# Service difficulty reports: Gates Lear Jet 25B

A list on [Gates Lear Jet 25B](https://openairdocs.org/model/gates-lear-jet-25b.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 100 reports

- [SDR KC8A20140130001](https://openairdocs.org/sdr/KC8A20140130001.md): Switch · unknown · Jan 30, 2014 · N150CK · Lear 25B · Rudder Tab Control System
  > RUDDER TRIM INOPERATIVE. COULD NOT DUPLICATE. TROUBLESHOT RUDDER TRIM SYSTEM, SUSPECT RUDDER TRIM SWITCH AND REPLACED SELECTOR SWITCH WITH NEW.
- [SDR G41A20130402001](https://openairdocs.org/sdr/G41A20130402001.md): Tire · separated · Mar 31, 2013 · N26AT · Lear 25B · Tire
  > AFTER 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. M
- [SDR KC8A20121121001](https://openairdocs.org/sdr/KC8A20121121001.md): Circuit Breaker · malfunctioned · Nov 21, 2012 · N150CK · Lear 25B · DC Power Distribution System
  > AFTER 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.
- [SDR KC8A20121116001](https://openairdocs.org/sdr/KC8A20121116001.md): Engine · flamed out · Nov 16, 2012 · N150CK · Lear 25B · Engine (Turbine/Turboprop)
  > DURING 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 AIRCRAFT
- [SDR G41A201207300005](https://openairdocs.org/sdr/G41A201207300005.md): Bonding Jumper · frayed · Jul 30, 2012 · N26AT · Lear 25B · Static Discharge System
  > DEPARTING 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. LOCA
- [SDR KC8AN150CK](https://openairdocs.org/sdr/KC8AN150CK.md): Circuit Breaker · unserviceable · Jul 22, 2011 · N150CK · Lear 25B · Electrical Power System
  > LEFT AND RIGHT ESSENTIAL BUSS CIRCUIT BREAKERS POPPED DURING NORMAL CRUISE. CREW ELECTED TO DIVERT INTO KMOR FOR REPAIRS.
- [SDR ZP7A20110311001](https://openairdocs.org/sdr/ZP7A20110311001.md): Engine · flamed out · Mar 8, 2011 · N606SM · Lear 25B · Engine (Turbine/Turboprop)
  > MX 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 FL
- [SDR 2011F00033](https://openairdocs.org/sdr/2011F00033.md): Filter · contaminated · Feb 10, 2011 · N26AT · Lear 25B · Air Distribution System
  > CABIN 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. REPL
- [SDR ZP72010F00000](https://openairdocs.org/sdr/ZP72010F00000.md): Motor · shorted · Mar 31, 2010 · N606SM · Lear 25B · Air Distribution Fan
  > CABIN BLOWER MOTOR SHORTED OUT, CAUSING ELECTRICAL SMOKE TO BE EMITTED INTO THE CABIN. SMOKE STOPPED WHEN THE CIRCUIT BREAKER POPPED.
- [SDR G41A2007003](https://openairdocs.org/sdr/G41A2007003.md): Engine · flamed out · Oct 9, 2007 · N26AT · Lear 25B · Engine (Turbine/Turboprop)
  > LEARJET 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
- [SDR 4262006N236CA](https://openairdocs.org/sdr/4262006N236CA.md): Compressor Wheel · fod · Apr 26, 2006 · N236CA · Lear 25B · Turbine Engine Compressor Section
  > AT 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.
- [SDR CED2006F00000](https://openairdocs.org/sdr/CED2006F00000.md): Rudder Pedal · stiff · Nov 1, 2005 · N233CA · Lear 25B · Rudder Control System
  > THE 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)
- [SDR CED2006F00021](https://openairdocs.org/sdr/CED2006F00021.md): Engine · shutdown · Oct 4, 2005 · N233CA · Lear 25B · Engine (Turbine/Turboprop)
  > THE 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 MAINTENA
- [SDR CED2006F00005](https://openairdocs.org/sdr/CED2006F00005.md): Altimeter · failed · Sep 1, 2005 · N233CA · Lear 25B · Altimeter, Barometric/Encoder
  > ON DEPARTURE, THE CAPTAIN`S ALTIMETER FAILED. REMOVED AND REPLACED ALTIMETER. SYSTEM OPS CHECK GOOD. (K)
- [SDR 6252004N8005Y](https://openairdocs.org/sdr/6252004N8005Y.md): Cabin Pressure · malfunctioned · Jun 25, 2005 · N8005Y · Lear 25B · Cabin Pressure Control System
  > WHILE 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 W
- [SDR 2006FA0000120](https://openairdocs.org/sdr/2006FA0000120.md): Static Line · loose · Jun 17, 2005 · N8005Y · Lear 25B · Cabin Pressure Control System
  > WHILE 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 INSPECT
- [SDR CED2006F00007](https://openairdocs.org/sdr/CED2006F00007.md): Tire · destroyed · Jun 14, 2005 · N236CA · Lear 25B · Tire
  > ON TAKEOFF ROLL THE AIRCRAFT BLEW THE LT MAIN GEAR TIRES IN ELP. (K)
- [SDR CED2006F00019](https://openairdocs.org/sdr/CED2006F00019.md): Fire Detector · false activation · May 28, 2005 · N8005Y · Lear 25B · Fire Detection
  > WHILE 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.
