Fokker F.27MK 600

Service difficulty reports · 74

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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 = 'F27MK600'
  ORDER BY difficulty_date DESC"

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SDR COEA0805742Connector · dirtyRETURN TO BLOCKS. FLIGHT NR 7757 MAF TO LBB. DURING TAXI OUT TO THE RUNWAY, THE RT ENG OIL PRESSURE GAGE BEGAN TO FLUCTUATE THEN DROPPED INTO THE RED. ACFT WAS SAFELY TAXIED BACK TO BLOCKS. MX FOUND THE CONNECTIONS AT THE OIL PRESS TRANSMITTER DIRTY. CLEAOct 16, 2008 · N742FE · Fokker F27MK600 · Engine Oil System WiringSDR COEA0804742Hose · leakingAIR TURN BACK. DURING CLIMB OUT AT APPROXIMATELY 7500 FT AGL, THE CREW NOTICED THE ODOR OF FUEL IN THE COCKPIT. AIR FLOW FROM THE AIR CONDITIONING SYSTEM WAS TURNED OFF. THE CREW MENTIONED THE ODOR DID NOT GET ANY WORSE AFTER THE A/C SYSTEM WAS TURNED OFF. MAISep 25, 2008 · N742FE · Fokker F27MK600 · Aircraft Fuel Distribution SystemSDR COEA0804703Spar · puncturedMAJOR REPAIR: LT WING FRONT SPAR WEB HAS A PUNCTURE HOLE AT WS 11560. DISCOVERED DURING MAINTENANCE AFTER TAXI INCIDENT. (S) CUT OUT THE DAMAGED AREA ON THE WING FRONT SPAR WEB PLATE. FABRICATED AND INSTALLED A REPAIR PLATE WITH FILLERS. ISSUED FIELD ENGAug 12, 2008 · N703FE · Fokker F27MK600 · Wing SparSDR COEA0803703Valve · failedBRAKE FAILURE. DURING MAINTENANCE TAXI ACFT LOST ALL STEERING AND NORMAL BRAKING FUNCTIONS. EMERGENCY BRAKING ACTIVATION WAS USED TO STOP THE ACFT. (S) TEARDOWN REPORT FROM VENDOR CONFIRMED THAT THE UNIT FAILED TO GIVE AIR PRESSURE. THE RINGS, SEALS, SEATSAug 8, 2008 · N703FE · Fokker F27MK600 · Landing Gear Brake SystemSDR COEA0803742Transmitter · failedABORTED TAKEOFF. FLIGHT 100 GEG. ABORTED TAKEOFF DUE TO LOSS OF TORQUE INDICATION ON LT ENGINE. TAXIED AIRCRAFT BACK TO RAMP WITHOUT INCIDENT. REMOVED AND REPLACED THE LT ENGINE TORQUE TRANSMITTER. (A)Jul 28, 2008 · N742FE · Fokker F27MK600 · Engine BMEP/Torque IndicatingSDR COEA0802742Connector · dirtyRETURN TO BLOCKS. FLT 8777. ON TAXI TO THE RUNWAY THE LT ENGINE OIL PRESSURE GAGE DROPPED TO AN INDICATION OF "0". THE LT ENGINE WAS SHUT DOWN AND THE A/C TAXIED SAFELY BACK TO THE RAMP. DISCONNECTED CONNECTORS AT THE OIL PRESSURE GAGE AND OIL PRESSURE TRAJul 16, 2008 · N742FE · Fokker F27MK600 · Engine Oil System WiringSDR COEA0801742Cover · tornABORTED TAKEOFF. FLT 8777 GEG TO YKM. DURING THE TAKEOFF ROLL THE COPILOT`S AIRSPEED SHOWED NO INDICATIONS. TAKEOFF WAS ABORTED AND THE ACFT TAXIED BACK TO THE RAMP SAFELY. MAINTENANCE FOUND THE PITOT STATIC TUBE HEAD TO BE OBSTRUCTED WITH A SMALL PIECE OFMay 21, 2008 · N742FE · Fokker F27MK600 · Pitot/Static SystemSDR COEA0802703Alternator · failedRETURN TO BLOCKS. FLT NR7276, DURING TAXI TO THE RUNWAY, THE LT ALTERNATOR FAILED. THE AC RETURNED TO THE RAMP (BLOCKS) WITHOUT ANY FURTHUR INCIDENT. LT ALTERNATOR WAS REPLACED ON THE LT ENGINE.Mar 19, 2008 · N703FE · Fokker F27MK600 · AC Generation SystemSDR COEA0801702Gyro · failedRETURN TO BLOCKS. FLIGHT NR 7276 ITC TO AFW. WHILE PREPAIRING FOR DEPARTURE THE CREW DISCOVERED THE CAPT HEADING AND SITUATION INDICATOR (HSI) COMPASS CARD WAS SPINNING ERRATICALLY. THE CREW REQUESTED TO RETURN TO THE RAMP, UPON WHICH TIME THE HSI COMPASS CMar 14, 2008 · N702FE · Fokker F27MK600 · Attitude Gyro and Indicating SystemSDR COEA0703742O-Ring · leakingAIR TURN BACK, FLT NR 7777. AFTER TAKE-OFF CREW OBSERVED LOW OIL PRESSURE ON THE RT ENGINE. AIRCRAFT RETURNED TO DEPARTURE. LANDING WAS MADE WITH BOTH ENGINES RUNNING. FOUND OIL TRANSFER TUBE LEAKING ON THE RT SIDE OF THE ENGINE (BEHIND FEATHERING PUMP). Aug 28, 2007 · N742FE · Fokker F27MK600 · Turbine Engine Oil SystemSDR COEA0701703Connector · loose(AIR TURNBACK) TURNING THE TAKEOFF ROLL, THE CREW NOTICED THE NR 1 ENGINE OIL PRESSURE FLUCTUATING BETWEEN YELLOW, RED AND ZERO, ALL OTHER INDICATIONS WERE NORMAL. A NORMAL TAKEOFF WAS COMPLETED AND THE CREW ELECTED TO RETURN TO BASE. MAINTENANCE CLEANED ANDJul 2, 2007 · N703FE · Fokker F27MK600 · Engine Oil System WiringSDR COEA0702742Transmitter · malfunctionedABORTED TAKEOFF, LEFT ENGINE INDICATED ZERO TORQUE AT TAKEOFF AND TAXI POWER SETTINGS. AIRCRAFT RETURNED TO RAMP AT GEG. MAINTENANCE REMOVED AND REPLACED LT TORQUE TRANSMITTER, INSPECTED INLET OIL LINE AND BLEED TRANSMITTER. AIRCRAFT RETURNED TO SERVICE. (Feb 20, 2007 · N742FE · Fokker F27MK600 · Engine Indicating SystemSDR COE2005F00002Inverter · inoperativeDEPARTURE, ENROUTE, NR 1 INVERTER WENT OFF LINE AND WOULD NOT COME BACK ON. CREW REPORTED A STRONG BURNING ODOR BUT NO SMOKE. AIRCRAFT DIVERTED. THE NR 1 INVERTER CB WAS POPPED. THE NR 1 INVERTER WAS REMOVED AND REPLACED. THE AIRCRAFT WAS RETURNED TO SERVOct 3, 2005 · N741FE · Fokker F27MK600 · AC InverterSDR COE2005F00000Wire Harness · inoperativeNR 2 TGT FLUCUTATED BETWEEN 0 AND 600 DEGREES IN FLIGHT. AIRCRAFT RETURNED TO AIRPORT. NO EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. FOUND BROKEN WIRE ON CONNECTOR PLUG BACKSHELL AT FIREWALL. ENTIRE HARNESS WAS REPLACED. AIRCRAFT WAJan 20, 2005 · N741FE · Fokker F27MK600 · Engine Indicating System WiringSDR COE2004F00001Alternator · failedON CLIMB OUT, RT ALTERNATOR FAIL LIGHT CAME ON. AIRCRAFT RETURNED TO DEPARTURE. NO EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RT ALTERNATOR. AIRCRAFT WAS RETURNED TO SERIVCE.Nov 3, 2004 · N702FE · Fokker F27MK600 · AC Generation SystemSDR 2004F00296Indicator · malfunctionedDURING CLIMB-OUT FROM SEA, NR 2 TGT INDICATOR FLUCTUATED BETWEEN 0 AND 8000 DEGREES. FLIGHT RETURNED TO SEA FOR TROUBLESHOOTING. MAINTENANCE REPLACED THE NR 2 TGT INDICATOR. AIRCRAFT WAS RETURNED TO SERVICE. (M)Jun 25, 2004 · N702FE · Fokker F27MK600 · Engine Indicating SystemSDR 2004F00188Switch · malfunctionedDURING CLIMB-OUT FROM RAP AT 11,000 FEET, THE RT ENGINE LOW OIL PRESSURE LIGHT ILLUMINATD. THE CREW SHUT DOWN THE RIGHT ENGINE AS A PRECAUTION. AN EMERGENCY WAS DECLARED. AIRCRAFT RETURNED TO RAP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT Jun 19, 2004 · N730FE · Fokker F27MK600 · Engine Oil PressureSDR 2004F00152Alternator · inoperativeLEFT AC ALTERNATOR FAILED ON CLIMB-OUT FROM KTN. AIRCRAFT RETURNED TO KTN WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. THE ALTERNATOR WAS REMOVED AND REPLACED. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)May 18, 2004 · N742FE · Fokker F27MK600 · DC Generating SystemSDR 2004F00311Inverter · failedNR 1 INVERTER FAILED IN FLIGHT AND WOULD NOT RESET. CRW ELECTED TO RETURN TO YVR. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 1 INVERTER. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Apr 27, 2004 · N703FE · Fokker F27MK600 · AC InverterSDR 2004F00268Indicator · inoperativeDURNG POEWR ADVANCE ON TAKEOFF, NR 1 TORQUE INDICATOR SHOWED '0'. CREW ABORTED TAKEOFF ROLL AND RETURNED TO THE RAMP. MAINTENANCE REMOVED AND REPLACED THE TORQUE INDCIATOR. AIRCRAFT WAS RETURNED TO SERVICE. (M)Apr 25, 2004 · N703FE · Fokker F27MK600 · Engine BMEP/Torque IndicatingSDR COE2004F00000Control Panel · failedAFTER TAKEOFF, LEFT ENGINE GENERATOR WOULD NOT CARRY A LOAD. CREW TURNED BACK WHERE MAINTNANCE WAS AVAILABLE. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LT GENERATOR CONTROL PANEL. AIRCRAFT WAS RETURNED TO SERVICE.Mar 4, 2004 · N741FE · Fokker F27MK600 · DC Generating SystemSDR 2004F00218Circuit Breaker · trippedAFTER DEPARTURE FROM FSD, THE AIRCRAFT EXPERIENCED A DC ELECTRICAL SYSTEM FAILURE. CREW SELECTED EMERGENCY POWER AND RETURNED TO FSD, NO EMERGENCY WAS DECLARED. TROUBLESHOT DC POWER SYSTEM, FOUND REVERSE CURRENT RELAY CIRCUIT BREAKER TRIPPED. RESET CIRCUIT Jan 28, 2004 · N702FE · Fokker F27MK600 · DC Power Distribution SystemSDR COE2003F00004Pin · failedPILOT REPORTED, HAD TO RECYCLE LANDING GEAR C/B TO GET THE LANDING GEAR TO RETRACT (ALL GEAR). MAINTENANCE REPLACED PIN CONNECTING LANDING GEAR LOCK SOLENOID TO LOCKING PAWL. PERFORMED GEAR SWING. AIRCRAFT RETURNED TO SERVICE.Dec 3, 2003 · N702FE · Fokker F27MK600 · Main Landing Gear Attach SectionSDR COEA0303742Linkage · brokenAFTER TAEKOFF, THE NOSE WHEEL FAILED TO UNLOCK FOR RETRACTION. CREW ELECTED TO RETURN TO RAP, NO EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND EYE END BROKEN THAT CONNECTS TO GEAR UNLOCK LATCH. REMOVED AND REPLACED EYE END. A/Oct 24, 2003 · N742FE · Fokker F27MK600 · Landing Gear Retraction/Extension SystemSDR COEA0304729Fire Loop · malfunctionedRT ENGINE FIRE WARNING ACTIVATED 5 MINUTES AFTER T/O FROM SEA. RT ENGINE SHUT DOWN. PILOTS