# Fokker F.27MK 500 - Type: Aircraft model (FAA registry) - Registry code: 4990629 - Manufacturer (registry): FOKKER - Model: F.27MK 500 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 2 · Turbo-prop - Seats: 55 - Weight class: 20,000 lb and over - Cruise speed: 219 mph - Certification: Type certificated - Registered aircraft: 0 - Page: https://openairdocs.org/model/fokker-f-27mk-500 Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. None matched. ## Registered aircraft None registered with this model now. ## NTSB investigations (4) From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [NTSB DCA04WA041](https://openairdocs.org/ntsb/DCA04WA041), Apr 27, 2004: Fokker F27-500 (N715FE), Melo, Uruguay, substantial damage - [NTSB ATL03LA056](https://openairdocs.org/ntsb/ATL03LA056), Mar 8, 2003: Fokker F.27MK 500 (N712FE), Kinston, NC, substantial damage. Probable cause: The fatigue failure of the main drag stay tube. A factor is no inspection procedure required. - [NTSB CHI89IA084](https://openairdocs.org/ntsb/CHI89IA084), May 4, 1989: Fokker F-27 MK500 (N511AW), Moline, IL, incident, minor damage. Probable cause: MATERIAL FAILURE OF THE LANDING GEAR RETRACTION AND EXTENSION ASSEMBLY. INADEQUATE MAINTENANCE AND TROUBLESHOOTING PROCEDURES IN COMPANY DIRECTIVES WERE FACTORS IN THIS INCIDENT. - [NTSB CHI88IA015](https://openairdocs.org/ntsb/CHI88IA015), Oct 29, 1987: Fokker F27-500 (N511AW), Chicago, IL, incident, no damage ## FAA accident and incident reports (28) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Accident 20030308008249A](https://openairdocs.org/incident/20030308008249A), Mar 8, 2003: Fokker F27MK500 (N712FE), Kinston, NC, Substantial damage. (-23) Inspector statement: on 03-08-2003 I was notified by FAA com center of an incident/accident in Kinston north carolina. The accident involved a Fokker… - [Incident 20010524012679I](https://openairdocs.org/incident/20010524012679I), May 24, 2001: Fokker F27MK500 (N712FE), Indianapolis, IN. (-23) On 05/24/01, mountain air cargo (mtna), F-27-MK500 aircraft registration N712FE, operating under flight 8201 inbound to ind from bna, declared an… - [Incident 20000314001469I](https://openairdocs.org/incident/20000314001469I), Mar 14, 2000: Fokker F27MK500 (N283EA), Grand Canyon, AZ. (-23) Due to spike from over voltage relay, causing the altitude alerter to over heat and provide smoke in the cockpit area, causing failure of both numbers 1… - [Incident 19970604014989I](https://openairdocs.org/incident/19970604014989I), Jun 4, 1997: Fokker F27MK500 (N721FE), Peoria, IL. Narrative: on June 4, 1997, at 4:46 am, CST, N721FE, Fokker F-27, on approach to the Peoria, Illinois airport had the fire warning light for the left engine… - [Incident 19931215051269I](https://openairdocs.org/incident/19931215051269I), Dec 15, 1993: Fokker F27MK500 (N980MA), Lihue, HI, Minor damage. Right fiberglass non-structural wing fairing panels departed aircraft inflight. Panels not properly installed. - [Incident 19930413012149I](https://openairdocs.org/incident/19930413012149I), Apr 13, 1993: Fokker F27MK500 (N727FE), Indianapolis, IN. Pilot unable to maintain directional control on rollout. Veered off runway. Nosewheel steering control valve faulty - [Incident 19930324022259I](https://openairdocs.org/incident/19930324022259I), Mar 24, 1993: Fokker F27MK500 (N712FE), Atlanta, GA, Minor damage. Left engine fire light after takeoff. Fired fire bottles. Engine secured. Returned. Landed safely. - [Incident 