Cessna 172S

Service difficulty reports · 1,104

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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"

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SDR N3XR202610130001Control Unit · burnedTHE ALTERNATOR CIRCUIT BREAKER POPPED AFTER A PREVIOUS RESET. THE ACU (ALTERNATOR CONTROL UNIT) P/N-AC2101, S/N-Y59830 FAILED. INSTALLED A NEW ACU, AND THE FUNCTION CHECK PASSED.Oct 9, 2026 · N923ER · Cessna 172S · AC Generator-AlternatorSDR 2026FA0000749Propeller · misinstalledPROPELLER INSTALLED INCORRECTLY AT THE FACTORY, INCORRECT CLOCKING CAUSING PROPELLER BUSHINGS TO BACK OUT: THE PROPELLER CLOCKED INCORRECTLY WITH #1 CYLINDER AT TOP DEAD CENTER. THE FACTORY SAFETY CABLES SHOWING THIS PROP HASN'T BEEN REMOVED SINCE TAKING DELISep 21, 2026 · N848FG · Cessna 172S · Propeller AssemblySDR 2026FA0000751Bushing · defectiveTHE RIGHT LANDING GEAR LEG BUSHING WHICH SECURES THE LEG TIGHTLY TO THE AIRFRAME STRUCTURE HAD A DELAMINATED BUSHING LINER WHICH COMPLETELY WORKED ITSELF OUT OF THE BUSHING. THE LANDING GEAR LEG WAS FLOPPING AROUND INSIDE THIS BUSHING.Sep 10, 2026 · N23177 · Cessna 172S · Main Landing Gear Attach SectionSDR 2026FA0000750Bushing · defectiveTHE LEFT LANDING GEAR LEG BUSHING WHICH SECURES THE LEG TIGHTLY TO THE AIRFRAME STRUCTURE HAD A DELAMINATED BUSHING LINER WHICH COMPLETELY WORKED ITSELF OUT OF THE BUSHING. THE LANDING GEAR LEG WAS FLOPPING AROUND INSIDE THIS BUSHING.Sep 10, 2026 · N23177 · Cessna 172S · Main Landing Gear Attach SectionSDR 2026FA0000766Bushing · defectiveTHE RIGHT LANDING GEAR LEG BUSHING WHICH SECURES THE LEG TIGHTLY TO THE AIRFRAME STRUCTURE HAD A DELAMINATED BUSHING LINER. WITHOUT THE LINER THE GEAR LEG IS NOT TIGHTLY SECURED TO THE AIRFRAME STRUCTURE, INSTEAD IT WILL FLOP AROUND.Sep 9, 2026 · N25152 · Cessna 172S · Main Landing Gear Attach SectionSDR 2026FA0000684Seal · failedAFTER COMPLETION OF THE ANNUAL INSPECTION, WE PERFORMED A POST INSPECTION RUN. DURING IDLE WE CHECKED EACH MAGNETO AND FOUND THAT THE ENGINE RAN SIGNIFICANTLY ROUGHER ON THE LEFT MAGNETO THAN THE RIGHT MAGNETO. AT HIGHER RPM OPERATION WAS NORMAL. REMOVED LEFSep 5, 2026 · N225WS · Cessna 172S · Magneto/DistributorSDR N3XR2026090100002Contactor · burnedALTERNATOR FAILED ON THE FINAL APPROACH WITH IGN PWR OFF ANNUNCIATOR. IP RECYCLED SWITCHES, BUT THE ANNUNCIATOR STILL EXISTED. REMOVED AND REPLACED CONTACTOR P/N: X61-0029 WITH NEW. THIS AIRCRAFT IS EQUIPPED WITH STC# SA02006CH: AIR CONDITIONING.Sep 1, 2026 · N870ER · Cessna 172S · DC Generator-AlternatorSDR 2026FA0000767Bushing · defectiveTHE RIGHT LANDING GEAR LEG BUSHING WHICH SECURES THE LEG TIGHTLY TO THE AIRFRAME STRUCTURE