Lycoming O-320-A2D

Service difficulty reports · 17

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 = 'O320A2D'
  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 2015FA0000317Master Cylinder · damagedWHILE BEING TAXIED FOR TAKEOFF, THE RT BRAKE FAILED, RESULTING IN THE ACFT PROPELLER TO CONTACT A TAXIWAY LIGHT RESULTING IN IRREPAIRABLE DAMAGE TO THE PROPELLER. UPON VISUAL INSPECTION OF THE RT BRAKE MASTER CYLINDER THE COVER CHAMPHER WAS DAMAGED NOT ALLOWIJul 10, 2015 · N40SP · Cessna 172M · Master Cylinder/Brake ValveSDR 2013FA0000441Spar · crackedDURING INSPECTION OF WING IAW AD 2000-25-02R1, FOUND CRACK IN REAR SPAR ABOUT THREE INCHES LONG. ORIGINATES FROM FLAP SUPPORT BRACKET ATTACH POINT OUTWARD.Jul 16, 2013 · N50564 · Blanca 7GCBC · Wing SparSDR 2013FA0000295Skin · crackedAIRCRAFT BROUGHT IN FOR REFURBISHMENT, ON REMOVAL OF FUSELAGE FABRIC, REAR TAIL SECTION WAS FOUND CRACKED IN THREE PLACES. (REF:CE-13-14) FUSELAGE REPAIRED STC SA4051NM.May 30, 2013 · Piper PA18A150 · Fuselage Main, Plate/SkinSDR CA111026005Tank · cracked(CAN) FUEL WAS NOTED DRIPPING FROM SUMP DRAIN BOSS WHEN TANK WAS FULL. DRAIN VALVE WAS REPLACED BUT DRIP CONTINUED. INVESTIGATION NOTED FUEL STAINING ON TANK INSIDE WING, OPENING OF FABRIC REVEALED A CRACK AT THE INBOARD END OF THE TOP FORWARD STIFFENING BEAD Oct 25, 2011 · Bbavia 7GCB · Fuel StorageSDR CA090915003Follower · broken(CAN) HEAD OF CAM FOLLOWER BROKE OFF AND JAMMED UNDER HEAD OF AJOINING FOLLOWER, DAMAGING CRANKCASE. (TC# 20090915003)Jul 29, 2009 · Blanca 7GCBC · Reciprocating Engine Power SectionSDR 2008FA0000323Sleeve · crimpedRIGHT RUDDER CABLE SEPARATED AT RUDDER BELLCRANK DURING RECOVERY OF INTENTIONAL LEFT SPIN. CABLE APPARENTLY PULLED OUT OF NICOPRESS SLEEVE. AIRPLANE WAS LANDED AT KCHA, WITHOUT INCIDENT, AFTER DECLARING AN EMERGENCY.May 4, 2008 · N53718 · Bbavia 7GCBC · Rudder Control SystemSDR CA061120006Rudder Pedal · cracked(CAN) DURING REPLACEMENT OF THE FUEL SHUTOFF VALVE THE LT FRONT RUDDER/BRAKE PEDAL WAS FOUND CRACKED BETWEEN THE BRAKE PEDAL UPRIGHT AND THE OB PEDAL HINGE. THE DEFECT APPEARS TO BE CAUSED BY BRAKING FORCES APPLIED BY THE FLIGHT INSTRUCTOR IN THE REAR SEAT, THNov 20, 2006 · Bbavia 7GCBC · Rudder Control SystemSDR CA041221003Muffler · cracked(CAN) AD CF90-03R2 REQUIRES PRESSURE TESTING OF MUFFLERS USED FOR CABIN HEAT. CRACK NOTED AT RT END PLATE ABOVE INLET PORT, AT OUTER EDGE OF PREVIOUS WELD REPAIR. CRACK WAS NOT INSIDE