REQUESTED RETURN TO SEA. AN EMERGENCY WAS DECLARED AND THE FLIGHT RETURNED TO SEA WITHOUT INCIDENT. INSPECTION OF THE AIRCRAFT NO EVIDENCE OF A FIRE. MAINTENANCE TEOct 23, 2003 · N729FE · Fokker F27MK600 · Fire DetectionSDR 2003F00584Battery · overheatedAPPROX 65 NM FROM SITKA, BATTERY OVERTEMP ILLUMINATED IN FLIGHT. CREW ELECTED TO DIVERT TO JUNEAU WHERE MAINTENANCE WAS AVAILABLE. LANDED UNEVENTFULLY. JNU MAINTENANCE REMOVED AND REPLACED BOTH BATTERIES. AIRCRAFT RETURNED TO SERVICE. COMPANY INITIATED A Aug 12, 2003 · N729FE · Fokker F27MK600 · Battery/Charger SystemSDR COE2003F00002Control Valve · intermittentDEPARTING, AFTER TAKEOFF, NOSE GEAR INTRANSIT LIGHT REMAINED ON AFTER GEAR SELECTED UP. GEAR DOWN WAS SELECTED AND NORMAL ILLUMINATED. FLIGHT CONTINUED. MAINTENANCE OPERATIONALLY CHECKED STEERING AND RETRACTION SYSTEMS AND COULD NOT DUPLICATE MALFUNCTION. Jul 23, 2003 · N742FE · Fokker F27MK600 · Landing Gear Steering SystemSDR 2003F00472Control Unit · intermittentNOSE WHEEL INTRANSIT LIGHT REMAINED ON AFTER TAKEOFF WITH LANDING GEAR SELECTOR UP. THE PRESSURE FAIL LIGHT DID NOT ILLUMINATE. NOSE WHEEL STEERING WAS THEN SWITCHED OFF AND THE LANDING GEAR WAS EXTENDED WITH SIX GREEN INDICATED, HOWEVER THE TILLER REMAINED Jun 23, 2003 · N703FE · Fokker F27MK600 · Landing Gear Steering SystemSDR 2003F00356Control Panel · malfunctionedAIRCRAFT DEPARTED SEA FOR JNU, RIGHT GENERATOR FAIL LIGHT ILLUMINATED AND UNABLE TO RESET. PILOT ADVISED TO RETURN TO SEA. NO EMERGENCY DECLARED. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RT DC CONTROL PANEL. AIRCRAFT RETURNED TO SERVICE. (M)May 12, 2003 · N730FE · Fokker F27MK600 · DC Generator-AlternatorSDR COEA0301730Drive Shaft · failedNR 1 ENGINE ACCESSORY GEARBOX DRIVESHAFT FAILED DURING AIRCRAFT APPROACH TO SEA. FLIGHT CREW PERFORMED PRECAUTIONARY ENGINE IN FLIGHT SHUT DOWN AND LANDED AT SEA WITHOUT FURTHER INCIDENT. ENGINE NACELLE AND FIREWALL SUSTAINED SUBSTANTIAL DAMAGE. ENGINE, ACCApr 17, 2003 · N730FE · Fokker F27MK600 · Accessory GearboxesSDR 2003F00114Inverter · malfunctionedVISIBLE SMOKE/HAZE IN CARGO COMPARTMENT ACCOMPANIED BY BURNING SMELL. SYMPTOMS WENT AWAY WHEN CHOKE VALVE WAS OPENED. REMOVED AND REPLACED EMERGENCY INVERTER. OPS CHECKS SERVICEABLE. AIRCRAFT RETURNED TO SERVICE. (M)Dec 28, 2002 · N703FE · Fokker F27MK600 · AC InverterSDR COEA0202740Switch · faultyLEFT FIRE WARNING LIGHT ILLUMINATED DURING CLIMB OUT DEPARTURE FROM GEG. NO FIRE REPORTED. AIRCRAFT RETURNED TO GEG WITHOUT INCIDENT. MAINTENANCE PERSONNEL REPLACED THE LEFT FIRE WARNING TEST SWITCH. AIRCRAFT RETURNED TO SERVICE. (M)Dec 11, 2002 · N740FE · Fokker F27MK600 · Fire DetectionSDR COEA02021742Alternator · failedFLIGHT CREW REPORTED LEFT ALTERNATOR FAILED INFLIGHT DURING ICING CONDITIONS WHILE DEPARTING FROM YVR. FLIGHT CREW RETURNED TO YVR