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 COEA2009040901797Switch · failedAIR TURNBACK, FUEL RESERVOIR LOW LIGHT AFTER TAKEOFF FROM DEPARTURE. AIRCRAFT RETURNED TO DEPARTURE WITHOUT INCIDENT. NO EMERGENCY DECLARED. REMOVED AND REPLACE FUEL RESERVOIR LOW LEVEL FLOAT SWITCH. OPS CHECK GOOD. LEAK CHECK GOOD.SDR CA090409001Tire · deflated(CAN) AFTER LANDING THE CREW WAS UNABLE TO MOVE THE ACFT OFF THE RUNWAY DUE TO A FLAT MAIN LT TIRE. THE TIRE WAS CHANGED AND ACFT REMOVED FROM RUNWAY. THE COMPANY IS AWAITING TEARDOWN OF THE WHEEL TO SEE WHAT THE FAULT WAS IF DETERMINABLE.SDR CA090408008Engine · flamed out(CAN) AT FL60, THE CHIP DETECTOR LIGHT CAME ON FOLLOWED BY ENGINE FLAMEOUT. A RE-LIGHT ATTEMPT WAS UNSUCCESSFUL AND A FORCED LANDING WAS ACCOMPLISHED ON A FROZEN LAKE WITH NO DAMAGE TO THE ACFT. THE OPERATOR WILL PROCEED WITH THE ENGINE CHANGE AND DECIDE ON ANSDR COEA2009033101788Governor · failedTAXI BACK, OVERSPEED GOVERNOR TEST FAILED DURING GROUND RUN UP. PROP RPM WENT TO RED LINE. REMOVED AND REPLACED OVERSPEED GOVERNOR. ACFT RETURNED TO SERVICE.SDR CA090331011Tire · flat(CAN) TIRE FOUND FLAT IN HANGAR - REPLACED WITH NEW.SDR COEA2009032601728Fitting · crackedHAIRLINE CRACK .4375 INCH IN LENGTH FOUND ON ENGINE FIREWALL SUPPORT FITTING JUST ABOVE NOSE GEAR SPRING BEARING SUPPORT. REMOVED AND REPLACED SUPPORT STRUCTURE FITTING.SDR CA090331009Tire · flat(CAN) RT MAIN TIRE WENT FLAT ON RAMP - REPLACED WITH NEW.SDR CA090331010Tire · flat(CAN) TIRE WENT FLAT PUTTING ACFT IN HANGAR - REPLACED WITH NEW.SDR BSYA2009016O-Ring · wornAIRCRAFT TOOK OFF OUT OF CRW, GROUND CREW NOTICED SMOKE COMING FROM LEFT LANDING GEAR. REQUESTED EMERGENCY EQUIPMENT AT BWI WHEN AIRCRAFT LANDED. MAINTENANCE FOUND LEFT BRAKE CALIPER LEAKING. REMOVED AND REPLACED BRAKE CALIPER. OK FOR CONTINUED SERVICE.SDR HSYA20090226Control Cable · brokenDURING SHUTDOWN THE CREW REPORTED A LOUD "POP" WHEN MOVING THE PROP LEVER INTO THE FEATHER POSITION. IT WAS NOTED THAT THE PROPELLER DID NOT FEATHER AND THE CONTROL MOVED VERY FREELY. MAINTENANCE REMOVED AND REPLACED A BROKEN PROP GOVERNOR CONTROL CABLE.SDR AXSA998FE022609Indicator · failedFLIGHT 8302 EWR-PBG DURING CRUISE THE PILOT NOTED THE LEFT ATTITUDE INDICATOR WAS IN A 10 DEGREE RIGHT BANK. INFORMATION WAS VERIFIED INACCURATE BY COPILOT’S ATTITUDE INDICATOR AND HEADING INFORMATION. WITHIN EIGHT MINUTES THE BANK INCREASED TO 15 DEGREES ANSDR CA090304015Filter · unknown(CAN) PILOT