN EMERGENCY PROCEDURE AND THE AIRCRAFT LANDED SAFELY. AFTER INVESTIGATION, FOUND THE ACTUATOR TO SDR C2SA99CL117Control Handle · failedTHE PILOT REPORTED, ON FINAL APPROACH DID NOT GET A DOWN AND LOCKED INDICATION FOR THE RIGHT MAIN GEAR. THE AIRCRAFT LANDED IN CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR CONTROL HANDLE IAW BEECHCRAFT MM 32-60-00 ANDSDR 99ZZZM733Brake · leakingNR 2 BRAKE SEEPING HYD FLUID. REPLACED NR 2 BRAKE ASSEMBLY IAW CLEVELAND MAINTENANCE MANUAL. (M)SDR C2XA99CL116Engine · malfunctionedFLT 3173 - THE CREW REPORTED THE RIGHT ENGINE LOST POWER. THE AIRCRAFT RETURNED TO ERI WITHOUT FURTHER INCIDENT. MAINTENANCE RAN THE NR 2 ENGINE, CHECKED ALL ENGINE RIGGING AND PERFORMED ENGINE RUNS. NO DEFECTS WERE NOTED IAW BEECHCRAFT MM 76-10-00. THE AISDR 2000ZZZX162Altimeter · failedCAPTAIN'S ALTIMETER FLAGGED IMMEDIATELY FOLLOWING TAKEOFF. THE SCHEDULED FLIGHT WAS ABORTED AND AIRCRAFT RETURNED TO THE STATION. UPON LANDING, ALTIMETER BEGAN TO FUNCTION. THE ALTIMETER WAS REMOVED AND REPLACED. P/N KEA-346/066-03062-00.SDR 99ZZZM795Altimeter · failedCAPTAINS ALTIMETER REPORTED TO HAVE FLAGGED AND GONE INOPERATIVE. REMOVED AND REPLACED ALTIMETER. SUBSEQUENT BENCH TEST RESULTED IN 'NO FAULT FOUND'. (M)SDR 99ZZZM754Altimeter · malfunctionedCAPTAINS ALTIMETER WAS REPORTED TO BE 100 TO 200 FEET OFF AT ALL ALTITUDES. REMOVED AND REPLACED ALTIMETER. SYSTEM TESTS SATISFACTORY. SUBSEQUENT BENCH TESTS FOUND THAT THE ALTIMETER WAS INDICATING 100 FEET HIGH AND THAT THE MILIBAR INDICATION DID NOT COINCSDR 2000ZZZX159Altimeter · failedCAPTAIN'S ALTIMETER FLAGGED DURING DESCENT. REMOVED AND REPLACED ALTIMETER. SYSTEM TESTS SATISFACTORY. SUBSEQUENT BENCH TESTS WERE UNABLE TO CONFIRM PROBLEM. THIS WAS THE THIRD SUCH FAILURE OF THIS INSTRUMENT IN THE PAST 9 MONTHS (714 HOURS) OF OPERATION. SDR 99ZZZM755Prop Governor · failedRIGHT PROP RPM SURGED TO 1800 RPM AT TAKEOFF SETTING. UNIT REPLACED, GROUND RUN AND TEST FLIGHT PERFORMED. (M)SDR C2XA99CL113Battery · dischargedFLT 3075 - PILOT REPORTED THAT THE BATTERY CHARGE LIGHT WOULD NOT GO OUT. THE AIRCRAFT RETURNED TO CLEVELAND WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE MAIN BATTERY IAW BEECHCRACT 1900D MM 24-32-00. THE AIRCRAFT WAS RELEASED TO SERVICE. SDR C2XA99CL112Warning Light · illuminatedFLT 3213 - PILOT REPORTED, THE AUTOFEATHER OFF AMBER CAUTION ANNUNCIATOR ILLUMINATED ON TAKEOFF ROLL. THE AIRCRAFT ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE RELEASED THE AIRCRAFT IAW MEL 61-3/3 PLACARD NUMBER 116062. THESDR MASA99159Switch · malfunctionedFLT 5347 - BOS-HYA - ON TAXI OUT, THE CREW HEAD A POPPING NOSE COMING FROM THE PEDESTAL. THE RUDDER BOOST YAW DAMP C/B POPPED WHEN THIS HAPPENED AND THIS CAUSED THERE TO BE SPARKS IN THE COCKPIT. THE AIRCRAFT RETURNED TO THE GATE AND MAINTEANCE WAS CALLED OUSDR CA991004028Wire · shorted(CAN) LANDING GEAR 2-AMP CONTROL CIRCUIT BREAKER TRIPPED WHEN GEAR SELECTED DOWN. PROBLEM TRACKED TO WIRE NR G16A22 ABOVE TERMINAL BOARD TB, RUBBING ON AIRFRAME. RUBBED THROUGH INSULATION, CAUSING INTERMITTENT SHORT. WIRE REPAIRED AND AIRFRAME TAPED TO PRESDR 99ZZZM714Efd84 · failedWHILE EN ROUTE CREW EXPERIENCED SMOKE IN THE COCKPIT. EMERGENCY