Reims F406

Service difficulty reports · 77

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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 CA151228007Engine · smoke(CAN) WHILE LANDING ON A TRAINING FLIGHT, AFTER THE REVERSE WAS APPLIED AND STOWED NORMALLY, THE LT ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED. THE PILOT TRIED TO INCREASE POWER BUT NO RESPONSE. WHITE SMOKE COULD BE SEEN LEAVING THE COWLING AFT AND EXHAUST. EDec 13, 2015 · Reims F406 · Engine (Turbine/Turboprop)SDR EPUA20151006001Circuit Breaker · overheatedDURING CRUISE FLIGHT WITH LT & RT PROP DE-ICE SELECTED ON, THE PILOT OBSERVED SMOKE COMING OUT OF THE LT PROP DE-ICE SWITCH & CB. THE PILOT ATTEMPTED TO TURN THE SWITCH & CB OFF, & DISCOVERED IT WAS STUCK IN THE ON POSITION. PILOT ISOLATED THE BUSS FOR THE SOct 6, 2015 · N6590Y · Reims F406 · AC Power Distribution SystemSDR EPUA20151006002Bar · crackedDURING INSPECTION IAW SB F406-104 PART B & AD 2015-16-07, CRACKS WERE DISCOVERED ON PN 5115260-1 LT & PN 5115260-3. RT RUDDER BARS VIA MAGNETIC PARTICLE INSPECTION.Oct 2, 2015 · N861FT · Reims F406 · Rudder Control SystemSDR EPUA080415004Bar · crackedDURING INSPECTION IAW SB F406-104 PART B A CRACK WAS DETECTED ON RT RUDDER BAR ASSEMBLY, PN 5115260-2, RT & LT RUDDER BAR ASSEMBLY PN 5115260-1 VIA MAG PARTICLE INSPECTION. THIS SERVICE BULLETIN IS REQUIRED.Aug 4, 2015 · N6590Y · Reims F406 · Rudder Miscellaneous StructureSDR EPUA080415003Bar · crackedDURING INSPECTION IAW SB F406-104 PART B A CRACK WAS DETECTED ON RT RUDDER BAR ASSEMBLY PN 5115260-2 VIA MAG PARTICLE INSPECTION. THIS SERVICE BULLETIN IS REQUIRED IAW EAD 2015-0159-E.Aug 4, 2015 · N6591R · Reims F406 · Rudder Miscellaneous StructureSDR CA150408006Engine · malfunctioned(CAN) DURING ROUTINE SURVEILLANCE MISSION, CREW REPORTED LOUD NOISE FOLLOWED BY A ROLL BACK IN TORQUE TO ZERO & CORRESPONDING YAW. THE HIGH PRESS NH & LOW PRESS NL COMPRESSOR ROTOR SPEED MAINTAINED ROTATION. THE CREW FEATHERED PROPELLER & COMPLETED SHUTDOWNMar 27, 2015 · Reims F406 · Engine (Turbine/Turboprop)SDR EPUA20141121001Caliper · leakingRIGHT BRAKE LEAKING HYD FLUID & NOT WORKING. REPLACED RT BRAKE CALIPER ASSEMBLY, BLED BRAKES & PERFORMED BRAKE BURN IN PROCEDURE.Nov 21, 2014 · N861FT · Reims F406 · BrakeSDR EPUA20140919001O-Ring · leakingDURING GND OPERATIONS THE LT MAIN BRAKE SYS FAILED. REPLACED THE O RINGS FOR THE LT MLG CALIPER & BLED THE HYD FLUID.Sep 17, 2014 · N6591R · Reims F406 · Landing Gear Brake SystemSDR EPUA20140220001Door · unsecureAFTER LANDING & DURING TAXI TO PARKING AREA, THE RT MLG DOOR WAS SEEN FALLING OFF OF ACFT. NO ADDITIONAL DAMAGE TO ACFT OCCURRED DURING THIS EVENT. DETERMINED THAT THE ATTACHED HARDWARE FOR THE GEAR DOOR HAD FALLEN OUT.Feb 20, 2014 · N6591R · Reims F406 · Landing Gear DoorsSDR CA131021018Blade · fractured(CAN) DURING CLIMB, THE PILOT HEARD A LOUD NOISE FROM NR 2 ENGINE. HE THEN NOTICED TORQUE HAD DROPPED TO 20 PERCENT BUT HE FELT NO PHYSICAL POWER CHANGE AND ASSUMED AN INDICATION PROBLEM. THE POWER LEVER WAS RETARDED, THE NOISE REMAINED BUT THE