Cessna S550

Service difficulty reports · 127

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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 = 'S550'
  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 CA031020010Bearing · worn(CAN) NR 2 GENERATOR WENT OFF LINE DURING TAXI TO THE RAMP. WOULD NOT RESET. MAINTENANCE DETERMINED THAT THE GENERATOR WAS DEFECTIVE. THERE WAS PLAY IN THE SHAFT BEARING GS CAUSING REJECTION OF THE UNIT. REPORT FROM THE OVERHAUL SHOP CONFIRMED A BEARING FAILUROct 6, 2003 · Cessna S550 · Starter-GeneratorSDR CA031020009Brushes · worn(CAN) LT ENGINE WOULD NOT ROTATE ON START. INSPECTION OF THE STARTER GENERATOR DETERMINED THAT THE BRUSHES WERE EXCESSIVELY WORN. THE ASSEMBLY ONLY HAD 139.5 HOURS SINCE OVERHAUL.Oct 1, 2003 · Cessna S550 · Engine StarterSDR IMJ2004F00001Controller · failedCABIN LOST PRESSURIZATION AT FL27 IN CRUISE WHEN CONTROLLER WAS ADJUSTED FOR DESCENT.Jul 22, 2003 · N550KM · Cessna S550 · Cabin Pressure ControllerSDR FTU2003F00007Valve · corrodedDURING REPLACEMENT OF PERI SEALS ON THE FORWARD SIDE OF THE ENGINE ANTI ICE SYSTEM, THE ANTI ICE VALVE HAD TO BE REMOVED. WHILE REMOVING THE ELECTRICAL CONNECTOR, DIFFICULTY WAS ENCOUNTERED BECAUSE THE CONNECTOR WAS OVER TORQUED OR CORROSION HAD CREATED A PROApr 24, 2003 · N126QS · Cessna S550 · Air Intake Anti/De-Ice SystemSDR I5WA933JSkin · damagedON 2/10/2003, AIRCRAFT WAS AT CRUISE ALTITUDE (FL350). THE CREW HEARD A LOUD BANG NEAR THE AFT BAGGAGE AREA. THE AIRCRAFT THEN BEGAN TO VIBRATE. THE SIC WALKED TO THE REAR OF THE AIRCRAFT AND NOTICED DAMAGE TO THE RIGHT OUTBOARD FLAP. THE SIC THEN INFORMEFeb 13, 2003 · N92ME · Cessna S550 · Trailing Edge FlapsSDR AHQA055NOxygen Mask · tornAT COMPLIANCE WITH AD DISCOVERED TWO O2 MASKS CONTAINED TEARS IN THE FACE CUSHION.Dec 27, 2002 · N598WC · Cessna S550 · Passenger Oxygen SystemSDR CA021016035Skin · cracked(CAN) PHASE 49 SKIN JOINT EDDY CURRENT INSPECTION INDICATED AN ANAMOLY AT FS 287.78 WL 146.6. FURTHER INVESTIGATION USING A 5000X MICROSCOPE REVEALED A 1 INCH LONG GOUGE AND CRACK IN SKIN DOUBLER BETWEEN SKIN EDGES. AIRCRAFT FERRIED UNPRESSURISED TO WICHITA CIOct 9, 2002 · Cessna S550 · Vertical Stabilizer, Plate/SkinSDR 2002FA0001038Stator · crackedAT HOT SECTION INSPECTION THE HT STATOR WAS FOUND TO HAVE AXIAL CRACKS IN SEVERAL PLACES IN THE INNER SHROUD RUNNING FROM THE TRAILING EDGE FORWARD TO 1/2IN. FROM INNER LUGS. AT ONE CRACK THE INNER SHROUD TRAILING EDGE LIFTED UP ENOUGH TO MAKE CONTACT WITH THESep 5, 2002 · N550DS · Cessna S550 · Turbine SectionSDR RJ22002F00000Bearing · failedINFLIGHT, CREW NOTICED NOISE IN LT ENGINE, FOLLOWED BY NR 1 