HAD A DELAMINATED BUSHING LINER. WITHOUT THE LINER THE GEAR LEG IS NOT TIGHTLY SECURED TO THE AIRFRAME STRUCTURE, INSTEAD IT WILL FLOP AROUND.Aug 27, 2026 · N25122 · Cessna 172S · Main Landing Gear Attach SectionSDR 2026FA0000754Bushing · defectiveTHE LEFT LANDING GEAR LEG BUSHING WHICH SECURES THE LEG TIGHTLY TO THE AIRFRAME STRUCTURE HAD A DELAMINATED BUSHING LINER. WITHOUT THE LINER THE GEAR LEG IS NOT TIGHTLY SECURED TO THE AIRFRAME STRUCTURE, INSTEAD IT WILL FLOP AROUND.Aug 21, 2026 · N25115 · Cessna 172S · Main Landing Gear Attach SectionSDR 2026FA0000755Bushing · defectiveTHE RIGHT LANDING GEAR LEG BUSHING WHICH SECURES THE LEG TIGHTLY TO THE AIRFRAME STRUCTURE HAD A DELAMINATED BUSHING LINER. WITHOUT THE LINER THE GEAR LEG IS NOT TIGHTLY SECURED TO THE AIRFRAME STRUCTURE, INSTEAD IT WILL FLOP AROUND.Aug 18, 2026 · N26110 · Cessna 172S · Main Landing Gear Attach SectionSDR 2026FA0000756Bushing · defectiveTHE LEFT LANDING GEAR LEG BUSHING WHICH SECURES THE LEG TIGHTLY TO THE AIRFRAME STRUCTURE HAD A DELAMINATED BUSHING LINER. WITHOUT THE LINER THE GEAR LEG IS NOT TIGHTLY SECURED TO THE AIRFRAME STRUCTURE, INSTEAD IT WILL FLOP AROUND.Aug 14, 2026 · N23176 · Cessna 172S · Main Landing Gear Attach SectionSDR N3XR2026090100001Contactor · burnedBUSS E & M VOLTS AT 24.2 AFTER ENGINE START. NO CHANGE IN VOLTAGE AT ANY POWER SETTING. BATTERY AMPS DISCHARGE -7 AT ALL POWER SETTINGS. R & R ALTERNATOR 24-VOLT CONTACTOR R & R ACU WITH NEW.Aug 8, 2026 · N813ER · Cessna 172S · DC Generator-AlternatorSDR 2026FA0000768Bushing · defectiveTHE LEFT LANDING GEAR LEG BUSHING WHICH SECURES THE LEG TIGHTLY TO THE AIRFRAME STRUCTURE HAD A DELAMINATED BUSHING LINER. WITHOUT THE LINER THE GEAR LEG IS NOT TIGHTLY SECURED TO THE AIRFRAME STRUCTURE, INSTEAD IT WILL FLOP AROUND.Aug 7, 2026 · N24251 · Cessna 172S · Main Landing Gear Attach SectionSDR 2026FA0000757Bushing · defectiveTHE LEFT LANDING GEAR LEG BUSHING WHICH SECURES THE LEG TIGHTLY TO THE AIRFRAME STRUCTURE HAD A DELAMINATED BUSHING LINER. WITHOUT THE LINER THE GEAR LEG IS NOT TIGHTLY SECURED TO THE AIRFRAME STRUCTURE, INSTEAD IT WILL FLOP AROUND.Aug 5, 2026 · N1730S · Cessna 172S · Main Landing Gear Attach SectionSDR 2026FA0000618Pump · failedENGINE DRIVEN FUEL PUMP FAILURE ALLOWED FUEL TO FLOOD ENGINE CRANKCASE. FOUND ON GROUND BEFORE FLIGHT.Aug 4, 2026 · N190LP · Cessna 172S · Engine Fuel PumpSDR 2026FA0000758Bushing · defectiveTHE RIGHT LANDING GEAR LEG BUSHING WHICH SECURES THE LEG TIGHTLY TO THE AIRFRAME STRUCTURE HAD A DELAMINATED BUSHING LINER. WITHOUT THE LINER THE GEAR LEG IS NOT TIGHTLY SECURED TO THE AIRFRAME STRUCTURE, INSTEAD IT WILL FLOP AROUND.Jul 17, 2026 · N22806 · Cessna 172S · Main