Williams FJ44-2A
Service difficulty reports · 63
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 = 'FJ442A' 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 engine_model_key = 'FJ442A' 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 HBKA202604160001Compressor · failed inspSHORTLY AFTER TAKE OFF, CREW WITNESSED THE LT ENGINE INDICATIONS STARTING TO ROLL BACK. THIS INDICATION HAPPENED BETWEEN 500 & 1000 FOR AGL. FELT THE DECELERATION OF THE ACFT. THE FLIGHT CREW REPORTED THERE WERE NO CAUTION OR WARNING LIGHTS PRESENT DURING THISDR 2025F00145Warning Light · multiple failTHROUGHOUT THE FLIGHT, OBSERVED THAT THE FUEL KEPT MOVING AROUND WITHOUT US MOVING THE FUEL TRANSFER SWITCH. WE WOULD EVENTUALLY TRY TO EVEN BOTH FUEL GAUGES OUT BUT THEY NEVER SEEMED TO BALANCE. THEY WOULD BALANCE FOR A SECOND, SO WE'D TURN THE FUEL SWITCH OFSDR ZKFA202408190193Pitot Line · contaminatedWHILE AT FL40 NOTED YELLOW IAS LIGHT ON BOTH PFD'S. DURING DESCENT NOTED A 60 KT SPLIT (BETWEEN PILOT AND COPILOT PFD). SWITCHED TO ADC2 AND A/S WERE NORMAL. PITCH TRIM ALSO WOULD NOT RESET, FLEW AIRCRAFT IN SBY TRIM. TECHNICIANS AT NASHVILLE, TN, KBNA WERE DISDR 5BMA2024050600359Engine · power lossWHILE CRUISING AT FL400 THE LEFT ENGINE ROLLED BACK. IMMEDIATELY, I TRIED TO MOVE THE THROTTLE TO A DIFFERENT POSITION TO SEE IF I HAD ANY AUTHORITY. I DID NOT. I DECLARED AN EMERGENCY WITH ATC AND STARTED A DESCENT TO KEEP THE SPEED UP. I DECIDED TO DIVERT TOSDR DIXA20220221Not Reported · not reportedDURING LANDING AIRCRAFT WAS ABOUT 50 FEET ABOVE THE GROUND JUST CROSSING RUNWAY THRESHOLD #2 ENGINE SHUTDOWN, AIRCRAFT LANDED WITHOUT INCIDENT, EMERGENCY WAS NOT DECLARED. WAITING ON TEXTRON AOG MAINTENANCE.SDR 2022FA0000036Engine · crackedON OCT 30,2021, #1 ENGINE HAD AN UN COMMANDED ENGINE SHUT DOWN. THE PILOTS LANDED AT THE SCHEDULED AIRPORT (KBKL) UNEVENTFUL. MAINTENANCE CONTACTED TEXTRON WHO CAME TO KBKL AND INVESTIGATED THE ISSUE. THEY DISCOVERED THE LP SWITCH TRIPPED. AFTER FURTHER INVESTSDR QZJA20210308004Valve · stuckUPON DEPARTURE, THE CREW NOTICED THE FOLLOWING MECHANICAL IRREGULARITY: “UNSCHEDULED BLEED AIR AS AIRCRAFT ROTATED OFF RUNWAY. PRESSURIZATION CONTROLLER INDICATED -1,400 FPM. ATTEMPTED TO STOP HOT AIR BY TURNING OFF PRESSURIZATION AND BLEED AIR. DID NOT SOLVE SDR WI5R2020111900001Rotor · damagedDURING DISASSEMBLY OF ENGINE SERIAL NUMBER 105163 FOR AN UNRELATED ISSUE, A LIBERATED 1ST-STAGE INTERMEDIATE PRESSURE COMPRESSOR (IPC) ROTOR BLADE WAS DISCOVERED. NO OPERATIONAL ISSUES RELATED TO THE IPC ROTOR BLADE ANOMALY WERE REPORTED BY THE FLIGHT-CREW.SDR QZJA20201119002Bleed Valve · intermittentON NOVEMBER 17, 2020 THE PILOT REPORTED: ABORTED THE TAKEOFF AT KABQ AT APPROXIMATELY 1712Z IN N1SH DUE TO A LOUD RUSHING OF AIR NOISE