WAS PREPARING FOR TAXIING, BUT WHEN HE ELECTED TO ADVANCE THE POWER LEVER THERE WAS NO RESPONSE FROM THE ENGINE. ACFT RETURNED TO GATE. THE P3 FILTER WAS REPLACED AND THE ACFT RETURNED TO SERVICE.SDR COEA2009022402899Support · crackedIN-FLIGHT FLAP CONTROL MALFUNCTION. FLAP MOTOR CB POPPED WHEN "FULL" FLAPS SELECTED IN-FLIGHT ALSO AFTER LANDING WHEN FLAPS SELECTED "UP". TROUBLESHOOTING FOUND CRACKS IN THE WING FLAP MOTOR/ACTUATOR SUPPORT ASSY AFT VERTICAL BRACKET AND FORE/AFT BRACKET. TSDR BSYA2009013Wire · damagedAIRCRAFT WAS EN ROUTE FROM CPS TO CLE WHEN THE WING DE-ICE BOOTS CIRCUIT BREAKER POPPED AND WOULD NOT RESET. PILOT DIVERTED TO LCK. MAINTENANCE FOUND A BARE WIRE AT LEFT WING ROOT BY TERMINAL BLOCK. REPAIRED WIRE, OPS CHECKS GOOD.SDR 2009F00013Hose · brokenPILOT REPORTED LOSS OF BRAKE PRESSURE/EFFECTIVNES FOR RT SIDE BRAKE SYS DURING TAXI. FOUND BRAKE FLEX HOSE HAD PULLED COMPLETELY OUT OF SWAGGED HOSE FITTING AT THE BRAKE CALLIPER RESULTING IN COMPLETE LOSS OF BRAKE FLUID.SDR CA090304016Turbine Blades · damaged(CAN) WHEN POWER WAS APPLIED FOR TAKEOFF, A LOUD NOISE WAS HEARD FROM THE ENGINE. THE ENGINE WAS SHUTDOWN AND EXTENSIVE PT BLADE DAMAGE WAS DISCOVERED. ENGINE IS TO BE REMOVED AND FORWARDED FOR INVESTIGATION AND REPAIR.SDR CA090206010Tire · deflatedAFTER LOADING THE AIRCRAFT THE LEFT MAIN TIRE WAS FOUND TO BE FLAT. THE TIRE WAS REPLACED AND THE AIRCRAFT RETURNED TO SERVICE.SDR CA090206006Tire · deflatedPREFLIGHT INSPECTION SHOWED A FLAT RIGHT TIRE. NO CAUSE FOR THE FLAT HAS BEEN DETERMINED AT THIS TIME.SDR 2009F00012Hose · brokenPILOT REPORTED LOSS OF BRAKE PRESSURE/EFFECTIVNES FOR LT SIDE BRAKE SYS DURING TAXI. FOUND BRAKE FLEX HOSE HAD PULLED COMPLETELY OUT OF SWAGGED HOSE FITTING AT THE BRAKE CALIPER RESULTING IN COMPLETE LOSS OF BRAKE FLUID.SDR COEA2009013002756Tube · failedABORTED TAKEOFF, DURING TAKEOFF ROLL, AT 30 TO 40 KTS. THE LT WING DIPPED FOLLOWED BY VIBRATION. THE PILOT ABORTED TAKEOFF AND STOPPED THE ACFT SAFELY. THE LT MAIN TIRE WENT FLAT. SINCE THE ACFT WAS TOWED FROM THE RUNWAY ON THE DEFECTIVE TIRE, CAUSE OF THE SDR COEA2009013001756Tire · failedABORTED TAKEOFF, DURING TAKE-OFF ROLL, AT 30 TO 40 KTS. THE LT WING DIPPED, FOLLOWED BY VIBRATION. THE PILOT ABORTED TAKEOFF AND STOPPED THE ACFT SAFELY. THE LT MAIN TIRE WENT FLAT. SINCE THE ACFT WAS TOWED FROM THE RUNWAY ON THE DEFECTIVE TIRE, CAUSE OF THSDR CA100202006Bearing Seal · leaking(CAN) ODD SMOKE SMELL IN CABIN