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 YN8R2014011700004Flap Track · corrodedDURING ANNUAL INSPECTION, FOUND SIGNIFICANT CORROSION FLAP TRACKS. R & R FLAP TRACKS.SDR YN8R2014011700003Flap Track · corrodedDURING ANNUAL INSPECTION, FOUND SIGNIFICANT EXFOLIATION CORROSION OF 4 OF 6 FLAP TRACKS. R & R FLAP TRACKS WITH NEW.SDR YN8R2014011700002Flap Track · corrodedDURING ANNUAL INSPECTION, FOUND SIGNIFICANT EXFOLIATION CORROSION ON 4 OF 6 FLAP TRACKS. R & R FLAP TRACKS WITH NEW.SDR YN8R2014011700001Flap Track · corrodedDURING ANNUAL INSPECTION, FOUND SIGNIFICANT CORROSION ON FLAP TRACKS. R & R FLAP TRACKS.SDR MTNA01152014001Skin · corrodedWHILE TROUBLESHOOTING AN AUTOPILOT PITCH PROBLEM, MAINTENCE DISCOVERED THE ELEVATOR HINGE PLATE HAD LEVEL 3 CORROSION.SDR CA140113011Switch · inoperative(CAN) WHEN TROUBLESHOOTING THE WINDSCREEN ANTI-ICE SYS THAT WAS REPORTED TO BE INOPERATIVE BY THE FLIGHT CREW IT WAS NOTED THE WINDSCREEN ANTI-ICE SYS SELECTOR SWITCH "OFF" TERMINAL SHOWED SIGNS OF OVERHEATING. REVIEW OF THE C208 WIRING DIAGRAM SHOWS THAT TERSDR HSYA201312281301Flap Track · corrodedCORROSION FOUND ON OTBD FLAP TRACK WEB, LS FOUND OUT OF LIMITS. AREA FOUND TO BE SEVERE INTERGRANULAR CORROSION.SDR HSYA2013122813Flap Track · corrodedCORROSION FOUND ON INBD FLAP TRACK WEB, LS FOUND OUT OF LIMITS. AREA FOUND TO BE SEVERE INTERGRANULAR CORROSION.SDR CA131230003Indicator · failed(CAN) DURING CRUISE OIL PRESSURE FLICKERED ABOUT 5 PSI AND REDUCED TO JUST ABOVE 85 PSI AND STAYED THERE THROUGHOUT ALL POWER RANGES.SDR CA131223013Door · unlocked(CAN) REJECTED TAKEOFF AFTER STARTING THE ROLL. NO ASSISTANCE REQUIRED, PILOT INDICATED A DOOR INDICATION/ALARM. ACFT TAXIED BACK TO COMPANY AND DEPARTED A SHORT TIME LATER. NO IMPACT ON OPERATIONS. ACFT WAS INSPECTED AFTER OCCURRENCE AND NO DEFECTS FOUND.SDR CA131218008Circuit Breaker · melted(CAN) AFTER TAKEOFF, 10 MINUTES INTO FLIGHT SMOKE IN COCKPIT. RETURNED TO DESTINATION OF TAKEOFF. UPON MAINTENANCE INVESTIGATION FOUND SEVERAL WIRES MELTED FROM THE FLAP MOTOR SYSTEM. FURTHER INVESTIGATION REQUIRED, WILL UPDATE AT A LATER DATE. INITIAL INVESDR CA131206002Flap System · inoperative(CAN) FLAP SYSTEM INOPERATIVE, FOUND ON MORNING WALK AROUND. PILOT CYCLED FLAPS AND WHEN FLAPS WHERE RETURNED TO ZERO, THE FLAP PRIMARY MOTOR COULD BE HEARD RUNNING. FLAP SYSTEM WOULD NOT FUNCTION IN EITHER PRIMARY OR STANDBY SYSTEM.SDR CA131215006Blade · fractured(CAN) THE PILOT HEARS A LOUD NOISE AND STATED TO LOST POWER. THE PILOT USED THE EMERGENCY POWER LEVER WITHOUT SUCCESS. THE ENGINE SHUTDOWN AND THE PILOT TRIED TO RESTART IT WITHOUT SUCCESS. THE PILOT DECLARED AN EMERGENCY DUE TO AN ENGINE FAILURE AND HE DIVSDR HVUA20131118001Oil Cooler · bypassingPILOT REPORTED ENGINE OIL TEMP AT RED LINE. OAT WAS 20 DEGREES F. RETURNED TO BASE. FOUND VERNATHERM