Rearwin Junior 4000
Service difficulty reports · 47
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 = '4000' 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.
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 = '4000' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR PRIA020247170001Heat Shield · inflt separation#4 MAIN WHEEL ASSEMBLY HEAT SHIELDS MISSING. THEY DEPARTED THE AIRCRAFT AND WERE FOUND ON THE APRON BY AIRPORT OPERATIONS.IN PELLSTON REGIONAL AIRPORT (KPLN)SDR 2024F00123Windshield · crackedCLIMBING THROUGH FL260, APPROXIMATELY 10MINS AFTER DEPARTURE FROM BFI, WE RECEIVED A R WINDSHIELD HEAT FAIL AMBER CAS MESSAGE. FOLLOWING CHECKLIST PROCEDURE, WE RESET THE SWITCH. AFTER APPROXIMATELY 20 SECONDS FROM SWITCH RESET, THE RIGHT COPILOT'S WINDSHIELD SDR 2024FA0000081Carriage · wornWE HAVE SEEN NUMEROUS INSTANCES OF LOOSE BOLTS THAT CONNECT THE LINKS TO THE CARRIAGE ON THE NORDAM THRUST REVERSERS. THERE IS CURRENTLY NO INSPECTIONS THAT REQUIRE THESE BOLT TO BE INSPECTED OR LUBRICATED. THE CMM STATES A TORQUE VALUE OF 300 IN LBS. FOR THESSDR 2022F00514Window · fracturedAFTER DEPARTURE IN CLIMB THROUGH APPROXIMATELY 12000 FT. COPILOTS SIDE WINDOW SHATTERED. FLIGHT CREW DECLARED EMERGENCY AND RETURNED TO ORIGIN AIRPORT, WHILE STILL IN FLIGHT FLIGHT CREW REPORTS SEEING SPARKS AND BURNING SMELL COMING FROM WINDOW AND WINDOW CONTSDR 2022F00515Window · leakingWHILE IN CRUISE FLIGHT CREW HEARD LOUD WHISTLING NOISE COMING FROM PILOTS SIDE WINDOW PANEL B. DUE TO CONTINUING FAILURES AND UNRESOLVED ISSUES WITH WITH THIS MAKE MODEL AIRCRAFT AND BOTH PILOTS AND COPILOTS SIDE COCKPIT WINDOWS. FLIGHT CREW ELECTED TO DIVERT SDR 9JLA2022101331840Actuator · defectiveDURING POST FLIGHT CHECKS IT WAS DISCOVERED A TAIL DE-ICE FAULT CODES RATC 18 AND LATC 18. THE MAINTENANCE TEAM DETERMINED THE LEFT HORIZONTAL LEADING EDGE DEICE ACTUATOR WAS DEFECTIVE. THE ACTUATOR WAS REMOVED, AND A SERVICEABLE UNIT WAS INSTALLED. OPS CHECKSSDR 9JLA2022101331839Manifold · failedTHE FLIGHT CREW REPORTED THAT ON LANDING, AMBER "GROUND SPOILER FAIL" CAS MESSAGE WAS POSTED. INBD SPOILERS FAILED TO DEPLOY. THE MAINTENANCE TEAM TROUBLESHOT AND DETERMINED THE GROUND SPOILER MANIFOLD WAS DEFECTIVE. THE DEFECTIVE UNIT WAS REMOVED, AND A SERVISDR 2022F00256Autopilot Sys · inoperativePILOTO AUTOMATICO INOPERATIVO / AUTOPILOT INOPERATIVE DIREFERENCIAS EN INDICACION DE COMBUSTIBLE/FUE DIASEGGRE.SDR 2022F00225Terminal Block · burnedCREW SMELLED BURNING ODOR AND NOTICED A TRIPPED CIRCUIT BREAKER FOR THE LH