Raytheon BAE 125-800A
Service difficulty reports · 282
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 = 'BAE125800A' 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 = 'BAE125800A' 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 2023FA0000353Outflow Valve · jammedAIRCRAFT LOST PRESSURIZATION AT FL039, PERFORMED AN EMERGENCY DECENT AND LANDED BACK TO PBI WITHOUT INCIDENT.SDR 2023FA0000352Air Duct · detachedAIRCRAFT LOST PRESSURIZATION AT FL015 AND RETURNED TO PBI. AFTER LANDING IT WAS DISCOVERED THAT AN AIR-CONDITIONING DUCT HAD SEPARATED FROM THE REAR PRESSURE BULKHEAD FITTING.SDR 2022FA0000279None · noneDURING CLIMB PASSING FL 355 THE "CABIN ALTITUDE" LIGHT CAME ON WITH DIFFERENTIAL PRESSURE INDICATOR SHOWING ZERO. CABIN DID NOT LOSE PRESSURIZATION; HOWEVER THE CREW FOLLOWED THE CHECKLIST DECLARED EMERGENCY, DESCENDED TO LOWER ALTITUDE AND RETURNED TO THE DEPSDR A8JA202103120035Circuit Breaker · faultedDURING APPROACH FROM KFXE TO KHOU AT APPROXIMATELY 1930 HRS LOCAL, FLIGHT CREW OBSERVED NO LANDING GEAR DOWN AND LOCKED INDICATION. CREW ELECTED TO ABORT LANDING AND CONTINUE FLIGHT TO COMPLETE ABNORMAL CHECKLIST, AND COMMUNICATED THIS TO KHOU TOWER. CREW COSDR JGVR20181102001Terminal · burnedINVESTIGATED SMOKE IN THE COCKPIT BEHIND THE CO-PILOT INSTRUMENT PANEL. FOUND THE -A- SCREEN ELECTROSTATIC FILTER WIRE TERMINALS BURNED ON SUPPLY SIDE. REMOVED AND REPLACED THE FILTER ASSEMBLY, REPLACED THE WIRING WITH NEW RING TERMINALS. RANG OUT WIRING TSDR 4TDA2018091300001Accumulator · low pressureAS AIRCRAFT WAS RELEASED FOR FLIGHT, THE PILOT RELEASED THE PARKING BRAKE, ACTIVATED THE REGULAR BRAKE SYSTEM AND NOTICED THE PRESSURES ROSE TO 1,000 PSI AND FELL OFF TO NEAR ZERO. AFTER SEVERAL ATTEMPTS TO CHECK THE SYSTEM THE PILOT CONTACTED MAINTENANCE CONTSDR E0YA2018062900087Starter Gen · failedDURING CRUISE THE NR 2 ENGINE STARTER/GENERATOR FAILED AND CAUSED VIBRATION.SDR 4TDA201805293805Controller · malfunctionedAT FL 400, THE CAPTAIN NOTICED AN INCREASE IN CABIN CLIMB RATE AND DECREASE IN CABIN PRESSURE. CREW DONNED OXYGEN MASKS AND MADE A DESCENT TO FL100. FLIGHT CONTINUED UNEVENTFUL, PRESSURIZATION WAS CONTROLLABLE AT THIS POINT.SDR 2018FA0000149Wire · pinchedWANDER LIGHT BEHIND CAPTAIN`S CHAIR, WIRING FOUND PINCHED AND ARCED. CREW REPORTED A SMALL FLAME FOR A MOMENT UNTIL THE CIRCUIT BREAKER. NOTHING FURTHER WAS REPORTED.SDR 6EMY20171105856Not Reported · fireAN EMPLOYEE OBSERVED BLACK SMOKE EMERGING FROM THE UPPER FUSELAGE REAR EQUIPMENT BAY ACCESS PANELS OF THE SUBJECT AIRCRAFT. POWER WAS IMMEDIATELY TURNED OFF AND ALL PERSONNEL REMOVED FROM THE AIRCRAFT. ON INSPECTION OF THE REAR EQUIPMENT BAY SMALL NAKED FLAMESSDR PAIR20160916S3570Air Duct · brokenCLIMBING THROUGH 23,000 FT, AIRCRAFT EXPERIENCED REAR BAY OVERHEAT WARNING FOLLOWED BY CABIN ALTITUDE STARTING TO CLIMB. ACFT RETURNED TO POINT OF DEPARTURE. MAINTENANCE INSPECTOR FOUND ACM INLET DUCT BROKEN, ACM OUTLET CLAMP BROKEN, AND ACM