WHEN BLEED HEAT WAS APPLIED. COMPRESSOR WASH PERFORMED WITH NO RESULTS. ENGINE BORESCOPE COMPLETED AND NR2 BRG FOUND TO BE LEAKING A BIT. ENGINE SENT AND REPAIRED. ENGINE REINSTALLED AND PROBLEM WAS CORRECTED. (TC 20100202006)SDR CA090127003Pump · failedAME NOTICED FUEL IN THE DRAIN CAN ON A DAILY CHECK. DURING A SUBSEQUENT GROUND RUN HE FEELS THAT THE ENGINE PERFORMANCE FROM LOW TO HIGH IDLE IS NOT AS FAST AS IT SHOULD BE. THE AIRCRAFT IS GROUNDED AND A REPLACEMENT PUMP ASSY AND SUPPORT PARTS HAVE BEEN DISSDR 2009FA0000085Hinge · corrodedDURING THE REMOVAL OF THE RUDDER, LWR STABILIZER HINGE ASSY WAS FOUND WITH HEAVY CORROSION. THIS CORROSION WAS NOT VISIBLE WITHOUT REMOVING THE RUDDER. (K)SDR CA090126009Tube · failedTIRE WENT FLAT IN HANGAR AFTER AIRCRAFT WAS PUT IN FOR THE NIGHT. WHEEL ASSEMBLY INSPECTED AND SMALL HOLE FOUND IN TUBE. NOTHING FOUND IN TIRE TO CAUSE HOLE.SDR 2009FA0000060Wire · chafedTHE PILOT REPORTED HIS TAIL BEACON INOPERATIVE. MX TECHS TROUBLESHOT THE WIRING AND FOUND THAT THE WIRING BUNDLE THAT CONTAINS THE POWER WIRE FOR THE TAIL BEACON WHERE IT ROUTES OVER THE GLOVE BOX HAD CHAFED ON THE GLOVE BOX. THE CHAFING CAUSED THE WIRE TO BSDR COEA2009012301700Indicator · malfunctionedABORTED TAKEOFF. DURING TAKEOFF ROLL, THE PROPELLER SPEED CAME UP TO ONLY 1300 RPM. NORMAL RPM IS 1900. THE PILOT ABORTED TAKEOFF AND THE ACFT SAFELY RETURNED TO THE RAMP. REPLACED NP (PROPELLER RPM) INDICATOR.SDR CA090122010Plunger · out of positionPILOT REPORT, EN ROUTE TO YQT AT 9000 FEET, THE UPPER HALF OF REAR CARGO DOOR OPENED IN FLIGHT AND DOOR WARNING ANNUNCIATOR ILLUMINATED. LOWERED FLAPS AND SLOWED AIRCRAFT TO 100 KTS AS PER AFM. REQUESTED DIRECT TO NEAREST AIRPORT (YQK) AND LANDED WITH OUT INSDR CA090120002Ring · cracked(CAN) DURING ROUTINE PHASE 5 INSPECTION A CRACK WAS FOUND ON THE RING ASSY, ENGINE MOUNT. THE CRACK IS LOCATED ON THE LOWER FWD RT THROUGH BOLT HOLE WELD. THE MOUNT RING ASSY WILL BE SENT FOR REPAIR. IF FOUND TO BE NOT REPAIRABLE, THE RING ASSY WILL BE REPLSDR BSYA2009002Striker · wornON TAKEOFF OUT OF LCK THE TOP CARGO DOOR CAME OPEN, PILOT THEN RETURNED TO LCK NO PROBLEMS. MAINTENANCE REPLACED WORN STRIKER PLATE AND PLUNGER.SDR 2009FA0000043Shroud · gougedENG PERFORMANCE RUNS INDICATED ITT WAS EXCEEDING TARGET TEMP +20 DEGREES C. THE ENGINE WAS SPLIT AT THE C-FLANGE AND THE ENG SEPARATED TO INSPECT THE HOT SECTION. IT WAS FOUND THAT THE CT BLADE SEGMENTS HAD SHIFTED AND ALSO THERE