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 8433001Bolt · looseDURING DETAIL NR 6 INSPECTION, FOUND RUDDER TORQUE TUBE TO CONTROL HORN MOUNT BOLTS LOOSE. REPLACED HORN AND HARDWARESDR 2003F00551Rib · crackedAT SCHEDULED EMPANNAGE ZONAL INSPECTION, VERTICAL STABILIZER TOP FORWARD RIB SHOWING CRACK ON RIGHT SIDE. STOPPED DRILLED CRACK. FABRICATED AND INSTALLED DOUBLER REPAIR IAW 1900D STRUCTURAL REPAIR MANUAL, CHAPTER 51-70-05. (M)SDR 2003F00550Spar · crackedAT SCHEDULED EMPANNAGE ZONAL INSPECTION, FOUR CRACKS FOUND RADIATING FROM PASSAGE HOLE IN FORWARD WEB OF THE HORIZONTAL STABILIZER FORWARD SPAR. REMOVED SECTION OF CRACKED SKIN. FABRICATED AND INSTALLED SHIM AND DOUBLER IAW FAA APPROVED DATA CONTAINED IN DERSDR GLBA2003107Annunciator · illuminatedFUEL QTY ANNUNCIATOR ILLUMINATED, PREFORMED OPERATIONAL RUN-UP OF A/C CND TEST OF SYSTEM OK.SDR S2YA03025Fire Loop · inoperativeFLT 1023 - MKE-ATW - DURING APPROACH, THE CREW NOTED THE NR 2 ENGINE T-HANDLE ILLUMINATED. THE CREW FOLLOWED THE QRH AND PULL THE T-HANDLE, SHUTTING DOWN THE RIGHT ENGINE. THE CREW ALSO DISCHARGED THE FIRE BOTTLE AND DECLARED AN EMERGENCY. MAINTENANCE INSPESDR 52531Gas Generator · failedON FLIGHT 702 FROM FARMINGTON NEW MEXICO TO ALBUQUERQUE NEW MEXICO, TAKEOFF WAS NORMAL. AS THEY DID THE INITIAL CLIMBOUT, THE CREW RECEIVED A LOW OIL PRESSURE INDICATION (ANNUNCIATOR). THE LEFT ENGINE OIL PRESSURE GAUGE INDICATED A RAPID AND CONTINUOUS DROP INSDR 52532Switch · out of adjustON FLIGHT 9415 FROM PANAMA CITY FLORIDA TO PENSACOLA FLORIDA, AFTER TAKEOFF FROM PANAMA CITY FLORIDA, THE STALL WARNING WENT OFF AND WOULD NOT SILENCE. THE AIRCRAFT RETURNED TO FIELD WITH NO FURTHER INCIDENT. MAINTENANCE RE-ADJUSTED THE SWITCHES. NO PARTS WSDR 52510Stall Warning · malfunctionedON FLIGHT 700 FROM FARMINGTON NEW MEXICO TO ALBUQUERQUE NEW MEXICO, DURING THE TAKEOFF ROLL STALL WARNING WENT OFF AND WOULD NOT RESET. THE AIRCRAFT WAS RETURNED TO GATE WITH NO FURTHER INCIDENT. THE CREW WAS THEN GIVEN AIRCRAFT 3199Q TO COVER THE LINE. MAISDR GLBA2003106Landing Gear · malfunctionedNOSE WHEEL CHANGED POSITION ABRUPTLY ON TAKEOFF. INSPECTED A/C PERFORMED HIGH SPEED TAXI CND.SDR GLBA2003104Indicator · failedNR 1 TORQUE INDICATOR FAILED. REMOVED AND REPLACED NR 1 TORQUE IND.SDR 52413Engine · malfunctionedON FLIGHT 5496, THE AIRCRAFT UPON REACHING CRUISE ALTITUDE NOTED LT ENGINE TORQUE HAD INCREASED ABOVE LIMITATIONS (4500 