Fokker F.27MK 500

Service difficulty reports · 64

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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 = 'F27MK500'
  ORDER BY difficulty_date DESC"

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SDR CA090116009Oil System · low pressure(CAN) DURING CRUISE, THE OIL PRESSURE DROPPED BELOW GREEN BAND AND THE CREW ELECTED TO SHUT THE ENGINE DOWN BEFORE THE FLIGHT WAS DIVERTED. A SINGLE ENGINE LANDING FOLLOWED. POST EVENT INSPECTION FOUND A VERY LOW OIL LEVEL AND A RE-START ATTEMPT WAS UNSUCCESJan 8, 2009 · Fokker F27MK500 · Engine Oil Indicating SystemSDR CA081217014Engine · making metal(CAN) DURING T/O CLIMB, THE ENGINE OUT LIGHT CAME ON AND THE CREW ELECTED TO SHUT THE ENGINE DOWN AND RETURN TO THE POINT OF DEPARTURE FOR AN UNEVENTFUL SINGLE LANDING. GROUND INSPECTION SHOWED OIL FILTER BYPASS INDICATORS ACTIVATED AND METAL WAS FOUND ON THEDec 8, 2008 · Fokker F27MK500 · Engine (Turbine/Turboprop)SDR MAC100603Display · failedDURING CRUISE FLT, THE CREW SMELLED A FAINT ELECTRICAL BURNING SMELL AND NOTICED AT THE SAME TIME THAT THE MFD HAD GONE BLANK.Oct 16, 2006 · N725FE · Fokker F27MK500 · Central DisplaySDR MAC10030601Warning Light · illuminatedTHE NR 2 GEAR BOX LOW OIL PRESSURE LIGHT ILLUMINATED IN FLIGHT.Oct 2, 2006 · N725FE · Fokker F27MK500 · Turbine Engine Oil SystemSDR MAC070602Warning Light · illuminatedTHE LT ENGINE GEARBOX LOW OIL PRESSURE LIGHT ILLUMINATED IN FLIGHT 7 MIN AFTER T/O.Jul 15, 2006 · N725FE · Fokker F27MK500 · Turbine Engine Reduction GearSDR MAC070601O-Ring · cutTHE LEFT ENGINE GEARBOX LOW OIL PRESSURE WARNING LIGHT ILLUMINATED DURING DESCENT INTO MBJ.Jul 14, 2006 · N725FE · Fokker F27MK500 · Accessory GearboxesSDR MAC030601Brake Assy · seizedA RIVET SHEARED IN THE BRAKE ASSEMBLY AND LOCKED THE WHEEL CAUSING DAMAGE TO THE TIRE (FLAT).Mar 22, 2006 · N726FE · Fokker F27MK500 · BrakeSDR MAC020601Garlock Seal · leakingON DESCENT THE NR 2 ENGINE GEARBOX OIL PRESSURE RED LIGHT ILLUMINATED.Feb 23, 2006 · N725FE · Fokker F27MK500 · Accessory GearboxesSDR MAC120502Fire Loop · chafedAFTER TAKEOFF, THE CREW HAD A FIRE WARNING ON THE NR 1 ENGINE.Dec 28, 2005 · N726FE · Fokker F27MK500 · Fire DetectionSDR MAC90502Amplifier · shortedAPPROXIMATELY AN HOUR INTO FLT, THE PIC EXPERIENCED SMOKE IN THE COCKPIT. DECLARED AN EMERGENCY AND RETURNED TO MIA. THE LANDING WAS WITHOUT INCIDENT. AFTER INVESTIGATION, THE CAUSE FOR THE SMOKE WAS AN INTERNAL SHORT IN THE INSTRUMENT AMP RACK. THE INSTRUSep 19, 2005 · N705FE · Fokker F27MK500 · Indicating/Recording SystemSDR