Learjet 35A

Service difficulty reports · 726

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 = '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 BSYA2012004Connector · looseCREW EXPERIENCED YAW DAMPER ISSUES SHORTLY AFTER TAKEOFF, RETURNED TO LCK. MAINTENANCE RE-SECURED PRIMARY YAW DAMPER RATE GYRO CONNECTOR, OPS CHECKS GOOD.Jan 9, 2012 · N959SA · Lear 35A · Auto Flight System WiringSDR JKIR2012010619587Line · corrodedNLG EXTEND ALUMINUM HYD LINE AT FRAME 9L, STRINGER 19, RUPTURED DUE TO INTERNAL CORROSION. THIS CAUSED ACFT TO LOSE HYD PRESSURE IN-FLIGHT. ACFT LANDED WITHOUT INCIDENT.Jan 6, 2012 · N754WS · Lear 35A · Hydraulic System, MainSDR G1IA2201212162013Downlock Switch · contaminatedAT APPROXIMATELY 20:00 HRS ON APPROACH INTO KTN SEVERAL GEAR CYCLES REQUIRED TO EXTEND RIGHT MAIN LANDING GEAR. ONCE THE GEAR WAS DOWN AND LOCKED THE CREW LANDED WITHOUT FURTHER PROBLEMS. MAINTENANCE FOUND WATER IN THE ACTUATOR SWITCH BOSS ON THE RIGHT MAIN Dec 16, 2011 · N35CY · Lear 35A · Landing Gear Position and WarningSDR RMV2012F00000Wire · brokenAFTER LEVEL OFF, HEARD A BANG, NOTICED AC STARTED TO DUTCH ROLL AND AP DISCONNECTED. INITIATED EMER DESCENT AND AC FLIGHT STABILIZED. NOTICED AFCS YAW CIRCUIT BREAKER WAS POPPED AND PRI AND SEC YAW DAMPER WAS INOPERATIVE, CREW ELECTED TO NOT RESET THE CIRCUIDec 14, 2011 · N456CL · Lear 35A · Auto Flight System WiringSDR O9IA2011120800011Controller · out of toleranceRIGHT ENGINE FIRE LIGHT CAME ON IN FLIGHT. PULLING POWER BACK THROUGH 86.7 PERCENT FAN, THE LIGHT WENT OUT.Dec 8, 2011 · N542LM · Lear 35A · Fire DetectionSDR CA111205005Actuator · leaking(CAN) THE PILOTS REPORTED THAT THEY HAD LOST HYDRAULIC PRESSURE AND THEN DECIDED TO RETURN TO BASE. THE LANDING GEAR WAS EXTENDED BY USING THE ABNORMAL CHECKLIST PROCEDURE. MAINTENANCE FOUND THAT THE RT MLG ACTUATOR TO BE LEAKING FLUID WHILE THE GEAR IS IN MNov 30, 2011 · Lear 35A · Landing Gear ActuatorSDR BKEA20111009 1Heater · smokeWHITE SMOKE AND FUMES FROM AFT RT PASSENGER OVERHEAD VENT. IMMEDIATELY RETURNED AND UNEVENTFUL LANDING AT DEPARTURE. FOUND AUX HEAT HEATER ODOR, PLACARDED AUX HEAT SWITCH INOPERATIVE IAW MEL 21-20.Oct 9, 2011 · N387HA · Lear 35A · Heating SystemSDR CVGA112792Unknown · malfunctionedCABIN PRESSURIZATION STARTED TO CLIMB AT A RATE OF 2000 FT PER MINUTE DURING DESCENT TO KLAS. PASSING THROUGH FL280, A LOUD POP WAS HEARD AND RUSH OF AIR BEHIND AIRCREW AND CREW IMMEDIATELY DONNED O2 MASKS. PASSING THROUGH FL220, REGAINED CONTROL OF PRESSURIOct 5, 2011 · N135DA · Lear 35A · Cabin Pressure Control SystemSDR ZP7A20110802001Brake Sys · contaminatedCREW REPORTED THAT THE BRAKES WORKED