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 2010FA0000981Control 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 SystemSDR 2010FA0000980Control 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 · N546ER · Cessna 172S · Aileron Control SystemSDR 201001079Control 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 SystemSDR 2010FA0000979Control 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 · N556ER · Cessna 172S · Aileron Control SystemSDR 2010FA0000978Control 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 · N556ER · Cessna 172S · Aileron Control SystemSDR 2010FA0000977Control Cable · frayedCABIN OVERHEAD CTR PANEL REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WAS ABLE TO CATCH FRAYED WIRES WITH A RAG & COULDAug 23, 2010 · N556ER · Cessna 172S · Aileron Control SystemSDR 201001043Control 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 · N556ER · Cessna 172S · Aileron Control SystemSDR 2010FA0000976Control 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 · N557ER · Cessna 172S · Aileron Control SystemSDR 2010FA0000975Control 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 · N557ER · Cessna 172S · Aileron Control SystemSDR 2010FA0000974Control 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 · N557ER · Cessna 172S · Aileron Control SystemSDR 201001006Control 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 · N557ER · Cessna 172S · Aileron Control SystemSDR 2010FA0000973Control 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 · N551ER · Cessna 172S · Aileron Control SystemSDR 2010FA0000972Control 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 · N551ER · Cessna 172S · Aileron Control SystemSDR 2010FA0000971Control 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 · N551ER · Cessna 172S · Aileron Control SystemSDR 201000738Control 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 · N551ER · Cessna 172S · Aileron Control SystemSDR 2010FA0000969Control 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 · N548ER · Cessna 172S · Aileron Control SystemSDR 2010FA0000968Control 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 · N548ER · Cessna 172S · Aileron Control SystemSDR 201000930Control 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 · N548ER · Cessna 172S · Aileron Control SystemSDR 2010FA0000967Control 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 · N541ER · Cessna 172S · Aileron Control SystemSDR 2010FA0000966Control 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 · N541ER · Cessna 172S · Aileron Control SystemSDR 2010FA0000965Control 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 · N541ER · Cessna 172S · Aileron Control SystemSDR BF8R201000987Control Cable · frayedCABIN OVERHEAD CENTER PANEL REMOVED FOR INSP. DURING FLAP & AILERON CABLE INSPECTION, FLAT SPOTS WERE NOTICED ON 2 AILERON CONTROL CABLES. ROLLED CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, ABLE TO CATCH FRAYED WIRES WITH A RAG AND COULD SEE A SUBSAug 23, 2010 · N541ER · Cessna 172S · Aileron Control SystemSDR 2010FA0000939Control Cable · frayedCABIN OVERHEAD CTR