WINDSHIELD ANTI-ICE, THEY DE-ACTIVATED LH WINDSHIELD ANTI-ICE. INVESTIGATION BY MAINTENANCE FOUND BURNT TERMINAL AT WIRING CONNECTIONS GOING TO LH WINDSHIELD HEAT PANELS.SDR 2022F00160Windscreen · crackedPIC REPORTS WHILE IN DESCENT AT APPROXIMATELY 27,000 FT. GETTING RED ECAS MESSAGE FOR RIGHT WINDSCREEN OVERHEAT, FLIGHT CREW TURNS OFF WINDSCREEN HEAT, HAS SIC CHECK RIGHT WINDSCREEN TO SEE IF IT FEELS HOT, SIC STATES WINDSCREENS ARE COLD. PIC TURNS ON RIGHT WSDR 2022F00106Windshield · damagedDURING PART 135 FLIGHT AIRCRAFT PILOTS SIDE FORWARD WINDSCREEN OUTER PANEL SHATTERED IN FLIGHT. FLIGHT CREW DIVERTED AND LANDED SAFELY. CAUSE OF FAILURE; INTERNAL SEAL AROUND THE WINDSCREEN ALLOWING WATER INTO WINDSCREEN HEATING ELEMENT WHICH SHORTED OUT, CAUSSDR 2022F00075Alternator · damagedALTERNATOR COOLING FAN ATTACHED TO DRIVE SHAFT SEIZED DURING TAXI CAUSING ALTERNATOR DRIVE SHAFT TO SHEAR AT SHEAR POINT ON ACCESSORY SPLINE. PROBLEM APPEARS TO BE TWO PINS PRESSED INTO COOLING FAN SHROUD WERE PRESSED IN TOO FAR DURING REASSEMBLY AT OVERHAUL.SDR 2022F00003None · noneDURING CRUISE FLIGHT THE CREW REPORTED GETTING A RIGHT THRUST REVERSER UNLOCK ANNUNCIATOR LIGHT ILLUMINATION. THEY DECLARED AN EMERGENCY WITH ATC AND BEGAN DECENT TO THE CLOSES AIRPORT THEY COULD LAND. THE CREW REPORTED THE UNLOCK ANNUNCIATOR LIGHT EXTINGUISHESDR 9JLA2021120831806Actuator · defectiveTHE FLIGHT CREW REPORTED THAT THE HORIZONTAL STABILIZER TRIM FAILED IN FLIGHT, THE FLIGHT CREW ELECTED TO DIVERT FLIGHT AND LAND TO INVESTIGATE THE FAULT. THE APPROACH AND LANDING WAS UNEVENTFUL. THE MAINTENANCE VENDOR TROUBLESHOT AND DETERMINED THE HORIZONTALSDR 9JLA2021120731804None · noneTHE FLIGHT CREW REPORTED THAT THE RIGHT ENGINE EXPERIENCED COMPRESSOR STALL DURING TAKEOFF POWER. THIS CONDITION WAS ALLOWED PER MEL AND OPERATIONS WERE CONTINUED WITH NO RESTRICTIONS. THE MAINTENANCE VENDOR DETERMINED THE FAULT WAS INTERNAL WITH THE ENGINE RESDR 9JLA2021093022798Control Module · defectiveTHE FLIGHT CREW REPORTED THAT AN AMBER STAB TRIM FAIL CAS MESSAGE POSTED ON TOP OF DESCENT. THE MAINTENANCE VENDOR TROUBLESHOT AND DETERMINED THE STABILIZER TRIM ELECTRONIC CONTROL MODULE WAS FAULTY. THE UNIT WAS REMOVED AND A REPAIRED UNIT WAS INSTALLED. OPS SDR 9JLA2021081222789Ecu · defectiveTHE FLIGHT CREW REPORTED AT APPROX. 