Textron 208B
Service difficulty reports · 1,669
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 = '208B' 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 = '208B' 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 CA120821011Transducer · malfunctioned(CAN) STALL WARNING CONTINUOUSLY SOUNDING WITH NEXT TO NO WIND BLOWING ACROSS IT WHILE ON GROUND. TRANSDUCER REPLACED.SDR RNVA2012022300001Compressor · seizedPILOT REPORTED A STRONG ODOR IN THE COCKPIT. "SMELLED LIKE BURNING FOOD" AND DECLARED AN EMERGENCY, F/O STATED THAT HE FELT HEAT ON HIS SIDE OF ACFT. PILOT STATED HE FELT NO HEAT ON HIS SIDE JUST ODOR. LANDED ACFT AND TAXIED WITHOUT INCIDENT. FOUND THAT SDR HSYA2012022312412Engine · contaminatedPILOT REPORTED DURING TAXI, A STRONG CHEMICAL ODOR IN COCKPIT. TAXIED ACFT BACK TO THE BLOCKS. FREIGHT INSPECTED AND NO DISCREPANCIES FOUND. MX TROUBLESHOT AND FOUND THAT THE APPARENT CAUSE TO BE RESIDUAL RECOVERY WASH FLUID FROM A COMPLETED COMPRESSOR TURSDR CA120223010Brush Block · damaged(CAN) 4 OUT OF THE 8 BRUSHES IN THE STARTER/GENERATOR HAD LOOSE WIRES AND THE LOOSE RIVETS ATTACHING THEM. 3 BRUSHES WERE ON ONE COMMUTATOR AND 1 WAS ON THE OTHER. THE UNIT WAS REPLACED AND SENT FOR O/H. A TEAR-DOWN REPORT WAS REQUESTED AND THE RESULTS WILLSDR MTNA2012F00050Line · crackedRIGHT BRAKE FAILED UPON LANDING, FOUND BRAKE LINE SEPARTED. DEFECTIVE BRAKE LINE WAS REPLACED AND BRAKE SYS OPS CHECKS ACCOMPLISHED IAW MM 32-40-00. ACFT RETURNED TO SERVICE.SDR CA120218001Ring · cracked(CAN) LOWER MOUNTING POINTS FOUND TO BE CRACKED DURING MAINTENANCE, NO ABNORMAL OCCURRENCES REPORTED MAINTENANCE IS INVESTIGATING AND HAS COMPLETED A HEAVY LANDING INSPECTION WITH NO FINDINGS. CREWS ARE BEING BRIEFED THROUGH SMS.SDR BSYA2012007Warning Light · false activationAFTER TAKE OFF, DOOR WARNING LIGHT ILLUMINATED, RETURNED AND LANDED. CHECKED DOOR AND FOUND THAT IT WAS CLOSED CORRECTLY. PILOT PROCEEDED TO OPEN AND RECLOSE DOOR, WARNING LIGHT STAYED OUT.SDR AWHA02012012Circuit Breaker · shortedTHE PILOT OF FLIGHT 7703 REPORTED THE PROPELLER HEAT INOPERATIVE IN FLIGHT. THE PROPELLER SPINNER WAS REMOVED AND VOLTAGE WAS CHECKED AT THE PROP BULKHEAD. VOLTAGE WAS FOUND AT 0VDC AT ALL THREE BOOTS. THE CIRCUIT BREAKER PANEL WAS REMOVED FOR INSPECTION ANSDR CA120202003Tube · failed(CAN) UPON LANDING, THE TUBE HAD A HOLE WHICH DEFLATED THE TIRE. THERE WAS NO HOLE IN THE TIRE, JUST THE TUBE. ON TEAR DOWN, THERE WAS NO EVIDENCE OF THE WHEEL ASSY BEING INCORRECTLY ASSEMBLED. THE TIRE ASSY WAS REPLACED AND THE ACFT WAS RETURNED TO SERVICESDR CA120131003Guard · damaged(CAN) ACFT REPORTED STIFF RT ELEVATOR TRIM IN FLIGHT, BUT TRIM ACTUATION WAS NORMAL ON THE GROUND. IT WAS FOUND THAT WHEN THE ELEVATOR WAS PLACED IN A NEUTRAL POSITION, THE TRIM WOULD BEGIN TO BIND. THE PHENOLIC PLATE THAT IS RIVETED ONTO THE CHAIN GUARD OF SDR AWHA02082012Remote Switch · defectiveTHE PILOT REPORTED ON TAXI THE ELT ACTIVATED. MX MANUALLY