Convair 440

Service difficulty reports · 206

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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 = '440'
  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 CA071026004Actuator · malfunctioned(CAN) DURING APPROACH WHEN LANDING GEARS SELECTED DOWN, THE LANDING GEARS UNLOCK LIGHT CAME ON, HOWEVER, NO NOSE WHEEL DOWN LIGHT CAME ON. THE CREW CONFIRMED VISUALLY GEAR NOT DOWN. AFTER A FEW CYCLES GEAR UP AND GEAR DOWN AND EMERGENCY UPLATCH RELEASE TO NO AOct 23, 2007 · Cvac 440 · Steering UnitSDR CA070816001Connector · unsecure(CAN) ENGINE NR 1 RPM UNSTABLE, REDUCED RPM TO 13,600. AIRCRAFT DIVERTED TO NEAREST AIRPORT. ENGINE WAS SHUTDOWN IN FINAL APPROACH, DUE TO RPM REDUCTION TO 13500 RPM. MAINTENANCE WAS SENT ON SITE AND FOUND THAT OIL PROPELLER FILLER PLUG WAS NOT SECURED PROPEAug 10, 2007 · Cvac 440 · Propeller AssemblySDR CA070824007Door · inoperative(CAN) AIRCRAFT WAS DISPATCHED FOR FIRE ACTION. AFTER DEPARTURE, THE RT OIL TEMPERATURE GAUGE WAS OBSERVED TO BE AT THE BOTTOM OF THE RED ARC, APPROXIMATELY 100 DEGREES C. THE FLIGHT CREW IMMEDIATELY SHUTDOWN THE RT ENGINE AS A PRECAUTION AND RETURNED TO BASE. Jul 25, 2007 · Cvac 440 · Engine Oil CoolerSDR CA070727009Lever · distorted(CAN) UPON SELECTION OF (GEAR DOWN), THE LOCKING ARM OF THE LANDING GEAR SELECTOR HANDLE STUCK IN THE EXTENDED POSITION, PREVENTING ASSOCIATED FUNCTION OF DEPRESSING THE GEAR WARNING LIGHT SWITCH. THE RESULT WAS NO GEAR DOWN INDICATING LIGHTS ON THE ANNUNCIATJul 23, 2007 · Cvac 440 · Landing Gear SelectorSDR RDS12120061Axle · crackedWHEN REMOVING NOSE AXLE TO C/W AD83-01-02 FOR THE 12,000 HOUR MAGNETIC PARTICLE TESTING. A CRACK AROUND THE AXLE FLANGE THAT THE BEARING SPACER RIDES AGAINST WAS NOTICED. REMOVED AND REPLACED WITH NEW AXLE, RETURNED AIRCRAFT TO SERVICE.Oct 18, 2006 · N587CA · Cvac 440 · Nose/Tail Landing Gear Strut/AxleSDR CA060617001Steering Sys · malfunctionedAFTER T/O, DURING L/G RETRACTION, NOSE WHEELS ENTERED W/W IN A RT TURN ATTITUDE, EVIDENT FROM WEAR MARKS ON TIRES AND RUBBER ON INTERIOR WALLS OF W/W. WHEN A/C LANDED, NOSE WHEELS WERE STILL TURNED TO THE RIGHT, UNKNOWN TO AIRCREW. CAPT TRIED TO STRAIGHTEN NJun 9, 2006 · Cvac 440 · Landing Gear Steering SystemSDR CA060516008Wire Harness · chafedDURING INSTALLATION OF ELT REMOTE SWITCH WIRING, ROUTING OF THE WIRE BEHIND THE FORWARD RT EQUIPMENT SHELF, SEVERAL WIRES WERE FOUND CHAFING INTO THE WIRE BUNDLE THAT RUNS VERTICALLY BEHIND THE SHELF. THE WIRES WERE CHAFING ON THE BACK EDGE OF THE FLOOR. THMay 12, 2006 · Cvac 440 · Electrical Power System WiringSDR CA060302012Wire Harness · misinstalledAIRCRAFT ON A TEST FLIGHT AND DURING AN RPM DECAY TEST, THE LT ENGINE POWER LEVER WAS REDUCED BELOW 1400 HP. THE RPM THEN STARTED TO DECAY BELOW