Textron 750

Service difficulty reports · 2,733

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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 = '750'
  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 3S9A998CX012011Control Handle · brokenLANDING GEAR LEVER WOULD NOT SELECT IN THE UP POSITION AFTER TAKEOFF. GEAR DID NOT GO UP, 3 GREENS REMAINED ON. TROUBLESHOT SYSTEM, REPLACED LANDING GEAR CONTROL HANDLE IAW CESSNA 750 MM 32-30-01. OPS CK'D GOOD.Jan 1, 2011 · N998CX · Cessna 750 · Landing Gear SelectorSDR DJFA2011003Windshield · crackedDURING FLIGHT, CREW NOTED THE COPILOTS WINDSHIELD HEAT FAIL MESSAGE ON THE EICAS. SHORTLY AFTER THE NOTIFICATION, THE COPILOTS WINDSHIELD SHATTERED. THE ACFT DIVERTED AND LANDED SAFELY. MX CONFIRMED THE FAILED WINDSHIELD AND REPLACED IT.Dec 31, 2010 · N702FL · Cessna 750 · Flight Compartment WindowsSDR DXTA2011010304391Pdu · failedFLAP FAIL WITH FLAPS EXTENDED TO 4 DEGREES AND SLATS EXTENDED. TROUBLESHOT TO A BAD PVD IAW MM 27-50-00. R & R PVD, OPS CHECKED GOOD IAW MM 27-52-00.Dec 31, 2010 · N946QS · Cessna 750 · Trailing Edge Flap Control SystemSDR DJFA2011004Line · rupturedDURING FLIGHT, CREW NOTED A LOSS OF HYD FLUID IN HYD SYS A. CREW DIVERTED AND USED EMERGENCY GEAR EXTENSION PROCEDURES FOR LANDING. ACFT LANDED SAFELY. MX DISCOVERED THE FLEXIBLE HYD LINE ON THE NLG DAMAGED. THE LINE WAS REPLACED.Dec 30, 2010 · N978DB · Cessna 750 · Hydraulic System, MainSDR 2011FA0000005Pump · failedAFTER ENGINE START UP, CREW RECEIVED AN EICAS MESSAGE "LOW FUEL PRESS L". CREW THEN SHUTDOWN ENGINE AND CONTACTED MX. TROUBLESHOT TO DEFECTIVE LT FUEL BOOST PUMP. INSTALLED O/H FUEL BOOST PUMP, PERFORMED LEAK AND OP'S CHECK. NO OTHER DEFECTS WERE NOTED.Dec 30, 2010 · N114VW · Cessna 750 · Fuel Boost PumpSDR DXTA2010122704378Rudder · malfunctionedUNCOMMANDED LT RUDDER INPUT DURING CRUISE FLIGHT. TROUBLESHOT RUDDER CONTROL SYS, PERFORMED TEST OF LINEAR ACTUATOR, ALL CHECKED NORMAL. PERFORMED OPS CHECK OF UPPER RUDDER, ALL CHECKED GOOD. INSPECTED COMMAND BUNGEE DURING RUDDER MOVEMENT, ALL CHECKED GOODec 26, 2010 · N987QS · Cessna 750 · Rudder Control SystemSDR DXTA2010122704381Unknown · unknownUPON GEAR RETRACTION , THERE WAS A LOUD "THUD" WHICH WAS FELT AS WELL AS HEARD. WHEN THE NOISE OCCURED THE ACFT MOMENTARILY YAWED. TROUBLESHOT PROCEDURES IAW MM 32-30-00. PERFORMED LANDING GEAR CONTROLS MANIFOLD INTERNAL BLEED RATE, OPS CHECKED GOOD, SERVICEDec 25, 2010 · N970QS · Cessna 750 · Main Landing GearSDR DXTA2010122304377Strut · dischargedON TAKEOFF GEAR HANDLE WOULD NOT COME UP. JACKED ACFT, FOUND NOSE STRUT SERVICE TO BE FLAT AND RESERVICED UPPER BARREL, SERVICED LOWER BARREL, VERIFIED BRAKE HANDLE OPERATION, ALLOWED STRUT TO SIT. COMPLETED LEAK CHECK. LEAK CHECKS GOOD. ALL WORK DONE IAW MDec 22, 2010 · N978QS · Cessna 750 · Nose/Tail Landing Gear Strut/AxleSDR DXTA2010122304375Elastomer · failedUPON LANDING GEAR RETRACTION, THERE IS A LOUD "CLUNKING/THUMPING" SOUND WITH ASSOCIATED SHAKING. THE SOUND OCCURS AT THE BEGINNING OF THE RETRACTION SEQUENCE, AS THE GEAR LEVER IS MOVED TO THE UP POSITION. NOISE AND VIBRATION ARE LIKELY LOUD ENOUGH FOR A PASSEDec 22, 2010 · N970QS · Cessna 750 · Nose/Tail Landing GearSDR DXTA2010121104358A/C Pack · leakingSTRONG TURBINE OIL ODOR IS COMING FROM THE ACMS WITH THE APU RUNNING. THE ODOR SOMEWHAT SUBSIDES WITH THE COCKPIT PAC OFF. THE OIL ON THE REAR (COCKPIT) ACM APPEARS DARK. R & R AFT ACM IAW MM. OPS AND LEAK CHECKED GOOD.Dec 9, 2010 · N944QS · Cessna 750 · Cabin Cooling SystemSDR DXTA2010120604348Damper · out of adjustUPPER RUDDER OSCILATES 30 PERECENT LT AND RT IN CRUISE AND DESCENT. FOUND YSAS DAMPER BUNGEE HAS .5" PLAY. REMOVED DISASSEMBLED, CLEANED AND REASSEMBLED. REINSTALLED AND RERIGGED YAW DAMPERS. ALL WORK IAW MM 27-24-00, OPS CHECKED GOOD, ALL YAW DAMPERS OPS Dec 3, 2010 · N997QS · Cessna 750 · Rudder Control SystemSDR DXTA2010120604347Strut · dischargedGEAR HANDLE WOULD NOT COME UP AFTER TAKEOFF. FOUND NOSE STRUT LOW, SERVICED NOSE STRUT IAW MM 12-10-38. CYCLED LANDING GEAR. NLG OPS CHECKED AND LEAK CHECKED GOOD.Dec 3, 2010 · N919QS · Cessna 750 · Nose/Tail Landing Gear Strut/AxleSDR DXTA2010120204343Rmu · failedNR 2 RMU FAILED. SCREEN BLACK BUT LINE SELECT LIGHTS WERE FLASHING ON AND OFF, TOXIC FUMES IN COCKPIT ELECTRICAL IN NATURE. REMOVED FAULTY NR 2 RMU, INSTALLED TESTED/INSPECTED RMU IN NR 2 POSITION IAW MM 23-80-01, OPS CHECKED GOOD.Dec 1, 2010 · N945QS · Cessna 750 · Communications SystemSDR DXTA2010120204342Actuator · failedAFTER TAKEOFF AMBER CAS "RUD LIMIT FAIL B" RUDDER LIMIT 90 PERCENT. RUDDER LOWER ACTUATOR FAILED CHECK. REMOVED LOWER ACTUATOR AND REPLACED WITH NEW. COMPLETED TASK 27-20-00-720, LOWER TRAVEL TEST, RUDDER CONTROL SYS LIMITER TEST, RUDDER TRIM TEST, UPPER RDec 1, 2010 · N907QS · Cessna 750 · Rudder Tab Control SystemSDR DXTA2010113004337Flap System · failedFLAPS FAILED ON CLIMB OUT IN UP