N255CA, cancelled Aug 23, 2013

Service difficulty reports · 47

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
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 n_number = 'N255CA' AND deregistration_id = 'N255CA-2013-08-23'
  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 COMA9910054Connector · looseLANDING GEAR SELECTOR LOCK DID NOT RELEASE AFTER TAKEOFF. SECURED LOOSE AIR/GROUND SENSOR WIRING CONNECTION (PO316).Apr 3, 1999 · N255CA · Emb EMB120RT · Landing Gear Retraction/Extension SystemSDR COMA9910049Sequence Valve · leakingHYDRAULIC LEAK, RIGHT HAND WHEEL WELL. REPLACED O RING AT DOOR SEQUENCE VALVE.Mar 29, 1999 · N255CA · Emb EMB120RT · Landing Gear Door Retract SectionSDR COMA9910013Door · not latchedDOOR WARNING DURING TAKEOFF. FOUND FUEL SERVICE DOOR OPEN, CLOSED AND LATCHED DOOR.Jan 16, 1999 · N255CA · Emb EMB120RT · Fluid Service DoorsSDR COMA9810247Door · not latchedDOOR WARNING DURING TAKEOFF. SINGLE POINT FUEL SERVICE DOOR NOT LATCHED. SECURED DOOR.Nov 1, 1998 · N255CA · Emb EMB120RT · Fluid Service DoorsSDR COMA9810145Beam · corrodedDURING AIRCRAFT MAINTENANCE, CORROSION WAS FOUND ON THE FUSELAGE FORWARD CABIN FLOOR SUPPORT STRUCTURE CENTER OMEGA BEAM. THE OMEGA BEAM WAS REPAIRED PER AERODESIGN REPORT NR 1957-5, REV IR, 6-23-98.Jun 24, 1998 · N255CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810144Strap · corrodedDURING AIRCRAFT MAINTENANCE, CORROSION WAS FOUND ON THE FUSELAGE FORWARD CABIN FLOOR SUPPORT STRUCTURE CENTER BUTT STRAP. THE BUTT STRAP WAS REPLACED PER AERODESIGN REPORT NR 1671-1, REV A, 1-28-97.Jun 24, 1998 · N255CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810143Tee Section · corrodedDURING AIRCRAFT MAINTENANCE, CORROSION WAS FOUND ON THE FUSELAGE FORWARD CABIN FLOOR SUPPORT STRUCTURE RIGHT HAND T-SECTION AT FRAME 16. THE T-SECTION WAS REPLACED PER SRM STANDARD PRACTICES.Jun 24, 1998 · N255CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810142Tee Section · corrodedDURING AIRCRAFT MAINTENANCE, CORROSION WAS FOUND ON THE FUSELAGE FORWARD CABIN FLOOR SUPPORT STRUCTURE LEFT HAND T-SECTION AT FRAME 16. THE T-SECTION WAS REPLACED PER SRM STANDARD PRACTICES.Jun 24, 1998 · N255CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810141Strap · corrodedDURING AIRCRAFT MAINTENANCE, CORROSION WAS FOUND ON THE FUSELAGE FORWARD CABIN FLOOR SUPPORT STRUCTURE CENTER BUTT STRAP. THE BUTT-STRAP WAS REPLACED PER SRM STANDARD PRACTICES.Jun 24, 1998 · N255CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9810124Fcu · malfunctionFLAP AND ADVANCED SWS INDICATIONS ON MAP. REPLACED THE FLAP CONTROL UNIT.May 19, 1998 · N255CA · Emb EMB120RT · Trailing Edge Flap Control SystemSDR COMA9810122Hose · leakingLOW OIL PRESSURE WARNING ON RIGHT HAND ENGINE INFLIGHT SHUTDOWN. REPLACED OIL COOLER HOSE ASSEMBLY THAT WAS LEAKING DUE TO CHAFING DAMAGE.May 