INTERMITTENTLY ON TAXI. A FEW MINUTES INTO THE TAXI, THE PEDALS WERE FIRM BUT BRAKING ACTION WAS MINIMAL OR NON-EXISTENT. CREW RETURNED TO THE FBO. MAINTENANCE CHECKED IT OUT - BLED THE BRAKE SYSTEM, SERVICED THE HYDRAULJul 30, 2011 · N38PS · Lear 35A · Landing Gear Brake SystemSDR KC8AN237CKPanel · arcedCO-PILOT NOTICED A FLASH ON HIS RIGHT SIDE AND HEARD A POPPING NOISE WITH NO SECONDARY INDICATIONS OR LOSS OF POWER. PILOT LOOKED AT HIS CIRCUIT BREAKER PANEL AND NOTICED SOME ARCING ON THE AC BUSS, TOP ROW CIRCUIT BREAKERS. CREW RETURNED TO BASE. MAINTENANJul 29, 2011 · N237CK · Lear 35A · Flight Compartment LightingSDR O9IA003Y 6.25.11Blower · burned outON DESCENT, THE FLIGHT CREW SMELLED AN ELECTRICAL BURNING ODOR IN THE CABIN. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. DURING THE APPROACH CREW HAD DEPLOYED OXYGEN MASKS FOR NURSES/PATIENT ON BOARD ACFT. INVESTIGATION OF ACFT FOUND NO HOT SPOTJun 25, 2011 · N544LM · Lear 35A · Air Distribution FanSDR O2MAN36062111Fire Warning · false activationDURING CLIMB TO ALTITUDE THE RT ENGINE FIRE LIGHT ILLUMINATED MOMENTARILY. THROTTLE LEVER WAS RETARDED MOMENTARILY BUT LIGHT WENT OUT WITH NO OTHER INDICATIONS OR WARNINGS. AIRCRAFT FIRE DETECTION SYSTEM CURRENTLY BEING INVESTIGATED FOR CAUSE OF MOMENTARY LIJun 21, 2011 · N360AX · Lear 35A · Fire DetectionSDR CA110622005Spoiler · mismanufacturedDURING INSPECTION, REPLACED FLIGHT CONTROL BECAUSE THEY ARE TIME EXPIRED. WHEN THE NEW SPOILER WAS RECEIVED WITH A KIT ALREADY INSTALLED, FITTING AND INSTALLING IT ON THE AIRPLANE WAS CARRIED OUT. BUT THE NEW SPOILER HAD THE CTR BRACKET ARM SUPPORT THRU BOLTJun 20, 2011 · Lear 35A · SpoilersSDR CVGA20110508001Cabin Pressure · malfunctionedCABIN PRESSURE CLIMBS AT 100 FPM AT FL 430, UPON DESCENT CABIN PRESSURE BEGAN 1000 FPM DESCENT AND WORKED NORMALLY THEREAFTER.May 8, 2011 · N135DA · Lear 35A · Cabin Pressure Control SystemSDR CVGA 11 120 1Unknown · malfunctionedCABIN FAILED TO MAINTAIN PROPER PRESSURE.Apr 30, 2011 · N135DA · Lear 35A · Cabin Pressure Control SystemSDR BSYA2011021Control Valve · inoperativeAFTER DEPARTING BKL AIRCRAFT WOULD NOT PRESSURIZE, CONTINUED ON TO LCK AT LOW ALTITUDE. LCK MAINTENANCE REMOVED AND REPLACED DEFECTIVE FLOW CONTROL VALVE, OPS CHECKS GOOD.Apr 20, 2011 · N15WH · Lear 35A · Cabin Pressure Control SystemSDR BSYA2011016Unknown · lack of lubeON TAKEOFF OUT OF PBI INBOARD GEAR DOORS DID NOT CLOSE, DOOR UNSAFE LIGHTS STAYED ON, SELECTED GEAR BACK DOWN AN RETURNED TO PBI NO PROBLEMS. GOT A FERRY PERMIT TO FLY AIRCRAFT GEAR DOWN TO MAINTENANCE BASE IN FXE. MAINTENANCE JACKED AIRCRAFT AND FOUND GEAR Mar 25, 2011 · N31WR · Lear 