- [SDR CED2006F00006](https://openairdocs.org/sdr/CED2006F00006.md): Fuel Tank · leaking · May 21, 2005 · N140CA · Lear 25B · Fuel Storage
  > ON 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 DI
- [SDR CED2006F00008](https://openairdocs.org/sdr/CED2006F00008.md): Case · cracked · May 17, 2005 · N239CA · Lear 25B · Engine Collector/Tailpipe/Nozzle
  > WHILE 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 DE
- [SDR CED2006F00017](https://openairdocs.org/sdr/CED2006F00017.md): Plate · malfunctioned · May 6, 2005 · N140CA · Lear 25B · Compressor Bleed Valve
  > ON DESCENT, THE NR 1 ENGINE STALLED. THE FLIGHT CREW LT THE ENGINE RUNNING AT IDLE AND LANDED WITHOUT INCIDENT. (K)
- [SDR 2005FA0000486](https://openairdocs.org/sdr/2005FA0000486.md): Floorbeam · cracked · Feb 24, 2005 · N911A · Lear 25B · Fuselage Main, Floor Beam
  > RIGHT DIVAN FLOOR ATTACH ANGLE P/N 2411395-26-526 CRACKED IN RADIOUS OF BEND 14 INCHES LONG. DISCOVERED WHILE PERFORMING CABIN PRESURE LEAK TEST.
- [SDR 110404](https://openairdocs.org/sdr/110404.md): Bleed Air Sys · leaking · Oct 23, 2004 · N65WH · Lear 25B · Pneumatic Distribution System
  > THE 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.
- [SDR 1013041](https://openairdocs.org/sdr/1013041.md): Control Module · malfunctioned · Oct 13, 2004 · N67HB · Lear 25B · Cabin Pressure Control System
  > ON 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, LA
- [SDR 2004F00421](https://openairdocs.org/sdr/2004F00421.md): Engine · shutdown · Oct 4, 2004 · N233CA · Lear 25B · Engine (Turbine/Turboprop)
  > AT 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 REQU
- [SDR 091304](https://openairdocs.org/sdr/091304.md): Wheel · out of position · Sep 10, 2004 · N425JL · Lear 25B · Nose/Tail Landing Gear
  > THE 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.
- [SDR 091304A](https://openairdocs.org/sdr/091304A.md): Wheel · out of position · Sep 10, 2004 · N425JL · Lear 25B · Steering Unit
  > THE 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.
- [SDR 2004F00338](https://openairdocs.org/sdr/2004F00338.md): Control Cable · broken · Sep 1, 2004 · N82TS · Lear 25B · Power Lever
  > THROTTLE CABLE BROKEN 12 INCHES FROM END OF CABLE. BROKEN AT AFT END OF FORWARD CABLE WHERE FORWARD CABLE ATTACHES TO AFT CABLE. (SO13200405891)
- [SDR 2004F00189](https://openairdocs.org/sdr/2004F00189.md): Line · loose · Jun 17, 2004 · N8005Y · Lear 25B · Engine (Turbine/Turboprop)
  > WHILE 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 INCID
- [SDR 2004F00192](https://openairdocs.org/sdr/2004F00192.md): Tire · failed · Jun 14, 2004 · N236CA · Lear 25B · Tire
  > ON TAKEOFF ROLL, THE AIRCRAFT BLEW THE LEFT MAIN GEAR TIRES IN ELP. (M)
- [SDR CED2004F00004](https://openairdocs.org/sdr/CED2004F00004.md): Fire Warning · false activation · May 28, 2004 · N8005Y · Lear 25B · Fire Detection
  > WHILE 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.
