Cessna 550

Service difficulty reports · 988

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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 = '550'
  ORDER BY difficulty_date DESC"

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SDR 2568Brake Assy · brokenRT MLG BRAKE LOCK UP DURING TAXI. AN INSP BY MAINT HAS DETERMINED THAT THE BRAKE STATOR CAME APART AND LOCKED UP THE BRAKE. THE C/A GIVEN WAS FOR THE REMOVAL AND REPLACEMENT OF THE OF THE RT WHEEL AND TIRE ASSY AND BRAKE. A GEAR SWING WAS ALSO PERFORMED IAW May 1, 2008 · N330DK · Cessna 550 · Landing Gear Brake SystemSDR 042908N319CSLamp · burned outDURING APPROACH,RT MLG, DOWN AND LOCKED INDICATOR DID NOT ILLUMINATE. AC FLIGHT MANUAL PROCEDURES FOLLOWED, GEAR WAS BLOWN DOWN AND EMERGENCY DECLARED. AC LANDED WITHOUT INCIDENT. TROUBLESHOOTING REVEALED A BAD LIGHT BULB. LIGHT BULB REPLACED AND OPERATIONALLYApr 29, 2008 · N319CS · Cessna 550 · Landing Gear Position and WarningSDR 6001LOXYGENOxygen Bottle · leakingINSTALLED REPAIRED EMERGENCY OXYGEN BOTTLE IN AC AND SERVICED. WHEN BOTTLE WAS TURN ON WAS FOUND TO LEAK FROM ON-OFF VALVE. UNIT WAS REPAIRED ON JANUARY 21,2008.Apr 23, 2008 · N6001L · Cessna 550 · Crew Oxygen SystemSDR 6001LENGAttach Angle · corrodedENGINE NACELLE ATTACHING FITTING ANGLE REMOVED FOR CORROSION. PARTS ARE CADMIUM PLATED, BUT NOT PAINTED. ALSO DISCOVERY IMPROPER DRILL HOLES AND RIVET SET DAMAGE AROUND SEVERAL HOLES.Mar 27, 2008 · N6001L · Cessna 550 · Nacelle/Pylon, Attach FittingsSDR 032108N318CSBulb · blownUPON LOWERING THE LANDING GEAR THERE WAS NO RT MAIN GEAR DOWN AND LOCKED GREEN LIGHT. LANDING GEAR ROTARY TEST SELECTED AND RT MAIN GEAR GREEN LIGHT DID NOT TEST. GEAR BLOW DOWN WAS PERFORMED AND AIRCRAFT LANDED UNEVENTFULLY. ALL DOWN AND LOCKED (GREEN LIGHTS)Mar 21, 2008 · N318CS · Cessna 550 · Landing Gear Position and WarningSDR ZESA032008004Warning Light · false activationAFTER TAKE OFF, PILOT NOTICE CABIN DOOR WARNING LIGHT, PILOT RETURNED TO AIRPORT, LANDED UNEVENTFULLY. PILOT RESET DOOR HANDLE AND LIGHT WENT OUT, PILOT VERIFIED THAT ALL LOCK FLAGS WERE VISIBLE WITH THE DOOR HANDLE SECURE PIN ENGAGED. NO FURTHER OCCURRENCE OFMar 20, 2008 · N824CB · Cessna 550 · Door Warning SystemSDR CSI0108Wire · backed outDURING FLIGHT, APPROACHING KSUS (SPIRIT OF ST LOUIS AIRPORT, MO), THE CREW OBSERVED THAT THE BRAKE PRESSURE LOW AND ANTI-SKID INOP, ANNUNCIATOR LIGHTS WERE ILLUMINATED. CHECKLIST PROCEDURES WERE FOLLOWED AND ATC WAS ADVISED. ATC HAD EMERGENCY EQUIPMENT RESPOMar 19, 2008 · N100WT · Cessna 550 · Landing Gear System WiringSDR B3OR20080079Actuator · out of positionAIRCREW REPORTED LANDING GEAR WARNING HORN SOUNDED AND GEAR-IN-TRANSIT INDICATOR ILLUMINATED AS AIRCRAFT WAS BEING TOWED OVER A BUMP (HANGAR THRESHOLD). SCHEDULED FLIGHT WAS CANCELLED. MAINTENANCE CREW WAS ABLE TO DUPLICATE EVENT BY SLIGHT ACCELERATION