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 AMWA92Plate · chafedDURING AN ABC STRUCTURAL INSPECTION, THE LEFT AND RIGHT PRESSURE PLATES HAD EVIDENCE OF RIVET CHAFE.SDR AMWA90Seat Track · crackedDURING AN ABC STRUCTURAL INSPECTION, THE FORWARD SEAT TRACK WAS FOUND TO BE CRACKED.SDR CA031223001Control Panel · odor(CAN) ON FINAL APPROACH THE CREW SMELLED A STRANGE ODOR IN COCKPIT. INVESTIGATION BY MAINTENANCE REVEALED THAT THE ODOR CAME FROM NR 1 FLIGHT CONTROL PANEL. IT WAS REPLACED ALONG WITH THE NR 1 FLIGHT COMPUTER WITH NO FURTHER REOCCURRENCES. BOTH UNITS WHERE FSDR AMWA89Firewall · crackedFOUND LEFT ENGINE FIREWALL CRACKED. REPAIRED CRACK IN FIREWALL IN ACCORDANCE WITH SRM 54-90-01 BY INSTALLING DOUBLER.SDR 344031Bulb · burnedLANDING GEAR INDICATION LIGHT NOT WORKING. REMOVED AND REPLACED LIGHT BULBS, OP CHECKED GOOD.SDR 8394094Bolt · bentDURING DETAIL NR 6 INSPECTION FOUND RUDDER CONTROL HORN MOUNT BOLT BENT AND TORQUE TUBE MOUNT BOLTS LOOSE.SDR CA040103004Brushes · worn(CAN) DURING ROUTINE BRUSH INSPECTION, MAINTENANCE FOUND STARTER GEN BRUSHES BELOW MINIMUM LIMITS. STARTER GEN REPLACED. NORMAL BRUSH LIFE 2200 HRS STARTER GEN OH 1500 HRS. BRUSHES ALWAYS REPLACED AT OH.SDR CA040103002Brushes · worn(CAN) COULD NOT GET LT GENERATOR ON LINE. MAINTENANCE REPLACED STARTER GENERATOR BRUSH INSPECTION ON REMOVED UNIT SHOWED EXCESSIVE WEAR. ONLY 755.9 HRS SINCE NEW. STARTER GEN OH 1500 HRS. BRUSH INSP EVERY 400 HRS. NORMAL BRUSH LIFE 2200 HRS BUT ALWAYS REPLACESDR AMWA88Rivet · looseLEFT WHEEL WELL GRAVEL FENDER INBOARD UPPER ATTACH POINT AT KEEL HAS LOOSE RIVETS CAUSING WEAR ON KEEL BEAM. REPAIRED BY INSTALLING DOUBLER ON KEEL BEAM USING ADHESIVE AND HUCK BOLT FASTENERS IN ACCORDANCE WITH ENGINEERING REPORT 4849-3.SDR GLBA20030514Wire · chafedWHEN TURNING ON TAXI LIGHT THERE WAS SPARK AND SMOKE, REPAIRED CHAFED WIRE REF 33-40-00. OPS CK GOOD.SDR 2004F00048Spar · crackedAT SCHEDULED EMPENNAGE ZONE INSPECTION, FOUR CRACKS FOUND RADIATING FROM PASSAGE HOLE IN FORWARD WEB OF THE HORIZONTAL STABILIZER FORWARD SPAR. STOP DRILLED CRACKS. FABRICATED AND INSTALLED AND EXTERNAL DOUBLER IAW FAA APPROVED DATA CONTAINED IN THE BEECH 19SDR GLBA20030513Fastener · crackedSEVERAL CHERRY MAX RIVET HEADS CRACKED AROUND EMERGENCY EXIT DOOR INNER FRAME SKIN, REMOVED AND REPLACED CRACKED RIVETS STATION R4C 273.75, 288.00, 327.63, 348.25 USED RIVETS PN CR3243-5 AND -3.SDR AMWA56724Powerpack · failedAFTER TAKE OFF FROM PFN TO VPS. LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO FIELD WITH NO FURTHER INCIDENT. PROBLEM WAS POWER