# Service difficulty reports: GE CF6-50C A list on [GE CF6-50C](https://openairdocs.org/engine/ge-cf6-50c.md). Newest first. General aviation reporting is voluntary. - [SDR FDEA201407261979](https://openairdocs.org/sdr/FDEA201407261979.md): Engine · overspeed · Jul 26, 2014 · N320FE · Doug MD1030F · Engine (Turbine/Turboprop) > REJECTED TAKEOFF AT 85 KIAS DUE TO NR 3 ENGINE EXCEEDANCE N1 120.6 FOR FIVE SECONDS. ACCOMPLISHED NR 3 ENGINE N1 OVERSPEED INSPECTION. CHECKED FAN ROTOR FOR FREEDOM ROTATION, CHECKED FIRST STAGE FAN FOR EXCESSIVE RUB, CHECKED INLET & EXHAUST AREA FREE OF PAR - [SDR FDEA201308131855](https://openairdocs.org/sdr/FDEA201308131855.md): Engine · malfunctioned · Aug 13, 2013 · N320FE · Doug MD1030F · Engine (Turbine/Turboprop) > REJECTED TAKEOFF AT 100 KTS FOR LEVEL 2 ENGINE RPM HIGH. N1 RPM NR 3 = 121.1. PERFORMED NR 3 ENGINE INSPECTION IAW MM 72-00-00-6-1, PAR B 1 & 2. CHECKED OK. NO DAMAGE NOTED. PERFORMED NR 3 ENGINE INSPECTION IAW MM 72-00-00-6-1 PAR B, 1 AND 2. CHECKED - [SDR FDEA201202240680](https://openairdocs.org/sdr/FDEA201202240680.md): Engine · flamed out · Feb 24, 2012 · N320FE · Doug MD1030F · Engine (Turbine/Turboprop) > DURING CLIMB OUT, LOST ENG NR 2 AFTER SHUTTING OFF ENG ANTI ICE AT ABOUT 18,000; RAN QRH AND RETURNED TO AIRPORT. ALL ENG INDICATIONS SEEMED NORMAL. ROLL BACK OF EGT AND N1 ONLY. CREW REPORTED THEY DID NOT TRY A RESTART. PERFORMED RIG CHECK OF FUEL LEVER A - [SDR FDEA201103261187](https://openairdocs.org/sdr/FDEA201103261187.md): Switch · failed · Mar 26, 2011 · N320FE · Doug DC1030F · Engine Oil Indicating System > ON INITIAL CLIMBOUT, RECEIVED ENG 2 OIL FILTER ALERT. USED MIN IDLE POWER AS ALERT WENT ON AND OFF SEVERAL TIMES FOR SEVEAL MINUTES EVENTUALLY REMAINED ON STEADY AT MIN IDLE. RED TABS FOR ALERT SHUTDOWN NR 2 ENGINE, RETURN TO DEPARTURE. NO OTHER ABNORMAL EN - [SDR CNMA20110001](https://openairdocs.org/sdr/CNMA20110001.md): Mec · defective · Feb 6, 2011 · N621AX · Doug DC1030 · Fuel Control/Turbine Engines > AFTER 1+ 25 INTO FLT. NOTICED NR 3 ENG N 2 FLUX BETWEEN 95-87 PERCENT N 2 ALSO NOTICE CONSIDERABLE VIBRATION NR 3 FUEL LEVER. AFTER NR 3 THROTTLE TO IDLE NOTICED NR 3 ENG FF/ EGT/ N2 ALSO FLUX. PERFORMED ENG FAILURE/ SHUTDOWN IN FLT. CKLIST IAW QRH 4-1-2-7. - [SDR AMTA200800242](https://openairdocs.org/sdr/AMTA200800242.md): Connector · damaged · Mar 27, 2008 · N701TZ · Doug DC1030 · Light System Wiring > AISLE EGRESS LIGHT AT 12JH INOPERATIVE. REPINNED SEAT 12 JH AISLE FLOOR PATH MARKING LIGHT CONNECTOR (SOCKET SIDE) IAW SWP`S IN WDM CH 20, LIGHT CHECKS GOOD AT THIS TIME. (K) - [SDR AMTA200800234](https://openairdocs.org/sdr/AMTA200800234.md): Wire · damaged · Mar 18, 2008 · N706TZ · Doug DC1030 · Light System Wiring > CARPET BY EMERGENCY FLOOR PATH LIGHTING AT D LAV PULLED UP, WIRES PULLED FROM SPLICE AT LIGHT STRIP. REAPIRED WIRES IAW SWPM 20-00-00 EMERGENCY LIGHTS. OPS CKS GOOD IAW MM 33-50-00. RESECURED CARPET AS REQUIRED. (K) - [SDR AMTA200800232](https://openairdocs.org/sdr/AMTA200800232.md): Battery · inoperative · Mar 17, 