MAC8501Generator · failedON TAKEOFF FROM POA, THE NR 2 GENERATOR OVERHEAT LIGHT ILLUMINATED. THE PIC DECLARED AN EMERGENCY AND RETURNED TO POA WITHOUT INCIDENT. THE A/C LANDED 100 LBS OVERWEIGHT WITH A SMOOTH LANDING. AFTER LANDING AND TAXIING TO THE RAMP, THE RIGHT NACELLE WAS INSAug 12, 2005 · N713FE · Fokker F27MK500 · DC Generator-AlternatorSDR MAC5403Generator · overtempEN ROUTE THE LEFT GENERATOR INDICATED AND OVERHEAT CONDITION. THE CREW MADE AN EMERGENCY IN POA FOR REPAIRS.Apr 8, 2005 · N716FE · Fokker F27MK500 · DC Generator-AlternatorSDR MAC5402Volt Regulator · failedNR 2 GENERATOR DROPPED OFFLINE DURING CLIMBOUT.Apr 5, 2005 · N716FE · Fokker F27MK500 · DC RegulatorSDR MAC5401Gearbox · leakingEN ROUTE TO GSO FROM ILM THE CREW OBSERVED A MASTER WARNING, THEN THE RIGHT GEAR BOX LIGHT. THE RIGHT ENGINE WAS SHUT DOWN AND THE PIC DECLARED AN EMERGENCY. THE A/C LANDED IN GSO WITHOUT FURTHER INCIDENT.Apr 3, 2005 · N728FE · Fokker F27MK500 · Accessory GearboxesSDR MAC4801Selector Valve · leakingDURING TAXI, PNEUMATIC PRESSURE WENT TO 200 PSI RESULTING IN LOSS OF BRAKES AND STEERING. THE LANDING GEAR SELECTOR VALVE WAS DETERMINED TO HAVE CAUSED THE LOSS OF PNEUMATIC PRESSURE. THE VALVE WAS REPLACED AND THE A/C RETURNED TO SERVICE.Aug 2, 2004 · N718FE · Fokker F27MK500 · Pneumatic Distribution SystemSDR AUS20040485Regulator · sticking(AUS) ELEVATOR CABLE TENSION REGULATOR STICKY IN OPERATION.May 10, 2004 · Fokker F27MK500 · Elevator Control SystemSDR MTNA20043Fire · detectedDURING FLIGHT FDX7145 EZE-POA THE CARGO SMOKE WARNING LIGHT ILLUMINATED. THE THIRD CREW MEMBER OCCUPYING THE JUMP SEAT CHECKED THE CARGO COMPARTMENT AND OBSERVED FLAMES IN THE REAR OF THE AIRCRAFT. THE CREW DECLARED AN EMERGENCY AND THE JUMPSEAT CREW MEMBER Apr 27, 2004 · N715FE · Fokker F27MK500 · Standard Practices/StructuresSDR MTNA20044Fire Loop · openAFTER TOUCHING DOWN IN IND FLIGHT 7201 BNA-IND THE LEFT ENGINE FIRE WARNING ILLUMINATED.THE CREW TAXIED THE AIRCRAFT OFF THE RUNWAY STOPPED THE AIRCRAFT PERFORMED THE ON GROUND EMERGENCY PROCEDURES AND DECLARED AND EMERGENCY WIHT ATC.NO EVIDENCE OF A FIRE WAS Apr 27, 2004 · N721FE · Fokker F27MK500 · Fire DetectionSDR AUS20040099Switch · faulty(AUS) RT ENGINE LOW TORQUE SWITCH FAULTY. WORKSHOP INVESTIGATION FOUND THE FOLLOWING DEFECTS WITH THE SWITCH: SLIGHT DISTORTION ON SWITCH BASE SWITCH CAP O'RING GROOVES SCORED. PIN TERMINAL ASSEMBLY HAD CORROSION ON PINS.Feb 12, 2004 · Fokker F27MK500 · Engine BMEP/Torque IndicatingSDR MTNA20041Boot · detachedAFTER TAKEOFF FROM MEM A VIBRATION WAS DETECTED AND THE AIRCRAFT RETURNED TO MEM. