Textron 172S
Service difficulty reports · 1,104
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 = '172S' 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 = '172S' 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 N3XR202507250821Hinge · crackedDURING A ROUTINE INSPECTION, THE LOWER RUDDER HINGE FITTING WAS FOUND CRACKED ON THE LOWER PORTION AROUND EACH CORNER BETWEEN RIVET HOLESSDR N3XR202507250811Hinge · crackedDURING A ROUTINE INSPECTION, THE LOWER RUDDER HINGE FITTING WAS FOUND CRACKED ON THE LOWER PORTION AROUND EACH CORNER BETWEEN RIVET HOLESSDR N3XR202507240852Hinge · crackedDURING A ROUTINE INSPECTION, THE LOWER RUDDER HINGE FITTING WAS FOUND CRACKED ON THE LOWER PORTION AROUND EACH CORNER BETWEEN RIVET HOLESSDR 2025FA0000516Engine · auto shutdownAIRCRAFT AND CREW EXPERIENCED ENGINE ROUGHNESS AND THE ENGINE QUITTING WHILE IN FLIGHT. THE CREW AND AIRCRAFT MADE AN UNPOWERED SAFE LANDING AT KARR (HOME AIRPORT). INITIAL INSPECTION FOUND THAT THE PROP WAS FREEWHEELING WITH NO RESISTANCE. NR 3 CYLINDER HAD ASDR N3XR202507230842Hinge · crackedDURING A ROUTINE INSPECTION, THE LOWER RUDDER HINGE FITTING WAS FOUND CRACKED ON THE LOWER PORTION AROUND EACH CORNER BETWEEN RIVET HOLESSDR N3XR20250718475Hinge · crackedDURING A ROUTINE INSPECTION, THE LOWER RUDDER HINGE FITTING WAS FOUND CRACKED ON THE LOWER PORTION AROUND EACH CORNER BETWEEN RIVET HOLESSDR N3XR202507180476Hinge · crackedDURING A ROUTINE INSPECTION, THE LOWER RUDDER HINGE FITTING WAS FOUND CRACKED ON THE LOWER PORTION AROUND EACH CORNER BETWEEN RIVET HOLESSDR N3XR202507170462Hinge · crackedDURING A ROUTINE INSPECTION, THE LOWER RUDDER HINGE FITTING WAS FOUND CRACKED ON THE LOWER PORTION AROUND THE RIGHT CORNER BETWEEN RIVET HOLESSDR N3XR202507140897Hinge · crackedDURING A ROUTINE INSPECTION, THE LOWER RUDDER HINGE FITTING WAS FOUND CRACKED ON THE LOWER PORTION AROUND EACH CORNER BETWEEN RIVET HOLESSDR N3XR202507140468Hinge · crackedDURING A ROUTINE INSPECTION, THE LOWER RUDDER HINGE FITTING WAS FOUND CRACKED ON THE LOWER PORTION AROUND EACH CORNER BETWEEN RIVET HOLESSDR N3XR202507140453Hinge · crackedDURING A ROUTINE INSPECTION, THE LOWER RUDDER HINGE FITTING WAS FOUND CRACKED ON THE LOWER PORTION AROUND EACH CORNER BETWEEN RIVET HOLESSDR N3XR202507150001Hinge · crackedDURING A ROUTINE INSPECTION, THE LOWER RUDDER HINGE FITTING WAS FOUND CRACKED ON THE LOWER PORTION AROUND EACH CORNER BETWEEN RIVET HOLESSDR 2025FA0000496Bushing · looseRIGHT MAIN GEAR ATTACH BUSHING P/N 0541202-4 LINER BECAME DISBONDED CREATING PLAY IN THE GEAR LEG. THIS AIRCRAFT IS OUTSIDE THE S.N. RANGE OF SEL-32-08 YET HAS THE SAME PROBLEM. THE FAILED BUSHING WAS INSTALLED ON 11/19/2024 AND HAD 291 HOURS IN SERVICE.SDR N3XR20250710002Hinge · crackedDURING