POSITION. WOULD NOT RESET IN AIR. SLATS WORKED. TROUBLESHOT, FOUND NO BITES ON CONTROLLER. OPERATED FLAPS DOWN, INSPECTED FLAPS, FOUND SAND TYPE MATERIAL ON INBD FLAP TRACKS. CLEANED AREA, OPERATED FLAPS 25 TIMES WHILE INSPECNov 29, 2010 · N947QS · Cessna 750 · Trailing Edge Flap Control SystemSDR DXTA2010112904329Metering Valve · malfunctionedLT BRAKE AT BOTH CAPTAINS AND COPILOTS STATIONS INITIALLY GRAB WITH INITIAL INPUT TO BOTH BRAKE PEDALS. OPERATED BRAKES AND FOUND LT CABLE DOES NOT RETURN TO THE COMPLETED RELEASED POSITON. REMOVED RT FWD REFRESHMENT CENTER. DISCONNECTED BOTH CABLES AND FNov 27, 2010 · N949QS · Cessna 750 · Landing Gear Brake SystemSDR DXTA2010112904326Apu · leakingWHEN PULLING POWER BACK FOR DESCENT, AS SOON AS HP VALVES OPENED, GOT VERY STRONG "LIGHTING A MATCH" ODOR IN THE COCKPIT. R & R APU IAW CMM 49-10-10. OPS & LEAK CHECKED GOOD.Nov 26, 2010 · N922QS · Cessna 750 · APU Core EngineSDR DXTA2010112904325Line · leakingLEFT BRAKE GRABS HARD WHEN LIGHTLY APPLIED. FOUND LEAKING HYD LINE AT BRAKE FUSE. TIGHTENED & VERIFIED BRAKE HYD PRESSURES AT BRAKE METERING VALVE, RUDDER PEDALS & BRAKES IAW MM 32-42-00. OPS & LEAK CHECKED GOOD. TAXI CHECKED GOOD.Nov 26, 2010 · N922QS · Cessna 750 · Hydraulic System, MainSDR DXTA2010112904324Apu · odorVERY STRONG FUEL ODOR IN CABIN WITH APU RUNNING. BURNS EYES. SEEMS TO DISSIPATE AFTER APU SHUTDOWN AND ONLY ENGINES RUNNING. REMOVED CABIN & COCKPIT COALESCER SOCKS & CLEANED IAW MM 12-10-01, REV 40. COMPRESSOR HOUSING IN INLET VERY OILY. PERFORMED GEARBOXNov 26, 2010 · N922QS · Cessna 750 · APU Core EngineSDR DXTA2010112904322Flap System · malfunctionedFLAPS FAIL LIGHT ON IACAS AND AFTER RUNNING APPROPRIATE CHECKLIST, COULD NOT GET FLAPS AND SLATS PAST 5 DEGREES FOR LANDING. LANDED WITH FLAPS 5 AND SLATS OUT. FOUND NO FAULTS DEPICTED ON FLAP CONTROLLER INDICATIONS. ROTARY TEST GOOD. FLAPS MOVE TO ALL COMMANNov 24, 2010 · N946QS · Cessna 750 · Trailing Edge Flap Control SystemSDR DXTA2010112904321Pdu · malfunctionedGOT AMBER FLAP FAIL CAS MESSAGE ON FINAL APPROACH. WILL NOT RESET. FLAP CONTROLLER SHOWED FAULT BIT 2 UPON ARRIVAL. PERFORMED PDU CLUTCH CHECK IAW MM 27-52-00. PDU FAILS CLITCH CHECK. R & R FLAP PDU IAW MM 27-52-00. SYS OPS CHECKED GOOD IAW MM 27-52-00.Nov 24, 2010 · N944QS · Cessna 750 · Trailing Edge Flap Control SystemSDR DXTA2010112404320Wire · brokenLANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. AFTER 5 MINS IN FLIGHT