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"

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 FRK2005F00000Clamp · failedCLAMP SECURING FIRE DETECTION SENSOR TO SUPPORT STRUCTURE FAILED ALLOWING SENSOR TO CONTACT ENGINE COWLING. THIS CONTACT WITH COWLING CHAFFED INTO SENSOR CAUSING A FALSE ENGINE FIRE WARNING. (K)Nov 8, 2005 · N245CC · Cessna 550 · Fire DetectionSDR CA051011008Support Bracket · crackedPILOT REPORTED THAT WHEN BRAKES WERE APPLIED FROM CAPTS POSITION, THE CO-PILOTS INSTRUMENTS LIGHTS WOULD GO OUT. MAINTENANCE WAS ABLE TO DUPLICATE THE SNAG. INVESTIGATION REVEALED CAPTS RUDDER SUPPORT BRACKET CRACKED AND BROKEN AT TOP AND BOTTOM ATTACH CHANNOct 7, 2005 · Cessna 550 · Rudder Control SystemSDR CA051011010Longeron · crackedDURING SCHEDULED INSPECTION, MAINTENANCE FOUND A CRACK ON THE LT THRUST REVERSER LT INNER UPPER LONGERON TAB. THE CRACK STARTED IN FASTENER HOLE AND PROPAGATED TO THE EDGE OF THE TAB. THE CRACK WAS REPAIRED BY FABRICATING AND INSTALLING REPAIR DOUBLER IAW NOOct 6, 2005 · Cessna 550 · Engine Thrust ReverserSDR 090605N342CS1Wire · brokenLANDING GEAR WOULD NOT INDICATE DOWN AND LOCKED. PERFORMED IN FLIGHT DIVERSION TO SWF, FACTORY SERVICE CENTER. RECYCLED GEAR WITH NO CHANGE SO COMPLIED WITH CHECKLIST PROCEDURE TO EMERGENCY EXTEND GEAR. STILL NO DOWN INDICATION SO EMERGENCY WAS DECLARED ANDSep 6, 2005 · N342CS · Cessna 550 · Landing Gear System WiringSDR CA050831008Hmu · damaged(CAN) DURING A TRAINING FLIGHT, ENGINE POWER WAS COMMANDED TO IDLE RESULTING IN A LOW FUEL PRESSURE WARNING AND AN UNCOMMANDED ENGINE SHUT DOWN. AN IN-FLIGHT RE-LIGHT WAS SUCCESSFULLY ACCOMPLISHED AND THE REMAINDER OF THE FLIGHT CARRIED OUT WITHOUT FURTHER INAug 30, 2005 · Cessna 550 · Fuel Control/Turbine EnginesSDR 2005FA0001212Attach Bracket · crackedUPPER CHAIR BASE ASSEMBLY CRACKED AT CHAIR BACK ATTACH POINTS. ALSO, PREVIOUS INAPPROPRIATE REPAIR. CHAIR WAS REPAIRED IAW STC SEAT REPAIR. (K)Aug 16, 2005 · N120Q · Cessna 550 · Flight Compartment EquipmentSDR CA050812001Stop · missing(CAN) COMPANY CAMPAIGN NOTICE 851-25-26-029 WAS CREATED TO INSPECT FOR PROPPER INSTALLATION OF PASSENGER SEAT STOPS. DURING INSPECTION IT WAS FOUND THAT 4 STOPS WERE MISSING ON THE LT BACK TO BACK SEAT INSTALLATION. PARTS ARE ORDERED AND WILL BE INSTALLED PRIAug 12, 2005 · Cessna 550 · Flight Compartment EquipmentSDR CA050812002Stop · missing(CAN) COMPANY CAMPAIGN NOTICE 851-25-26-029 WAS CREATED TO INSPECT FOR PROPPER INSTALLATION OF PASSENGER SEAT STOPS. DURING INSPECTION IT WAS FOUND THAT 4 STOPS WERE MISSING ON THE LT BACK TO BACK SEAT INSTALLATION. PARTS ARE ORDERED AND WILL BE INSTALLED PRIOAug 11, 2005 · Cessna 550 · Flight Compartment EquipmentSDR 