RESET THE ELT AND DEFERRED THE SYSTEM. ON SECOND TAXI OUT THE ELT ACTIVATED AGAIN. ELT WAS DEACTIVATED AND REMOVED FROM THE AIRCRAFT. THE FOLLOWING DAY THE ELT WAS REPLACED WITH A NEW UNIT THE DEFERSDR BSYA2012001Indicator · inoperativeDURING TAKEOFF ROLL OUT OF DPA, PILOTS AIRSPEED INDICATOR INOPERATIVE. PILOT ABORTED TAKEOFF AND RETURNED TO RAMP. AVIONICS SHOP REPLACED DEFECTIVE AIRSPEED INDICATOR, OPERATIONAL CHECK NORMAL.SDR EPUA20120120004Brake Sys · weakBRAKES SEEM WEAK.SDR TWYA011412Boot · separatedDURING CLIMBOUT THE PILOTS NOTICED SOMETHING BLACK COME OFF THE PROP. THEY EXPERIENCED VIBRATION IN THE ENGINE. TURNED BACK FOR SJU AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THAT ONE OF THE PROP DEICE BOOTS HAD COME OFF THE PROP. THE AIRCRAFTS PROP WASSDR CA120113014Wire Harness · burned(CAN) THERE WAS A NEWLY O/H PROPELLER INSTALLED. AFTER 10.4 HRS, THE PILOT SNAGGED THE PROP DE-ICE SYS FOR LOW AMPERAGE. THE MAINTENANCE DEPARTMENT FOUND 2 OUT OF THE 3 WIRES WERE BROKEN INTERNALLY. 1 OF THE WIRE HARNESS SHORTED AND SPARKED WHEN MOVED. THE SDR CA120112002Tube · failed(CAN) UPON LANDING, THE RT MAIN WHEEL POPPED AND CAUSE THE TIRE TO COMPLETLY DEFLATE. HAVE NOT HEARD BACK FROM THE CREW AS TO THE EXACT DETAILS OF THE LANDING.SDR EPUA2012012501Bulkhead · crackedAFT CANTED BULHEAD AT STA 474.40 HAS TWO CRACKS EACH APPROX. 1.5 INCHES IN LENGTH. DURING REMOVAL OF THIS PART OTHER DAMAGE WAS FOUND. BOTH VERTICAL STAB WEBS (PNS: 2631021-15 AND 2631022-2)WERE REPLACED TO SIGNIFICANT FRETTING. THE AFT BULKHEAD ASSEMBLY WASDR HSYA2012011112Linkage · obstructedON SHORT FINAL, PILOT COULD NOT GET POWER LEVER TO GO INTO IDLE & ELECTED TO GO AROUND. AN EMERGENCY WAS DECLARED AND THE POWER LEVER FREED UP. FLIGHT LANDED WITHOUT FUTHER INCIDENT. MX WAS UNABLE TO DUPLICATE THE PROBLEM. THROTTLE LINKAGE WAS INSPECTED ANDSDR RNVA20130325006Timer · faultyPILOT REPORTED THE ANTI-ICE CIRCUIT BREAKER TRIPPED AND HE HAD SMELL OF MELTING PLASTIC IN COCKPIT. MAINTENANCE REPLACED ANTI-ICE TIMER AND RELAY, PERFORMED OPS CHECK. SMELL WAS GONE AND BREAKER STAYED ACTIVATED.SDR HSYA2012010612Spring · brokenPILOT REPORTED ON LANDING, THE POWER LEVER STUCK IN IDLE POSITION AFTER TOUCHDOWN. POWER LEVER WOULD NOT GO INTO FEATHER POSITION OR ADVANCE. RELEASED WHEN OFF THE RUNWAY AND ONTO TAXIWAY. IT JAMMED OR STUCK AGAIN AFTER ENGINE SHUTDOWN. DISCOVERED A BROKESDR HSYA2012F00038Stop · brokenPILOT REPORTED THE POWER LEVER STUCK IN IDLE POSITION AFTER TOUCHDOWN. POWER LEVER WOULD NOT GO INTO FEATHER POSITION OR ADVANCE. PILOT STATED THAT IT WAS OK AGAIN ONCE OFF RUNWAY AND ON TAXIWAY. ALSO REPORTED THAT IT JAMMED OR STUCK AGAIN AFTER ENGINE SHUTSDR CA120109008Indicator · malfunctioned(CAN) AT ENGINE START UP, THE CREW NOTED THAT THE OIL PRESSURE INDICATOR MOVEMENT WAS `STICKY`. WHEN THE AIRCRAFT RETURNED TO MAINTENANCE THE FAULT WAS VERIFIED AND THE INSTRUMENT WAS REPLACED WITH AN OVERHAULED UNIT.SDR