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 2012FA0000349Hose · leakingENGINE HAD SLIGHT VIBRATIONS ON DOWNWIND, THROTTLE WAS ADDED WITH VIBRATION INCREASE. ENGINE DIED ON FINAL AND ACFT GLIDED TO RUNWAY SAFELY. ENGINE RESTARTED BUT WOULD NOT RUN WELL. ON INSPECTION, THE FUEL SERVO TO FLOW DIVIDER FUEL HOSE WAS FOUND TO HAVE EVSDR 2012FA0000288Strut · faultedDURING PHASE INSPECTION, NOSE GEAR STRUT BOROSCOPED AND CONECTING PINS FOR INNER STRUT TUBE FOUND TO BE LOOSE AND MIGRATING. ORIGINAL BONDED DESIGNED INNER STRUT TUBE WAS INSTALLED.SDR 2012FA0000287Tire · deflatedNOSE TIRE DEFLATED ON LANDING.SDR NX4R201205220053Control Cable · brokenDURING A ROUTINE INSPECTION, THE AFT UPPER ELEVATOR CONTROL CABLE WAS FOUND TO HAVE BROKEN STRANDS AT THE REAR PULLEY AT BULKHEAD 205.81. MANY OF THE BROKEN STRANDS APPEARED TO HAVE BROKEN DUE TO TENSION, NOT CHAFING.SDR NX4R201204200054Control Cable · wornDURING A ROUTINE INSPECTION OF THE RUDDER CABLE, WAS FOUND WORN AND SEPARATE STRAND CAUGHT ON A SHOP RAG. THIS WEAR OCCURED AT FS 65-33.SDR 2012FA0000322Unknown · failedSOMETHING INSIDE CYLINDER LET GO SO THAT THE ROD WAS NO LONGER CONNECTED TO THE PISTON. BOTTOM OF THE PISTON WAS DESTROYED. WRIST PIN RIDES WAS DESTROYED FROM BANGING INTO BOTTOM OF CYLINDER. EITHER THE PISTON LET GO, OR THE ROD LET GO OF THE WRIST PIN.SDR NX4R2012031900031Shaft · wornDURING A ROUTINE INSPECTION, CONTROL COLUMN SHAFT WAS SIGNIFICANTLY WORN AT THE 6 O'CLOCK POSITION WHERE IT EXITS THE INSTRUMENT PANEL. IT RIDES ON A BUSHED SURFACE.SDR 2012FA0000161Wire · misinstalledWHILE CONDUCTING THE ESSENTIAL AND CROSSFEED BUSS DIODES INSPECTION AS CALLED OUT IN MM 5-10-01 AND 24-61-01, 2 WIRES SLIPPED OUT OF BUSS 1 AND BUSS 2 CONNECTOR ON MALE END. WIRES APPEARED TO HAVE INCORRECT CRIMP CAUSING WIRES TO PULL OUT CREATING POWER LOSS.SDR 2012FA0000165Cable · brokenONE OF TWO ATTACHING CABLES FOR THE SEAT TRACK LOCK PINS, FOUND BROKEN AT THE SWEDGE POINT, LEAVING THE CABLE FLAPPING LOOSE AND ONLY ONE PIN LOCKED IN SEAT TRACK. PULLING ON TEE HANDLE ONLY RELEASED PIN ON ONE SIDE. R & R CABLE ASSY. OPS CHECKED GOOD. CABLSDR NX4R2012031501028Control Cable · frayedDURING A ROUTINE INSPECTION, THE TOP ELEVATOR CABLE AT THE PULLEY PNS-378-3, F/S-205.81 WAS FOUND TO BE FRAYED WITH SEVERAL BROKEN STRANDS. THERE WAS NO ABNORMAL WEAR ON THE PULLEY AND THE CABLE WAS NOT WORN. THE STRANDS APPEARED TO BE BROKEN DUE TO A TENSIONSDR NX4R2012031200028Control Cable · frayedDURING A ROUTINE INSPECTION, THE AILERON CABLE, FOUND FRAYED WITH BROKEN STRANDS. THE WEAR IS AT WS: 65.33SDR NX4R2012031200027Control Cable · frayedDURING A PHASE INSPECTION, THE UPPER, AFT ELEVATOR CABLE PN-0510105-308, HAD BROKEN STRANDS AT FS 205.81 AT PULLEY PN-378-3.SDR NX4R2012031200026Control Cable · frayedDURING A PHASE INSPECTION THE UPPER, AFT ELEVATOR CABLE PN-0510105-391 HAD BROKEN STRANDS AT FS 205.81 AT PULLEY PN-378-3.SDR NX4R2012031200025Control Cable · frayedDURING A PHASE INSPECTION THE UPPER, AFT