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.

SDR NX4R000017Control Cable · frayedDURING A ROUTINE INSP, THE TECH DISCOVERED THAT THE FORWARD ELEVATOR CONTROL CABLE PN-0510105-308 WAS FRAYED AND WORN AT FS 65.33.Jun 30, 2011 · N368ER · Cessna 172S · Elevator Control SystemSDR NX4R000014Control Cable · frayedTHE AILERON CABLE PN-0510105-364 WAS FRAYED AND WORN SHOWING BROKEN STRANDS AT FUSELAGE STATION 65.33 WHERE THE CABLES PASS THOUGH THE 3 CEILING MOUNTED NYLON PULLEYS.Jun 28, 2011 · N483ER · Cessna 172S · Aileron Control SystemSDR BGSR20110628001Cable · frayedCOMPLIED WITH SAIB: CE-11-36 (5-31-2011) ON FRAYED AILERON CABLES AND NOTED THAT AILERON BALANCE CABLE WAS WEARING AND FEW BROKEN STRANDS OF CABLE. REMOVED DEFECTIVE CABLE AND SERVICED WITH NEW PN: MC0510105-364 AND MC0510105364365 CABLE ASSEMBLIES IAW CHAPTEJun 23, 2011 · N2225A · Cessna 172S · Aileron Control SystemSDR NX4R000020Control Cable · frayedDURING A ROUTINE INSP, THE AILERON RT DIRECT CABLE, PN-0510105-360 WAS FOUND FRAYED WITH MANY BROKEN STRANDS WHERE IS PASSES THROUGH THE NYLON PULLEY (S394) IN THE CENTER CEILING AT FS 65.33.Jun 22, 2011 · N483ER · Cessna 172S · Aileron Control SystemSDR NX4R000018Control Cable · frayedDURING A ROUTINE INSP, THE AILERON LT DIRECT CABLE WAS FOUND FRAYED WITH MANY BROKEN STRANDS WHERE IS PASSES THROUGH THE NYLON PULLEY (S394) IN THE CENTER CEILING AT FS 65.33.Jun 21, 2011 · N368ER · Cessna 172S · Aileron Control SystemSDR NX4R000015Control Cable · frayedDURING A ROUTINE INSP THE AILERON RT DIRECT CABLE PN-0510105-364 WAS FOUND FRAYED WITH MANY BROKEN STRANDS WHERE IS PASSES THROUGH THE NYLON PULLEY (S394) IN THE CENTER CEILING AT FS 65.33.Jun 21, 2011 · N368ER · Cessna 172S · Aileron Control SystemSDR CA110620008Distributor Gear · looseAT ROUTINE 500 HR MAGNETO INSPECTION, THE DISTRIBUTOR FINGER OF THE DISTRIBUTOR GEAR WAS FOUND TO BE LOOSE - DISTRIBUTOR GEAR REPLACED.Jun 17, 2011 · Cessna 172S · Magneto/DistributorSDR OG5R20110714001Tire · deflatedLT MAIN TIRE WENT FLAT ON TAXI. RECURRING PROBLEM.Jun 17, 2011 · N536ND · Cessna 172S · TireSDR 2011FA0000388Tube · flatWHILE TAXIING, ACFT EXPERIENCES A FLAT TIRE ON THE LT MAIN GEAR AT THE END OF THE TAXIWAY. MX WAS NOTIFIED AND THE TIRE WAS REPLACED. HAVE BEEN EXPERIENCING SEVERAL OF THESE PROBLEMS AND WE HAVE BEEN INSTRUCTED BY OUR SAFETY DEPARTMENT TO SUBMIT SDR FORMS.Jun 17, 2011 · N536ND · Cessna 172S · Tire TubeSDR 2011FA0000431Alternator · failedCOMPLETE ELECTRICAL FAILURE IN CRUISE WITHOUT ANY INDICATION OR WARNING. PROBLEM TRACED TO FAULTY ALTERNATOR.Jun 16, 2011 · N4577 · Cessna 172S · DC Generator-AlternatorSDR NX4R000019Control Cable · frayedDURING A ROUTINE INSP THE AILERON RT DIRECT CABLE PN-0510105-364 WAS FOUND FRAYED WITH MANY BROKEN STRANDS WHERE IS PASSES THROUGH THE NYLON PULLEY (S394) IN THE CENTER CEILING AT FS 65.33.Jun 14, 2011 · N368ER · Cessna 172S · Aileron Control SystemSDR OG5R20110610001Tire · deflatedNOSE LANDING GEAR TIRE FLAT ON TAXI.Jun 10, 2011 · N546ND · Cessna 172S · TireSDR CA110610005Control Cable · wornSTAINLESS STEEL AILERON CABLES FOUND WORN AT