PACK, HYDRAULIC. R&R'D POWER PACK/RPRD BROKEN WIRE OPS OK P/N 1143880001-3 S/N MX607544SDR CA031205014Pump · leaking(CAN) CREW NOTED THAT FUEL WAS LEAKING FROM THE RT ENGINE COWL. MAINTENANCE FOUND THAT THE LOW PRESSURE FUEL PUMP HAD BLOWN OUT THE GASKET BETWEEN THE MAIN BODY AND THE REGULATOR ASSEMBLY ALLOWING FUEL UNDER PRESSURE TO ESCAPE. THE PUMP WAS REPLACED AND THE ASDR 56696Latch · brokenUPON ARRIVAL CREW HAD DOOR WARNING ANNUNCIATOR. IT WOULD NOT EXTUNGUISH. MAINT WAS CALLED AND FOUND LATCH CABLE BROKEN. CABIN DOOR INOPERATIVE CAMS ON AFT SIDE WILL NOT CLOSE. REMOVED AND REPLACED AFT DOOR LATCH CABLE. P/N 129-514059-25SDR GLBA20030508Tube · failedLT BLEED AIR FAILED, REMOVED AND REPLACED BLEED TUBE PN 129-910033-15.SDR 56653Handle · stuckWHEN LANDING GEAR WAS PLACED IN DOWN POSITION LANDING GEAR FAILED TO EXTEND GEAR MANUALLY PUMPED DOWN IND THREE GREENS ACFT LANDED WITH NO FURTHER INCIDENT...CAUSE OF PROBLEM WAS CONTROL, LANDING GEAR HANDLE. WE HAVE RR LDG GEAR SELECTOR HANDLE. P/N 101384137SDR GLBA20030507Switch · malfunctionedALL WARNING ANNUNCIATORS ILLUMINATED, CLEANED PRESS TO TEST SWITCH PN 3PB1. OPS CK GOOD.SDR GLBA20030506Tube · failedLT BLEED FAIL, REPAIRED EVA TUBING PN 131823E6M02060.SDR S2YA03034Guide · failedFLT 1655 - GRB-CWA - DURING FLIGHT, THE CREW SELECTED 17 DEGREES OF FLAPS BUT TH FLAPS CONTINUED TO 35 DEGREES. MAINTENANCE INSPECTED THE FLAP SYSTEM WHICH OPERATED NORMALLY AND FOUND FLAP SWITCH PANELS DETENTS TO BE WORN. MAINTENANCE REPLACED THE PANEL AND SDR GLBA2003160Indicator · slowFO'S AIRSPEED IND SLOW, TURNED PITOT HEAT ON FOR LONGER PERIOD OPS CK GOOD PN 130-380005-7SDR AMWA87Rib · crackedDURING THE D-6 INSPECTION THERE WAS TWO CRACKS FOUND ON THE RIB ON RT SIDE AT STRINGER. CRACK LOCATED AT END OF RIVET ON JOGGLE OVER STRINGER. RIB NR 3 FROM TOP. REPAIRED CRACKS IAW BMM. P/N 101-640000-25, 39.289SDR AMWA86Rib · crackedDURING THE D-6 INSPECTION THERE WERE TWO CRACKS FOUND AT THE LOWER RT SIDE VERTICAL RIB ON JOGGLE THROUGH RIVET HOLE. REPAIRED CRACKS IAW BMM. P/N 101-640000-21, 54.026SDR AMWA85Rib · crackedDURING THE D-6 INSPECTION. THERE WAS TWO CRACKS FOUND AT THE UPPER RIB LT AT BOTH SLOTS FOR STRINGER. REPAIRED CRACKS IAW BMM. P/N 101-640000-17,69.184SDR GLBA2003158Motor · failedFLAPS WILL NOT RETRACT, REPLACED SWITCH PN 27RW82255518T AND FLAP MOTOR PN 100-384040. OPS CK GOOD.SDR GUU2004F00008Bracket · corrodedAT SCHEDULED ROUTINE MAINTENANCE, RT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED RT OB ELEVATOR HINGE BRACKET.SDR GUU2004F00007Bracket · corrodedAT SCHEDULED ROUTINE