2005FA0001354Drive Assy · stiffTHE PILOT REPORTED THAT THE CONTROLS WERE STIFF IN THE ROLL AXIS. THE AUTOPILOT WAS TURNED OFF AND THE CB WAS CYCLED WITH NO CHANGE IN THE CONDITION. AFTER LANDING, WITHOUT INCIDENT, TECHNICIANS ARRIVED AND TROUBLESHOOT THE A/P SYSTEM. THEY DISCOVERED THE AJul 26, 2005 · N5408G · Cessna 550 · Autopilot SystemSDR 2005FA0001129Drive Assy · inoperativeTHE PILOT REPORTED THAT THE CONTROLS WHERE STIFF IN THE ROLL AXIS. THE AUTOPILOT WAS TURNED OFF AND THE C/B WAS CYCLED WITH NO CHANGE IN THE CONDITION. AFTER LANDING WITHOUT INCIDENT, TECHS ARRIVED AND TROUBLESHOT THE A/P SYSTEM. THEY DISCOVERED THE AILERONJul 26, 2005 · N5408G · Cessna 550 · Auto Flight SystemSDR 2005FA0001113Seat · crackedUPPER CHAIR BASE ASSEMBLY CRACKED AT CHAIR BACK ATTACH POINTS. STRESS ON CHAIR BACK AND METAL FATIGUE PROBABLE CAUSE. CHAIR WAS REPAIRED IAW STC ST01042WI STRUCTURAL SEAT REPAIR. (K)Jul 26, 2005 · N123VP · Cessna 550 · Flight Compartment EquipmentSDR DYCR200532202Brake Assy · damagedBRAKE IS PART OF MTOW STC BY NEWFLIGHT. BRAKE AND WHEEL ASSEMBLY FIT FINE, HOWEVER AFTER SEVERAL FLIGHT HOURS THE BRAKE LUGS ON THE INNER WHEEL HALF RUB THE PIN IN THE LOWER TORQUE LINK DAMAGING THE WHEEL HALF AND THE TORQUE LINK. AXLE NUT IS TORQUED AT INITIAJul 26, 2005 · N550KA · Cessna 550 · Landing Gear Brake SystemSDR B3OR20050614Pump · seizedDURING APPROACH, WHILE LOWERING GEAR, PILOT IN COMMAND NOTICED "ANTI SKID INOP" LIGHT ILLUMINATED. PILOTS FOLLOWED EMERGENCY CHECKLIST PROCEDURES & MADE AN UNEVENTFUL LANDING AT HOME FIED. HOWEVER, EMERGENCY BRAKE SYS HAD TO BE USED TO BRING ACFT TO A STOP. MXJun 13, 2005 · N26496 · Cessna 550 · Landing Gear Brake SystemSDR 2005FA0000870Attach Bracket · crackedUPPER CHAIR BASE ASSEMBLY CRACKED AT CHAIR BACK ATTACH POINTS. ALSO, PREVIOUS INAPPROPRIATE REPAIR. CHAIR WAS REPAIRED IAW STC ST01042WI STRUCTURAL SEAT REPAIR. (K)Jun 2, 2005 · N157DW · Cessna 550 · Flight Compartment EquipmentSDR 052305N304CS1Outflow Valve · malfunctionedAT FL 350 EXPERIANCED LOUD BANG AND RAPID LOSS OF PRESSURIZATION. DECLARED EMERGENCY, DESCENDED RAPIDLY AND DEPLOYED PASSENGER OXYGEN MASKS (2 PAX ON BOARD). DIVERTED TO DALLAS LOVE FIELD AND LANDED ASAP. AIRCRAFT INSPECTED AND REPAIRED AT FACTORY AUTHORIZEMay 23, 2005 · N304CS · Cessna 550 · Pressure Regulator/Outflow ValveSDR 5330Bracket · crackedAVIONICS SHELF BRACKET CRACKED, LOCATED IN NOSE AVIONICS COMPARTMENT ON RT SIDE OF NOSE WHEEL WELL, FRAME STA 50. REPLACED BROKEN ANGLE BRACKET WITH NEW BRACKET FROM THE MFG. METHOD OF PREVENTION IS UNKNOWN.May 9, 2005 · N52RF · Cessna 550 · Fuselage Main, Attach FittingsSDR CA050506013Threshold · cracked(CAN) INSP ON AIRFRAME, THRESHOLD INSP