Learjet 35A

Service difficulty reports · 726

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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 20000811SH015Hose · loosePILOT REPORTED LOSS OF HYDRAULIC PRESSURE DURING FLIGHT. AIRCRAFT LANDED AT MAIN BASE WITHOUT INCIDENT. INSPECTION REVEALED A LOOSE HYDRAULIC LINE (HOSE) AT THE LEFT MAIN GEAR ACTUATOR. POSSIBLE CAUSE, INCORRECT TORQUE AT INSTALLATION OF HOSE DURING PREVIOUJul 28, 2000 · N78MC · Lear 35A · Landing Gear ActuatorSDR 20001030SH001Gasket · defectivePASSENGER INFORMED FLIGHT CREW OF SMOKE IN AREA AT LT REAR CABIN BY DIVAN SEAT AND NOTED CARPET APPEARED TO BE MELTED. AIRCRAFT DIVERTED TO LAS VEGAS AS EMERGENCY LANDING. MAINTENANCE DISCOVERED DEFECTIVE GASKET AT EXIT DUCT THAT ROUTES BLEED AIR TO LT WING.Jul 13, 2000 · N261PG · Lear 35A · Airfoil Anti/De-ice SystemSDR 20001027SH003Gasket · tornAIRCRAFT EN ROUTE, WHEN PASSENGER NOTED ODOR AND SMOKE IN AREA AT LEFT REAR OF CABIN AT CARPETING. CARPET APPEARED HOT, UNDERSIDE MELTED. FLIGHT CREW DIVERTED TO LAS VEGAS. MAINTENANCE DISCOVERED TORN GASKET AT CABIN AIR DUCT, EXIT TO LT WING HEAT PLUMBING Jul 13, 2000 · N261PG · Lear 35A · Air Distribution SystemSDR 20000831SH008Downlock Switch · dirtyDSM - GOING INTO DSM, COULD NOT GET RIGHT GEAR DOWN AND LOCK INDICATION. CLEANED AND LUBED DOWN AND LOCK SWITCH. OPS CHECKED GOOD. (X)Jul 6, 2000 · N72JF · Lear 35A · Landing Gear Position and WarningSDR 20000720SH005Bearing · crackedDURING REMOVAL OF BOTH LEFT AND RIGHT LANDING GEAR, FORWARD TRUNNION BEARINGS. FOUND THE OUTER HOUSING WAS CRACKED COMPLETELY THROUGH ON BOTH BEARINGS. OLD BEARINGS WERE BEING REMOVED BECAUSE OF LOOSE BALLS. LANDINGS, 6,570. (X)Jun 23, 2000 · N19RP · Lear 35A · Main Landing Gear Attach SectionSDR 20000724SH006Tire · failedON TAKEOFF ROLL, PILOT FELT A TIRE BLOW. TAKEOFF REJECTED AND ACFT COASTED TO A STOP JUST AFTER TURNING OFF THE RUNWAY. INSPECTION REVEALED BOTH RIGHT MAIN TIRES HAD BLOWN WITH MINOR DAMAGE TO ANTI-SKID WIRING AND HYDRAULIC BRAKE LINES. REPLACEMENT TIRES INJun 9, 2000 · N69BH · Lear 35A · TireSDR 20001030SH002Actuator · leakingLANDING GEAR DID NOT RETRACT AFTER TAKEOFF. JACKED AIRCRAFT AND CONFIRMED PROBLEM. DETERMINED RIGHT GEAR ACTUATOR LEAKING FLUID FROM WEEP HOLE INDICATING AN INTERNAL LEAK. REPLACED ACTUATOR WITH SERVICEABLE ACTUATOR. (X)Jun 6, 2000 · N261PG · Lear 35A · Landing Gear ActuatorSDR 20001027SH004Actuator · leakingLANDING GEAR DID NOT RETRACT ON TAKEOFF; RETURN TO LAND. AIRCRAFT JACKED BY MAINTENANCE CONFIRMED THAT GEAR WOULD RETRACT TO ''IN-TRANSIT'' MODE ONLY. DETERMINED RIGHT MAIN