Learjet 35A

Service difficulty reports · 726

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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 = '35A'
  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 DELA200700006Downlock Sensor · false indicationON APPROACH, LOWERED LANDING GEAR AND HAD RED LIGHT ON RT MLG. RECYCLED GEAR, SAME RESULT. PERFORMED ELECTRICAL MALFUNCTION ALTERNATE GEAR EXTENSION, SAME RESULT. CHANGED LANDING LOCATION; LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED MALFUNCTIONING RT MLG Aug 20, 2007 · N431AS · Lear 35A · Landing Gear Position and WarningSDR 2007F00048Wire · burnedON DESCENT INTO HLN, SMOKE WAS NOTICED IN THE COCKPIT. THIS WAS PRECEDED BY AN AUG/AIL ANNUNCIATOR LIGHT ON THE GLARESHIELD. AN EMERGENCY WAS DECLARED, THE EMERGENCY CHECKLIST WAS ACCOMPLISHED, AND AN EMERGENCY LANDING WAS MADE. TWO COCKPIT CREW AND TWO MEDAug 16, 2007 · N55FN · Lear 35A · Electrical Power System WiringSDR 2007F00047Wire · burnedON DESCENT INTO HLN, SMOKE WAS NOTICED IN THE COCKPIT. THIS WAS PRECEDED BY AN AUG/AIL ANNUNCIATOR LIGHT ON THE GLARESHIELD. AN EMERGENCY WAS DECLARED, THE EMERGENCY CHECKLIST WAS ACCOMPLISHED, AND AN EMERGENCY LANDING WAS MADE. TWO COCKPIT CREW AND TWO MEDAug 16, 2007 · N55FN · Lear 35A · Electrical Power System WiringSDR 2007FA0000836Static System · misinstalledTHIS RVSM AIRCRAFT HAD AN ALTIMETRY SYSTEM SPLIT. CONTACTED STC GROUP HOLDER FOR PROPER ROUTING OF STATIC SYSTEM PLUMBING. FOUND CO-PILOTS SYSTEM WAS NOT CROSS COUPLED WITH PILOTS SYSTEM. INSTALLED FABRICATED HOSES TO THE CO-PILOTS SYSTEM TO MEET STC NR ST Aug 6, 2007 · N621RB · Lear 35A · Pitot/Static SystemSDR YNTA200777003Bolt · incorrectBINDING OF ELEVATOR FLIGHT CONTROL SYSTEM WITH RUBBING SOUND. DURING REMOVAL OF RIGHT HAND NOSE PANEL TO GAIN ACCESS TO BOB WEIGHT PANEL FOUND ONE BOLT SECURING BOB WEIGHT PANEL TO BE INCORRECT LENGTH AND TYPE PER THE LEAR 35/36 ILLUSTRATED PARTS CATALOG 27-3Aug 6, 2007 · N770JP · Lear 35A · Elevator Control SystemSDR 2007FA0000703Static Line · misinstalledTHIS RVSM AIRCRAFT HAD AN ALTIMETRY SYSTEM SPLIT. CONTACTED STC GROUP HOLDER FOR PROPER ROUTING OF STATIC SYSTEM PLUMBING. FOUND CO-PILOTS STATIC SYSTEM INSTALLATION WAS NOT CROSS-COUPLED WITH PILOTS SYSTEM. INSTALLED FABRICATED HOSES TO THE CO-PILOTS SYSTEM TAug 6, 2007 · N621RB · Lear 35A · Pitot/Static SystemSDR BSYA200700014Tube · bentAIRCRAFT ON IT'S WAY FROM DAL TO LCK WHEN THE PILOT NOTICED THE OIL PRESSURE DROPPING, HE THEN ELECTED TO SHUT THE ENG DOWN AND DIVERTED INTO MEM. ENGINE SHOP FOUND OIL TUBES BENT AND GASKET BAD. REPLACED ALL TUBES AND ONE GASKET AT THE N1 MONOPOLE.Jul 31, 2007 · N813AS · Lear 35A · Turbine Engine Oil SystemSDR BSYA200700013Fire Loop · defectiveAIRCRAFT EN ROUTE FROM ILG TO SDF WHEN THE LT ENGINE