Landing Gear Attach SectionSDR 2026FA0000591Bushing · delaminatedDURING 100HR INSPECTION FOUND LANDING GEAR BUSHING DELAMINATED AND SEPARATED FROM METAL. NO DAMAGE TO LANDING GEAR LEG WAS FOUND BUT UNSURE WHEN BUSHING FAILED BETWEEN THIS AND LAST 100HR. PICTURES AVAILABLE.Jul 16, 2026 · N26BQ · Cessna 172S · Main Landing GearSDR 2026FA0000759Bushing · defectiveTHE LEFT LANDING GEAR LEG BUSHING WHICH SECURES THE LEG TIGHTLY TO THE AIRFRAME STRUCTURE HAD A DELAMINATED BUSHING LINER. WITHOUT THE LINER THE GEAR LEG IS NOT TIGHTLY SECURED TO THE AIRFRAME STRUCTURE, INSTEAD IT WILL FLOP AROUND.Jul 15, 2026 · N24268 · Cessna 172S · Main Landing Gear Attach SectionSDR 2026FA0000590Bushing · delaminatedDURING 100HR INSPECTION FOUND LANDING GEAR BUSHING DELAMINATING FROM METAL SURFACE. TEXTRON RELEASED SEL-32-08R1 FOR WHICH THIS AIRCRAFT IS NOT INCLUDED.Jul 15, 2026 · N25BQ · Cessna 172S · Main Landing Gear Attach SectionSDR 2026FA0000592Bushing · delaminatedBOTH LANDING GEAR BUSHING FOUND DELAMINATED DURING 100HR INSPECTION.Jul 12, 2026 · N636EM · Cessna 172S · Fuselage, Landing Gear Attach FittingsSDR 2026FA0000761Bushing · defectiveTHE RIGHT LANDING GEAR LEG BUSHING WHICH SECURES THE LEG TIGHTLY TO THE AIRFRAME STRUCTURE HAD A DELAMINATED BUSHING LINER. WITHOUT THE LINER THE GEAR LEG IS NOT TIGHTLY SECURED TO THE AIRFRAME STRUCTURE, INSTEAD IT WILL FLOP AROUND.Jul 10, 2026 · N25187 · Cessna 172S · Main Landing Gear Attach SectionSDR 2026FA0000760Bushing · defectiveTHE LEFT LANDING GEAR LEG BUSHING WHICH SECURES THE LEG TIGHTLY TO THE AIRFRAME STRUCTURE HAD A DELAMINATED BUSHING LINER. WITHOUT THE LINER THE GEAR LEG IS NOT TIGHTLY SECURED TO THE AIRFRAME STRUCTURE, INSTEAD IT WILL FLOP AROUND.Jul 10, 2026 · N25187 · Cessna 172S · Main Landing Gear Attach SectionSDR 2026FA0000519Cylinder · crackedPILOT REPORTED LOUD NOISE FROM ENGINE, SIGNIFICANT POWER LOSS, AND LOUD VIBRATIONS. PILOT LANDED AT A NEARBY AIRPORT WHERE MANTIENCE DISCOVERED A LARGE CRACK IN CYLINDER #2(HEAD SEPERATING FROM THE BARREL).Jun 15, 2026 · N5251Z · Cessna 172S · Reciprocating Engine Cylinder SectionSDR 2026FA0000762Bushing · defectiveTHE LEFT LANDING GEAR LEG BUSHING WHICH SECURES THE LEG TIGHTLY TO THE AIRFRAME STRUCTURE HAD A DELAMINATED BUSHING LINER. WITHOUT THE LINER THE GEAR LEG IS NOT TIGHTLY SECURED TO THE AIRFRAME STRUCTURE, INSTEAD IT WILL FLOP AROUND.Jun 10, 2026 · N25181 · Cessna 172S · Main Landing Gear Attach SectionSDR 2026FA0000769Bushing · defectiveTHE LEFT LANDING GEAR LEG BUSHING WHICH SECURES THE LEG TIGHTLY TO THE AIRFRAME STRUCTURE HAD A DELAMINATED BUSHING LINER. WITHOUT THE LINER THE GEAR LEG IS NOT TIGHTLY SECURED TO THE AIRFRAME STRUCTURE, INSTEAD