Beech C90A

Service difficulty reports · 461

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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 = 'C90A'
  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 G1IA2017020100001Blower Motor · failedTHE PILOT REPORTS WHILE RELOCATING THE AIRCRAFT FROM KLND TO KOGD. DURING CRUISE PORTION OF FLIGHT, NOTED HEATER BLOWER MOTOR STOPPED WORKING, AND SHORTLY THEREAFTER OBSERVED LIGHT SMOKE IN THE COCKPIT, AND AN ELECTRICAL BURNING SMELL. DIVERTED TO KEVW AND LANJan 27, 2017 · N98KS · Beech C90A · Heating SystemSDR J4YR201611021528Skin · crackedDURING INSPECTION OF THE LEFT AILERON, A CRACK WAS NOTED ON THE UPPER SKIN IN THE RADIUS OF THE TRIM TAB HINGE AREA.Nov 2, 2016 · N92RK · Beech C90A · AileronsSDR 2016F00185Actuator · inoperativeNEW PART WOULD NOT ALLOW FOR THE RT. MAIN LANDING GEAR TO INDICATE DOWN AND LOCKED.Sep 14, 2016 · N400EM · Beech C90A · Landing Gear Position and WarningSDR HMGR2016050626405Blower · overheatedCREW REPORTED HEAVY SMOKE IN COCKPIT AND PERFORMED EMERGENCY DECENT IAW CHECKLIST. SUBSEQUENT INSPECTION FOUND VENT BLOWER DISPLAYED HEAT DAMAGE AND APPARENT BEARING FAILURE. ALSO FOUND SUPPLY HOSE TO PILOT'S LT BRAKE MASTER CYLINDER HEAT DAMAGED. REPLACEDApr 29, 2016 · N370U · Beech C90A · Air Distribution FanSDR DDNA2016041400180Bracket · crackedNOTICED CRACK IN RT ELEVATOR TRIM TAB NEAR ACTUATOR BRACKET. DISCONNECTED ACTUATOR FROM TRIM TAB AND FOUND EXCESSIVE MOVEMENT IN BRACKET. UPON FURTHER INSPECTION FOUND FORWARD TWO RIVETS THAT HOLD ACTUATOR ARM TO TRIM TAB HAD SHEARED IN HALF. AND FWD RADIUS OApr 14, 2016 · N119SA · Beech C90A · Elevator StructureSDR DDNR20160414001Arm · crackedNOTICED CRACK IN RT ELEVATOR TRIM TAB NEAR ACTUATOR ARM. DISCONNECTED ACTUATOR AND FOUND EXCESSIVE PLAY IN TRIM TAB ACTUATOR ARM. UPON FURTHER INSPECTION AND DISASSEMBLY FOUND FWD 2 RIVETS THAT FASTEN ACTUATOR ARM TO RIB HORN HAD SHEARED. ALSO FOUND RIB HORApr 8, 2016 · N119SA · Beech C90A · Elevator StructureSDR CA160314009Intercostal · cracked(CAN) DURING AN INSPECTION OF THE PRESSURIZED AREAS OF THE CABIN, BOTH DOOR HANDLE SUPPORT INTERCOSTAL BRACKETS WERE FOUND CRACKED. ONE BRACKET HAD A 1/2 INCH CRACK RADIATING FROM THE CORNER OF THE INSIDE SECTION OF THE FRAME.Mar 14, 2016 · Beech C90A · Passenger/Crew DoorsSDR CA160315016Rib · cracked(CAN) DURING A SCHEDULED INSPECTION OF THE LT ELEVATOR, THE INBOARD RIB WAS FOUND TO BE CRACKED. IT IS BELIEVED THAT THE REASON THE RIB WAS CRACKED WAS DUE TO THE FACT THAT NO WASHERS WERE FOUND UNDER THE NUTS SECURING THE RIB TO THE ELEVATOR TORQUE TUBE. ONCEFeb 15, 2016 · Beech C90A · Elevator, Spar/RibSDR CA160301002Engine · malfunctioned(CAN) THE AIRCRAFT WAS DEPARTING WHEN THE RIGHT ENGINE HAD AN ISSUE DURING LIFT OFF. THE AUTO FEATHER SYSTEM DID NOT FEATHER THE AFFECTED PROPELLER. