Gates Lear Jet 25B

Service difficulty reports · 100

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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 = '25B'
  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 KC8A20140130001Switch · unknownRUDDER TRIM INOPERATIVE. COULD NOT DUPLICATE. TROUBLESHOT RUDDER TRIM SYSTEM, SUSPECT RUDDER TRIM SWITCH AND REPLACED SELECTOR SWITCH WITH NEW.Jan 30, 2014 · N150CK · Lear 25B · Rudder Tab Control SystemSDR G41A20130402001Tire · separatedAFTER LANDING IN MMPR, WHILE PERFORMING THE WALK AROUND INSPECTION, THE CAPTAIN NOTICED A SECTION OF THE TREAD MISSING ON THE NR 1 MAIN TIRE. NO OTHER DAMAGE WAS REPORTED BUT THE TREAD SEPARATION. THE CAUSE OF THE TREAD SEPARATION COULD NOT BE DETERMINED. MMar 31, 2013 · N26AT · Lear 25B · TireSDR KC8A20121121001Circuit Breaker · malfunctionedAFTER AIRCRAFT DEPARTED KYIP, NOTICED THE RT ESSENTIAL BUSS CIRCUIT BREAKER POPPED. THEN THE LT ESSENTIAL BUSS CIRCUIT BREAKER ALONG WITH THE ESSENTIAL BUSS TIE CIRCUIT BREAKER. EVALUATED THE SITUATION AND DETERMINED THE RIGHT ESSENTIAL BUSS WAS THE PROBLEM.Nov 21, 2012 · N150CK · Lear 25B · DC Power Distribution SystemSDR KC8A20121116001Engine · flamed outDURING CLIMBOUT FROM KOSC EN ROUTE TO KJFK THROUGH FLIGHT LEVEL 390, THE RIGHT ENGINE FLAMED OUT. ATC WAS CONTACTED, A LOWER ALTITUDE AND RETURNED TO KYIP WAS REQUESTED. DURING DESCENT THROUGH THE RE-LIGHT ENVELOPE, THE ENGINE WAS RE-STARTED AND THE AIRCRAFTNov 16, 2012 · N150CK · Lear 25B · Engine (Turbine/Turboprop)SDR G41A201207300005Bonding Jumper · frayedDEPARTING ELP ON AN EMPTY LEG TO IAH, 5 MIN AFTER TAKEOFF, THE CAPTAIN REPORTED THAT AFTER FLYING THROUGH A RAIN CLOUD TRANSMITTING ON THE NR 1 AND NR 2 COMM RADIOS BECAME GARBLED AND UNREADABLE. RECEIVING SEEMED NORMAL. CAPTAIN CHOSE TO RETURN TO ELP. LOCAJul 30, 2012 · N26AT · Lear 25B · Static Discharge SystemSDR KC8AN150CKCircuit Breaker · unserviceableLEFT AND RIGHT ESSENTIAL BUSS CIRCUIT BREAKERS POPPED DURING NORMAL CRUISE. CREW ELECTED TO DIVERT INTO KMOR FOR REPAIRS.Jul 22, 2011 · N150CK · Lear 25B · Electrical Power SystemSDR ZP7A20110311001Engine · flamed outMX PERFORMED AN ADJUSTMENT ON THE FUEL DENSITY AND IDLE RPM ON THE LT ENGINE, WHICH REQUIRES A MAX ALTITUDE ACCELERATION CHECK IAW THE MM CHAP 72-00. FLIGHT CREW LT RDU FOR THE PURPOSE OF PERFORMING THIS CHECK. FLIGHT CREW CLIMBED AND STARTED THE CHECK AT FLMar 8, 2011 · N606SM · Lear 25B · Engine (Turbine/Turboprop)SDR 2011F00033Filter · contaminatedCABIN WAS PRESSURIZING BUT PILOT REPORTED ERRATIC CABIN RATE OF CLIMB AND ELECTED TO RETURN TO BASE. MX CHECKED TAILCONE FOR PRESSURE LEAKS NONE