MAIN GEAR RETRACTED AND EXTENDED BY ITSELF. TROUBLESHOT SYS IAW MM 32-30-00 AND WDM 32-30-01. FOUND WIRE GG001-EPY014 BROKEN OFF OF GROUND STUD GG001. REPAIRED WIRE AS REQUIRED IAW WDM 20-1Nov 23, 2010 · N918QS · Cessna 750 · Landing Gear System WiringSDR DXTA2010112204312Line · chafedFUEL BOOST ON LT EICAS MESSAGE ILLUMINATED IN FLIGHT AT 41000 FT. FOUND FUEL LINE COUPLINGS AND PINS CHAFED. REMOVED AND REPLACED LINE IAW MM 28-20-01.Nov 18, 2010 · N931QS · Cessna 750 · Fuel Boost PumpSDR DXTA2010111804310Coalescer Bag · dirtyDURING DESCENT THRU 9000 FT, STRONG FUMES WERE SMELLED IN THE PLANE. NO SMOKE WAS SEEN. THE FUMES SMELLED LIKE FROM ACM. REMOVED WATER SEPARATOR. COALESCER SOCKS FOR THE COCKPIT & CABIN PACK. FOUND THE CABIN SOCK WORN AND DIRTY. CLEANED SEPARATOR AND INSTALNov 17, 2010 · N906QS · Cessna 750 · Humidity Control SystemSDR DXTA2010111504307Flap System · malfunctionedON DEPARTURE, FLAPS FAILED TO RETRACT COMPLETELY & STOPPED AT 5 DEGREES WITH SLATS EXTENDED. ON ARRIVAL, MECH NOTED BITE CODE 2. CHECKLIST FOLLOWED FOR FLAPS 5 SLATS EXTENDED LANDING. FOUND LINT & DIRT IN FLAP BOX AROUND OPTICAL SWITCHES. REMOVED DEBRIS FNov 14, 2010 · N986QS · Cessna 750 · Trailing Edge Flap Control SystemSDR DXTA2010110804299Acm · seizedEVIDENCE OF SMOKE FROM COCKPIT A/C PACK. REMOVED AND REPLACED SEIZED ACM IAW MM 21-50-00. OPS CHECKED GOOD. NO EVIDENCE OF SMOKE IAW MM 21-50-00.Nov 5, 2010 · N930QS · Cessna 750 · Cabin Cooling SystemSDR DXTA2010110304288Brake Assy · malfunctionedDURING TAXI, ACFT PULLS TO THE RT AND TAKES EXCESSIVE POWER TO KEEP THE ACFT ROLLING. RT BRAKE IS HARD TO PRESS AS WELL. VISUALLY INSPECTED ACFT BRAKES. CYCLED BRAKES NUMEROUS TIMES. CHECKED TIRE PRESSURES. NO DEFECTS NOTED. HAD A CREW PERFORM A HIGH SPEED Nov 2, 2010 · N905QS · Cessna 750 · Landing Gear Brake SystemSDR DXTA2010110204285Acm · failedON INITIAL DESCENT, CREW & PAX NOTICED STRONG, PUNGENT ODOR (LIKE A STRUCK MATCH). ON REACHING A LOWER ALTITUDE, ISOLATED EACH PACK AND FOUND THE COCKPIT PACK TEMPERATURE TO BE UNCONTROLABLE IN AUTO & MANUAL. REMOVED AND INSTALLED COCKPIT ACM IAW MM 21-51-00Nov 1, 2010 · N920QS · Cessna 750 · Cabin Temperature ControllerSDR DXTA2010110104284Uplock Switch · out of adjustRED GEAR UNLOCK LIGHT DID NOT EXTINGUISH AFTER GEAR RETRACTION. NO ABNORMAL NOISE OR INDICATION GEAR WAS NOT UP NOTED. PERFORMED ABNORMAL CHECKLIST AND GEAR EXTENDED NORMALLY. JACKED ACFT, NLG STRUT EXTENSION CHECKED