N340BE, cancelled Feb 11, 2003

Service difficulty reports · 17

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N340BE' AND deregistration_id = 'N340BE-2003-02-11'
  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 PLGA981111AValve · malfunctionedLGA - FLT 4541 - DURING APPROACH, CREW NOTICED MAIN AND EMERGENCY HYDRAULIC PRESSURE STARTED TO DROP. LANDING GEAR WAS EXTENDED USING EMERGENCY PROCEDURES. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND DUMP VALVE ON MAIN AND EMERGENCY ACCUMULATOR HAD Nov 11, 1998 · N340BE · Saab SF340A · Hydraulic System, MainSDR PLGA981016ASmoke Detector · contaminatedBTV - FLT 4221 - DURING DESCENT INTO BTV, THE CARGO COMPARTMENT SMOKE WARNING LIGHT ILLUMINATED. THE CREW FOLLOWED PROCEDURES AND DISCHARGED THE FIRE EXTINGUISHER BOTTLE. THE WARNING LIGHT EXTINGUISHED. AIRCRAFT CONTINUED TO BTV AND LANDED WITHOUT INCIDENT.Oct 16, 1998 · N340BE · Saab SF340A · Smoke DetectionSDR PLGA980619AHandle · seizedBGR - DURING HEAVY MAINTENANCE INSPECTION, AN OPERATION TEST OF THE PITCH DISCONNECT SYSTEM WAS BEING PERFORMED. DURING THIS TEST THE PITCH DISCONNECT HANDLE WOULD NOT PULL OUT. MAINTENANCE REMOVED AND REPLACED ASSY PER MM. OPERATIONAL CHECK GOOD. (M)Jun 19, 1998 · N340BE · Saab SF340A · Elevator Control SystemSDR PLGA980309ASwitch · failedBOS - FLT 4324 - AFTER TAKEOFF, THE MAIN PASSENGER DOOR WARNING LIGHT ILLUMINATED. AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND DOOR HANDLE SWITCH AND FAILED. SWITCH WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. (M)Mar 9, 1998 · N340BE · Saab SF340A · Door Warning SystemSDR PLGA971208DSpar · crackedBGR - DURING C-CHECK, FOUND LEFT AND RIGHT FLAPS CRACKED IN REAR SPAR AT WS 142. REPAIRED IAW SAAB SRM 57-80-10, PAGES 208-214. (X)Dec 8, 1997 · N340BE · Saab SF340A · Trailing Edge FlapsSDR PLGA971107ABleed Valve · failedBOS - FLT 4383 - ON CLIMB-OUT, THE RIGHT ENGINE ANTI-ICE BLEED VALVE FAIL LIGHT ILLUMINATED. AIRCRAFT RETURNED TO BOS DUE TO WEATHER CONDITIONS. MAINTENANCE REPLACD THE RIGHT ANTI-ICE BLEED VALVE SYSTEM CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE. (M)Nov 7, 1997 · N340BE · Saab SF340A · Engine Anti-Icing SystemSDR PLGA970825ASmoke Deetector · malfunctionedALB - FLT 4706 - WHILE EN ROUTE LGA/SYR, THE CARGO COMPARTMENT SMOKE WARNING ILLUMINATED. CREW FOLLOWED PROCEDURES AND ACTIVATED CARGO FIRE EXTINGUISHER BOTTLE. AIRCRAFT LANDED IN ALB WITHOUT INCIDENT. MAINTENANCE FOUND NO INDICATION OF FIRE OR SMOKE. BOTHAug 25, 1997 · N340BE · Saab SF340A · Smoke DetectionSDR PLGA970514BChip Det Light · illuminatedJFK - FLT 4427 - AFTER TAKEOFF THE RIGHT ENGINE CHIP DETECTOR LIGHT ILLUMINATED THEN EXTINGUISHED. AIRCRAFT RETURNED TO JFK AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED DETECTOR AND FOUND NO SIGNIFICANT MATER. ENGINE GROUND RAN PER GE MANUAL AND PROBLMay 14, 1997 · N340BE · Saab SF340A · Turbine Engine Accessory DriveSDR PLGA970405AT/O Warning · activatedLGA - FLT 4712 - TAKEOFF WAS ABORTED DUE TO CREW RECEIVING CONFIGURATION WARNING. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE RAN ENGINES BUT COULD NOT DUPLICATE PROBLEM. AIRCRAFT WAS RETURNED TO SERVICE. (M)Apr 5, 1997 · N340BE · Saab SF340A · Central WarningSDR PLGA9607312Engine · failedALB - FLT 4693 - EN ROUTE FROM BTV TO LGA, THE RIGHT ENGINE OIL LOW PRESSURE WARNING LIGHT ILLUMINATED. THE RIGHT ENGINE OIL PRESSURE GAUGE READ 10 PSI. THE CREW SHUT DOWN THE ENGINE AND DIVERTED INTO ALB AND LANDED WITHOUT INCIDENT. THE OIL LEVEL WHEN CHECJul 31, 1996 · N340BE · Saab SF340A · Engine (Turbine/Turboprop)SDR PLGA9606191Hyd Pump · failedBOS - FLT 4372 - DURING APPROACH TO BOS, EXPERIENCED FAILURE OF THE HYDRAULIC SYSTEM. THE HYDRAULIC PUMP AND MOTOR ASSEMBLY WERE REPLACED AND THE AIRCRAFT RETURNED TO SERVICE. TEARDOWN OF THE ELECTRIC MOTOR FOUND THE ARMATURE BEARING HAD FAILED. BEARING P/NJun 19, 1996 · N340BE · Saab SF340A · Hydraulic Pump (Electric/Engine), MainSDR PLG5196G1Pump · failedSYR/BOS - FLT 4372 - ON APPROACH, THE HYDRAULIC SYSTEM FAILED TO PRESSURIZE IN BOTH NORMAL AND OVERRIDE MODES. THE CREW HAND PUMPED THE SYSTEM TO MAINTAIN SYSTEM PRESSURE AND LANDED WITHOUT INCIDENT. BOS MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT AND REPLACEMay 1, 1996 · N340BE · Saab SF340A · Hydraulic Pump (Electric/Engine), MainSDR PLG4896G1Agb Driveshaft · brokenBOS/DCA - FLT 4609 - THIS SDR IS TO CLOSE OUT AN OPEN SDR DATED 1-1-96 IN WHICH FLIGHT EXPERIENCED A FLAME-OUT OF THE LEFT ENGINE AND CHIP LIGHT ILLUMINATION. MAINTENANCE WAS DISPATCHED TO THE AIRCRAFT WHICH HAD DIVERTED TO ACY, AND REMOVED AND REPLACED THE EJan 1, 1996 · N340BE · Saab SF340A · Turbine Engine Accessory DriveSDR PLG1296E1Engines · flamed outFLT NR 4609 - BOS-DCA - DURING CRUISE, THE LEFT ENGINE FLAMED OUT AND THE ASSOCIATED CHIP LIGHT ILLUMINATED. THE AIRCRAFT DIVERTED INTO ACY AND LANDED WITHOUT INCIDENT. (M)Jan 1, 1996 · N340BE · Saab SF340A · Engine (Turbine/Turboprop)SDR PLG111795E1Door Warning · illuminatedDURING DEPARTURE FROM BOS, FLT NR 4414, HAD A FORWARD CABIN DOOR WARNING LIGHT ILLUMINATE. THE AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE DOOR WARNING SYSTEM AND FOUND NO FAULT. THE SYSTEM WAS OPS CHECKED AND ALL INDICATNov 16, 1995 · N340BE · Saab SF340A · Door Warning SystemSDR PLGA92795E1Switch · out of adjustFLT NR 4561 - BOS-ACK - DURING CLIMB-OUT, THE MAIN CABIN DOOR HANDLE WARNING LIGHT ILLUMINATED. THE AIRCRAFT RETURNED TO BOS AND LANDED WITHOUT INCIDENT. THE DOOR WAS CONFIRMED LATCHED AND THE DOOR WARNING HANDLE LIGHT WAS DEFERRED PER MEL 57-70-1. AIRCRAFTSep 27, 1995 · N340BE · Saab SF340A · Door Warning SystemSDR PLGA51952Rear Seal · wornJFK - 4308 - THE AC STARTED VIBRATING, THE CREW ISOLATED THE VIBRATION TO THE RT SIDE OF THE AC. SHORTLY AFTER REACHING CRUISE ALTITUDE, THE RT ENG PROP GEARBOX OIL PRESS DROPPED TO 0 PSI. UPON REACHING 0 PSI THE RT PROP RPM DROPPED FROM 1220 TO 1040 RPM THEMay 1, 1995 · N340BE · Saab SF340A · Propeller Hub Section
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