Gates Learjet 55C

Service difficulty reports · 16

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 = '55C'
  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 CJPA202001210001Hydraulic Line · split20 MINUTES INTO CRUISE AT FL380 PIC NOTICED A LOW HYDRAULIC PRESSURE AMBER LIGHT ON THE ANNUNCIATOR. A QUICK LOOK AT THE HYDRAULIC PRESSURE GAUGE SHOWED ZERO PRESSURE IN THE HYDRAULIC SYSTEM. PIC AND FO TOOK OUT THE QRH AND FOLLOWED THE APPROPRIATE CHECKLIST. Jan 20, 2020 · N322GC · Lear 55C · Hydraulic System, MainSDR 2020F00047Tire · failedDURING A NORMAL TAKEOFF ROLL ON 19L AT KLAS ONE OF THE LEFT MAIN TIRES BLEW DUE TO A SUSPECTED ENCOUNTER WITH FOD AT APPROXIMATELY 105 KNOTS WITH A V1 TAKEOFF DECISION SPEED OF 136; THIS WAS ASSOCIATED WITH AN AUDIBLE "BANG". SHORTLY THEREAFTER THE AIRCRAFT BENov 14, 2019 · N178AM · Lear 55C · TireSDR 2017F00178Flow Valve · faultyON DEPARTING KCXY "CABIN ALT" LIGHT ILLUMINATED PASSING THROUGH 10,000 FEET. CAPTAIN ELECTED TO LAND AT KMDT INSTEAD OF THE FILED DESTINATION (FXE).Sep 20, 2017 · N178AM · Lear 55C · Cabin Pressure Control SystemSDR A8JA201606040022Circuit Breaker · trippedDURING APPROACH, FLIGHT CREW HEARD A POP AND EXPERIENCED A LOSS OF FLIGHT INSTRUMENTS AND RADIOS. PIC REPORTED ALL EFIS SCREENS, ALTIMETERS, AIRSPEED INDICATORS, FLAP INDICATION, GEAR INDICATION, YAW DAMPER, AND PRIMARY AND SECONDARY TRIMS INOPERATIVE. INVESJun 4, 2016 · N552T · Lear 55C · AC Power Distribution SystemSDR 2016FA0000016Strut · leakingUPON REACHING CRUISE ALTITUDE, THE GEAR UNSAFE INDICATOR ILLUMINATED. UPON INSPECTION OF THE NLG IT, WAS DISCOVERED THAT THE NITROGEN/FLUID DEPLETED THE PISTON ENOUGH TO CAUSE A SLIGHT MISALIGNMENT IN THE NOSE WHEEL WELL, CAUSING AN UNSAFE INDICATION IN THE FDec 21, 2015 · N717HB · Lear 55C · Nose/Tail Landing Gear Strut/AxleSDR 2011FA0000457Wheel Half · failedPRIOR TO LIFTOFF, THE OUTER RIM OF THE RIGHT INBD MAIN WHEEL SEPARATED FROM THE WHEEL ASSEMBLY. THE FLIGHT CREW WAS NOTIFIED BY RADIO THAT A "TIRE BLEW" DURING TAKEOFF. THE ACFT RETURNED TO BASE AND MADE AN UNEVENTFUL LANDING. BOTH RT MAIN WHEEL ASSEMBLIES Jul 10, 2011 · N385RC · Lear 55C · Wheel/Ski/FloatSDR OZCA11082009Valve · defectiveDURING A REPOSITIONING FLIGHT FROM FLL TO ORL AFTER DEPARTURE THE CAPTAIN NOTICED SMOKE FORMING IN THE CABIN AND RETURNED TO FLL FOR AN UNEVENTFUL LANDING. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE EMERGENCY PRESSURIZATION VALVE TO BE DEFECTIVE. THE UNov 8, 2009 · N211BC · Lear 55C · Cabin Pressure Control SystemSDR A8J2006F00001Hinge · failedAIRCRAFT DEPARTED, DURING CLIMB AT ABOUT 13,000 FT THE CREW NOTICED A STRANGE AIRFLOW NOISE AS IF A GEAR DOOR WAS OPEN, ALL INSTRUMENT INDICATIONS WERE GOOD. (3 GREEN). UPON LANDING, VISUAL INSPECTION NOTED THAT RT GEAR OB DOOR WAS MISSING. VISUAL INSP