GEAR ACTUATOR WAS LEAKING FROM WEEP-HOLE WHEN IN ''RETRACT'' POSITION AND A RETRACTIOJun 6, 2000 · N261PG · Lear 35A · Landing Gear ActuatorSDR 20000713SH014Actuator · leakingLANDING GEAR DID NOT RETRACT AFTER TAKEOFF. JACKED AIRCRAFT AND CONFIRMED PROBLEM. DETERMINED RIGHT GEAR ACTUATOR TO BE LEAKING FLUID FROM WEEP HOLE INDICATING AN INTERNAL LEAK. REPLACED ACTUATOR WITH SERVICEABLE ACTUATOR. (X)Jun 6, 2000 · N261PG · Lear 35A · Landing Gear ActuatorSDR 20000622SH029Wire · shearedUPPER CABIN ENTRY DOOR LATCH SWITCH WIRING, PLASTIC CONDUIT AND SHEARED WIRES. THIS KEPT DOOR WARNING LIGHT FROM COMING ON WHEN UPPER DOOR LATCH PINS WERE NOT ENGAGED. (X)Jun 3, 2000 · N593LR · Lear 35A · Door System WiringSDR 20000622SH030Battery · crackedBATTERY HAD APPROXIMATELY 2.5 INCH HORIZONTAL CRACK, APPROXIMATELY .25 INCH UP FROM BOTTOM ON THE SIDE OPPOSITE THE ELECTRICAL CONNECTOR OR THE FORWARD SIDE AS MOUNTED IN AIRCRAFT. CORROSION WAS SPOTTED ON BATTERY TRAY DURING PRE-FLIGHT. NO DAMAGE WAS DONE. Jun 2, 2000 · N593LR · Lear 35A · Battery/Charger SystemSDR CA000518017Wire · cut(CAN) LT MLG HAD NO LIGHT INDICATION. EMERG GEAR USED. BROKEN WIRE AT CR73 LT EQUIPMENT TRAY.May 16, 2000 · Lear 35A · Landing Gear System WiringSDR CA000614052Wire · broken(CAN) LEFT MAIN LANDING GEAR LIGHT HAD NO INDICATION. EMERGENCY GEAR DOWN WAS USED. FOUND A BROKEN WIRE AT CR73 LT EQUIPMENT TRAY (REAR BAY). SEVERAL GEAR SWINGS CARRIED OUT. EMERGENCY SYSTEM VERIFIED AND AIRCRAFT RETURNED TO SERVICE. (X)May 16, 2000 · Lear 35A · Landing Gear System WiringSDR CA000614053Engine · failed(CAN) RT ENGINE FLAME OUT IN DESCENT. AIR IGNITION WAS ALREADY ON. ENGINE SPOOL DOWN THEN RELIGHT WITH NO ACTION TAKEN. FUEL FILTERS AND OUTPUT PRESSURE CHECK. PERFORMANCE CARRIED OUT AND ACCEL/DECEL CARRIED OUT. SUSPECT HEAVY PRECIPITATION.May 16, 2000 · Lear 35A · Engine (Turbine/Turboprop)SDR 20000508SH008Bolt · crackedTWO OF 12 WHEEL BOLTS (FROM 2 WHEELS) WERE FOUND REJECTABLE FOR CRACKS. ALL 12 BOLTS WILL BE REPLACED. THESE PARTS WERE TESTED FOR MILLION AIR, SALT LAKE CITY, UT, IAW ASTM E-1444-94A.Apr 14, 2000 · N911AE · Lear 35A · Wheel/Ski/FloatSDR 20001030SH004Packing · leakingPACKINGS LEAKED HYDRAULIC FLUID FROM LEFT INBOARD BRAKE FITTING BETWEEN HOSE AND BRAKE HOUSING. RAYTHEON ACFT SERVICES REPLACED PACKING AND O-RING AT BRAKE FITTING. BLED BRAKE SYSTEM AND SERVICED HYDRAULIC RESERVOIR. AIRCRAFT RETURNED TO SERVICE. (X)Mar 27, 2000 · N110FT · Lear 35A · BrakeSDR 20001030SH003Fitting · leakingLEFT INBOARD WHEEL BRAKE ASSY LEAKED HYDRAULIC FLUID. MAINTENANCE FOUND FITTING IN BRAKE HOUSING TO