FACE NOT SEATING CORRECTLY. FOUND UNEVEN WEAR ON OIL COOLER VERNATHERM SEAT.SDR CA131201003Engine · distressed(CAN) THE PILOT REPORTED ENGINE DISTRESS AFTER JUST LEVELING OFF AT CRUISE, 6000 FT. THE PILOT HEARD A LOUD NOISE, THEN HEARD THE ENGINE WINDING DOWN WHILE EXPERIENCING LOSS OF POWER. THE PILOT TRIED TO RE-START THE ENGINE WITHOUT SUCCESS. THE PILOT PERFORMESDR CA131126001Coupling · cracked(CAN) WHILE TRANSFERRING ASSEMBLY ON A NEW ENGINE, SPLINED COUPLING WAS FOUND CRACKED. CRACK NOT EVIDENT ON FIRST SIGHT AND REQUIRED A LITTLE FORCE TO SPREAD FOR CRACK TO SHOW.SDR CA131118019Control Unit · failed(CAN) DURING A ROUTINE FLIGHT THE PILOT NOTICED THE THE STANDBY ALTERNATOR HAD FAILED. THE FLIGHT CONTINUED WITH OUT INCIDENT. MAINTENANCE REPLACED THE ACU AND THE SYSTEM WAS GROUND FUNCTION CHECKED SERVICEABLE.SDR 2013FA0000638Gearshaft · damagedDURING ROUTINE INSPECTION, FOUND AIR CONDITIONING DRIVE LEAKING OIL, REMOVED ACFT DRIVE AND FOUND GEAR SHAFT SPLINES, PN 3100450-01 AND DRIVEN GEAR SHAFT SPLINES, PN 2601267-1 COMPLETELY WORN BEYOND LIMITS, SPLINES ON BOTH DRIVE AND DRIVEN GEAR SHAFTS ALMOST GSDR 2013FA0000637Drive Shaft · damagedDURING ROUTINE INSPECTION, FOUND AIR CONDITIONING DRIVE LEAKING OIL, REMOVED ACFT DRIVE AND FOUND GEAR SHAFT SPLINES, AND DRIVEN GEAR SHAFT SPLINES, COMPLETELY WORN BEYOND LIMITS, SPLINES ON BOTH DRIVE AND DRIVEN GEAR SHAFTS ALMOST GONE.SDR MK9A11152013002Drive Shaft · damagedDURING ROUTINE INSPECTION FOUND AIR CONDITIONING DRIVE LEAKING OIL, REMOVED ACFT DRIVE AND FOUND GEAR SHAFT DRIVE SPLINES, AND DRIVEN GEAR SHAFT SPLINES, COMPLETELY WORN BEYOND LIMITS SPLINES ON BOTH DRIVE AND DRIVEN GEAR SHAFTS ALMOST GONE.SDR MK9A11152013001Gearshaft · damagedDURING ROUTINE INSPECTION, FOUND AIR CONDITIONING DRIVE LEAKING OIL, REMOVED ACFT DRIVE AND FOUND GEAR SHAFT DRIVE SPLINES, AND DRIVEN GEAR SHAFT SPLINES COMPLETELY WORN BEYOND LIMITS SPLINES ON BOTH DRIVE AND DRIVEN GEAR SHAFTS ALMOST GONE.SDR MTNA11132013001Master Cylinder · failedDURING TAXI, AFTER LANDING. THE LT BRAKE WENT TO THE FLOOR. PAUSED THEN PUMPED PEDAL. BRAKE EFFECTIVENESS RETURNED BUT FELT MUSHY. TROUBLESHOT SYSTEM, REPLACED LEFT BRAKE MASTER CYLINDER. LEAK AND OPS CHECKED GOOD IAW MM 32-41-00.SDR CA131118018Pump · noisy(CAN) THE PILOT NOTED THAT THE BOOST PUMP ON ENGINE START WAS "NOISY", BUT FUNCTIONING PROPERLY. MAINTENANCE REPLACED THE PUMP AND THE SYS WAS FUNCTION CHECKED SERVICEABLE.SDR CA131112014Regulator Valve · malfunctioned(CAN) AT ALTITUDE WITH BLEED AIR ON, TEMP CONTROL KNOB TO FULL HOT. VERY LIMITED AMOUNT OF HEATED AIR ENTERING CABIN. OUTSIDE AIR 19C SURFACE TEMPERATURE ON GROUND AROUND -6C. AT CRUISE ITT 610C. CABIN HEAT DOES NOT START FLOWING TILL APPROXIMATELY 15-20 SSDR CA131118017Indicator · erratic(CAN) ON GPS APPROACH, VFR CONDITIONS, THE PILOT NOTICED