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO LAND WITHOUT FURTHER INCIDENT. IT WAS FOUND THAT MAINTENFeb 11, 2016 · Beech C90A · Propeller Controlling SystemSDR CA160121020Washer · wrong part(CAN) SUSPECT UNAPPROVED PART. FLAT WASHER P/N 35-105111-3 LOT#M3286BX QTY 1 AND LOT#212191 QTY 3 RECEIVED BY TRANSPORT CANADA, AIRCRAFT SERVICES STORES. ALL 4 WASHERS FOUND NOT TO BE OF PROPER THICKNESS AS PER BEECHCRAFT EMAIL CORRESPONDENCE. WASHERS WERE SUPJan 19, 2016 · Beech C90A · Wing, Fuselage Attach FittingsSDR DDNR20151217001Rib · crackedLEFT OTBD FLAP NOSE RIBS CRACKED AT THE ACTUATOR ATTACH POINTS. FOUND UPON PHASE INSPECTION THROUGH INSPECTION HOLES. FLAP ALSO HAD CRACK MIDWAY IN THE SKIN OF THE L/E.Dec 3, 2015 · N119SA · Beech C90A · Leading Edge DevicesSDR E07A20151202001Actuator · bindsDURING DESCENT ELEVATOR TRIM WOULDN'T MOVE. ONCE ACFT REACHED LOWER ALTITUDE, TRIM WORKED AGAIN. SUSPECT MOISTURE IN ELEVATOR TRIM ACTUATOR MAY HAVE FROZEN. PURGED ELEVATOR TRIM ACTUATOR WITH NEW GREASE. OPERATIONS CHECKED OK. ACFT WAS RETURNED TO SERVICEDec 1, 2015 · N395AS · Beech C90A · Elevator Tab Control SystemSDR CA150923006Lock · missing(CAN) DURING PREPARATION FOR RUN-UP IT WAS NOTICED THAT THE PILOT OXYGEN MASK WAS HALFWAY OUT OF IT`S STORAGE POUCH. WHILE RE-STOWING THE MASK IT WAS NOTICED THAT THE REGULATOR ASSY HAD COME SEPARATED FROM THE MASK ASSY. UPON EXAMINATION IT WAS DISCOVERED THSep 21, 2015 · Beech C90A · Crew Oxygen SystemSDR BGSA2015FA0000454Motor · failedVENTILATION BLOWER MOTOR FAILED AND FILLED COCKPIT WITH SMOKE.Sep 3, 2015 · N70VR · Beech C90A · Air Distribution FanSDR VIB420150805001Vane · brokenTHIRD STAGE VANE AND SHROUD FAILURE IN NR 1 ENGINE.Aug 6, 2015 · N632MT · Beech C90A · Turbine Engine Combustion SectionSDR 2015FA0000258Indicator · tumblesDURING CLIMBOUT, FIVE MINUTES INTO FLIGHT, THE PILOT OBSERVED THE RT ATTITUDE INDICATOR TUMBLED, MADE 180 DEGREE TURN BACK TO MAINTENANCE BASE. ATTITUDE INDICATOR STOPPED ITS TUMBLE AND RIGHTED ITSELF. MX PERFORMED OPS CHECK, FOUND NO DEFECTS NOTED AND COULDJun 1, 2015 · N13GZ · Beech C90A · Attitude Gyro and Indicating SystemSDR 2015F00056Cap · dislodgedFUEL CAP WAS POSSIBLY NOT SEATED PROPERLY, A VISUAL INSPECTION WAS MADE AND TENSION ADJUSTED. OPERATIONAL CHECK FLIGHT COMPLETED WITH NO FURTHER DISCREPANCY NOTED.Mar 31, 2015 · N170SE · Beech C90A · Fuel StorageSDR 2015F00045Cap · out of positionPILOT NOTED FUEL LEAKING FROM CAP AFTER TAKEOFF. PILOT THEN RETURNED TO AIRPORT AND LANDED WITHOUT INCIDENT. CAP