IN THE COCKPIT, FOLLOWED BY A LOT OF HOT AIR ENTERING THE COCKPIT. THIS HAPPENED AS THE THROTTLES WERE BROUGHT TO THEIR T/O SDR WI5R2020091190001Turbine · damagedFLIGHT CREW REPORTED THAT DURING TAKEOFF, AT APPROXIMATELY 3000 FT AGL, LT ENGINE EXHIBITED AN UNUSUAL NOISE ACCOMPANIED BY AN INCREASE IN INDICATED INTER-TURBINE TEMPERATURE (ITT) AND FOLLOWED BY UNCOMMANDED IN-FLIGHT SHUTDOWN OF THE ENGINE. AIRCRAFT LANDED SDR 2021FA0000083Fuel Feed · pilot errorCREW WAS FLYING IN CRUISE AND CROSSFEEDING FUEL FROM THE RIGHT TO THE LEFT TO CORRECT A FUEL IMBALANCE (R WING HEAVY). CREW WAS THEN INSTRUCTED BY ATC TO CLIMB; AT THIS POINT TOTAL FUEL WAS APPROX 950 LB (555 LB IN THE RIGHT WING, 395 LB IN THE LEFT WING). CRSDR SVGA20200527001Tire · blownWE TOOK OFF FROM 30C AT KIWA TO KSTS, WHERE OUR RT MAIN LANDING GEAR TIRE BLEW AFTER PASSING V1 AND CROSSED FROM THE CONCRETE PORTION OF THE RUNWAY TO THE ASPHALT. OUR TAKEOFF WEIGHT WAS 12,500LBS, THE WEATHER WAS VFR AND WE HAD FOUR PASSENGERS ON BOARD. ON SDR 2020FA0000519Potentiometer · contaminatedFLAP POTENTIOMETERS USED FOR INDICATION AND CONTROL OF THE TRAILING EDGE FLAPS WERE FOUND TO BE NOT ENVIRONMENTALLY SEALED. THE COMPONENTS WERE QUALIFIED FOR AN ENCLOSED LOCATION, NOT AN EXPOSED LOCATION WHERE THEY ARE INSTALLED. AFTER REPEATED FLAP FAILURESSDR WI5R20191218002Rotor · fracturedDURING A PRE-BUY BORESCOPE INSPECTION A MISSING IP BLADE AND HPC DAMAGE WAS NOTED.
DISASSEMBLY OF THE ENGINE CONFIRMED THAT ONE OF THE 3RD STAGE IPC ROTOR BLADES WAS MISSING.SDR WI5R2019090400001Blade · fracturedENGINE RETURNED TO REPAIR STATION AFTER FIELD REPORT OF "AFTER TAKE OFF ROLL, LOUD GRINDING NOISE FROM ENGINE AND ENGINE SHUTDOWN. ENGINE N1 WILL NOT ROTATE BY HAND." DISASSEMBLY IN THE REPAIR STATION FOUND SEVERAL COMPONENTS DAMAGED AND AN INVESTIGATION CONTSDR ODAR20190405001Bellows · rupturedRETURN FLIGHT KCHO TO KFCI, PILOT ENCOUNTERED RIGHT ENGINE FIRE ANNUNCIATION. SHUT RIGHT ENGINE DOWN AND DEPLOYED FIRE EXTINGUISHER PER AIRCRAFT ENGINE FIRE EMERGENCY CHECKLIST. PILOT DECLARED INFLIGHT EMERGENCY AND LANDED WITHOUT INCIDENT AT KFCI. MAINTENASDR 2020FA0000086Pump · failedAFTER TAKEOFF AND UPON PLACING THE GEAR TO THE UP POSITION THE HYD PRESS ON ANNUNCIATION REMAINED ON AND THE RED GEAR UNSAFE LIGHT ANNUNCIATION AND THE PUMP CONTINUED TO STAY RUNNING. FIRST OFFICER CALLED FOR THE HYD PRESS ON EMERGENCY PROCEDURES CHECKLIST. SDR 3EJA20161025001Fcu · failedAIRCRAFT ON APPROACH AT 5000FT. PF RETARDED THROTTLES TO IDLE TO SLOW DOWN AND RT ENGINE FLAMED OUT. SECURED ENGINE AND DECLARED AN EMERGENCY. AIRCRAFT LANDED UNEVENTFULLY. MANUFACTURER DETERMINED THAT THE FCU IS THE CAUSE OF THIS PROBLEM.SDR W9BA2016F00148Engine · shutdownDESCENDING THROUGH 10,000 MSL, THE THROTTLES WERE RETARDED