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 MTNA02231100002Engine · malfunctionedDURING CLIMB AT 10000 FT THE PILOT HEARD A LOUD BANG AND HAD A SEVERE VIBRATION. THE OIL PRESSURE DROPPED THE PILOT SHUT THE ENGINE DOWN AND FEATHERED THE PROP. THE PILOT MADE A SUCCESSFUL LANDING AT (MBAC) AT THE DIRECTION OF MIA. ATC,SDR CA110215007Transistor · failedA CUSTOMER SENT AUTOPILOT COMPUTER FOR REPAIR WITH THE DEFECT DESCRIPTION A/P WILL NOT DISCONNECT/DISENGAGE. BENCH TROUBLESHOOTING CONFIRMED THAT PITCH BOARD SOLENOID DRIVE TRANSISTOR Q211 WAS LEAKING CURRENT TO THE PITCH AND ROLL SOLENOID OUTPUTS J1922-3. TSDR N5C2011F00000Capacitor · failedAUTOPILOT FAILED DURING DESCENT, PILOT SMELLED ELECTRICAL ODOR/FUMES. PILOT SAW SMOKE COMING FROM AUTOPILOT ENGAGE BUTTON. PILOT PULLED AND SECURED AUTOPILOT CIRCUIT BREAKER, SMOKE CLEARED IMMEDIATELY. AN INTERNAL INVESTIGATION OF THE AUTOPILOT COMPUTER REVSDR 2011F00038Capacitor · burnedAUTOPILOT FAILED, PILOT SMELLED ELECTRICAL ODOR/FUMES. PILOT SAW SMOKE COMING FROM AUTOPILOT ENGAGE BUTTON. PILOT PULLED AND SECURED AUTOPILOT CIRCUIT BREAKER, SMOKE CLEARED IMMEDIATELY. AN INTERNAL INVESTIGATION OF THE AUTOPILOT COMPUTER REVEALED A BURNED SDR AXSA20120405004Anti-Ice System · failedPILOT TURNED ON THE TKS SYSTEM PRIOR TO ENTERING ICING CONDITIONS. STATED THAT IT WAS TAKING LONGER THAN NORMAL TO SECRETE THE TKS FLUID OUT OF THE PANELS. AFTER A FEW CYCLES THE RED WARNING LIGHT CAME ON FOLLOWED BY THE YELLOW CAUTION LIGHT TOGETHER. THE SDR HSYA817E001O-Ring · leakingSTRONG FUEL ODOR NOTED BY CREW DURING FLIGHT, ON POST FLIGHT, NOTED FUEL POOLED ON BOTTOM OF ENGINE COMPARTMENT AND STREAMED ALONG BOTTOM OF FUSELAGE. MX INSPECTED FUEL LINES AND FITTINGS, NOTED FUEL LEAKING FROM EDP FILTER ASSY. REMOVED AND FOUND O-RING DAMSDR CA110208022Bushing · loose(CAN) WING REAR ATTACH BOLT & ECCENTRIC BUSHING ROTATED WHICH LED TO A INCIDENCE ANGLE CHANGE ON THE R/H WING. AN INSPECTION OF THE ATTACH BOLT & BUSHINGS WAS CONDUCTED WITH NO DEFECTS FOUND. AN INSPECTION OF THE WING STRUCTURE, SKINS, FLAP SYSTEM & FUEL SYSTESDR CA110208001Engine · flamed out(CAN) ACCIDENT ON A CARGO FLIGHT, DURING APPROACH, THE PILOT COULD NOT REDUCE POWER BELOW 1400 FT-LB AND THE THROTTLE LEVER WAS UNRESPONSIVE. DECIDED TO RETURN. TWO UNSUCCESSFUL LANDING ATTEMPTS WERE MADE AND ON THE 3RD ATTEMPT, THE ENGINE FLAMED OUT. THE ACFTSDR CA110208002Engine · failed(CAN) IFSD/FORCED LANDING SHORTLY AFTER T/O, THE PILOT FELT VIBRATIONS IN HIS CONTROL COLUMN FOLLOWED BY A LOSS OF POWER. THE THROTTLE WAS RETARDED AND THE VIBRATION