35A · Landing Gear Retraction/Extension SystemSDR BSYA2011015Adc · failedAIRCRAFT TAXIING OUT OF MSN FOR DEPARTURE IN A HEAVY DOWN POUR WHEN THE AIR DATA COMP FAILED FLAGGING ALTIMETER, ALTITUDE ALERTER HORN AND FLAGS. TAXIED BACK TO WISCONSIN AIR. REMOVED AND REPLACED AIR-DATA COMPUTER, AIRCRAFT REMAINS RVSM COMPLIANT.Mar 19, 2011 · N27BL · Lear 35A · Air Data ComputerSDR 2011FA0000173Control Box · detachedAUTOPILOT FAILED AT CRUISE FOLLOWED BY PRIMARY PITCH TRIM FAIL, MACH TRIM FAIL, DURING DESCENT AC BUSS TIE C/B POPPED. AMMETERS INDICATED 50 AMP DIFFERENCE. DURING TROUBLESHOOTING OF THE AUTOPILOT, PITCH TRIM, MACH TRIM & AC BUSS SYSTEMS FOUND CONNECTOR P213Mar 9, 2011 · N27AX · Lear 35A · AC Generation SystemSDR 2011FA0000161Unknown · odorCRUISING AT FL400 FOR APPROX 1 HR 45 MIN WITH NO INDICATION AT ANYTIME, SUSPECTED LIGHT EMERGENCY BLEED AIR ACTIVATED, SUSPECTED LIGHT DUE TO THE INCREASE IN THE CABIN TEMP. WITH A DISTINCT HOT ODOR FILLING UP IN THE ACFT CABIN, THE FLIGHT CREW DESCENDED TO FMar 8, 2011 · N990LC · Lear 35A · Air Distribution SystemSDR 2011FA0000159Sensor · failedDUCT TEMP SENSOR FAILED TO ALLOW THE PRESSURIZARION SYS TO OVERTEMP THE DUCTING.Mar 7, 2011 · N991AL · Lear 35A · Detection SystemSDR YRR82011020200001Turbine Blades · brokenAT 400 FEET AGL AFTER TAKEOFF, CREW HEARD LOUD BANG FROM LEFT (NR 1) ENGINE AND ENGINE RPM WENT TO 'ZERO'. CREW CIRCLED AND MADE SAFE EMERGENCY LANDING. ENGINE WAS REMOVED AND SENT TO MRO FACILITY; DURING ENGINE TEARDOWN, FIVE (5) HP TURBINE ROTOR BLADES WERE Feb 28, 2011 · Lear 35A · Turbine SectionSDR 2011F00045Fire Loop · false activationDURING APPROACH, THE LT FIRE WARNING LIGHT ILLUMINATED AND DID NOT EXTINGUISH AFTER LANDING WHEN THE ENGINE WAS SHUTDOWN. THERE WAS NO OTHER ABNORMAL INDICATIONS. NOTE THAT THE NACELLE HEAT WAS "ON" DURING APPROACH (DUE TO CLOUDS AND RAIN). TECH WAS SENT TOFeb 18, 2011 · N354CL · Lear 35A · Fire DetectionSDR BSYA2011009Switch · defectiveAIRCRAFT EN ROUTE FROM DPA TO MKC WHEN THE LANDING GEAR WOULD NOT COME UP, DIVERTED TO MAINTENANCE BASE IN LCK. MAINTENANCE FOUND GEAR UP TRUNNION SWITCH DEFECTIVE. REMOVED AND REPLACED SWITCH, OPS CHECKS GOOD.Feb 8, 2011 · N27BL · Lear 35A · Landing Gear Position and WarningSDR BSYA2010051Vertical Gyro · failedAIRCRAFT DEPARTED LCK WHEN THE V-G MONITOR LIGHT CAME ON, RETURNED TO LCK. MAINTENANCE REMOVED AND REPLACED VERTICAL GYRO, OPS CHECKED GOOD.Dec 28, 2010 · N474AN · Lear 35A · Attitude Gyro and Indicating SystemSDR CA101108004Bracket · cracked(CAN) DURING THE INSPECTION OF THE NOSE LANDING GEAR ASSEMBLY, A CRACK WAS DETECTED EXTENDING FROM THE PRESSED IN GREASE FITTING