TO IDLE. THE RT ENGINE IMMEDIATELY ROLLED BACK AND SHUTDOWN. LEFT THROTTLE WAS ADVANCED TO MAINTAIN AIRSPEED AND ALTITUDE. IGNITIONS WERE TURNED ON IAW THE CHECKLIST AND THE RT ENGINE STARTED BACK USDR SI6R20160705002Door · failedREMOVED CONDITIONED AIR DUCT FROM AFT PRESSURE BULKHEAD TO EXPOSE PLASTIC DOORS THAT ARE HINGED TO CHECK VALVE. PRESSURIZED AIRCRAFT IN HANGAR IN ACCORDANCE WITH MAINTENANCE MANUAL TO 8.0 PSI. PUSHED ON CHECK VALVE HINGED DOORS WITH HANDLE OF PLIERS, WHEN RESDR SI6R20160705001Check Valve · failedAIRCRAFT AT CRUISE AT 43,000'. CONDITIONED AIR DUCT CAME LOOSE FROM WATER SEPARATOR, CABIN BEGAN DEPRESSURIZING. CHECK VALVE LOCATED ON AFT PRESSURE BULKHEAD FAILED WHEN IT CLOSED BREAKING APART INTO CONDITIONED AIR DUCT LINE. AIRCRAFT BUILT IN 1980. HINGESDR YCOA20160113001Circuit Breaker · faultyAPPROXIMATELY 1300 LOCAL TIME, DEPARTED ON A POSITIONING FLIGHT FROM KPDK. CLIMBING THROUGH ~1000 FT AGL, CREW NOTED "R BLEED OVHT" ANNUNCIATION INDICATING A DUCT OVER HEAT CONDITION. CREW PERFORMED THE APPROPRIATE CHECKLIST WITH NO IMMEDIATE CHANGE IN CONDISDR CA150908019Valve · malfunctioned(CAN) ON CLIMBOUT, THE PILOT NOTICED AN UNUSUAL NOISE COMING FROM THE REAR OF THE ACFT. RECOGNIZING THE NOISE WAS COMING FROM THE RT ENGINE AND HEAT WAS COMING INTO THE ACFT FROM THE CABIN AIR-CONDITIONING SYS HE QUICKLY CONCLUDED THE PROBLEM WAS ORIGINATING SDR 3EJA2015FA0000327Landing Gear · malfunctionedDURING DECENT, A HYDRAULIC PRESSURE LIGHT ILLUMINATED AND RED GEAR UNLOCK LIGHT STEADY FLASHED WITH ASSOCIATED THUMPING. PULLED GEAR CONTROL CIRCUIT BREAKER AND HYDRO LIGHT EXTINGUISHED BUT RED "GEAR UNLOCKED LIGHT REMAINED ILLUMINATED. RIGHT MAIN GEAR DOWN SDR CA150629010Compressor · corroded(CAN) ON RT ENG START, N1 DID NOT TURN, PILOT SHUTDOWN THE ENG. HE WENT TO TURN THE FAN BY HAND & HE FIGURED THAT N1 FAN WAS STUCK IN PLACE. AFTER INSPECTION BY MX DEPT, N1 FAN IS STUCK IN CORROSION. ENG NEEDS TO BE REPAIRED. LT ENG INSPECTION DONE & FOUNDSDR CNQR2015050100174Fdu · stoppedDURING DESCENT, THROUGH 340FL THE RT ENGINE NR 2 SHUT-DOWN UNCOMMANDED. 2 ATTEMPTS WERE MADE TO RESTART THE ENGINE AT LOWER ALTITUDES BOTH BY WIND MILLING AND STARTER ASSIST UNSUCCESSFULLY. EMERGENCY LANDING DECLARED AND LANDED WITHOUT INCIDENT.SDR CA150415001Actuator · malfunctioned(CAN) "FLAP FAIL" ANNUNCIATOR ILLUMINATES IN FLIGHT SYSTEM CHECKS SERVICEABLE ON THE GROUND FLIGHT CONDITIONS: AFTER TAKEOFF AND ACFT AT CRUISE ALTITUDE AND SPEED WITH NO FLAP MOVEMENTS AND ABOUT 30 MINS INTO THE FLIGHT, FAULT RE-APPEARS, BUT ONCE THE ACFT LASDR CA141124004Valve · defective(CAN) RT BLEED OVERHEAT LIGHT ON DURING TAKEOFF.SDR 2014FA0000555Wheel · failedTHE BEAD ON THE RT HALF OF THE NOSE WHEEL SEPARATED CAUSING EXTENSIVE DAMAGE TO FUSELAGE