FIRE LIGHT CAME ON, PULLED FIRE HANDLE AND FIRED BOTH FIRE BOTTLES THEN DIVERTED TO LCK, LANDED NO PROBLEMS. MAINTENANCE FOUND ENGINE ACCESSORY FIRE LOOP DEFECTIVE, REMOVED AND REPLACED FIRE LOOP, OPS CHECKJul 30, 2007 · N400JE · Lear 35A · Fire DetectionSDR G41A2007002Unknown · unknownWAS ON AN AIR AMBULANCE TRIP FROM ABQ TO LAS WHEN ON ROLL OUT THE CAPTAIN NOTICED THE NR 2 ENGINE N1 INDICATION WAS 4 PERCENT LOWER THAN THE NR 1 ENGINE INDICATION. THE CREW REPORTED THE SITUATION AND WERE INSTRUCTED TO CHANGE AIRCRAFT. ON THE MORNING OF THEJul 26, 2007 · N46MF · Lear 35A · Engine (Turbine/Turboprop)SDR Y2PA200700024Bulb · burned outAIR WAS ENTERING DOWNWIND LEG AT AMA, AT APPROPRIATE TIME GEAR DOWN WAS CALLED FOR. LANDING GEAR SELECTED DOWN, LEFT MAIN DID NOT INDICATE DOWN "NO GREEN". LANDING GEAR WAS CYCLED BACK UP THEN BACK DOWN. UPON 2ND GEAR DOWN ATTEMPT ONLY THE NOSE WHEEL INDICAJul 24, 2007 · N135DE · Lear 35A · Landing Gear Position and WarningSDR DELA200700005Wire Harness · damagedLT ENGINE N1 LAGGED BEHIND RT ENGINE N1 ON TAKEOFF ROLL, AND ALSO LT ENGINE COMPUTER LIGHT CAME ON. FOUND (B) SOLENOID OF SERVO VALVE CONNECTOR HAD EXPOSED WIRE. RE-TERMINATED PINS (A) AND (B) OF CONNECTOR PLUG. CREW CONDUCTED HIGH POWER RUN AND HIGH SPEED Jun 27, 2007 · N431AS · Lear 35A · Turbine Engine System WiringSDR G41A2007001Unknown · malfunctionedFLYING AT 450 FROM MMUN TO ABQ THE CABIN ALTITUDE STARTED CLIMBING AND COULD NOT BE STOPPED, THE CREW STARTED A DESCENT TO 270 AND LANDED IN ELP. A FUNCTIONAL TEST OF THE PRESSURIZATION SYSTEM AND A CABIN LEAK RATE CHECK WERE COMPLETED. THE PROBLEM COULD NOTApr 30, 2007 · N43MF · Lear 35A · Cabin Pressure Control SystemSDR BSYA200700007Bevel Gear · damagedEN ROUTE FROM DAL TO APA AT FLIGHT LEVEL 36,000 FEET LEFT ENGINE COMPUTER FAIL LIGHT CAME ON AND THE ENGINE SHUT DOWN. RECYCLED COMPUTER AND IT CAME BACK ON LINE ATTEMPTED A START, WOULD NOT RELIGHT. LANDED APA NO PROBLEMS. FOUND 90 DEGREE GEAR BOX BEVELED Mar 20, 2007 · N98LC · Lear 35A · Turbine Engine Reduction GearSDR 2007FA0000162Spar Cap · corrodedVISUAL CONDITION CHECK PERFORMED ON HORIZONTAL STABILIZER AFT SPAR CAP AND ELEVATOR HINGE BRACKETS FOR CORROSION, BROKEN FASTENERS, ETC. FOUND SEVERE CORROSION ON UPPER SPAR CAP ASSEMBLY ALONG ENTIRE LENGTH. THIS REQUIRED REMOVAL AND REPLACEMENT OF UPPER SPAFeb 6, 2007 · N96FN · Lear 35A · Horizontal Stabilizer, Spar/RibSDR BSYA200700005Landing Gear · malfunctionedON ARRIVAL INTO STP SELECTED GEAR DOWN NOTHING HAPPENED, THEN BLEW GEAR DOWN AND LANDED NO PROBLEMS. MAINTENANCE COULD NOT DUPLICATE PROBLEM, CLEANED AND LUBED SWITCHES CYCLED GEAR MANY TIMES, OPS CHECKS GOOD.Jan 31, 2007 · N64CP · Lear 35A · Landing Gear SystemSDR 2007FA0000346Adc · malfunctionedDURING PRE-FLIGHT, THE CREW NOTED THAT