TURBINE BLADES ASDR ZP7A2016F00039Fuel Control · defectiveAT FL400, ENGINE NR 2 BEGAN LOOSING POWER, N1 REDUCED TO BELOW 60 PERCENT, DESCENDED TO 14,000 FT N1 REDUCED TO BELOW 40 PERCENT. AT BELOW 8000 FT MSL ENGINE POWER BECAME FULLY RESPONSIVE.SDR 9PVA2015F00111Seal · shiftedCABIN ALTITUDE TOD CABIN ALTITUDE INCREASED VIELENTY AT 200 FT + IAE MINUTE ALL THE WAY TO 20,000 FT. PAX O2 MASK PARTIALLY DEPLOYED. DOOR SEAL SHIFTED.SDR 2015F00105Bolt · corrodedREMOVED AND INSPECTED MASS BALANCE WEIGHTS, AND SPIGOTS. THE BOLT HAD EXCESSIVE CORROSION AND HAD TO BE REPLACED. WEIGHTS WERE CLEANED AND REUSED. BROKEN BOLT COULD LEAD TO JAMMING AND LOSS OF ELEVATOR CONTROL.SDR 9PVA2015F00110Irs · misalignedHAD TO RETURN TO THE AIRPORT BECAUSE THERE WAS 30 TO 90 DEGREES HEADING DIFFERENCE DUE TO A MISS ALIGNMENT OF THE IRS SYSTEM.SDR JLTA20150824001Engine · malfunctionedON FRIDAY, AUGUST 21ST AT APPROX 1900Z, ACFT DEPARTED EMPTY & ENTERED CRUISE, EVERYTHING WAS NORMAL. ON THE INITIAL DESCENT CREW HEARD A STRANGE NOISE & OBSERVED AN ENG COMPUTER LIGHT FOR THE NR 2 ENG. ALL OF THE INSTRUMENTS FOR THE NR 2 ENG THEN FLUCTUATED SDR DIXA2015F00097Overheat Sensor · intermittentCREW REPORTED CLIMBING THROUGH FL 150, RED REAR BAY OVERHEAT LIGHT ILLUMINATED, CREW FOLLOWED CHECKLIST PROCEDURES. LIGHT EXTINGUISHED WHILE STILL CLIMBING THROUGH FL 180 RED REAR BAY OVER HEAT LIGHT ILLUMINATED FOLLOWED BY A BURNING ODOR AND LIGHT SMOKE IN CSDR T6FA2015072903Intercostal · crackedFOUND CRACKED DENT IN FUSELAGE RT SIDE INTERCOSTAL UNDER LAVATORY FLOOR BETWEEN FRAME 16 TO FRAME 17. REPAIRED IAW FIELD REPAIR.SDR T6FA2015072902Skin · corrodedCORROSION FOUND ON FUSELAGE KEEL SKIN & DOUBLER BETWEEN FRAMES 12 & 12A. REPAIRED IAW FIELD REPAIR INSTRUCTIONS.SDR T6FA2015072901Skin · corrodedCORROSION FOUND ON LT SIDE MLG LEG FAIRING OUTER SKIN. REPAIRED IAW FIELD REPAIR.SDR CA150525014B-Nut · cracked(CAN) DURING THE REPLACEMENT OF THE OXYGEN SYS CHARGING VLV WHICH WAS SUSPECTED OF A LEAK, IT WAS NOTICED THAT THE B NUT WHICH CONNECTS TO THE FILTER & IS PART OF THE MANIFOLD WAS CRACKED.SDR CA150113022Tube · leaking(CAN) POST ARRIVAL, FLIGHT CREW CONDUCTED POST FLIGHT INSPECTION OF ACFT AND NOTED SIGNIFICANT OIL LEAKAGE ON LT ENGINE COWLINGS, NO INFLIGHT INDICATIONS WERE EVIDENT TO FLIGHT CREW DURING APPROXIMATE 4.5 HR FLIGHT. OIL LEVEL COULD NOT BE SEEN THROUGH OIL TANKSDR 9JLA2014122607198Position Switch · shortedDURING TAXI THE SSU STALL IDENT LIGHT ILLUMINATED & THE NR 1 STALL CHANNEL DOES NOT TEST. EXTENSIVE TROUBLESHOOTING FOUND THE LT INBD FLAP POSITION MICRO SWITCH GNDED OUT INTERNALLY. THE DEFECTIVE SWITCH WAS REMOVED & A NEW SWITCH INSTALLED PN 9002EN3.SDR 9JLA2014122607197Ahrs · intermittentNUMBER 2 AHRS UNIT INTERMITTENTLY ROLLS COPILOTS ATTITUDE INDICATOR CREATING A COMPARATOR MONITOR DISAGREE. THE DEFECTIVE UNIT WAS REMOVED PN7003360-943 SN 95083260 & AN OVERHAULED UNIT WAS INSTALLED.SDR 2014FA0000506Indication Sys · failedFAILURE OF