PANEL WAS REMOVED OR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSP, FLAT SPOTS WERE NOTICED ON 3 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRES WITH A RAG ANAug 23, 2010 · N554ER · Cessna 172S · Aileron Control SystemSDR 2010FA0000938Control Cable · frayedCABIN OVERHEAD CTR PANEL WAS REMOVED OR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSP, FLAT SPOTS WERE NOTICED ON 3 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRES WITH A RAG ANAug 23, 2010 · N554ER · Cessna 172S · Aileron Control SystemSDR 201000338Control Cable · frayedCABIN OVERHEAD CTR PANEL WAS REMOVED OR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSP, FLAT SPOTS WERE NOTICED ON 3 AILERON CONTROL CABLES. ROLLED THE CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS, WE WERE ABLE TO CATCH FRAYED WIRES WITH A RAG ANAug 23, 2010 · N554ER · Cessna 172S · Aileron Control SystemSDR CA100813011Muffler · crackedEXHAUST MUFFLER WAS BROUGHT IN AFTER CRACKS WERE DISCOVERED. CRACK LOCATED AT CONNECTION WITH PART 9954100-7. PART 9954100-7 IS SUSPECT TO BE EITHER SHORT OR LONG. PART 9954100-7 IS REPLACED 4:1. CRACK WILL BE WELDED UP IAW AC43.13 AND PRESSURE TESTED FOR OTAug 13, 2010 · Cessna 172S · Engine Noise SuppressorSDR ZB0R201000005Starter · bindsWHILE ATTEMPTING TO START THE ENGINE, THE PILOT REPORTED THE STARTER WOULD NOT ROTATE THE ENGINE. PLANE TAKEN TO MAINTENANCE WHERE IT WAS DISCOVERED THE STARTER WAS FROZEN. REPLACED WITH REPAIRED LIKE PART AND OPS CHECK OK. THIS IS THE SECOND OCCURRENCE OF Jun 23, 2010 · N272RP · Cessna 172S · Engine StarterSDR ZB0R20100002Master Switch · burned((ZB0R)) PILOT REPORTED BURNING SMELL AND FAILURE OF AVIONICS BUSS NR 2 ON RUN-UP. ACFT REPORTED TO MX. TROUBLESHOOTING REVEALED AVIONICS MASTER SWITCH RT SIDE (BUSS 2) ARCING INTERNALLY. REPLACED AVIONICS SWITCH AND OPS CK OK.May 31, 2010 · N963AC · Cessna 172S · DC Power Distribution SystemSDR CA100805006Gasket · wrong partTHE PILOT, WHILE IN CRUISE, GOT AN INDICATION OF A VACUUM PUMP FAILURE, AND AS THESE MODELS HAVE 2 VACUUM PUMPS, HE RETURNED TO DEPARTURE. UPON INSP, AT FIRST APPEARED TO BE A ROUTINE VACUUM PUMP REPLACEMENT, BUT MX DECIDED TO REMOVE THE DRIVE HSG FROM THE ENGMay 26, 2010 · Cessna 172S · Reciprocating Engine Oil SystemSDR 2010FA0000507Control Cable · frayedDURING INSPECTION THE AILERON CABLES ARE INSPECTED WITH MAGNIFICATION WHERE KNOWN WEAR/FRAYING IS COMMON. THIS CABLE, P/N-0510105-360 WAS FOUND WORN AT F.S.: 65.53. THERE WERE BROKEN STRANDS AND THE AREA IS EXTREMELY SHINY. THIS IS A COMMON DISCREPANCY FOR May 25, 2010 · N442ER · Cessna 172S · Aileron Control SystemSDR 2010FA0000492Control Cable · frayedDURING INSPECTION THE AILERON CABLES ARE INSPECTED WITH MAGNIFICATION WHERE KNOWN WEAR/FRAYING IS COMMON. THIS CABLE, CESSNA P/N-0510105-364 WAS FOUND WORN AT W.S.: 71.125. THERE WERE BROKEN STRANDS AND THE AREA IS EXTREMELY SHINY. THIS IS A COMMON DISCREPANCYMay 19, 2010 · N442ER · Cessna 172S · Aileron Control SystemSDR 2010FA0000491Control Cable · frayedDURING INSPECTION THE AILERON CABLES ARE INSPECTED WITH MAGNIFICATION WHERE KNOWN WEAR/FRAYING IS COMMON. THIS