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 SBAA201410030002Governor · defectiveWHILE TURNING TO FINAL APPROACH, PROPELLER BEGAN TO SHAKE & RATE OF DESCENT INCREASED. POWER LEVER MOVED FWD BUT APPEARED TO BEHIND THE BETA REVERSE GATE ON CONTROL QUADRANT. APPEARED PROPELLER HAD GONE INTO AN UNCOMMANDED BETA RANGE DURING FLIGHT. POWER LSDR CA140905003Skin · cracked(CAN) DURING A SCHEDULED MAINTENANCE INSPECTION THE HORIZONTAL STABILIZER WAS NOTED TO HAVE A VERY LOUD OIL CANNING NOISE COMING FROM INSIDE THE TAIL SECTION WITH LIGHT PRESSURE APPLIED UP OR DOWN ON THE STABILIZER TIPS. UPON FURTHER INVESTIGATION THE AME FOUSDR COEA2014083001937Connector · dirtyAIR TURN BACK, LOW VOLTAGE ANNUNCIATOR LIGHT ILLUMINATED IN FLIGHT & STAYED ON. CREW RETURNED TO BLOCK, NO EMER WAS DECLARED. CLEANED CONNECTORS & PERFORMED GND RUN UP. NO DISCREPANCIES FOUND, COULD NOT DUPLICATE. ACFT RETURNED TO SERVICE.SDR CA140908007Engine · malfunctioned(CAN) DURING AN OPERATIONAL FLIGHT, THE COMMANDER REPORTED: THE OIL TEMPERATURE WAS RAISED TO THE MAXIMUM. THE OIL PRESSURE AND TORQUE WERE VERY LOW AND DID NOT REACT WITH EITHER THE POWER LEVER AND THE EMERGENCY POWER LEVER. THE PILOT PERFORMED A EMERGENCY SDR EPUA20140815001Unknown · odorPASSENGER COMPLAINT OF JET FUEL SMELL IN ACFT. INSPECTED ACFT INTERNALLY & EXTERNALLY FOR SIGNS OF FUEL LEAKAGE, NONE NOTED. ONLY THE SMELL OF LIVE ANIMAL WAS NOTED.SDR COEA20140801953Gyro · failedDEPARTED OUT ON TIME, DURING CLIMB OUT THE RMI & HSI COMPASS CARDS BEGAN TO SPIN. THE RMI FLAGGED HDG & HSI FLAGGED COMPASS AS THE PILOT ENTERED IMC CONDITIONS. THE PILOT ADVISED AIR TRAFFIC CONTROL HE NEEDED TO RETURN. RETURNED FOR MX. REPLACED REMOTE DIRSDR CA140728002Lever · broken(CAN) THE INERTIAL SEPARATOR WAS "STUCK IN BYPASS" IN FLIGHT. FOUND THE ACTUATOR LEVER ASSY BROKEN IN HALF AT THE EYEBOLT.SDR YRRR2014082200495Blades · crackedWHILE THE ENGINE WAS SPLIT FOR A HOG SECTION INSPECTION AND PT VANE CHANGE IT WAS FOUND THAT 1 OF THE POWER TURBINE BLADES WERE CRACKED.SDR CA140723005Roll Pin · missing(CAN) A ROLL PIN WAS FOUND TO BE MISSING FROM A GEAR ON THE AILERON TRIM CONTROL IN THE PEDESTAL IN THE COCKPIT ALLOWING NO INPUT FOR USE OF AILERON TRIM.SDR CA140721012Engine · malfunctioned(CAN) DURING A TRAINING FLIGHT, IN CRUISE CONDITION, THE CREW EXPERIENCED AN UNCOMMAND POWER INCREASE. THEY WERE UNABLE TO REDUCE THE ENGINE POWER. ENGINE WAS SHUTDOWN BY THE CREW. THEY LANDED UNEVENTFULLY TO THE DESTINATION AIRPORT. TROUBLESHOOTING IS IN PSDR 9PER201407090001Trunnion · chafedDURING AN ANNUAL INSPECTION, BOTH GEAR FAIRINGS FOUND CHAFED INTO THE LOWER SIDE OF BOTH MAIN GEAR TRUNNIONS. DAMAGE ON LT WAS .156" IN DEPTH AND RT WAS .176" IN DEPTH. INFORMED THE TRUNNIONS REQUIRED REPLACEMENT.SDR DEMA2014063000002Engine · failedDURING CRUISE, THE PILOT NOTICED A FLUCTUATION OF THE ENGINE TORQUE INDICATOR. THE FLUCTUATION WAS BETWEEN 50-100 FT/LBS. IMMEDIATELY