GENERATOR FAILURE. INSPECTORS FOUND AFT BEARING ON LT STARTER GENERATOR HAD COMPLETELY FAILED ALLOWING ARMATURE TO HIT FIELD POLES. S/G HAD APPROXIMATELY 500 HOURS SINCE LAST OVERHAUL. EXCHANGE STAAug 20, 2002 · N1VA · Cessna S550 · Starter-GeneratorSDR 2002FA0000464Pressure Switch · failedTKS DEICE SYSTEM PRESSURE SWITCHES ARE FAILING IN THE OPEN POSTION. WHEN THE SWITCHES FAIL OPEN THEY CAN NOT ILLUMINATE THE DEICE PRESSURE FAIL LIGHTS ON THE ANNUCIATOR. THE LIGHTS ILLUMINATE TO INDICATE LOW PRESSURE. THERE IS NO WAY TO TELL LOW PRESSURE IN THApr 10, 2002 · N126QS · Cessna S550 · Airfoil Anti/De-ice SystemSDR 2002FA0000631Starter Gen · failedSTATER GEN UNIT FAILED TO START ENGINE. NO OTHER OPERATION PROBLEM NOTED. SUBSEQUENT TEARDOWN REVEALED WORN AND / OR DAMAGED PARTS. UNIT WAS REPORTED AND TAGGED OVERHAULED 60 HRS PRIOR TO FAILURE BY WECO OF LINCOLN, CA.Apr 5, 2002 · N200CV · Cessna S550 · Starter-GeneratorSDR AUS20011239Wire Harness · intermittent(AUS) LT ANTISKID TRANSDUCER WIRING HAD AN INTERMITTENT FAULT. NO BRAKING DURING LANDING RESULTED IN EMERGENCY BRAKING SYSTEM OPERATION. RH TYRE FAILED DUE TO WHEEL SKIDDING. RT MAIN WHEEL HUB ALSO DAMAGED.Nov 21, 2001 · Cessna S550 · Landing Gear System WiringSDR CA010913004Valve · failed(CAN) FOLLOWING AN UNEVENTFUL LANDING AND WHILE TAXING AFTER THE LANDING ROLL OUT, THE CREW ENCOUNTERED A BRAKE FAILURE AND HAD TO APPLY THE EMERGENCY BRAKE IN ORDER TO STOP THE AIRCRAFT. MAINTENANCE TROUBLESHOOTING AND INSPECTION OF THE SYSTEM DETERMINED THATSep 12, 2001 · Cessna S550 · Master Cylinder/Brake ValveSDR AU001246Spar · corroded(AUS) HORIZONTAL STABILISER REAR SPAR AND UPPER SPAR CAP CORRODED.FOUND DURING REMOVAL OF THE UPPER RH SKIN DUE TO DELAMINATION.Dec 30, 2000 · Cessna S550 · Horizontal Stabilizer, Spar/RibSDR CA001006003Door Seal · frozen(CAN) AT CRUISE ALTITUDE, THE CREW DETECTED AN AIR WHISTLING SOUND FOLLOWED BY A DECREASE IN PRESSURIZATION AND THE ABILIITY TO CONTROL IT. THE CREW BEGAN A DESCENT PER THE AFM PROCEDURES. WHEN DESCENDING THROUGH 19,000 FEET, THE PRESSURIZATION RETURNED TO NAug 16, 2000 · Cessna S550 · Passenger/Crew DoorsSDR CA000530074Wire · chafed(CAN) DURING CLIMB, THE FLAP CONTROL CIRCUIT BREAKER TRIPPED AS THE FLAPS WERE BEING RETRACTED. THE BREAKER WAS RESET AND IT TRIPPED AGAIN. THE FLIGHT WAS CONTINUED WITH THE FLAPS PARTIALLY EXTENDED. MAINTENANCE PERSONNEL FOUND THE FLAP CONTROL CIRCUIT WIRINMay 18, 2000 · Cessna S550 · Trailing Edge Flap Control SystemSDR CA000316005Support Bracket · failed(CAN) ON LANDING ROLL, THE PILOT EXPERIENCED A LEFT BRAKE FAILURE. MAINTENANCE FOUND THE BRAKE CYLINDER HAD TORN THE MOUNTING