RT MLG INDICATION WHEN GEAR SELECTED DOWN FOR LANDING.SDR FVJA2014082600148Cooling Turbine · failedDURING THE CLIMB, CREW REPORTED LOUD SQUEAL FOLLOWED BY ODOR OF BURNED OIL AND REPORT OF SMOKE COMING FROM AIR VENTS. THE ACM, COOLING TURBINE FOUND TO HAVE FERROUS MATERIAL ON THE MAGNETIC DRAIN PLUG, COOLING TURBINE WAS DISCOVERED TO BE FAILED, INTERNAL BEASDR 9JLA201405217509Switch · stuckTHE CREW REPORTED THAT AFTER TAKEOFF & GEAR RETRACTION AN UNSAFE GEAR INDICATION, 3 RED LIGHTS & 1 MAIN GEAR GREEN LIGHT. THE CREW CYCLED THE GEAR BACK DOWN & RETURNED BACK TO THE AIRPORT FOR MAINTENANCE. TROUBLESHOOTING FOUND THE RT NORMAL LG MICRO SWITCH CSDR CA140407014Wire Harness · chafed(CAN) FLIGHT CREW REPORTED LANDING GEAR SELECTOR WOULD NOT MOVE AFTER TAKEOFF. CHECKLIST CARRIED OUT AND FLIGHT CREW DECIDED TO RETURN TO AIRPORT AFTER CIRCLING SUFFICIENT TIME TO LOWER FUEL WEIGHT TO OBTAIN PROPER LANDING WEIGHT. ACFT LANDED WITHOUT INCIDENTSDR CA140303002Switch · failed(CAN) FLIGHT CREW REPORTED AIRBRAKE SPOILER CIRCUIT BREAKER WAS FOUND TRIPPED AFTER SHUTDOWN. THE CIRCUIT BREAKER WAS RESET AND DID NOT OPEN AGAIN. DURING MAINTENANCE DAILY INSPECTION, THE CIRCUIT BREAKER WAS AGAIN FOUND TRIPPED. IT WAS RESET AND WITHIN A FSDR BN5A20142190001Seal · weakCREW REPORTED REAR BAY OVERHEAT AT FL 250. TROUBLESHOOTING FOUND BLEED AIR LEAK AT LT BLEED AIR VLV & LT NON-RETURN VLV. REMOVED LT BLEED AIR SOV & LT NON-RETURN VLV. REPLACE DEFECTIVE SEALS WITH NEW PN 20496-200A, 6-464-1PAR & HTE580-3060-112A & REINSTALLESDR BJYA 20130717001Warning Light · illuminatedCABIN HIGH ALTITUDE LIGHT ILLUMINATE AFTER REACHING FL 370. ON LEVEL OFF DURING ACCELERATION, CABIN HIGH ALTITUDE LIGHT ILLUMINATED. DONNED OXYGEN MASKS, DEPLOYED PAX MASKS AND COMPLETED CHECKLIST ITEMS. REFERRED TO CHECKLIST, ELECTED TO DECEND. PERFORMESDR 2013FA0000351Relay · blownRIGHT WINDSHIELD HEAT WAS FOUND INOPERATIVE ALONG WITH TAXI LIGHTS. INVESTIGATION FOUND THAT RELAY FOR RT WINDHSHIELD DEICE HAD BLOWN THE GUTS OUT OF THE RELAY AND ACROSS TO THE CIRCUIT BREAKERS AND IT BUSTED THE POWER TAB OFF OF THE TAXI LIGHT CIRCUIT BREAKESDR WTXR2013060329204Line · chafedTHE VENTURI VACUUM LINE, FROM THE PRESSURIZATION CONTROLLER TO THE CABIN AIR OPERATED VENTURI IS BEING RUBBED THROUGH BY THE AILERON CONTROL CABLE THAT SITS DIRECTLY ABOVE IT. THE LINE SHOULD HAVE A BEND THAT GIVES IT GREATER CLEARANCE FROM THE FLIGHT CONTROSDR VIBR20131202001Stud · unsecureENGINE STARTER GENERATOR "B" STUD NOT SECURE IN STARTER GENERATOR TERMINAL BLOCK.SDR JLTA20130520001Bolt · corrodedDURING A POSTFLIGHT INSPECTION, DISCOVERED THE RT AIRBRAKE OTBD COVERS WERE NOT ALIGNED. FOUND BOLTS IN BRACKET WERE LOOSE. SAFETY WIRE WAS STILL INTACT. SAFETY WIRE REMOVED AND AN ATTEMPT WAS MADE TO TORQUE THE BOLTS, NO JOY. BOLTS REMOVED AND FOUND SEVERSDR V0JA20130506001Filter · malfunctionedPILOTS SIDE WINDSHIELD HEAT ELECTROSTATIC FILTER PRODUCED SMOKE DURING OPERATION AND OPENED CIRCUIT BREAKER.SDR