MAINTENANCE, LT OB ELEVATOR HINGE BRACKET SHOWS SIGNS OF EXFOLIATION. REMOVED AND REPLACED LT OB ELEVATOR HINGE BRACKET.SDR 56473Warning Horn · false activationSTALL WARNING SOUNDED ON TAKE OFF ROLL. THE CREW ABORTED TAKEOFF AND RETURNED TO GATE WITH NO FURTHER INCIDENT. IAW HIGH SPEED TAXI CK/CNDSDR 328031Wheel · lockedAIR RETURN DUE TO MANUAL RUDDER TRIM WHEEL LOCKING UP IN CENTER POSITION, PILOTS RUDDER PEDALS RESPONDED NORMAL.SDR GLBA2003157Indicator · inoperativeNR 1 PROP INDICATOR NEVER WENT ABOVE 1000 ON TAKEOFF ROLL, GROUND RUN OPS CK GOOD.SDR GLBA2003156Indicator · failedFO'S AIRSPEED FAILED TO WORK ON TAKE OFF, REMOVED AND WARMED FO'S AIRSPEED IND PN1303800057 INSTALLED ASI RUN UP ON PITOT STATIC TEST OPS CK GOOD.SDR GLBA2003152Bearing Race · brokenLOOSE BLADES FOUND DURING SCHEDULED INSPECTION, REPLACED PROPELLER ASSEMBLY, TEARDOWN RESULTS FOUND BROKEN LOWER BEARING RACE PN C-792-1B REV (H) SN H123.SDR GLBA2003153Indicator · malfunctionedLT ENGINE ITT EXCEEDED 900C ON ADVANCEMENT OF POWER ON TAKE OFF ROLL, REMOVED AND REPLACED LT ITT GAUGE.SDR GLBA2003151Flap · stuckFLAPS STUCK AT 17 DEGREES. ADJUSTED FLAP SAFETY SWITCH B27RW82255518T OPS CK GOODSDR 2004F00217Turbine Blades · failedFLT 9236 - EYQ/TPA - AFTER CLEARANCE FOR TAKEOFF, LEFT ENGINE FAILED. ENGIEN IMMEDIATELY SECURED. ABORTED TAKEOFF. AIRCRAFT RETURNED TO THE GATE. DEMATED POEWR SECTION FROM GAS GENERATOR AND DETERMINED THAT POWER TURBINE BLADES WERE BROKE OFF AT THE BLADE SDR 2004F00171Blade · failedDURING TAKEOFF, LOUD BANG OCCURRED ON LEFT ENGINE. ABORTED TAKEOFF. DEMATED POEWR SECIOTN FROM GAS GENERTOR AND DETERMINED THAT POWER TURBINE BLADES WERE BROKE OFF. REPLACED LEFT POWER SECTION MODULE AND ROUTED FAILED UNIT FOR FURTHER ANALYSIS AND REPAIR. CSDR 2004F00047Turbine Blades · brokenDURING TAKEOFF, LOUD BANG OCCURRED ON LT ENGINE. ABORTED TAKEOFF. SEPARATED POWER SECTION FROM GAS GENERATOR AND DETERMINED THAT POWER TURBINE BLADES WERE BROKE OFF. REPLACED LEFT POWER SECITON MODULE AND ROUTED FAILED UNIT FOR FURTHER ANALYSIS AND REPAIR. SDR 2004F00046Turbine Blades · failedAFTER CLEARANCE FOR TAKEOFF, LT ENGINE FAILED. ENGINE IMMEDIATELY SECURED. ABORTED TAKEOFF. AIRCRAFT RETURNED TO THE GATE. DEMATED POWER SECTION FROM GAS GENERATOR AND DETERMINED THAT POWER TURBINE BLADES WERE BROKE OFF AT THE BLADE ROOT. POWER SECTION HASDR 56207Line · brokenDURING CRUISE FLIGHT RT ENGINE QUIT. CREW RETURNED TO ABQ AND LANDED WITHOUT ANY INCIDENTS. PASSENGERS DEPLANED AT PRECAUTION WITH NO FURTHER INCIDENTS. REMOVED AND REPLACED P-3 BROKEN LINE. CHANGE IT TO P-3 