HOLE OUT OF THE CYLINDER MOUNTING BRACKET. THE RIGHT HAND BRAKE CYLINDER MOUNTING BRACKET WAS FOUND IN POOR CONDITION ALSO.Mar 3, 2000 · Cessna S550 · Fuselage, Equipment Attach FittingsSDR 99ZZZX3321Oxygen Mask · tornDURING ROUTINE INSPECTION OF THE PASSENGER OXYGEN MASKS, A TEAR WAS FOUND AROUND THE COLLAR OF THE BAG WHERE THE OXYGEN FEED TUE ENTERS IT.Jul 26, 1999 · N288QS · Cessna S550 · Passenger Oxygen SystemSDR 99ZZZX2952Control Cable · frayedPILOT NOTED FLAP HYDRAULIC LIGHT WOULD STAY ILLUMINATED IN FLAP UP CONDITION UNLESS FLAP LEVER WAS PULLED BACK JUST OFF THE UP (ZERO DEGREES) STOP. INVESTIGATION REVEALED CABLE FRAYED AT LOWER PULLEY/DRUM TO WITHIN 2 STRANDS OF BREAKING. FAILURE TOOK MINIMAL Jul 2, 1999 · N200CV · Cessna S550 · Trailing Edge Flap Control SystemSDR 99ZZZX1144Panel · corrodedREMOVAL OF TKS PANELS REVEALED LIGHT TO MODERATE CORROSION ON TKS PANEL WING ATTACH FLANGES. NUTPLATES ARE INSTALLED ON ATTACH FLANGES FOR SECURING TKS PANELS TO THE WING STRUCTURE. INVEST SHOWED DURING SYS OPER, TKS FLUID MIGRATED PAST ATTACH SCREWS TO THE Dec 10, 1998 · N39TF · Cessna S550 · Fuselage Main, Plate/SkinSDR 99ZZZX814Engine · malfunctionedSTARTED DESCENT FROM 31,000 FEET. AT 25,000 FEET, REDUCED POWER AND FELT VIBRATION ON RIGHT SIDE. SHUT NR 2 DOWN IMMEDIATELY. SINCE TOTAL TIME WAS 3,450 HOURS, OVERHAULED BOTH MAIN BEARINGS, STARTED TO FAIL.Dec 7, 1998 · N1982U · Cessna S550 · Engine (Turbine/Turboprop)SDR AU980597Fitting · corroded(AUS) RT AILERON HINGE FITTINGS CONTAINED INTERGRANNULAR CORROSION. PART TC: 7,910.May 27, 1998 · Cessna S550 · AileronsSDR AU980598Hinge · broken(AUS) LT AILERON HINGE FLANGE BROKEN. INTERGRANNULAR CORROSION WAS ALSO FOUND IN THE HINGES. PART TC: 7,910.May 25, 1998 · Cessna S550 · AileronsSDR 98ZZZX2952Valve · failedAS AIRCRAFT CLIMBED THROUGH 10,000 FEET, CABIN WOULD NOT PRESSURIZE. INSPECTION FOUND BOTH FLOW CONTROL VALVES HAD FAILED INTERNALLY. SUBMITTER STATED EXERCISE VALVES MORE FREQUENTLY DURING MAINTENANCE RUNS OR EVALUATION FLIGHTS OR ESTABLISH A TBO OR REPLACEMay 7, 1998 · N550KM · Cessna S550 · Pressure Regulator/Outflow ValveSDR 98ZZZX2951Valve · failedAS AIRCRAFT CLIMBED THROUGH 10,000 FEET, CABIN WOULD NOT PRESSURIZE. INSPECTION FOUND BOTH FLOW CONTROL VALVES HAD FAILED INTERNALLY. SUBMITTER STATED EXERCISE VALVES MORE FREQUENTLY DURING MAINTENANCE RUNS OR EVALUATION FLIGHTS OR ESTABLISH A TBO OR REPLACEMay 7, 1998 · N550KM · Cessna S550 · Pressure Regulator/Outflow ValveSDR 98ZZZX1539Switch · shortedPILOT REPORTED FLAP CONTROL CIRCUIT BREAKER TRIPPED WHEN FLAPS SELECTED UP. C/B WOULD NOT RESET. MAINTENANCE FOUND FLAP LIMIT SWITCH ON LT FLAP