AND LANDED WITHOUT INCIDENT. NO EMERGENCY DECLARED. MAINTENANCE PERSONNEL REPLACED LEFT ALTERNATOR. AIRCRAFT RETURNED TO SERVDec 10, 2002 · N742FE · Fokker F27MK600 · DC Generator-AlternatorSDR COEA0201702Wire · brokenAIRCRAFT RETURNED TO BASE AFTER FIRST OFFICER REPORTED SMELL OF SMOKE IN COCKPIT. MAINTENANCE PERSONNEL REPAIRED BROKEN WIRE THAT CONTROLS LIGHTING TO VERTICAL SPEED INDICATOR (VSI). (M)Nov 25, 2002 · N702FE · Fokker F27MK600 · Light System WiringSDR COEA02021740Generator · failedFLIGHT CREW REPORTED RIGHT GENERATOR FAIL LIGHT ILLUMINATED DURING CRUISE FLIGHT AT FL2000. MAINTENANCE PERSONNEL REPLACED LEFT DC GENERATOR. AIRCRAFT RETURNED TO SERVICE. (M)Sep 24, 2002 · N740FE · Fokker F27MK600 · DC Generator-AlternatorSDR COEA0203729Actuator · leakingAIRCRAFT RETURNED TO BASE AFTER IT WAS DISCOVERED THAT PNEUMATIC PRESSURE FOR OPERATION OF THE LANDING GEAR DROPPED TO ZERO WITH GEAR IN UP POSITION. LANDING GEAR SELECTOR VALVE AND NOSE LANDING GEAR ACTUATOR FOUND LEAKING AND REPLACED. NOSE LANDING GEAR ACTSep 4, 2002 · N729FE · Fokker F27MK600 · Landing Gear ActuatorSDR COEA0202729Line · leakingON DEPARTURE FROM GEG, NOSE GEAR IN TRANSIT LIGHT REMAINED ON AFTER GEAR SELECTED UP. MAINTENANCE REMOVED AND REPLACED LEAKING STEERING MOTOR SWIVEL LINE AND FOLLOW UP CONTROL VALVE TO CORRECT PROBLEM. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)Mar 28, 2002 · N729FE · Fokker F27MK600 · Landing Gear Steering SystemSDR COEA0103702Gasket · wornNR 2 ENGINE GEAR BOX OIL PRESSURE LIGHT CAME ON IN FLIGHT. PILOT PERFORMED PRECAUTIONARY IN FLIGHT SHUTDOWN ON NR 2 ENGINE. NO EMERGENCY DECLARED. MAINTENANCE FOUND OIL LEAKING FROM AROUND MOUNTING PAD OF PNEUMATIC COMPRESSOR. GASKET AND OIL TRANSFER BOBBINov 16, 2001 · N702FE · Fokker F27MK600 · Turbine Engine Accessory DriveSDR 2001F00049Inverter · failedDEPARTED LAS VEGAS EN ROUTE TO OAK - FLT 7709 - SHORTLY, AFTER TAKEOFF, THE NR 1 INVERTER FAILED. THE FLIGHT CREW DECLARED AN INFLIGHT EMERGENCY AND RETURNED TO LAS. MAINTENANCE WAS DISPATCHED AND REPLACED THE NR 1 INVERTER. THE AIRCRAFT WAS RETURNED TO SERJun 1, 2001 · N701FE · Fokker F27MK600 · AC InverterSDR COEA0101740Motor · leakingON DEPARTURE FROM GEG, NOSE GEAR IN TRANSIT LIGHT REMAINED ON AFTER GEAR SELECTED UP. MAINTENANCE REMOVED AND REPLACED LEAKING STEERING MOTOR TO CORRECT PROBLEM. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)May 1, 2001 · N740FE · Fokker F27MK600 · Steering UnitSDR COEA102740Valve · leakingDURING LANDING APPROACH TO PSC, LEFT MAIN LANDING GEAR WOULD NOT EXTEND. AFTER SEVERAL ATTEMPTS, FLIGHT CREW LOWERED GEAR USING EMERGENCY GEAR EXTENSION SYSTEM. LANDING GEAR PRESSURE REDUCER VALVE WAS FOUND TO BE THE CAUSE AND WAS SUBSEQUENTLY REPLACED. AIRApr 30, 2001 · N740FE · Fokker F27MK600 · Landing Gear Retraction/Extension SystemSDR 