MTNA0101051200001Connector · corrodedEN ROUTE FROM BWI TO EWR ON FLIGHT 8311. THE STANDBY ELECTRICAL POWER ON, CAUTION LIGHT CAME ON. THE PILOT TRIPPED AND RESET THE GENERATOR. THE GENERATOR DID NOT COME BACK ON LINE. THE FOLLOWING C/BS TRIPPED BUS POWER NR 2, STANDBY POWER, BLEED AIR HEAT, BSDR BSYA2012002Tire · deflatedTIRE WENT FLAT ON RUN WAY. REMOVED AND REPLACED TIRE AND TUBE, AIRCRAFT GOOD TO GO.SDR MT9A2012F00009Support · crackedTHE LEFT PULLEY SUPPORT WEB BELOW THE FLOOR AT FS 120.0, LBL 10.0 CRACKED FROM THE FWD ELEVATOR BELLCRANK MOUNT BOLT ACCESS HOLE TO THE END OF THE WEB.SDR MT9A2012F00008Support · crackedTHE LEFT PULLEY SUPPORT WEB BELOW THE FLOOR AT FS 120.0, LBL 10.0 CRACKED FROM THE FWD ELEVATOR BELLCRANK MOUNT BOLT ACCESS HOLE TO THE END OF THE WEB.SDR MT9A2012F00007Support · crackedTHE LEFT PULLEY SUPPORT WEB BELOW THE FLOOR AT FS 120.0, LBL 10.0 CRACKED FROM THE FWD ELEVATOR BELLCRANK MOUNT BOLT ACCESS HOLE TO THE END OF THE WEB.SDR MT9A2012F00006Support · crackedTHE LEFT PULLEY SUPPORT WEB BELOW THE FLOOR AT FS 120.0, LBL 10.0 CRACKED FROM THE FWD ELEVATOR BELLCRANK MOUNT BOLT ACCESS HOLE TO THE END OF THE WEB.SDR MT9A2012F00005Support · crackedTHE LEFT PULLEY SUPPORT WEB BELOW THE FLOOR AT FS 120.0, LBL 10.0 CRACKED FROM THE FWD ELEVATOR BELLCRANK MOUNT BOLT ACCESS HOLE TO THE END OF THE WEB.SDR MT9A2012F00004Support · crackedTHE LEFT PULLEY SUPPORT WEB BELOW THE FLOOR AT FS 120.0, LBL 10.0 CRACKED FROM THE FWD ELEVATOR BELLCRANK MOUNT BOLT ACCESS HOLE TO THE END OF THE WEB.SDR MT9A2012F00003Support · crackedTHE LEFT PULLEY SUPPORT WEB BELOW THE FLOOR AT FS 120.0, LBL 10.0 CRACKED FROM THE FWD ELEVATOR BELLCRANK MOUNT BOLT ACCESS HOLE TO THE END OF THE WEB.SDR MT9A2012F00002Support · crackedTHE LEFT PULLEY SUPPORT WEB BELOW THE FLOOR AT FS 120.0, LBL 10.0 CRACKED FROM THE FWD ELEVATOR BELLCRANK MOUNT BOLT ACCESS HOLE TO THE END OF THE WEB.SDR MT9A2012F00001Support · crackedTHE LEFT PULLEY SUPPORT WEB BELOW THE FLOOR AT FS 120.0, LBL 10.0 CRACKED FROM THE FWD ELEVATOR BELLCRANK MOUNT BOLT ACCESS HOLE TO THE END OF THE WEB.SDR 2011FA0000809G Switch · inoperativeELT FAILED G-SWITCH TEST.SDR 2011FA0000808G Switch · no testELT FAILED G-SWITCH TEST.SDR 2011FA0000807G Switch · no testELT FAILED G-SWITCH TEST.SDR CA111227002Engine · power loss(CAN) 10 MINUTES INTO CRUISE, THE PILOT REPORTED AN UNCOMMANDED ACCELERATION OF THE ENGINE AND ALL PARAMETERS. TORQUE ESTABLISHED AT 2200 FT LB, NG 108 PERCENT. THE PILOT INCREASED ALTITUDE AND CONTINUED TOWARDS HERVY BAY AIRPORT. ONCE WITHIN SAFE GLIDING RSDR RNVA20130325007Engine · power lossPILOT REPORT THAT HE HAD A 400 FT/LB DROP IN TORQUE DURING TAKEOFF, HE RETURNED TO AIRPORT. MAINTENANCE WAS DISPATCHED, WHERE A OPERATIONAL FLIGHT WAS PERFORMED. THE DROP IN POWER COULD NOT BE DUPLICATE, AIRCRAFT WAS RETURNED TO SERVICE.SDR AWHA121311Unknown · malfunctionedTHE PILOT REPORTED AS HE WAS TAXIING N763FE BACK TO THE PARKING SPACE AND MAKING