IT WILL FLOP AROUND.Jun 3, 2026 · N25194 · Cessna 172S · Main Landing Gear Attach SectionSDR 2026FA0000770Bushing · defectiveTHE LEFT LANDING GEAR LEG BUSHING WHICH SECURES THE LEG TIGHTLY TO THE AIRFRAME STRUCTURE HAD A DELAMINATED BUSHING LINER. WITHOUT THE LINER THE GEAR LEG IS NOT TIGHTLY SECURED TO THE AIRFRAME STRUCTURE, INSTEAD IT WILL FLOP AROUND.May 29, 2026 · N26010 · Cessna 172S · Main Landing Gear Attach SectionSDR 2026FA0000471Shutoff Valve · leakingFUEL SHUT OFF VALVE NOT STOPPING FUEL COMPLETELY. FUEL DRIPPING FROM FUEL STRAINER DURING INSPECTION.May 29, 2026 · N25167 · Cessna 172S · Aircraft Fuel Distribution SystemSDR 2026FA0000437Stringer · bentAIRCRAFT FAILED THE INSPECTION CRITERIA OUTLINED IN TEXTRON SERVICE LETTER SEL-53-04, DATED JANUARY 14, 2026. BOTH UPPER STRINGERS IN THE TAILCONE ASSEMBLY (P/N'S 0512001-9 AND 0512001-10) HAVE BENDS IN EXCESS OF THE 0.040" LIMIT DESCRIBED IN THE SERVICE LETTEMay 27, 2026 · N369DA · Cessna 172S · Fuselage Main, Longeron/StringerSDR 2026FA0000436Stringer · bentAIRCRAFT FAILED THE INSPECTION CRITERIA OUTLINED IN TEXTRON SERVICE LETTER SEL-53-04, DATED JANUARY 14, 2026. BOTH UPPER STRINGERS IN THE TAILCONE ASSEMBLY (P/N'S 0512001-9 AND 0512001-10) HAVE BENDS IN EXCESS OF THE 0.040" LIMIT DESCRIBED IN THE SERVICE LETTEMay 27, 2026 · N129K · Cessna 172S · Fuselage Main, Longeron/StringerSDR 2026FA0000763Bushing · defectiveTHE RIGHT LANDING GEAR LEG BUSHING WHICH SECURES THE LEG TIGHTLY TO THE AIRFRAME STRUCTURE HAD A DELAMINATED BUSHING LINER. WITHOUT THE LINER THE GEAR LEG IS NOT TIGHTLY SECURED TO THE AIRFRAME STRUCTURE, INSTEAD IT WILL FLOP AROUND.May 21, 2026 · N25204 · Cessna 172S · Main Landing Gear Attach SectionSDR 2026FA0000771Bushing · defectiveTHE RIGHT LANDING GEAR LEG BUSHING WHICH SECURES THE LEG TIGHTLY TO THE AIRFRAME STRUCTURE HAD A DELAMINATED BUSHING LINER. WITHOUT THE LINER THE GEAR LEG IS NOT TIGHTLY SECURED TO THE AIRFRAME STRUCTURE, INSTEAD IT WILL FLOP AROUND.May 19, 2026 · N24249 · Cessna 172S · Main Landing Gear Attach SectionSDR 2026FA0000470Shutoff Valve · leakingFUEL SHUT OFF VALVE NOT STOPPING FUEL COMPLETELY. FUEL DRIPPING FROM FUEL STRAINER DURING INSPECTION.May 15, 2026 · N25158 · Cessna 172S · Aircraft Fuel Distribution SystemSDR 2026FA0000764Bushing · defectiveTHE LEFT LANDING GEAR LEG BUSHING WHICH SECURES THE LEG TIGHTLY TO THE AIRFRAME STRUCTURE HAD A DELAMINATED BUSHING LINER. WITHOUT THE LINER THE GEAR LEG IS NOT TIGHTLY SECURED TO THE AIRFRAME STRUCTURE, INSTEAD IT WILL FLOP AROUND.May 11, 2026 · N309TX · Cessna 172S · Main Landing Gear Attach SectionSDR 2026FA0000772Bushing · defectiveTHE RIGHT LANDING GEAR LEG BUSHING WHICH SECURES