FOUNOct 30, 2006 · N552TL · Lear 55C · Landing Gear DoorsSDR CIEA200500011Latch · out of adjustAFTER TAKEOFF, THE LEFT THRUST REVERSER LIGHT FLASHED ON THEN WENT OUT. THE PILOT ELECTED TO LAND AND HAVE IT LOOKED AT. THERE WAS NO EVIDENCE THAT THERE WAS A PROBLEM. THE UNIT WORKED GOOD ON THE GROUND. THE T/R'S WERE PINNED AND DEFERRED AND THE FLIGHT CJul 24, 2005 · N113YS · Lear 55C · Engine Thrust ReverserSDR 2000ZZZX583Rivet · misinstalledSIX RIVETS MISSING FROM RT FUSELAGE BETWEEN MIDDLE AND AFT WING ATTACH POINTS. BS 401.92 AND BS 410.30. THESE RIVETS DO NOT GO THROUGH THE PRESSURE VESSEL, BUT DO GO THROUGH RT FUSELAGE OVERWING LONGERON. THREE RIVETS MISSING FROM AFT SIDE OF MIDDLE ATTACH Feb 7, 2000 · Lear 55C · Fuselage Miscellaneous StructureSDR 99ZZZX3497Fiting · failedAFTER TAKEOFF DURING GEAR REATRACTION, LOUD NOISE WAS HEARD IN CABIN. ALL SYSTEMS APPEARED NORMAL. UPON LANDING CREW FOUND RIGHT OUTBOARD GEAR DOOR ATTACH FITTING BROKEN AT TURNBUCKLE ATTACH POINT, AND BOLT, NUT, AND BUSHING STILL IN TURNBUCKLE. SUBMITTER REJul 29, 1999 · N10CR · Lear 55C · Landing Gear DoorsSDR NI2R032LLatch Pin Arm · crackedPERFORMED EDDY CURRENT TEST PER LEAR NDT MANUAL PART 3 52-10-01. DETECTED LINEAR INDICATION AT AREA 'F' AT APPROX 4 O'CLOCK POSITION. REFERENCE ST LOUIS TEST LAB 98F-0350. ACFT LANDINGS: 1,621. ACFT TT: 2,372 HOURS. TEST PERFORMED MARCH 2, 1998. (X)Feb 1, 1998 · N40CR · Lear 55C · Passenger/Crew DoorsSDR 97ZZZX3504Coupling · failedCLAMP ON COUPLING OPENED AND FELL OFF. COUPLING LOCATED IN FUEL SUPPLY LINE JUST BELOW LEFT FUEL FILTER IN TAIL CONE. AIRCRAFT CREW NOTICED DECREASING FUEL QUANTITY AND DIVERTED TO BNA. LEFT ENGINE THROTTLE SET TO IDLE WHEN PROBLEM NOTICED. ENGINE FLAMED OUJul 16, 1997 · N111US · Lear 55C · Aircraft Fuel Distribution SystemSDR 95ZZZX5253Clamp · defectiveINSPECTION FOUND FUEL FILTER CLAMP FAULTY. THIS IS FOLLOW-UP ON PREVIOUSLY SUBMITTED REPORT. SUBMITTER RECOMMENDED THAT CLAMPS UTILIZED IN AREAS SUBJECT TO VIBRATION BE SAFTIED WITH WIRE TO PREVENT INADVERTENT OPENING.Sep 7, 1995 · N40CR · Lear 55C · Aircraft Fuel Distribution SystemSDR 95ZZZX3690Pump · shaft strippedNR 1 ENGINE DRIVEN HYDRUALIC PUMP SHAFT WAS COMPLETELY STRIPPED OF ALL GEAR MATING SURFACE AREA RESULTING IN NO HYDRAULIC OUTPUT FROM THAT ENGINE. FOUND ON INITIAL ENGINE HOT SECTION INSPECTION.Jul 7, 1995 · N40CR · Lear 55C · Hydraulic Pump (Electric/Engine), MainSDR 95ZZZX3596Clamp · openedMAIN FUEL LINE SUPPLY FROM RT WING TO RT ENGINE CLAMP OPENED UP WHILE AIRCRAFT WAS IN FLIGHT CAUSING FUEL LOSS. FUEL IMBALANCE AND RIGHT ENGINE FLAME-OUT AFTER LANDING. THIS CLAMP IS EASILY OPENED BY JUST BUMPING IT. RIGHT MAIN FUEL LINE HAS NO STAND-OFF TOJul 1, 1995 · N40CR · Lear 55C · Aircraft Fuel Distribution System
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