19921116053079I](https://openairdocs.org/incident/19921116053079I), Nov 16, 1992: Fokker F27MK500 (N513AW), Peoria, IL, Minor damage. Aircraft aborted takeoff after striking a deer on takeoff roll. - [Incident 19921111052149I](https://openairdocs.org/incident/19921111052149I), Nov 11, 1992: Fokker F27MK500 (N728FE), Cleveland, OH. Right engine quit in flight. Attempted to restart. Found both boost pump switches were off. - [Incident 19920920051299I](https://openairdocs.org/incident/19920920051299I), Sep 20, 1992: Fokker F27MK500 (N244MA), Baltimore, MD. Right propeller RPM surge on climb. Right gearbox warning system illumination. Returned. Landed safely. - [Incident 19920516019329I](https://openairdocs.org/incident/19920516019329I), May 16, 1992: Fokker F27MK500 (N706FE), Des Moines, IA. Smoke in cockpit inflight. Turned off heater. Smoke lingered. Diverted. Avionics cooling fan had failed. - [Incident 19920418010369I](https://openairdocs.org/incident/19920418010369I), Apr 18, 1992: Fokker F27MK500 (N705FE), Springfield, MO, Minor damage. Aircraft settled back on runway after liftoff with landing gear retracted. - [Incident 19920204004289I](https://openairdocs.org/incident/19920204004289I), Feb 4, 1992: Fokker F27MK500 (N714FE), Charleston, WV. Right engine lost RPM. Did not respond to commands. Returned. Throttle control push pull tube had disconnected. - [Incident 19911222059699I](https://openairdocs.org/incident/19911222059699I), Dec 22, 1991: Fokker F27MK500 (N513AW), Fort Wayne, IN, Minor damage. NR2 engine gearbox oil pressure warning on climb. Shut down and returned. Oil line defective along 90 degree bend. - [Incident 19910705032749I](https://openairdocs.org/incident/19910705032749I), Jul 5, 1991: Fokker F27MK500 (N513AW), Peoria, IL. Left engine gearbox low pressure warning. Landed without incident. Oil level low. - [Incident 19910122006549I](https://openairdocs.org/incident/19910122006549I), Jan 22, 1991: Fokker F27MK500 (N715FE), Houston, TX. Low oil pressure on left engine. Returned. Found wheel casing scavenge oil filter securing nut bolts stripped. - [Incident 19910101002029I](https://openairdocs.org/incident/19910101002029I), Jan 1, 1991: Fokker F27MK500 (N503AW), Champaign-Urban, IL. Reduction gearbox warning light on right engine. Returned. Replaced reduction gear box oil pressure switch. - [Incident 19900919053629I](https://openairdocs.org/incident/19900919053629I), Sep 19, 1990: Fokker F27MK500 (N513AW), Champaign-Urban, IL. Right engine reduction gearbox low oil pressure light on. Returned. Low oil pressure switch faulty. - [Incident 19900815043579I](https://openairdocs.org/incident/19900815043579I), Aug 15, 1990: Fokker F27MK500 (N511AW), Green Bay, WI. Odor of ether on taxi. Returned to gate. Ether bottle leaking in cargo area. Crew relieved of duty from effect. - [Incident 19891206059569I](https://openairdocs.org/incident/19891206059569I), Dec 6, 1989: Fokker F27MK500 (N282MA), Detroit, MI. Crew reported an aileron trim problem on climbout. Returned. - [Incident 19891022058659I](https://openairdocs.org/incident/19891022058659I), Oct 22, 1989: Fokker F27MK500 (N282MA), Mosinee, WI, Minor damage. Right wheel bearing fire while taxiing to gate. Used extinguisher and deplaned. - [Incident 19890306026019I](https://openairdocs.org/incident/19890306026019I), Mar 6, 1989: Fokker F27MK500 (N706FE), Manchester, NH. Drop in right engine oil pressure. Shut it down and returned. Found a cracked engine oil cooler. - [Incident 