N867AF

Service difficulty reports · 21

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N867AF' AND registry_match = 'registration'
  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 2011FA0000535Control Cable · failedPILOT REPORTED DURING FLIGHT HE EXPERIENCED A TOTAL LOSS OF MIXTURE CONTROL. INVESTIGATION REVEALED THE MIXTURE CONTROL CABLE HAD BROKEN AT THE CONTROL IN THE CABIN. NO RECOMMENDATIONS AT THIS TIME.Aug 19, 2011 · N867AF · Grob G120A · Mixture ControlSDR 2011FA0000144Pump · leakingMECHANIC WAS PERFORMING A POST MAINTENANCE CHECK ON AIRCRAFT AND NOTICED FUEL STAINS ON THE DOG HOUSE, MECHANIC THEN PERFORMED A LEAK CHECK AND FOUND FUEL LEAKING FROM VENT ON ADJUSTMENT COVER ON ENGINE DRIVEN FUEL PUMP. NO PROBABLE CAUSE OR RECOMMENDATIONS ATMar 2, 2011 · N867AF · Grob G120A · Engine Fuel PumpSDR 2005FA0000801Plate · debondedDURING FLEET-WIDE INSPECTION OF AIRCRAFT, TECH FOUND EXCESSIVE MOVEMENT BETWEEN RUDDER AND RUDDER LEVER ASSY. FURTHER INSPECTION SHOWED DISBONDING BETWEEN THE RUDDER SPAR AND THE RUDDER LEVER ASSY SPACER PLATE. PROBABLE CAUSE APPEARS TO BE EXCESSIVE FLEXING May 13, 2005 · N867AF · Grob G120A · Rudder, Spar/RibSDR 2005FA0000649Hinge · crackedON ROUTINE INSPECTION, MECHANIC FOUND HINGE ON LT AILERON TRIM TAB CRACKED AT ATTACH POINT FOR PUSH PULL ROD. CAUSE AT THIS TIME UNKNOWN, NO RECOMMENDATIONS AT THIS TIME. (K)Mar 28, 2005 · N867AF · Grob G120A · Aileron Control SystemSDR 2005FA0000152Bolt · crackedINSPECTION OF NOSE GEAR UPPER TRUNNION BOLTS FOUND CRACKS AROUND WELDS AND ON THE EARS FOR THE SWIVEL TUBE. PROBABLE CAUSE EXCESSIVE STRESSES IN THIS AREA. AT THIS TIME NO RECOMMENDATION UNTIL MFG MAKES DETERMINATION OF CAUSES. (K)Nov 24, 2004 · N867AF · Grob G120A · Main Landing GearSDR 2003FA0001013Lever · bindingDURING FLEET WIDE INSPECTION, FOUND BEARINGS IN AILERON LEVER 2 ASSY. PN 120A4242 TO BE DAMAGED AND BINDING. DAMAGE APPEARS TO BE CAUSED BY THE BUSHING PN 120A4435.02 IN THE FORK ENDS PN 120A4435.01. IT APPEARS THAT DESIGN LIMITATIONS OF THE BEARINGS ALLOWISep 29, 2003 · N867AF · Grob G120A · Aileron Control SystemSDR 2003FA0000722Light · intermittentPILOT REPORTED RT GEAR LIGHT INOPERATIVE IN FLIGHT, AFTER TOUCH DOWN GEAR INDICATOR LIGHT CAME ON. ON FURTHER INVESTIGATION WE BELIEVE WE HAD AN INTERMITTENT LIGHT INSIDE THE GEAR HANDLE, AFTER FOUR GEAR CYCLES THE LIGHT QUIT WORKING.Jun 18, 2003 · N867AF · Grob G120A · Landing Gear SelectorSDR 2003FA0000717Manifold · inoperativeDURING FLIGHT THE FLIGHT CREW REPORTED THAT THE LEFT GEAR WAS SLOW TO EXTEND. MAINTENANCE PERSONNEL TROUBLESHOT SYSTEM AND FOUND LEFT EXTENSION VALVE BAD. PROBABLE CAUSE IS BELIEVED PARTICIALS INSIDE OF VALVE WHICH PREVENTED FLUID TO FLOW UNRESTRICTED.Jun 6, 2003 · N867AF · Grob G120A · Landing Gear Retraction/Extension SystemSDR 2003FA0000750Actuator · failedDURING FLIGHT, TRIM WOULD NOT STOP AND CONTINUED TO MOVE TO THE LEFT. PROBABLE CAUSE IS INTERNAL COMPONENT FAILURE IN THE AILERON TRIM ACTUATOR UNIT.May 13, 2003 · N867AF · Grob G120A · Aileron Tab Control SystemSDR 2003FA0000559Bearing · failedDURING INSPECTION OF AIRCRAFT, FOUND BEARING TO BE FAILING. RETAINING CLIP AND