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE LEFT OUTBOARD HORIZONTAL STABILIZER DEICE BOOT HAD SEPARATED FROM THE LEADING EDGE ON TOP FOR ABOUT A 5 FOOT SECTION.Jan 21, 2004 · N725FE · Fokker F27MK500 · Airfoil Anti/De-ice SystemSDR 2003F00620Amplifier · inoperativeON TAKEOFF FROM ANCHORAGE, THE RT ATTITUDE INDICATOR FAILED, RIGHT AFTER ROTATION. THE AIRCRAFT RETURNED TO ANC. NO EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. THE RACK INSTRUMENT AMPLIFIER WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICOct 13, 2003 · N711FE · Fokker F27MK500 · Attitude Gyro and Indicating SystemSDR COEA0301711Selector Valve · malfunctionedAFTER DEPARTING ANC CREW NOTICED WITH GEAR UP AND IN LOCKED POSITION THE MAIN PNEUMATIC PRESSURE LEAKED EXCESSIVELY. CREW ELECTED TO RETURN TO ANC. NO EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED LANDING GEAR SOct 7, 2003 · N711FE · Fokker F27MK500 · Landing Gear Retraction/Extension SystemSDR MTNA20035Clamp · looseON DESCENT INTO KIN THE LT GEARBOX OIL LIGHT CAME ON. THE EMERGENCY CHECK LIST WAS ACCOMPLISHED AND THE ENGINE SHUT DOWN. AN EMERGENCY WAS DECLARED WITH ATC. THE AIRCRAFT LANDED WITH OUT ANY OTHER INCIDENT. MAINTENANCE TROUBLESHOT THE PROBLEM AND FOUND A CLAMPAug 25, 2003 · N709FE · Fokker F27MK500 · Accessory GearboxesSDR MTNA20033Actuator · stuckAFTER TAKEOFF FROM MEM EN ROUTE TO MLU. THE FLIGHT CREW FOUND THE RIGHT FUEL TRIMMER WOULD NOT ADJUST. IT WAS STUCK AT 81 PERCENT. THE CREW DECLARED AN EMERGENCY DUE TO THE NEED TO MAKE A OVERWEIGHT LANDING. THE CREW LANDED THE AIRCRAFT WITH A SMOOTH LANDIJul 8, 2003 · N726FE · Fokker F27MK500 · Fuel Controlling SystemSDR MTNA20032Propeller · malfunctionedIN FLIGHT FROM CRW TO LCK THE LEFT ENGINE AUTO-FEATHERED. AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED UNEVENTFULLY AT LCK. THE CAUSE IS UNKNOWN AT THIS TIME.Apr 2, 2003 · N728FE · Fokker F27MK500 · Propeller Feathering/ReversingSDR MTNA20031Drag Brace · brokenTHE RIGHT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED ON APPROACH INTO EWN. THE FLIGHT CREW PERFORMED THE EMERGENCY LANDING GEAR PRECEDURES AND DID A FLY-BY AT EWN. THE AIRCRAFT WAS DIVERTED TO ISO. THE AIRCRAFT LANDED AT ISO WITH THE RIGHT MAIN LANDING GEARMar 11, 2003 · N712FE · Fokker F27MK500 · Main Landing Gear Strut/Axle/TruckSDR MTNA20021Relief ValveDURING CLIMB OUT FROM SGF. THE RIGHT MLG AND NLG WOULD NOT RETRACT, PNEUMATIC PRESSURE HAD DROPPED TO 400 PSI. THE CREW ELECTED TO RETURN TO SGF. WHEN THE CREW SELECTED GEAR DOWN THE PRESSURE BEGAN TO INCREASE