FLEX. HYDRAULIC HOSE WAS LEAKING. REPLACED O-RING AND BACK-UP RING ON FITTING. LEAK CHECKED AND BLED BRAKES. NO DEFECTS NOTED. (X)Mar 27, 2000 · N110FT · Lear 35A · BrakeSDR 20000425SH043Wheel · failedWHEN AIRCRAFT RETURNED FROM TRIP, IT WAS NOTICED THAT PART OF THE NR 4 OUTER WHEEL HALF WAS MISSING AND THE TIRE WAS RIPPED IN THE SIDEWALL. APPROXIMATELY ONE-HALF OF THE BEAD RADIUS WAS MISSING FROM WHEEL. A CRACK IN THE WHEEL MAY HAVE BEEN MISSED DURING THMar 20, 2000 · N18ST · Lear 35A · Wheel/Ski/FloatSDR 20000414SH003Wheel · damagedWHEN AIRCRAFT ROLLED UP TO GATE, NOTICED PART OF THE NR 4 OUTER WHEEL HALF WAS MISSING. APPROXIMATELY ONE-HALF OF THE WHEEL BEND WAS GONE AND TIRE DESTROYED. NO DAMAGE WAS FOUND AT NR 3 TIRE OR WHEEL. (X)Mar 20, 2000 · N18ST · Lear 35A · Wheel/Ski/FloatSDR 20000331SH022Valve · failedAIRCRAFT CABIN DID NOT PRESSURIZE WHEN DEPARTING. AIRCRAFT RETURNED TO LAS VEGAS FOR REPAIR. CABIN FLOW CONTROL VALVE WAS FOUND DEFECTIVE. AN OVERHAULED CABIN FLOW CONTROL VALVE WAS INSTALLED. GROUND RUNS STILL WERE NOT SATISFACTORY. FURTHER INVEST REVEALMar 10, 2000 · N45AE · Lear 35A · Pressure Regulator/Outflow ValveSDR 20000504SH019Valve · failedDEN - LOST PRESSURIZATION AFTER TAKEOFF OUT OF DENVER. FOUND FLOW CONTROL VALVE STUCK CLOSED. REMOVED AND REPLACED FLOW CONTROL VALVE. OPS CHECKED GOOD. (X)Mar 9, 2000 · N56JA · Lear 35A · Fuel Controlling SystemSDR 20000413SH052Smoke · detectedCARPET EDGE CAME INTO CONTACT WITH WING HEAT DUCT. WING HEAT WAS USED LONGER THAN NORMAL DUE TO WEATHER CONDITIONS. THE CARPET EDGE WAS HEATED UNTIL IT STARTED SMOKING. THE AIRCRAFT DIVERTED FOR PRECAUTION. THE CARPET WAS TRIMMED BACK AND ADDITIONAL INSULAMar 3, 2000 · N77NR · Lear 35A · Air Distribution SystemSDR CA000308005Thrust Reverser · unlocked(CAN) UPON LANDING, LT THRUST REVERSER DID NOT DEPLOY COMPLETELY WITH NO DEPLOY LIGHT. AFTER USING EMERGENCY, T/R WAS STILL IN UNLOCKED MODE. NORMAL ENGINE SHUT DOWN WAS CARRIED OUT. FURTHER INVESTIGATION REVEALED 4 RODS BENT AND PDU SHAFT SHEARED. IT APPEFeb 26, 2000 · Lear 35A · Engine Thrust ReverserSDR 20000329SH001Jackscrew · galledCREW BEGAN TO DESCEND OUT OF CRUISE, AIRCRAFT BECAME NOSE HEAVY. THE CREW COULD NOT TRIM AIRCRAFT STABILIZER AS BOTH PRIMARY AND SECONDARY PORTIONS OF THE STAB ACTUATOR FUNCTIONALLY FAILED. THIS UNIT HAD APPROXIMATELY 500 HOURS ON IT SINCE ITS 12,000 HOUR INFeb 11, 2000 · N573LP · Lear 35A · Elevator Tab Control SystemSDR CA000209010Attach Angle · damaged(CAN) FLIGHT LOADS AND FREE PLAY HAD ELONGATED THE BOLT HOLES FOR THE HORIZONTAL PITCH TRIM ACTUATOR ATTACHMENT, IN THE BUILD UP STEEL AND