CABIN HEAT MUFF AREA.Dec 10, 2004 · Bbavia 7GCBC · Engine Noise SuppressorSDR CA040512005Spar · chafed(CAN) ON METAL-SPAR WINGS RETROFITTED TO THIS AC THE AFT SPARS HAVE THREE FOOT STIFFENERS RIVETED TO THEM AT AFT STRUT ATTACH POINT. CLEARANCE BETWEEN FABRIC AND STIFFENER IS MINIMAL, AND INSPECTION HOLE COVER CLIPS CAN CONTACT STIFFENER AND CHAFE GROOVES INTOMay 7, 2004 · Bbavia 7GCBC · Wing SparSDR CA030708007Window · damaged(CAN) THE ONLY EXPLANATION WE HAVE FOR THIS BURNED AREA COMES FROM THE FEW TIMES THIS AIRCRAFT HAS BEEN PARKED OUTSIDE, OR DURING FLIGHT. IT MIGHT SOUND CRAZY, BUT SUNLIGHT MUST HIT THE GLASS AT THE RIGHT PERFECT ANGLE, BUNDLE THE LIGHT LIKE A MAGNIFYING GLASSApr 15, 2003 · Bbavia 7GCBC · Flight Compartment WindowsSDR CA030106017Cotter Pin · broken(CAN) DURING A SCHEDULED INSPECTION THE FLAP HANDLE RELEASE ASSEMBLY WAS NOT ENGAGING THE FLAPS IN THE CORRECT DEGREES SETTING. UPON INVESTIGATING THE FLAP HANDLE ASSEMBLY, WE FOUND A BROKEN COTTER PIN PN 38022 LOCATED IN THE RELEASE ASSEMBLY. THE FLAP HANDLEAug 27, 2002 · Bbavia 7GCBC · Trailing Edge Flap Control SystemSDR 2002FA0000542Control Cable · brokenLEFT AILERON DIRECT CONTROL CABLE SEPARATED IN FLIGHT RESULTING IN A FATAL ACCIDENT. THE CABLE P/N 0510105-224 WAS VERY BADLY RUSTED AT THE POINT OF FAILURE LOCATED ABOVE THE RIGHT DOORPOST WHERE THE CONTROL CABLE RIDES OVER A PULLEY. THE PULLEY IN THIS AREAApr 26, 2002 · N75908 · Cessna 172N · Aileron Control SystemSDR AUS20011454Bolt · failed(AUS) TAIL WHEEL ATTACHMENT BOLT FAILED. TAIL WHEEL SEPARATED FROM TAIL LEAF SPRING.Dec 28, 2001 · Bbavia 7GCAA · Nose/Tail Landing Gear Strut/AxleSDR AUS20010642Bolt · corroded(AUS) LOWER RH SIDE STRUT LOWER BOLT SEIZED. FOLLOWING BOLT REMOVAL ITWAS FOUND TO BE VERY RUSTED AND PITTED.Jun 14, 2001 · Bbavia 7GCAA · Wing, Attach FittingsSDR 2002FA0000238Spar · crackedINSPECTED AIRCRAFT AS PER AD, FOUND LEFT AFT SPAR HAS COMPRESSION CRACK AT OUTBOARD END OF DOUBLER PLATES FOR STRUT ATTACH FITTING.May 7, 2001 · N5038A · Bbavia 7GCAA · Wing SparSDR CA000530027Axle · cracked(CAN) CRACK FOUND IN BEND JUST BELOW FORWARD UPPER BOLT HOLEApr 11, 2000 · Bbavia 7GCBC · Main Landing Gear Strut/Axle/TruckSDR AU960856Shaft · worn(AUS) ENGINE CRANKSHAFT LH IDLER GEAR SHAFT ATTACHMENT HOLES ELONGATED,LOCKWIRE BROKEN, BOLTS NECKED AND SHAFT LOOSEApr 25, 1996 · Bbavia 7GCBC · Reciprocating Engine Rear Section
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