THAT THE FLIGHT COMMAND INDICATOR WAS OSCILLATION VERTICALLY PRIOR TO THE AUTO PILOT DISCONCERTING. THE APPROACH WAS CARRIED OUT MANUALLY WITH OUT INCONTINENT. MAINTENANCE REPLACED THE FLIGHT COMMAND INSDR AJAA2014F00027Transponder · failedUPON TAKEOFF THE PILOT NOTICED A BURNED ODOR IN THE COCK-PIT. ALL CIRCUIT BREAKERS WERE IN, NOTHING TRIPPED. PILOT NOTICED THAT THE TRANSPONDER WAS DISPLAYING A "FAILURE" ON THE SCREEN. TURNED POWER OFF TO TRANSPONDER, AND CAME BACK AROUND FOR A SAFE LANDINSDR EPUA20131107003Skin · crackedLEFT AILERON L/E SKIN CRACKED AT INBD BALANCE WEIGHT ATTACH POINT. R & R LT AILERON L/E SKIN IAW SRM 57-40-00 PARA 4(A) AND 51-40-00.SDR CMRR2013110718089Spar Cap · corrodedHORIZONTAL T/E SPAR CAPS, UPPER & LOWER, HAD CORROSION.SDR EPUA20131107002Structure · crackedLEFT AILERON L/E SKIN CRACKED AT OTBD BALANCE WEIGHT ATTACH POINT. R & R LT AILERON L/E SKIN IAW SRM 57-40-00, PARA 4(A) AND 51-40-00.SDR CA131101010Indicator · inoperative(CAN) ON ENGINE START UP AND TAXI THE PILOT NOTICED THE FLIGHT COMMAND INDICATOR NOT RESPONDING TO THE ACFT MOVEMENT. THE ACFT RETURNED TO THE BLOCKS AND MAINTENANCE REPLACED THE UNIT WITH AN O/H UNIT. THE SYSTEM FUNCTION CHECKED SERVICEABLE.SDR CA131101005Adc · failed(CAN) AHARS 1 FAIL MESSAGE ON G600 UPON START UP. X PRESENT OVER GS, TAS, OAT.SDR 201310310005Tube · separatedAFTER THREE HUNDRED AND THIRTY TWO LANDINGS, LANDED AT AIRPORT, TIRE WENT FLAT ON RAMP.SDR 201310310004Tube · separatedAFTER FOUR HUNDRED AND FORTY TWO LANDINGS, TIRE WENT FLAT WHILE PARKED.SDR 201310310003Tube · separatedAFTER ELEVEN LANDING, TAKE OFF OK, PILOT FELT TIRE GO FLAT ON LANDING ROLL, STOPPED ON RUNWAY.SDR 201310310002Tube · separatedAFTER NINTY FIVE LANDINGS, PILOT FELT THE TIRE GO FLAT WHILE ON TAXI AND PRE TAKE OFF ROLL. ABORTED TAKE OFF.SDR 201310310001Tube · separatedAFTER FIFTY SEVEN LANDINGS, TIRE WENT FLAT DURING LANDING ROLLOUT. ACFT TAXIED TO RAMP BEFORE COMPLETE DEFLATION.SDR CA131104022Compressor · seized(CAN) PER NEWS REPORTS, THE ACFT LANDED ON THE HIGHWAY FOLLOWING AN ENGINE POWER LOSS. THE LANDING WAS MADE SAFELY WITHOUT ANY COLLISIONS WITH CARS OR INJURIES TO THOSE ON BOARD. MFG WILL FOLLOW UP WITH THE ENGINE INVESTIGATION. UPDATE NR 1: IAW PILOT REPORT,SDR MK9A20131030001Structure · damagedFOLLOWING AN EMERGENCY LANDING, RT WING SUSTAINED DAMAGE WHEN THE RT WING STRUCK A ROADWAY SIGN. THE DAMAGE EXTENDS FROM WS 227 OUT TO WS 312, WING TIP. INITIAL INVESTIGATION REVEALS DAMAGE TO THE L/E SKIN, OUTER UPPER AND LOWER WING SKINS, NOSE RIBS, AND MAINSDR MK9A201310300001Engine · failedDURING CLIMB, ENGINE FAILED. AN EMERGENCY LANDING WAS SUCCESSFULLY CONDUCTED. NO INJURIES REPORTED.SDR EPUA20131107001Structure · crackedLEFT AILERON L/E SKIN CRACKED AT OTBD BALANCE WEIGHT ATTACH POINT. REPLACED AILERON ASSEMBLE WITH SERVICEABLE