THE LEG TIGHTLY TO THE AIRFRAME STRUCTURE HAD A DELAMINATED BUSHING LINER. WITHOUT THE LINER THE GEAR LEG IS NOT TIGHTLY SECURED TO THE AIRFRAME STRUCTURE, INSTEAD IT WILL FLOP AROUND.Apr 22, 2026 · N25205 · Cessna 172S · Main Landing Gear Attach SectionSDR 2026FA0000435Stringer · bentAIRCRAFT FAILED THE INSPECTION CRITERIA OUTLINED IN TEXTRON SERVICE LETTER SEL-53-04, DATED JANUARY 14, 2026. BOTH UPPER STRINGERS IN THE TAILCONE ASSEMBLY (P/N'S 0512001-9 AND 0512001-10) HAVE BENDS IN EXCESS OF THE 0.040" LIMIT DESCRIBED IN THE SERVICE LETTEApr 21, 2026 · N82MH · Cessna 172S · Fuselage Main, Longeron/StringerSDR 2026FA0000285Throttle Cable · severedLOSS OF THROTTLE CONTROL IN FLIGHT, DUE TO SEVERED THROTTLE CABLE.Apr 21, 2026 · N454AG · Cessna 172S · Power LeverSDR 2026FA0000391Stiffener · shearedFLAP TRACK STIFFENERS THAT KEEP THE FLAP TRACKS STRAIGHT AND TRUE WERE FOUND TO BE SHEARED OFF AND/OR CRACKED.Apr 14, 2026 · N1057R · Cessna 172S · Wing Miscellaneous StructureSDR 2026FA0000358Stiffener · shearedFLAP TRACK STIFFENERS THAT KEEP THE FLAP TRACKS STRAIGHT AND TRUE WERE FOUND TO BE SHEARED OFF AND/OR CRACKEDApr 14, 2026 · N988BE · Cessna 172S · Trailing Edge FlapsSDR 2026FA0000355Stiffener · shearedFLAP TRACK STIFFENERS THAT KEEP THE FLAP TRACKS STRAIGHT AND TRUE WERE FOUND TO BE SHEARED OFF AND/OR CRACKEDApr 14, 2026 · N437SP · Cessna 172S · Trailing Edge FlapsSDR 2026FA0000441Stringer · bentAIRCRAFT FAILED THE INSPECTION CRITERIA OUTLINED IN TEXTRON SERVICE LETTER SEL-53-04, DATED JANUARY 14, 2026. BOTH UPPER STRINGERS IN THE TAILCONE ASSEMBLY (P/N'S 0512001-9 AND 0512001-10) HAVE BENDS IN EXCESS OF THE 0.040" LIMIT DESCRIBED IN THE SERVICE LETTEApr 10, 2026 · N91FF · Cessna 172S · Fuselage Main, Longeron/StringerSDR 2026FA0000438Stringer · bentAIRCRAFT FAILED THE INSPECTION CRITERIA OUTLINED IN TEXTRON SERVICE LETTER SEL-53-04, DATED JANUARY 14, 2026. BOTH UPPER STRINGERS IN THE TAILCONE ASSEMBLY (P/N'S 0512001-9 AND 0512001-10) HAVE BENDS IN EXCESS OF THE 0.040" LIMIT DESCRIBED IN THE SERVICE LETTEApr 6, 2026 · N46FF · Cessna 172S · Fuselage Main, Longeron/StringerSDR 2026FA0000442Stringer · bentAIRCRAFT FAILED THE INSPECTION CRITERIA OUTLINED IN TEXTRON SERVICE LETTER SEL-53-04, DATED JANUARY 14, 2026. BOTH UPPER STRINGERS IN THE TAILCONE ASSEMBLY (P/N'S 0512001-9 AND 0512001-10) HAVE BENDS IN EXCESS OF THE 0.040" LIMIT DESCRIBED IN THE SERVICE LETTEMar 19, 2026 · N9283A · Cessna 172S · Fuselage Main, Longeron/StringerSDR NX422026031600013Crankcase · gougedUPON DISASSEMBLY FOR ITS FIRST OVERHAUL, DAMAGE WAS FOUND ON THE LEFT HAND CRANKCASE HALF ON ALL FOUR THRU STUD BORE LOCATIONS. THE DAMAGE APPEARS TO BE A GOUGE WITH DISPLACED