ALUMINUM STABILIZER RIB ASSY. IT IS SUSPECTED THAT THE LOW TORQUE APPLICATION AT PREVIOUS INSTALLATION HAD ALLOWED THE BOJan 29, 2000 · Lear 35A · Horizontal Stabilizer StructureSDR 2000ZZZX373Rod End · wornDURING A 1,200 HOUR T/R INSPECTION, FOUND WORN ACTUATOR ROD END BUSHING BRACKET. THE BRACKETS ARE ACTUALLY PART OF THE THRUST REVERSER DOOR. THEY ARE CAST INTO THE DOOR.Jan 20, 2000 · N10AH · Lear 35A · Engine Thrust ReverserSDR 2000ZZZX617Switch · failedGOING INTO BWI, HAD TO CYCLE GEAR 3 TIMES TO LET LEFT GEAR TO SHOW DOWN AND LOCK INDICATION. FERRIED AIRCRAFT BACK TO CMH. REMOVED AND REPLACED LEFT GEAR ACTUATORS SWITCH. OPS CHECKED GOOD.Jan 5, 2000 · N15WH · Lear 35A · Landing Gear Position and WarningSDR 99ZZZX4511Hose · leakingPILOT COMPLAINED OF HYDRAULIC LEAK IN WHEELWELL AREA. INVESTIGATION DISCLOSED MAIN GEAR ACTUATOR HOSE LEAKING AT B-NUT. CLEANED, OPERATED SYSTEM TO VERIFY, FOUND FLUID COMING FROM B-NUT CRACK. FURTHER INVESTIGATION DISCLOSED B-NUT TO BE CRACKED END TO END ANov 16, 1999 · N30GJ · Lear 35A · Landing Gear ActuatorSDR 2000ZZZX10Blower · inoperativeSMOKE CAME FROM VENTS ON APPROACH, 8 MILES FROM DESTINATION. TURNED OFF COCKPIT BLOWER, WENT ON OXYGEN, AND DECLARED EMERGENCY. GROUND RUN DETERMINED BLOWER WAS SMOKING. MEL'D AND RETURNED TO BASE. FOUND BLOWER MOTOR DEFECTIVE.Nov 15, 1999 · N235AC · Lear 35A · Air Distribution FanSDR 99ZZZX4612Wire · chafedRIGHT 'ROLEX' PANEL AFT OF CIRCUIT BREAKERS HOT, MELTED, AND PILOT CHECKLIST LYING NEXT TO PANEL IS MELTED ALSO. DISASSEMBLED RT CIRCUIT BREAKER PANEL. FOUND AND REMOVED 2 BUTT SPLICES ON NR 20 GAUGE WIRE FOR 40-AMP ESS BUSS. SOLDERED NR 10 GAUGE WIRE AND GNov 12, 1999 · N242MT · Lear 35A · Electrical Power System WiringSDR CA991208065Switch · failed(CAN) WHEN THE GEAR WAS SELECTED DOWN ON APPROACH, THE NOSE GEAR FAILED TO INDICATE DOWN AND LOCKED. THE EMERGENCY EXTENSION SYSTEM WAS USED AND THE AIRCRAFT LANDED SAFELY. THE NOSE GEAR DOWN AND LOCKED SWITCH ON THE NOSE GEAR WAS DIAGNOSED TO BE AT FAULT.Nov 10, 1999 · Lear 35A · Landing Gear Position and WarningSDR 99ZZZX4320Blower · failedCABIN AIR BLOWER SN 1092 INSTALLED 712-99. FAILED 10-29-99 WITH ONLY 106 HRS TSO. (STARTED MAKING NOISE THEN LOCKED UP AND CREATED BURNING SMELL IN CABIN). REPLACEMENT BLOWER SN 1102 INSTALLED 11-2-99 AND IT DID NOT LAST FIVE MINUTES. (BEGAN MAKING NOISE ANov 2, 1999 · N258G · Lear 35A · Air Distribution SystemSDR 99ZZZX4319Blower · failedCABIN AIR BLOWER SN 1092 INSTALLED 712-99. FAILED 10-29-99 WITH ONLY 106 HRS TSO. (STARTED MAKING NOISE THEN LOCKED UP AND CREATED BURNING SMELL IN CABIN). REPLACEMENT