TO 4600 LBS FOR ABOUT 10 SECONDS). THE CREW THEN EXECUTED A PRECAUTIONARY SHUT OFF OF LEFT ENGINE AND RETURNED TO FIELD. THEY LANDED SAFELSDR GLBA2003103Screen · dirtyCABIN WILL NOT PRESSURIZE. CLEANED PRESSURE CONTROLLER INLET SCREEN, OPS CHECK GOOD.SDR GLBA2003102Relay · failedLANDING GEAR HAD TO BE MANUALLY EXTENDED. REPLACED K3 RELAY, OPS CHECK GOOD.SDR 52268Indicator · inoperativeUPON ARRIVAL, ON FLIGHT 700, THE LANDING GEAR HANDLE DOWN, NO GREEN INICATORS ON. THE RIGHT MAIN MANUAL EXTENSION WAS PERFORMED. FLYBY TOWER CONFIRMED GEAR APPEARED DOWN. THE AIRCRAFT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE GEAR DSDR 52223Engine · damagedON FLIGHT 6848, ON POWER UP FOR TAKEOFF THE LT ENGINE BEGAN TO SHAKE AND MAKE NOISES. THE CREW SHUT THE ENGINE DOWN AND RETURNED TO GATE WITH NO FURTHER INCIDENT. UPON RETURN TO GATE, MAINTENANCE INSPECTED THE LEFT ENGINE. THE PROP WOULD NOT TURN AND DAMAGE WASDR GLBA2003101Link · stuckFLAPS STUCK AT 17 DEG, R&R RT FLAP SAFETY LINK OPS CHECKED GOOD.SDR GLBA2003100Display · inoperativeFO EHSI WENT BLANK, REMOVED AND REPLACED FO LOWER EFIS DISPLAY. OPS CHECKED GOOD.SDR 2003FA0000814Control Cable · brokenDURING A GROUND OPERATIONAL CHECK, THE ELEVATOR TRIM CABLE BROKE. THE PART HAD 7208.0 FLIGHT HOURS AND COMPLIED WITH AD 2003-03-18 AND SAFETY COMMUNIQUE NR 216 ON 02/17/03.SDR GLBA2003099Fire Loop · malfunctionedNR 1 FIRE HANDLE ILLUM IN FLIGHT. REMOVED AND REPLACED FWD FIRE LOOP.SDR GLBA2003098Wire · damagedGEAR WOULD NOT RETRACT. REPAIRED WIRING FROM P522 TO J168, OPS CK GOOD.SDR GLBA2003097Actuator · malfunctionedRIGHT ENG WILL NOT MAKE T/O POWER. REMOVED AND REPLACED RT ENG ACTUATOR.SDR 52055Brake Assy · contaminatedTHE RIGHT BRAKES GO FLAT WHEN PRESSURE WAS APPLIED. MAINTENANCE BLED THE BRAKES. NO PARTS WERE USED, THEREFORE NO TEARDOWN REPORT WILL BE REQUIRED.SDR GLBA2003096Powerpack · malfunctionedGEAR WOULD NOT RETRACT. REMOVED AND REPLACED LANDING GEAR HANDLE & POWER PACK.SDR 52034Uplock Switch · faultyDURING THE APPROACH ON FLIGHT 5493 FROM PHILADELPHIA PENNSYLVANIA TO ITHICA NEW YORK, THE GEAR WOULD NOT EXTEND NORMALLY. THE CREW USED THE MANUAL EXTENSION WITH (3GREEN) INICATIONS. LANDING NORMAL WITH NO FURTHER INCIDENT. THE PASSENGERS WERE DEPLANED ON TSDR 52034AMWA2Valve · failedDURING THE APPROACH ON FLIGHT 5493 FROM PHILADELPHIA PENNSYLVANIA TO ITHICA NEW YORK, THE GEAR WOULD NOT EXTEND NORMALLY. THE CREW USED THE