REDUCED. RE-ADVANCING THE THROTTLE RESULTED IN A MOMENTARY INCREASE OF POWER BEFORE EVERYTHINGSDR MTNA01111100001Switch · faultyWHILE EN ROUTE OF FLIGHT 8115 BQN-PLS THE ENGINE FIRE WARNING LIGHT ILLUMINATED FOR FIVE SECONDS, THEN WENT OUT. THE FLIGHT CONTUNED WITH NO OTHER PROBLEMS. THE MECHANIC CHECKED AND FOUND SEVERAL FIRE LOOP INSULATORS OUT OF ALIGMENT WITH THE CLIPS AND THE TESDR 2011FA0000052Shaft · failedNOTICING HIGH FAILURE RATE BETWEEN SHAFT PN 2601267-2 AND GEAR PN 3100450-01.SDR COEA2011010501752Indicator · failedMFR / ABORTED TAKEOFF: NR 1 ATTITUDE INDICATOR FAILED ON TAKEOFF. PILOT ABORTED TAKEOFF AND LANDED AND RETURNED TO RAMP WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED FLIGHT COMMAND INDICATOR.SDR BSYA2011001Regulator · failedPILOT NOTICED LT WINDOW SIDE POST GETTING HOT IN FLIGHT. MX R & R BLEED AIR REGULATOR, OPS CHECKS GOOD.SDR HSYA2010122110Controller · failedPRIOR TO STARTING AN ILS APPROACH, STBY PWR LIGHT ILLUMINATED. NOTED 3 OF BUSS 1 C/B'S HAD POPPED, ALL SYSTEMS FUCTIONED NORMAL. TURNED LIGHTS OFF & ANTI-ICE SYSTEM LEFT ON DUE TO ICING CONDITIONS. TURNED ON TAXI & LANDING LIGHTS BEFORE LANDING & SEVERAL ANNUNSDR CA101230010Skin · damagedRIVETS HOLDING LEADING EDGE OF AIRFOIL LOOSENED UP CAUSING AIR PRESSURE TO CATCH SKIN AND PEEL IT BACK BLOCKING AIRFLOW INTO ENGINE. PILOT REPORTED 300LBS TORQUE PRESSURE LOSS.SDR BSYA2010049Latch · out of adjustDOOR LIGHT (CARGO-DOOR) CAME ON JUST AFTER TAKEOFF OUT OF CLT, PILOT THEN RETURNED TO CLT. MAINTENANCE THEN ADJUSTED DOOR LATCH OPS CHECKS GOOD.SDR CA101209008Circuit Breaker · tripped(CAN) 35 MINUTES BEFORE LANDING, PILOT HAD A FIRE LIGHT INDICATION WITH NO AURAL WARNING, THE STANDBY POWER LIGHT IMMEDIATELY CAME ON AND ALL THE NR 1 & 2 BUSS CIRCUIT BREAKERS POPPED. MAINTENANCE WAS CONTACTED IMMEDIATELY AND SUGGESTED RESETTING ALL THE CIRCSDR COEA2010120301895Unknown · malfunctionedAIR TURNBACK: ON FLIGHT 7699 ON CLIMBOUT FROM BLI GENERATOR WENT OFF LINE, THEN STANDBY ELEC POWER INOP ILLUMINATED. BOTH STBY PWR CIRCUIT BREAKERS TRIPPED. RESET BREAKERS AND BREAKERS DID NOT TRIP. COULD NOT GET GENERATOR OR STBY PWR TO RESET. PILOT ELECTSDR FJT04061242Wheel · corrodedMX FOUND EXCESSIVE CORROSION IN THE CTR OF BOTH HALVES OF THE NOSE WHEEL ASSY, WHILE PERFORMING PHASE 1 THROUGH 4 INSP. DISASSEMBLY OF THE NOSE WHEEL ASSY REVEALED CORROSION BEYOND ACCEPTABLE LIMITS. BOTH NOSE WHEEL HALVES WERE REPLACED WITH NEW PARTS AND THSDR CA101130013Support · distortedDURING ANNUAL INSPECTION, IT WAS DISCOVERED THAT THE ELEVATOR DOWN STOP BRACKET WAS NOT FULLY INSTALLED