14, 1998 · N255CA · Emb EMB120RT · Engine Oil CoolerSDR COMA9810083Sensor · dirtyTHE LT MLG INTRANSIT LIGHTS REMAINED ON AFTER GEAR RETRACTION. LANDING GEAR WAS CYCLED AND 2ND RETRACTION WAS NORMAL. COULD NOT DUPLICATE DISCREPANCY. CLEANED INDICATION SENSORS AND CONNECTIONS. AIRCRAFT RETURNED TO SERVICE.Mar 30, 1998 · N255CA · Emb EMB120 · Landing Gear Position and WarningSDR COMA9810049Spinner Bulkhead · crackedDURING PREFLIGHT INSPECTION, THE RIGHT PROPELLER SPINNER BULKHEAD WAS FOUND TO BE CRACKED APPROXIMATELY 1.5 INCH ALONG THE BULKHEAD OUTER WALL BEHIND BLADE NR 2. AIRCRAFT WAS FERRIED BACK TO CVG HANGAR AND BULKHEAD REMOVED FOR REPAIR. DAMAGE APPEARS TO BE DUMar 2, 1998 · N255CA · Emb EMB120RT · Propeller Spinner SectionSDR COMA9710498Sensor · defectiveLANDING GEAR DID NOT EXTEND WHEN SELECTED DOWN. EMERGENCY SYSTEM USED TO LOWER LANDING GEAR. REPLACED DEFECTIVE RT MLG DOWNLOCK PROXIMITY SENSOR.Dec 15, 1997 · N255CA · Emb EMB120RT · Landing Gear Retraction/Extension SystemSDR COMA9710415Stator · crackedDURING TEARDOWN OF BRAKE ASSY P/N 2-1585, THE ACCESSORY SHOP FOUND THE NUMBER ONE STATOR CRACKED. OVERHAULED BRAKE.Sep 19, 1997 · N255CA · Emb EMB120RT · BrakeSDR COMA9710372Tee Section · corrodedDURING 4C INSEPCTION TASK 5320-151-01I, REVEALED RIGHT T-SECTION AT FRAME 28 TO BE CORRODED. REMOVED CORRODED T-SECTION AND INSTALLED SERVICEABLE PART USING EMB SRM STANDARD PRACTICES CHAPTER 51.Aug 12, 1997 · N255CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710371Sill · corrodedDURING 4C INSPECTION TASK 5330-161-01I, REVEALED RIGHT CARGO COMPARTMENT SILL TO BE CORRODED BEYOND LIMITS. REMOVED SILL AND INSTALLED SERVICEABLE SILL USING EMB SRM STANDARD PRACTICES CHAPTER 51.Aug 12, 1997 · N255CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710370Floorbeam · corrodedDURING 4C INSPECTION TASK 5320-151-01I, REVEALED RIGHT FLOORBEAM AT FRAME 33 TO BE HEAVILY CORRODED. REMOVED CORRODED PART AND INSTALLED SERVICEABLE PART USING EMB SRM STANDARD PRACTICES CHAPTER 51 FOR LIKE TO LIKE PART REPLACEMENT.Aug 12, 1997 · N255CA · Emb EMB120RT · Fuselage Main, Floor BeamSDR COMA9710369Angle · corrodedDURING 4C INSPECTION TASK 5320-151-01I, REVEALED AFT EMERGENCY EXIT GUIDE PIN FITTINGS TO HAVE CORROSION BETWEEN FITTINGS AND THE EXIT SILL LOWER ATTACHE ANGLE. FURTHER INVESTIGATION REVEALED THAT THERE IS NO PRIMER OR SEALANT BETWEEN OR ON THESE PIECES. REPAug 12, 1997 · N255CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710368Fitting · corrodedDURING 4C INSPECTION TASK 5320-151-01I, REVEALED AFT EMERGENCY EXIT GUIDE PIN FITTINGS TO HAVE CORROSION BETWEEN THE FITTINGS AND THE EXIT SILL LOWER ATTACH ANGLE. FURTHER INVESTIGATION REVEALED THAT THERE IS NO PRIMER OR SEALANT BETWEEN OR ON THESE PIECES. Aug 12, 1997 · N255CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9710332Solenoid · failedON C-CHECK TASK 35-09, THE PASSENGER OXYGEN MASKS AT SEAT 1BC FAILED TO DEPLOY. THE OXYGEN MASK DOOR SOLENOID AT THAT LOCATION WAS REPLACED, SYSTEM TESTS NORMAL.Jul 17, 1997 · N255CA · Emb EMB120RT · Passenger Oxygen SystemSDR COMA9710181Connector · brokenLANDING GEAR WOULD NOT RETRACT. REPLACED DEFECTIVE WIRING CONNECTOR AT RT MLG UPLOCK.Mar 17, 1997 · N255CA · Emb EMB120RT · Landing Gear Retraction/Extension SystemSDR COMA9710099Pitchlock Screw · damagedPROPELLER ASSEMBLY REMOVED FROM AIRCRAFT DUE TO BEING STRUCK BY LAVORATORY CART WHILE STATIC ON AIRCRAFT RAMP. DURING PROPELLER IMPACT INSPECTION ACTUATOR FEATHER STOP TAB WAS FOUND TO BE DISPLACED APPROXIMATELY .125 FEET. ACTUATOR S/N 20383 WAS SUBSEQUENTLYFeb 3, 1997 · N255CA · Emb EMB120RT · Propeller Controlling SystemSDR COMA9710088Rollers · dirtyOUTBOARD FLAPS FAILED TO RETRACT. REPLACED THE ROLLERS ON THE RT OUTBOARD FLAP.Jan 25, 1997 · N255CA · Emb EMB120RT · Leading Edge DevicesSDR COMA9710047Flap Tracks · dirtyFLAP DISAGREEMENT AFTER TAKEOFF. CLEANED LEFT OUTBOARD FLAP TRACKS.Jan 20, 1997 · N255CA · Emb EMB120RT · Trailing Edge FlapsSDR COMA9710039Flap · bentFLAP FAIL WARNING. REPLACED LEFT OUTBOARD FLAP, OPERATIONAL CHECK GOOD.Jan 16, 1997 · N255CA · Emb EMB120RT · Trailing Edge FlapsSDR COMA9710030Roller · malfunctionedFLAP DISAGREEMENT UPON FLAP RETRACTION AFTER TAKEOFF. REPLACED LT OUTBOARD FLAP ROLLERS 4 EACH. OPERATIONAL CHECK GOOD.Jan 13, 1997 · N255CA · Emb EMB120RT · Trailing Edge FlapsSDR COMA9710025Fuel Door · looseDOOR LIGHT ON MAP CAME ON DURING TAKEOFF. RESECURED FUEL DOOR FASTENERS.Jan 12, 1997 · N255CA · Emb EMB120RT · Fluid Service DoorsSDR COMA9610256Stringer · crackedINSPECTION REVEALED A CRACK IN THE RIGHT NACELLE LT STRINGER 1. THE STRINGER WAS REPAIRED PER AERODESIGN REPORT NR 2000-1, DATED 8-17-96.Aug 19, 1996 · N255CA · Emb EMB120RT · Nacelle/Pylon, Longeron/StringerSDR COMA9610250Butt Strap · corrodedINSPECTION REVEALED CORROSION ON THE FORWARD CABIN FLOOR SUPPORT OM26A BEAM BUTT STRAP ON THE LEFT SIDE GALLEY AREA. THE BUTT STRAP WAS REPLACED WITH A NEW PART PER EMB120 5RM STANDARD PRACTICES.Aug 19, 1996 · N255CA · Emb EMB120RT · Fuselage Miscellaneous StructureSDR COMA9610240Hyd Syst · moisture contamRT HYDRAULIC RESERVOIR LOW PRESSURE WARNING ILLUMINATED. DRAINED MOISTURE FROM RESERVOIR, SYSTEM CHECK NORMAL.Aug 3, 1996 · N255CA · Emb EMB120RT · Hydraulic System, MainSDR COMA9610171Overheat Switch · defectiveRT BLEED AIR DUCT OVERHEAT WARNING CAME ON DURING FLIGHT. REPLACED DEFECTIVE DUCT OVERHEAT SWITCH.Jun 8, 1996 · N255CA · Emb EMB120RT · Pneumatic Indicating SystemSDR COMA9610144Sig Cond Unit · malfunctionAUTO FEATHER SYSTEM WILL NOT TEST OR ARM. REPLACED THE RT ENGINE SIGNAL CONDITIONER UNIT.May 15, 1996 · N255CA · Emb EMB120RT · Propeller Controlling SystemSDR COMA9610070Prox Sensor · defectiveTAKEOFF TRIM AURAL WARNING SOUNDED DURING TAKEOFF. TRIM WAS CONFIRMED IN THE GREEN BAND. REPLACED THE LT ELEVATOR TRIM PROXIMITY SENSOR.Feb 7, 1996 · N255CA · Emb EMB120RT · Central WarningSDR COMA9610072Hose Assy · leakingRT ENGINE IS LEAKING FUEL. REPLACED THE MOTIVE FLOW FUEL RETURN HOSE AND FITTING AT THE ENGINE HMU, DUE TO DAMAGED THREADS.Feb 6, 1996 · N255CA · Emb EMB120RT · Engine Fuel DistributionSDR COMA9610045Aural Warn Unit · malfunctionedTAKEOFF AURAL WARNING SOUNDED DURING TAKEOFF ROLL. REPLACED THE AURAL WARNING UNIT.Jan 28, 1996 · N255CA · Emb EMB120RT · Central WarningSDR COMA9610040Pump Hyd · failedRT ELECTRIC HYDRAULIC PUMP IS INOP. REPLACED THE RT ELECTRIC MOTOR DRIVEN HYDRAULIC PUMP.Jan 25, 1996 · N255CA · Emb EMB120RT · Hydraulic Pump (Electric/Engine), MainSDR COMA9610006Vsi · defectivePILOTS VSI TUBE BLANK. REPLACED THE 1VA-81A TA/VS1.Jan 9, 1996 · N255CA · Emb EMB120RT · Rate of Climb IndicatorSDR COMA9512040Rollers · defectiveFLAP DISAGREEMENT WARNING DURING TAKEOFF CLIMB. REPLACED THE OUTBD FLAP SECTION ROLLERS.Dec 23, 1995 · N255CA · Emb EMB120RT · Trailing Edge Flap Control SystemSDR COM11952Power Wire · failedSTRONG SMELL OF ELECTRICAL BURNING IN COCKPIT AREA. FOUND BURNED GALLEY POWER WIRE. SECURED POWER TO GALLEY BY PULLING BREAKERS AND PLACED ON DEFERRED MAINT LIST.Aug 13, 1995 · N255CA · Emb EMB120RT · Electrical Power SystemSDR COM11905Computer · defectiveDURING TAKEOFF ROLL, THE STALL WARNING CAME ON. REPLACED STALL WARNING COMPUTER.May 26, 1995 · N255CA · Emb EMB120RT · Stall Warning SystemSDR COM11878Power Lever · wornCREW REPORTED, THAT POWER LEVERS WERE NOT EVEN AT FLIGHT IDLE STOP. THE RT POWER LEVER FLIGHT IDLE STOP PIN AND ROLLER WERE FOUND TO BE WORN OVER 50 PERCENT. THE RT POWER LEVER ASSY WAS REPLACED.Apr 24, 1995 · N255CA · Emb EMB120RT · Power LeverSDR COM11845Trim Actuator · bindingELEVATOR TRIM IS BINDING. REPLACED THE RT ELEVATOR TRIM ACTUATOR.Mar 31, 1995 · N255CA · Emb EMB120RT · Elevator Tab Control SystemSDR COM11798Angle · crackedDURING INSPECTION TASK 5530-324-03I AND 5530-324-02I, VERTICAL STABILIZER TO FUSELAGE ANGLE WAS FOUND TO BE CRACKED. REPLACED ANGLE IAW AERODESIGN REPORT 1446-1 AND EMB SRM.Feb 23, 1995 · N255CA · Emb EMB120RT · Vertical StabilizerSDR COM11783Swivel · leakingHYDRAULIC LEAK, LEFT MLG. TIGHTENED FITTINGS ON HYDRAULIC SWIVEL.Feb 12, 1995 · N255CA · Emb EMB120RT · Landing Gear Retraction/Extension SystemSDR COM11777Swivel · leakingHYDRAULIC LEAK, LEFT MLG. REPLACED LEAKING BRAKE LINE SWIVEL.Feb 12, 1995 · N255CA · Emb EMB120RT · Landing Gear Brake SystemSDR COM11738Prox Sensor · defectiveLT MLG GREEN SAFE LIGHT IS INOP, AND RED INTRANSIT LIGHT IS ILLUMINATED. REPLACED THE DOWN LOCK PROXIMITY SENSOR.Jan 23, 1995 · N255CA · Emb EMB120RT · Landing Gear Position and Warning
Back to N255CA, cancelled Aug 23, 2013