REVEALED DAMAGE TO PAINT, FILLER WHERE MN CABIN DOOR SEAL INFLATES AGAINST. ONCE STAIR BRACKETS WERE REMOVED, DEFECT NOTED AS 1 INCH CRACK FROM MAIN FASTENER HOLE ON AFT STAIR BRACKET HOLE. DEFECT WAS CAUSED BY IMPROPER May 4, 2005 · Cessna 550 · Emergency ExitsSDR 2005FA0000733Static Line · chafedALTERNATE STATIC LINE CHAFED THROUGH IN CO-PILOTS SIDEWALL IN COCKPIT. REPLACED LINE WITH NEW BUT THE LOCATION IS VERY DIFFICULT TO PREVENT CONTINUED CHAFING. RECOMMEND MFG LOOK AT THIS AREA AND POSSIBLE REROUTING.May 3, 2005 · N669B · Cessna 550 · Pitot/Static SystemSDR 2005FA0000732Static Line · chafedALTERNATE STATIC LINE CHAFED THROUGH IN CO-PILOTS SIDEWALL IN COCKPIT. REPLACED LINE WITH NEW BUT THE LOCATION IS VERY DIFFICULT TO PREVENT CONTINUED CHAFING. RECCOMEND MFG LOOK AT THIS AREA AND POSSIBLE REROUTING.May 3, 2005 · N669B · Cessna 550 · Pitot/Static SystemSDR 2005FA0000731Static Line · chafedALTERNATE STATIC LINE CHAFED THROUGH IN CO-PILOTS SIDEWALL IN COCKPIT. REPLACED LINE WITH NEW BUT THE LOCATION IS VERY DIFFICULT TO PREVENT CONTINUED CHAFING. RECOMMEND MFG LOOK AT THIS AREA AND POSSIBLE REROUTING.May 3, 2005 · N669B · Cessna 550 · Pitot/Static SystemSDR 2005FA0000730Static Line · chafedALTERNATE STATIC LINE CHAFED THROUGH IN CO-PILOTS SIDEWALL IN COCKPIT. REPLACED LINE WITH NEW BUT THE LOCATION IS VERY DIFFICULT TO PREVENT CONTINUED CHAFING. RECOMMEND MFG LOOK AT THIS AREA AND POSSIBLE REROUTING.May 3, 2005 · N669B · Cessna 550 · Pitot/Static SystemSDR CA050527019Engine · malfunctionedDURING GROUND HANDLING OPERATIONS, THE ENGINE EXPERIENCED AN UNCOMMANDED ACCELERATION. THE ENGINE DID NOT RESPOND TO THROTTLE OR SHUTOFF LEVER INPUT. THE CREW SECURED THE ENGINE VIA AIRFRAME FIREWALLSHUT-OFF. PWC WILL INVESTIGATE THE EVENT AND ADVISE OF ROOMay 2, 2005 · Cessna 550 · Engine (Turbine/Turboprop)SDR CA050518018Chain · misinstalled(CAN) DURING MAJOR INSP, TRIM ACTUATOR WAS REMOVED AND REINSTALLED. WHEN ENGINEER MOUNTED TRIM CONTROL CABLE CHAIN ONTO ACTUATOR SPROCKET, INSTALLED OPPOSITE TO WAY IT WAS REMOVED. THIS CAUSED ELEV TRIM CONTROL SYS TO WORK BACKWARDS. MM DOES NOT FULLY DESCRIBEApr 30, 2005 · Cessna 550 · Elevator Tab Control SystemSDR CA050425003Lead · mislocated(CAN) PILOTS REPORTED THAT THE RT ENGINE TAKEOFF POWER WAS LOW. TECHNICIANS DISCOVERED THAT THE 5 O'CLOCK POSITION IGNITER LEAD WAS INTERFERING WITH THE FUEL FLOW DIVIDER LINKAGE. THE IGNITER LEAD WAS REPOSITIONED AND FUNCTION CHECK OF THE POWER LEVERS PERFOApr 19, 2005 · Cessna 550 · Ignition System WiringSDR CA050425006Switch · failedFOLLOWING TAKEOFF AND AFTER SELECTING GEAR UP, GEAR FAILED TO LOCK UP. CREW SELECTED GEAR DOWN AND RETURNED TO LAND WITHOUT INCIDENT. AIRCRAFT FERRIED