A ROUTINE INSPECTION, THE LOWER RUDDER HINGE FITTING WAS FOUND CRACKED ON THE LOWER PORTION AROUND EACH CORNER BETWEEN RIVET HOLESSDR N3XR202507100001Hinge · crackedDURING A ROUTINE INSPECTION, THE LOWER RUDDER HINGE FITTING WAS FOUND CRACKED ON THE LOWER PORTION AROUND EACH CORNER BETWEEN RIVET HOLESSDR N3XR202507090001Hinge · crackedDURING A ROUTINE INSPECTION, THE LOWER RUDDER HINGE FITTING WAS FOUND CRACKED ON THE LOWER PORTION AROUND EACH CORNER BETWEEN RIVET HOLESSDR N3XR202507090003Hinge · crackedDURING A ROUTINE INSPECTION, THE LOWER RUDDER HINGE FITTING WAS FOUND CRACKED ON THE LOWER PORTION AROUND EACH CORNER BETWEEN RIVET HOLESSDR N3XR202507090002Hinge · crackedDURING A ROUTINE INSPECTION, THE LOWER RUDDER HINGE FITTING WAS FOUND CRACKED ON THE LOWER PORTION AROUND EACH CORNER BETWEEN RIVET HOLESSDR 2025FA0000400Valve Guide · cokedCREW REPORTED ROUGH RUNNING ENGINE/VIBRATION IN CRUISE FLIGHT LASTING 2-3 MINUTES ALONG WITH A # 2 CYLINDER EGT FLUCTUATION. TROUBLESHOT PROBLEM TO FIND # 2 CYLINDER EXHAUST VALVE STICKING.SDR 2025FA0000384Indication Sys · erraticENGINE OIL PRESSURE INDICATION ERRATIC. ONLY FLUCTUATES IN FLIGHT. STEADY DURING GROUND OPERATIONS.SDR 2025FA0000357Piston · cloggedRIGHT BRAKE LOCKED UP WHEN TAXIING TO RUNWAY, AIRCRAFT WENT INTO THE GRASS. NO DAMAGE TO AIRCRAFT.SDR 2025FA0000318Diode · failedTHIS HAS BEEN A RECURRING ISSUE SEEN IN THIS SHOP, BY THIS REPORTER. THE FOLLOWING WAS ORIGINALLY DISCOVERED ON OTHER AIRCRAFT BY COMPLYING WITH AD93-05-06. WHILE THE AIRCRAFT IN QUESTION (172R AND 172S MODELS) COME FROM THE FACTORY WITH THE DIODE, CURIOSITYSDR 2025FA0000296Exhaust Valve · stuckEXTREME VIBRATION OF AIRCRAFT ENGINE AFTER START UP. TROUBLESHOT AND FOUND #4 CYLINDER EXHAUST VALVE STUCK OPENSDR 2026FA0000187Bulkhead · crackedSPINNER BULKHEAD DISCOVERED CRACKED AFTER A COMPANY MAINT SAFETY STAND DOWN WHEN OTHERS IN OUR FLEET WERE FOUND CRACKED USING MAGNIFICATION. SINCE THE DISCOVERY ON 4/18/25. THIS ACFT HAS HAD 7 BULKHEAD REPLACEMENTS. AVERAGE TIME BETWEEN BULKHEADS VARIED BETWSDR 2026FA0000185Bulkhead · crackedINSPECTED SPINNER BULKHEAD FOR CRACKS DURING A FLEET SAFETY STAND DOWN AFTER DISCOVERING CRACKS IN SPINNER BULKHEADS OF OUR OTHER AIRCRAFT. CRACKS ARE VERY HARD TO SEE VISUALLY WITH THE NAKED EYE. USING A 10X MAGNIFIER AND KNOWING WHERE TO LOOK THAT RADIATESDR 2025FA0000277Bushing · failedFOUND DURING FIRST 100HR INSPECTION RIGHT LANDING GEAR BUSHING COMPLETELY WORN/ BLOWN OUT WITH NO INDICATIONS OF A HARD LANDING TO CAUSE THIS. DEFECTIVE MAIN LANDING GEAR BUSHING HAVE BEEN AN ONGOING TREAD WITH THE LAST FEW YEARS MODELS OF 172S.SDR 2025FA0000275Control Cable · brokenAILERON CARRY THROUGH CABLE HAS BROKEN STRANDS IN THE LEFT WING AT STATION 71.125.SDR