FROM THE FACTORY. EIGHT RIVETS ON THE LOWER SUPPORT ASSEMBLY WERE NOT INSTALLED. THIS ALLOWED THE SUPPORT BRACKET TO BEND OUT OF PLACE AND AFFECTED TRAVELSDR CA101130003Powerplant · failedIFSD (SINGLE ENGINE) DURING CRUISE AT FL80, THE PILOT RECEIVED A CHIP DETECTOR WARNING FOLLOWED BY A DROP OF OIL PRESSURE TO ZERO. SMOKE WAS SEEN COMING OUT OF THE ENGINE COWLING. THE ENGINE WAS SHUT DOWN AND A FORCED LANDING WAS MADE ON AN UNAPPROVED RUNWAYSDR CA101116009Spar Cap · worn(CAN) WHILE COMPLETING AN UNRELATED REPAIR, THE AME`S NOTICED WEAR (FRETTING) DAMAGE TO THE UPPER REAR SPAR CAP. THIS APPEARS TO HAVE BEEN CAUSED DURING INITIAL MANUFACTURE. THE REAR RIB AT THAT LOCATION WAS RUBBING INTO THE RADIUS OF THE SPAR CAP. THE SRM SDR BSYA2010045Indicator · failedEN ROUTE, WHEN THE ATTITUDE INDICATOR FAILED. DIVERTED. MX R & R INDICATOR, OPS CHECKED GOOD.SDR COEA2010110401752Regulator · faultyFLT 8830 PDX TO MFR: DURING CLIMB, SMOKE AND ELECTRICAL ODOR APPEARED FROM PILOT SIDE CIRCUIT BREAKER PANEL. CREW DECLARED AN EMERGENCY AND LANDED IN EUG WITHOUT INCIDENT. MAINTENANCE INSPECTED CB, SWITCHES, RELAYS & WIRING FOR SIGNS OF BURNING. NO DISCREPSDR CA101102005Oil Filter · unserviceable(CAN) INNER CORE (SCREEN) UNSERVICEABLE (186.6 HOURS ON FILTER).SDR CA101118006Bracket · broken(CAN) WHILE THE A/C WAS DOWN FOR SCHEDULED MAINTENANCE, THE GUYS FOUND A BROKEN LOWER FLAP MOTOR BRACKET SUPPORT DURING PHASE 5 INSPECTION, THIS WAS FOUND VISUALLY. THE SUPPORT P/N IS 2611144-5. THERE WERE NO ISSUES WITH THE OPERATION OF THE FLAPS, NO BINDINSDR COEA2010101501899Mount · crackedGEG PHASE INSPECTION: MAJOR REPAIR: DURING MAINTENANCE INSPECTION FOUND ONE CRACK .250" IN LENGTH ON LT ENGINE MOUNT RING ASSEMBLY. MAINTENANCE REMOVED AND REPLACED ENGINE MOUNT RING ASSY IAW CESSNA 208 MM.SDR CA101014005Bridal Cable · failedAUTOPILOT LOST ROLL CONTROL. CREW DISENGAGED AUTOPILOT AND CONTINUED TO HOME BASE. ON TROUBLESHOOTING AUTOPILOT THE ROLL BRIDLE CABLE WAS FOUND TO BE BROKEN.SDR CA101019005Tube · leakingOIL PRESSURE LOSS WHILE PREPARING FOR APPROACH INTO DESTINATION AIRPORT, THE CREW NOTED A LOW OIL PRESSURE WARNING LIGHT WITH THE OIL PRESSURE GAGE READING SLIGHTLY BELOW 40PSI. THE POWER WAS REDUCED UNTIL THE WARNING EXTINGUISHED AND AN UNEVENTFUL LANDING FOLSDR CA101018002Engine · failedACCIDENT, THE ACFT APPARENTLY LOST POWER AND THE PILOT FORCED LANDED IN SMALL TREES. THERE WERE NO INJURIES. THE ACFT IS SUBSTANTIALLY DAMAGED. OFFER OF ASSISTANCE TO THE RUSSIAN AUTHORITIES IS BEING MADE. UPDATE NR 1: THE RUSSIAN AIR ACCIDENT AVIATION COMSDR