OF TOMar 18, 2008 · N26621 · Cessna 550 · Landing Gear ActuatorSDR 031308N338CS1Actuator · intermittentON APPROACH, CREW REPORTED RT MAIN GEAR DOWN INDICATOR LIGHT FAILED TO ILLUMINATE. CREW FOLLOWED CHECKLIST AND WAS UNABLE TO RESOLVE PROBLEM. CREW ELECTED TO DIVERT. APPROACH WAS ABORTED; ON APPROACH INTO CREW BLEW GEAR DOWN AND DECLARED AN EMERGENCY. PRIOR TOMar 13, 2008 · N338CS · Cessna 550 · Landing Gear ActuatorSDR FAA031008001Wire · arcedPILOT REPORTED CB LABELED LT CB PANEL OPENED IN FLIGHT, PILOT BLEW THE GEAR DOWN AND INITIATED A FLYBY OF THE TOWER TO ASSURE THE GEAR WAS DOWN. AC LANDED WITHOUT FURTHER INCIDENT. MAINT INVESTIGATION REVEALED THAT THE CROSSOVER POWER WIRE FROM THE CO-PILOTS Mar 10, 2008 · N43SA · Cessna 550 · Electrical Power System WiringSDR ZESA2008002Strut · defectivePILOT NOTICED AFTER LANDING GEAR WAS SELECTED UP, GEAR WARNING LIGHT AND HYDRAULIC ON LIGHT WERE ON. SELECTED GEAR DOWN, HAD THREE GREEN DOWN AND LOCKED INDICATION. WENT BACK TO ORIGINAL AIRPORT AND LANDED UNEVENTFULLY. JACKED AIRCRAFT SWUNG GEAR AND FOUND Feb 28, 2008 · N824CB · Cessna 550 · Main Landing Gear Strut/Axle/TruckSDR CA080305013Engine · flamed out(CAN) WHILE DEICING THE AC AND PERFORMING SYSTEMS CHECKS, THE ENGINE FLAMED OUT WHEN BROUGHT TO IDLE POWER. THE ENGINE FLAMED OUT (2) ADDITIONAL TIMES UNDER SIMILAR CIRCUMSTANCES DURING TROUBLESHOOTING. ATTENTION IS FOCUSING ON THE FUEL CONTROL AND AIRFRAME RIFeb 19, 2008 · Cessna 550 · Engine (Turbine/Turboprop)SDR 021708N339CS1Bulb · inoperativeON APPROACH, THE RT MAIN GEAR INDICATOR LIGHT WOULD NOT ILLUMINATE. CREW FOLLOWED AFM CHECKLIST PROCEDURE. THE LANDING GEAR EMERGENCY BLOW DOWN BOTTLE WAS USED. AC DIVERTED, LANDING WAS UNEVENTFUL, EMERGENCY VEHICLES WERE STANDING BY. MAINT TROUBLESHOT THE DIFeb 17, 2008 · N339CS · Cessna 550 · Landing Gear Position and WarningSDR 021408N329CS1Trim Tab · lack of lubeDURING DESCENT FROM FL36, AUTO PILOT MIS TRIM LIGHT ILLUMINATED. ELEVATOR TRIM WOULD NOT TRIM PAST 1 INCH FROM FULL DOWN POSITION. THE AC DIVERTED AND AN EMERGENCY WAS DECLARED. AC LANDING WAS UNEVENTFUL. MAINT LUBRICATED THE ELEVATOR TRIM TABS AND PERFORMED AFeb 14, 2008 · N329CS · Cessna 550 · Elevator Tab Control SystemSDR 021408458FDownlock Switch · malfunctionedDURING THE APPROACH INTO PALWAUKEE (PWK), THE GEAR HANDLE WAS SELECTED TO THE DOWN POSITION TO EXTEND THE GEAR. AFTER THE GEAR EXTENDED IT WAS NOTED THAT THE LEFT MAIN GEAR GREEN DOWN AND LOCK LIGHT WAS NOT ILLUMINATED. THE GEAR WAS CYCLED UP AND DOWN TWICE,Feb 14, 2008 · N458F · Cessna 550 · Landing Gear Position and WarningSDR 2008FA0000106Bracket · corrodedLT GENERATOR VOLTAGE REGULATOR MOUNT BRACKET FOUND TO HAVE CORROSION AT MOUNT SURFACE. ELECTRICAL GROUND PATH AFFECTED. CORROSION REMOVED ALLOWING GOOD GROUND AND ABLE TO ADJUST VOLTAGE REGULATOR, TO SPEC.Feb 11, 2008 · N554MB · Cessna 550 · Fuselage Main, Attach FittingsSDR CA080211002Roller · out of adjust(CAN) CAMPAIGN NOTICE 851-27-50-043, FLAP CTR AFT BEARING INSTALLATION, COMPLIED WITH. NO FAULTS FOUND ON LT FLAP INSTALLATION. RT FLAP AFT CENTER ROLLER BEARING FOUND TIGHT, BEARING WOULD NOT TURN UNLESS FLAP WAS HELD WITH PRESSURE APPLIED. NO DAMAGE TO BEARIFeb 5, 2008 · Cessna 550 · Trailing Edge Flap Control SystemSDR CA080212003Support · worn(CAN) DURING A CAMPAIGN NOTICE OF THE RT FLAP CENTER BRG INSTALLATION, BOTH OF THE AFT FLAP BEARINGS WERE FOUND LOOSE AND WORN DUE TO THE LOCATING PIN ON THE BEARINGS NOT INSTALLED INTO MATING HOLES OF FLAP RIB EXTENSIONS. FLAP ROLLER PN KJS 112603 AND BOTH CFeb 1, 2008 · Cessna 550 · Trailing Edge FlapsSDR CA080206013Oil Cap · loose(CAN) DURING CLIMB AT FL150, THE LOW OIL PRESSURE WARNING ANNUNCIATED AND PRESSURE WAS OBSERVED TO DROP TO 35 PSIG. THE ENGINE WAS SHUTDOWN BY THE CREW WHEN THE PRESSURE REDUCED TO 20 PSIG AND THE AC RETURNED TO BASE. POST FLIGHT INVESTIGATION INDICATES THAT Jan 29, 2008 · Cessna 550 · Turbine Engine Oil SystemSDR CA080206012Engine · making metal(CAN) THE CREW NOTED A LOW OIL PRESSURE WARNING DURING CRUISE AND ELECTED TO SHUTDOWN THE ENGINE. POST FLIGHT INSPECTION REVEALED OIL RESIDUE IN THE TAIL PIPE AND METAL PARTICLES ON THE OIL FILTER. THE ENGINE WAS REMOVED FOR INVESTIGATION. MFG WILL CONTINUE TJan 24, 2008 · Cessna 550 · Engine (Turbine/Turboprop)SDR FAA012408001Cable · wornDURING A PHASE 5 IT WAS FOUND THAT THE AILERON CABLES WERE LOCATED IN THE WRONG GROVES OF THE FUSELAGE SECTOR, CAUSING GROOVES TO BE WORN INTO THE SECTOR BY THE CABLES. THERE IS A SPECIAL "NOTE" IN THE MAINTENANCE MANUAL 27-11-08 SECTION 7 FOR THE AILERON LEFTJan 24, 2008 · N338B · Cessna 550 · Aileron Control SystemSDR CA080124015Bearing · missing(CAN) ACFT ARRIVED AT OUR FACILITY FOR PAINT. UPON DISASSEMBLY MX NOTED THE BOLT SECURING THE RT FLAP CENTRE AFT ROLLER WAS LOOSE. FURTHER INVESTIGATION AND REMOVAL DETERMINED THAT THE BEARING AND SHIM REQUIRED TO BE UNDER THE HEAD OF BOLT WAS MISSING AND PRJan 23, 2008 · Cessna 550 · Trailing Edge FlapsSDR 010808N341CS1Frame · crackedFUSELAGE FRAME CRACKED AT FS 263.4 LBL 15.35 FRAME PN 6511131-2 MFG AT ICT IN PROCESS OF REPAIR DEFINITION S-550-ATA53/16RD.Jan 8, 2008 · N341CS · Cessna 550 · Fuselage Main, FrameSDR CA080116014Fuel Sys · low pressure(CAN) DURING PRE TAKEOFF ACTIVITES, THE LOW FUEL PRESSURE WARNING ILLUMINATED. AS THE AC TAXIED BACK TO THE RAMP, THE ENGINE SHUT ITSELF DOWN. ENGINE RESTARTS WERE UNSUCCESSFUL. THE FUEL FLOW DIVIDER WAS REPLACED AND THE AC RETURNED TO SERVICE. (TC NR 2008011Jan 6, 2008 · Cessna 550 · Engine Fuel DistributionSDR CA080108008Valve Seat · damaged(CAN) WHEN PRESSURE IS APPLIED TO THE UPLOCK ACTUATOR THE ACTUATOR MUST TRAVEL FULL STROKE BEFORE ALLOWING FLUID TO THE GEAR ACTUATOR. IN THIS ACTUATOR THE DAMAGED