FOLLOWING THE TORQUE FLUCTUATION, THE OIL PRESSURE DROPPED AND THE OIL TEMPERATURE ROSE. AN EMERGENCY WAS DECLARED AND THE SDR CA140625001Lever · malfunctioned(CAN) EMERGENCY LANDING IN A FIELD AFTER THE PILOTS NOTED THE RPM`S WERE SLOWLY BLEEDING AND THEY COULD NOT GET THE PROPELLER TO RESPOND TO INCREASED RPM ADJUSTMENTS. THE PROP BLED RPM`S UNTIL IT WENT INTO FEATHER AND THE PILOTS SAFELY LANDED THE ACFT IN A FISDR HSYA2014053014Connector · damagedSTBY POWER ON ANNUNCIATOR ILLUMINATING IN CLIMB WITH 2ND CB OF POWER 2 BUS & 3RD CB OF POWER 1 BUS POPPED.SDR CA140611001Tube · failed(CAN) DURING PRE-FLIGHT INSPECTION, PRIOR TO DEPARTURE IN THE AM THE RT MAIN TIRE WAS FOUND TO BE FLAT, ASSY WAS REMOVED AND SERVICEABLE ASSY WAS INSTALLED. WHEEL ASSY WAS INSPECTED ON 2014-06-10 AND THE TUBE WAS FOUND WITH A RUB MARK THAT CORRESPONDS WITH SOMSDR CA140509005Mount · corroded(CAN) CORROSION WAS FOUND DURING ROUTINE INSPECTION ON THE TOP ENGINE MOUNT BRACKET. FURTHER INVESTIGATION FOUND THAT THERE WAS CORROSION 0.027" DEEP INTO THE 0.050" BRACKET, CORRODED OVER HALFWAY THROUGH THE MATERIAL. NOTE: THE STAINLESS STEEL FIREWALL THAT SDR CA140512002Bulkhead · cracked(CAN) DISCOVERED ON PRESEASON INSPECTION, WHILE COMPLETING THE ANNUAL COMPLETE FLOAT INSPECTION. RIGHT FLOAT BULKHEAD NR 9, DISCOVERED MULTIPLE CRACKS RADIATING FROM CORNERS. CURRENTLY CONSULTING WITH ENGINEERING REPAIR AND LOGISTICS ON REPAIR .SDR 2014F00083Gps · failedDURING TAKING OFF, AIR CREW NOTICED A BURNING ODOR IN THE COCKPIT. ELECTED TO LAND BACK AT DEPARTURE AIRPORT. MAINTENANCE DETERMINED THAT THE GNS 530, GPS/COMM WAS THE SOURCE OF THE ODOR. THE GPS/COMM WAS R & R. ACFT PLACED BACK IN SERVICE WITH NO FURTHESDR CA140429001Push-Pull Rod · corroded(CAN) THE AFT END OF THE PUSH-PULL CONTROL ROD WAS FOUND CORRODED AT THE FORK-END NEAR THE ATTACHMENT BOLT HOLE. THE ACFT WAS REMOVED FROM SERVICE AWAITING A REPLACEMENT ROD.SDR DEM2014F00000Propeller · out of balanceDURING CRUISE FLIGHT, ACFT EXPERIENCED A VIBRATION CONSIDERED EXCESSIVE. REDUCED PROPELLER SPEED FROM NORMAL CRUISE SETTING. CLEARED THE VIBRATION FOR A SHORT TIME. ELECTED TO KEEP 1800 RPM SETTING AND AS FLIGHT CONTINUED THE VIBRATION RETURNED. DECLARED ASDR MK9A20140421001Master Cylinder · weakPIC & SIC BRAKES FAILED COMPLETELY DURING TAXI.SDR SBAA201400001Panel · deformedDURING VISUAL INSPECTION NOTICED THAT LT & RT WING INBD TKS PANELS WERE SLIGHTLY DEFORMED ALONG LE FROM APPROX WS 37.00 TO WS 51.00. TKS PANELS DID NOT APPEAR LOOSE & SEEMED TO OPERATE NORMALLY.SDR CA140908003Bellows · cracked(CAN) THE PILOT REPORTED THAT, WHILE FLYING, THE POWER LEVER WAS MOVED TO IDLE POSITION BUT THERE WAS NO CHANGE IN ENGINE POWER. TORQUE STAYED BETWEEN 1250 AND 1400 LBS". DURING THE ON GROUND TROUBLESHOOTING, THE FCU WAS SENT TO MFG FOR INVESTIGATION. FOUNDSDR HSYA2014041014Brake Sys · malfunctionedDURING AN ATTEMPTED RT TURN DURING TAXI OUT TO THE RUNWAY