FAIRLEAD IN RT WING ABOVE ROLL SERVO, AT FAIRLEAD IN LT WING, AND AT THE 3 SMALL PULLEYS IN THE CABIN CEILING. TT 1645, RT AILERON CABLES SHOWED THIS SAME PROBLEM AT ABOUT 600 TT, CABLES WERE REPLACED AND SDR SUBMITJun 7, 2011 · Cessna 172S · Aileron Control SystemSDR NX4R000021Control Cable · frayedDURING A ROUNTINE INSPECTION, THE LT AILERON PRIMARY CABLE, PN-0510105-360 WAS FOUND WORN AND FRAYED IN THE CABIN CEILING WHERE IT PASSES ACROSS THE 3 SMALL NYLON PULLEYS AT FS 65.33.Jun 2, 2011 · N483ER · Cessna 172S · Aileron Control SystemSDR OG5R20110601001Tire · deflatedFLAT NOSE WHEEL DURING TAXI.Jun 1, 2011 · N550ND · Cessna 172S · TireSDR CA110526001Transmitter · malfunctionedWE HAVE HAD SEVERAL REPORTS OF LOW FUEL LIGHTS COMING ON OR FLICKERING WHEN THE FUEL TANKS ARE FILLED TO THE MAX. THE FIX IS USUALLY REMOVING A FEW GALLONS OF FUEL FROM THE TANK. WE HAVE HAD SEVERAL PROBLEMS WITH THESE FUEL TRANSMITTERS OVER THE YEARS BUT MFMay 25, 2011 · Cessna 172S · Fuel Indicating SystemSDR NX4R000010Shaft · wornDURING AN INSPECTION, THE TECH NOTICED AN INDENTATION IN THE PILOT'S YOKE SHAFT. ALTHOUGH SMOOTH, IT WAS NOTICED THAT A SUBSTANTIAL AMOUNT OF THE WALL THICKNESS WAS WORN AWAY. IF SITTING IN THE CO-PILOT'S SEAT, THE WEAR WOULD BE LOCATED AT THE 6 O'CLOCK POSITApr 11, 2011 · N453ER · Cessna 172S · Control Column SectionSDR NX4R00009Shaft · wornDURING A PHASE INSP, THE TECH NOTICED A WORN AREA ON PILOT'S YOKE SHAFT AT THE 6 O'CLOCK POSITION WHERE THE SHAFT RIDES ON THE INSTRUMENT PANEL BEARING AREA. THE MFG STATES THAT A MAXIMUM WEAR OF .009" IS ALLOWED. THIS WEAR WAS ABOUT .019". IT IS A SUBSTANTIAApr 11, 2011 · N466ER · Cessna 172S · Control Column SectionSDR NX4R00008Shaft · wornDURING INSPECTION THE TECH NOTICED AN INDENTATION IN THE CO-PILOT'S YOKE SHAFT. ALTHOUGH SMOOTH, IT WAS NOTICED THAT A SUBSTANTIAL AMOUNT OF THE WALL THICKNESS WAS WORN AWAY. IF SITTING IN THE CO-PILOT'S SEAT, THE WEAR WOULD BE LOCATED AT THE 6 O'CLOCK POSITIMar 25, 2011 · N376ER · Cessna 172S · Control Column SectionSDR 2011FA0000259Master Switch · arcedTOWER STATED TRANSPONDER WASN'T SHOWING ALTITUDE. THERE WAS AN ALERT THAT STATED "TRANSPONDER 1 INOPERABLE--RETURN FOR SERVICE. USED SOFT KEY, IT SHOWED TRANSPONDER ON STANDBY. TRIED SWITCH IT TO ON, ALT OR GROUND, IT WOULD SWITCH BACK TO STANDBY AFTER A SEMar 24, 2011 · N1307A · Cessna 172S · Ignition SwitchingSDR 2011FA0000191Screw · looseDURING TRAINING FLIGHT STUDENT PILOT REPORTED HIS SEAT WOULD NOT LOCK IN POSITION. ACFT RETURNED TO BASE WITHOUT INCIDENT. UPON TROUBLESHOOTING OF PROBLEM MX FOUND THE ATTACHMENT SCREWS OF THE LT AND RT SEAT STOP PINS HAD BACKED OUT ALLOWING THEM TO BE DETACHMar 20, 2011 · N570ND · Cessna 172S · Flight Compartment EquipmentSDR 2011FA0000179Pump · leakingEVIDENCE OF OIL STREAMING DOWN BELLY TO TAIL. OIL NOTED DRIPPING FROM A DRAIN TUBE BELOW FIRE WALL. DRAIN TUBE CONNECTED TO AN OVERFLOW FITTING ON ENGINE MOUNTED MECHANICAL FUEL PUMP. PUMP R & R. PUMP CORE DISASSEMBLED & OIL FOUND LEAKING THROUGH 1ST OF 2 Mar 16, 2011 · N383TC · Cessna 172S · Magneto/DistributorSDR NX4R00006AControl Cable · wornDURING A 100 HR INSP, THE "UP" ELEVATOR CABLE WAS FOUND WORN AT FS-65.33. THE CABLE HAD MANY STRANDS WORN GREATER THAN 50 PERCENT THROUGH.Mar 14, 2011 · N490ER · Cessna 172S · Elevator Control SystemSDR 2011FA0000141Control Cable · frayedTHE AILERON CABLE WAS FRAYED AND WORN SHOWING BROKEN STRANDS AT FUSELAGE STATION 65.33 WHERE THE CABLES PASS THOUGH THE 3 CEILING MOUNTED NYLON PULLEYS.Mar 1, 2011 · N375ER · Cessna 172S · Aileron Control SystemSDR 2011FA0000015Ignition Switch · failedTHE IGNITION SWITCH HAS NEVER BEEN INSPECTED IAW SEB91-5R1 TO COMPLY WITH AD 93-05-06. UPON DISASSEMBLY OF THE SWITCH, THE CIRCUIT BOARD PLATE WAS FOUND TO BE SEVERLY WORN AND 1 CONTACT POINT WAS BURNED. 1 CONTACT CUP WAS BURNED COMPLETELY THROUGH CREATING AJan 6, 2011 · N348ME · Cessna 172S · Ignition SwitchingSDR CA101222005Pressure Switch · leaking(CAN) OIL LEAKING THROUGH TOP OF OIL PRESSURE SWITCH PN 83278 AND OUT AROUND ELECTRICAL PLUG (FOR LOW OIL PRESSURE WARNING LIGHT AND HOUR METER). PILOT HAD RED OIL PRESSURE ANNUCIATOR ILLUMINATE AND LANDED AS SOON AS POSSIBLE. SB07-79-01 CITES INTERNAL WEAR ASDec 10, 2010 · Cessna 172S · Engine Oil PressureSDR CA101210006Circuit Breaker · failed(CAN) FLAPS FAILED TO EXTEND FOUND CIRCUIT BREAKER NOT CARRYING POWER WITH ANY CURRENT DRAW AND SEEMED TO "POP" WITH NO INDICATION ON THE BREAKER .CIRCUIT BREAKER REPLACED WITH NEW AND FLAPS OPERATED NORMAL.Dec 9, 2010 · Cessna 172S · Trailing Edge Flap Control SystemSDR 2010FA0001230Strut · damaged(OG5S) DURING ROUTINE (PHASE) INSP, THE NOSE GEAR OLEO STRUT WAS DISASSEMBLED FOR REPLACEMENT OF O-RINGS. DURING DISASEMBLY, THE TECH FOUND THE INNER STRUT TUBE AT THE TOP HAD RETAINING PINS WHICH WERE DAMAGED ALLOWING LOWER PART OF TUBE TO BE WORKED LOOSE FRODec 2, 2010 · N538ND · Cessna 172S · Main Landing Gear Strut/Axle/TruckSDR 2010FA0001163Control Cable · frayed(U72S) DURING PASE III INSP FOUND RT AILERON CONTROL CABLES FRAYED AGAINST PN 0522647-10, FAIRLEAD ASSY, FWD OF AILERON AUTOPILOT SERVO. BOTH CABLES PN 0510105-362 AND 0510105-365 EFFECTED.Nov 9, 2010 · N5291W · Cessna 172S · Aileron Control SystemSDR 2010FA0001162Control Cable · frayed(U72S) DURING PHASE III INSP FOUND RT AILERON CONTROL CABLES FRAYED AGAINST PN 0522647-10 FAIRLEAD ASSY, FWD OF AILERON AUTOPILOT SERVO. BOTH CABLES PN 0510105-362 AND 0510105-365 EFFECTED.Nov 9, 2010 · N65956 · Cessna 172S · Aileron Control SystemSDR 2010FA0001187Gyro · failedINSTALLED O/H ATTITUDE GYRO, PN 1U14901515 OR S3326-2RX, SN T92573Q. UNDER W/O 0358583, DATED 09/23/10. GYRO FLAG RETRACTED AND SPUN UP BUT GYRO WOULD NOT ERECT. INSTALLED O/H GYRO PN S3326-2RX, SN T91155Q, O/H UNDER W/O 0358831 DATED 09/23/2010. OPS AND LNov 3, 2010 · N168CB · Cessna 172S · Attitude Gyro and Indicating SystemSDR 2010FA0001183Bulkhead · cracked(O2GS) CRACK WAS FOUND PROTRUDING FROM PROP ATTACH BOLT HOLES IN THE FWD SPINNER BULKHEAD.Oct 27, 2010 · N536ND · Cessna 172S · Propeller Spinner SectionSDR 2010FA0001184Bulkhead · cracked(OG5S) CRACK WAS FOUND PROTRUDING FROM PROP ATTACH BOLT HOLES IN THE FWD SPINNER BULKHEAD.Oct 22, 2010 · N529ND · Cessna 