WAS INSPECTED AND DETERMINED NOT TO BE SEATED PROPERLY. CAP WAS RESEATED AND TEST FLIGHT SHOWED NO SUBSEQUENT LEAKS.Mar 19, 2015 · N170SE · Beech C90A · Fuel StorageSDR 7AJA2015031500001Brake · brokenAIRCRAFT TOOK OFF FROM AIRPORT WITH NO INDICATION OF ANY DIFFICULTIES IN FLIGHT AND UNEVENTFUL LANDING. UPON PARKING ACFT, PILOT PERFORMED POST FLIGHT INSPECTION AND FOUND RT MLG BRAKE CALIPER BROKEN, ALSO DAMAGES TO RT MLG WHEEL WELL, FUEL LINES IN WHEEL WELLMar 15, 2015 · N587PB · Beech C90A · Main Rotor BrakeSDR CA150213012Screw · bent(CAN) RUDDER PEDAL FALLS FULL FORWARD WITHIN THE ADJUSTMENT RANGE. FOUND THE RUDDER PEDAL ADJUSTING LEVER STOP (SCREW - MS24693-S30) BENT. THIS ALLOWED THE ADJUSTING LEVER (ITEM 55) TO OVER TRAVEL AND ALLOW THE PEDAL ADJUSTING PIN (ITEM 140)TO FULLY DISENGAGE Feb 12, 2015 · Beech C90A · Rudder Control SystemSDR 7AJD2015FA0000062Warning Light · false activationDURING TAXI PILOT OBSERVED ALL ANNUNCIATOR LIGHTS ILLUMINATED WHILE TAXING OUT FOR DEPARTURE, ACFT RETURNED TO PARKING UNEVENTFULLY.Feb 3, 2015 · N438CA · Beech C90A · Central WarningSDR 7AJA20150113010Blower Motor · burned outAFTER LANDING COULD SMELL SOMETHING THAT WAS DESCRIBED AS BURNING CHARCOAL. UPON FURTHER DISCOVERY IT WAS DETERMINED THAT THE BLOWER MOTOR, LOCATED BELOW THE RUDDER PEDALS ON THE LT SIDE, HAD BECOME INOPERATIVE & WAS REPLACED WITH A NEW PART. THE OPERATIONALJan 11, 2015 · N1076K · Beech C90A · Heating SystemSDR 7AJA20141116009Unknown · malfunctionedCRUISING AT 16000 FEET, THE CABIN TEMP KNOB BECAME LOOSE & WAS UNUSABLE. PULLED THE KNOB OFF SO WOULDN'T LOSE IT. MOVED THE CABIN TEMP MODE SELECTOR SWITCH TO MAN HEAT & INCREASED THE TEMP BY HOLDING UP ON THE MANUAL TEMP SWITCH. CONTINUED TO ADJUST THE CABNov 16, 2014 · N1079D · Beech C90A · Heating SystemSDR CA141107006Doubler · cracked(CAN) WHILE UNDERGOING REPAIR FOR THE LT ELEVATOR CRACKED INBD CLOSE OUT RIB, THE STA 36.18 DOUBLER, FOR LT ELEVATOR FRONT SPAR, PN 50-610000-387, WAS FOUND TO BE CRACKED LONGITUDINALLY IN THE UPPER AND LOWER RADII AT THE INBD HINGE ATTACHMENT LOCATION.Nov 7, 2014 · Beech C90A · Elevator StructureSDR CA141107008Rib · cracked(CAN) WHILE COMPLYING WITH A COMPANY FLEET CAMPAIGN CN-681-55-20-035 CONSISTING OF A BORESCOPE INSPECTION OF THE ELEVATOR TORQUE TUBE ATTACHMENT, A CRACK WAS DISCOVERED IN THE LEFT HAND ELEVATOR CLOSE OUT RIB.Nov 6, 2014 · Beech C90A · Elevator, Spar/RibSDR CA141104004Rib · cracked(CAN) WHILE THE ACFT WAS DOWN FOR MAINTENANCE, ALL GEAR REPLACEMENT, LEFT ELEVATOR CLOSE OUT RIB FOUND WITH TWO SIMILAR CRACKS AT THE TORQUE TUBE ATTACHMENT. ONE ON THE UPPER AFT AREA AND ONE ON THE LOWER AFT AREA. THE UPPER CRACK IS