CA101222007Starter Gen · failed(CAN) ON A FLIGHT THE PILOT NOTED THAT THE GENERATOR HAD FAILED. THE STARTER/GENERATOR WAS REPLACED AND NO FURTHER INCIDENT PREVAILED.SDR MTNA0922100002Cooling Fan · seizedWHILE EN ROUTE OF FLIGHT 8124 THE PILOT REPORTED A STRONG ELECTRICAL SMELL IN THE COCKPIT. THE PILOT DID A AIR TURN BACK TO SJU. THE AIRCRAFT LANDED WITHOUT INCIDENT. AFTER TROUBLESHOOTING THE MECHANIC FOUND THE AVIONICS COOLING FAN WOULD NOT ROTATE. THE FSDR COEA2010091002863Warning System · malfunctionedFLIGHT 7800 FROM PDT TO GEG: ON CLIMB IT WAS DISCOVERED THAT THE REAR CARGO DOOR WARNING ENUNCIATOR LIGHT CAME ON. PILOT LANDED BACK IN PDT AND OPENED AND RECLOSED THE DOOR. ENUNCIATOR LIGHT WENT OUT AND PILOT DEPARTED PDT AND ARRIVED IN GEG WITH NO INCIDENTSDR MTNA0910100001Brushes · wornDURING THE TAKEOFF ROLL THE AIRCRAFT LOST POWER DUE TO UN-COMMANDED FEATHERING OF THE PROPELLER. THE TAKEOFF WAS ABORTED. AFTER TROUBLESHOOTING THE MECHANIC FOUND A WORN BATA BRUSH THE PART WAS REPLACED. THE SYSTEM CHECKED GOOD AND THE AIRCRAFT WAS RETURNEDSDR BSYA2010041Regulator · faultyEN ROUTE FROM LCK TO DPA PILOT NOTICED DOOR FRAME NEXT TO WINDSHIELD WAS HOT TO THE TOUCH, THEN DIVERTED TO FWA. REMOVED AND REPLACED DEFECTIVE BLEED AIR REGULATOR OPS CHECKS GOOD.SDR CA100921002Engine · failedACCIDENT DURING A FLIGHT WITH FINAL DESTINATION, WHILE OVER THE SEA, THE ENGINE LOST POWER. AN EMERGENCY LANDING WAS MADE IN A SUGAR CANE FIELD. RESULTING IN HEAVY DAMAGE TO THE ACFT AND MINOR INJURIES TO ALL ON BOARD. OFFER OF ASSISTANCE TO THE FRENCH BEA SDR CA100913004Engine · failedACCIDENT DURING A FLIGHT WITH FINAL DESTINATION, WHILE OVER THE SEA, THE ENGINE LOST POWER. AN EMERGENCY LANDING WAS MADE IN A SUGAR CANE FIELD. RESULTING IN HEAVY DAMAGE TO THE ACFT AND MINOR INJURIES TO ALL ONBOARD. OFFER OF ASSISTANCE WILL BE MADE.SDR 2010FA0001063Case · brokenPILOT REPORTED TO MX THAT WITH THE THROTTLE LEVER AT THE GATE (FWD SIDE OF GATE) THE ENGINE WAS GOING INTO REVERSE. THE SUBSEQUENT INSP FOUND THE REVERSE ROPE CASING HAD BROKEN AT THE SWIVEL JOINT. THE REVERSE ROPE ITSELF WAS STILL ATTACHED.SDR CA100902002Starter Gen · failedGENERATOR FAILURE ON CLIMBOUT. STARTER GENERATOR REPLACED WITH O/H UNIT. ACFT GROUND RUN, DC GENERATION FUNCTION CHECK CARRIED OUT SERVICEABLE IAW MM 80-10-00.SDR MTNA0820100001Exhaust Duct · crackedTHE FIRE WARNING LIGHT CAME ON. THE LIGHT WENT OUT AFTER POWER WAS PULLED BACK, AFTER LANDING IN GND WITH OUT INCIDENT. THE MAINTENANCE PEOPLE FOUND A CRACKED EXHAUST DUCT. AFTER THE DUCT WAS REPLACED THE SYSTEM CHECKED GOOD AND THE AIRCRAFT