PRESCRIBED LIMITS. DUE TO THIS, THE CREW ELECTED TO SHUT DOWN THE ENGINE. THE PROBLEM ONLY OCCURRED BELOW 1400 HJan 18, 2006 · Cvac 440 · Turbine Engine System WiringSDR CA050823007Hook · failed(CAN) WITH AN AIRCRAFT MECHANIC AND 2 FLIGHT ATTENDANTS ON BOARD, THE REAR SERVICE DOOR OPEN WARNING LIGHT CAME ON AT 14,000 FEET. AIRCRAFT DEPRESSURIZE AND RETURN TO DEPARTURE. INVESTIGATION REVEALED THAT LOWER REAR HOOK WAS NOT GOING IN PLACE PROPERLY, DOOAug 19, 2005 · Cvac 440 · Service DoorsSDR CA050823005Bearing · failed(CAN) WITH AN AIRCRAFT MECHANIC AND 2 FLIGHT ATTENDANTS ON BOARD, NR 1 ENGINE FLAMED OUT IN DESCENT, AIRCRAFT LANDED SAFELY AT AIRPORT. AFTER EVALUATION, THE POWER SECTION ACCESSORIES GEARBOX WAS FOUND AT FAULT, TOWER SHAFT BEARING (RR. IPC 72-60-00 FIG. 3 IAug 19, 2005 · Cvac 440 · Turbine Engine Accessory DriveSDR CA050727004Selector · failedON APPROACH TO AIRPORT, THE THREE (3) MLG DOWN GREEN LIGHT DID NOT ILLUMINATE AFTER GEAR EXTENSION, THE HORN DID NOT SOUND AND THE RED GEAR UNSAFE LIGHT EXTINGUISHED. MAINTENANCE WAS UNABLE TO DUPLICATE THE SNAG ON GROUND, THE (LANDING) GEAR LEVER SWITCH WAS Jul 26, 2005 · Cvac 440 · Landing Gear SelectorSDR JRAA587060705Longeron · corrodedINTERGRANULAR CORROSION WAS FOUND ON THE LONGERON CHANNEL AT FUSELAGE BUTTOCK LINE 0, WING STATION 403.0. THIS CORROSION NOTED ON THE LT SIDE, 10 INCHES FORWARD OF THE REAR LOWER WING SPAR. ACCESS THROUGH THE LT WING IB DRY BAY PANEL. (K)Jun 7, 2005 · N587CA · Cvac 440 · Wing, Longeron/StringerSDR CA050527007Switch · inoperativeON FINAL APPROACH TO MONTREAL, THE RT MAIN LANDING GEAR DOWN ANNUNCIATION LIGHT FAIL TO INDICATE. AFTER INVESTIGATION, THE DOWN MICROSWITCH WAS FOUND INOPERATIVE, UNIT REPLACED AND ADJUSTED IAW MAINTENANCE MANUAL. GEAR SWING C/O SERVICEABLE, AIRCRAFT RETURN May 26, 2005 · Cvac 440 · Landing Gear Position and WarningSDR VGC2005F00001Unknown · unknownNR 2 FUEL PUMP FAILED. RT DC GENERATOR OFF LINE, FOLLOWED BY LT DC GENERATOR OFF LINE. (ELECTRIC ODOR NOTED). TRU TO EMERGENCY SELECTED FOR DC BUSS POWER. PRECAUTIONARY LANDING MADE. (K)May 16, 2005 · N171FL · Cvac 440 · Standard Practices/StructuresSDR CA041104001Drain · obstructed(CAN) ON DEPARTURE, CARGO SMOKE DETECTOR LIGHT CAME ON WITH NO ODOR OR SMOKE IN COCKPIT. EMERGENCY DECLARE AND RETURNED AFTER 10 MINUTES AIR TIME. LIGHT EXTINGUISH DURING TAXI. CARGO CONTAINER AND A/C INSPECTED, NOTHING UNUSUAL DETECTED. PROBLEM TREATED LIKE ANov 2, 2004 · Cvac 440 · Humidity Control SystemSDR CA051006001Fitting · cracked(CAN) AIRCRAFT RETURN TO BLOCK AFTER LOSS OF HYDRAULIC FLUID. AFTER INVESTIGATION MAINTENANCE FOUND FROM LT ENGINE DRIVE HYDRAULIC PUMP PRESSURE LINE AND AC HYDRAULIC PUMP, T-FITTING AT FS 319 CRACKED. THE FITTING WAS REPLACED, SYSTEM REPLENISHED AND LEAK CHOct 27, 