CABLE, CESSNA P/N-0510105-364 WAS FOUND WORN AT FS 65.33. THERE WERE BROKEN STRANDS AND THE AREA IS EXTREMELY SHINY. THIS IS A COMMON DISCREPANCY FORMay 19, 2010 · N442ER · Cessna 172S · Aileron Control SystemSDR 2010FA0000490Control Cable · frayedDURING INSPECTION THE AILERON CABLES ARE INSPECTED WITH MAGNIFICATION WHERE KNOWN WEAR/FRAYING IS COMMON. THIS CABLE, P/N-0510105-360 WAS FOUND WORN AT F.S.: 65.53. THERE WERE BROKEN STRANDS AND THE AREA IS EXTREEMLY SHINY. THIS IS A COMMON DISCREPANCY FOR THIMay 19, 2010 · N442ER · Cessna 172S · Aileron Control SystemSDR 2010FA0000452Contact · burnedAD 93-05-06 (IGNITION SWITCH INSPECTION) DOES NOT APPLY BY S/N TO 2001 CESSNA 172S - BUT THE AD STATES: REPEAT INSPECTION AND LUBRICATE IAW ACS SB92-01 EACH 2000 HRS. CHOOSE TO INSPECT & RE-LUBE BECAUSE OF THE MFR'S, 2000 HR SERVICE LIFE. UPON INSPECTION THMay 6, 2010 · N851SP · Cessna 172S · Ignition SwitchingSDR 2010FA0000451Strut · separatedDURING FIREWALL REPLACEMENT THE NOSE LANDING GEAR WAS REMOVED TO FACILITATE REPLACEMENT. WHEN THE TECHNICIAN DEPRESSED THE NOSE STRUT TO CHECK FLUID LEVEL IN DEFLATED STRUT THE TOP OF THE INNER STRUT TUBE DEPARTED THE STRUT OUT THE TOP. UPON FURTHER DISASSEMMay 6, 2010 · N519ND · Cessna 172S · Nose/Tail Landing Gear Strut/AxleSDR 2010FA0000411Control Cable · frayedDURING A ROUTINE INSP, THIS CABLE WAS FOUND WORN WITH BROKEN STRANDS. IT IS VERY DIFFICULT TO SEE WITHOUT MAGNIFICATION AND APPEARS ONLY AS A SHINY SPOT ON THE CABLE. THIS CABLE AND (2) OTHERS PASS ACROSS THE CEILING THROUGH 3 PULLEYS JUST ABOVE THE REAR SEAT Apr 23, 2010 · N464ER · Cessna 172S · Aileron Control SystemSDR 2010FA0000425Guide · broken(HE8S) PILOT`S SEAT HARNESS GUIDE BROKE AT SHOULDER HARNESS MOUNT TUBE. SUGGEST MAKING THIS PART WITH MORE DURABLE MATERIAL OR HAVING A REINFORCEMENT AT AREA OF BREAKAGE. THE BROKEN PART HAS A STRESS AREA WHERE IT WAS BROKEN DUE TO THE HOLE WHERE HEAD REST MApr 19, 2010 · N55SV · Cessna 172S · Flight Compartment EquipmentSDR CA100222003Switch · faulty(CAN) CREW REPORTED A BURNING ODOR IN THE CABIN AND SAW SMOKE COME FROM THE LANDING LIGHT SWITCH. THE PIC CONTACTED DEPARTURE TO INFORM OF THE SITUATION, AND WAS CLEARED TO RETURN NR 1. ACFT ELECTRICAL FIRE CHECKLIST WAS COMPLETED AND THE SMOKE CEASED ONCE ALLFeb 21, 2010 · Cessna 172S · Exterior LightingSDR CA100813012Muffler · crackedMUFFLER O/H BY CRS WAS BROUGHT IN FOR REPAIR EVALUATION. MUFFLER IS CRACKED IN DOUBLER AT THE TAILPIPE ATTACHMENT POINT WAS BROUGHT IN. MULTIPLE CRACKS LOCATED AT CO GUARD ATTACHMENT TO CAN. CRACK WAS DISCOVERED DURING INSP IAW TCCA AD CF-90-03R2. REPLACEMFeb 19, 2010 · Cessna 172S · Engine Noise SuppressorSDR 2010FA0000085Tube · flatDURING TOUCH-AND-GO LANDINGS, PILOTS REPORTED TO HEAR A STRANGE NOISE IN THE LANDING GEAR AT ROTATION AFTER SECOND LANDING. REMAINDER OF FLIGHT WAS NONEVENTFUL. AFTER NORMAL LANDING TOUCHDOWN AND ACFT DECELERATION, ACFT STARTED VEERING TO THE LT OF CTR. LT Feb 3, 2010 · N52519 · Cessna 172S · Tire TubeSDR 2010FA0000035Control Cable · frayedDURING FLAP & AILERON CABLE INSP FLAT SPOTS WERE NOTICED ON 3 AILERON CONTROL