ACTUATOR INTERNALLY SHORTED TO GROUND. INSTALLED NEW SWITCH, P/N 602EN16-6, AND ADJUSTED AND SAFETIED IAW CESSNA Apr 9, 1998 · N98QS · Cessna S550 · Trailing Edge Flap Control SystemSDR 99ZZZX135Probe · malfunctionedORIGINAL PROBE WOULD ONLY READ HALF OF A TANK WHEN FULL. INSTALLED NEW PROBE. WITH TANK FULL GAUGE READ ZERO. INSTALLED SERVICEABLE PROBE AND SYSTEM WORKED CORRECTLY.Feb 4, 1998 · N98QS · Cessna S550 · Engine Fuel Indicating SystemSDR 99ZZZX129Probe · malfunctionedAFTER INSTALLATION IN TKS TANK, WITH TANK FULL, GAUGE READ ZERO. INSTALLATION OF ANOTHER NEW GAUGE SHOWED SYSTEM WORKED CORRECTLY.Feb 4, 1998 · N106QS · Cessna S550 · Engine Fuel Indicating SystemSDR 98ZZZX93Rudder · lightning strikeAIRCRAFT ENTERED SHOP FOR ROUTINE MAINTENANCE AND DURING PRELIM INSPECTION NOTICED RUDDER TIP CAP BURNED AND LOOSE. TEAR DOWN INSP OF RUDDER SHOWED INTERNAL SIGNS OF OVERHEATING. OWNER QUESTIONED AND WAS DETERMINED THAT AT SOME PREVIOUS TIME, ACFT HAD A LIGHDec 12, 1997 · N674JM · Cessna S550 · Rudder StructureSDR 97ZZZX4776Bearing · mismanufacturedDURING AIRCRAFT INSPECTION, DETERMINED THE FLAP ATTACH BEARINGS WERE WORN. RETRIEVED TWO NEW BEARINGS FROM STOCK. INSPECTED NEW BEARINGS. ONE BEARING HAD COTTER KEY HOLE DRILLED TOO FAR DOWN ON THREADED PORTION OF SHANK TO ALLOW PROPER ATTACHMENT OF NUT. TNov 4, 1997 · N211QS · Cessna S550 · Trailing Edge FlapsSDR 97ZZZX4775Bearing · wornDURING AIRCRAFT INSPECTION, DETERMINED THE FLAP ATTACH BEARINGS WERE WORN. RETRIEVED TWO NEW BEARINGS FROM STOCK. INSPECTED NEW BEARINGS. ONE BEARING HAD COTTER KEY HOLE DRILLED TOO FAR DOWN ON THREADED PORTION OF SHANK TO ALLOW PROPER ATTACHMENT OF NUT. TNov 4, 1997 · N211QS · Cessna S550 · Trailing Edge FlapsSDR 97ZZZX4533Solenoid Valve · malfunctionNOTED TKS ANTI-ICING FLUID FLOWED FROM WING OUTBOARD LEADING EDGES WITHOUT ANTI-ICING BEING SELECTED ON BY CREW. SUSPECT CAUSE - STUCK SOLENOID VALVE. SUBMITTER RECOMMENDS PERIODIC CHECKS TO ENSURE VALVES FUNCTION PROPERLY.Sep 29, 1997 · N550KM · Cessna S550 · Airfoil Anti/De-ice SystemSDR 97ZZZX3785Seal Grommet · failedPILOT REPORTED RAPID DE-PRESSURIZATION AT ALTITUDE AND NOTED DOOR SEAL AT MAIN ENTRANCE DOOR LEAK. MAINTENANCE FOUND DOOR SEAL GROMMET DRY-ROTTED AND CRACKED. INSTALLED NEW GROMMET, P/N MS35489-41, AND PERFORMED OPERATIONAL CHECK, NO DEFECTS OF DOOR SEAL NOTAug 6, 1997 · N72AM · Cessna S550 · Passenger/Crew DoorsSDR 97ZZZX4154Bolt · loosePILOT'S AND COPILOT'S CONTROL COLUMN ASSY HAD EXCESSIVE PLAY AND CLICKING WAS HEARD WHEN PRESSURE APPLIED TO OPPOSITE CONTROL COLUMN. PLAY WAS NOTICED IN FORWARD AND AFT OF INBD AND OTBD PRESSURE. BOLTS WERE FOUND LOOSE