GOING THROUGH THE AFT RNov 3, 2014 · Beech C90A · Elevator, Spar/RibSDR CA141029007Bracket · cracked(CAN) DURRING INSPECTION OF AIRCRAFT IT WAS FOUND THAT A CRACK WAS EMINATING FROM AN ATTACH BOLT HOLE FOR ATTACHING TORQUE TUBE. IT WAS NOTED UPPON DISSASSEMBLY OF THE ELEVATOR FOR REPAIR THAT WASHER WAS MISSING FROM UNDER NUT OF TORQUE TUBE P/N 50-610000-234Oct 29, 2014 · Beech C90A · Elevator StructureSDR CA141024016Structure · cracked(CAN) WHILE REPLACING LT OTBD HORIZONTAL STABILIZER ELEVATOR BEARING PLATES 50-620000-352 & 50-620000-354, DUE TO LOOSENESS, NUMEROUS CRACKED PARTS WERE FOUND ON THE LT ELEVATOR. A CAMPAIGN WILL BE ISSUED TO INSPECT THE REMAINDER OF THE FLEET. 50-610000-397 Oct 23, 2014 · Beech C90A · Elevator StructureSDR CA141010013Piston · cracked(CAN) ACTUATOR PISTON FOUND CRACKED WITH APPROXIMATELY A 4.5" CRACK EMANATING FROM THE ROLL PIN HOLE THAT RETAINS PLUG, PN 50-521196-1.Oct 10, 2014 · Beech C90A · Trailing Edge Flap ActuatorSDR CA141009002Piston · cracked(CAN) DURING OPS 1 INSPECTION A CRACK WAS FOUND RUNNING THE LENGTH OF THE PISTON ON THE RIGHT HAND OUTBOARD FLAP ACTUATOR.Oct 8, 2014 · Beech C90A · Trailing Edge Flap ActuatorSDR CA140929008Doubler · cracked(CAN) DURING MAINTENANCE THE FORWARD DOUBLER AT THE FORWARD EMERGENCY EXIT BULKHEAD FS 196 WAS FOUND CRACKED COMPLETELY THROUGH. DOUBLER REPLACED.Sep 29, 2014 · Beech C90A · Fuselage Main, BulkheadSDR 7AJA2014100700590Motor · unknownAFTER DEPARTURE, NOTICED WHAT APPEARED TO BE SPARKS STREAMING FROM THE LT EXTERIOR NOSE PORTION OF THE FUSELAGE. AT APPROXIMATELY A MINUTE THE SPARKS STOPPED. NO OTHER SYMPTOMS WERE NOTICED. ACFT MAINTENANCE FOUND THAT THE AIR CONDITIONING COMPRESSOR MOTOR Sep 22, 2014 · N1083S · Beech C90A · Cabin Cooling SystemSDR CA140822005Feeder Cable · chafed(CAN) DURING A DAILY INSPECTION IT WAS NOTICED THAT THE RT ENGINE STARTER GENERATOR WIRING HARNESS WAS CHAFING AGAINST THE IGNITOR BOX. AFTER REMOVING THE HARNESS, DAMAGE WAS FOUND ON WIRE K70A, B AND C. FURTHER INVESTIGATION SHOWED AN INCORRECT CLAMP SIZE HAug 20, 2014 · Beech C90A · Electrical Power System WiringSDR 7EMA201407310001Bolt · damagedUPON PERFORMING THE 1000 CYCLE LG ACTUATOR CLEVIS INSPECTION THE LT MAIN GEAR ACTUATOR CLEVIS WAS FOUND EXCESSIVELY ELONGATED & THE RETENTION BOLT SEVERELY NOTCHED. DRAG BRACE & BOLT WERE REPLACED.Jul 31, 2014 · N424EM · Beech C90A · Landing Gear Retraction/Extension SystemSDR CA140414002Filter · dirty(CAN) DURING THE OPS-1 INSPECTION AND FOLLOWING THE "SCHEDULED INSPECTION PROGRAM", PHASE 1, MAINTENANCE PRACTICES, LJ-1063 AND AFTER, ITEM F.11.A. PERFORM THE GEAR-UP AND GEAR-DOWN PORT FINGER SCREEN CLEANING PROCEDURE. WHEN THE