19890118023839I](https://openairdocs.org/incident/19890118023839I), Jan 18, 1989: Fokker F27MK500 (N509AW), Champaign-Urban, IL. Cockpit filled with smoke while taxiing for departure. Engine shut down. Engine blower intake cover still installed - [Incident 19881226069659I](https://openairdocs.org/incident/19881226069659I), Dec 26, 1988: Fokker F27MK500 (N513AW), Chicago, IL. After liftoff, aircraft began to roll to right. Recovered and returned. Snow contamination on one wing. - [Incident 19870304028759I](https://openairdocs.org/incident/19870304028759I), Mar 4, 1987: Fokker F27MK500 (N503AW), Milwaukee, WI. Right fire warning light came on with bell warning. Engine shutdown. Safe landing. Faulty connection on fire loop. - [Incident 19860313016309I](https://openairdocs.org/incident/19860313016309I), Mar 13, 1986: Fokker F27MK500 (N239MA), Chicago, IL, Minor damage. Failed to stop when signaled by ground personnel. Wingtip struck other aircraft who was loading at another gate. - [Incident 19860122010319I](https://openairdocs.org/incident/19860122010319I), Jan 22, 1986: Fokker F27MK500 (N240MA), Muskegon, MI. Engine failed during climb. Returned. Fuel was probably cut off when HP cock was moved beyond the open detent. - [Incident 19840924061879I](https://openairdocs.org/incident/19840924061879I), Sep 24, 1984: Fokker F27MK500 (N239MA), Rhinelander, WI. Cabin blower overtemp light came on. Returned to airport. Temperature switch PN21557 1 8 2 replaced. ## Service difficulty reports (64, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR CA090116009](https://openairdocs.org/sdr/CA090116009), Jan 8, 2009: OIL 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 LAND - [SDR CA081217014](https://openairdocs.org/sdr/CA081217014), Dec 8, 2008: ENGINE. 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 - [SDR MAC100603](https://openairdocs.org/sdr/MAC100603), Oct 16, 2006: DISPLAY. FAILED. DURING CRUISE FLT, THE CREW SMELLED A FAINT ELECTRICAL BURNING SMELL AND NOTICED AT THE SAME TIME THAT THE MFD HAD GONE BLANK. - [SDR MAC10030601](https://openairdocs.org/sdr/MAC10030601), Oct 2, 2006: WARNING LIGHT. ILLUMINATED. THE NR 2 GEAR BOX LOW OIL PRESSURE LIGHT ILLUMINATED IN FLIGHT. - [SDR MAC070602](https://openairdocs.org/sdr/MAC070602), Jul 15, 2006: WARNING LIGHT. ILLUMINATED. THE LT ENGINE GEARBOX LOW OIL PRESSURE LIGHT ILLUMINATED IN FLIGHT 7 MIN AFTER T/O. - [SDR MAC070601](https://openairdocs.org/sdr/MAC070601), Jul 14, 2006: O-RING. CUT. THE LEFT ENGINE GEARBOX LOW OIL PRESSURE WARNING LIGHT ILLUMINATED DURING DESCENT INTO MBJ. - [SDR MAC030601](https://openairdocs.org/sdr/MAC030601), Mar 22, 2006: BRAKE ASSY. SEIZED. A RIVET SHEARED IN THE BRAKE ASSEMBLY AND LOCKED THE WHEEL CAUSING DAMAGE TO THE TIRE (FLAT). - [SDR MAC020601](https://openairdocs.org/sdr/MAC020601), Feb 23, 2006: GARLOCK SEAL. LEAKING. ON DESCENT THE NR 2 ENGINE GEARBOX OIL PRESSURE RED LIGHT ILLUMINATED. - [SDR MAC120502](https://openairdocs.org/sdr/MAC120502), Dec 28, 2005: FIRE LOOP. CHAFED. AFTER TAKEOFF, THE CREW HAD A FIRE WARNING ON THE NR 1 ENGINE. - [SDR MAC90502](https://openairdocs.org/sdr/MAC90502), Sep 19, 2005: AMPLIFIER. SHORTED. APPROXIMATELY AN HOUR INTO FLT, THE PIC EXPERIENCED SMOKE IN THE COCKPIT. DECLARED AN EMERGENCY AND RETURNED TO MIA. THE LANDING WAS WITHOUT INCIDENT. AFTER INV - [SDR MAC8501](https://openairdocs.org/sdr/MAC8501), Aug 12, 2005: GENERATOR. FAILED. ON 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 O - [SDR