1 HOUR INTO FLIGHT A YAW DAMPENER 1 AND 2 FAIL CAS AMBER MESSAGE WAS POSTED ALONG WITH A RUDDER FAULT CYAN CAS MESSAGE. THE MAINTENANCE TEAM TROUBLESHOT AND DETERMINED A DEFECTIVE RUDDER ELECTRONIC CONTROL UNIT. THE DEFECTIVSDR 9JLA2021072922790Pressure Sensor · defectiveTHE FLIGHT CREW REPORTED THAT DURING CLIMB OUT RECEIVING A RIGHT BLEED FAULT CAS MESSAGE. THE CREW RAN THE CHECKLIST AND ELECTED TO RETURN BACK TO THE AIRPORT AND LAND. LANDING WAS UNEVENTFUL. THE MAINTENANCE TEAM TROUBLESHOT AND DETERMINED THE FAULT HAD BEEN SDR 2021FA0000392None · wornPILOT REPORTS THE RIGHT HAND STARTER GENERATOR HAS SMOKE COMING FROM IT DURING START UP. COMPLIED WITH R&R OF AIRCRAFT STARTER GENERATOR. OPS TEST OK, AIRCRAFT OK FOR RTS.SDR 9JLA2021007012278Wire Harness · defectiveTHE FLIGHT CREW REPORTED THAT AFTER LANDING AN ANTI-SKID FAIL CAS MESSAGE WAS DISPLAYED. THE MAINTENANCE TEAM DETERMINED THAT THE RIGHT HAND OTBD MAIN LANDING GEAR WIRING HARNESS WAS DEFECTIVE. THE HARNESS WAS REPLACED WITH A NEW UNIT. OPS CHECKS GOOD, NO DEFESDR OZTA2021060323Windshield · failedA/C EXPERIENCED A FAILURE OF THE OUTER PANEL OF THE CO-PILOTS SIDE REAR WINDOW WHILE PASSING THRU FL250 & WITHIN MOMENTS OF CHECKING THE CHECKLIST THE WINDOW HAD A COMPLETE FAILURE FOLLOWED BY DECOMPRESSION. CREW EXECUTED AN EMERGENCY DESENT PROCEDURES & DECLASDR 2020F00108Anti-Ice Valve · bindsFLT. CREW REPORTS DURING CRUISE NUMEROUS CAS MESSAGES RELATED TO AIRCRAFT ANTI-ICE FAIL. AIRCRAFT DIVERTS BACK TO MAINTENANCE BASE KFRG, AFTER TROUBLESHOOTING FAILURE DETERMINED TO BE RH ENGINE ANTI-ICE VALVE INOPERATIVE. VALVE IS REPLACED WITH SERVICEABLE UNISDR 2020F00086Starter · overheatedAIR TURBINE STARTER SEVERE OVERHEAT RH ENGINE CAUSED FLIGHT CREW TO RECEIVE A RH ENGINE FIRE INDICATION DURING TAKEOFF. TAKEOFF WAS ABORTED AT 100 KTS. AIRCRAFT TAXIED BACK TO RAMP AIRPORT FIRE RESCUE DID RESPOND AND DETERMINE THERE WAS NO FIRE BUT AIR TURBINESDR ZLWA201903150001Unknown · malfunctionedGEAR SYSTEM FAIL CAS MESSAGE AFTER SELECTING GEAR DOWN. LEFT MAIN LANDING GEAR WOULD NOT EXTEND. GEAR DID FINALLY EXTEND ON IT'S OWN A COUPLE MINUTES LATER DURING THE MISSED APPROACH. THE LANDING GEAR WAS PINNED AND THE AIRCRAFT WAS FERRIED FOR INVESTIGATIOSDR CA160216008Warning Light · illuminated(CAN) THE AIRCRAFT WAS FLYING AT 43000 FT, WHEN THE PILOT EXPERIENCED FADEC FAULT BLUE WARNING THEN FADEC FAULT YELLOW WITH THE EVENTUAL UNCOMMANDED IN FLIGHT SHUTDOWN. THE AIRCRAFT WAS DIVERTED AND LANDED. TROUBLESHOOTING ONGOING.SDR CA151030008Warning System · activated(CAN) DURING TAKEOFF WITH AUTO-THROTTLE ENGAGED AT AN SPEED OF 60KTS, THE LEFT ENGINE FADEC FAULT CAME ON. THE TAKEOFF WAS ABORTED. THE FAULT MESSAGE DISAPPEARED WHEN THE THROTTLES WERE RETARDED TO IDLE. A 2ND