2004 · Cvac 440 · Hydraulic System, MainSDR CA041004004Pump · out of adjust(CAN) AIRCRAFT DISPATCH LIKE USUAL FROM HANGAR WITH 28 PASSENGER ONBOARD AND CAME BACK DUE TO FUEL UNBALANCE AND ONE PASSENGER HAD REPORT SEEING FUEL COMING OUT OF RT HAND TANK OVERWING FUEL CAP AND CREW REALIZED IT HAD TAKEN OFF WITH FUEL CROSS-FEED OPEN. MASep 21, 2004 · Cvac 440 · Engine Fuel PumpSDR CA041005002Door · out of rig(CAN) AIRCRAFT DISPATCH WITH 29 PASSENGER ABOARD AT 13:32 GMT AND CAME BACK AT 14:14 WITH C2 DOOR OPEN. MAINTENANCE DISCOVERED THAT THE C2 DOOR COULD BE CLOSE IMPROPERLY IN SOME OCCASION AND NO DAMAGE WAS FOUND. MAINTENANCE CLOSE THE DOOR AND CONFIRM THE LOCK Sep 8, 2004 · Cvac 440 · Cargo/Baggage DoorsSDR CA040823002Circuit Breaker · sticking(CAN) DURING CRUISE THE OIL TEMPERATURE ON THE LT ENGINE CLIMBED TO LIMITS. THE OIL COOLER DOOR WAS NOT OPERATING. THE ENGINE WAS SHUT DOWN AND THE PROPELLER WAS FEATHERED AS A PRECAUTION. THE AIRCRAFT RETURNED TO BASE. UPON INVESTIGATION BY MAINTENANCE THE CIAug 19, 2004 · Cvac 440 · Engine Oil CoolerSDR CA040819013Line · ruptured(CAN) AC WAS ORBITING OVER FIRE. A LOUD SURGING SOUND WAS HEARD. A CHECK OF HYDRAULIC RESERVOIR INDICATED THAT NO HYDRAULIC FLUID WAS REMAINING. FLAPS WERE SELECTED FROM 15 TO 0 DEGREES. HYD BYPASS WAS SELECTED UP. RETARDANT LOAD WAS JETTISONED. AC RETURNED Aug 17, 2004 · Cvac 440 · Hydraulic System, MainSDR 2004F00349Check Valve · corrodedBAK - DURING WATER METHANOL SYSTEM TROUBLESHOOTING, MAINTENANCE PERSONNEL FOUND SEVERE CORROSION ON SEVERAL OF THE WATER METHANOL SYSTEM COMPONENTS LOCATED INSIDE THE LEFT AND RIGHT TANKS. PART REPLACED. (M)Aug 6, 2004 · N587CA · Cvac 440 · Water Injection SystemSDR 2004F00347Tube · corrodedBAK - DURING WATER METHANOL SYSTEM TROUBLESHOOTING, MAINTENANCE PERSONNEL FOUND SEVERE CORROSOIN ON SEVERAL OF THE WATER METHANOL SYSTEM COMPONENTS LOCATED INSIDE THE LEFT AND RIGHT TANKS. PARTS REPLACED. (M) JRAAAug 6, 2004 · N587CA · Cvac 440 · Water Injection SystemSDR 2004F00346Transmitter · corrodedDUIRNG WATER METHANOL SYSTEM TROUBLESHOOTING, MAINTENANCE PERSONNEL FOUND SEVERE CORROSION ON SEVERAL OF THE WATER METHANOL SYSTEM COMPONENTS LOCATED INSIDE THE LEFT AND RIGHT TANKS. TRANSMITTER REPLACED. (M)Aug 6, 2004 · N587CA · Cvac 440 · Water Injection SystemSDR 2004F00344Door · corrodedBAK - DUIRNG WATER METHANOL SYSTEM TROUBLESHOOTING, MAINTENANCE PERSONNEL FOUND SEVERE CORROSION ON SEVERAL OF THE WATER METHANOL SYSTEM COMPONENTS LOCATED INSIDE THE LEFT AND RIGHT TANKS. DOOR REPLACED. (M)Aug 6, 2004 · N587CA · Cvac 440 · Water Injection SystemSDR 2004F00343Bellmouth · corrodedDURING WATER METHANOL SYSTEM TROUBLESHOOTING, MAINTENANCE PERSONNEL FOUND SEVERE CORROSION AND SEVERAL OF THE WATER METHANOL SYSTEM COMPONENTS LOCATED INSIDE THE LEFT AND