METAL JUST UNDER THE CYLINDER PADS JUST INSIDE THE THRU STUD BORES. SIMILAR DAMAGE OMar 13, 2026 · N923ER · Cessna 172S · Reciprocating Engine Power SectionSDR NX422026031600012Stud · damagedUPON DISASSEMBLY FOR IT'S FIRST OVERHAUL, DAMAGE WAS FOUND ON ONE OF THE THRU STUDS. THE DAMAGE APPEARS TO BE DIPLSACED STEEL UNDER THE THREADED PORTION ON THE SHOULDER OF THE THRU STUD. A RELEVANT INDICATION IS SEEN UNDER MAGNETIC PARTICLE INSPECTION. THE LEFMar 13, 2026 · N979ER · Cessna 172S · Reciprocating Engine Power SectionSDR NX422026031600011Crankcase · gougedUPON DISASSEMBLY FOR ITS FIRST OVERHAUL, DAMAGE WAS FOUND ON THE LEFT HAND CRANKCASE HALF TO THREE THRU STUD BORE LOCATIONS. THE DAMAGE APPEARS TO BE A GOUGE WITH DISPLACED METAL JUST UNDER THE CYLINDER PADS JUST INSIDE THE THRU STUD BORES. SIMILAR DAMAGE ON OMar 13, 2026 · N979ER · Cessna 172S · Reciprocating Engine Power SectionSDR 2026FA0000753Bushing · defectiveTHE RIGHT LANDING GEAR LEG BUSHING WHICH SECURES THE LEG TIGHTLY TO THE AIRFRAME STRUCTURE HAD A DELAMINATED BUSHING LINER. WITHOUT THE LINER THE GEAR LEG IS NOT TIGHTLY SECURED TO THE AIRFRAME STRUCTURE, INSTEAD IT WILL FLOP AROUND.Mar 10, 2026 · N23177 · Cessna 172S · Main Landing Gear Attach SectionSDR 2026FA0000752Bushing · defectiveTHE LEFT LANDING GEAR LEG BUSHING WHICH SECURES THE LEG TIGHTLY TO THE AIRFRAME STRUCTURE HAD A DELAMINATED BUSHING LINER. WITHOUT THE LINER THE GEAR LEG IS NOT TIGHTLY SECURED TO THE AIRFRAME STRUCTURE, INSTEAD IT WILL FLOP AROUND.Mar 10, 2026 · N23177 · Cessna 172S · Main Landing Gear Attach SectionSDR 2026FA0000440Stringer · bentAIRCRAFT FAILED THE INSPECTION CRITERIA OUTLINED IN TEXTRON SERVICE LETTER SEL-53-04, DATED JANUARY 14, 2026. BOTH UPPER STRINGERS IN THE TAILCONE ASSEMBLY (P/N'S 0512001-9 AND 0512001-10) HAVE BENDS IN EXCESS OF THE 0.040" LIMIT DESCRIBED IN THE SERVICE LETTEMar 6, 2026 · N928ZA · Cessna 172S · Fuselage Main, Longeron/StringerSDR 2026FA0000439Stringer · bentAIRCRAFT FAILED THE INSPECTION CRITERIA OUTLINED IN TEXTRON SERVICE LETTER SEL-53-04, DATED JANUARY 14, 2026. BOTH UPPER STRINGERS IN THE TAILCONE ASSEMBLY (P/N'S 0512001-9 AND 0512001-10) HAVE BENDS IN EXCESS OF THE 0.040" LIMIT DESCRIBED IN THE SERVICE LETTEMar 5, 2026 · N73MH · Cessna 172S · Fuselage Main, Longeron/StringerSDR 2026FA0000774Bushing · defectiveTHE LEFT LANDING GEAR LEG BUSHING WHICH SECURES THE LEG TIGHTLY TO THE AIRFRAME STRUCTURE HAD A DELAMINATED BUSHING LINER. WITHOUT THE LINER THE GEAR LEG IS NOT TIGHTLY SECURED TO THE AIRFRAME STRUCTURE, INSTEAD IT WILL FLOP AROUND.Mar 2, 2026 · N23175 · Cessna 172S · Main Landing Gear Attach Section
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