BELLY. THE WHEEL DID NOT DEFLATE.SDR CA140902006Pump · leaking(CAN) ON DESCENT, CREW NOTICED A LOSS IN HYDRAULIC QTY AND FLUCTUATING HYDRAULIC PRESSURE. A/C LANDED SAFELY WITH OUT FURTHER INCIDENT. UPON INSPECTION, LT ENGINE HYD PUMP WAS FOUND LEAKING FLUID FROM A CRACK IN THE PUMP HOUSING. MAINTENANCE REPLACED THE HYD PSDR E81R2013052923713Spring · disengagedPILOT REPORTED LT ENGINE DC GENERATOR FAIL INDICATION DEPARTING AIRPORT. INVESTIGATED LT ENGINE STARTER/GENERATOR CONDITION UPON ARRIVAL AT DESTINATION. SUSPECTED INTERNAL ELECTRICAL FAILURE OF STARTER/GENERATOR DUE TO COMMUTATOR CONDITION AND AREA RESIDUE/ODOSDR WI5R20121218Blade · brokenDURING A PRE-BUY BOROSCOPE INSPECTION, IT APPEARED THAT AN IP ROTOR BLADE HAD BROKEN OFF AND GONE THROUGH THE CORE OF THE ENGINE. THIS WAS CONFIRMED UPON DISASSEMBLY. BLADE ON THE 3RD STAGE OF THE IP ROTOR WAS MISSING.SDR CNQR12172012585Oil System · low pressureLOSS OF OIL PRESSURE ON LEFT ENGINE AND HAD EXHAUST ODOR IN COCKPIT AND CABIN.SDR CA121017006Skin · unknown(CAN) MAINTENANCE WHEN TROUBLESHOOTING A RECURRING PROBLEM WITH THE RUDDER BOOST, FOUND WATER LEAKING INTO THE PYLON THROUGH A VENT HOLE THAT IS THERE TO PREVENT OVERHEATING OF THE PYLON.SDR CA120320005Duct · ruptured(CAN) DURING PHASE 4 INSPECTION, LT ENGINE COWL ANTI-ICING DUCTING WAS FOUND TO BE RUPTURED IN INTAKE COWL. PILOTS DID NOT REPORT ANY ABNORMAL OCCURANCES.SDR CA120109001Fuel Filter · contaminated(CAN) AN INTERMITTENT FUEL BYPASS INDICATION IN CRUISE ON THE ENGINE. UPON REFERENCING THE FLIGHT MANUAL, IT STATED TO EXPECT PARTIAL OR FULL POWER LOSS SO PRECAUTIONARY MEASURES WERE TAKEN. THE ENGINE SHOWED NO SIGNS OF PARAMETER SHIFTING AND ALL TEMPERATURESSDR 2011FA0000455Blade · failedTHE PILOT REPORTED A LOUD BANG AT 40K FT. DURING THE NEXT START, AT 15-20 PERCENT N2, THERE WAS A VIBRATION AND START ABORTED. AFTER WAITING 15-20 MINS, ANOTHER START ATTEMPTED, SOME VIBRATIONS AT 40 PERCENT N2, ENGINE STABILIZED. 40 MINS INTO FLT WAS ANOTSDR E81RJW3033120Oxygen Mask · sticking(E81R) DURING FUNCTIONAL TEST OF PAX OXYGEN SYS FOLLOWING SCHEDULED SOLENOID SHUTOFF VALVE O/H. NOTED FLOW INDICATORS IN ALL SIX CABIN PAX OXYGEN MASK ASSY'S, STICKING. FOUND OILY TYPE FILM & EVIDENCE OF MOISTURE CONTAMINATION IN AFFECTED MASK ASSY'S. CAUSINGSDR CA100927004Bearing · corrodedDURING INSP, FOUND BOTH BEARING CORRODED AND BOTH BEARING REPLACED.SDR CA100927003Bearing · corrodedNOSE WHEEL BEARING NOISY DURING TAXI AND GETS LOUDER WITH RUDDER APPLICATION (SIDE LOADING). DURING TROUBLESHOOTING, FOUND BOTH BEARING CORRODED.SDR E81R_JW30282_3Control Cable · seized(E81R) DURING REPLACEMENT OF RT ENG FWD POWER CONTROL CABLE ASSY FOR EXCESSIVE LEAKAGE IN CONJUNCTION WITH COMPLIANCE WITH SB 76-3907 FOUND NEW REPLACEMENT CABLE ASSY. SEIZED