AND NO TORQUE PUTTY WAS PRESENT ON BOLJun 11, 1997 · N103QS · Cessna S550 · Control Column SectionSDR 97ZZZX2903Bellcrank · corrodedDURING INSPECTION, FOUND LT INBOARD FLAP OUTBOARD BELLCRANK WITH EXCESSVIE SIDE-TO-SIDE PLAY. UPON REMOVAL, FOUND UPPER AND LOWER BEARINGS FROZEN AND/OR CORRODED. A LARGE QUANTITY OF RUSTY WATER FLOWED OUT OF THE BELLCRANK TUBE. IT APPEARS THE TUBE WAS FILLJun 2, 1997 · N134QS · Cessna S550 · Trailing Edge Flap Control SystemSDR 97ZZZX2362Valve Assy · wornWHEN CLIMBING OUT OF 31,000 FEET, A LOUD BOOM WAS HEARD IN THE REAR OF AIRCRAFT. CABIN ALTITUDE ROSE AT 5,000 FPM. EMERGENCY DESCENT INITIATED AND AIRCRAFT LANDED AT PIT. TAIL CONE PRESSURIZATION DUCT BLOWN OFF AT CONNECTOR TO WATER SEPARATOR. BEADING ON FMay 2, 1997 · N92QS · Cessna S550 · Air Distribution SystemSDR 97ZZZX1329Regulator · defectiveDURING POST-INSPECTION RUN UP, NOTICED CO-PILOT'S ATTITUDE GYRO AIR PRESSURE LOW AND GYRO UNSTABLE. FOUND FIRST STAGE AIR PRESSURE REGULATOR LOWER THAN NORMAL AND UNADJUSTABLE. REPLACED REGULATOR. FOUND CORROSION, DIRT, AND WATER INSIDE REGULATOR. AIR FILTEJan 27, 1997 · N211QS · Cessna S550 · Vacuum Distribution SystemSDR 97ZZZX1330Terminal Lug · wrong partDURING ENGINE INSPECTION, FOUND IMPROPER TERMINAL LUG ON RIGHT ENGINE T1 PROBE. THE TERMINAL APPEARS TO BE THE PROPER MATERIAL (AL), BUT IS NOT A 1-322338-0 TERMINAL. IT APPEARS THAT THIS TERMINAL LUG WAS INSTALLED WHEN THE PROPER ONE WAS UNAVAILABLE.Jan 13, 1997 · N93QS · Cessna S550 · Engine Temperature Indicating SystemSDR 97ZZZX269Lead · defectiveDURING INSPECTION, LEFT ENGINE OUTBOARD IGNITER WOULD NOT OPS CHECK. FOUND IGNITION CABLE DEFECTIVE DUE TO AN INTERNAL FAULT. COULD NOT DETERMINE CAUSE AS EXTERNAL INSPECTION OF IGNITION CABLE APPEARED SERVICEABLE.Dec 14, 1996 · N101QS · Cessna S550 · Ignition Harness (Distribution)SDR 97ZZZX351Connector · meltedDURING INSPECTION, FOUND BATTERY CONNECTOR CORRODED AND MELTED. CAUSE IS BELIEVED TO BE EXCESSIVE LOOSENESS OF PLUGS. CLOSELY INSPECTED BATTERY CONNECTOR FOR CONDITION AND LOOSENESS.Nov 30, 1996 · N299QS · Cessna S550 · DC Generating SystemSDR 97ZZZX355Tank · leakingDURING AIRCRAFT CLEANING, FOUND AIRCRAFT TOILET LEAKING. FOUND TANK UNIT LEAKING FROM IMPROPER REPAIR. TOILET MAINTENANCE MANUAL DOES NOT PERMIT SEALING OF THE TANK UNIT. TANK UNIT SHOULD BE REPLACED IF FOUND LEAKING DUE TO THE VERY REAL CORROSION PROBLEM FNov 18, 1996 · N86QS · Cessna S550 · Waste Disposal SystemSDR 97ZZZX36Seal · leakingENTRANCE DOOR SEAL LEAKING AT ALTITUDE. FOUND BAD CABIN DOOR SEAL.Nov 7, 1996 · N93QS · Cessna S550 · Passenger/Crew DoorsSDR 97ZZZX4155Bolt · looseBOTH PILOT'S AND