LANDING WAS DECLARED AND LANDED WITHOUT INCIDENT. IT WAS DETERMINED THAT THE NR 2 EHSI, EFD-84, WAS THE CAUSE OF THE SMOKE. THE EFD-84 WAS REMOVED AND REPLACED WITH A SERVICEABLE UNIT AND SYSTESDR AU990966Switch · faulty(AUS) RIGHT ENGINE FIRE EXTINGUISHING SYSTEM FIRE PULL T-HANDLE MICROSWITCH FAULTY. EVIDENCE OF WEAR WAS FOUND ON ONE OF THE MICROSWITCH CONTACT PLATES.SDR AU990965Switch · faulty(AUS) LEFT ENGINE FIRE EXTINGUISHING SYSTEM FIRE PULL T-HANDLE MICROSWITCH PIN 8 TO PIN 9 HAD NO CONTINUITY.SDR 99ZZZX4085Altimeter · malfunctionedCAPTAIN'S ALTIMETER READS 80 FEET - 100 FEET HIGH AT ALL ALTITUDES AND ENCODER TRANSITION POINTS ARE OUT OF TOLERANCE. REMOVED AND REPLACED ALTIMETER. BENCH TEST VERIFIED ALTIMETER TO BE INDICATING 80 FEET HIGH AT 1,500 FEET AND 110 FEET HIGH AT 10,000 FEET. SDR 99ZZZM708Altimeter · failedPILOTS ALTIMETER FLAGGED ON TAKEOFF. REMOVED AND REPLACED ALTIMETER. TESTED OK. (M)SDR CA991007022Rivets · missing(CAN) FIRST STAGE COMPRESSOR DAMAGE FOUND FIELD REPAIR COMPLETED. DATA PLATE RETAINING RIVET FAILURE SUSPECTED BY OPERATOR. NOTE: SUBMITTER STATED P&W ARE REVIEWING HARDWARE ATTACHMENT OF DATA PLATES ON THESE ENGINES. POSSIBLE CHANGES TO COME IN 4TH QUARTSDR CA991007021Rivets · missing(CAN) ITT SPLIT REPORTED. FIRST STAGE COMPRESSOR DAMAGE FOUND BEYOND FIELD REPAIR DATA PLATE RETAINING RIVET FAILURE SUSPECTED BY OPERATOR. NOTE: SUBMITTER STATED P&W ARE REVIEWING HARDWARE ATTACHMENT OF DATA PLATES ON THESE ENGINES POSSIBLE CHANGES TO COMSDR 99ZZZX4086Altimeter · malfunctionedCAPTAIN'S ALTIMETER FLAGGED DURING CRUISE FLIGHT. REMOVED AND REPLACED ALTIMETER. SUBMITTER STATED THIS IS THE SECOND REPORT OF A FLAGGING PROBLEM WITH THIS ALTIMETER IN THE PAST 12 MONTHS. BENCH TEST DID NOT VERIFY THE FAULT. COMP P/N KEA-346/066-03062-00SDR 99ZZZM699Hose · chafedEN ROUTE BETWEEN PLB AND IAD, ON A REPOSITION FLIGHT, LEFT ENGINE OIL PRESSURE BEGAN TO FLUCTUATE. UPON FURTHER OBSERVANCE BY CREW OIL PRESSURE ANNUNCIATOR BEGAN FLASHING, AT WHICK TIME ENGINE WAS SHUT DOWN AND AIRCRAFT DIVERTED TO ABL. LEFT ENGINE OIL LINE SDR 99ZZZM720Altimeter · malfunctionedCAPTAINS ALTIMETER FLAGGED ON DESCENT. REMOVED AND REPLACED ALTIMETER. THIS IS THE FOURTH REPORT OF A FLAGGING PROBLEM WITH THIS ALTIMETER. BENCH TEST DID NOT VERIFY THE FAULT. (M)SDR 99ZZZM778Turbine · failedEN ROUTE BETWEEN ROC AND HPN LEFT ENGINE SUFFERED LOSS OF TORQUE FOLLOWED BY HIGH INTERNAL TURBINE TEMPERATURE INDICATIONS, ENGINE WAS THEN SHUT DOWN IN FLIGHT, AIRCRAFT DIVERTED TO BGM FOR EMERGENCY LANDING. LEFT ENGINE WAS REPLACED IN BGM IAW PRATT AND WHITSDR 99ZZZX3504Fork · crackedFORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. FOUR CRACKS. SUBMITTER STATED RECURRING PROBLEM.SDR 99ZZZX3503Fork · crackedFORWARD EAR OF PITCH CHANGE FORK CRACKED IN INBOARD RADIUS OF PITCH PIN ENGAGEMENT SLOTS. TWO CRACKS.SDR MASA99152Actuator · internal leakFLT 6461 - FMN-PHX - AFTER DEPARTURE, THE CREW REPORTED THE MAIN LANDING GEAR CIRCUIT BREAKER POPPED. THE CREW RESET THE CIRCUIT BREAKER AND IT POPPED AGAIN. THE CREW MANUALLY EXTENDED THE GEAR. THE AIRCRAFT RETURNED TO THE FIELD AND LANDED WITHOUT FURTHER SDR CA991209086Valve · failed(CAN) AS THE CREW WAS