NOISE PITCH Oct 15, 2013 · Reims F406 · Turbine SectionSDR CA130513003Engine · flamed out(CAN) THE OPERATOR REPORTED THE ENGINE FLAMED OUT WHILE TRANSITIONING FROM REVERSE TO IDLE AFTER LANDING. THE ACFT WILL BE FERRIED FOR AN INVESTIGATION WITH THE PRESENCE OF MFG REP. MFG WILL INVESTIGATE TO ESTABLISH ROOT CAUSE AND SUPPLEMENT THE REPORT ONCE Apr 23, 2013 · Reims F406 · Engine (Turbine/Turboprop)SDR EPUA20121107001Landing Gear · inoperativeDURING LANDING PROCEDURES, ON APPROACH, THE PILOT REPORTED THE NOSE GEAR FAILED TO EXTEND. ACFT LANDED WITH THE NOSE LANDING GEAR RETRACTED.Nov 7, 2012 · N861FT · Reims F406 · Nose/Tail Landing GearSDR CA120813014Engine · stopped(CAN) REPORTEDLY, THE NR 1 ENGINE HAD A SUDDEN STOPPAGE IN FLIGHT. THE ACFT LANDED SAFELY. FSR REQUESTING FURTHER DETAILS. MFG IS FULLY COMMITTED TO ADDRESS THIS ISSUE PROACTIVELY AND WE WILL KEEP OPERATORS INFORMED OF OUR PROGRESS.Aug 7, 2012 · Reims F406 · Engine (Turbine/Turboprop)SDR EPUA20120530001Switch · contaminatedLANDING GEAR POPPED BREAKER WHEN GEAR HANDLE SWITCHED DOWN TO UP; CLEANED MOISTURE IN NOSE GEAR SWITCHES, SWUNG GEAR IAW F406 MM NUMEROUS TIMES. CHECKED GOOD. SENT OF OPS TEST FLIGHT. FLIGHT CHECKED GOOD.May 29, 2012 · N861FT · Reims F406 · Landing Gear Position and WarningSDR EPUA20120320003Brake · malfunctionedNO LEFT BREAK, RT & LT MAIN BRAKE CALIPER, LEAK AND OPS CHECKED GOOD.Mar 17, 2012 · N6590Y · Reims F406 · Landing Gear Brake SystemSDR 2012FA0000118Fork · shearedAFTER LANDING AND WHILE TAXIING TO THE END OF A ROUGH ASPHALT RUNWAY, THE 2 INCH ROUND BAR SHEARED 9 INCHES FROM THE AXLE. NO PREVIOUS INDICATION OF POTENTIAL FAILURE HAD BEEN NOTED. TEMPS WERE AT -28 DEGREES F.Jan 28, 2012 · N406SD · Reims F406 · Main Landing GearSDR EPUA20120112002Switch · faultyGREEN LIGHT-GEAR DOWN LIGHT ON NOSE WHEEL DOES NOT TURN ON, MX REPLACED 602EN600-6 SWITCH FOR THE NOSE GEAR DOWN LOCK OVER CENTER INDICATOR SYS.Dec 7, 2011 · N861FT · Reims F406 · Landing Gear Position and WarningSDR CA110627012Turbine Blades · fractured(CAN) UNCONTAINED EVENT SHORTLY AFTER DEPARTURE, THE PILOT NOTED THAT THE LT ENGINE TORQUE WAS FLUCTUATING, WHICH WAS FOLLOWED BY A LOUD NOISE AND FLAMES FROM THE EXHAUST. THE ENGINE WAS SHUTDOWN AND A UNEVENTFUL SINGLE ENGINE LANDING WAS MADE AT THE DEPARTURJun 16, 2011 · Reims F406 · Turbine SectionSDR EPUA040808Skin · crackedDURING A ROUTINE INSPECTION A LARGE STRESS CRACK WAS DISCOVERED EMANATING FROM THE BASE OF THE UPPER VHS COMM ANTENNA BASE AT FS 154.80 RIGHT OF CENTERLINE. THE DAMAGED SKIN WAS REMOVED AND REPLACED, WITH NEW DOUBLER AND ANTENNA. AIRCRAFT WAS RETURNED TO SERApr 8, 2008 · N406GV · Reims F406 · Fuselage Main, Plate/SkinSDR EPUA120107Spar · crackedDURING ROUTINE SCHEDULED MAINTENANCE, A CRACK WAS DISCOVERED APPROX 6.5" LONG IN A U-SHAPED PATTERN ON THE LT WING MAIN SPAR AT LT CWS 51.00 TO CWS 48.00, EMANATING FROM THE UPLOCK BRACKET ATTACHMENT POINT TO THE MAIN SPAR. THE UPLOCK BRACKETS WERE ALSO BROKEDec 1, 2007 · N6590Y · Reims F406 · Wing SparSDR CA070704012Seal · fractured(CAN) IN CRUISE, ENGINE OIL PRESSURE WAS SEEN TO FLUCTUATE AND SUBESQUENTLY DECREASE. OIL WAS SEEN ESCAPING FROM THE ENGINE NACELLE. THE ENGINE WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INVESTIGATION REVEALED A FRACTURED HYDRAULIC PUMP PAD OIL SEAL. (TC NR 2007070May 11, 2007 · Reims F406 · Hydraulic Pump (Electric/Engine), MainSDR AU510002062Tire · deflated(AUS) RT MAIN LANDING GEAR TIRE DEFLATED. SUSPECT TIRE DAMAGED BY FOD.