IKBR2025041400264Elec Connector · failedCREW REPORTS TEMPORARY OIL PRESSURE LOSS ON APPROACH. ALL OTHER ENGINE INDICATIONS WERE NORMAL. UPON LANDING OIL PRESSURE RETURNED TO NORMAL. MECHANICS INSPECTED ENGINE. NO DEFECTS WERE NOTED. AVIONICS TECHNICIAN REPLACED THE OIL PRESSURE TRANSDUCER ELECTRICALSDR 2026FA0000182A/C Pack · crackedDURING A COMPANY SAFETY STAND DOWN FOR SPINNER BULKHEAD CRACKS.. FOUND SPINNER BULKHEAD CRACKS AT PROPELLER BOLT HOLES. CRACKS ARE HARD TO SEE WITH VISUAL EYE. CAN BE SEEN WITH 10X MAGNIFIER. BULKHEAD P/N: 0552231-1SDR 2025FA0000218Engine · power lossWHILE IN STRAIGHT AND LEVEL FLIGHT PILOT REPORTED THE ENGINE RPM REDUCED SIGNIFYINGLY RESULTING IN POWER LOSS. AFTER A BRIEF TIME THE ENGINE RPM BEGAN TO OPERATE NORMALLY AND POWER WAS RESTORED. PILOT LANDED WITHOUT INCIDENT. TROUBLESHOOTING COULD NOT DUPLISDR 2025FA0000206Propeller · brokenN500GP LINED UP CENTERLINE ON RWY 05 @ KDYL, APPLIED TAKEOFF POWER, APPROXIMATELY 30-50FT ON ROLLOUT EXPERIENCED SUDDEN VIBRATION, PULLED POWER AND EXITED RWY AT NEAREST TAXIWAY. SHUT DOWN AND VISUALLY INSPECTED AIRCRAFT. NOTIFIED MAINTENANCE.SDR 2025FA0000146Strut · brokenAIRCRAFT WAS ON THE RUNWAY, HOLDING POSITION WITH BRAKES ON IN ORDER TO PERFORM SHORT FIELD TAKE OFF PROCEDURE. THE STUDENT PILOT, UNDER GUIDANCE OF THE CFI, RELEASED THE BRAKES AND THE RIGHT WHEEL GRABBED MOMENTARILY, AS THE LEFT WHEEL STARTED TO MOVE FORWARDSDR N3XR202502280001Seal · failedFUEL WAS DISCOVERED IN ENGINE OIL. INSPECTION REVEALED THAT THE FUEL PUMP LW-15473 SEAL HAD FAILED AND LEAKED INTO THE OIL. THE ENGINE WAS CHANGED.SDR 2025FA0000135Muffler · crackedCREW ALERTED OF CARBON MONOXIDE PRESENT FROM G1000 WARNING. SHUTOFF CABIN HEAT AND OPENED WINDOWS. RETURNED TO BLOCK. VISUAL INSPECTION OF ENGINE MUFFLER FOUND CRACKED.SDR 2025FA0000134Muffler · crackedCREW REPORTS EXHAUST SMELL IN CABIN. VISUAL INSPECTION FOUND MUFFLER CRACKED.SDR 2025FA0000133Cylinder Head · crackedENGINE CYLINDER #2 CRACKED ACROSS COOLING FINS. CREW NOTICED LOSS OF POWER/SHUDDER. BURNING SMELL COMING THROUGH CABIN AIR VENTS.SDR 2025FA0000069Fuel Control · failedDEFECTIVE PRECISION FUEL SERVO CAUSED LOSS OF POWER AND ENGINE SHUT DOWN IN FLIGHT. AIRCRAFT ABLE TO LAND WITH NO DAMAGES OR INJURIES. NEWLY OVERHAULED BY PRECISION AIRMOTIVE WO# I1D3E WITH 11 HRS SINCE OVERHAUL.SDR 2025FA0000143Bushing · looseLEFT MAIN GEAR ATTACH BUSHING P/N 0541202-4 LINER BECAME DISBONDED CREATING PLAY IN THE GEAR LEG. THIS AIRCRAFT IS OUTSIDE THE S.N. RANGE OF SEL-32-08 YET HAS THE SAME PROBLEM.SDR 2025FA0000142Bushing · looseLEFT MAIN GEAR ATTACH BUSHING P/N 0541202-4 LINER BECAME DISBONDED CREATING PLAY IN THE GEAR LEG. THIS AIRCRAFT IS OUTSIDE THE S.N. RANGE OF SEL-32-08 YET HAS THE SAME PROBLEM.SDR