TAKEOFF WAS ATTEMPTED WITHOUT AUTO-THROTTLE. WITH SDR 7SSA2015102801Radome · cockedAIRCRAFT WAS ON ITS 2ND LEG OF THE DAY ENROUTE. THE LANDING GEAR DID NOT DEPLOY WHEN SELECTED GEAR DOWN. DURING INVESTIGATION IT WAS DETERMINED THE RADOME HAD MOVED AFT ALLOWING THE AFT PORTION TO COVER THE FRONT LIP OF THE NOSE LANDING GEAR DOORS PREVENTING TSDR OZTA20150513001Reservoir · bypassingDURING CRUISE FL 410, THE RT HYD OVERHEAT CAS MSG POSTED. CREW FOLLOWED CHECKLIST DESCENDING TO FL350, CREW NOTED HYD TEMP RISING. AS TEMP STEADILY ROSE CREW ACCOMPLISHED A PRECAUTIONARY RT ENG SHUTDOWN. CREW DECLARED AN EMER & DIVERTED.SDR OZTA2015F00033Manifold · failedCREW EXPERIENCED AN ABNORMAL GEAR EXTENSION. WHEN THE GEAR WAS SELECTED DOWN THE NOSE GEAR DOORS OPENED AND THE NOSE GEAR DID NOT EXTEND. CREW DECLARED A MISS APPROACH AND HELD. CREW CYCLED GEAR 4 TIMES WITH NOSE GEAR NOT DEPLOYING. EMERGENCY GEAR EXTENSION SDR CA131007003Engine · failed(CAN) 5 MINUTES AFTER TAKEOFF, THE PILOT NOTICED A VIBRATION AND OBSERVED THE NR 2 ENGINE OIL PRESSURE HAD DROPPED TO ZERO. THE ENGINE THEN SHUTDOWN BY ITSELF. THE ACFT RETURNED TO THE DEPARTURE AIRPORT WHERE A SINGLE ENGINE LANDING WAS SAFELY ACCOMPLISHED. SDR 2012FA0000629Module · faultedON CLIMBOUT, FADEC FAULT INDICATED, AT 15000 FT ALTITUDE ENGINE NR 1 (LT) ROLLED BACK TO IDOL WITH FADEC FAIL INDICATION. PILOTS WERE UNABLE TO GET CONTROL OF ENGINE. DECLARED AN EMERGENCY AND LANDED WITH LT ENGINE AT IDLE. CONTROL OF RT ENGINE WAS NORMAL. SDR ZKFR2012011103243Actuator · leakingRT ENGINE, INBD THRUST REVERSER ACTUATOR LEAKING. MM SPECIFICALLY STATES THERE ARE NO ALLOWABLE LEAKAGE FOR COMPONENTS, FILTERS, PRESSURE SWITCHES, TRANSDUCERS, VALVES OR TUBING UNLESS SPECIFICALLY MENTIONED AND TO CONTACT MFG CUSTOMER SUPPORT WHEN ANY MX ON SDR ZKFR201201113243Actuator · leakingLT ENGINE, INBD THRUST REVERSER ACTUATOR LEAKING. MM SPECIFICALLY STATES THERE ARE NO ALLOWABLE LEAKAGE FOR COMPONENTS, FILTERS, PRESSURE SWITCHES, TRANSDUCERS, VALVES OR TUBING UNLESS SPECIFICALLY MENTIONED AND TO CONTACT MFG CUSTOMER SUPPORT WHEN ANY MX ON SDR ZKFR201112223218ACheck Valve · faultyPOTABLE WATER IN LAV HAS LOW PRESSURE AND PUMP CONTINUOUSLY CYCLES. R & R DRAIN CHECK VALVE. OPS CHECKED GOOD. INSPECTED CHECK VALVE ON BENCH AND FOUND VALVE NOT COMPLETELY CLOSING AND REQUIRING EXCESSIVE PRESSURE TO CLOSE AT ALL.SDR ZKFR201112223218CProcessor · faultedWITH ONLY APU RUNNING, MAU 2B FAULTED RESULTING IN THE APU SHUTING DOWN. PILOT RESTARTED APU AND FAULT DID NOT RETURN. MX COULD NOT