MAC5403](https://openairdocs.org/sdr/MAC5403), Apr 8, 2005: GENERATOR. OVERTEMP. EN ROUTE THE LEFT GENERATOR INDICATED AND OVERHEAT CONDITION. THE CREW MADE AN EMERGENCY IN POA FOR REPAIRS. - [SDR MAC5402](https://openairdocs.org/sdr/MAC5402), Apr 5, 2005: VOLT REGULATOR. FAILED. NR 2 GENERATOR DROPPED OFFLINE DURING CLIMBOUT. - [SDR MAC5401](https://openairdocs.org/sdr/MAC5401), Apr 3, 2005: GEARBOX. LEAKING. EN 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. TH - [SDR MAC4801](https://openairdocs.org/sdr/MAC4801), Aug 2, 2004: SELECTOR VALVE. LEAKING. DURING 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 - [SDR AUS20040485](https://openairdocs.org/sdr/AUS20040485), May 10, 2004: REGULATOR. STICKING. (AUS) ELEVATOR CABLE TENSION REGULATOR STICKY IN OPERATION. - [SDR MTNA20043](https://openairdocs.org/sdr/MTNA20043), Apr 27, 2004: FIRE. DETECTED. DURING FLIGHT FDX7145 EZE-POA THE CARGO SMOKE WARNING LIGHT ILLUMINATED. THE THIRD CREW MEMBER OCCUPYING THE JUMP SEAT CHECKED THE CARGO COMPARTMENT AND OBSERVE - [SDR MTNA20044](https://openairdocs.org/sdr/MTNA20044), Apr 27, 2004: FIRE LOOP. OPEN. AFTER 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 PERFORM - [SDR AUS20040099](https://openairdocs.org/sdr/AUS20040099), Feb 12, 2004: SWITCH. 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 - [SDR MTNA20041](https://openairdocs.org/sdr/MTNA20041), Jan 21, 2004: BOOT. DETACHED. AFTER TAKEOFF FROM MEM A VIBRATION WAS DETECTED AND THE AIRCRAFT RETURNED TO MEM. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE LEFT OUTBOARD HORIZONTAL STAB - [SDR 2003F00620](https://openairdocs.org/sdr/2003F00620), Oct 13, 2003: AMPLIFIER. INOPERATIVE. ON TAKEOFF FROM ANCHORAGE, THE RT ATTITUDE INDICATOR FAILED, RIGHT AFTER ROTATION. THE AIRCRAFT RETURNED TO ANC. NO EMERGENCY WAS DECLARED. AIRCRAFT LANDED WITH - [SDR COEA0301711](https://openairdocs.org/sdr/COEA0301711), Oct 7, 2003: SELECTOR VALVE. MALFUNCTIONED. AFTER 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 - [SDR MTNA20035](https://openairdocs.org/sdr/MTNA20035), Aug 25, 2003: CLAMP. LOOSE. ON 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. TH - [SDR MTNA20033](https://openairdocs.org/sdr/MTNA20033), Jul 8, 2003: ACTUATOR. STUCK. AFTER 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 EMERGENC - [SDR MTNA20032](https://openairdocs.org/sdr/MTNA20032), Apr 2, 2003: PROPELLER. MALFUNCTIONED. IN 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. - [SDR MTNA20031](https://openairdocs.org/sdr/MTNA20031), Mar 11, 2003: DRAG BRACE. BROKEN. THE 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 E - [SDR MTNA20021](https://openairdocs.org/sdr/MTNA20021), Jan 3, 2002: RELIEF VALVE. DURING 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 - [SDR MTNA200201](https://openairdocs.org/sdr/MTNA200201), Jan 3, 2002: RELIEF VALVE. DURING 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 - [SDR MTNA200113](https://openairdocs.org/sdr/MTNA200113), Dec 7, 2001: WIRE. SHORTED. IN 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 OTHE - [SDR MTNA200112](https://openairdocs.org/sdr/MTNA200112), Nov 28, 2001: SELECTOR VALVE. LEAKING. ON 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 EM - [SDR MTN2001F00000](https://openairdocs.org/sdr/MTN2001F00000), Sep 14, 2001: CONNECTOR. LOOSE. DURING 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 CHE - [SDR MTNA200111](https://openairdocs.org/sdr/MTNA200111), Sep 14, 2001: CONNECTOR. LOOSE. During 