Lycoming IO-360-L2A

Service difficulty reports · 994

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 engine_model_key = 'IO360L2A'
  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 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 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 CA101210008Rod · misinstalled(CAN) FOUND THE TRIM TAB CONTROL ROD INSTALLED UPSIDE-DOWN. IT WAS DETERMINED THAT THE ROD WAS INSTALLED INCORRECTLY AT FACTORY SINCE THERE WAS NO PAINT ON OTHER SIDE. ROD REMOVED AND INSTALLED IN CORRECT ORIENTATION. CHECKED TRAVEL AND RIGGING, NO CHANGE, CHEDec 8, 2010 · Cessna 172R · Elevator Tab 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 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 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 2010FA0000959Bulkhead · crackedCRACK FOUND ON UPPER FWD SECTION OF THE LT BULKHEAD ASSY, DIRECTLY UNDER THE PILOT`S RUDDER PEDALS. CRACK DISCOVERED DURING A 100 HR INSP.Aug 25, 2010 · N2369P · Cessna 172R · Fuselage Main, BulkheadSDR 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 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 System
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