- [SDR CED2004F00003](https://openairdocs.org/sdr/CED2004F00003.md): Fuel Sys · leaking · May 21, 2004 · N140CA · Lear 25B · Fuel Storage
  > ON 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 FOUN
- [SDR CED2004F00001](https://openairdocs.org/sdr/CED2004F00001.md): Case · cracked · May 17, 2004 · N239CA · Lear 25B · Engine Collector/Tailpipe/Nozzle
  > WHILE 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 N
- [SDR 2004F00424](https://openairdocs.org/sdr/2004F00424.md): Engine · stalled · May 6, 2004 · N140CA · Lear 25B · Engine (Turbine/Turboprop)
  > ON DESCENT INTO MEMPHIS, TN, THE NR 1 ENGINE STALLED. THE FLIGHT CREW LEFT THE ENGINE RUNNING AT IDLE AND LANDED WITHOUT INCIDENT. (M)
- [SDR 2004F00212](https://openairdocs.org/sdr/2004F00212.md): Flow Valve · inoperative · Jan 16, 2004 · N140CA · Lear 25B · Cabin Pressure Control System
  > DEPARTED 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 F
- [SDR DRU2004F00000](https://openairdocs.org/sdr/DRU2004F00000.md): Fire Detector · false indication · Jan 13, 2004 · N7810W · Lear 25B · Fire Detection
  > FALSE 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 LOOKED
- [SDR 2004F00045](https://openairdocs.org/sdr/2004F00045.md): Fire Loop · dirty · Jan 13, 2004 · N7810W · Lear 25B · Fire Detection
  > FALSE 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
- [SDR 2004F00223](https://openairdocs.org/sdr/2004F00223.md): Nozzle · damaged · Jan 8, 2004 · N233CA · Lear 25B · Engine Collector/Tailpipe/Nozzle
  > BRO - 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
- [SDR CED2004F00000](https://openairdocs.org/sdr/CED2004F00000.md): Tire · separated · Jan 8, 2004 · N233CA · Lear 25B · Tire
  > ON 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, FOU
- [SDR 2004FA0000020](https://openairdocs.org/sdr/2004FA0000020.md): Pump · leaking · Jan 6, 2004 · Lear 25B · Engine Fuel Pump
  > INSTALLED OVERHAULED FUEL PUMP FROM MFG ON 4NOV03. DURING AIRCRAFT INSPECTION 22DEC04 HAD FUEL SEEP FROM WIRES ON PUMP.
- [SDR CED2003F00000](https://openairdocs.org/sdr/CED2003F00000.md): Filter · inoperative · Nov 15, 2003 · N233CA · Lear 25B · Aircraft Fuel Filter/Strainer
  > ON 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 20
- [SDR 2004F00326](https://openairdocs.org/sdr/2004F00326.md): Engine · flamed out · Sep 24, 2003 · N67HB · Lear 25B · Engine (Turbine/Turboprop)
  > ON 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 STA
- [SDR 2003F00580](https://openairdocs.org/sdr/2003F00580.md): Panel · departed · Aug 24, 2003 · N8005Y · Lear 25B · Fuselage Structure (General)
  > AIRCRAFT 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)
- [SDR CYO2003F00000](https://openairdocs.org/sdr/CYO2003F00000.md): Indicator · shorted · Jul 16, 2003 · N140CA · Lear 25B · DME/TACAN System
  > AIRCRAFT 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.
- [SDR 070103](https://openairdocs.org/sdr/070103.md): Bleed Valve · out of adjust · Jul 1, 2003 · N425JL · Lear 25B · Compressor Bleed Valve
  > WHILE 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.
- [SDR 2003FA0000480](https://openairdocs.org/sdr/2003FA0000480.md): Fire Loop · loose · May 12, 2003 · N23RZ · Lear 25B · Smoke Detection
  > FIRE 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.
- [SDR DRU2003F00000](https://openairdocs.org/sdr/DRU2003F00000.md): Blanket · burned · Feb 10, 2003 · N7810W · Lear 25B · Airfoil Anti/De-ice System
  > DURING 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 BURNT
- [SDR CA030110006](https://openairdocs.org/sdr/CA030110006.md): Starter Gen · failed · Dec 12, 2002 · Lear 25B · Starter-Generator
  > (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 IDL
- [SDR 110702](https://openairdocs.org/sdr/110702.md): Engine · flamed out · Nov 6, 2002 · N254SC · Lear 25B · Engine (Turbine/Turboprop)
  > ENGINE 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
- [SDR 102302](https://openairdocs.org/sdr/102302.md): Regulator Valve · malfunctioned · Oct 22, 2002 · N425JL · Lear 25B · Hydraulic Pressure Relief Valve, Main
  > AT 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 RE

Next page: https://openairdocs.org/model/gates-lear-jet-25b/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/model/gates-lear-jet-25b/reports

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