TECH PULLED THE SCREENS FOR CApr 11, 2014 · Beech C90A · Hydraulic System, MainSDR CA140227003Powerpack · failed(CAN) THE PILOTS REPORTED THAT WHEN THEY SELECTED GEAR UP THE SELECTOR WENT UP BUT THE GEAR DID NOT MOVE. THE 60 AMP MOTOR CIRCUIT BREAKER WAS FOUND TO BE POPPED. WHEN MAINTENANCE RESET THE CIRCUIT BREAKER THE PUMP AND MOTOR OPERATED HOWEVER THE GEAR FAILED TOFeb 27, 2014 · Beech C90A · Hydraulic System, MainSDR CA140212004Piston · cracked(CAN) WHILE DOING ROUTINE MAINTENANCE, WE RETRACTED THE FLAPS AND HEARD A CHATTERING SOUND AT THE TOP OF THE TRAVEL. THE FLAPS WERE DEPLOYED AND WE NOTICED A CRACK ON THE RT OTBD FLAP ACTUATOR PISTON. THE CRACK STARTED AT THE LOWER ROLL PIN HOLE AND WENT UP Feb 11, 2014 · Beech C90A · Trailing Edge Flap ActuatorSDR CA140131002Tube · worn(CAN) DURING A ROUTINE PRE-FLIGHT INSPECTION OF THE OIL LEVEL ON THE LEFT ENGINE, THE FIRST ONE CHECKED, INDICATED THAT OIL NEEDED TO BE ADDED. DURING THE ADDITION OF OIL, IT WAS NOTICED THAT THE INSIDE EDGE OF THE OIL FILLER HAD SOME WEAR MARKINGS BOTH AT THEJan 30, 2014 · Beech C90A · Turbine Engine Oil SystemSDR 7AJA20131227008Engine · malfunctionedPILOT REPORTED THAT WHILE IN ROUTE, SMELLED WHAT HE THOUGHT WOULD BE ENG OIL SMOKE. HE WAS CLOSE TO DESTINATION AT THE TIME SO HE SHUT OFF THE ENG BLEED VLVS & FOUND THE PROBLEM TO GO AWAY. THE ACFT WAS GROUNDED FOR MORE TROUBLESHOOTING & REPAIR. UPON FURTHDec 24, 2013 · N771PD · Beech C90A · Engine (Turbine/Turboprop)SDR CA131205002Arm · separated(CAN) PILOT REPORTED THAT THE RT ENGINE ICE FAIL LIGHT CAME ON IN FLIGHT. MAINTENANCE INSPECTED THE ENGINE AND FOUND THAT THE ACTIVATION ARM HAD SEPARATED FROM THE REAR ICE VANE. THE BOLT THAT HOLDS THE ARM ON HAD BROKEN OFF MID THREADS. THIS ALLOWED THE ARNov 29, 2013 · Beech C90A · Air Intake Anti/De-Ice SystemSDR 7AJA20130919007Warning Light · inoperativeWHILE ON A MX TEST FLIGHT AND ON FINAL APPROACH IT WAS DISCOVERED THAT THE RT MLG DOWN INDICATION LIGHT WAS NOT ILLUMINATED. THE PILOT, AT THAT TIME MADE THE ATTEMPT TO DEPLOY USING EMERGENCY PROCEDURES WITH NO SUCCESS. THE FLY OVER AND GROUND VISUAL INSPECTISep 16, 2013 · N1076K · Beech C90A · Landing Gear Position and WarningSDR 7AJA2013091600001Landing Gear · malfunctionedDURING APPROACH, PILOT EXTENDED LANDING GEAR AND NOTICED NO GREEN LIGHT ON THE RT MAIN GEAR. DECLARED AN EMERGENCY AND MADE AN ATTEMPT TO DEPLOY USING EMERGENCY EXTENSION PROCEDURE. GREEN EXTENDED AND LOCKED LIGHT FAILED TO ILLUMINATE BUT THE EMERGENCY HANDSep 14, 2013 · N1076K · Beech C90A · Landing Gear Retraction/Extension SystemSDR 7AJA20130827006Hsi · unknownSHORTLY AFTER DEPARTURE, EXPERIENCED AN EADI FAILURE, WHILE STAYING