BLOWER SN 1102 INSTALLED 11-2-99 AND IT DID NOT LAST FIVE MINUTES. (BEGAN MAKING NOISE ANov 2, 1999 · N258G · Lear 35A · Air Distribution SystemSDR 99ZZZX4536Valve · crackedAS A RESULT OF A RECENT PRESSURE VESSEL INSP, FOUND THE SAFETY VALVE, PN 130406-1, SN 121-2018, DATED 12-22-81 BY LEAR, WAS FOUND TO HAVE A CRACKED NR 1 BOSS. BY DATE AND S/N, THIS VALVE IS NOT AFFECTED BY AD 95-20-03 (LEARJET SB 35-21-19). TO LOCATE CRACK, Oct 29, 1999 · N317TT · Lear 35A · Pressure Regulator/Outflow ValveSDR 99ZZZX4323Bolt · bentAILERON BOLT FOUND BENT. THIS IS A LIFE-LIMIT PART TO BE REPLACED EVERY 3,600 HOURS.Oct 26, 1999 · N98AC · Lear 35A · Elevator StructureSDR 99ZZZX4444Transmitter · fluctuatedCMH - LEFT RING OIL PRESSURE FLUCTUATING. RETURNED TO COLUMBUS. REMOVED AND REPLACED OIL PRESSURE TRANSMITTER. OPS CHECKED GOOD.Oct 25, 1999 · N684HA · Lear 35A · Engine Oil PressureSDR 99ZZZX4238Bearing · crackedDURING REMOVAL OF RIGHT MAIN LANDING GEAR ASSY FOUND OUTER HOUSING OF FORWARD TRUNNION BEARING CRACKED COMPLETELY THROUGH. INSTALLED NEW ONE. BALL WAS EXTREMELY LOOSE IN HOUSING. LANDINGS: 8,189.Oct 21, 1999 · N37FA · Lear 35A · Main Landing Gear Attach SectionSDR 99ZZZX4425Motor · failedPILOTS NOTICED COCKPIT BLOWER SEEMED TO BE SHUT OFF. KNOB INDICATED IT WAS ON HIGH. SHUT OFF BLOWER AND IMMEDIATELY TURNED IT BACK ON. A FEW SECONDS LATER, A PUFF OF SMOKE CAME FROM COCKPIT . IMMEDIATELY TURNED OFF BLOWER AND DIVERTED TO DENVER. TECH VERIOct 11, 1999 · N950SP · Lear 35A · Air Distribution FanSDR 99ZZZX3980Switch · failedMEM - RT MAIN GEAR NOT SHOWING DOWN AND LOCK, RETURNED TO CMH AND LANDED, NO PROBLEMS. REMOVED AND REPLACED SWITCH. OPS CHECK GOOD.Sep 14, 1999 · N959SA · Lear 35A · Landing Gear Retraction/Extension SystemSDR 99ZZZX3537Unknown · smokeMKC - AFTER TAKEOFF, GOT SMOKE IN CABIN. RETURNED TO MKC. MAINTENANCE COULD NOT FIND ANY PROBLEMS, TEST FLEW AIRCRAFT HAD NO PROBLEMS. SUSPECT AUXILIARY CABIN HEATER MIGHT HAVE BEEN ON.Sep 2, 1999 · N700SJ · Lear 35A · Air Distribution SystemSDR 99ZZZX2971Engine · failedTHE AIRCRAFT WAS EN ROUTE TO PICK UP PASSENGERS IN SARASOTA, FL PASSING THROUGH 41,000 FEET HEADING FOR 43,000 FEET, THE LEFT ENGINE FLAMED OUT. PILOT'S DESCENDED TO 25,000 FEET AND RELIT THE ENGINE ACCORDING TO CHECKLIST PROCEDURES. ACFT WAS LANDED WITHOUT Aug 9, 1999 · N78MC · Lear 35A · Engine (Turbine/Turboprop)SDR 99ZZZX3005Bulb · failedCMH - LEFT MAIN GEAR NO DOWN AND LOCK INDICATION. DID A FLY-BY CMH TOWER, LANDING LIGHTS WERE ON. LANDED, NO PROBLEM. REMOVED AND REPLACED BULB. OPS CHECKS OK.Jul 15, 1999 · N39DK · Lear 35A · Landing Gear