Reims F406

Service difficulty reports · 77

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 = 'F406'
  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 AUS20021189Lead · broken(AUS) STARTER-GENERATOR FAULTY. INSPECTION FOUND SEVERAL BRUSH LEADS BROKEN AND COMMUTATOR DAMAGED.Oct 16, 2002 · Reims F406 · Electrical Power System WiringSDR AUS20021058Rudder · fod(AUS) RUDDER DAMAGED BY ANOTHER AIRCRAFT TAXIING PAST. THE RUDDER SKINWAS DENTED AND BUCKLED AT THE MID POINT OF THE TRAILING EDGE. DURING DISASSEMBLY FOR REPAIR A PORTION OF THE RIB WAS ALSO DAMAGED.Sep 17, 2002 · Reims F406 · Rudder StructureSDR AUS20020918Link · cracked(AUS) COPILOTS OUTBOARD BRAKE PEDAL RH LINK ASSEMBLY CRACKED IN THE AREA OF THE WELD ATTACHING THE CLEVIS RODEND.Aug 12, 2002 · Reims F406 · Landing Gear Brake SystemSDR AUS20020678Motor · failed(AUS) REAR AIRCONDITIONING COMPRESSOR ELECTRIC MOTOR FAULTY. THECIRCUIT BREAKER WAS POPPED AND WHEN RESET, THE MOTOR WAS SPARKING EXCESSIVELY AND EMITTING SMOKE AT THE COMMUTATOR.Jun 29, 2002 · Reims F406 · Cabin Cooling SystemSDR AUS20020403Switch · faulty(AUS) DURING CRUISE THE LT WING OVERHEAT LIGHT ILLUMINATED. INVESTIGATION FOUND NO EVIDENCE OF BLEED AIR LEAK OR OVERHEAT CONDITION. SUSPECT FAULTY OVERHEAT SWITCH.Apr 27, 2002 · Reims F406 · Overheat DetectionSDR AUS20011294Cooling Fan · failed(AUS) SURVEILLANCE RADAR COOLING FAN FAILED.Dec 9, 2001 · Reims F406 · Air Distribution SystemSDR AUS20011311Ignition Lead · chafed(AUS) RT IGNITER LEAD ON BOTH ENGINES CHAFING ON FUEL LINE TO FLOW DIVIDER.Dec 6, 2001 · Reims F406 · Ignition Harness (Distribution)SDR AUS20011310Channel · cracked(AUS) NOSE LANDING GEAR ACTUATOR ATTACHMENT STRUCTURE CHANNEL CRACKED.FOUND DURING INSPECTION IAW AD/F406/7.Dec 6, 2001 · Reims F406 · Fuselage, Landing Gear Attach FittingsSDR AUS20011309Actuator · contaminated(AUS) ELEVATOR TRIM TAB ACTUATORS LUBRICATED WITH THE INCORRECT GREASE. ACTUATORS FREEZING IN FLIGHT. MAINTENANCE MANUAL SPECIFIES "TRIBOLUBE" ONLY. PERSONNEL/MAINTENANCE ERROR. UNAPPROVED PART.Dec 6, 2001 · Reims F406 · Elevator Tab Control SystemSDR AUS20011004Pump · failed(AUS) HYDRAULIC PUMP FAULTY. INVESTIGATION FOUND THE PUMP CIRCLIP GROOVE WORN ALLOWING THE CIRCLIP TO SEPARATE AND THE SPLINE ADAPTER PNO 24100-646 TO DISENGAGE FROM THE ENGINE DRIVE.Sep 18, 2001 · Reims F406 · Hydraulic Pump (Electric/Engine), MainSDR AUS20010690Detector · faulty(AUS) LIFT DETECTOR FAULTY. INVESTIGATION FOUND THAT THE AIRCRAFT WIRING (WIRE NO A2K4S-20P3) HAD BEEN CUT APPROXIMATELY 76.2MM (3IN) UP FROM THE FORWARD SIDE CONSOLE CONNECTOR AND CONNECTED TO THE STALL WARNING HORN. PERSONNEL/MAINTENANCE ERROR. UNAPPROVED MOJul 2, 2001 · Reims F406 · Stall Warning SystemSDR AUS20010655Detector · faulty(AUS) LIFT DETECTOR FAULTY. SWITCH OPERATES IN OPPOSITE SENSE.Jun 26, 2001 · Reims F406 · Stall Warning SystemSDR AUS20010734Control