UNIT.SDR 2014F00023Boot · missingDURING CRUISE, PILOT NOTICE A VIBRATION WITHIN ACFT. ELECTED TO MAKE A PRECAUTIONARY LANDING. NOTICED ONE ONE OF THREE PROPELLER DE-ICE BOOTS MISSING FROM A BLADE. DETERMINED TO BE THE CAUSE OF THE VIBRATION.SDR HSYA2013101800013Trim System · malfunctionedFLIGHT 8573. DURING CLIMB OUT, ATTEMPTING TO TRIM ACFT VIA ELECTRIC TRIM BUT WHEEL WOULD NOT TURN. ATTEMPTED TO TURN TRIM WHEEL MANUALLY BUT WHEEL WOULD SNAP BACK TO STARTING POSITION. ELECTED TO RETURN TO DEPARTURE.SDR CA131021012Fuel Control · faulted(CAN) UPON REDUCING POWER FOR INITIAL DESCENT TO DESTINATION, THE ENGINE DID NOT REACT. THE PILOT REDUCED THE POWER LEVER TO FLIGHT IDLE AND STILL NO RESPONSE. HE THEN ELECTED TO RETURN TO THEIR MAINTENANCE BASE. ON SHORT FINAL, THE ENGINE WAS SHUTDOWN USISDR EPUA20131011002Fuel Control · defectiveENGINE STUCK AT HIGH POWER. POWER LEVER NON-RESPONSIVE, MADE EMERGENCY IDLE CUT-OFF LANDING. NO CONTAMINATION OF FCU INLET OR OUTLET FILTERS FOUND. NO CONTAMINATION OF P3 FILTER ASSY. DISCREPANCY DISCOVERED DURING LANDING. LANDING WAS ABORTED AND ACFT RETURNESDR MTNA10042013001Hose · separatedDURING TAXI OUT, THE PILOT`S RT BRAKE BECAME INOPERATIVE. AFTER TROUBLESHOOTING SYS A, RT BRAKE HOSE WAS FOUND SEPARATED FROM THE BRAKE CALIPER. THE HOSE AND CALIPER WAS REPLACED IAW CMM 32-00-00. THE SYS OPS CHECKED GOOD AND THE ACFT WAS RETURN TO SERVICESDR CA131102003Piston · scored(CAN) UPON ENGINE SHUTDOWN THE CREW NOTED OIL STREAKING DOWN THE BLADES FROM THE PROPELLER, MORE THAN NORMAL. THE PROPELLER WAS REMOVED AND SENT FOR REPAIR AND THE SHOP REPLACED THE PISTON AND SEALS DUE TO SCORING INSIDE FROM MFG. THE PROP WAS REINSTALLED ANSDR CA130909002Brake Sys · malfunctioned(CAN) UPON LANDING, LT BRAKE WAS FLAT. ACFT STOPPED WITH RT BRAKE AND REVERSE. AS STEERING IS LIMITED TO DIFFERENTIAL BRAKE ACFT HAD TO BE TOWED FROM RUNWAY. INVESTIGATION REVEALED A LOOSE BLEEDER SCREW ON NR 2 BRAKE ASSY. THE ACFT IS NOT EQUIPPED WITH BRAKSDR CA130907001Bolt · failed(CAN) TOP BOLT-ANCHOR, LT, SHEARED ON LANDING CAUSING WHEEL AND BRAKE ASSY TO LOCK. ACFT SKID ALONG RUNWAY CAUSING TIRE FAILURE. ACFT VEERED TO LT DUE TO SKID AND CAME TO REST OFF THE RUNWAY.SDR CA130909008Skin · cracked(CAN) DURING THE 1ST 200 HR INSPECTION A CRACK WAS DISCOVERED IN THE ELEVATOR SKIN COLOLATED WITH A STATIC WICK RIVET. STATIC WICK BASE REMOVED, PATCH INSTALLED IAW SRM 55-00-00 AND 51-00-00. STAIC WICK BASE RE-INSTALLED. SUBSEQUENT INSPECTION AT +10HRS HASSDR CA130903002Nut · missing(CAN) DURING CLIMB, THE OIL PRESSURE STARTED TO FLUCTUATE FROM GREEN TO YELLOW BAND. THE PILOT ELECTED TO RETURN TO DEPARTURE. THE TORQUE READING THEN STARTED FLUCTUATING. THE PILOT DECLARED AN EMERGENCY. HE REPORTED OIL SPRAYING ON THE WINDSHIELD AND SMOKE E
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