Position and WarningSDR 99ZZZX1912Indicator · malfunctionedLEFT ENGINE EGT ERRATIC. ENGINE SHUT DOWN AND UNEVENTFUL LANDING ACCOMPLISHED. INSPECTION REVEALED TEMPERATURE INDICATING SYSTEM MALFUNCTION. REPLACED TURBINE TEMP GAUGE WITH SERVICEABLE UNIT, SYSTEM OPERATIONALLY CHECKS GOOD. NO RECOMMENDATION FOR PREVENTApr 27, 1999 · N72CK · Lear 35A · Engine Temperature Indicating SystemSDR 99ZZZX1966Volt Regulator · failedUPON START-UP, NR 1 GENERATOR WAS SELECTED ON. NO AMPERAGE LOAD SHOWED ON AMMETER. SUBMITTER SUGGESTED CAUSE OF FAILURE, INTERNAL PART.Apr 22, 1999 · N50MJ · Lear 35A · DC Generating SystemSDR 99ZZZX1727Bracket · crackedBRACKET CRACKED AT OPPOSITE END OF WHERE ACTUATOR MOUNTS. LEFT FLAP ACTUATOR BRACKET FOUND CRACKED AT INSPECTION. THE ENTIRE BRACKET IS COMPOSED OF 5 PIECES. THE TOP BRACKET IS CRACKED.Apr 9, 1999 · N10AH · Lear 35A · Trailing Edge Flap ActuatorSDR 99ZZZX1827Switch · failedAFTER TAKEOFF, THE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO THE AIRPORT WITHOUT INCIDENT. UPON MAINTENANCE EXAMINATION, DETERMINED THE RIGHT MAIN GEAR 'SQUAT SWITCH' HAD MALFUNCTIONED AND ELECTRICALLY PREVENTED GEAR RETRACTION. THE SWITCH WAApr 1, 1999 · N358PG · Lear 35A · Landing Gear Position and WarningSDR 99ZZZX2121Valve · malfunctionedSDL/IND - WHILE EN ROUTE AFTER CLIMB-OUT TO 40,000 FEET MSL, FLIGHT CREW NOTICED CABIN PRESSURIZATION CLIMBING. FLIGHT CREW MADE A PRECAUTIONARY EMERGENCY DESCENT AND DIVERTED TO GUP. MAINTENANCE REMOVED AND REPLACED BLEED AIR REGULATING VALVES. AIRCRAFT RETMar 20, 1999 · N292ME · Lear 35A · Pneumatic Distribution SystemSDR AU990351Turbine · failed(AUS) RIGHT ENGINE TURBINE FIR TREE ROOT FAILURE RESULTED IN TURBINE BLADE LOSS. EXTENSIVE FOD AND OUT OF BALANCE DAMAGE TO HIGH PRESSURE AND LOW PRESSURE TURBINE ASSEMBLIES.Mar 19, 1999 · Lear 35A · Turbine SectionSDR 99ZZZX3383Selector Valve · intermittentLANDING GEAR WOULD NOT RETRACT WHEN 'GEAR UP' SELECTED. SNOW, ICE AND SLUSH WERE SUSPECT. AIRCRAFT WAS JACKED AND CLEANED OF ALL MOISTURE AND GEAR OPERATED NORMALLY. AFTER TAKEOFF WITH DE-ICED GEAR, LANDING GEAR DID NOT RETRACT AGAIN. AIRCRAFT WAS JACKED AMar 15, 1999 · N925DM · Lear 35A · Landing Gear Door Retract SectionSDR 99ZZZX1377Bearing · roughAILERONS FELT A LITTLE STIFF IN FLIGHT. CHECKED FOR FREEDOM OF MOVEMENT AND GROUND BY MOVING AILERONS UP AND DOWN BY HAND. NO ABNORMALITIES NOTED. WHILE RESTRICTING AILERON MOVEMENT BY HOLDING PRESSURE ON THE AILERON SURFACE, ROUGH BEARINGS WERE NOTED. ALLMar 11, 1999 · N593LR · Lear 35A · Aileron Control System
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