DUPLICATE PROBLEM. FAULT HISTORY DOWNLOADED, CHANGE THE MAU 2 NIC 2 MODULE ASSY WITH PROCESSOR. OPS CHECKED GOOD.SDR ZKFR201112223218BWire · brokenAFT BAY MX LIGHT WILL NOT STAY ON. FOUND MULTIPLE BROKEN WIRES AT AFT STEP FAIRING, SWITCH TO SPLICE, ON LT AND RT SIDE OF ACCESS DOOR. REPAIRED AFFECTED WIRES. OPS CHECKED GOOD.SDR ZKFR201111153188BFan · inoperativeDURING POSTFLIGHT FOUND BOTH AFT BAY HEAT EXCHANGER FANS INOPERATIVE. R & R BOTH HEAT EXCHANGERS FANS. OPS CHECKED GOOD.SDR ZKFR113188AFan · inoperativeDURING POSTFLIGHT, FOUND BOTH AFT BAY HEAT EXCHANGER FANS INOP. R & R BOTH HEAT EXCHANGERS FANS. OPS CHECKS GOOD. MX RECOMMENDS OTHER OPERATORS CHECK FOR OPS AS THERE IS NO COCKPIT INDICATION WHEN THESE FANS FAIL AND THEY ARE FOR HEAT PROTECTION FOR THE COMSDR ZKFR201111153188DShutoff Valve · failedLT PACK FAILED IN FLIGHT WHEN THROTTLES PULLED TO IDLE. R & R LT PACK PRESSURE RELIEF SHUTOFF VALVE (PRSOV). SYS OPS CHECKS GOOD.SDR ZKFR201111153188Connector · disconnectedWHILE CHANGING LT AFT BAY HEAT EXCHANGER FOUND CB PANEL 3, PLUG P1634D, PIN: M FOR WIRE A201-W01-16 CAPPED AND TIED BACK CAUSING LT AFT BAY BLOWER TO BE INOPERATIVE. MECHANIC BELIEVES THIS TO BE DONE DURING ACFT PRODUCTION OR AT BLOCK 20 UPGRADE. MECHANIC RESDR ZKFR2011131600003Display · inoperativeDURING POST FLIGHT, FOUND CMC INOPERATIVE ON CO-PILOTS MFDU. FOUND FILE SERVER 2 AFSEM 2 FAULTED. PERFORMED TARGET LOAD OF SOFTWARE LOAD 20 AND SYS CHECKED GOOD.SDR ZKFR2011131600002Heater · inoperativeGALLEY DRAIN INOPERATIVE AT SINK AND COFFEE MAKER. FOUND HEATED DRAIN LINE IS NOT HEATING UP.SDR ZKFR201109286209Circuit Card · failedFOUND CMC CARD TO BE FAILED. R & R CMC MODULE ASSY (CARD). OPS CHECKS GOOD.SDR ZKFR201109233149Pump · leakingERS PUMP LEAKING. FOUND LEAKING FROM OVERBOARD DRAIN LINE. R & R ERS PUMP ASSY.SDR CA110818003Line · damaged(CAN) CUSTOMER REPORTED FUEL LEAK INBOARD IGNITER AREA. DURING WET MOTORING TEST FOUND FUEL COMING FROM BRAIDED FUEL LINE NEXT TO THE IGNITER GUIDE BOSS. PARTICULAR FUEL LINE IS CRIMPPED AND APPEARS TO BE BUBBLING OUT OF THE BOTTOM OF THE CRIMP. AS FUEL PRESSUSDR 2010F00110Pump · making metalDPI FOUND EXTENDED DURING PF INSPECTION. REMOVED FILTER AND FOUND MINOR METAL IN FILTER AND FILTER HOUSING. REPLACE RT HYDRAULIC ENGINE DRIVEN PUMP.SDR 2010F00109Pump · making metalDPI FOUND EXTENDED DURING INITIAL 100 HOUR INSPECTION. REMOVED FILTER AND FOUND METAL IN FILTER AND FILTER HOUSING. REPLACE RT HYDRAULIC ENGINE DRIVEN PUMP.
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