IN VFR CONDITIONS RETURNED TO DEPARTURE. TROUBLESHOT THE SYS WHILE RETURNING TO AIRPORT BY CYCLING THE EFIS AND INVERTERS AND WAS NOT ABLE TO GET THE EADI TO COME BACK ON. MECHANIC WAS NOAug 25, 2013 · N771PD · Beech C90A · Attitude and Direction Data SystemSDR CA130826002Motor · failed(CAN) AIR CONDITIONING STOPPED WORKING COMPLETELY. TROUBLESHOOTING FOUND MOTOR DID NOT WORK. REMOVAL SHOWED EXTENSIVE DAMAGE/MELTING OF THE CASE AND INTERNAL COMPONENTS OF THE COMPRESSOR MOTOR.Aug 22, 2013 · Beech C90A · Cabin Cooling SystemSDR 7AJA20130729005Motor · failedDURING APPROACH, PILOT ATTEMPTED TO LOWER MLG AND DISCOVERED IT WOULD NOT FUNCTION, PERFORMED AN EMERGENCY GEAR EXTENSION AND LANDED. FOUND A FLAT OR DEAD SPOT IN THE MLG POWER PACK MOTOR. MOTOR REPLACED AND SYSTEM FUNCTION CHECKED GOOD.Jul 29, 2013 · N3221M · Beech C90A · Landing Gear Retraction/Extension SystemSDR CA130729019Switch · malfunctioned(CAN) ORIGINAL DEFECT, UNSAFE GEAR INDICATION, GEAR HORN SOUNDING WHILE 3 GREEN INDICATING AND RED LIGHT OUT IN GEAR HANDLE ON GO AROUND. LEFT GEAR DID NOT INDICATE RETRACTION. TROUBLESHOOTING PROVED THAT THE SWITCH, PN MS21321-2, WAS NOT OPERATING PROPERLY.Jul 26, 2013 · Beech C90A · Landing Gear Retraction/Extension SystemSDR CA130729018Switch · malfunctioned(CAN) UNSAFE GEAR INDICATION, GEAR HORN SOUNDING WHILE 3 GREEN INDICATING AND RED LIGHT OUT IN GEAR HANDLE ON GO AROUND. LEFT GEAR DID NOT INDICATE RETRACTIION. TROUBLESHOOTING PROVED THAT THE SWITCH, PN MS21321-2, WAS NOT OPERATING PROPERLY. FAILED TO SHOWJul 26, 2013 · Beech C90A · Landing Gear Position and WarningSDR DYVA201307230001Shroud · brokenDURING CRUISE FLIGHT, PILOT THOUGHT HE SAW MOMENTARY FLASHES OF LIGHT REFLECTING OFF OF LT PROP SPINNER. NO ACFT SYS WERE AFFECTED OR PERFORMANCE DETERIORATED IN ANY WAY. FLIGHT & LANDING WAS UNEVENTFUL. INSPECTED ACFT, NO DAMAGES OR ANYTHING OUT OF THE ORJul 21, 2013 · N947AM · Beech C90A · Air Distribution FanSDR 7AJA20130711004Unknown · vibrationTAXI TO RWY, , ADDING POWER FOR TAKEOFF, AT 1000 FT TORQUE ITT WAS AT 670 LE AND 680 RE. AT ROTATION, 95 KNOTS EXPERIENCED STRONG VIBRATION FROM THE SEAT NOT YOKE. AIRPLANE WASN’T PERFORMING NORMALLY, IT COULD BARELY CLIMB, STALL WARNING WAS GOING ON AND OJul 10, 2013 · N1079D · Beech C90A · Fuselage Structure (General)SDR 7AJA20130501003Unknown · malfunctionedPILOT NOTICED OIL PRESSURE & TORQUE INDICATION DROP BELOW SAFE PARAMETERS ON RIGHT ENGINE IN CRUISE FLIGHT, THE ENGINE WAS THEN STOWED. THE PILOT DECLARED AN EMERGENCY AND SAFELY LANDED THE AIRCRAFT.May 1, 2013 · N1076K · Beech C90A · Engine Oil System (Airframe Furnished)
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