FOR A TRAINING FLIGHT, THE CREW ADVISED THEY WERE UNABLE TO MAKE THE RT TURN & REQUESTED A RETURN TO THE CARGO RAMP. UPON ARRIVING IN THE CARGO AREA, THE CREW ADVISED AIRCRAFT LOST BRAKING ABILITY & WESDR MK9A2014040901Fuel Control · faultyWHILE FLYING, POWER LEVER WAS MOVED TO IDLE POSITION BUT THERE WAS NO CHANGE IN ENG POWER. TORQUE STAYED BETWEEN 1250 & 1400 FLB.SDR CA140407002Link · failed(CAN) DURING THE PILOTS WALK AROUND, HE NOTED THE AILERON TRIM SYS WAS UNSERVICEABLE. UPON INSPECTION IT WAS FOUND THAT 1 OF THE MASTER, CONNECTING LINKS, WHICH ATTACH THE TRIM CABLE TO CHAIN AT THE TRIM ACTUATOR WAS MISSING. THE COMPLETE ASSY WAS GONE, NO PSDR FXTA2014F00122Bolt · failedLEFT WHEEL BOLT FAILED ON LANDING. HEARD A CLICKING OR GRINDING NOISE ON ROLL OUT AFTER LANDING. ABLE TO TAXI THE ACFT WITH NO DIFFICULTY'S TO RAMP. DISCOVERED A BROKEN WHEEL BOLT EXTENDED OUT OF THE INBD WHEEL HALF. BROKEN WHEEL BOLT HIT THE BRAKE TORQUE PSDR FXTA2014032400180G Switch · no testWHEN COMPLYING WITH ELT ANNUAL INSPECTION, UNABLE TO ACTIVATE THE G-SWITCH AS REQUIRED.SDR 2014FA0000164Pitot Line · blockedAFTER TAKEOFF THE PILOT NOTICED THE PILOT SIDE AIRSPEED INDICATOR WAS INDICATING 20-30KT DIFFERENCE FROM COPILOT SIDE. PILOT RETURNED TO BASE WHERE MAINTENANCE FOUND MOISTURE IN THE PILOTS SIDE PITOT LINE. MAINTENANCE REMOVED MOISTURE AND OPS CHECK PITOT HEAT SDR HYTA2014F00084Servo · failedSERVO, FAILURE OF THE TACH GENERATOR.SDR HSYA201403061405Flap Track · corrodedCORROSION FOUND ON INBD FLAP TRACK WEB RS FOUND OUT OF LIMITS. AREA FOUND TO BE SEVERE INTERGRANULAR CORROSION.SDR HSYA201403061404Flap Track · corrodedCORROSION FOUND ONCENTER FLAP TRACK WEB, R.S. FOUND OUT OF LIMITS. AREA FOUND TO BE SEVERE INTERGRANNULAR CORROSION.SDR HSYA201403061403Flap Track · corrodedCORROSION FOUND ON OTBD FLAP TRACK WEB RS FOUND OUT OF LIMITS. AREA FOUND TO BE SEVERE INTERGRANULAR CORROSION.SDR HSYA201403061402Flap Track · corrodedCORROSION FOUND ON OTBD FLAP TRACK WEB, LS FOUND OUT OF LIMITS. AREA FOUND TO BE SEVERE INTERGRANULAR CORROSION.SDR HSYA201403061401Flap Track · corrodedCORROSION FOUND ON CTR FLAP TRACK WEB, LS FOUND OUT OF LIMITS. AREA FOUND TO BE SEVERE INTERGRANULAR CORROSION.SDR MTNA02014306001Brake Assy · failedFLT 8122. DURING TAXI OUT, RT BRAKE BECAME INEFFECTIVE. REPLACED THE RT SIDE BRAKE AFTER TROUBLESHOOTING.SDR 2014FA0000104Spar · crackedFOUND FLAP LOWER SKIN CRACKED JUST ON THE OTBD SIDE OF THE INBD FLAP ATTACHMENT. AFTER REMOVAL OF THE SKIN THE AFT SPAR, AND RIB WHERE ALSO DAMAGED & CRACKED.SDR 2014FA0000103Skin · crackedWHILE PERFORMING INSPECTION, FOUND FLAP LOWER SKIN CRACKED JUST ON THE OTBD SIDE OF THE INBD FLAP ATTACHMENT. AFTER REMOVAL OF THE SKIN THE AFT SPAR, AND RIB, WHERE ALSO DAMAGED & CRACKED.SDR CA140224027Bolt · broken(CAN) ON LANDING, PILOT COMPLAINED ABOUT RT WHEEL BEING LOCKED UP, THEN LETTING LOOSE AGAIN. ON INSPECTION, FOUND BRAKE CYLINDER