FOUND. MX CHECKED PRESSURE CONTROLLER AND FOUND CONTAMINATION IN THE FILTER WHICH APPEARED TO BE AN INSECT. REPLFeb 10, 2011 · N26AT · Lear 25B · Air Distribution SystemSDR ZP72010F00000Motor · shortedCABIN BLOWER MOTOR SHORTED OUT, CAUSING ELECTRICAL SMOKE TO BE EMITTED INTO THE CABIN. SMOKE STOPPED WHEN THE CIRCUIT BREAKER POPPED.Mar 31, 2010 · N606SM · Lear 25B · Air Distribution FanSDR G41A2007003Engine · flamed outLEARJET N26AT WAS ON THE WAY FROM ELP TO LAX AT FL 410, THE CREW WAS EXPERIENCING SEVERE WEATHER AND REQUESTED TO GO TO FL 450. DURING THE CLIMB THEY HIT TURBULENCE AND THE LT ENGINE FLAMED OUT. THEN REQUESTED TO GO DOWN TO FL 250, RELIT THE LT ENGINE, THEN Oct 9, 2007 · N26AT · Lear 25B · Engine (Turbine/Turboprop)SDR 4262006N236CACompressor Wheel · fodAT 285 KNOTS AT FL270 THE LT ENGINE WENT DOWN TO 20 PERCENT N1. THE AIRCRAFT DIVERTED AND LANDED UNEVENTFUL. MAINTENANCE FOUND FOD ON THE 1ST STAGE OF THE COMPRESSOR.Apr 26, 2006 · N236CA · Lear 25B · Turbine Engine Compressor SectionSDR CED2006F00000Rudder Pedal · stiffTHE FLIGHT CREW ABORTED TAKEOFF ROLL. THE FLIGHT CREW NOTICED ON TAKEOFF ROLL THAT THE RUDDER PEDALS FELT STIFF AND HAD VERY LITTLE MOVEMENT. MAINTENANCE INSPECTED AIRCRAFT RUDDER CONTROL CABLE SYSTEM AND FOUND NO DEFECTS. (K)Nov 1, 2005 · N233CA · Lear 25B · Rudder Control SystemSDR CED2006F00021Engine · shutdownTHE NR 2 ENGINE SHUTDOWN. THE FLIGHT CREW FOLLOWED THE EMERGENCY CHECKLIST AND DIVERTED WITHOUT INCEDENT. MAINTENANCE HAS NOT YET INSPECTED THE AIRCRAFT TO DETERMINE THE SPECIFIC PROBLEM. ADDITIONAL INFORMATION WILL BE SUPPLIED AT YOU REQUEST AFTER MAINTENAOct 4, 2005 · N233CA · Lear 25B · Engine (Turbine/Turboprop)SDR CED2006F00005Altimeter · failedON DEPARTURE, THE CAPTAIN`S ALTIMETER FAILED. REMOVED AND REPLACED ALTIMETER. SYSTEM OPS CHECK GOOD. (K)Sep 1, 2005 · N233CA · Lear 25B · Altimeter, Barometric/EncoderSDR 6252004N8005YCabin Pressure · malfunctionedWHILE ENROUTE, AT FLIGHT LEVEL 410 THE CABIN ALTITUDE EXCEEDED 10000 FT, THE FLIGHT CREW FOLLOWED THE CHECKLIST PROCEDURES AND DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE HAS NOT YET INSPECTED THE AIRCRAFT TO DETERMINE THE SPECIFIC PROBLEM. I WJun 25, 2005 · N8005Y · Lear 25B · Cabin Pressure Control SystemSDR 2006FA0000120Static Line · looseWHILE ENROUTE, CABIN ALTITUDE EXCEEDED 10,000 FT. THE FLIGHT CREW FOLLOWED EMERGENCY PROCEDURES BUT WAS UNABLE TO RETURN THE CABIN PRESSURIZATION WITHIN NORMAL PIRAMETERS. THE FLIGHT CREW DECIDED TO DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. UPON INSPECTJun 17, 2005 · N8005Y · Lear 25B · Cabin Pressure Control SystemSDR CED2006F00007Tire · destroyedON TAKEOFF ROLL THE AIRCRAFT BLEW THE LT MAIN GEAR TIRES IN ELP. (K)Jun 14, 2005 · N236CA · Lear 25B · TireSDR CED2006F00019Fire Detector · false activationWHILE ENROUTE, THE CREW EXPERIENCED INDICATION OF FIRE ON THE NR2 ENGINE. THE CREW THEN FOLLOWED THE EMERGENCY CHECK LIST AND COULD NOT EXTINGUISH THE FIRE LIGHT. THE CREW THEN DECLARED AN EMERGENCY AND LANDED AT THEIR DESTINATION WITHOUT FURTHER INCIDENT. May 28, 2005 · N8005Y · Lear 25B · Fire DetectionSDR CED2006F00006Fuel Tank · leakingON TAKEOFF ROLL AND INITIAL CLIMBOUT, FUEL WAS OBSERVED LEAKING FROM THE LT WING TIP. INFORMED THE CREW OF THE LEAK AND INSTRUCTED THEM TO COME AROUND AND LAND. THE CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE LT FUEL VENT AND FOUND NO DIMay 21, 2005 · N140CA · Lear 25B · Fuel StorageSDR CED2006F00008Case · crackedWHILE ENROUTE, AT FLIGHT LEVEL 390, FLIGHT CREW OBSERVED A FIRE INDICATION ON THE NR 2 ENGINE. THE FLIGHT CREW WAS ABLE TO EXTINGUISH THE FIRE INDICATION LIGHT USING STANDARD EMERGENCY PROCEDURES. THE FLIGHT CREW THEN DECLARED AN EMERGENCY AND RETURNED TO DEMay 17, 2005 · N239CA · Lear 25B · Engine Collector/Tailpipe/NozzleSDR CED2006F00017Plate · malfunctionedON DESCENT, THE NR 1 ENGINE STALLED. THE FLIGHT CREW LT THE ENGINE RUNNING AT IDLE AND LANDED WITHOUT INCIDENT. (K)May 6, 2005 · N140CA · Lear 25B · Compressor Bleed ValveSDR 2005FA0000486Floorbeam · crackedRIGHT DIVAN FLOOR ATTACH ANGLE P/N 2411395-26-526 CRACKED IN RADIOUS OF BEND 14 INCHES LONG. DISCOVERED WHILE PERFORMING CABIN PRESURE LEAK TEST.Feb 24, 2005 · N911A · Lear 25B · Fuselage Main, Floor BeamSDR 110404Bleed Air Sys · leakingTHE AIRCREW EXPERIENCED ELECTRICAL POWER FAILURE. IT WAS FOUND THAT A BLEED AIR LEAK WAS OVERHEATING THE GENERATOR CONTROL PANEL, CAUSING THE GENERATORS TO GO OFF LINE.Oct 23, 2004 · N65WH · Lear 25B · Pneumatic Distribution SystemSDR 1013041Control Module · malfunctionedON A FLIGHT, THE FLIGHT CREW NOTICED THAT THE PRESSURIZATION SYSTEM WAS NOT INCREASING CABIN PRESSURE AT A RATE TYPICAL TO NORMAL AIRCRAFT OPERATION. AT 17,000 FT, WITH A CABIN ALTITUDE LOWER THAN THEY WERE USE TO SEEING, THE FLIGHT CREW DECIDED TO RETURN, LAOct 13, 2004 · N67HB · Lear 25B · Cabin Pressure Control SystemSDR 2004F00421Engine · shutdownAT FL370, THE NR 2 ENGINE SHUTDOWN. THE FLIGHT CREW FOLLOWED THE EMERGENCY CHECKLIST AND DIVERTED TO LIT WITHOUT INCIDENT. MAINTENANCE HAS NOT YET INSPECTED THE AIRCRAFT TO DETERMINE THE SPECIFIC PROBLEM. ADDITIONAL INFORMATION WILL BE SUPPLIED AT YOUR REQUOct 4, 2004 · N233CA · Lear 25B · Engine (Turbine/Turboprop)SDR 091304Wheel · out of positionTHE