RIGHT TANKS. PARTS REPLACED. (M)Aug 6, 2004 · N587CA · Cvac 440 · Water Injection SystemSDR CA040804001Gasket · missing(CAN) DURING DESCENT THE LT ENGINE ZONE 2 FIRE ALARM ACTIVATED.Aug 3, 2004 · Cvac 440 · Detection SystemSDR CA040806001Actuator · failed(CAN) DURING CRUISE THE FLIGHT CREW NOTICED THAT THE OIL TEMPERATURE ON THE LT ENGINE WAS CLIMBING. THE CREW TRIED TO MANUALLY CONTROL THE OIL TEMP BUT WAS UNSUCCESSFUL. THE ENGINE WAS SHUT DOWN AND THE PROP WAS FEATHERED AS A PRECAUTION. THE AIRCRAFT RETURAug 3, 2004 · Cvac 440 · Engine Oil CoolerSDR CA040719006Turnbuckle · shearedDURING INSPECTION MAINTENANCE CREW NOTED THAT THE RIGHT HAND ENGINE OUTBOARD EXHAUST SUPPORT TURNBUCKLE HAD SHEARED CAUSING THE TAILPIPE TO REST ON THE BOTTOM OF THE EXHAUST SHROUD INSTEAD OF BEING SUPPORTED IN THE CENTER. THE TURNBUCKLE WAS REPLACED WITH A SJul 16, 2004 · Cvac 440 · Engine Collector/Tailpipe/NozzleSDR CA040702003Bar · broken(CAN) DURING CRUISE THE FLIGHT CREW NOTICED SEVERE SURGING ON THE NR 1 ENGINE. THE FUEL FLOW WAS ALSO DROPPING AND SURGING. THE ENGINE WAS SHUT DOWN AND THE PROPELLER WAS FEATHERED. THE AIRCRAFT RETURNED TO DEPARTURE. DURING INVESTIGATION MAINTENANCE CREW FOUNJun 30, 2004 · Cvac 440 · Engine Fuel DistributionSDR CA040628005Door · failed(CAN) DURING CLIMB OUT THE FLT CREW NOTICED THE OIL TEMPERATURE RISING TO THE RED LINE. THE OIL COOLER SWITCH WAS SELECTED FROM (AUTO) TO (MANUAL) OPEN WITH NO RESOMNSE. THE OIL TEMPERATURE CONTINUED TO CLIMB. THE ENGINE WAS SHUT DOWN ANDTHE PROP WAS FEATHEREDJun 25, 2004 · Cvac 440 · Engine Oil Temperature RegulatorSDR MV1R04231Switch · intermittentLT MLG DOWN AND LOCKED LIGHT INTERMITTENT. PERFORMED GEAR SWING AND PROBLEM VERIFIED. LT MAIN GEAR SWITCH INTERNAL WIRING LOOSE AT MOUNTING LUGS. INSTALLED NEW LOCK WASHERS AND RE TORQUED. RETRACTION CHECKS NORMAL IAW MM.Jun 16, 2004 · N39 · Cvac 440 · Landing Gear Position and WarningSDR JRAA0520042Floorbeam · corrodedDURING A SCID INSPECTION 53-20, CORROSION WAS FOUND ON FLOORBEAM AT STA 681.0 RT SIDE AT BELTFRAME. AN AREA OF APPROX 3 INCHES X 5 INCHES ON THIS FLOORBEAM WAS FOUND CORRODED AT BELTFRAME ATTACH POINT AROUND RIVETS. THE CORROSION HAD PROGRESSED THROUGH 50 PEMay 20, 2004 · N587CA · Cvac 440 · Fuselage Main, Floor BeamSDR JRAA0520041Floorbeam · corrodedDURING A SCID INSPECTION 53-20, A MISSING RIVET HEAD WAS FOUND AT STA 712.0. RT SIDE AT THE FLOORBEAM TO BELTFRAME ATTACH POINT. CORROSION WAS FOUND UNDER RIVET HEAD. NO OTHER RIVETS WERE FOUND TO BE CORRODED AT THIS TIME. RIVET REPLACEMENT IN PROGRESS AT May 20, 2004 · N587CA · Cvac 440 · Fuselage Main, Floor BeamSDR 15HA0358005Smoke · detectedCREW NOTICED SMOKE IN THE COCKPIT AND CARGO COMPARTMENT JUST AFTER RT ENG WAS STARTED IN PREP FOR THE REGULARLY SCHEDULED FLIGHT. ENG WAS