COPILOT'S CONTROL COLUMN ASSY HAD EXCESSIVE PLAY. WHEN PRESSURE WAS APPLIED TO OPPOSITE COLUMN, FORWARD AND AFT OR INBOARD AND OUTBOARD, FOUND BOLTS HAD EXCESSIVE PLAY AND CLICKING NOISE WAS HEARD. (NO PUTTY WAS ON ANY BOLTS). TOTAL AIRCRAFOct 15, 1996 · N106QS · Cessna S550 · Control Column SectionSDR 96ZZZX5255Exciter · inoperativeDURING OPERATIONAL CHECK OF NEW ENGINE IGNITER, IGNITION EXCITER FAILED TO FIRE IGNITER. PROPER VOLTAGE OBSERVED AT CANNON PLUG. INTERNAL PROBLEM WITH EXCITER BOX.Aug 30, 1996 · N111QS · Cessna S550 · ExciterSDR 96ZZZX5256Switch · corrodedDURING PHASE 5 INSPECTION, FOUND LT WING CUFF TKS PANEL PRESSURES SWITCH BADLY CORRODED AND METAL EXFOLIATED ON THE SURFACE OF THE SWITCH. SUBMITTER STATED POOR QUALITY OF METAL USED IN MAKING SWITCH BODY WITH POSSIBLE TKS FLUID LEAKAGE LIKELY CAUSE.Aug 23, 1996 · N112QS · Cessna S550 · Airfoil Anti/De-ice SystemSDR 96ZZZX5051Line · chafe/failBRAKE PRESSURE LOST ON LANDING. INVESTIGATION OF PROBLEM REVEALED THE BRAKE LINE GOING TO THE LT BRAKE HAD BEEN CHAFED THROUGH BY AN ELEVATOR CONTROL CABLE. THE LINE WAS REMOVED AND REPLACED. THE NEW LINE WAS INSTALLED WITH ADEQUATE CLEARANCE BETWEEN THE BRAug 20, 1996 · N91ML · Cessna S550 · Landing Gear Brake SystemSDR 96ZZZX4171Pump · motor seizedCREW REPORTED TOILET WOULD NOT FLUSH. FOUND MOTOR/PUMP ASSEMBLY LOCKED UP TIGHT. THIS IS A COMMON OCCURRENCE AS THE PUMP IMPELLER SWELLS AND JAMS IN THE PUMP HOUSING. NEED TO USE A MOTOR/PUMP ASSEMBLY THAT IS RESISTANT TO 'BLUE WATER'.Aug 12, 1996 · N299QS · Cessna S550 · Waste Disposal SystemSDR 96ZZZX4168Control Cable · frayedDURING PHASE 12 INSPECTION, FOUND LOWER INBOARD AILERON CABLE WITH BROKEN WIRES. THIS WEAR/DAMAGE OCCURS AT FAIRLEADS P/N S338-1. INSPECTION FOUND TEFLON FAIRLEAD DAMAGES THIS CABLE ABOUT 75 PERCENT OF THE TIME. SUBMITTER STATED SOMETHING NEEDS TO BE DONE AJun 30, 1996 · N157QS · Cessna S550 · Aileron Control SystemSDR 96ZZZX3822Capacitor Assy · explodedGENERATOR AND GENERATOR CONTROL UNIT FILTER INSTALLATION, CAPACITOR ASSEMBLY. CAPACITOR PART NUMBER BLEW A HOLE IN THE END, BLEW ONE LEAD OFF ITS CONTACT, AND BURNED THE INSULATION FROM THE WIRE, FOR APPROXIMATELY 1 INCH.Jun 24, 1996 · N260QS · Cessna S550 · DC RegulatorSDR 96ZZZX2903Bolt · misinstalledPHASE INSPECTION. INSPECTOR WAS CHECKING FLAP TENSION AND FOUND FLAP CABLE MISALIGNED WHEN FLAPS RETRACTED. FURTHER INVESTIGATION REVEALED INBD FLAP CONTROL BELLCRANK FWD PUSHROD BOLT INSTALLED WITH HEAD OF BOLT UP. THIS CAUSED INTERFERENCE WITH THE SHANK, Apr 30, 1996 · N9GT · Cessna S550 · Trailing Edge Flap Control System
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