172S · Propeller Spinner SectionSDR CA101006008Cable · brokenAFTER LANDING THE PILOT PULLED THE HANDLE TO MOVE HIS SEAT BACK. THE CABLE BROKE AND THE PILOT HAD DIFFICULTY EXITING THE ACFT.Oct 2, 2010 · Cessna 172S · Flight Compartment EquipmentSDR YN8R11227Hose · splitUPON VISUAL INSP, FOUND FUEL HOSES CRACKED. BATCH NR 062308B, 17 PIECES.Sep 3, 2010 · Cessna 172S · Aircraft Fuel Distribution SystemSDR YN8R11226Hose · splitUPON VISUAL INSP FOUND FUEL HOSES TO BE CRACKED. HOSE BATCH CODE NR 062308B, 17 PIECES.Sep 3, 2010 · N9147H · Cessna 172S · Aircraft Fuel Distribution SystemSDR CA100830006Wire · damagedFUEL CAP ATTACH CHAIN BECAME DISCONNECTED FROM THE TAB ON THE FILLER NECK ALLOWING THE LOOSE END TO FALL INTO THE TANK STILL ATTACHED TO THE CAP. THE LOOSE END OF THE CHAIN WRAPPED AROUND THE FINE WIRE ON THE FUEL SENDING UNIT. THIS CAUSED THE WIRE TO BECOME Aug 30, 2010 · Cessna 172S · Fuel System WiringSDR 2010FA0000992Control Cable · frayed(BF8R) CABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRESAug 23, 2010 · N549ER · Cessna 172S · Aileron Control SystemSDR 2010FA0000990Control Cable · frayed(BF8R) CABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRESAug 23, 2010 · N549ER · Cessna 172S · Aileron Control SystemSDR 2010FA0000989Control Cable · frayed(BF8R) CABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRESAug 23, 2010 · N549ER · Cessna 172S · Aileron Control SystemSDR 201001095Control Cable · frayedCABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRES WITH AAug 23, 2010 · N549ER · Cessna 172S · Aileron Control SystemSDR 2010FA0000988Control Cable · frayed(BF8R) CABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRESAug 23, 2010 · N540ER · Cessna 172S · Aileron Control SystemSDR 2010FA0000987Control Cable · frayed(BF8R) CABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRESAug 23, 2010 · N540ER · Cessna 172S · Aileron Control SystemSDR 2010FA0000986Control Cable · frayed(BF8R) CABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRESAug 23, 2010 · N540ER · Cessna 172S · Aileron Control SystemSDR 201001094Control Cable · frayed(BF8R) CABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRESAug 23, 2010 · N540ER · Cessna 172S · Aileron Control SystemSDR 2010FA0000985Control Cable · frayed(BF8R) CABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRESAug 23, 2010 · N552ER · Cessna 172S · Aileron Control SystemSDR 2010FA0000984Control Cable · frayedCABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRES WITH AAug 23, 2010 · N552ER · Cessna 172S · Aileron Control SystemSDR 2010FA0000983Control Cable · frayed(BF8R) CABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRESAug 23, 2010 · N552ER · Cessna 172S · Aileron Control SystemSDR 201001089Control Cable · frayed(BF8R) CABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRESAug 23, 2010 · N552ER · Cessna 172S · Aileron Control SystemSDR 2010FA0000982Control Cable · frayedCABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRES WITH AAug 23, 2010 · N546ER · Cessna 172S · Aileron Control System
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