WAS SEGMENT TIP CURL AT SEVERSDR COEA2009010901850Tube · cutFLAT TIRE ON LANDING. ON TOUCHDOWN THE PILOT FELT THE ACFT PULL TO THE LT AND THE LT TIRE THUMPING. THE PILOT BROUGHT THE ACFT TO A STOP ON THE RUN WAY JUST SHORT OF THE TAXI WAY. ACFT TAXIED TO THE RAMP AFTER REPLACING THE WHEEL. INSP OF THE WHEEL ASSY FOUSDR COEA2009010901899Fairing · brokenBODY FAIRING LOST IN FLIGHT: POST FLIGHT INSP, THE RT MLG LEG TO FUSELAGE FAIRING WAS DISCOVERED BROKEN WITH A PORTION OF IT MISSING. REPLACED RT BODY FAIRING.SDR CA081208008Starter Gen · failed(CAN) GENERATOR FAILED IN FLIGHT 12 MILES FROM YWG ENROUTE TO YQT. AIRCRAFT RETURNED TO YWG (TC NR 20081208008).SDR 2008FA0000903Tube · leakingTHE PILOT REPORTED A FLAT TIRE. MAINT FOUND AN INNER-TUBE LEAKING WITH NO APPARENT DAMAGE TO THE TIRE. THE TUBE WAS REPLACED WITH A NEW TUBE. SIX DAYS LATER THE SAME PILOT IN CHARGE OF THE SAME ACFT REPORTED THE SAME TIRE FLAT. MX AGAIN FOUND THE INNER TUBSDR COEA2008120102775Torque Tube · corrodedTHE RT INBOARD CONTROL HORN ATTACHMENT RIVETS FOUND WORKING ON ELEVATOR TORQUE TUBE ASSY. RT ELEVATOR CONTROL HORN EXHIBITED ROTATIONAL AND LATERAL MOVEMENT ON TORQUE TUBE. RIVET HOLES, CONTROL HORN AND TORQUE TUBE EXHIBITED FRETTING CORROSION. REMOVED AND SDR COEA2008120101976Torque Tube · looseTHE LT INBOARD CONTROL HORN ATTACHMENT RIVETS FOUND WORKING ON ELEVATOR TORQUE TUBE ASSY. LT ELEVATOR CONTROL HORN EXHIBITED ROTATIONAL MOVEMENT ON TORQUE TUBE. UPON REMOVAL OF HORN FROM TORQUE TUBE, FOUND WEAR WAS LIMITED TO RIVETS. REMOVED AND REPLACED TORSDR OMKR2008-0003None · noneNEW ACFT FROM FACTORY. PERFORMED AD SEARCH DUE TO EXPORT REQUIREMENT DURING ANNUAL. FOUND NUMEROUS ADS SIGNED OFF AS COMPLIED WITH THAT WERE N/A TO ACFT. MANY LISTED PARTS THAT WERE SUPPOSEDLY CHANGED. CONTACTED CESSNA. WAS ASKED WHY WITH SO MANY NEW ACFTSDR 2008FA0000867Mount · crackedTHE LT ENGINE MOUNT BRACKET WAS FOUND TO HAVE CRACKS INSIDE THE ASSY AT THE TERMINATION END OF BOTH WELDS. (K)SDR 2008FA0000866Mount · crackedTHE CENTER ENGINE MOUNT BRACKET WAS FOUND TO HAVE CRACKS INSIDE THE ASSY AT THE TERMINATION END OF BOTH WELDS. (K)SDR SBAA200800003Flow Valve · failedDURING TAKEOFF THE BLEED AIR HEAT CAME ON WITHOUT PILOT INPUT. PILOT ATTEMPTED TO TURN HEAT OFF WITH SYS SWITCH AND TEMP. CONTROL KNOB. NEITHER ACTION WORKED. COCKPIT WAS GETTING EXCESSIVELY HOT SO PILOT OPENED UP ALL AIR VENTS AND PULLED FIREWALL SHUTOFF VALVSDR CA081125007Engine · vibration(CAN) AT FL100 IN STEADY STATE, THE PILOT HEARD A STRONG NOISE COMING FROM THE ENG AND THE INSTRUMENTS INDICATED TEMP AT 800°C, NG AT 100 PERCENT AND TORQUE AT 2000 FT-LB. THE POWER LEVER WAS RETARDED AND PARAMETERS CAME BACK TO (NORMAL). THE FLIGHT CONTINUEDSDR MT92008F00008Transistor · burnedTHE PILOT REPORTED SMOKE IN THE COCKPIT TO ATC, DECLARED AN EMERGENCY, AND RETURNED TO DEPARTURE. THE SMOKE THAT WAS SEEN BY THE PILOT APPEARED TO BE COMING FROM UNDER THE GLARE SHIELD ABOVE THE FUEL FLOW AND FUEL QUANTITY INDICATORS. THE PILOT SAID THERE WASDR MTNA1008003Master Cylinder · defectiveDURING TAXI-OUT THE PILOT NOTED THAT THE LEFT BRAKE LOST PRESSURE AS THE PLANE TURNED ONTO THE MAIN RUNWAY. THE ENGINE WAS SHUT DOWN AND THE AIRCRAFT WAS TOWED BACK TO THE RAMP. MAINTENANCE DETERMIND THE AIRCRAFT NEEDED A BRAKE MASTER CYLINDER.SDR HSYA20081002Brake Sys · malfunctionedDURING AN ATTEMPTED LEFT HARD TURN OFF OF THE TAXI WAY ONTO THE RUNWAY THE CREW REPORTED THE AIRCRAFT CONTINUED IN A STRAIGHT LINE AND LOST BRAKING. THE CREW WAS ABLE TO STOP THE AIRCRAFT WITH NO INCIDENT. MAINTENANCE TOWED THE AIRCRAFT TO THE HANGAR. AFTERSDR HSYA20081001Unknown · smokeSTRONG SMELL OF BURNING OR BURNT INSULATION AND A SLIGHT HAZE OF SMOKE IN COCKPIT. BOTH THE LEFT AND RIGHT INSTRUMENT PANELS AND WIRING WERE INSPECTED FOR OBVIOUS DAMAGE. PERFORMED GROUND RUNS WITH ALL COCKPIT INSTRUMENTS ON AND COULD NOT DUPLICATE THE PROBLSDR COEA0802788Switch · inoperativeRETURN TO BLOCKS. FLT NR 8690 PDX TO MFR. ACFT TAXIED TO RUNWAY RUN UP AREA. WITH ENGINE RUNS COMPLETED, ATTEMPTS TO CONTACT CLEARANCE DELIVERY FOUND NO VOICE BEING TRANSMITTED FROM EITHER NR 1 OR NR 2 RADIOS. ACFT WAS TAXIED BACK SAFELY TO BLOCKS FOR MX. SDR CA081103004Bearing · failed(CAN) NR 1 BRG FAILED WITHOUT OUTSIDE INFLUENCE. RESULTANT METAL CONTAMINATION CONTAINED TO THE GB, MAIN OIL FILTER AND OIL PUMP.SDR BSY2008F00004Starter · noisyAFTER TAKEOFF, AT 5,000 FT, ENGINE STARTER TO MAKE A SQUEALING NOISE WITH A RISE IN EGT, LOW TORQUE AND NO. PILOT THEN RETURNED TO DEPARTURE NO PROBLEMS. CAUSE UNKNOWN AT THIS TIME. (K)SDR COEA0801899Unknown · malfunctionedDURING CLIMB OUT AT APPROXIMATELY 1500 FT AGL THE FUEL FLOW DROPPED TO 75 PPH. THE PARS UNIT CONFIRMED A 75 PPH FUEL FLOW. THE AC RETURNED TO SAFELY. TROUBLESHOOT ON THE GROUND WITH ENGINE RUNS COULD NOT DUPLICATE THE PROBLEM. THE FUEL FLOW INDICATOR WAS R
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