A LEFT TURN THE LEFT BRAKE PEDAL WENT ALL THE WAY DOWN TO THE FLOOR. HE STATED HE WAS ABLE TO CONTROL THE AIRCRAFT WITH LEFT BRAKE AND A LITTLE REVERSE. AIRCRAFT WAS INVOLVED INSDR MT9A2012F00000Engine · failedSHORTLY AFTER TAKEOFF, ENROUTE, ACFT EXPERIENCED AN ENGINE FLAMEOUT ACCOMPANIED BY A LOUD BANG. THE PILOT WAS ABLE TO SAFELY LAND WITH NO FURTHER INCIDENTS. MX INVESTIGATED AND FOUND THAT THE ENGINE HAD SUFFERED A CATASTROPHIC FAILURE, DESTROYING ALL ROTATINSDR AWHA113011Master Cylinder · failedPILOT FOR FLIGHT 7706 REPORTED AS HE WAS TAXIING FROM THE RAMP FOR DEPARTURE THE AIRCRAFT WAS OPERATING NORMAL, WINDS AT THE TIME WERE FROM 02 AT 14G22KTS (TAXIING WITH A TAILWIND). UPON REACHING FOR TAKEOFF AND MAKING A RT TURN FOR DEPARTURE THE RT BRAKE PEDSDR EPUA20111201005Vane · crackedBYPASS DOOR LOOSE (WILL NOT CLOSE ALL THE WAY). UPON INVESTIGATION FOUND FWD INERTIAL VANE ASSY SHAFT CRACKED. WHILE REPAIRING THE PREVIOUS DISCREPENCY, THE MECHANIC NOTICED THAT THE INLET SPLITTER PN 200803-513-01 WAS CRACKED AT THE CORNER.SDR COEA2011112903899Roll Pin · shearedATB TO LMT FLIGHT 7675: SHORTLY AFTER TAKEOFF PILOT REPORTED LOSS OF AILERON TRIM CONTROL. PILOT ELECTED TO RETURN TO LMT AND DECLARE AN EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND SHEARED ROLL PIN IN THE LOWER HORIZONTAL SPROCKET OF THESDR EPUA20111201006Frame · crackedFUSELAGE FORMER AT STATION 385.6 HAS A CRACK 2" TO RT OF BOTTOM CENTER LINE.SDR COEA2011112101976Cargo Track · corrodedINSP PDX / LEVEL 2 CORROSION: DURING INSPECTION IN PDX, FOUND LEFT INBOARD AND CENTER CARGO AREA SEAT TRACKS CORRODED BEYOND SERVICEABLE LIMITS IN VARIOUS LOCATIONS. DAMAGE RANGES BETWEEN FUSELAGE STATIONS 166 TO 332. REMOVED AND REPLACED SEAT TRACKS PN 261SDR COEA2011111701788Cargo Track · corrodedINPS PDX / LEVEL 2 CORROSION: DURING INSPECTION FOUND ALL 5 CARGO AREA SEAT TRACKS CORRODED BEYOND SERVICEABLE LIMITS IN VARIOUS LOCATIONS. DAMAGE RANGES BETWEEN FUSELAGE STATION 166 - 332. REMOVE AND REPLACE SEAT TRACKS WITH FACTORY REPLACEMENT PARTS. (PNSDR CA111117004Fitting · used(CAN) CRACK WAS FOUND DURING EDDY CURRENT INSPECTION IAW MM 5, 5-14-28.SDR COEA2011111501797Seat Track · corrodedINSP GEG / LEVEL 2 CORROSION: DURING INSPECTION, FOUND LEFT INBOARD CARGO SEAT TRACK CORRODED BEYOND SERVICEABLE LIMITS. DAMAGE MOSTLY FOUND BETWEEN FUSELAGE STATION 282 AND 332. REMOVED AND REPLACED SEAT TRACK USING FACTORY REPLACEMENT PART.SDR EPUA20111201004Lever · brokenWHEN IN BYPASS, DOOR IS HALF WAY BETWEEN NORMAL AND BYPASS. ON INVESTIGATION IT WAS FOUND THAT FWD INERTIAL SEPERATOR LEVER WAS BROKEN.SDR CA111121010Actuator · failed(CAN) SHORTLY AFTER DEPARTURE FROM MAIN BASE, THE ACFT SUFFERED A FLAP SYS MALFUNCTION. THE FLAP SYSTEM CIRCUIT BREAKER POPPED ON FLAP RETRACTION FROM 20 DEGREES TO 10 DEGREES. THE PILOT FOLLOWED CHECKLIST PROCEDURES BUT THE FLAP CIRCUIT BREAKER POPPED A SEC
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