Cable · worn(AUS) LH AND RH AILERON CABLES (4OFF) LOCATED IN WING WORN.Jun 22, 2001 · Reims F406 · Aileron Control SystemSDR AUS20010656Detector · faulty(AUS) LIFT DETECTOR FAULTY. DETECTOR MICROSWITCH OPERATES IN OPPOSITE SENSE. SWITCH SPRING LOADED UP. PERSONNEL/MAINTENANCE ERROR.MANUFACTURING ERROR.Jun 20, 2001 · Reims F406 · Stall Warning SystemSDR AU010004Computer · faulty(AUS) AUTOPILOT COMPUTER SUSPECT FAULTY.Jan 4, 2001 · Reims F406 · Autopilot ComputerSDR AU000837Switch · faulty(AUS) LEFT AUTOFEATHER MICROSWITCH FAULTY. (X)Aug 28, 2000 · Reims F406 · Propeller Feathering/ReversingSDR AU000881Wire · misinstalled(AUS) NR 2 FIRE BOTTLE SQUIB WIRING INCORRECTLY WIRED TO THE BOTTLE ARM/FIRING SWITCH. SUBMITTER STATED THIS WOULD HAVE PREVENTED OPERATION OF THE FIRE BOTTLE. SUSPECT MANUFACTURING ERROR. (X)Aug 10, 2000 · Reims F406 · Extinguishing SystemSDR AU000912Strut · failed(AUS) NOSE LANDING GEAR OLEO OVER EXTENDED ALLOWING TORQUE LINKS TO INVERT. CAUSED BY OLEO UPPER BEARING LOOSENING FROM PISTON BARREL. (X)Jul 6, 2000 · Reims F406 · Nose/Tail Landing Gear Strut/AxleSDR AU000559Mount · cracked(AUS) LEFT ENGINE MOUNT CRACKED. FOUND DURING MAGNETIC PARTICLE INSPECTION.Jul 4, 2000 · Reims F406 · Engine Mount SectionSDR AU000203Retainer · damaged(AUS) LEFT PROPELLER FEEDBACK RING RETAINING CIRCLIP DEFORMED. PROPELLER WENT TO UNCOMMANDED FULL REVERSE ON LANDING.Apr 20, 2000 · Reims F406 · Propeller Blade SectionSDR AU990927Stall Warning · faulty(AUS) STALL WARNING VANE TIGHT TO MOVE IN BEARINGS CAUSING INTERMITTENT STALL WARNING INDICATIONS.Aug 6, 1999 · Reims F406 · Stall Warning SystemSDR AU990401Frame · mismanufactured(AUS) CANTED RIB UPPER CAP AT FS 177.45 CONTAINED MISDRILLED HOLES. FOUND DURING INSPECTION IAW RHEIMS SERVICE BULLETIN CAB 98-16.Jan 28, 1999 · Reims F406 · Fuselage Main, FrameSDR AU981618Rib · cracked(AUS) DURING INSPECTION, SEVERAL HAIR LINE CRACKS WERE DISCOVERED IN THE CANTED RIB UPPER CAP IN THE CENTER WING CARRY-THROUGH AREA. THIS IS SECOND AIRCRAFT IN THE FLEET WITH CRACKS - REFER OPERATOR CONTROL NR AU981565. FOUND IAW RHEIMS SB CAB98-16.Dec 7, 1998 · Reims F406 · Fuselage Miscellaneous StructureSDR AU981565Rib · cracked(AUS) CANTED RIB CRACKED. FOUND DURING INSPECTION IAW SB CAB98-16.Nov 27, 1998 · Reims F406 · Fuselage Miscellaneous StructureSDR AU980943Manifold · corroded(AUS) GYRO PRESSURE MANIFOLD CORRODED. MANIFOLD IS CONSTRUCTED FROM CADMIUM PLATED STEEL. STEEL ELBOW ALSO CORRODED.Jul 26, 1998 · Reims F406 · Pitot/Static SystemSDR AU980811Door · warning(AUS) DOOR UNLOCKED WARNING LIGHT ILLUMINATED. LIMITED INFORMATION PROVIDED.Jul 15, 1998 · Reims F406 · Door Warning SystemSDR AU980066Tire · damaged(AUS) TIRE CONTAINED FLAT SPOT. FOUND DURING INSPECTION FOLLOWING ABORTED TAKEOFF DUE TO BIRD STRIKE AVOIDANCE.Jan 30, 1998 · Reims F406 · Tire
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