AND WAS AT 1000 PSI. AT SHUT DOWN.Jan 3, 2002 · N717FE · Fokker F27MK500 · Landing Gear SystemSDR MTNA200201Relief ValveDURING CLIMB OUT FROM SGF. THE RIGHT MLG AND NLG WOULD NOT RETRACT, PNEUMATIC PRESSURE HAD DROPPED TO 400 PSI. THE CREW ELCETED TO RETURN TO SGF. WHEN THE CREW SELECTED GEAR DOWN THE PRESSURE BEGAN TO INCREASE AND WAS AT 1000 PSI AT SHUT DOWN.Jan 3, 2002 · N717FE · Fokker F27MK500 · Landing Gear Retraction/Extension SystemSDR MTNA200113Wire · shortedIN FLIGHT FROM MEM TO SDF, THE LEFT ENGINE FIRE INDICATION ILLUMINATED. THE CREW DECLARED AN EMERGENCY AND RETURNED TO MEM. THE AIRCRAFT LANDED WITHOUT ANY OTHER PROBLEMS. MAINTENANCE FOUND TWO BAD FIRE WIRES. MAINTENANCE REMOVED AND REPLACED TWO EACH FIREDec 7, 2001 · N719FE · Fokker F27MK500 · Fire DetectionSDR MTNA200112Selector Valve · leakingON TAKEOFF OUT OF MEM, WHEN THE LANDING GEAR WAS SELECTED UP THE MAIN PNEUMATIC SYSTEM WENT TO ZERO. THE LANDING GEAR WOULD NOT RETRACT. THE CREW DECLARED AN EMERGENCY AND RETURNED TO MEM. THE AIRCRAFT LANDED WITHOUT ANY OTHER PROBLEMS.Nov 28, 2001 · N717FE · Fokker F27MK500 · Landing Gear SelectorSDR MTN2001F00000Connector · looseDURING CLIMB OUT FROM SGF. THE LEFT OIL PRESSURE GAUGE DROPPED TO ZERO THEN FLUCTUATED BETWEEN ZERO AND FIVE PSI. THE CREW PERFORMED THE EMERGENCY SHUT DOWN CHECK LIST. AFTER DECLARING AN EMERGENCY THEY RETURNED TO SGF AND LANDED WITHOUT INCIDENT.Sep 14, 2001 · N718FE · Fokker F27MK500 · Engine Oil PressureSDR MTNA200111Connector · looseDuring climb out from SGF. The left oil pressure gauge dropped to zero then fluctuated between zero and five PSI. The crew performed the emergency shut dowm check list, declared an emergency. The crew returned the aircraft to SGF. and landed with out incident.Sep 14, 2001 · N718FE · Fokker F27MK500 · Engine Oil PressureSDR MTNA200109Fire LoopDuring take off and climb out of LCK. the right engine fire warning light illuminated. The crew performed the emergency check list procedures, declared an emergency and returned to LCK. The aircraft landed with out further incident.Jul 31, 2001 · N716FE · Fokker F27MK500 · Fire DetectionSDR AU001196Skin · delaminated(AUS) RT HORIZONTAL STABILISER LEADING EDGE (LAMINATED TIMBER CONSTRUCTION) BADLY DELAMINATED , THE TIMBER SECTION ROTTED AND THE BONDED SECTION FULL OF WATER. RUBBER BOOT DISBONDED AND INFLATION CELLS PERISHED ON THE TOP SURFACE.Dec 17, 2000 · Fokker F27MK500 · Horizontal Stabilizer StructureSDR 20001204SH008Fire Loop · malfunctionedJUST AFTER TAKEOFF, ENGINE FIRE WARNING ON RIGHT ENGINE. DEFECTIVE FIRE LOOP