WITH GEAR DOWN. MAINTENANCE DETERMINED NLG ACTUATOR HAD FAILED. A SERVICEABLE ACTUATOR WAS INSTALLED ANApr 6, 2005 · Cessna 550 · Landing Gear ActuatorSDR CA050425005Switch · failedDURING APPROACH, CREW SELECTED GEAR DOWN AND NOTED THAT NOSE GEAR DID NOT INDICATE DOWN AND LOCKED. CREW USED EMERGENCY LANDING GEAR EXTENSION SYSTEM AND FLEW BY TOWER FOR GEAR POSITION CONFIRMATION. GPWS SOUNDED A CONTINUOUS WARNING BELOW 1500 FEET UNTIL LApr 4, 2005 · Cessna 550 · Landing Gear ActuatorSDR CA050406004Duct · cracked(CAN) DURING OTHER MAINTENANCE ON AIRCRAFT, NOTICED RAM AIR DUCT IN REAR EQUIPMENT BAY CRACKED. UPON CLOSER INSPECTION OF RAM AIR DUCT, NOTICED SEVERE CHAFFING BETWEEN RAM AIR DUCT AND RT ENGINE BLEED AIR LINE JUST PRIOR TO BLEED AIR CHECK VALVE. RAM AIR DUCApr 4, 2005 · Cessna 550 · Engine Air Intake SystemSDR 03132005Exhaust Duct · damagedPILOTS REPORT THAT WHILE EN ROUTE FROM MERRILL FIELD TO ANCHORAGE INTL, HEARD AN UNUSUAL NOISE AND FEEL A LOW FREQUENCY VIBRATION. ALL SYSTEM AND ENGINE INDICATIONS WERE NORMAL. POST FLIGHT INSPECTION REVEILED DAMAGE ON THE NR 1 ENGINE TURBINE WHEEL AND REARMar 13, 2005 · N88NM · Cessna 550 · Engine Collector/Tailpipe/NozzleSDR CA050314003Line · worn(CAN) DURING THE ACCOMPLISHMENT OF MFG SB 550-28-14 WING FUEL BOOST PUMP WIRING IMPROVEMENT, LINE ASSEMBLY P/N 6526355-37 FOUND DAMAGED, WHICH THE ELECTRIC FUEL PUMP HARNESS CUT THROUGH THE WALL OF TUBING. NO DAMAGED FOUND ON ELECTRICAL HARNESS.Mar 7, 2005 · Cessna 550 · Aircraft Fuel Distribution SystemSDR CA050224010Engine · failed(CAN) THE ENGINE EXPERIENCED AN UNCOMMANDED SHUTDOWN IN DESCENT. MFG WILL INVESTIGATE THE INCIDENT AND WILL SUPPLEMENT THIS REPORT TO REFLECT ROOT CAUSE ONCE ESTABLISHED.Feb 19, 2005 · Cessna 550 · Engine (Turbine/Turboprop)SDR 021705N308CS1Switch · out of toleranceTHRUST REVERSER UNLOCK LIGHT ILLUMINATED AFTER TAKEOFF. PILOT PERFORMED EMERGENCY PROCEDURES CHECKLIST AND LANDED AIRCRAFT BACK AT DEPARTURE FIELD (TEB). MAINTENANCE PERFORMED OVERWEIGHT LANDING INSPECTION AND TROUBLESHOOT FAULT TO INDICATION PROBLEM. REPLAFeb 17, 2005 · N308CS · Cessna 550 · Engine Thrust ReverserSDR 2005FA0000194Seat Back · crackedUPPER CHAIR BASE ASSEMBLY CRACKED AT CHAIR BACK ATTACH POINTS. STRESS ON CHAIR BACK AND METAL FATIGUE PROBABLE CAUSE. ALSO, PREVIOUS INAPPROPRIATE REPAIR. CHAIR WAS REPORTED IAW STC ST01042WI, STRUCTURAL SEAT REPAIR. (CE05200503843) (K)Feb 11, 2005 · N1250V · Cessna 550 · Flight Compartment EquipmentSDR B30R20050405Motor · inoperativeAFTER LANDING DURING TAXI BACK TO THE RAMP, PILOT EXPERIENCED POWER BRAKE FAILURE. WAS ABLE TO CONTROL THE AIRCRAFT AND RETURN IT TO THE PARKING RAMP SAFELY. MECHANIC'S TROUBLESHOOTING REVEALED THAT