CABLES. ROLLED CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS & WAS ABLE TO CATCH FRAYED WIRES WITH A RAG & COULD SEE A SUBSTANTIAL GROOVE IN CARRY-THRU CABLE. CABLE TENSIONSJan 8, 2010 · N558ER · Cessna 172S · Flight Control SystemSDR 2010FA0000034Control Cable · groovedCABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSP FLAT SPOTS WERE NOTICED ON 3 AILERON CONTROL CABLES. ROLLED CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS AND WAS ABLE TO CATCH FRAYED WIRES WITH A RAG AND COUJan 8, 2010 · N558ER · Cessna 172S · Flight Control SystemSDR 2010FA0000033Control Cable · damagedCABIN OVERHEAD CTR PANEL WAS REMOVED FOR PROGRESSIVE INSP. DURING FLAP & AILERON CABLE INSP FLAT SPOTS WERE NOTICED ON 3 AILERON CONTROL CABLES. ROLLED CABLES FOR BETTER VIEW OF CONTACT POINT WITH PULLEYS AND WAS ABLE TO CATCH FRAYED WIRES WITH A RAG AND COUJan 8, 2010 · N558ER · Cessna 172S · Aileron Control SystemSDR CA091126005Ring Gear · failed(CAN) ONE TOOTH ON RING GEAR ASSEMBLY WAS MISSING, TOOTH BROKEN AT BASE, NO EVIDENCE OF DAMAGE ON STARTER PINION GEAR FOUND. NO EVIDENCE OF STARTER KICK BACK/ENGINE KICK BACK NOTED. NO OTHER DAMAGE NOTED ON ANY GEAR TEETH. SUSPECT QUALITY CONTROL AT POINT ONov 23, 2009 · Cessna 172S · Engine StarterSDR CA091125003Alternator · failed(CAN) THE AIRCRAFT PFD INDICATED CHARGING SYSTEM FAILURE IN FLIGHT. AIRCRAFT RETURNED TO BASE TROUBLE SHOOTING C/O FOUND ALTERNATOR FAILED, UNIT ONLY HAD 300 HRS SINCE OVERHAUL. MANUFACTURER RECOMENDS 500 HR INTERVAL. (TC NR 20091125003)Nov 22, 2009 · Cessna 172S · AC Generator-AlternatorSDR 2009FA0000956Control Cable · chafedDURING A ROUTINE INSP, THE AILERON CABLE PN-0510105-364 WAS FOUND SHINY WHERE IT PASSES THROUGH THE CEILING PULLEY CLUSTER. WHEN VIEWED THROUGH A STRONG MAGNIFYING GLASS, MANY BROKEN STRANDS CAN BE SEEN.Nov 13, 2009 · N375ER · Cessna 172S · Aileron Control SystemSDR 2009FA0000955Control Cable · chafedDURING A ROUTINE INSPECTION THE AILERON CABLE P/N-0510105-365 WAS FOUND CHAFING AND WORN IN THE CENTER CEILING AREA WHERE IS PASSES THROUGH THE 3 PULLEY CLUSTER. THE STRANDS APPEAR SHINY TO THE NAKED EYE, BUT WITH A SUITABLE MAGNIFYING GLASS CAN BE SEEN TO HAVNov 13, 2009 · N375ER · Cessna 172S · Aileron Control SystemSDR CA091102009Piston Rod · broken(CAN) LT BRAKE MASTER CYL PISTON ROD BROKE IN THREAD AREA.Nov 2, 2009 · Cessna 172S · Master Cylinder/Brake ValveSDR 2009FA0000975Bushing · inaccurateCYLINDER NR 4 ROCKER SHAFT BUSINGS IMPROPER INTERFERENCE FIT WITH ROCKER SHAFT. DEFECT FOUND DURING DISASSEMBLY PHASE OF OVERHAUL WHILE ATTEMPTING TO REMOVE ROCKER SHAFT FROM CYLINDER. PROBABLE CAUSE IS IMPROPER MFG. (K)Oct 29, 2009 · N453ER · Cessna 172S · Reciprocating Engine Cylinder SectionSDR CA091020002Line · chafed(CAN) LT HAND BRAKE LINE WAS FOUND CHAFED WHERE IT PASSES OUT OF THE GEAR LEG FAIRING AND INTO THE FUSELAGE. BRAKE LINE REPLACED AND BRAKES BLED. SB 09-32-02 ADDRESSES SIMILAR DAMAGE ON 182 SERIES AIRCRAFT BUT IT DOES NOT INCLUDE INSP OF THE UPPER END OF THE Oct 19, 2009 · Cessna 172S · Landing Gear Brake System
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