MANUAL EXTENSION WITH (3 GREEN) INDICATIONS. LANDED NORMALLY WITH NO FURTHER INCIDENT. THE PASSENGERS WERE DEPLANED OSDR GLBA2003095Tube · damagedRIGHT BLEED AIR FAIL. REPAIRED SPLIT EVA TUBING, OPS CK GOOD.SDR GLBA2003094Rib · crackedMAINTENANCE INSPECTION FOUND LT INBOARD KEEL RIB CRACK .625 INCH LONG. PENDING CORRECTIVE ACTION.SDR 2003F00528Control Head · burnedFLT 9158 - NAS - AFTER TAKEOFF, SMOKE IN COCKPIT FROM TRANSPONDER FACE PANEL. RETURNED TO NAS. LANDED WITHOUT INCIDENT. FOUND TRANSPONDER CONTROL HEAD BURNED INTERNALLY. REMOVED AND REPLACED CONTROL HEAD. NO DEFECTS NOTED. (M)SDR 51894Control Rod · out of positionON FLIGHT 5445 FROM PANAMA CITY FLORIDA TO TAMPA FLORIDA, DURING TAKEOFF ROLL THE RIGHT POWER LEVER WAS STUCK. THE AIRCRAFT DID NOT MAKE TAKEOFF TORQUE. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO GATE WITH NO FURTHER INCIDENT. MAINTENANCE REPOSITISDR 51904Lead · looseON FLIGHT 5517, DURING THE FLIGHT THE RIGHT ENGINE ITT WENT TO 1000 DEGREES CELSIUS THEN WENT BACK TO NORMAL. SHORTLY THERE AFTER THE ITT AGAIN WENT TO 1000 DEGREES CELSIUS AND STAYED THERE. THE CREW REDUCED POWER ON THE RIGHT ENGINE AND RETURNED TO AIRPORT WISDR GLBA2003092Controller · malfunctionedRIGHT ENVIRO FAIL ANNUNCIATOR ILLUMINATED. REMOVED AND REPLACED A317 PCB, OPS CHECK GOOD.SDR GLBA2003091Switch · out of adjustFLAPS INOPERATIVE. CND ADJUSTED RIGHT FLAP SPLIT SWITCH.SDR 2003F00527Engine · failedFLT 9214 - MIA - DURING TAKEOFF JUST AFTER BRAKE RELEASE, AN EXPLOSION WAS HEARD IN THE LEFT ENGINE. ABORTED TAKEOFF. REMOVED LEFT ENGINE. DETERMINED POEWR SECTION HAS MAJOR INTERNAL DAMAGE. REPLCED LEFT ENGINE. ROUTED FAILED ENGINE FOR FURTHER ANALYSIS ANSDR GUU2003F00007Blade · failedDURING TAKEOFF JUST AFTER BRAKE RELEASE, AN EXPLOSION WAS HEARD IN THE LT ENGINE. ABORTED TAKEOFF. REMOVED LEFT ENGINE. DETERMINED POWER SECTION HAS MAJOR INTERNAL DAMAGE. REPLACED LEFT ENGINE. ROUTED FAILED ENGINE FOR FURTHER ANALYSIS AND REPAIR. VENDORSDR GLBA2003090Indicator · inoperativeWEATHER RADAR INOP. OPS CHK WX RADAR, OPS CK GOOD.SDR NSVA20030027Electrical Box · contaminatedSMOKE REPORTED COMING OUT OF CIRCUIT BREAKER PANEL RT SIDE. REMOVED PANEL AND FOUND WATER IN THE AREA. CLEANED OFF WATER AND INSPECTED AREA FOR SIGNS OF DAMAGE AND OVERHEATING, FOUND SATISFACTORY.SDR 8564188Fitting · leakingLANDING GEAR WOULD NOT EXTEND ELECTRICALLY. LANDING GEAR WAS EXTENDED USING HAND PUMP. UPON