DURING INITIAL POST-INSTALLATION RIGGING CHECKS. REPLACED 1ST REPLACEMENT CABLE ASSSDR 2010FA0000458Lever · bindingAT START OF APPROACH, DISENGAGED AUTO-PILOT BUT FOUND CONTROLS AND TRIM STIFF OR JAMMED. COMMANDED AUTO-PILOT DISCONNECT AGAIN BUT NO CHANGE. TRIED ELECTRIC TRIM ALSO BUT WITHOUT CHANGE AND GOT NO TRIM MOTION. THEN SAW THAT AUTO-PILOT ENGAGE LEVER HAD NOT MSDR E81RJT227501Shutoff Valve · malfunctionedTROUBLESHOT INOPERATIVE RT ENG NACELLE INLET HEAT INDICATION AT IDLE. FOUND RT NACELLE INLET HEAT PRESSURE REGULATING/SHUTOFF VALVE FAILED. VALVE WAS INSTALLED 1/19/2010, AFTER O/H, REPLACED VALVE ASSY WITH ANOTHER O/H VALVE ASSY AND FUNCTIONAL CHECKS ON ENG GSDR E81RJW30228Fuel Control · malfunctionedINVESTIGATED REPORTED LT ENG SURGING AND "POPPING" AFTER START. REPLACED FUEL CONTROL ASSY. (HMU) WITH REPAIRED EXCHANGE UNIT, ENGINE OPERATIONS NORMAL. RECOMMEND ACCY MFG INVESTIGATE AT TEARDOWN FOR FAULTS TO DETERMINE IF ONE-TIME PROBLEM, OR FURTHER INVESTIGSDR S30R1000022Precooler · rupturedTHE RT ENGINE BLEED AIR TO BYPASS AIR PRE COOLER RUPTURED IN FLIGHT CAUSING THE UPPER AND LOWER PYLON SKINS AS WELL AS THE ACFT SKIN TO BE COME EXPOSED TO HOT EXHAUST GASES WHICH SUBSEQUENTLY RESULTED IN WARPAGE OF THESE SKINS. PILOT REPORTED, HEARD A NOISE ASDR CA091002006Line · leaking(CAN) PILOT NOTED FUEL LEAKING OUT OF LT ENG LWR COWLING DURING WALKAROUND INSP. REMOVED COWLING, CLEANED FUEL RESIDUE FROM LT ENG ASSY, THEN ACFT GROUND RUN FOR LEAK CHECK. DURING LEAK CHECK THE AME OBSERVED A STEADY, HIGH PRESSURE FUEL SPRAY EMANATING FROM SDR 2009F00053Brake Assy · destroyedNORMAL BRAKE PRESSURE APPLIED TO BRAKE AFTER LANDING, ACFT VEERED TO THE RT DUE TO RT BRAKE LOCKING UP. ACFT WOULD NOT MOVE/TAXI UNDER ITS OWN POWER, TUG REQUIRED. ACFT LANDING WEIGHT WAS APPROX 9600 LBS. ACFT WAS AT SLOW TAXI SPEED 3-5 MPH WHEN EVENT OCCURSDR CA090206004Throttle Cable · frozen(CAN) PREMIER 1A ACFT, NR 2 THROTTLE CABLE FROZEN (MOISTURE) IN FLIGHT. THROTTLE CABLES BOTH FORE AND AFT SHEATHING BLOWN THROUGH WITH PRESSURIZED DRY NITROGEN AND FOUND SIGNIFICANT MOISTURE PRESENT. ACFT CABLES TO BE REPLACED PRIOR TO NEXT FLIGHT IAW MM.SDR 2009FA0000033Fcu · malfunctionedPILOT REPORTED FLAPS WOULD NOT RETRACT AFTER LANDING. TROUBLESHOT SYS IAW THE MM 27-50-00-101 AND HBC TECH SUPPORT RECOMMENDATIONS. RECEIVED NUMEROUS FAULT CODES NOT FOUND IN TROUBLESHOOTING MATRIX. REPLACED FLAP CONTROL UNIT WITH REPAIRED FLAP CONTROL UNIT IASDR 2008FA0000662Seal · dislodgedPRESSURE REFUELING CONNECTION CAP FOUND WITH SEALING RING DISLODGED AND HOLDING THE CHECK VALVE OPEN WHEN THE CAP IS INSTALLED. FUEL LEAKING FROM CAP CAUSING FUEL TO FLOW FROM IT UP THE SIDE OF THE AIRCRAFT. THE FUEL FLOWING UP THE OUTSIDE OF THE AIRCRAFT HAS
Back to Williams FJ44-2A