ASSY, CALIPER LOOSE ON DISK. BOTTOM RETAINING PIN, ANCHOR BOLT WAS MISSING, WITH THE THREAD AND LOCKNUT MISSING AS WELL. THE TOP SDR CA140313004Bolt · looseDURING TAXI, THE ENGINE SHOWED HIGH VIBRATIONS. PILOT SHUTDOWN THE ENGINE. INSPECTION FOUND ENGINE PROPELLER WITH A LOOSE BOLT, CAUSING THE BLADE ANGLE TO CHANGE, WHICH CREATED IMBALANCE. ENGINEERING RECOMMENDED TO REMOVE POWER SECTION FOR INSPECTION & REPAIRSDR CA140224010Engine · malfunctioned(CAN) DURING FLIGHT, THE CREW NOTICED A HIGH ENGINE TORQUE AND THEY WERE NOT ABLE TO REDUCE POWER. AN EMERGENCY WAS DECLARED AND LANDING WAS PERFORMED AT HIGHER THAN NORMAL SPEED. THE POWER LEVER WAS ABLE TO BE REDUCED TO FLIGHT IDLE ON APPROACH. THE ENGINE DSDR AWHA20140218001Lever · misinstalledPILOT EXPERIENCED A LOSS OF PROP RPM & PROP CONTROL. IMMEDIATELY CONTACTED ATC & DECLARED AN EMERGENCY. ATC GAVE DIRECTIONS, WEATHER & CLEARED TO NEAREST AIRPORT. PILOT REALIZED BECAUSE OF THE WINDS, WOULD BE UNABLE TO MAKE THE AIRPORT. ALSO, BECAUSE DESCESDR ENHA2014020Tube · failedUPON LANDING RT MLG TIRE WENT FLAT. PILOT WAS UNABLE TO TAXI THE ACFT CLEAR OF THE ACTIVE RUNWAY WITHOUT DOING DAMAGE TO THE ACFT. THIS RESULTED IN RUNWAY BEING CLOSED FOR A PERIOD OF 30 MINUTES. MX WAS SUMMONED TO THE ACFT & THEY REPLACED THE WHEEL & TIRE SDR COEA2014020601752Switch · stuckON CLIMB OUT THE CAPTAIN BEGAN TO SMELL WHAT SEEMED LIKE BURNING RUBBER. HE THEN SAW SMOKE COMING FROM THE LT CB PANEL. THE FLIGHT WAS IN IMC CONDITIONS. THE CAPTAIN DECLARED AN EMERGENCY & WAS VECTORED TO KLMT RUNWAY 32 ILS APPROACH. THE AIRCRAFT LANDED SSDR CA140128016Bolt · wrong part(CAN) INCORRECT BOLTS FOUND INSTALLED IN LT & RT AILERON OUTER, WING, PUSHROD AFT ATTACH LOCATION. PN AN4H13A, DRILLED HEAD FOR LOCKWIRE, FOUND NOT INSTALLED.SDR CA140128015Bolt · wrong part(CAN) INCORRECT BOLTS FOUND INSTALLED IN LT & RT AILERON OUTER, WING, PUSHROD AFT ATTACH LOCATION. PN AN4H13A, DRILLED HEAD FOR LOCKWIRE, FOUND NOT INSTALLED.SDR MK9A20140128001Unknown · malfunctionedSHORTLY AFTER TAKEOFF FROM OGG AIRSPEED & VERTICAL SPEED BEGAN WILD FLUCTUATIONS. FIRST OFFICER`S INSTRUMENTS SEEMED STABLE & CORRESPONDED TO STBY INSTRUMENTS. STABILIZED ACFT & RETURNED TO OGG.SDR CA140124019Doubler · cracked(CAN) LT WING PANEL DOUBLER AND WING SKIN FOUND CRACKED ON PILOT WALK AROUND PRE-FLIGHT INSPECTION AT PANEL LOCATION 501BB. REMOVED DAMAGE ON LT WING PANEL 501BB, INSTALLED FLUSH PATCH 1.5" X 1.5" 2024T3 WITH AN INSPECTION HOLE DOUBLER AND NEW FASTENER PLATE SDR CA140124004Ring · cracked(CAN) DURING THE ENGINE CHANGE THE HORSE COLLAR ASSY WAS FOUND TO BE CRACKED. TAFT IS 19041.2, CYCLES ARE 25651. PREVIOUSLY, DURING AN INSPECTION ON THE HORSE COLLAR WAS FOUND CRACKED IN MULTIPLE LOCATIONS, LARGE CRACKS, ON NOV 21, 3013. TAFT WAS 20366.6, CYCSDR MK9A201401170001Engine · smokeAFTER SHUTDOWN SMOKE WAS OBSERVED COMING FROM THE ENGINE.
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