KKYA20121031001Filter · unknownAFTER DEPARTURE NR 1 ENGINE FUEL LIGHT CAME ON. REDUCED NR 1 THROTTLE TO IDLE - LIGHT REMAINED ON. REPLACED THE ENGINE FUEL FILTER WITH NEW PER HONEYWELL TFE731-5R LMM CH 73-21-02. PERFORMED SATISFACTORY GOUND OPERATIONAL CHECKS WITH NO DEFECTS NOTED.SDR KKYA20120924001Pitot System · obstructedCOMPUTER MONITOR NR 1 AND NR 2 AIRSPEEDS PLUS ALTITUDE DISCREPANCIES. FOUND DEBRIS IN BOTH PITOT SYSTEMS AND ADC NR 1 SYSTEM WAS PLUGGED.SDR 9JLA2012073106330Computer · defectiveCREW REPORTED THE LT ENGINE DEEC LIGHT COMES ON STEADY IN FLIGHT. THE ENGINE COMPUTER WAS REMOVED. A NEW COMPUTER WAS INSTALLED. FUNCTIONAL CHECKS WERE SATISFACTORY.SDR 2012FA0000490Autopilot Sys · malfunctionedAT 24000 FT, INBOUND TO DESTINATION, AUTOPILOT WARNING HORN SOUNDED CONTINUOUSLY AND ALL AUTOPILOT WARNING LIGHTS WERE ON AND AUTOPILOT ENGAGE LIGHTS WERE ON WITH AUTOPILOT OFF. DETECTED A BURNED WIRE ODOR THAT PROGRESSIVELY INCREASED, DECIDED TO LAND. PULLESDR 2012F00067Transducer · inoperativeON THE LAST LEG OF THE TRIP, ON START UP, THE RT ENGINE COMPUTER INOPERATIVE LIGHT ILLUMINATED. FOUND BAD N2 TRANSDUCER. REPLACED THE TRANSDUCER, OPS CHECKED GOOD.SDR L7OA201203270127Valve · malfunctionedON CLIMBOUT FROM SJU, IT WAS NOTICED THAT FUEL WAS COMING FROM THE LEFT WING VENT AREA. THE AIRCRAFT RETURNED TO SJU WITHOUT INCIDENT.SDR L7OA2012F00066Fuel Sys · leakingON CLIMB OUT, NOTICED FUEL COMING FROM THE LT WING VENT AREA. ACFT RETURNED TO DEPARTURE WITHOUT INCIDENT.SDR E81R2011122632222Pump · low pressureINVESTIGATED REPORTED "HYD 2 LO PRESS" ANNUNCIATOR LIGHT INDICATION. REPLACED FAILED NR 2 ENGINE HYD PUMP WITH AN O/H PUMP AND DRAINED HYD SYS RESERVOIR, REPLACED SYS SUCTION FILTER. HYDR SYS OPS NORMAL AFTER PUMP REPLACEMENT. HYD PUMP TSN/TSOH UNKNOWN, TRANSSDR BLUA2012F00025Monopole · failedNR 2 ENGINE COMPUTER LIGHT ILLUMINATED IN FLIGHT. FOUND MONOPOLE FAILED.SDR UVCA20110418001Starter Gen · malfunctionedRT STARTER GENEREATOR WOULD NOT START.SDR CA110209027B-Nut · cracked(CAN) DURING INSPECTION A CRACK IN THE B-NUT ATTACHED TO THE SEQUENCE VALVE IN THE LT LANDING GEAR WELL AS NOTED. THE CRACK WAS RUNNING PERPENDICULAR TO THE THREADS OF THE NUT. THERE WERE NO PREVIOUS REPORTS OF HYDRAULIC FLUID LEAKAGE.SDR CA110209031Frame · cracked(CAN) DURING 24 YEAR INSP, A CRACK IN THE TOP CTR MEMBER OF THE LOWER PRESSING WAS FOUND.SDR CA110209028Nut · crackedDURING REMOVAL OF THE VENTRAL FUEL TANK, THE ABOVE MENTIONED NUT WAS FOUND TO BE SEIZED IN PLACE. 2 CRACKS WERE NOTED ON THE OUTER SURFACE OF THE NUT: 1 PERPENDICULAR TO THE DIRECTION OF THE THREADS. AFTER DISASSEMBLY, SEVERE CORROSION OF THE THREADED PORTIONSDR CA110209026B-Nut · crackedDURING INSP, A CRACK IN THE B-NUT ATTACHED TO THE SEQUENCE VALVE IN THE LT LANDING GEAR WELL AS NOTED. THE CRACK WAS RUNNINQ PERPENDICULAR TO THE THREADS OF THE NUT. THERE WERE NO PREVIOUS REPORTS OF HYD FLUID LEAKAGE.
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