FILTER. P/N 3123019-01.SDR CA040103003Brushes · worn(CAN) DURING ROUTINE BRUSH CHECK, BRUSHES FOUND BELOW MINIMUM LIMIT. STARTER GEN REPLACED. STARTER GEN O/H 1500 HRS NORMAL BRUSH LIFE 2200 HRS ALWAYS REPLACED AT OH.SDR AMWA84Rib · crackedWHILE PERFORMING AN INSPECTION IN THE VERT STAB., THE RIB FLANGES AT CANTED STAB STA 69.184 WAS FOUND CRACKED IN ONE PLACE ON THE LEFT SIDE AT THE CENTER STRINGER. REPAIRED CRACKS TO RIB FLANGE IAW BMM P/N 114-590021-9, 51-70-03.SDR AMWA83Rib · crackedWHILE PERFORMING AND INSPECTION IN THE VERT. STAB., THE RIB FLANGES AT CANTED STAB STA 54.026 WERE FOUND CRACKED IN FOUR PLACES ON THE LEFT AND TWO PLACES ON THE RIGHT. REPAIRED CRACKS TO RIB FLANGE IAW BMM P/N 114-590021-9, 51-70-03SDR 56120Switch · dirtyDURING LANDING APPROACH MAIN LANDING GEARS FAILED TO EXTEND. THE CREW MANUALLY PUMPED DOWN THE GEARS. RECEIVED 3 GREEN INDICATIONS, LANDED WITH NO FURTHER INCIDENTS. CLEANED CONTACT ON SERVICE VALVE SWITCH.SDR GLBA2003148Relay · stuckFLAPS STUCK AT 17 DEG, REMOVED AND REPLACED FLAP RELAY PN SM50D7. OPS CHECKS GOOD.SDR 56041Autofeather Sys · malfunctionedDURING APPROACH TO LANDING IN PNC. THE RIGHT PROPELLER AUTOFEATHER SYS CYCLED THE PROP IN AND OUT OF FEATHER SEVERAL TIMES. WHILE THE ENGINE CONTINUED TO PRODUCE POWER.SDR CA031110003Engine · leaking(CAN) DURING APPROACH AND LANDING, CREW NOTED BURNING ODOR AND LIGHT SMOKE IN CABIN. LAVATORY SMOKE DETECTOR TRIPPED AND RIGHT ENGINE OIL PRESSURE BEGAN TO DROP. LANDING AND ROLL WAS COMPLETED SO THE EGNINE WAS SECURED AT THE GATE. SEVERAL QUARTS OF OIL WERE ESDR 55918Uplock Switch · malfunctionedCREW REPORTED WITH LANDING GEAR RAISED INTRANSIT LIGHTS REMAINED ILLUM. CREW DECLARED AN EMERGENCY, AND RETURNED TO FIELD WITH NO FURTHER INCIDENTS. ACFT FERRIED TO DUJ FOR MAINTENANCE. GEAR INTRANSIT LIGHT W/N EXTINGUISH WHEN UP. REMOVED AND REPLACED RT GESDR 55959Computer · malfunctionedSTALL WARNING SYS WON`T GIVE WARNING AT 84-90 KNOTS. DURING TAKEOFF ROLL STALL WARNING HORN SOUNDED. CREW ABORTED TAKEOFF AND RETURNED TO GATE. REMOVED AND REPLACED STALL WARNING COMP. P/N 1143800515, S/N 285.SDR GLBA2003145Radome · bird strikeBIRD STRIKE, DAMAGED RT I/B WING, RT O/B WING AND RADOME. REPLACED LT INBD LEADING EDGE PN 114-120028-23SDR AMWA73Rib · crackedWHILE PERFORMING AN INSPECTION IN THE VERTICAL STAB, TO THE RIB FLANGES AT CANTED STAB STA 54.026 WERE FOUND CRACKED IN THREE PLACES ON THE LEFT AND THREE PLACES ON THE RIGHT. REPAIRED CRACKS TO RIB FLANGE IN ACCORDANCE WITH BMM P/N 114-590021-9, 51-70-03.
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