ON TAKEOFF ROLL DOWN THE RUNWAY AND THE POWER LEVERS WERE ADVANCED TO FULL POWER, THEY RECEIVED A RT ENVIRONMENTAL FAIL INDICATION LIGHT. THEY REJECTED THE TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE WAS ADVISED AND UPON FURTHER INVSDR C2XA99CL106Indicator · failedCLE - FLT 3129 - THE CREW REPORTED THE RIGHT TQ DID NOT INCREASE OR RISE DURING TAKEOFF, IT WAS STUCK AT 300. THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE RT TQ INDICATOR IAW B1900D MM 77-10-00 OPERATIONAL SDR MASA99149Lock · dirtyFLT 5972 - PIT-DUJ - PRIOR TO DEPARTURE, THE CREW REPORTED THE CABIN DOOR ANNUNCIATOR LIGHT EXTINGUISHED PRIOR TO LOCKING THE DOOR. MAINTENANCE CLEANED AND LUBED THE SHAFT DOOR LOCK, OPS CHECK GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR MASA99148Bracket · jammedFLT 5384 - BOS-PQI - DURING PREPARATION FOR LANDING IN PQI, THE CREW RECEIVED A GEAR UNSAFE INDICATION. THE AIRCRAFT DIVERTED TO BGR WHERE THEY DECLARED AN EMERGENCY. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A BOLT LODGED BETWEEN THE DOWNLOCKSDR MASA99146Engine · deer strikeFLT 6450 - IN DSM, DURING TAKEOFF ROLL, THE AIRCRAFT STRUCK A DEER. THE AIRCRAFT DEPLANED ON THE TAXIWAY. MAINTENANCE FOUND THE RIGHT PROP HAD LOST THREE BLADES. THERE WAS A HOLE IN THE LOWER RIGHT SIDE OF FUSELAGE. THE ENGINE AND NACELLE WERE PUSHED AFT ASDR C2XA99CL099Switch · dirtyMBS-CLE - FLT 3240 - THE CREW REPORTED THE RIGHT GEAR LIGHT 'R AND H' ARE INTERMITTENT. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE CLEANED THE PRESS/RESET PUSHBUTTON, CLEANED ALL THE SWITCHES AND INSPECTED THE WIRING HARNESSES, AND PERFORMED OSDR C2XA99CL098Actuator · failedMDT-CLE - FLT 3131 - THE CREW REPORTED THE 'L' GEAR LIGHT WOULD NOT ILLUMINATE AFTER GEAR EXTENSION UNTIL ON SHORT FINAL, AT ABOUT 500 FT. THE LIGHT ILLUMINATED WITH THE PRESS TO TEST. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. (M)SDR C2XA99CL097Pc Board · failedPIT-CLE - FLT 3037 - THE CREW REPORTED THEY HAD TO CYCLE THE LANDING GEAR THREE TIMES TO GET THE 'L' GREEN LIGHT TO ILLUMINATE. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED PC BOARD A319 AND PERFORMED OPERATIONAL CHECKS IAW SDR MASA99145Disconnect Cam · failedFLT 5482 - BOS-MVY - WHEN PREPARING FOR LANDIN IN MVY, THE CREW REPORTED THEY RECEIVED NO DOWN AND LOCK INDICATION FOR THE NOSE GEAR UPON GEAR EXTENSION. THE CREW RECYCLED THE GEAR BUT THE NOSE GEAR DID NOT EXTEND. THIS WAY CONFIRMED BY THE TOWER. THE CREW SDR C2XA99CL095Duct · looseCLE - FLT 3129 - THE CREW REPORTED THE LEFT FIRE T-HANDLE ILLUMINATED DURING TAXI TO THE RUNWAY, THE LIGHE EXTINGUISHED AFTER PULLING T-HANDLE. THE AIRCRAFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE RESECURED THE NR 1 ENGINE RIGHT INLET DE-ISDR C2XA99CL093Actuator · failedMBS-CLE - FLT 3250 - THE CREW REPORTED THAT WHEN THE GEAR WAS EXTENDED TO THE LEFT MAIN GEAR DOWN LIGHT WAS DELAYED APPROX FIVE SECONDS THEN CAME ON. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT MAIN GEAR ACTUATOR ASDR MASA99144Air Dist · odorFLT 5756 - PHL-STL - ON TAXI INTO STL, THE CAPTAIN REPORTED A FUEL SMELL IN THE COCKPIT WHEN THE ENVIRONMENT WAS ON. (M)
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