THE PILOTS ALTIMETER AND ALTITUDE ALERTER WERE FLAGGED. ATTEMPTS TO RECYCLE THE SYSTEM WERE NOT SUCCESSFUL. THE CREW GROUNDED THE AIRCRAFT. AN AVIONICS TECH WAS DISPATCHED TO THE AIRCRAFTS LOCATION AND DETERMINED THATJan 22, 2007 · N813AS · Lear 35A · Air Data ComputerSDR 2007FA0000345Adc · malfunctionedWHILE ENROUTE, THE PILOTS ALTIMETER (FROZE UP) AT ABOUT 8000 FT AND THE OVERSPEED HORN WENT OFF. THE PILOT RECYCLED THE ADC AND ITS OPERATION WAS RESTORED. THE ADC WAS TESTED AND NO DEFECTS WERE FOUND. THERE WAS NO EVIDENCE OF WATER OR MOISTURE IN OR AROUNDJan 17, 2007 · N700SJ · Lear 35A · Air Data ComputerSDR BSYA200700002Valve · malfunctionedAIRCRAFT DEPARTED LCK AND WAS CLIMBING THRU 16,000 FT WHEN CABIN PRESSURIZATION STARTED TO CLIMB. AIRCRAFT RETURNED TO LCK WHERE MAINTENANCE FOUND BAD SAFETY VALVE PRESSURIZATION DIFFERENTIAL VALVE.Jan 9, 2007 · N51LC · Lear 35A · Cabin Pressure Control SystemSDR CA070105007Shaft · sheared(CAN) LT GENERATOR CAME OFF LINE .5 HR BEFORE LANDING . THE INDICATOR SHOWED 0 AMPS, A RESET WAS ATTEMPED BUT DID NOT COME ONLINE. WHEN MAINTENANCE REMOVED THE GENERATOR FOR INSPECTION, THE GENERATOR SHAFT WAS FOUND SHEARED. THE GENERATOR WAS INSPECTED FURTHERJan 3, 2007 · Lear 35A · Starter-GeneratorSDR A8J2007F00000Wheel · damagedON 1/2/2007, AC DEPARTED, DURING THE TAKEOFF ROLL. GROUND PERSONNEL REPORTED SMOKE FROM THE LT SIDE OF THE AC AROUND THE GEAR AREA. THE CREW WAS NOTIFIED. AC LOWERED ITS GEAR AND PERFORMED A FLIGHT BY THE TOWER. THE TOWER CONFIRMED THAT THE LT SIDE TIRES WJan 2, 2007 · N135FA · Lear 35A · Wheel/Ski/FloatSDR 2006FA0001230Wire · misinstalledCELL DIP SWITCH INSTALLED 180 DEGREES OUT. CELL WIRING MISROUTED AND IMPROPER GAUGE WIRE. MULTIPLE COLD CRACKED SOLDER JOINTS BROKEN AND POORLY REPAIRED TRACES. BATTERY T3 AND P3 ARE BROKEN. UNIT SENT BACK, AS CORE SEEMS TO BE A WORKMANSHIP ISSUE. (K)Dec 14, 2006 · N421SV · Lear 35A · Electrical Power System WiringSDR N382007F00000Throttle Cable · bindingNR 1 ENGINE FORWARD THROTTLE CABLE DISCOVERED TO HAVE A VERY ROUGH GRINDING FEEL. REPLACED FORWARD AND AFT NR 1 ENGINE THROTTLE CABLE ASSEMBLIES AND RIGGED IAW MM, OPERATION CHECKED NORMAL. DURING RESOLUTION OF THIS CONDITION. IT WAS DISCOVERED THAT BOTH CADec 11, 2006 · N825LJ · Lear 35A · Power LeverSDR JGV2006F00000Switch · malfunctionedDURING TAXI OPERATION FOLLOWING LANDING, THE PIC EXPERIENCED A FAILURE OF THE AIRCRAFT BRAKING SYSTEM AFTER COMPLETION OF A RT 90 DEGREE TURN. THE SIC THEN ATTEMPTED TO UTILIZE THE NORMAL BRAKING SYSTEM WITH SIMILAR RESULTS. THE PIC THEN ACTUATED THE EMERGENNov 29, 2006 · N452DA · Lear 35A · Landing Gear SystemSDR RISWS80701Turbine Blades · failedON 10/22/2006 AIRCRAFT WAS CLIMBING THROUGH 20,000 FT, CREW HEARD A BANG FROM THE BACK OF THE AIRCRAFT. THERE WAS NEW