THE POWER PACK PUMP MOTOR HAD FAILED. THE POWER PACK ASSEMFeb 4, 2005 · N26496 · Cessna 550 · Landing Gear Brake SystemSDR CA050202005Bearing · destroyed(CAN) WHILE IN CRUISE BACK TO BASE, CREW ENCOUNTERED AIRFRAME VIBRATION FROM THE AFT CABIN, FOLLOWED BY THE RT GENERATOR FAIL LIGHT 10 MINUTES LATER. CREW CONFIRMED LOSS OF RT GENERATOR, AND DECLARED AN EMERGENCY DUE TO THE INTENSITY OF VIBRATION. A/C LANDED Feb 1, 2005 · Cessna 550 · Starter-GeneratorSDR CA050121001Connector · burned(CAN) RT LND LIGHT WOULD NOT EXTING. (RELAY STUCK (ON)). RELAY WAS REPLACED, FAULT STILL PERSISTED, (SHORT) DISCOVERED TO X2. (COIL GROUND) TERM OF RELAY. BETWEEN RT GEAR WHEELWELL CNTR P/J 64 PIN W, RELAY TERM X2. WHEN P/J 62 WAS DISCONTD PIN SMALL (E) ANDJan 20, 2005 · Cessna 550 · Light System WiringSDR CA050126004Fcu · malfunctioned(CAN) THE ENGINE EXPERIENCED AN UNCOMMANDED INFLIGHT SHUTDOWN FOLLOWING POWER REDUCTION FOR DESCENT. A RELIGHT ATTEMPT WAS UNSUCCESSFUL. SUBSEQUENT INSPECTION REVEALED A MALFUNCTIONING FUEL CONTROL UNIT. MFG WILL INVESTIGATE THE INCIDENT AND WILL SUPPLIMENT Jan 17, 2005 · Cessna 550 · Fuel Control/Turbine EnginesSDR 2005FA0000478Actuator · wornINSTALLED NEWLY OVERHAULED NLG ACTUATOR AND FOUND TO HAVE EXCESSIVE IN LINE MOVEMENT OF TNE LOCKING MECHANISM. MOVEMENT IN EXCESS OF .1250, MAX ALLOWED .035. (K)Jan 10, 2005 · N228CC · Cessna 550 · Landing Gear ActuatorSDR CA050117002Switch · failed(CAN) WHILE CARRYING OUT NIGHT LANDINGS ON A LOCAL TRAINING FLIGHT, THE LT MAIN GEAR DOWNLOCK INDICATION FAILED TO ILLUMINATE ON THE NINTH LANDING APPROACH. THE CREW CARRIED OUT AN EMERGENCY EXTENSION PROCEDURE AND LANDED SAFELY. MAINTENANCE CREW SERVICED THE Jan 6, 2005 · Cessna 550 · Landing Gear ActuatorSDR B3OR20050205Trim Motor · jammedAIRCRAFT WAS AOG FOR ELEVATOR ELECTRIC TRIM ACTUATOR. WHEN PART WAS RECIEVED FROM VENDOR IT WAS DISCOVERED THAT THE AFT TRIM CABLE WAS ROUTED BETWEEN THE CABLE DRUM AND THE CLUTCH ASSEMBLY JAMMING THE CLUTCH ASSEMBLY. THE CABLE DRUM CLUTCH COULD NOT DISENGAGE Jan 4, 2005 · N26496 · Cessna 550 · Elevator Tab Control SystemSDR B3OR20050105Trim Motor · jammedAIRCRAFT WAS AOG FOR ELEVATOR ELECTRIC TRIM ACTUATOR. WHEN PART WAS RECIEVED FROM VENDOR IT WAS DISCOVERED THAT THE AFT TRIM CABLE WAS ROUTED BETWEEN THE CABLE DRUM AND THE CLUTCH ASSEMBLY JAMMING THE CLUTCH ASSEMBLY. THE CABLE DRUM CLUTCH COULD NOT DISENGAGE Jan 4, 2005 · N26496 · Cessna 550 · Elevator Tab Control SystemSDR B30R20050105Actuator · malfunctionedDURING PREFLIGHT OF AIRCRAFT, PILOT HEARD A NOISE IN WHILE OPERATING ELEVATOR ELECTRIC TRIM. TROUBLESHOOTING REVEALED THAT THE TRIM CABLES IN THE ELEVATOR ELECTRIC TRIM ACTUATOR HAD CROSSED. A REPLACEMENT ELECTRIC