WAS RETURNED TOSDR AXSA996FE8/18/10Control Unit · inoperativeFLIGHT WIG046A DEPARTED MHT-MVY NORMALLY. WHILE CLIMBING THRU 4500 FEET THE PILOT NOTED ELECTRICAL FUMES. THE PILOT DID NOT NOTICE SMOKE BUT ELECTED TO RETURN TO MHT AS A PRECAUTION AND LANDED WITHOUT INCIDENT. MAINTENANCE EVALUATED THE AIRCRAFT AND DETERMISDR MT92010F00000Switch · failedAFTER DEPARTING RUNWAY 19 AND AT AN ALTITUDE OF 300 FT, THE ENGINE WARNING LIGHT ILLUMINATED AND THE WARNING SIREN SOUNDED. THE PILOT MAINTAINED ALTITUDE; PULLED THE FIRE-WARNING BRAKER; AND EXECUTED A 270 DEGREE TURNBACK TO THE AIRPORT. NO EMERGENCY WAS DECSDR CA100713003Cone · unserviceable(CAN) INNER CONE UNSERVICEABLE (600 HRS ON 1000 HR FILTER) CONE OPENS UP AT JOINT.SDR BSYA2010033Light · malfunctionedPILOT SMELLED SMOKE IN COCKPIT SHORTLY AFTER TAKEOFF, THEN RETURNED TO OMA. MAINTENANCE FOUND PILOTS MAP LIGHT BULB PLASTIC AROUND BULB MELTING. REMOVED AND REPLACED BULB.SDR MTNA062810Fuel Control · unknownAFTER DEPARTURE FROM MIA THE PILOT EXPERIENCED A 400 POUND DECREASE IN ENGINE TORQUE ALONG WITH A DECREASE IN POWER AT 800FT AGL. THE PILOT DECLARED AN EMERGENCY AND AIR TURNBACK TO MIA. THE PILOT LANDED THE AIRCRAFT WITHOUT FURTHER INCIDENT.SDR MTNA 062810Fuel Control · malfunctionedAFTER DEPARTURE FROM MIA THE PILOT EXPERIENCED A 400 POUND DECREASE IN ENGINE TORQUE ALONG WITH A DECREASE IN POWER AT 800FT AGL. THE PILOT DECLARED AN EMERGENCY AND DID A AIR TURNBACK TO MIA. THE PILOT LANDED THE AIRCRAFT WITHOUT FURTHER INCIDENT.SDR BSYA2010031Audio Panel · intermittentAFTER TAKEOFF OUT OF PMU BOTH RADIO'S HAD WEAK RECEIVE. REMOVED AND REPLACED AUDIO PANEL, OPS CHECKS GOOD.SDR COEA2010061001720Indicator · faultyON FLIGHT 7690 ATB TO RBG: AFTER DEPARTURE FROM RBG THE ATTITUDE INDICATOR TUMBLED CONTINUOUSLY SHOWING 20 DEGREES NOSE UP WINGS LEVEL ATTITUDE. PILOT RETURNED TO AIRPORT AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE ATTITUDE INDICATOR. SDR CA100810001Fcu · inoperative(CAN) THE PILOT REPORTED THE ENGINE WAS HAVING HUNG START ISSUES, THE FCU WAS REPLACED AND THE TEARDOWN INSP REVEALED THAT THE MAIN BODY, GOVERNOR LEVER, CUT OFF LEVER, AND THE THROTTLE STOP LEVER BUSHINGS WERE WORN BEYOND LIMITS PN 3240658, 2523613, 2523646, SDR 2010FA0000586Spring · brokenPILOT FELT VIBRATION ON THE NOSE GEAR WHEEL. IT BOUNCES ABOUT 3 TIMES AND THE NOSE GEAR COLLAPSE. AFTER TOUCH DOWN, PILOT FELT VIBRATION ON NOSE WHEEL FOLLOWED BY 3 BOUNCES AFTER THAT NOSE GEAR ASSY DISPLACED FWD CAUSING THE PROPELLER TO HIT OR STRIKE THE NO
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