INDICATION OF ENGINE FAILURE. CREW ESTABLISHED LEVEL FLIGHT AT 22,000FT AND REVIEWED ENGINE INSTRUMENTS WITH NO INDICATION OF ENGINE FAILUREOct 22, 2006 · N995CR · Lear 35A · Turbine SectionSDR G41A2006001Engine · shutdownON 10/21/2006 ON AN AIR AMBULANCE TRIP, ON THE SECOND LEG, THE AIRCRAFT WAS ON THE GROUND FOR ABOUT 1.5 HRS WHILE TAXIING TO RUNWAY THE LT ENGINE SHUTDOWN FOR UNKNOWN REASON. THE CAPTAIN RESTARTED THE ENGINE AND CONTINUED THE TRIP WITH NO FURTHER PROBLEMS.Oct 21, 2006 · N46MF · Lear 35A · Engine (Turbine/Turboprop)SDR BSYA200600027Connector · damagedAFTER TAKEOFF OUT OF LCK PILOT SELECTED GEAR UP BUT NOTHING HAPPENED, RETURNED TO LCK WITH NO PROBLEMS. MAINTENANCE FOUND A PIN IN THE CONNECTOR PUSHED BACK THAT OPERATES GEAR UP SOLENOID. REPLACED DEFECTIVE PIN, OPS CHECKS GOOD.Oct 4, 2006 · N31WR · Lear 35A · Landing Gear System WiringSDR 2007FA0000094Adc · failedWHILE ENROUTE, THE PILOTS ALTIMETER FLAGGED AND OVERSPEED HORN TRIGGERED. THE ADC BEGAN TO WORK AGAIN AT THE END OF THE FLIGHT. THE ADC WAS FOUND TO BE DEFECTIVE AND REPLACED. THE SYSTEM WAS TESTED AND INSPECTED AND FOUND TO COMPLY WITH FAR 91-411, PART 43 Sep 29, 2006 · N813AS · Lear 35A · Air Data ComputerSDR CIEA200600007Check Valve · failedDURING MAINTENANCE OF THE BLEED AIR DISTRIBUTION SYSTEM DUCTING IN THE AFTER EQUIPMENT BAY AREA OF THE AIRCRAFT, SPECIFICALLY REMOVAL OF THE 3 WAY VALVE IN ORDER TO REPLACE SOME LEAKING SEALS, THE CHECK VALVE FOR THE RT ENGINE BLEED AIR SOURCE AIR WAS FOUND TOSep 7, 2006 · N222BE · Lear 35A · Air Distribution SystemSDR YNTA200677301Gasket · deteriorated1000 AGL NOTICED BURNING SMELL THAT INTENSIFIED BY 8000 AGL. NOTICED SMOKE IN THE CABIN FOLLOWED BY SMOKE IN COCKPIT. ALL CB'S, HEAT AND AC SWITCHES WERE CHECKED AND TURNED OFF RETURNED UNEVENTFULLY. GASKET P/N 2619036-1 BETWEEN DEICE DUCTS 2619033-11 AND 2619Aug 12, 2006 · N773DL · Lear 35A · Airfoil Anti/De-ice SystemSDR BSYA200600021Connector · dirtyGOING INTO CLT PILOT GOT A FIRE WARNING LIGHT ON THR RT ENGINE, FIRED ONE FIRE BOTTLE, STILL HAD THE LIGHT, FIRE THE SECOND BOTTLE NO HELP LANDED NO PROBLEM. MAINTENANCE CHECKED RESISTANCE IN ALL 3 FIRE LOOPS ALL WITHIN SPECKS, CLEANED CONNECTORS, RECONNECTEJul 23, 2006 · N400JE · Lear 35A · Fire DetectionSDR KC82006F00004Computer · inoperativeRT ENGINE, AT TAKEOFF POWER SETTING, WOULD NOT RESPOND TO A REDUCED POWER SETTING DURING TAKEOFF ROLLOUT. PILOT ABORTED TAKEOFF AND TAXIED BACK TO THE FBO. AFTER ENGINE SHUTDOWN AT THE FBO, THE LT MAIN OB AND BOTH RT MAIN TIRES WENT FLAT DUE TO OVER TEMPERATJun 12, 2006 · N72CK · Lear 35A · Fuel Control/Turbine EnginesSDR MFG2006F00000Fitting · crackedWHILE IN FLIGHT THE CREW EXPERIENCED A LOW HYDRAULIC PRESSURE LIGHT, THEY LANDED UNEVENTFULLY AND TAXIED TO THE FBO. IT WAS FOUND THAT