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 che - [SDR MTNA200109](https://openairdocs.org/sdr/MTNA200109), Jul 31, 2001: FIRE LOOP. During take off and climb out of LCK. the right engine fire warning light illuminated. The crew performed the emergency check list procedures, declared an emerg - [SDR AU001196](https://openairdocs.org/sdr/AU001196), Dec 17, 2000: SKIN. DELAMINATED. (AUS) RT HORIZONTAL STABILISER LEADING EDGE (LAMINATED TIMBER CONSTRUCTION) BADLY DELAMINATED , THE TIMBER SECTION ROTTED AND THE BONDED SECTION FULL OF WATER. - [SDR 20001204SH008](https://openairdocs.org/sdr/20001204SH008), Nov 15, 2000: FIRE LOOP. MALFUNCTIONED. JUST AFTER TAKEOFF, ENGINE FIRE WARNING ON RIGHT ENGINE. DEFECTIVE FIRE LOOP SEGMENT CAUSING FIRE WARNING INDICATION ONLY. NO FIRE. REPLACED BOTH ENGINE FIRE BO - [SDR 20001204SH009](https://openairdocs.org/sdr/20001204SH009), Nov 14, 2000: RACK. CRACKED. PILOTS REPORTED THAT AIRCRAFT STEERING WAS INOPERATIVE. MAINTENANCE FOUND THE STEERING RACK HAD CRACKED AT THE FIRST TOOTH SERRATION. THE STEERING RACK WAS REPL - [SDR 20001025SH024](https://openairdocs.org/sdr/20001025SH024), Oct 11, 2000: LEVER. BROKEN. PILOT 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 CONTRO - [SDR 20000602SH013](https://openairdocs.org/sdr/20000602SH013), May 15, 2000: BEARING. FAILED. CREW 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 ATTE - [SDR AU990615](https://openairdocs.org/sdr/AU990615), Jul 1, 1999: DUCT. 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 - [SDR COEA9901720](https://openairdocs.org/sdr/COEA9901720), Feb 1, 1999: SWITCH. MALFUNCTIONED. DURING 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 AS - [SDR 98ZZZM565](https://openairdocs.org/sdr/98ZZZM565), Jul 10, 1998: LINE. LOOSE. DURING CRUISE, LEFT GEARBOX LOW OIL PRESSURE LIGHT ILLUMINATED. (M) - [SDR 98ZZZX2571](https://openairdocs.org/sdr/98ZZZX2571), Jun 21, 1998: COMBUSTION CAN. CRACKED. DURING 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 REMOV - [SDR COEA9802720](https://openairdocs.org/sdr/COEA9802720), Feb 17, 1998: FIRE LOOP. MALFUNCTIONED. DURING 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. FO - [SDR 97ZZZX3928](https://openairdocs.org/sdr/97ZZZX3928), Aug 3, 1997: WIRE. BROKEN. ON 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 - [SDR 97ZZZX3926](https://openairdocs.org/sdr/97ZZZX3926), Jul 21, 1997: WIRING HARNESS. CHAFED. ON 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 - [SDR 97ZZZM747](https://openairdocs.org/sdr/97ZZZM747), Jun 27, 1997: DOOR FRAME. CRACKED. DURING AN SCHEDULED INSPECTION, A CRACK WAS FOUND IN THE PASSENGER ENTRY DOOR FRAME STRUCTURE UNDER THE STAIRS AFT ATTACH BRACKET. THE CRACK EXTENDED THROUGH TH - [SDR 97ZZZX3440](https://openairdocs.org/sdr/97ZZZX3440), Jun 4, 1997: FIRE LOOP. SHORTED. IND/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. AF - [SDR 97ZZZX2093](https://openairdocs.org/sdr/97ZZZX2093), Apr 29, 1997: FUEL PUMP. SHAFT SHEARED. ON 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 SH - [SDR 97ZZZX2360](https://openairdocs.org/sdr/97ZZZX2360), Apr 4, 1997: UPPER MEMBER. CRACKED. INSPECTION FOUND MLG UPPER MEMBER CRACKED. PART TOTAL CYCLES, 56,096. PART TSO CYCLES, 6,712. (X) - [SDR 97ZZZX2094](https://openairdocs.org/sdr/97ZZZX2094), Feb 6, 1997: ENGINE. DAMAGED. EWR/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 DEC All 64: https://openairdocs.org/model/fokker-f-27mk-500/reports.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.