TRIM ACTUATOR WAS ORDERED. UPON RECEIPT OFJan 3, 2005 · N26496 · Cessna 550 · Elevator Tab Control SystemSDR 122304N338CS1Sensor · contaminatedDURING APPROACH GEAR WAS SELECTED DOWN AND THERE WAS NO DOWN AND LOCKED INDICATION FOR RT MAIN GEAR. CREW DECLARED AN EMERGENCY AND BLEW THE GEAR DOWN AS A SAFETY PRECAUTION. LANDING WAS NORMAL BUT THERE NEVER WAS A GREEN INDICATION FOR THE RT GEAR. SUSPECTDec 22, 2004 · N338CS · Cessna 550 · Landing Gear Position and WarningSDR 2005R0037Brake Disc · crackedBRAKE ASSEMBLY P/N: 2-1528-6, S/N'S: 0110 AND 1390. BOTH OF THESE BRAKES ARE IN COMPLIANCE WITH MFG SB 2-1528-32-2, REV 5, DATED 3 APR, 2003. BOTH BRAKES WERE UNDERGOING VISUAL INSPECTION AT 202 LANDINGS AND 194.7 HRS SINCE OVERHAUL. BOTH BRAKES HAD STATORSDec 16, 2004 · N2663Y · Cessna 550 · BrakeSDR CA041209013Engine · malfunctioned(CAN) THE ENGINE EXPERIENCED AN UNCOMMANDED ACCELERATION IN FLIGHT AND WAS SHUTDOWN BY THE PILOT DUE TO AN ASSOCIATED ITT INCREASE TOWARDS RED-LINE. AN INFLT RELIGHT CARRIED OUT AND THE INCIDENT REOCCURRED. THE ENGINE WAS AGAIN SHUT DOWN.A SECOND RELIGHT WAS CDec 6, 2004 · Cessna 550 · Engine (Turbine/Turboprop)SDR CA041130001Coupler · disconnected(CAN) COUPLING DISCONNECTED WHEN AIRCRAFT WAS AT FLIGHT LEVEL AND AIRCRAFT AT A OPERATING CABIN PRESSURE ALTITUDE. AIRCRAFT CABIN LOST PRESSURIZATION.Nov 28, 2004 · Cessna 550 · Cabin Pressure Control SystemSDR 2005FA0000477Actuator · wornRECEIVED SECOND NLG TO REPLACE THE FIRST ONE SENT TO US OUT OF LIMITS AND FOUND THE SAME PROBLEM. FOUND TO HAVE EXCESSIVE IN LINE MOVEMENT OF THE LOCKING MECHANISM. MOVEMENT IN EXCESS OF .1250 INCH, MAX ALLOWED .035. (K)Nov 22, 2004 · N228CC · Cessna 550 · Landing Gear ActuatorSDR 112204N336CS1Landing Gear · malfunctionedUNSAFE NOSE GEAR INDICATION, GEAR MANUALLY DROPPED. CAUSE TO BE DETERMINED AT SERVICE CENTER.Nov 22, 2004 · N336CS · Cessna 550 · Nose/Tail Landing GearSDR 111904N336CS1Pin · backed outUNSAFE GEAR INDICATION ON APPROACH, GEAR WAS MANUALLY LOCKED DOWN USING EMERGENCY BLOWDOWN BOTTLE. RESET PUSHED BACK PIN AND ALL FUNCTIONAL CHECKS GOODNov 19, 2004 · N336C · Cessna 550 · Landing Gear Retraction/Extension SystemSDR 2005FA0000246Frame · crackedUPPER CHAIR BASE ASSEMBLY CRACKED AT CHAIR BACK ATTACH POINTS. ALSO, PREVIOUS INAPPROPRIATE REPAIR. CHAIR WAS REPAIRED IAW STO1042WI STRUCTURAL SEAT REPAIR. (K)Nov 3, 2004 · N219MS · Cessna 550 · Passenger Compartment EquipmentSDR 2005FA0000245Frame · crackedUPPER CHAIR BASE ASSEMBLY CRACKED AT CHAIR BACK ATTACH POINTS. CHAIR WAS REPAIRED IAW STO1042WI STRUCTURAL SEAT REPAIR. (K)Nov 3, 2004 · N219MS · Cessna 550 · Passenger Compartment Equipment
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