SEAL WERE BEING FORCED OUT OF BEARING.May 12, 2003 · N867AF · Grob G120A · Aileron Control SystemSDR 2003FA0000554Bearing · failedDURING INSPECTION OF AIRCRAFT, FOUND BEARING TO BE FAILING. RETAINING CLIP AND SEAL WERE BEING FORCED OUT OF BEARING.May 12, 2003 · N867AF · Grob G120A · Aileron Control SystemSDR 2003FA0000553Bearing · failedDURING INSPECTION OF AIRCRAFT, FOUND BEARING TO BE FAILING. RETAINING CLIP AND SEAL WERE BEING FORCED OUT OF BEARING.May 12, 2003 · N867AF · Grob G120A · Aileron Control SystemSDR 2003FA0000548Bearing · failedDURING INSPECTION FO AIRCRAFT, FOUND BEARING TO BE FAILING. RETAINING CLIP AND SEAL WERE BEING FORCED OUT OF BEARING. PROBABLE CAUSE IS A DESIGN FLAW IN THE CONTROL SYSTEM WHICH ALLOWS THE CONTROL ROD DEFLECTION TO EXCEED THE DESIGN LIMIT OF THE BEARING. REMay 12, 2003 · N867AF · Grob G120A · Aileron Control SystemSDR 2003FA0000541Bearing · failedDURING INSPECTION OF AIRCRAFT, FOUND BEARING TO BE FAILING. RETAINING CLIP AND SEAL WERE BEING FORCED OUT OF BEARING. PROBABLE CAUSE IS A DESIGN FLAW IN THE CONTROL SYSTEM WHICH ALLOWS THE CONTROL ROD DEFLECTION TO EXCEED THE DESIGN LIMIT OF THE BEARING. REMay 12, 2003 · N867AF · Grob G120A · Aileron Control SystemSDR 2003FA0000348Pump · overheatedTHE HYDRAULIC PUMP CIRCUIT BREAKER KEEPS POPPING WHILE PUMP BUILDS UP PRESSURE. NO WARNING LIGHT COMES ON TO INDICATE PUMP IS GETTING HOT. HOWEVER WHEN YOU TOUCH THE PUMP WITH YOUR HAND IT IS HOT.Mar 20, 2003 · N867AF · Grob G120A · Hydraulic Pump (Electric/Engine), MainSDR 2003FA0000345Relay · damagedDURING PROGRESSIVE INSPECTION FOUND BAD RELAY AND DIODES BOARD HAD OPEN ON PC BOARD BETWEEN PC BOARD AND GEAR CONTROL RELAY.Mar 20, 2003 · N867AF · Grob G120A · Landing Gear Retraction/Extension SystemSDR VJ32003F00022Clock · brokenLT HAND STOP PIN BROKEN OFF FROM NORMAL USE.Jan 24, 2003 · N867AF · Grob G120A · Independent InstrumentsSDR VJ32003F00006Motor · failedDURING PROGRESSIVE INSPECTION AFTER BLOWING GEAR DOWN AND CYCLING GEAR MOTOR WINDING SMELLED AS BURNED OUT. GEAR WOULD NOT CYCLED AFTER THAT AND WOULD POP CIRCUIT BREAKER TO THE HYDRAULIC PUMP RCCB. MOTOR ACTED AS IF THE LOAD WAS TO HEAVY FOR THE MOTOR TO PRDec 9, 2002 · N867AF · Grob G120A · Hydraulic Pump (Electric/Engine), MainSDR VJ32003F00014Pump · erraticDURING GROUND RUN FUEL PRESSURE READINGS WERE ERRATIC AND HIGH. FUEL PUMP SHAFT FEELS ROUGH COULD BE CAUSE TO HIGH READINGS. NO RECOMMENDATION AT THIS TIME.Nov 27, 2002 · N867AF · Grob G120A · Engine Fuel PumpSDR VJ32002F00090Valve · leakingDURING ANNUAL INSPECTION OF AIRCRAFT HYDRAULIC PRESSURE WOULD NOT HOLD. TROUBLESHOOTING INDICATED THAT THE EMERGENCY MAINIFOLD VALVE WAS BLEEDING DOWN. REPLACED MANIFOLD VALVE.Oct 14, 2002 · N867AF · Grob G120A · Hydraulic System, MainSDR VJ32002F00088Ring · damagedFOLLOWING A ROUTINE FLIGHT, A ROUTINE INSPECTION FOUND THAT THE AFT ALTERNATOR BELT GROOVE HAD BROKEN AWAY FROM THE STARTER RING ASSY. THIS HAD CAUSED THE BELT TO BE DAMAGED BEYOND USE. PIECES OF MATERIAL FROM THE STARTER RING AND RUBBER FROM THE BELT WERE FOct 11, 2002 · N867AF · Grob G120A · Engine Starter
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