CREW DID NOT NOTICE THAT THE NOSE WHEEL WAS TURNED 180 DEGREES, THEREFORE WHEN THE CREW RETRACTED THE LANDING GEAR THE NOSE GEAR COULD NOT LOCK IN THE UP POSITION, WHICH WOULD NOT ALLOW THE GEAR DOORS TO CLOSE. THEREFORE THE GEAR UNSAFE LIGHTS.Sep 10, 2004 · N425JL · Lear 25B · Nose/Tail Landing GearSDR 091304AWheel · out of positionTHE CREW DID NOT NOTICE THAT THE NOSE WHEEL WAS TURNED 180 DEGREES, THEREFORE WHEN THE CREW RETRACTED THE LANDING GEAR THE NOSE GEAR COULD NOT LOCK IN THE UP POSITION, WHICH WOULD NOT ALLOW THE GEAR DOORS TO CLOSE. THEREFORE THE GEAR UNSAFE LIGHTS.Sep 10, 2004 · N425JL · Lear 25B · Steering UnitSDR 2004F00338Control Cable · brokenTHROTTLE CABLE BROKEN 12 INCHES FROM END OF CABLE. BROKEN AT AFT END OF FORWARD CABLE WHERE FORWARD CABLE ATTACHES TO AFT CABLE. (SO13200405891)Sep 1, 2004 · N82TS · Lear 25B · Power LeverSDR 2004F00189Line · looseWHILE EN ROUTE FROM MFE-LIT, CABIN ALTITUDE EXCEEDED 10,000 FT. THE FLIGHT CREW FOLLOWED EMERGENCY PROCEDURES BUT WAS UNABLE TO RETURN THE CABIN PRESSURIZATION WITHIN NORMAL PERIMETERS. THE FLIGHT CREW DECIDED TO DIVERT TO ADS AND LANDED WITHOUT FURTHER INCIDJun 17, 2004 · N8005Y · Lear 25B · Engine (Turbine/Turboprop)SDR 2004F00192Tire · failedON TAKEOFF ROLL, THE AIRCRAFT BLEW THE LEFT MAIN GEAR TIRES IN ELP. (M)Jun 14, 2004 · N236CA · Lear 25B · TireSDR CED2004F00004Fire Warning · false activationWHILE ENROUTE, THE CREW EXPERIENCED INDICATION OF FIRE ON THE NR 2 ENGINE. THE CREW THEN FOLLOWED THE EMERGENCY CHECK LIST AND COULD NOT EXTINGUISH THE FIRE LIGHT. THE CREW THEN DECLARED AN EMERGENCY AND LANDED AT THEIR DESTINATION WITHOUT FURTHER INCIDENT. May 28, 2004 · N8005Y · Lear 25B · Fire DetectionSDR CED2004F00003Fuel Sys · leakingON TAKEOFF ROLL AND INITIAL CLIMB OUT, FUEL WAS OBSERVED LEAKING FROM THE LEFT WING TIP. ATC INFORMED THE CREW OF THE LEAK AND INSTRUCTED THEM TO COME AROUND AND LAND. THE CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED THE LT FUEL VENT AND FOUNMay 21, 2004 · N140CA · Lear 25B · Fuel StorageSDR CED2004F00001Case · crackedWHILE ENROUTE, AT FLIGHT LEVEL 390 FLIGHT CREW OBSERVED A FIRE INDICATION ON THE NR 2 ENGINE. THE FLIGHT CREW WAS ABLE TO EXTINGUISH THE FIRE INDICATION LIGHT USING STANDARD EMERGENCY PROCEDURES. THE FLIGHT CREW THEN DECLARED AN EMERGENCY AND RETURNED WITH NMay 17, 2004 · N239CA · Lear 25B · Engine Collector/Tailpipe/NozzleSDR 2004F00424Engine · stalledON DESCENT INTO MEMPHIS, TN, THE NR 1 ENGINE STALLED. THE FLIGHT CREW LEFT THE ENGINE RUNNING AT IDLE AND LANDED WITHOUT INCIDENT. (M)May 6, 2004 · N140CA · Lear 25B · Engine (Turbine/Turboprop)SDR 2004F00212Flow Valve · inoperativeDEPARTED DTW, EN ROUTE TO ADS, AFTER ABOUT 5 MINUTES AT FLIGHT LEVEL 390 THE ALTITUDE ALERTER CAME ON. THE FLIGHT CREW FOLLOWED EMERGENCY PROCEDURES AND LANDED AT SUS WITHOUT INCIDENT. INSPECTED AIRCRAFT AND FOUND FLOW CONTROL VALVE HAD GONE BAD. REPLACED FJan 16, 2004 · N140CA · Lear 25B · Cabin Pressure Control SystemSDR DRU2004F00000Fire Detector · false indicationFALSE FIRE WARNING DURING FLIGHT. AFTER THE AIRCRAFT LANDED, THE PILOT REPORTED THAT THE INDICATION WAS INTERMITTENT. THE RT ENGINE COWLING WAS REMOVED, AND THE ENGINE WAS INSPECTED. THERE WAS NO INDICATION OF FIRE IN THE ENGINE AREA. THE FIRE LOOP LOOKEDJan 13, 2004 · N7810W · Lear 25B · Fire DetectionSDR 2004F00045Fire Loop · dirtyFALSE FIRE WARNING DURING FLIGHT. AFTER A/C LANDED, PILOT REPORTED INDICATION WAS INTERMITTENT. COWL WAS REMOVED, ENGINE INSPECTED, NO INDICATION OF FIRE/OVERHEAT. DETECTION LOOP INTACT/NO DAMAGE. WIRING CONNECTIONS AT FIREWALL DISCONNECTED, APPEARED TO BE Jan 13, 2004 · N7810W · Lear 25B · Fire DetectionSDR 2004F00223Nozzle · damagedBRO - ON CLIMB-OUT, THE NR 1 ENGINE FLAMED OUT AT 39,600 FEET. THE AIRCRAFT DESCENDED TO FLIGHT LEVEL 25,000 FEET AND RESTARTED THE ENGINE. THE AIRCRAFT THEN DIVERTED TO ADS, AND LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS INSPECTED AND THE EXHAUST NOZZLE Jan 8, 2004 · N233CA · Lear 25B · Engine Collector/Tailpipe/NozzleSDR CED2004F00000Tire · separatedON CLIMB OUT, THE NOSE GEAR UNSAFE LIGHT ILLUMINATED. THE CREW CYCLED THE GEAR NUMEROUS TIMES WITH NO CHANGE IN THE UNSAFE INDICATION, THEY THEN RETURNED WITHOUT INCIDENT AND NOTICED THE NOSE WHEEL TIRE WAS MISSING TREAD. UPON INSPECTION OF THE AIRCRAFT, FOUJan 8, 2004 · N233CA · Lear 25B · TireSDR 2004FA0000020Pump · leakingINSTALLED OVERHAULED FUEL PUMP FROM MFG ON 4NOV03. DURING AIRCRAFT INSPECTION 22DEC04 HAD FUEL SEEP FROM WIRES ON PUMP.Jan 6, 2004 · Lear 25B · Engine Fuel PumpSDR CED2003F00000Filter · inoperativeON NOV 20, 2003, THE AIRCRAFT EXPERIENCED LOW FUEL PRESSURE WARNING LIGHTS. UPON INVESTIGATION OF THE DISCREPANCY WE CHANGED THE FUEL FILTERS BECAUSE THE FELT SEAL HAD CONE UNGLUED AND CLOGGED THE FILTER. THE AIRCRAFT WAS IN FOR A INSPECTION OF THE 15 NOV 20Nov 15, 2003 · N233CA · Lear 25B · Aircraft Fuel Filter/StrainerSDR 2004F00326Engine · flamed outON A TEST FLIGHT AFTER ENGINE INSTALL. ENGINE BEING TESTED FLAMED OUT AT 42,500 FT. AT A LOWER ALTITUDE OF 23,000 FT ENGINE RESTARTED AND RAN WITH NO FURTHER TROUBLE AND NO INDICATIONS OF ENGINE PROBLEMS. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED FIRST STASep 24, 2003 · N67HB · Lear 25B · Engine (Turbine/Turboprop)SDR 2003F00580Panel · departedAIRCRAFT LOST NOSE PANEL ON TAKEOFF DURNG A PART 91 FLIGHT AIRCRAFT RETURNED TO BASE. UPON RECOVERY INSPECTION, FOUND THAT NOSE PANEL WAS LEFT UNFASTENED BY MAINTENANCE PERSONEL. (M)Aug 24, 2003 · N8005Y · Lear 25B · Fuselage Structure (General)SDR CYO2003F00000Indicator · shortedAIRCRAFT WAS ENROUTE FROM BRO TO LIT. FLIGHT CREW EXPERIENCED SLIGHT SMOKE AND A BURNING ODOR, THEY THEN DIVERTED TO SHV. MAINTENANCE CREW INSPECTED AND FOUND DME INDICATOR SHORTED INTERNALLY.Jul 16, 2003 · N140CA · Lear 25B · DME/TACAN SystemSDR 070103Bleed Valve · out of adjustWHILE CLIMBING THROUGH FL40.5, NR 1 ENGINE FLAMEOUT. AIRCRAFT DESENDED TO FL290, THE ENGINE WAS RELIGHT AND AIRCRAFT CONTINUED TO SRQ AT FL240. MAINTENANCE DETERMINED THAT THE BLEED VALVES WERE OUT OF ADJUSTMENT.Jul 1, 2003 · N425JL · Lear 25B · Compressor Bleed ValveSDR 2003FA0000480Fire Loop · looseFIRE DETECTION LIGHT CAME ON IN FLIGHT. REDUCED ENGINE POWER TO IDLE, AFTER 1 MINUTE SHUT DOWN ENGINE AND EXTIGUISHED BOTH BOTTLES. ONCE ON THE GROUND ENGINE WAS INSPECTED, NO EVIDENCE OF FIRE, FOUND LOOSE CONNECTION ON FIRE LOOP.May 12, 2003 · N23RZ · Lear 25B · Smoke DetectionSDR DRU2003F00000Blanket · burnedDURING INSP BY MECH, A BLACK STREAK (FORE TO AFT) WAS NOTICED ON LT HORIZ STAB, THAT BOOT LOOKED BURNT ON L.E. EXAMINATION REVEALED THAT BOOT MUST HAVE SHORTED AGAINST L.E., BURNING BOTH BOOT AND HORIZ STAB CONSISTED OF NICKEL SIZE HOLE BEING COMPLETELY BURNTFeb 10, 2003 · N7810W · Lear 25B · Airfoil Anti/De-ice SystemSDR CA030110006Starter Gen · failed(CAN) DEPARTED AIRPORT AND LEVELED OFF AT FL410. VERY LIGHT TURBULENCE WAS ENCOUNTERED. APPROXIMATELY TWO MINUTES INTO CRUISE, THE RT ENGINE PRODUCED A LIGHT BANG & BEGAN TO SPOOL DOWN. THE RPM'S SETTLED A T 25-30 PERCENT. THE R/H THROTTLE WAS REDUCED TO IDLDec 12, 2002 · Lear 25B · Starter-GeneratorSDR 110702Engine · flamed outENGINE FLAMED OUT AT FL 390, 20 MIN. INTO THE FLIGHT. PILOT DECLARED AN EMERGANCY. THE PILOT RELITE THE ENGINE. THE AIRCRAFT RETURNED TO THE GROUND AT FXE. THE PROBLEM COULD NOT BE DUPLITCATE ON THE GROUND. A/C WAS RETURNED TO SERVICE. AFTER A TEST FLIGHT WAS Nov 6, 2002 · N254SC · Lear 25B · Engine (Turbine/Turboprop)SDR 102302Regulator Valve · malfunctionedAT FLIGHT LEVEL 430 HYRDRALIC PRESSURE INDICATED 0, AIRCRAFT WAS DIVERTED TO LIT. DURING DESENT THE LT ENGINE OIL LIGHT CAME ILLUMINATED. THIS ENGINE WAS SHUT DOWN. AIRCRAFT WAS PREPARE FOR EMERGANCY LANDING PROCEDURES. CAUSE OF THE HYD FAILURE WAS PRESSURE REOct 22, 2002 · N425JL · Lear 25B · Hydraulic Pressure Relief Valve, Main
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