(OTHER CAUSE: MATERIAL ) (CASA NR 510002062)Dec 12, 2005 · Reims F406 · TireSDR AU510001897Cooling Fan · odor(AUS) ODOR IN COCKPIT. INVESTIGATION FOUND ODOR ONLY BECAME PRESENT WHEN THE AIR CONDITIONING SYSTEM WAS SELECTED OFF. FURTHER INVESTIGATION FOUND THE ODOR CAME FROM RECENTLY INSTALLED AVIONICS INSTRUMENT COOLING FANS. FANS WERE CHECKED SERVICEABLE. FANS HAD BDec 12, 2005 · Reims F406 · Air Distribution FanSDR AU510001479Indicator · faulted(AUS) LH VERTICAL SPEED INDICATOR (VSI) NEEDLE FLUCTUATING. GROUND TEST COULD FIND NO FAULTS WITH THE SYSTEM. NO FURTHER REPORTS OF PROBLEMS. (OTHER CAUSE: UNKNOWN ) (CASA# 510001479)Dec 12, 2005 · Reims F406 · Rate of Climb IndicatorSDR AU510001853Control Column · sticking(AUS) CONTROL YOKE STICKING DURING ROLL INPUT. INVESTIGATION FOUND THE CONTROL YOKE CONTACTING THE LT DEFOG VENT. FURTHER INVESTIGATION FOUND THE BOLT HOLES CONTAINED WITHIN THE CONTROL COLUMN YOKE WERE ELONGATED. (CASA NR 510001853)Nov 9, 2005 · Reims F406 · Control Column SectionSDR AU510001986Engine · failed(AUS) RT ENGINE FAILED DURING LANDING ROLL WHEN REVERSE THRUST WAS DE-SELECTED. THOROUGH INVESTIGATION COULD FIND NO CAUSE FOR THE DEFECT. SUSPECT THE FUEL FLOW MAY HAVE DROPPED TOO FAR WHILE REDUCING NEGATIVE THRUST TO A POINT THAT THE ENGINE FLAMED OUT. THEOct 10, 2005 · Reims F406 · Engine (Turbine/Turboprop)SDR AU510001441Antenna · failed(AUS) NR 2 HF ANTENNA BROKE AT EMPENNAGE ATTACHMENT POINT.May 6, 2005 · Reims F406 · HF Communications SystemSDR AU510001450Odor · detected(AUS) ELECTRICAL BURNING ODOR IN CABIN. INVESTIGATION CONTINUING. (OTHER CAUSE: PENDING FINAL REPORT ) (CASA 510001450)Apr 6, 2005 · Reims F406 · Air Distribution SystemSDR AU510001480Motor · failed(AUS) REAR AIR CONDITIONING SYSTEM ELECTRIC MOTOR FAILED. (CASA# 510001480)Apr 5, 2005 · Reims F406 · Cabin Cooling SystemSDR AU510001669Wheel · cracked(AUS) LT MLG WHEEL ASSEMBLY HAD 2 SECTIONS OF THE BEAD MISSING. TIRE DEFLATED DURING LANDING ROLL. (CASA NR 510001669)Jan 8, 2005 · Reims F406 · Wheel/Ski/FloatSDR CA050419002Engine · inoperative(CAN) DURING TAKEOFF, THE ENGINE EXPERIENCED AN UNCOMMANDED POWER REDUCTION. MFG WILL MONITOR THE INVESTIGATION OF THIS INCIDENT AND WILL ADVISE OF ROOT CAUSE, ONCEESTABLISHED.Nov 25, 2004 · Reims F406 · Engine (Turbine/Turboprop)SDR AUS20040496Truss · corroded(AUS) LT ENGINE LOWER LT ATTACHMENT TRUSS CORRODED.Jun 7, 2004 · Reims F406 · Engine Mount SectionSDR AUS20040374Wire · broken(AUS) FLAP CONTROL SYSTEM WIRE BROKEN. FAULT TRACE TO BROKEN WIRE A157B-A25799200 TO FLAP UP CONTROL SWITCH.May 7, 2004 · Reims F406 · Flight Control System WiringSDR AUS20040350Strip · separated(AUS) STALL STRIP MISSING.Apr 23, 2004 · Reims F406 · Stall Warning SystemSDR AUS20040385Computer · faulty(AUS) AUTOPILOT COMPUTER FAULTY.Apr 14, 2004 · Reims F406 · Autopilot ComputerSDR AUS20040214Clamp · failed(AUS) LT ENGINE PROPELLER REVERSING LEVER CABLE CLAMP BOLT FAILED ALLOWING PROPELLER REVERSING PY LEVER TO DISCONNECT FROM PUSH/PULL CABLE.Mar 20, 2004 · Reims F406 · Propeller Feathering/ReversingSDR EPUA070304AFire Loop · chafedAS FLIGHT ENTERED DOWNWIND, THE RT FIRE WARNING LIGHT ILLUMINATED. ENGINE WAS SHUTDOWN AND FLIGHT LANDED WITHOUT INCIDENT. MX FOUND THE AFT FIRE LOOP WAS CHAFFED UNDER CLAMP.Mar 7, 2004 · N406GV · Reims F406 · Fire DetectionSDR AUS20040137Servo · faulty(AUS) AUTOPILOT ROLL SERVO CAPSTAN FOUND IN PIECES ON AIRCRAFT FLOOR. SIX FASTENEING SCREWS FOUND IN CLOSE PROXIMITY TO THE SERVO MOUNT.Feb 29, 2004 · Reims F406 · Autopilot Main ServoSDR AUS20040060Altimeter · faulty(AUS) ALTIMETER FITTED TO AIRCRAFT WITH INCORRECT ALTITUDE RANGE. PERSONNEL/MAINTENANCE ERROR.Feb 3, 2004 · Reims F406 · Altimeter, Barometric/EncoderSDR AUS20040059Altimeter · faulty(AUS) ALTIMETER FITTED TO AIRCRAFT WITH INCORRECT ALTITUDE RANGE. PERSONNEL/MAINTENANCE ERROR.Feb 3, 2004 · Reims F406 · Altimeter, Barometric/EncoderSDR AUS20040071Controller · failed(AUS) COMMUNICATION SYSTEM CONTROL BOX FAILED.Jan 25, 2004 · Reims F406 · Communications SystemSDR AUS20031121Tire · deflated(AUS) NOSE WHEEL TIRE DEFLATED. NO DAMAGE TO WHEEL RIM. NOSE WHEEL MUD GUARD MISSING. INVESTIGATION FOUND THE VALVE STEM SHEARED FROM THE TUBE. SUSPECT VALVE STEM FAILURE CAUSED BY FATIGUE AND AGING OF THE RUBBER AROUND THE VALVE BASE.Nov 6, 2003 · Reims F406 · TireSDR AUS20031067Spar Cap · corroded(AUS) RT WING MAIN SPAR LOWER SPAR CAP CORRODED. MICROBIOLOGICAL GROWTH FOUND ON INSIDE OF FUEL ACCESS PANELS 621BB AND 521BB AND 521CB.Oct 15, 2003 · Reims F406 · Wing SparSDR AUS20031013Switch · faulty(AUS) RT MAIN LANDING GEAR UPLOCK SWITCH FAILED.Oct 2, 2003 · Reims F406 · Landing Gear Position and WarningSDR AUS20031155Wire · broken(AUS) FLAP UP MICROSWITCH WIRE BROKEN. SWITCH IS LOCATED BEHINDFLAP SELECTOR.Aug 29, 2003 · Reims F406 · Flight Control System WiringSDR AUS20030775Motor · failed(AUS) FORWARD AIR CONDITIONER ELECTRIC MOTOR FAILED.Jul 31, 2003 · Reims F406 · Cabin Cooling SystemSDR AUS20030575Radome · bird strike(AUS) BIRDSTRIKE ON SURVEILLANCE RADOME.Jun 4, 2003 · Reims F406 · Aerodynamic FairingsSDR AUS20030457Switch · failed(AUS) NOSE LANDING GEAR ACTUATOR FAULTY. SWITCH OUT OF ADJUSTMENT.Apr 22, 2003 · Reims F406 · Landing Gear ActuatorSDR AUS20030403Clamp · corroded(AUS) NR 1 ENGINE SHUT DOWN FOLLOWING LT WING OVERHEAT WARNING.INVESTIGATION FOUND THE CLAMP ATTACHED TO THE PNEUMATIC FLOWCONTROL VALVE DOWNSTREAM FROM THE NO1 ENGINE BLEED PORT CORRODEDAND RUPTURED CAUSING EXCESSIVE AIR LEAKS.Apr 6, 2003 · Reims F406 · Pneumatic Distribution SystemSDR AUS20030378Actuator · faulty(AUS) NOSE LANDING GEAR ACTUATOR FAULTY.Mar 20, 2003 · Reims F406 · Landing Gear Actuator
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