SHUTDOWN AND INSPECTED. NOTHING OUT OF ORDINARY WAS DISCOVERED. MECHANIC HAD CREW DISCONNECT EDC AND ENG WAS RESTARTED.May 18, 2004 · N582P · Cvac 440 · Air Distribution SystemSDR 15HA0458004Compressor · damagedDURING THE DESCENT, AT APPROX 12,000 FT, THE CREW HEARD A LOUD BANG A MOMENT LATER, THE LT FIRE WARNING LIGHT ILLUMINATED AND THE CREW (E) HANDLED THE ENGINE. THE AC MADE AN UNEVENTFUL LANDING. INSPECTION OF THE LT ENGINE HAS REVEALED THE PRESENCE OF A PIECFeb 21, 2004 · N582P · Cvac 440 · Turbine Engine Compressor SectionSDR 2004FA0000219O-Ring · cutAT CRUISE FLIGHT NR 1 PROP EXPERIENCED RPM FLUCTUATIONS. AS A PRECAUTIONARY MEASURE, PROP WAS FEATHERED. PILOT LANDED UNEVENTFULLY. FOUND REGULATOR TO PROP, OIL TRANSFER TUBE, O-RING CUT. INSTALLED NEW O-RING. GROUND RUN FUNCTIONAL AND LEAK CHECKS GOOD.Jan 13, 2004 · N49 · Cvac 440 · Propeller Controlling SystemSDR CA040113011Drive Assy · stripped(CAN) AFTER PROPS WENT OUT OF SYNC, ENG DRIVEN COMP LOW OIL LIGHT ILLUMINATED. EDC DISCONNECT WAS SELECTED, FLUCTUATING GB OIL PRESSURE WAS OBSERVED. PRESS FLICKERED FROM 200 PSI TO 120 PSI ABOUT EVERY 5 SECONDS. SHUTDOWN CARRIED OUT, AC RETURNED TO BASE OEI.Dec 1, 2003 · Cvac 440 · Turbine Engine Reduction GearSDR CA030718003Actuator · misoverhauled(CAN) RECIEVED ACTUATOR THROUGH OUR SUPPLIER. UPON INSTALLATION, FOUND IT BINDING. REMOVED IT AND FOUND THAT TWO SEPERATE CABLES THIS UNIT HAS WERE GOING THROUGH THE SAME PULLEY WHICH LEFT THE OTHER PULLEY NOT IN USE AND BINDING THE UNIT AS WELL AS DAMAGING TJul 18, 2003 · Cvac 440 · Landing Gear Steering SystemSDR I5HA0358003Engine · malfunctionedON THE TAKEOFF ROLL DEPARTING CVG, EN ROUTE TO CLE THE LEFT ENGINE WOULD ONLY PRODUCE 888 DEGREES, NOMINAL IS 971 DEGREES. THE PILOT ABORTED THE TAKEOFF. THE TEMPERATURE DATRUM (TD) SYSTEM WAS NULLED AND FULL POWER WAS THEN AVAILABLE. THE TD SYSTEM WAS DEFEMay 7, 2003 · N582P · Cvac 440 · Engine (Turbine/Turboprop)SDR 15HA0358002Line · brokenWHILE EN ROUTE BETWEEN CVG AND PIT, THE CAPTAIN NOTICED A DROP FROM 65 PSI TO 50 PSI IN THE LEFT POEWR SECTION OIL PRESSURE, FLUCTUATING REDUCTION GEARBOX OIL PRESSURE AND A THREE GALLON DROP IN OIL QTY. THE CAPTAIN PULLED THE LEFT 'E' HANDLE AND SECURED THE Apr 23, 2003 · N582P · Cvac 440 · Turbine Engine Oil SystemSDR NQ52003F00000Support Bracket · crackedAPPROX .2500 CRACK DETECTED IN WEB/FLANGE RADIUS OF AFT TEE OF SUPPORT BRACKET ASSEMBLY FOR ATTACHMENT OF MAIN ENTRANCE DOOR ACTUATOR. THIS TEE BRACKET IS ATTACHED TO THE FORWARD FACE OF FUSELAGE BELTFRAME AT FS 176.50, STRINGER L-26 AND IS APPROX 4 INCHES LOJan 29, 2003 · N51255 · Cvac 440 · Fuselage Miscellaneous StructureSDR BKJ2003F00000Brake Assy · leakingDURING LANDING CHECK, UPON ARRIVAL TO AIRPORT. PILOTS NOTICED LOW HYDRAULIC RESEVOIR LEVEL. TOWER WAS