ON THE FORWARD ATTACH BRACKET. THIS BRACKET ATTACHES THE NOSE GEAR ACTUATOR TO THE NOSE LANDING GEAR ASSEMBLE. THE NEW UNIT INSTANov 4, 2010 · Lear 35A · Fuselage Miscellaneous StructureSDR BSYA2010044Pitot Tube · shortedEN ROUTE, WHEN THE LT PITOT CIRCUIT BREAKER POPPED. DIVERTED. MX R & R PITOT TUBE, OPS CHECKS GOOD.Nov 3, 2010 · N39DK · Lear 35A · Pitot/Static SystemSDR VIBR20110119002Throttle Cable · stiffACFT FERRIED INTO MX WITH SQUAWK AND A TENSION CHECK WAS ACCOMPLISHED ON THE THROTTLES. THROTTLE CABLES WERE FOUND EXTREMELY STIFF AND WORN OUT. THROTTLE CABLES WERE REPLACED WITH THROTTLE CONTROL ASSY. REF ENGINEERING LETTER 35121-17741.Oct 3, 2010 · N752AC · Lear 35A · Power LeverSDR O9IA 9.1.10Fire Loop · failedWE EXPERIENCED A FIRE WARNING INDICATION ON THE LT ENGINE IN 543 ON OUR DESCENT. THIS OCCURRED ABOUT 2330 LOCAL TIME. WE WERE AT FLIGHT IDLE AND DESCENDING THROUGH 13000 FEET WHEN THE LT ENGINE FIRE WARNING SYS ACTIVATED. WE HAD BEEN AT FLIGHT IDLE FOR OVERSep 1, 2010 · N543LM · Lear 35A · Fire DetectionSDR O9I2010F00000Fire Loop · shortedRETURNING WITH A PATIENT ON BOARD, RECEIVED A FIRE LIGHT ON NR 1 ENGINE DESCENDING THROUGH FL370 FROM OUR CRUISE ALTITUDE OF FL390. THE F/O WAS FLYING AND PILOT ACCOMPLISHED THE REQUIRED ITEMS FOR AN ENGINE FIRE. FIRELIGHT DID NOT GO OUT UNTIL 3 TO 4 MINUTESAug 16, 2010 · N543LM · Lear 35A · Fire DetectionSDR EZKA2010F00193Unknown · multiple failON VISUAL APPROACH, EXPERIENCED ELECTRICAL FAILURE IN ACFT. SELECTED FLAPS 8, AND COMPLIED WITH SPEED RESTRICTION OF 170 KNOTS, STARTED A DECENT FROM 2000 FT. FELT CABIN LOSE PRESSURIZATION AND GREEN NOSE WHEEL STEERING ANNUNCIATOR ILLUMINATED WITHOUT NOSE Aug 13, 2010 · N35GC · Lear 35A · Electrical Power SystemSDR CA100721007Alternator · failedPILOTS REPORTED THAT THEY HAD A DOUBLE GENERATOR FAILURE ENROUTE. THEY WERE ABLE TO RESET THE LT GENERATOR BUT COULD NOT RESET THE RT GENERATOR. UPON ARRIVAL, MX FOUND THAT THE CURRENT LIMITER ON THE RT GENERATOR WAS `OPEN`. THE GENERATOR WAS REMOVED IN ORDER Jul 20, 2010 · Lear 35A · AC Generator-AlternatorSDR BSYA2010032Pump · defectiveON APPROACH INTO CPS RIGHT ENGINE LOW OIL PRESSURE LIGHT CAME ON AND OIL PRESSURE GAUGE WAS AT THE TOP OF RED LINE. PILOT ELECTED TO SHUT THE ENGINE DOWN, AND LANDED NO PROBLEMS. REMOVED AND REPLACED OIL PUMP.Jun 30, 2010 · N400JE · Lear 35A · Turbine Engine Oil SystemSDR CA100706007Shutoff Valve · failed(CAN) WHEN RETRIEVING ITEM FROM THE TAIL LOCKER, OBSERVED THE LATCH TO BE VERY HOT TO THE TOUCH. UPON FURTHER INVESTIGATION, DISCOVERED AN ELEVATED TEMPERATURE IN THE TAIL CONE AREA. ALSO, OBSERVED THE FIRE BOTTLE PRESSURE TO BE