SEGMENT CAUSING FIRE WARNING INDICATION ONLY. NO FIRE. REPLACED BOTH ENGINE FIRE BOTTLES ON RIGHT ENGINE. ALSO, BLOW-OUT DISCS. (X)Nov 15, 2000 · N284MA · Fokker F27MK500 · Fire DetectionSDR 20001204SH009Rack · crackedPILOTS REPORTED THAT AIRCRAFT STEERING WAS INOPERATIVE. MAINTENANCE FOUND THE STEERING RACK HAD CRACKED AT THE FIRST TOOTH SERRATION. THE STEERING RACK WAS REPLACED. RACK CRACKED IN AN AREA THAT IS SUBJECTED TO RECURRENT MAGNETIC PARTICLE INSPECTIONS EVERY Nov 14, 2000 · N283EA · Fokker F27MK500 · Landing Gear Steering SystemSDR 20001025SH024Lever · brokenPILOT NOTED THE RIGHT BRAKE WAS INOPERATIVE FROM THE PILOT''S SIDE. BRAKE LEVER FOR PILOT''S SIDE BROKE AT FORWARD RIVET HOLE AND WOULD NOT ACTUATE BRAKE CONTROL VALVE. PART SCRAPPED. X)Oct 11, 2000 · N283EA · Fokker F27MK500 · Landing Gear Brake SystemSDR 20000602SH013Bearing · failedCREW REPORTED THE SMELL OF SMOKE IN THE CABIN ON CLIMB-OUT. CREW SELECTED RAM AIR AND SMOKE DISSIPATED. RETURNED TO LAS WHERE REPAIRS COULD BE MADE. FLIGHT ATTENDANT REPORTED SHE HEARD A GRINDING SOUND COMING FROM THE AFT PORTION OF THE CABIN. MAINTENANCE May 15, 2000 · N283EA · Fokker F27MK500 · Cabin Cooling SystemSDR AU990615Duct · cracked(AUS) LEFT CABIN COMPRESSOR AIR DUCT LOCATED BETWEEN THE SILENCER AND THE WING REAR SPAR P/N 8540-153-569 CRACKED AROUND THE FLANGE FOR APPROXIMATELY 85 PERCENT OF THE CIRCUMFERENCE. THE CRACK HAD PENETRATEDTHE FULL DEPTH OF THE FLANGE AND EXHIBITED DELAMINATJul 1, 1999 · Fokker F27MK500 · Air Distribution SystemSDR COEA9901720Switch · malfunctionedDURING TAKEOFF ROLL, THE AUTOFEATHER LIGHT AND BELOW FLIGHT FINE LIGHT ON THE NR 1 ENGINE FLASHED SEVERAL TIMES. PILOT ABORTED TAKEOFF AND TAXIED TO RAMP, NO ASSISTANCE REQUIRED. MAINTENANCE TROUBLESHOT PROP SYSTEM. SERVICED ENGINE OIL AND PERFORMED TWO ENGFeb 1, 1999 · N720FE · Fokker F27MK500 · Propeller Indication SystemSDR 98ZZZM565Line · looseDURING CRUISE, LEFT GEARBOX LOW OIL PRESSURE LIGHT ILLUMINATED. (M)Jul 10, 1998 · N284MA · Fokker F27MK500 · Turbine Engine Oil SystemSDR 98ZZZX2571Combustion Can · crackedDURING A SCHEUDLED INSPECTION, THE NR 1 COMBUSTION CAN ASSY ON THE LEFT ENGINE WAS REJECTED DUE TO AN OUTER CASING BURN-THROUGH NEAR THE AFT END. UPON CAN REMOVAL, THE FLAME TUBE WAS FOUND CRACKED 360 DEGREES AND SEPARATED APPROXIMATELY 4 INCHES - 5 INCHES FRJun 21, 1998 · N284MA · Fokker F27MK500 · Turbine Engine Combustion SectionSDR COEA9802720Fire Loop · malfunctionedDURING TAXI INTO ONT, NR 2 ENGINE FIRE WARNING LIGHT AND BELL CAME ON. NO SIGNS OF SMOKE OR FIRE WERE DETECTED. MAINTENANCE