NOTIFIED AND A NORMAL LANDING WAS MADE. AS A PRECAUTION, THE AIRCRAFT WAS TOWED TO PARKING. INSPECTION REVEALED A LEAKING BRAKE ASSEMBLY.Jan 11, 2003 · N24DR · Cvac 440 · Landing Gear Brake SystemSDR CA021007011Windshield · failed(CAN) ON CLIMB OUT OF YUL, LT WINDSHIELD SHATTERED. AIRCRAFT DEPRESSURIZED AND CAME BACK TO MONTREAL. UNABLE TO ESTABLISH THE REASON FOR WINDSHIELD SHATTERED. WINDSHIELD REPLACED AND AIRCRAFT RETURNED TO SERVICE.Sep 13, 2002 · Cvac 440 · Flight Compartment WindowsSDR CA021104006Wire · chafed(CAN) PILOT REPORTED THAT BETA LIGHT WAS 'ON' DURING TAKEOFF ATTEMPT, PILOT ABORT TAKEOFF. MAINTENANCE INVESTIGATION FOUND THAT, BETA LIGHT AND THE FEATHER SOLENOID ENERGIZE. FURTHER INVESTIGATION FOUND THAT WIRING WAS CHAFING ON THE RT RADIO RACK AFT OF THE Jul 26, 2002 · Cvac 440 · Turbine Engine System WiringSDR NQ52002F00000Intercostal · crackedSLIGHT SURFACE CRACKING DETECTED IN THE RADIUS OF INTERCOSTAL (TEE) PN3403310252-21 (FORWARD RIGHT ESCAPE HATCH FRAME). INTERCOSTAL IS PART OF FUSELAGE BELTFRAME ASSEMBLY AT FS 334.749 AND PROVIDES THE FORWARD, VERTICAL SEATING SURFACE FOR THE ESCAPE HATCH.Jul 9, 2002 · N51255 · Cvac 440 · Fuselage Miscellaneous StructureSDR CA020624006Socket · burned(CAN) DURING CLIMBOUT, THE FLIGHT ATTENDANT HAD INFORMED THE CAPTAIN THAT SMOKE WAS EMITTING FROM AN OVERHEAD ISLE LIGHT (NUMBERS 3 AND 4) IN ROWS 4 AND 5. THE OVERHEAD LIGHT SWITCH HAD ALREADY BEEN PLACED IN THE OFF POSITON AT THIS POINT. WHEN THE FLIGHT ATJun 13, 2002 · Cvac 440 · Flight Compartment LightingSDR CA010809006Pump · failed(CAN) EMERGENCY LANDING WITH SMOKE IN COCKPIT. FOUND ELECTRIC HYDRAULIC PUMP BYPASSING THRU CASE DRAIN AND PUMP DEVELOPING 2,700 PSI ONLY. AFTER INSPECTION AIRCRAFT WAS FERRIED TO MAINTENANCE BASE WITH GEAR DOWN AND PUMP OFF. AC PUMP REPLACED. MULTIPLE GEAR REJul 25, 2001 · Cvac 440 · Hydraulic Pump (Electric/Engine), MainSDR CA010726038Insulator · damaged(CAN) FOUND INSULATOR MISSING ON SERVICE CHECK NEW PART INSTALLED. NO OTHER PROBLEM FOUND AND A/C RETURNED TO SERVICE. LT ENGINE REAR SCAVENGE PUMP INSULATOR WAS MISSING IT HAD BEEN REPORTED BY GROUND PEOPLE THAT A PART FALL FROM AIRCRAFT ON APPRAOCH TO LAND IJun 30, 2001 · Cvac 440 · Engine Oil Distribution (Airframe Furnished)SDR 20010312CW015Engine · failedINTERNAL ENGINE FAILURE IN CRUISE FLIGHT, UNKNOWN SPECIFIC CAUSE PENDING TEARDOWN.Feb 10, 2001 · N24DR · Cvac 440 · Engine (Turbine/Turboprop)SDR CA010103011Receptacle · shorted(CAN) FOLLOWING TAKEOFF NR1 AND NR2 V.H.F. UNABLE TO TRANSMIT OR RECEIVE. AIRCRAFT LANDED AT AIRPORT. CAPTAINS MICROPHONE JACK REPLACED. SYSTEMS TESTED SERVICEABLE. AIRCRAFT RELEASED FOR FLIGHT WITH NO FURTHER REPORT.Nov 21, 2000 · Cvac 440 · VHF Communications System
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