THE HYDRAULIC HOSE ON THE LT MAIN GEAR ACTUATOR HAD COME LOOSE ON THE FITTING. AFTER INSPECTION OF THE HOSE AND FITTING IT May 16, 2006 · N42HN · Lear 35A · Landing Gear ActuatorSDR 2006FA0000473Hydraulic Line · leakingPRE-FLIGHT FOR SECOND LEG OF FLIGHT CREW REPORTED HYDRAULIC FLUID DRIPPING OUT OF REAR EQUIPMENT BAY. INSPECTION REVEALED THAT THE HYDRAULIC PRESSURE LINE HAD CHAFED THROUGH AND WAS LEAKING FLUID. INSTALLED NEW LINE. COMPLIED WITH PRESSURE CHECK OF SYSTEM WITHMay 10, 2006 · N222BG · Lear 35A · Hydraulic System, MainSDR 2006FA0000479Circuit Breaker · tripped(ELECTRICAL ANOMALY), LT AND RT ESSENTIAL (A) CIRCUIT BREAKERS DEPLOYED. ALL EFIS WENT DARK. YAW DAMP AND AUTO PILOT DISENGAGED. LOST ALL NAV AND COMM. RADIOS, LOST ANNUNCIATOR PANEL LIGHTS. MAY HAVE LOST AIRSPEED INDICATORS AND FUEL COMPUTERS. LOST BOTH May 8, 2006 · N242MT · Lear 35A · Electrical Power SystemSDR 11221Frame · crackedRH FUSELAGE FRAME 20 CRACKED APPROX. 11/8 IN LENGTH AT THE AFT WING ATTACH POINT.Apr 14, 2006 · N98LC · Lear 35A · Fuselage Main, FrameSDR CA060404001Hose · crackedDURING A SCHEDULED INSPECTION, THE AVIONICS TECHNICIAN VISUALLY DISCOVERED SEVERAL HOSES CRACKED IN THE RT PITOT/STATIC CIRCUIT. HOSES WERE FOUND CRACKED AND LEAKING ON THE LT PITOT/STATIC CIRCUIT APPROXIMATELY 1 MONTH AGO. THESE PARTICULAR HOSES WERE INSTALApr 3, 2006 · Lear 35A · Pitot/Static SystemSDR 2006FA0000380Fitting · misinstalledAIRCRAFT EXPERIENCED HORIZONTAL STABILIZER STALL DURING APPROACH, DURING SEVERE ICING. AIRCRAFT RECOVERED FROM STALL AND LANDING NORMAL. INSPECTION OF TAIL DE-ICE SYSTEM FOUND BLEED AIR LEAKING IN AFT PART OF TAIL AT 90 DEGREE ELBOW. DURING REMOVAL OF 90 DEMar 30, 2006 · N288JP · Lear 35A · Engine Anti-Icing SystemSDR BSYA200600013Flow Divider · low pressureCOMING INTO LCK LEFT ENGINE FLAMED OUT WHEN THROTTLE WAS BROUGHT BACK TO IDLE, LANDED AT LCK NO PROBLEMS. FOUND FLOW DIVIDER LOW PRESSURE, REMOVED AND REPLACED FLOW DIVIDER AND UPDATED N1DEEC ENGINE COMPUTER PER S/B TFE731-76-3076.Mar 22, 2006 · N31WR · Lear 35A · Powerplant SystemSDR BSYA200600012Engine · failedAIRCRAFT WAS EN ROUTE FROM UCA TO CYOW WHEN THE RIGHT ENGINE ITT WENT TO 963 DEGREES AND THE CREW FELT A VIBRATION AND SOUNDED STRANGE. AFTER LANDING IN CYOW CREW LOOKED UP TAIL PIPE AND NOTICED METAL LAYING IN TAIL PIPE. REMOVED AND REPLACED ENGINE.Mar 16, 2006 · N55F · Lear 35A · Engine (Turbine/Turboprop)SDR BSYA200600010Throttle Cable · brokenON TAKEOFF OUT OF PHL THE RIGHT ENGINE THROTTLE CABLE BROKE AND THE ENGINE WENT BACK TO IDLE, PILOT THEN ABORTED TAKEOFF. MAINTENANCE DID FIND AFT THROTTLE CABLE BROKEN. REMOVED AND REPLACED CABLE, OPS CHECKS GOOD.Mar 1, 2006 · N51LC · Lear 35A · Power LeverSDR BSY2006F00000Adc · defectiveDURING TAXI OUT, THE OVERSPEED WARNING ACTIVATED AND THE PILOTS ALTIMETER AND ALTITUDE ALERTER FLAGGED. THE CREW ABORTED THE DEPARTURE AND RETURNED TO THE RAMP. THE ADC WAS FOUND TO BE DEFECTIVE AND WAS REPLACED ON 2/27/2006. THE SYSTEM WAS TESTED AND INSPEFeb 27, 2006 · N27BL · Lear 35A · Pitot/Static SystemSDR 11143Fitting · crackedLT AND RT WING ATTACH POINT FITTING AT FRAME 20 IS CRACKED. LT IS CRACKED APPROX. 