SEAT ALLOWED FLUID TO THE GEAR ACTUATOR BEFORE THE UPLOCK HAD RELEASED THE GEAR. WE HAVE HAD A Dec 17, 2007 · Cessna 550 · Landing Gear Retraction/Extension SystemSDR CA071218004Wheel · damaged(CAN) ON PILOTS WALK AROUND THEY FOUND METAL AROUND NOSE WHEEL TIRE. AIRCRAFT WAS TOWED INTO A HEATED HANGER AND PILOT PHONED MAINTENANCE . ENGINEER JACKED NOSE WHEEL AND INSPECTED NOSE WHEEL SPIN-UP KIT AND FOUND LT TURBINE AND LT SPIN-UP COVER WERE DAMAGED. Dec 17, 2007 · Cessna 550 · Wheel/Ski/FloatSDR CA071212012Screw · missing(CAN) SL 550-27-14 FOUND 2 SCREWS, P/N MS350206-228, MISSING FROM PILOTS LT RUDDER SUPPORT BRACKET AND 2 LOOSE SCREWS P/N MS 350206-228 ON THE CO-PILOTS RT RUDDER SUPPORT BRACKET.CARRY OUT ACCOMPLISHMENT INSTRUCTIONS PARAGRAPH 1THRU 4. (TC NR 20071212012)Dec 11, 2007 · Cessna 550 · Rudder Control SystemSDR CA071206004Bulb · burned out(CAN) PILOTS REPORT, ON FINAL TO LANDING RUNWAY, SELECTED THE GEAR DOWN HOWEVER THE RT MAIN GEAR GREEN LIGHT FAILED TO ILLUMINATE. THE RED (GEAR UNLOCKED) LIGHT WAS EXTINGUISHED. ADVISED TOWER AND CONDUCTED A MISSED APPROACH WITH REQUEST FOR VECTORS TO REMAIN Dec 5, 2007 · Cessna 550 · Landing Gear Position and WarningSDR 112607N458FDownlock Switch · intermittentTHE GEAR HANDLE WAS MOVED TO THE EXTEND SELECTION DURING APPROACH TO GRR, THE GREEN INDICATOR FOR THE NLG DID NOT ILLUM. PERFORMED THE EMERGENCY PROCEDURES TO ENSURE THE NLG WAS DOWN AND LOCKED. THE NLG INDICATOR FAILED TO ILLUM. FLY-BY OF THE TOWER, TO VISNov 26, 2007 · N458F · Cessna 550 · Landing Gear Position and WarningSDR 112207N336CS1Actuator · failedLT MLG DOWN INDICATION FAILED TO ILLUMINATE WHEN GEAR WAS EXTENDED. PERFORMED AFM ABNORMAL PROCEDURES. DECLARED EMERGENCY, BLEW GEAR DOWN AFTER A SHORT TIME, GREEN DOWN INDICATION DID ILLUMINATE AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE STAFF REPLACEDNov 22, 2007 · N336CS · Cessna 550 · Landing Gear ActuatorSDR SFO57SFWheel · brokenON LANDING, ENCOUNTERED SEVERE CROSSWIND GUSTS CAUSING ACFT TO YAW ON TOUCHDOWN. AFTER A SUCCESSFUL LANDING, NOTED A SEVERE SWAYING OF THE NLG & VIBRATION FELT IN RUDDER PEDALS. ACFT STOPPED & DISCOVERED THE NLG TIRE BLOWN & RIMS BROKEN OFF. AT THE HANGER NNov 16, 2007 · N57SF · Cessna 550 · Wheel/Ski/FloatSDR CA071109002Lever · inoperative(CAN) PILOT ABORTED TAKEOFF. UPON INSPECTION FOUND ELEVATOR TRIM TAB WAS ALMOST ON FULL NOSE DOWN TRIM POSITION. TRIM INDICATION IN THE COCKPIT WAS AT TAKEOFF. FOUND THAT THE INDICATOR LEVER HAD JUMPED ON THE CONTROL WHEEL TO GIVE THE WRONG INDICATION. TRIM CONov 7, 2007 · Cessna 550 · Elevator Tab Control SystemSDR CA071107003Lever · worn(CAN) PILOT ABORTED TAKEOFF DUE TO NO RESPONSE TO CONTROL COLUMN INPUT. UPON INSPECTION FOUND ELEVATOR TRIM TAB WAS ALMOST ON FULL NOSE DOWN POSITION AND TRIM INDICATION IN COCKPIT WAS AT TAKEOFF. FOUND INDICATOR LEVER AND CONTROL WHEEL