VLAR20241211001Control Cable · brokenAUTOPILOT FAILED, WILL HOLD ALTITUDE, WILL NOT TRACK HEADING BUT OR NAV TRACK. SQUAWK WAS ENTERED ON 12/5/2024 AT 2117, SQUAWK UPDATED ON 12/06/2024.REMOVED ACCESS PANELS ON RH WING, FOUND CABLE PN 0522647-3 BROKEN.THE CABLE HAS TWO PARTS: A SHORT CABLE (PN: 0SDR 2024FA0000940Bushing · looseRIGHT MAIN GEAR ATTACH BUSHING P/N 0541202-4 LINER BECAME DISBONDED CREATING PLAY IN THE GEAR LEG. THIS AIRCRAFT IS OUTSIDE THE S.N. RANGE OF SEL-32-08 YET HAS THE SAME PROBLEM. THIS BUSHING HAD BEEN REPLACED AT THE LAST 100HR INSPECTION, IT LASTED 100HRS.SDR N3XR20241204002Transducer · fluctuatesDURING TAXI, NOTED OIL PRESSURE NOT WITHIN THE GREEN AT 1000 RPM. DURING RUN-UP, OIL PRESSURE ENTERED THE GREEN BUT FLUCTUATED BETWEEN THE FIRST 1/4 OF THE GREEN. AFTER RUN-UP WHEN THROTTLE WAS REDUCED BACK TO 1000, OIL PRESSURE 47 (TEMP 195). THE OIL PRESSURESDR N3XR20241204001Transducer · fluctuatesDURING CRUISE FLIGHT THE CREW OBSERVED OIL PRESSURE FLUCTUATIONS. THE OIL PRESSURE TRANSDUCER WAS REPLACED AND CORRECTED THE PROBLEM.SDR 2024FA0000865Bushing · wornFOUND R/H MAIN LANDING GEAR LEG BUSHING WORN/LOOSE.SDR 2024FA0000863Bushing · wornFOUND R/H MAIN LANDING GEAR LEG BUSHING WORN/LOOSE.SDR 2024FA0000809Packing · leakingUPON REMOVAL OF VENTURI FOUND EVIDENCE OF FUEL BETWEEN VENTURI BODY AND SERVO BODY AS WELL AS UNDER THE O-RINGS IN THE O-RING GROOVES. FUEL EVIDENCE WAS ALSO FOUND UNDER THE "G" PLUG. INSPECTION PROMPTED BY CESSNA FLEET GROUNDING FOLLOWING AN UNCONTROLLED IN-FSDR 2024FA0000808Packing · leakingUPON REMOVAL OF VENTURI FOUND EVIDENCE OF FUEL BETWEEN VENTURI BODY AND SERVO BODY AS WELL AS UNDER THE O-RINGS IN THE O-RING GROOVES. FUEL EVIDENCE WAS ALSO FOUND UNDER THE "G" PLUG. INSPECTION PROMPTED BY CESSNA FLEET GROUNDING FOLLOWING AN UNCONTROLLED IN-SDR 2024FA0000805Packing · leakingUPON REMOVAL OF VENTURI FOUND EVIDENCE OF FUEL BETWEEN VENTURI BODY AND SERVO BODY AS WELL AS UNDER THE O-RINGS IN THE O-RING GROOVES. FUEL EVEIDENCE WAS ALSO FOUND UNDER THE "G" PLUG. INSPECTION PROMPTED BY CESSNA FLEET GROUNDING FOLLOWING AN UNCONTROLLED IN-SDR 2024FA0000804Packing · leakingUPON REMOVAL OF VENTURI FOUND EVIDENCE OF FUEL BETWEEN VENTURI BODY AND SERVO BODY AS WELL AS UNDER THE O-RINGS IN THE O-RING GROOVES. FUEL EVIDENCE WAS ALSO FOUND UNDER THE "G" PLUG. INSPECTION PROMPTED BY CESSNA FLEET GROUNDING FOLLOWING AN UNCONTROLLED IN-FSDR 2024FA0000803Packing · leakingUPON REMOVAL OF VENTURI FOUND EVIDENCE OF FUEL BETWEEN VENTURI BODY AND SERVO BODY AS WELL AS UNDER THE O-RINGS IN THE O-RING GROOVES. FUEL EVIDENCE WAS ALSO FOUND UNDER THE "G" PLUG. INSPECTION PROMPTED BY CESSNA FLEET GROUNDING FOLLOWING AN UNCONTROLLED IN-F
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