20010410AP027Pump · failedON ATTEMPTING TAKEOFF FROM OAK AT APPROXIMATELY 0200 (L), PILOT REPORTED THE WARNING LIGHT FOR THE LEFT NR 2 FUEL BOOST PUMP ILLUMINATED. AS THE NR 1 PUMP FOR THIS ENGINE WAS ALREADY DEFERRED, PILOT ELECTED TO ABORT THE TAKEOFF AND RETURN TO THE RAMP FOR MAINFeb 1, 2001 · N702FE · Fokker F27MK600 · Fuel Boost PumpSDR 20010112SG017Control Valve · inoperativeNOSE GEAR WOULD NOT RETRACT. MAIN BOTTLE PSI 2000. PILOT ELECTED TO ABORT FLIGHT AND RETURNED TO AIRPORT. LANDING GEAR RETRACTION TEST REVEALED MALFUNCTIONING FOLLOW UP CONTROL VALVE. FOLLOW UP CONTROL VALVE REPLACED. NOSE GEAR NOW FUNCTIONS NORMALLY. (MNov 10, 2000 · N740FE · Fokker F27MK600 · Landing Gear Retraction/Extension SystemSDR 20010523CW004Gasket · unserviceablePILOT REPORTED DROP IN RIGHT ENGINE OIL PRESSURE DURING CLIMB THROUGH 10,000 FT AFTER DEPARTURE FROM FSD. NO EMERGENCY WAS DECLARED. PILOT RETURNED AIRCRAFT TO FSD WHERE MAINTENANCE DISCOVERED A FAILED PROPELLER LOCK LIMIT SWITCH GASKET; CAUSING THE LOSS OF Jul 6, 2000 · N702FE · Fokker F27MK600 · Propeller Controlling SystemSDR COEA0001702Gasket · failedPILOT REPORTED THAT AS HE WAS CLIMBING THROUGH, 10,000 FT HE OBSERVED THE OIL PRESSURE DROPPED TO 9 PSI AND THE OIL LIGHT ILLUMINATED. AT THIS TIME HE ELECTED TO RETURN TO SIOUX FALLS, SOUTH DAKOTA. THE PILOR REPORTED HE WAS ABLE TO LAND WITHOUT INCIDENT. NJul 6, 2000 · N702FE · Fokker F27MK600 · Propeller Controlling SystemSDR AU000536Bearing · failed(AUS) RT ENGINE ACCESSORY GEARBOX INPUT BEARING FAILED ALLOWING OIL TOLEAK OUT OF CASE.Jun 19, 2000 · Fokker F27MK600 · Turbine Engine Accessory DriveSDR AU000155Compressor · failed(AUS) LH ENGINE DRIVEN PNEUMATIC COMPRESSOR FAILED. OIL LINE FOUNDBROKEN AT BRAZED FITTING.Mar 23, 2000 · Fokker F27MK600 · Pneumatic Distribution SystemSDR 20000417AP004Engine · failedPILOT REPORTED NR 1 ENGINE FAILED IN FLIGHT WHILE APPROACH LAS. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED SAFELY AT LAS. INITIAL ASSESSMENT BY MAINTENANCE INDICATES AN APPARENT INTERNAL ENGINE FAILURE. ENGINE GEARS APPEAR TO BE SEIZED UP. OIL SCREEFeb 1, 2000 · N730FE · Fokker F27MK600 · Engine (Turbine/Turboprop)SDR COEA9901702Skin · dentedLAS VEGAS - A/C WAS HIT BY A UPS CARGO CONTAINER WHILE THE AIRCRAFT WAS PARKED ON THE AIRPORT RAMP. THE CONTAINER WAS BLOWN ACROSS THE RAMP BY A HIGH WIND. STRUCTURAL DAMAGE OCCURRED TO THE REAR SECTION OF THE AIRCRAFT FUSELAGE. REMOVED AND REPLACED FRAME SDec 9, 1999 · N702FE · Fokker F27MK600 · Fuselage Main, Plate/SkinSDR AU990148Seal · failed(AUS) NR 2 ENGINE AUXILIARY GEARBOX OUTPUT SHAFT SEAL LEAKING. ENGINE HAD SUFFERED A PREVIOUS AUXILIARY GEARBOX DRIVESHAFT FAILURE WHICH MAY HAVE CONTRIBUTED TO THE DEFECT.Feb 11, 1999 · Fokker F27MK600 · Turbine Engine Accessory Drive
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