WORN, INDICATOR LEVER HNov 7, 2007 · Cessna 550 · Elevator Tab Control SystemSDR 110607N336CS1Bypass Valve · faultyWHEN LANDING GEAR WAS EXTENDED, NO LT GEAR DOWN INDICATION OBSERVED. CREW FOLLOWED EMERGENCY PROCEDURES AND BLEW GEAR DOWN AND DECLARED EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT. PRIOR TO LANDING, THE LT MAIN GEAR GREEN DOWN INDICATION ILLUMINATED. AIRCRAFTNov 6, 2007 · N336CS · Cessna 550 · Landing Gear Retraction/Extension SystemSDR 102207N338CS2Frame · crackedFUSELAGE FRAME CRACKED AT FS 275.6, LBL 15.35 AND RBL 15.35. FRAME P/N 6511136-2. NOTE: FIVE OTHER AIRCRAFT IN FLEET CHECKED AND FOR HAD CRACKS AT THE SAME LOCATION. THIS SDR IS A REVISION TO SDR 102207N338CS.Oct 22, 2007 · N338CS · Cessna 550 · Fuselage Main, FrameSDR 102207N338CS1Frame · crackedFUSELAGE FRAME CRACKED AT FS 263.4 -- LBL 15.35 TO RBL 15.35. FRAME P/N 6511131-2. NOTE: FIVE OTHER AIRCRAFT IN FLEET CHECKED AND FOUR HAD CRACKS AT THE SAME LOCATION. THIS SDR IS A REVISION TO SDR 102207N338CSOct 22, 2007 · N338CS · Cessna 550 · Fuselage Main, FrameSDR CA071101001Squat Switch · loose(CAN) ON FINAL APPROACH APPROXIMATELY 3 MILES FROM TOUCH DOWN, THE LT THRUST REVERSER (T/R) ARM AND UNLOCK LIGHTS ILLUMINATED BRIEFLY. AT APPROXIMATELY 1.5 FROM TOUCH DOWN THE LT T/R ARM, UNLOCK AND DEPLOY LIGHTS ILLUMINATED AND THE LT POWER LEVER AUTOMATICALLOct 19, 2007 · Cessna 550 · Landing Gear Position and WarningSDR 100407N342CSDownlock Switch · failedON APPROACH, AFTER LANDING GEAR SELECTION NOSE LANDING GEAR DOWNLOCK GREEN LIGHT DID NOT ILLUMINATED. AIRCRAFT LANDED UNEVENTFULLY. NOSE LANDING GEAR ACTUATOR REPLACED AND AIRCRAFT RETURNED TO SERVICE.Oct 4, 2007 · N342 · Cessna 550 · Landing Gear Position and WarningSDR 092607N324CS1Bulb · inoperativeUPON APPROACH, CREW NOTICED NO RT GEAR DOWN INDICATION AFTER GEAR EXTENSION. CREW FOLLOWED AFM ABNORMAL PROCEDURES. NO RT GEAR DOWN IN TEST. CREW ELECTED TO DECLARE EMERGENCY. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE PERSONNEL FOUND BULB OUT FOR RT GEARSep 26, 2007 · N324CS · Cessna 550 · Landing Gear Position and WarningSDR CA070910004Buckle · disconnected(CAN) WHILE COMPLYING WITH COMPANY CAMPAIGN NOTICE 010-25-10-011 CREW SEAT BELT BUCKLE INSPECTION, (REFER TO FAA SAIB NM-06-29)INTERFERENCE BETWEEN THE COCKPIT SEATBELT BUCKLES AND THE CONTROL COLUMN WOULD UNLATCH THE SEATBELT BUCKLE WHEN THE YOKE WAS MOVED THSep 9, 2007 · Cessna 550 · Flight Compartment EquipmentSDR CA070911009Skin · corroded(CAN) DE-ICE BOOT REPLACEMENT AT MFG. AFTER REMOVAL OF DE-ICE BOOT NOTED AREA OF FUEL STAINING, CORROSION NOTED. DISCONTINUED BOOT REPLACEMENT, OBTAINED FERRY PERMIT AND RELOCATED AIRCRAFT. FURTHER INVESTIGATION SHOWS: SEVERAL LOCATIONS OF CORROSION DAMAGE WEAug 30, 2007 · Cessna 550 · Wing, Plate/SkinSDR 081507N316CS1Accumulator · malfunctionedPOWER BRAKE VALVE REPLACED FOR MAKING UNUSUAL NOISES DURING BRAKING. ON TAXI OUT, COPILOT'S RT BRAKE PEDAL LOST BRAKING ACTION. AIRCRAFT RETURNED TO GATE, MAINTENACE TROUBLESHOOTING FOUND BRAKE ACCUMULATOR TO BE AT FAULT, REINSTALLED ORIGINAL POWER BRAKE VALVEAug 15, 2007 · N316CS · Cessna 550 · Landing Gear Brake SystemSDR CA071003018Engine · smoke(CAN) IN CRUISE SMOKE BECAME EVIDENT IN THE AIRCRAFT CABIN REQUIRING THE ENGINE AIR BLEED TO BE SELECTED OFF. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20071003018)Aug 13, 2007 · Cessna 550 · Engine (Turbine/Turboprop)SDR 2007FA0000617Actuator · wornAT THE PHASE 5 INSPECTION THE ELEVATOR FAILED THE FREE PLAY CHECK. A OVERHAULED UNIT P/N 5565450-98 S/N 0320-63 WAS INSTALLED AND COULD NOT GET THE UP AND DOWN LIMITS TO COME IN TO SPECS. ON CLOSER INSPECTION IT WAS FOUND THAT THE PRIMARY DRIVE GEAR HAS 16 TEEJul 18, 2007 · N26494 · Cessna 550 · Elevator Tab Control SystemSDR CA070618001Bearing · worn(CAN) THIS SDR IS BEING SUBMITTED TO SATISFY THE REQUIREMENT OF AIRCRAFT SERVICES DIRECTORATE CAMPAIGN NOTICE CN-1 851-32-40-040R1 THE INTERNAL TEFLON MATERIAL OF THE BEARING HAD DETERIORATED CAUSING THE BEARING TO BE DIFFICULT TO ROTATE. (TC NR 20070618001)Jun 17, 2007 · Cessna 550 · Main Landing GearSDR ZES2007F00002Hydromech Unit · inoperativeLT ENGINE ON AIRCRAFT, WOULD NOT REDUCE POWER TO IDLE, GROUND RAN AIRCRAFT TO CONFIRM POWER WOULD NOT REDUCE BELOW 75 PERCENT N2. REMOVED AND REPLACED HFO (HYDROMECHANICAL FUEL CONTROL). GROUND RUN AND PERFORMED FUNCTIONAL CHECK FLIGHT AND RETURNED TO SERVICJun 15, 2007 · N824CB · Cessna 550 · Fuel Control/Reciprocating EnginesSDR 061307N300CS1Switch · failedBRAKES FAILED ON LANDING, WITH LOW PRESSURE LIGHT ILLUMINATED AS WELL AS THE ANTI SKID LIGHT ILLUMINATED. EMERGENCY BRAKE HANDLE USED TO STOP AIRCRAFT.Jun 9, 2007 · N300CS · Cessna 550 · Landing Gear Brake SystemSDR CA070607008Uplock Roller · worn(CAN) CAMPAIGN NOTICE 851-32-40-040 AND 851-32-40-040R1 CARRIED OUT. ACTION WAS REQUIRED TO THE RT MAIN GEAR BEARING P/N MS21240-10C40. THE INSIDE BEARING MATERIAL WHEN INSPECTED WAS FOUND TO HAVE PIECES MISSING AND FURTHER INSPECTION REVEALED THE REMAINDER OFJun 7, 2007 · Cessna 550 · Landing Gear Retraction/Extension SystemSDR 2007FA0000538Floor Support · crackedCABIN FLOOR SUPPORT WEB CRACKED AND BROKEN, FUSELAGE STATION 151. FOUND CRACK DURING PHASE INSPECTION. UNABLE TO FIND PN IN MFG PARTS CATALOG. (K)Jun 4, 2007 · N905CW · Cessna 550 · Fuselage Miscellaneous StructureSDR 2007FA0000494Cable · frayedWE HAVE FOUND THE ELEVATOR CABLE AT THIS SERVO P/N 4006719-904 SHOWING EXCESSIVE WEAR ON AIRCRAFT UNDERGOING PHASE 1-4 AND ALSO PHASE 5 INSPECTIONS. THE CABLE WAS FOUND WHERE IT PASSES THROUGH AT FS. 428.50 AND IS DIFFICULT TO SEE. THIS CABLE HAD APROX. 3 STRAJun 4, 2007 · N4614N · Cessna 550 · Autopilot Trim Servo
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