1.0 INCHES IN LENGTH. RT IS CRACKED APPROX. 1.25 INCHES IN LENGTH.Feb 23, 2006 · N81FR · Lear 35A · Fuselage, Wing Attach FittingsSDR WTXR10549Attach Bracket · crackedFOUND CRACK AT LT AND RT FUSELAGE FRAME 20 AT THE WING ATTACH POINT. LT CRACK IS APPROX 1.0 INCHES IN LENGTH, RT CRACK IS APPROX .75 INCHES IN LENGTH.Feb 8, 2006 · Lear 35A · Fuselage Main, Attach FittingsSDR BSYA200600004Throttle Cable · brokenON TAKE OFF OUT OF FXE, RIGHT THROTTLE CABLE BROKE, AIRCRAFT RETURNED TO FXE. MAINTENANCE FOUND RIGHT AFT THROTTLE CABLE BROKEN. REMOVED AND REPLACED THROTTLE CABLE, OPS CHECKS GOOD.Feb 2, 2006 · N122JW · Lear 35A · Power LeverSDR BSYA200600003Downlock Switch · defectiveON APPROACH INTO LCK LANDING GEAR WOULD NOT COME DOWN, CIRCUIT BREAKER POPS. PILOT BLEW GEAR DOWN, LANDED NO PROBLEMS. REMOVED AND REPLACED DEFECTIVE SWITCH, OPS CHECKS GOOD.Feb 2, 2006 · N56JA · Lear 35A · Landing Gear Position and WarningSDR BSYA200600007Control Valve · weakTAXING OUT OF AIRNETS RAMP AT LCK AIRPORT AIRCRAFT TAXIED OFF RAMP INTO THE MUD. AIRCRAFT RETURNED TO AIRNETS RAMP. MAINTENANCE REMOVED AND REPLACED TIRE AND WHEEL ASSY.ADJUSTED NOSE STEERING COMPUTER. A FEW DAYS LATER CHANGED ANTI SKID CONTROL VALVES FOR WEAKFeb 1, 2006 · N56EM · Lear 35A · Brake Anti-Skid SectionSDR HAG060001Wheel · failedRT OB MAIN WHEEL, BRAKE HALF, STRUCTURAL FAILURE DURING GROUND HANDLING, (TOWING). RESULTED IN DAMAGE TO LOWER LANDING GEAR TORQUE KNEE.Jan 20, 2006 · N11UF · Lear 35A · Wheel/Ski/FloatSDR HAG06001Wheel Half · failedRT OB MAIN WHEEL, BRAKE HALF, STRUCTURAL FAILURE DURING GROUND HANDLING, (TOWING). RESULTED IN DAMAGE TO LOWER LANDING GEAR TORQUE KNEE.Jan 20, 2006 · N11UF · Lear 35A · Wheel/Ski/FloatSDR 2006FA0000223Pitot System · intermittentON 1/4/06 PILOT REPORTED ALTIMETER JUMPS DURING DESCENT, 300 FT, AND WARNING HORN SOUNDS. NO OVERSPEED. ALTIMETER SYSTEM WAS TESTED, IAW SRM AND FOUND TO BE OPERATIONAL. NO TROUBLE NOTED. AIRCRAFT REMAINS RVSM COMPLAINT. (K)Jan 6, 2006 · N122JW · Lear 35A · Pitot/Static SystemSDR CA070402005Wheel · wrong part(CAN) DURING ROUTINE PRE-FLIGHT INSPECTION, NR 3 MAIN WHEEL ASSY FOUND TO BE ASSEMBLED INCORRECTLY. WHEEL HALF`S WERE MISALIGNED BY ONE BOLT HOLE. AMM 32-A2-00 PG.210. FORGED NRS AND LOT NRS WERE NOT ALIGNED. MAIN WHEEL ASSEMBLY REMOVED FROM AIRCRAFT, REPAIREDJan 2, 2006 · Lear 35A · Wheel/Ski/Float
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