VERY HIGH. AFTER DISCUSSING Jun 25, 2010 · Lear 35A · Windshield/Door Rain/Ice RemovalSDR N382010F00000Fire Loop · out of positionDURING CLIMB, LT ENGINE FIRE T-HANDLE ILLUMINATED. ALL ENGINE GAUGES INDICATED NORMAL. REDUCED POWER ON LT ENGINE. LIGHT EXTINGUISHED IN ABOUT 3 SECONDS AND FIRE LOOP TESTED NORMALLY. RAN THE APPROPRIATE CHECK LIST AND CONTINUED WITHOUT FURTHER ISSUE. WROTJun 17, 2010 · N825LJ · Lear 35A · Fire DetectionSDR 2010FA0000396Line · chafedTHE SOURCE OF A FUEL LEAK WAS TRACED TO THE RT MAIN FUEL LINE TO THE FILTER AND SHUTOFF VALVE IN THE AFT EQUIPMENT BAY JUST FWD OF THE RT MAIN SHIP BATTERY. THE FUEL LINE WAS CHAFED BY THE UNION FITTING OF A HYD LINE RUNNING PARALLEL TO THE FUEL LINE. UPON REMApr 21, 2010 · N10AH · Lear 35A · Aircraft Fuel Distribution SystemSDR BSYA2010020Actuator · failedDURING FINAL APPROACH INTO CLT DID NOT GET DOWN AND LOCK INDICATION ON RIGHT GEAR. BLEW GEAR DOWN AS A PRECAUTIONARY MEASURE. MAINTENANCE REMOVED AND REPLACED GEAR ACTUATOR AND DOWN LOCK SWITCH, OPS CHECKS GOOD.Apr 7, 2010 · N400JE · Lear 35A · Landing Gear ActuatorSDR BHKRSDR0110Fire Detector · false activationAFTER SIMULATED EMERGENCY DECENT TO 19K, LT FIRE WARNING LIGHT ILLUMINATED. EMERGENCY CHECKLIST MEMORY ITEMS COMPLETED (ENGINE FIRE-SHUTDOWN). LT FIRE WARNING LIGHT REMAINED ON. CREW DETERMINED THERE WAS NO FIRE (NO SECONDARY INDICATIONS) AND ELECTED TO RETMar 26, 2010 · N50FN · Lear 35A · Fire DetectionSDR 2010FA0000186Acoustic Liner · inadequateAFTER INSTALLATION OF ACOUSTIC OVERFRAME BLANKET, PN BK-8160 LOT NR 123009-BL60, MECHANICS NOTICED THAT ALL THEIR TOOLS USED TO CUT AND FIT THE BLANKETS RUSTED OVERNIGHT. FURTHER INVESTIGATION BY WAY OF A TEST, USING 2 NEW RAZORS, ONE USED TO CUT A PIECE OF BLFeb 25, 2010 · Lear 35A · Fuselage Miscellaneous StructureSDR 2010F00045Downlock Switch · intermittentWHEN SELECTING "GEAR DOWN" ON APPROACH TO DESTINATION AIRPORT THERE WAS NO RT DOWNLOCK "GREEN" ANNUNCIATOR. LANDING GEAR WAS CYCLED 5 TIMES. THE 5TH TIME SHOWED "3 GREEN" AND ACFT WAS LANDED WITHOUT INCIDENT. ACFT WAS JACKED AND GEAR WAS SWUNG. FOUND INTERMITTFeb 16, 2010 · N70AX · Lear 35A · Landing Gear Position and WarningSDR CA100204007Downlock Switch · out of rig(CAN) GEAR SWING CARRIED OUT AFTER REPLACEMENT OF STEERING MOTOR. FOUND SERVICEABLE. ACFT ACCEPTANCE TEST FLIGHT WAS CARRIED OUT AND CREW EXPERIENCED NO DOWN LOCK INDICATION ON LT MAIN. SECONDARY INDICATION FOR DOWN & LOCK ALSO NOT PRESENT. GEAR EMERGENCY EXTFeb 2, 2010 · Lear 35A · Landing Gear Position and WarningSDR BSYA2010007Light · inoperativeON APPROACH INTO RIC SELECTED GEAR DOWN BUT DID NOT HAVE A RIGHT MAIN GEAR