ELEVATOR CABLE P/N-2012-01500 HAD BROKEN STRANDS AT FS 205.81 AT PULLEY P/N-378-3.SDR NX4R2012030800029Control Cable · frayedDURING A ROUTINE INSP, THE AILERON CABLE PN-01510105 AT WS 65.33 WAS FOUND FRAYED WITH BROKEN STRANDS.SDR 2012FA0000132Strut · failedDURING PHASE INSPECTION, NOSE GEAR WAS BORESCOPED AND THE CONNECTING PINS FOR THE INNER STRUT TUBE WERE FOUND TO BE WORKING AND BEGINNING TO MIGRATE FROM THEIR HOLES. THIS IS A KNOWN PROBLEM WITH THE MANUFACTURER AND HAVE BEEN TOLD A NEW STYLE INNER STRUT IS SDR 2013FA0000035O-Ring · damagedBRAKE FAILED FOLLOWING A LONG FAST TAXI. IT APPEARS THAT THE PIOT HOLDS POWER ON AND RIDES THE BRAKE. PILOT REPORTED THE HE STEPPED ON BRAKE WITH NO RESPONSE. PROBLEM COULD NOT BE DUPLICATED. HOLDING BRAKE AT VARIOUS PRESSURES FOR PERIODS OF 5 MINUTES EACHSDR 2012FA0000152Line · out of positionFUEL LINE, TOUCHING UPPER LIP OF LOWER FUSELAGE FORMER. THIS IS THE 3RD ACFT SEEN WITH THIS PROBLEM.SDR 2012FA0000043Arm · detachedLOST FUEL PRESSURE IN FLIGHT. FOUND FUEL PUMP ARM DETACHED FROM PUMP DIAPHRAGM.SDR CA111219003Engine · power loss(CAN) PILOT EXPERIENCED PARTIAL POWER LOSS ON DOWNWIND WHEN REDUCING POWER OF SETTING UP APPROACH CONFIGURATION. INSTRUCTOR TOOK CONTROL AND LANDED THE ACFT UNDER PARTIAL POWER WITH NO FURTHER INCIDENT. ENGINE RAN POORLY ON GROUND. ENGINE RAN NORMALLY THE FSDR NX4R201111010024Control Cable · frayedDURING A ROUTINE INSPECTION, THE AILERON PRIMARY CABLE, PN-0510105-360, WAS FOUND WORN AND FRAYED WHERE IT PASSES THROUGH THE SMALL NYLON PULLEYS AT FS 65.33.SDR NX4R2011110100023Control Cable · frayedDURING A ROUTINE INSPECTION, THE AILERON PRIMARY CABLE, PN-0510105-360, WAS FOUND WORN AND FRAYED WHERE IT PASSES THROUGH THE SMALL NYLON PULLEYS AT FS 65.33.SDR 2011FA0000695Control Cable · wornINSPECTED CONTROL CABLES FOR WEAR IAW SB 11-27-05. CONTROL CABLES WORN AND REPLACED.SDR CA111003004Control Cable · worn(CAN) AILERON CONTROL CABLE APPEARED TO HAVE SHINY WEAR MARKS ON CONTROL CABLE STRANDS WHERE IT CONTACTS WEAR RUB STRIP IN THE RT WING AT THE AUTOPILOT SERVO AREA. THE CABLE WAS REMOVED FOR FURTHER INSPECTION AND WHEN CABLE WAS BENT INTO A LOOP, MANY BROKEN SSDR 2011FA0000658Pin · migratedDURING SPECIAL INSPECTION, ALL 4 LOCKING PINS WERE FOUND EXHIBITING MOVEMENT AND ABOUT TO FALL OUT.SDR CA111011012Starter · failed(CAN) STARTER WILL SPIN BUT THE SHAFT DOES NOT EXTEND TO ENGAGE THE RING GEAR. STARTER REPLACED.SDR NX4R20110930001Control Cable · frayedDURING A ROUTINE INSPECTION, THIS CABLE WAS FOUND WORN AND FRAYED WHERE IT CONTACTS THE 3 NYLON PULLEYS IN THE CABIN CEILING.SDR 2011FA0000645Pin · shearedNLG STRUT PINS SHEARED.SDR 2011FA0000644Pin · shearedNLG STRUT HAS PINS SHEARED INTERNALLY.SDR 2011FA0000643Tube · damagedNLG INNER TUBE SEPARATED.SDR 2011FA0000641Pin · shearedNLG PINS SHEARED ON INNER STRUT TUBE.SDR 2011FA0000640Tube · separatedNLG STRUT TUBE SEPARATED.SDR 2011FA0000642Tube · damagedNLG STRUT TUBE HAS PIN HOLES ELONGATED.SDR 2011FA0000649Pin · brokenNLG STRUT TUBE HAS A BROKEN PIN.SDR 2011FA0000647Pin · missingPINS MISSING.SDR 2011FA0000639Tube · separatedNLG INNER STRUT TUBE PIN MIGRATING LOOSE.SDR 2011FA0000606Strut · separatedDURING SPECIAL INSPECTION INNER STRUT TUBE FOUND SEPARATED AT CAP AND TUBE CONNECTION.SDR 2011FA0000605Strut · separatedINNER STRUT TUBE FOUND SEPARATED AT CAP AND TUBE CONNECTION.SDR 2011FA0000604Shim · damagedDURING PHASE INSP NOSE GEAR SHIMS WERE FOUND TO BE TORN AND COMPRESSED. INTERIOR INSP OF STRUT FOUND THE INNER STRUT TUBE CAP WAS SEPARATED FROM THE METERING TUBE. UPON DISASSEMBLY THE 4 PIN HOLES WERE FOUND TO BE ELONGATED AND THE SECURING PINS WERE FOUND ISDR 2011FA0000603Strut · separatedINNER STRUT TUBE FOUND SEPARATED DURING SPECIAL INSPECTION. OTHER ACFT IN FLEET HAVE BEEN FOUND. MFG AND LOCAL FSDO HAVE BEEN MADE AWARE OF ISSUE.SDR 2011FA0000602Pin · looseDURING HARD LANDING INSPECTION, INNER STRUT TUBE CAP PINS WERE FOUND TO BE LOOSE AND ELONGATING. THIS HAS BEEN FOUND IN NUMEROUS ACFT IN OUR FLEET OF 62 ACFT RANGING FROM LOOSE PINS TO PIN DISPLACEMENT CAUSING CAP AND TUBE SEPERATION. MFG AND LOCAL FSDO HAVE SDR 2011FA0000601Strut · separatedDURING INSP, NOSE GEAR INNER STRUT TUBE WAS FOUND TO BE SEPARATED AT CAP AND TUBE CONNECTION. NO LEAKS WERE NOTED BUT A SPONGY STRUT WAS REPORTED DURING PRE-INSPECTION RUN-UP.SDR 2011FA0000648Tube · separatedINNER TUBE SEPARATED.SDR 2011FA0000646Tube · separatedNLG STRUT INNER TUBE SEPARATING.SDR 2011FA0000633Tube · leakingTUBE FAILED DUE TO AN INTERNAL DEFECT, THIS IS ONE OF NUMEROUS TUBE FAILURES (OVER 20 IN THE LAST 12 MONTHS) THE FAILURES CAUSE THE TUBE TO START LEAKING AND GO FLAT WITH NO WARNING. THIS HAS CAUSED DAMAGE TO THE WHEEL FAIRINGS ON NUMEROUS OCCASIONS AS THE FSDR 2011FA0000579Switch · failedALL NAV LIGHTS INOPERATIVE ON PREFLIGHT , TROUBLESHOOT SYS FOUND SWITCH CM3589-5 FAILED, THIS IS THE 5TH SWITCH OF THIS PN CHANGED ON THIS MODLE OF ACFT. HOURS VARY FROM 500 TO 3714.SDR CA110824005Master Switch · failed(CAN) DURING FLIGHT THE AVIONICS MASTER SWITCH FAILED. IT STARTED ARCING AND THERE WAS AN ELECTRICAL BURNING SMELL, SUBSEQUENTELY THE AVIONICS CIRCUIT BREAKER POPPED. THE AVIONICS WERE SHUTOFF AND THE ACFT DIVERTED AND LANDED AT AN UNCONTROLLED AIRPORT. UPOSDR CA110713002Starter · burnedSHORTLY AFTER START UP, THE PILOT NOTICED ONCE TAXIING, THAT AN ELECTRICAL SMOKE ODOR WAS PRESENT. THE PILOT QUICKLY SHUTDOWN THE ENGINE AND THE AIRCRAFT WAS TOWED BACK TO THE HANGAR FOR MAINTENANCE. IT WAS FOUND THAT THE STARTER WAS NOT FUNCTIONAL AND THAT ASDR CA110719010Servo · leakingFUEL SERVO FOUND TO BE LEAKING DURING 100 HR INSP. FUEL SERVO REPLACED.SDR MNGR18728Tube · leakingMAIN TIRE WENT FLAT SHORTLY AFTER LANDING. FOUND TUBE TO HAVE A SMALL TEAR ACROSS FROM THE VALVE STEM. THE TEAR AT FIRST APPEARED TO BE A CUT BUT FURTHER INVESTIGATION REVEALED THAT THIS SAME FAILURE HAS BEEN SEEN ON OVER 6 TUBES RECENTLY. INVESTIGATION REVE
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