WITHIN LIMITS. OPERATED GEAR AND FOUND Oct 30, 2010 · N958QS · Cessna 750 · Landing Gear Position and WarningSDR DXTA2010102604274Warning Light · illuminatedDURING START FOR ARRIVAL, STAB BLEED LEAK-RT RED CAS MESSAGE ILLUMINATED & RED MASTER WARNING LIGHT. LIGHT REMAINED UNTILL 1,000 FT AGL. LIGHT OFF FOR 1 SEC & REILLUMINATED FOR DURATION. INTERROGATED DAV2 BOTH A TO B CHANNELS FOUND "STAB AFT STRUCTURE TEMP Oct 25, 2010 · N903QS · Cessna 750 · Airfoil Anti/De-ice SystemSDR DXTA2010102904282A/C Pack · inoperativeCABIN PAC TEMPERATURE CLIMBS UNCONTROLLABLY. SMOKE PRESENT IN COCKPIT. R & R CABIN (FWD) ACM IAW MM 21-52-00. OPS & LEAK CHECKED GOOD.Oct 23, 2010 · N931QS · Cessna 750 · Cabin Cooling SystemSDR DXTA2010101904266Coupling · wornWHEN TURNING LT, ABOUT 20 DEGREES OF BANK, BELOW 180 KT, FULLY CONFIGURED, THE AIRPLANE LT WING SUDDENLY DROPPED PULLING THE YOKE LT EVEN MORE. THIS HAPPENED MORE THAN 3 TIMES. FOUND LT AILERON POSITION SENSOR FLEXIBLY COUPLING LOOSE ON SHAFT AND RETRACTING Oct 18, 2010 · N948QS · Cessna 750 · Flight Control SystemSDR DJFA2010033Seal · leakingDURING CLIMB PHASE, CREW REPORTED "OIL LEVEL LOW - R" CAS MESSAGE. THE CREW CHECK THE RIGHT ENGINE OIL QUANTITY AND FOUND IT 8 QUARTS LOW. SHORTLY THEREAFTER, IT DROPPED TO 8.5 QUARTS LOW. CREW DECIDED TO DIVERT AND LAND AS SOON AS PRACTICAL. 5 MINUTES FROMOct 14, 2010 · N708LX · Cessna 750 · Turbine Engine Oil SystemSDR DJFA2010032Skin · corrodedRT WING DWG WT6792502-2, WT6792510 ZONE B2, LOWER SKIN WS 359.595 AT REAR SPAR CORROSION FOUND ON LOWER SKIN, REMOVED .016 OF MATERIAL MORE CORROSION STILL REMAINS. LOWER WING SKIN WAS REPLACED IAW REPAIR DEFINITION REPORT S-750-0145/08RD.Oct 14, 2010 · N709LX · Cessna 750 · Wing, Plate/SkinSDR DXTA2010101204260Strut · dischargedAFTER TAKEOFF, LANDING GEAR HANDLE WOULD NOT RETRACT. A SYS PRESSURE GOOD. CHECKLIST COMPLIED WITH. FOUND NLG STRUT NOT FULLY EXTENDED WHEN ACFT JACKED. PERFORMED NLG STRUT SERVICING IAW MM 12-10-38. PERFORMED LANDING GEAR EXTENSION AND RETRACTIONS CHECKED Oct 10, 2010 · N901QS · Cessna 750 · Nose/Tail Landing Gear Strut/AxleSDR DJFA2010026Hydraulic System · warning messageIN CRUISE FLIGHT, CREW NOTED HYDRAULIC QUANTITY LOW CAS MESSAGE AND CONFIRMED THE A-SYSTEM HYDRAULIC FLUID QUANTITY INDICATED 15 PERCENT. CREW NOTED ALSO THAT THE HYDRALIC FLUID TEMPERATURE WAS RISING. CREW BEGAN PREPARATIONS TO DIVERT, AS HYDRAULIC TEMPERATSep 27, 2010 · N709LX · Cessna 750 · Hydraulic System, MainSDR DXTA2010092204249Isolation Valve · inoperativeDURING OPS CHECKED NOTED THE COCKPIT TEMP CONTROL WOULD NOT OPERATE IN MANUAL OTC AUTO MODE. TURNED ON BLEED AIR, OPENED THE ISOLATION VALVE (UT007), NOTED THE COCKPIT OAC WOULD OPERATE WITH THE ISOLATION VALVE OPEN. R & R ISOLATION VALVE. OPS/LEAK CHECK GOOSep 21, 2010 · N918QS · Cessna 750 · Cabin Cooling SystemSDR DXTA2010092004242Squat Switch · out of adjustNOSE GEAR WOULD RETRACT AFTER T/O. GEAR EXTENDED WITH NO PROBLEM. ADJUSTED & CHECKED SQUAT SWITCH IAW MM 32-60-00. LANDING GEAR SYS OPS CHECKS GOOD. SQUAT SWITCH OPS CHECKED GOOD.Sep 19, 2010 · N960QS · Cessna 750 · Landing Gear Retraction/Extension SystemSDR DXTA2010092004247Line · leakingDURING FLIGHT - HYD PERCENT QTY A 15, 'HYD VOL LOW A' CAS, 'HYD O'TEMP A' CAS, A TEMP DEG C 101. COMPLIED WITH PILOTS ABBREVIATED CHECKLIST ABNORMAL PROCEDURED N2 "A" HYD SYS FLUID APPEARS TO BE LEAKING FROM CTR BELLY OF ACFT FWD OF MLG AT AFT PORTION OF SKID Sep 18, 2010 · N952QS · Cessna 750 · Hydraulic System, MainSDR DXTA2010091704239Acm · leakingHAD HEAVY SULFUR SMELL MULTIPLE TIMES OUT OF WEMACS, DURING FLIGHT. POST FLIGHT INSP REVEALED OIL DRIPPING OFF OF AFT ACM CASING. CLEANED HEAT EXCHANGERS. INSTALLED NEW AFT ACM TURBINE IAW MM 21-51-16. OPS CHECKED GOOD. LEAK CHECKED FAIL. 1 CONNECTION LESep 16, 2010 · N918QS · Cessna 750 · Cabin Cooling SystemSDR DXTA2010091604238Squat Switch · failedAFTER DEPARTURE, LANDING GEAR WOULD NOT RETRACT. LANDING GEAR HANDLE WOULD NOT MOVE. INSPECTED LANDING GEAR ASSY AND FOUND ON THE RT MAIN GEAR THAT THE COLLAR WAS MISSING FROM THE SQUAT SWITCH. R & R THE RT MAIN SQUAT SWITCH. OPS CHECK WAS GOOD. WORK PERFOSep 15, 2010 · N958QS · Cessna 750 · Landing Gear Retraction/Extension SystemSDR DXTA2010091304232Aileron Sys · bindingPLAY IN AILERON CONTROL & BINDING WHEN MOVING BOTH LT & RT OF NEUTRAL. BINDING NOTICABLE AT SPEEDS ABOVE 210 KIAS & BECAME WORSE AS SPEED INCREASED. AS SPEED DECREASED, BINDING & PLAY DECREASED. NOTHING ABNORMAL NOTICED DURING FLT CONTROL CHECK BEFORE & AFTESep 10, 2010 · N989 · Cessna 750 · Aileron Control SystemSDR 2010FA0001005Frame · crackedTHE PN 6760141-5 FRAME IS PART OF THE AILERON POWER CONTROL UNIT SUPPORT ASSY AND IS APPLICABLE TO ACFT 750-0001 TO 750-0149 THAT HAVE NOT BEEN MODIFIED BY SB750-27-44. DURING SCHEDULED INSP, THE FRAME WAS FOUND TO BE FATIGUE CRACKED. THE PART WAS REPLACED. Sep 8, 2010 · N948QS · Cessna 750 · Aileron Control SystemSDR DXTA2010090704224Landing Gear · malfunctionedNOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF, MAINS RETRACTED, GEAR EXTENDED NORMAL, WITH 3 GREEN LIGHTS RETURNED TO LAND.Sep 6, 2010 · N940QS · Cessna 750 · Landing Gear Retraction/Extension SystemSDR DXTA2010090704223Acm · seizedUNUSUAL ACRID ODOR IN COCKPIT AND CABIN. EMERGENCY DECLARED, DIVERTED AND LANDED WITHOUT INCIDENT. PAX STATED THAT ODOR DID NOT DISSIPATE UNTIL IMMEDIATELY BEFORE LANDING. R & R ACM IAW MM 21-51-00. OPS CHECKED GOOD LEAK CHECKED BAD. R & R BAD SEALS LEAK CHSep 6, 2010 · N918QS · Cessna 750 · Cabin Cooling SystemSDR DXTA2010090704219Engine · malfunctionedAFTER TAKEOFF, PASSING 5000 FT, FELT A SURGE AND LOOKED AND SAW THAT TURBINE PERCENT WAS RED AND SHOWING 101. BROUGHT THE POWER LEVERS BACK TO CLIMB AND THEN GOT AN AMBER "FAN DAMAGE R" CAS MESSAGE. FAULT CODES FOUND ON RT A & B FADECS ARE 401, 422, & 452. Sep 4, 2010 · N910QS · Cessna 750 · Engine (Turbine/Turboprop)SDR DXTA2010090104216Unknown · odorDURING DESCENT WHEN THRUST WAS REDUCED WE HEARD A BUMP NOISE FROM REAR OF AIRCRAFT. IMMEDIATELY WE BEGAN TO DETECT A BURNED OIL ODOR THAT LASTED APPROX 3 MIN. COCKPIT PAC TEMP WAS UNCONTROLLABLE FOR REST OF FLIGHT.Aug 30, 2010 · N999QS · Cessna 750 · Air Distribution SystemSDR DXTA2010083004213Brake Sys · malfunctionedRT BRAKE GRABS AND PULLS AIRPLANE TO THE RT ON LANDING AND DURING TAXI WHEN BRAKES ARE APPLIED. PERFORMED POWER BRAKE SYSTEM FUNCITONAL TEST; APPLIED PEDAL TORQUE TOOL AND BOTH R/H BRAKES WERE WITHIN 200PSI OF EACH OTHER, AND RESIDUAL PRESSURES WERE 50-60 PSIAug 28, 2010 · N942QS · Cessna 750 · Landing Gear Brake SystemSDR DXTA2010082704208Fadec · malfunctionedFAN DAMAGE RT ON DEPARTURE CLIMBING THROUGH 1,600 FT. N2 HAD A BRIEF SPIKE AT 102 PERCENT. RT FADEC A & B POSTING CODES 401, 422, & 452 ON POST FLIGHT. DOWNLOADED EICAS MESSAGES AND E-MAILED. REMOVED RT ENG CUG ACTUATOR, CLEANED AND APPLIED STABILANT 22 TOAug 27, 2010 · N910QS · Cessna 750 · Engine Indicating SystemSDR DXTA2010082604207Steering Unit · inoperativeON DEPARTURE, NOSE GEAR DID NOT RETRACT. CYCLED GEAR-OPS NORMAL. GEAR EXTENDED NORMALLY. TROUBLESHOT SYS AND FOUND NOSE STEERING UNIT NOT CTG WHEN NOSE GEAR RETRACTED. R & R NOSE WHEEL STEERING UNIT WITH A MODIFIED ONE. PERFORMED RIGGING PROCEDURES ON NOSEAug 25, 2010 · N940QS · Cessna 750 · Nose/Tail Landing Gear
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