DOWN AND LOCK LIGHT, LANDED NO PROBLEMS. MAINTENANCE REMOVED AND REPLACED BULB, OPS CHECKS GOOD.Jan 25, 2010 · N72JF · Lear 35A · Landing Gear Position and WarningSDR CA100127001Throttle Cable · sheared(CAN) ACFT WAS LEAVING AT ABOUT 0330AM. AT THE THRESHOLD, PILOT STARTED TO PUSH THE THROTTLES FWD, WHEN HE NOTICED THAT AT 60 PERCENT N1 THE RT ENGINE WAS ABNORMAL, RETARDED THE THROTTLE AND THE ENGINE SHUTDOWN. PILOT TRIED MULTIPLE RESTARTS, WITH NO SUCCESJan 23, 2010 · Lear 35A · Power LeverSDR BSYA2010003Actuator · malfunctionedON APPROACH GOING INTO DPA HAD NO RIGHT GEAR DOWN AND LOCK LIGHT, BLEW THE GEAR DOWN AND LANDED NO PROBLEMS. REMOVED AND REPLACED DEFECTIVE LANDING GEAR ACTUATOR, OPS CHECKS GOOD.Jan 8, 2010 · N27TT · Lear 35A · Landing Gear ActuatorSDR BSYA2009067Check Valve · defectiveSHORTLY AFTER TAKEOFF OUT OF APA CREW TURNED ON NACELLE HEAT AND THE CABIN FILLED WITH SMOKE, RETURNED TO APA NO PROBLEMS. MAINTENANCE FOUND THE BLEED AIR CHECK VALVE AT THE HYD RESERVOIR FAILED. REMOVED AND REPLACED CHECK VALVE, OPS CHECKED GOOD.Dec 30, 2009 · N27TT · Lear 35A · Pneumatic Distribution SystemSDR BSYAPin · bentON APPROACH INTO APA WHEN GEAR SELECTED DOWN HAD NO RIGHT MAIN DOWN AND LOCK INDICATION, CREW THEN USED EMERGENCY AIR TO BLOW THE GEAR DOWN THEN THE LIGHT CAME ON, LANDED OK. MAINTENANCE FOUND A BENT PIN AT THE GEAR ACTUATOR DISCONNECT CONNECTOR, STRAIGHTENEDDec 29, 2009 · N27TT · Lear 35A · Landing Gear System WiringSDR BSYA2009063Pressure Switch · failedAFTER TAKEOFF AT 15,000 FT THE LEFT ENGINE OIL-PRESSURE LIGHT CAME ON, GAUGE READ NORMAL PRESSURE, PILOT ELECTED TO RETURN TO BASE. MAINTENANCE REMOVED AND REPLACED DEFECTIVE OIL PRESSURE SWITCH, OPS CHECKS GOOD.Dec 25, 2009 · N39DK · Lear 35A · Engine Oil PressureSDR CA091123005Skin · cracked(CAN) DURING TROUBLESHOOTING OF AN UNRELATED DOOR SNAG, A CRACK WAS DISCOVERED ON THE FUSELAGE SKIN STARTING AT THE LWR FWD CORNER OF MAIN ENTRY DOOR CUTOUT. USING A 10X LOUPE, THE CRACK WAS MEASURED AT 0.270". EDDY CURRENT AND FPI INSP CARRIED OUT WHICH DETERNov 20, 2009 · Lear 35A · Fuselage Main, Plate/SkinSDR BSYA2009057Actuator · leakingEN ROUTE FROM CLT TO DPA WHEN THE CREW NOTICED ZERO HYDRAULIC PRESSURE, THEN DIVERTED TO ORL. BLEW GEAR DOWN AND LANDED NO PROBLEM. REMOVED AND REPLACED LEAKING RIGHT INBOARD GEAR DOOR ACTUATOR.Nov 17, 2009 · N701AS · Lear 35A · Landing Gear Door ActuatorSDR BHKR20091106001Fluid · leakingEXPERIENCED A PARTIAL IN-FLIGHT HYDRAULIC FLUID LOSS. GEAR BLOWN DOWN IAW ABNORMAL CHECKLIST. PARTIAL FLAP LANDING, EMERGENCY BRAKING NOT REQUIRED.Nov 3, 2009 · N51FN · Lear 35A · Hydraulic System, Main
Back to Learjet 35A