INSPECTED AND TROUBLESHOT SYSTEM. FOUND THE FIRE WIRE SECTION AT INBOARD, LOWER FIREWALL SHORTED. REMOVED AND REPLACED FIRE WIRE SEGFeb 17, 1998 · N720FE · Fokker F27MK500 · Fire DetectionSDR 97ZZZX3928Wire · brokenON TAKEOFF AT ROTATION, THE NOSE GEAR STEERING PRESSURE WARNING LIGHT ILLUMINATED. THE CREW DID NOT RETRACT THE GEAR AND RETURNED TO MAKE AN UNSCHEDULED LANDING. MAINTENANCE FOUND A BROKEN WIRE AT THE STEERING CONVERTER PRESSURE SWITCH. THE WIRE WAS REPAIREDAug 3, 1997 · N283EA · Fokker F27MK500 · Landing Gear System WiringSDR 97ZZZX3926Wiring Harness · chafedON TAKEOFF OUT OF MEM, THE RT PROPELLER AUTOFEATHERED. THE FLIGHT CREW DECLARED AN EMERGENCY AND RETURNED TO MEM WITHOUT ANY OTHER PROBLEMS. THE MECHANIC IN MEM REMOVED AND REPLACED THE FUEL CONTROL AND FUEL PUMP. THIS DID NOT SOLVE THE PROBLEM. AFTER MOREJul 21, 1997 · N727FE · Fokker F27MK500 · Engine Indicating SystemSDR 97ZZZM747Door Frame · crackedDURING AN SCHEDULED INSPECTION, A CRACK WAS FOUND IN THE PASSENGER ENTRY DOOR FRAME STRUCTURE UNDER THE STAIRS AFT ATTACH BRACKET. THE CRACK EXTENDED THROUGH THE THREE BRACKET MOUNTING HOLES AND WAS PROPOGATING AFT. THE TOTAL LENGTH OF THE CRACK WAS APPROX 4Jun 27, 1997 · N284MA · Fokker F27MK500 · Fuselage Miscellaneous StructureSDR 97ZZZX3440Fire Loop · shortedIND/PIA - IN-FLIGHT, THE LEFT ENGINE FIRE WARNING LIGHT CAME ON. THE FLIGHT CREW ACCOMPLISHED THE EMERGENCY CHECK LIST AND LANDED WITHOUT ANY OTHER PROBLEMS. AFTER TROUBLESHOOTING, THE MECHANIC FOUND A BAD FIRE WARNING LOOP. THE SYSTEM CHECKED GOOD IAW THE Jun 4, 1997 · N721FE · Fokker F27MK500 · Fire DetectionSDR 97ZZZX2093Fuel Pump · shaft shearedON CLIMB-OUT OF LCK, THE LEFT ENGINE AUTOFEATHERED. THE CREW DECLARED AN EMERGENCY AND RETURNED TO LCK WITH NO FURTHER PROBLEMS. THE MECHANIC FOUND A SHEARED SHAFT ON THE FUEL PUMP. THE ENGINE CHECKED GOOD IAW THE FOKKER MM AFTER THE FUEL PUMP WAS REPLACED.Apr 29, 1997 · N709FE · Fokker F27MK500 · Engine Fuel PumpSDR 97ZZZX2360Upper Member · crackedINSPECTION FOUND MLG UPPER MEMBER CRACKED. PART TOTAL CYCLES, 56,096. PART TSO CYCLES, 6,712. (X)Apr 4, 1997 · N724FE · Fokker F27MK500 · Main Landing Gear Strut/Axle/TruckSDR 97ZZZX2094Engine · damagedEWR/YMX - EN ROUTE, THE LEFT ENGINE STARTED TO AUTOFEATHER. THE LEFT ENGINE TEMP STARTED TO RISE, THE FLIGHT CREW THEN MANUALLY FEATHERED THE PROP. THE CREW DECLARED AN EMERGENCY AND WAS CLEARED TO LAND IN ALB. THE PILOT TRIED TO RESTART THE ENGINE, BUT IT WFeb 6, 1997 · N721FE · Fokker F27MK500 · Turbine Section
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