INSPECTION, MAINTENANCE DISCOVERED FLUID LEAKING FROM THE SWAGE FITTING ON THE LT MAIN LANDING GEAR RETRACT ACTUATOR HOSE. SUSPECT CAUSE WAS FLEX FATIGUE. MAINTENANCE PSDR GLBA2003089Skin · crackedCRACK IN BELLY SKIN NEAR COMM ANT. REPAIRED SKIN IAW BEECH SRM.SDR GLBA2003088Skin · crackedCRACK IN BELLY SKIN NEAR COMM ANT. REPAIRED CRACK IAW BEECH SRM.SDR GLBA2003087Skin · crackedCRACK IN BELLY SKIN NEAR COMM ANT. REPAIRED CRACK IAW BEECH SRM.SDR GLBA2003086Odor · detectedSMOKE ODOR IN CABIN. INSPECTED A/C, NO DISCREPANCIES NOTED. OPERATIONAL CK FLIGHT SATISFACTORY.SDR GLBA2003085Transducer · malfunctionedRUDDER PEDALS STIFF WHEN POWER ADDED. REMOVED AND REPLACED RT RUDDER BOOST TRANSDUCER, OPS CK GOOD WITH DEAD WEIGHT TESTER.SDR GLBA2003084Indicator · stuckRIGHT TORQUE INDICATOR STUCK AT 300 LBS. SWAPPED IND SIDE TO SIDE FOR TROUBLESHOOTING PURPOSES, OPS CK GOOD ON GROUND RUN.SDR GLBA2003083Switch · dirtyFLAPS WOULD NOT RETRACT AFTER T/O. CLEANED SPLIT FLAP SWITCH, OPS CK GOOD.SDR GLBA2003082Oxygen Mask · failedCAPTS O2 MASK HOSE BURST. REPLACED O2 MASK/ HOSE ASSY.SDR 51552Flex Line · defectiveWHILE ON APPROACH ON FLIGHT 5578 INTO PITTSBURGH PENNSYLVANIA, THE GEAR WAS SELECTED DOWN BY NORMAL EXTENSION. WHEN FAILED, THE EMERGENCY EXTENSION WAS PERFORMED WITH GEAR DOWN AND LOCKED. AIRCRAFT LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REMOVED AND RESDR 51492Connector · looseTHE AIRCRAFT WAS RUNNING A FIRE LOOP TEST. DURING FLIGHT, THE LEFT FIRE LOOP FAILED THE TEST. THE AIRCRAFT RETURNED WITH NO FURTHER INCIDENT. MAINTENANCE TIGHTENED THE CANNON PLUG ON AFT FIREWALL. THEN, MAINTENANCE SYSTEM CHECKED IT AND IT WAS FINE. NO PARTS SDR GLBA2003078Switch · inoperativeFLAPS WOULD NOT RETRACT BEYOND 17 DEG. REPLACED THE SPLIT FLAP LINKS ON BOTH SIDES.SDR S2YA03021Switch · out of adjustDURING FLIGHT 1070, THE CABIN DOOR ANNUNCIATOR ILLUMINATED AT 2 POUNDS OF DIFFERENTIAL PRESSURE. THE CREW DID AN AIR TURNBACK. THE SYSTEM WAS PUT ON MEL AND THE AIRCRAFT RETURNED TO SERVICE. ON 06/09 MECHANIC CLEARED THE MEL BY ADJUSTING THE LOWER SILL SWITSDR CA030610009Window · cracked(CAN) DURING A ROUTINE CABIN WINDOW INSPECTION MAINTENANCE FOUND A SMALL CRACK IN WINDOW SURROUND STRUCTURE OF A LT CABIN WINDOW BETWEEN STA 303.25 AND 318.25. THE CRACK MEASURED O.800 INCHES IN LENGTH, PASSED 1/4 INCH PAST A FASTENER, AND WAS 3/4 INCH FROM TH
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