2008 · N705TZ · Doug DC1030 · Escape Slide > INSPECT INSTALLATION AND OPERATION OF THE R-2 DOOR REMOTE SLIDE PACK IND SYS BATTERIES. INSPECTED INSTALLATION AND OPERATION OF THE R-2 DOOR REMOTE SLIDE PACK INDICATION SYSTEM BATTERIES; C/W IAW MM 25-61-01. OPS NORMAL. (K) - [SDR AMTA200800214](https://openairdocs.org/sdr/AMTA200800214.md): Charger · unserviceable · Mar 9, 2008 · N705TZ · Doug DC1030 · Emergency Lighting > FWD GALLEY EMERGENCY LIGHTING AND LT AND RT ROWS 2-4 EGRESS LIGHTING INOPERATIVE. FOUND FWD BATTERY POWER SUPPLY FAULTY. REMOVED AND REPLACED FWD POWER SUPPLY ASSY IAW MM 33-51-01. SEAT ROWS 2-4, OPS CKS GOOD. (K) - [SDR AMTA200800114](https://openairdocs.org/sdr/AMTA200800114.md): Bottle · blown · Feb 19, 2008 · N705TZ · Doug DC1030 · Passenger/Crew Doors > L1 EMERGENCY ASSIST BOTTLE BLOWN INADVERTENTLY. SERVICE L1 DOOR EMERGENCY ASST BOTTLE IAW MM 52-11-07. (K) - [SDR AMTA200800100](https://openairdocs.org/sdr/AMTA200800100.md): Slide · deployed · Feb 15, 2008 · N706TZ · Doug DC1030 · Escape Slide > RT OVERWING DOOR SLIDE DEPLOYED NOT USED. REMOVED AND REPLACED DOOR SLIDE IAW 25-61-07. OK FOR SERVICE. (K) - [SDR AMTA200800023](https://openairdocs.org/sdr/AMTA200800023.md): Battery · discharged · Jan 19, 2008 · N702TZ · Doug DC1030 · Escape Slide > L3 DOOR REMOTE SLIDE PACK PRESSURE INDICATOR TEST WEAK. REMOVED AND REPLACED BATTERY IAW AMM 25-61-03. - [SDR AMTA200800024](https://openairdocs.org/sdr/AMTA200800024.md): Battery · discharged · Jan 19, 2008 · N702TZ · Doug DC1030 · Escape Slide > R4 DOOR REMOTE SLIDE PACK PRESSURE INDICATOR TEST WEAK. REMOVED AND REPLACED BATTERY IAW AMM 25-61-03. (K) - [SDR AMTA200800025](https://openairdocs.org/sdr/AMTA200800025.md): Wire · broken · Jan 19, 2008 · N702TZ · Doug DC1030 · Light System Wiring > AFTER LANDING, FOUND EMERGENCY LIGHTS OVERHEAD CIRCUIT BREAKER (D-4) POPPED. WILL NOT RESET. FOUND BROKEN WIRE LEADING TO OVERWING EMERGENCY LIGHTS BATTERY POWER SUPPLY. REPAIRED IAW SWP EMERGENCY LIGHT. OPS CHECKS NORMAL. (K) - [SDR AMTA200800026](https://openairdocs.org/sdr/AMTA200800026.md): Bottle · blown · Jan 19, 2008 · N705TZ · Doug DC1030 · Passenger/Crew Doors > L1 DOOR EMERGENCY BOTTLE BLOWN. RESERVICED L1 DOOR EMERGENCY BOTTLE IAW MM 52-11-07, OK FOR SERVICE. (K) - [SDR AMTA200700618](https://openairdocs.org/sdr/AMTA200700618.md): Unknown · odor · Nov 17, 2007 · N705TZ · Doug DC1030 · Air Distribution System > STRONG ELECTRICAL SMELL NEAR 3R EXIT DOOR. INSP AREA AND CONNECTORS OP DOOR SEVERAL TIMES NO ODOR, SMELL. OK FOR SERVICE. (K) - [SDR AMTA200700598](https://openairdocs.org/sdr/AMTA200700598.md): Accumulator · unserviceable · Nov 15, 2007 · N705TZ · Doug DC1030 · Hydraulic System, Main > SYS 3 HYD FLUID QTY SLOWLY DECREASED TO.5 GALS. PRESS STAYED AT 2800 PSI, TEMP STAYED AT 33 DEGREES. REMOVED AND REPLACED NR 3 HYD SYS TRANSMITTER FOUND LEAKING IAW 29-12-01. REPLACED SYSTEM ACCUMULATOR. (K) - [SDR AMTA200700619](https://openairdocs.org/sdr/AMTA200700619.md): Bottle · blown · Nov 15, 2007 · N705TZ · Doug DC1030 · Passenger/Crew Doors > DOOR 1L BLEW THE BOTTLE. RESERVICED L1, DOOR RESERVOIR IAW MM 52-10-01, CYLINDER, PSI NOW GOOD. (K) - [SDR AMTA200700594](https://openairdocs.org/sdr/AMTA200700594.md): Hydraulic System · malfunctioned · Nov 13, 2007 · N705TZ · Doug DC1030 · Hydraulic System, Main > ON FINAL AFTER SELECTING GEAR DOWN THE HYD SYS 3 ELEV OFF LIGHT CAME ON. NR 3 QUANTITY DROPPED TO 19 QTS. TAXIING IN AT ETAR THE QUANTITY CAME BACK UP TO 12 GALLONS AND LIGHT WENT OUT SERVICED AND BLED NR 3 HYD SYSTEM IAW MM 12-13-01. NR 3 QTY AND SYSTEM PSI - [SDR ARWA20071003](https://openairdocs.org/sdr/ARWA20071003.md): Engine · making metal · Oct 26, 2007 · N478CT · Doug DC1030F · Engine (Turbine/Turboprop) > AFTER DEPARTURE FROM SVVA, FELT VIBRATION IN COCKPIT, THEN SMOKE IN COCKPIT, NR 1 ENGINE OIL QUANTITY TO ZERO AND OIL PRESSURE BEGAN FLUCTUATING; SHUTDOWN ENGINE NR 1 AT 1758Z. TROUBLESHOOT NR 1 ENGINE PER TAFI 79-00-00; FOUND METAL CONTAMINATION ON SCAVAGE P - [SDR AMTA200700417](https://openairdocs.org/sdr/AMTA200700417.md): Slide · unserviceable · Sep 4, 2007 · N702TZ · Doug DC1030 · Escape Slide > L2 DOOR SLIDE/ AIR BOTTLE LOW PRESSURE LIGHT WILL NOT TEST. REMOVED AND REPLACED L2 DOOR SLIDE REF MM 25-61-07. SLIDE BOTTLE LOW PRESS LIGHT NOW CHECKS NORMAL. (K) - [SDR 0500641225](https://openairdocs.org/sdr/0500641225.md): Compressor · stalled · Apr 29, 2005 · N225NW · Doug DC1030 · Turbine Engine Compressor Section > DURING TAKEOFF ROLL, THE NR 1 ENGINE EXPERIENCED A COMPRESSOR STALL WITH EGT EXCEEDING RED LINE. TAKEOFF WAS ABORTED AT 110 KTS. THE ENGINE WILL BE REPLACED. - [SDR 0500451233](https://openairdocs.org/sdr/0500451233.md): Nozzle · departed · Apr 9, 2005 · N233NW · Doug DC1030 · Engine Collector/Tailpipe/Nozzle > AFTER TAKEOFF FROM MSP, THE NR 2 ENGINE EXHAUST NOZZLE DEPARTED FROM THE AIRCRAFT. THERE WERE NO ABNORMAL AIRCRAFT OR ENGINE INDICATIONS SO THE CREW WAS UNAWARE OF THE CONDITION. THE FLIGHT CONTINUED TO HNL WITHOUT INCIDENT. MAINTENANCE INSTALLED A REPLACEM - [SDR 0500051236](https://openairdocs.org/sdr/0500051236.md): Engine · failed · Jan 12, 2005 · N236NW · Doug DC1030 · Engine (Turbine/Turboprop) > WHILE AT CRUISE, THE CREW REPORTED THE NR 3 ENGINE FAILED WITH NO INDICATION OF OIL PRESSURE OR N2 SPEED. THE CREW SECURED THE ENGINE PER COM AND CONTINUED TO AMS LANDING WITHOUT INCIDENT. THE ENGINE WAS REPLACED. OPERATIONAL CHECK GOOD. - [SDR 0402061223](https://openairdocs.org/sdr/0402061223.md): Engine · fire · Nov 23, 2004 · N223NW · Doug DC1030 · Engine (Turbine/Turboprop) > DURING NR 2 ENGINE START, GROUND CREW REPORTED A TAILPIPE FIRE. CFR WAS CALLED OUT AND SPRAYED FIRE EXTINGUISHING AGENT INTO THE TAILPIPE OF THE NR 2 ENGINE. THE ENGINE WILL BE REMOVED. - [SDR 03FDEA02070](https://openairdocs.org/sdr/03FDEA02070.md): Engine · failed · Dec 5, 2003 · N310FE · Doug DC1030 · Engine (Turbine/Turboprop) > AT LEVEL OFF FL 330 EXPERIENCED HARD THUMP FOLLOWED BY GRINDING VIBRATION. IMMEDIATELY SHUT NR 1 DOWN. FOLLOWED QRH PROCEDURES, LANDED KPHX. PHX U C/W MD10-30 WORK CARD 71T0101-1, AND 71T0701-1. - [SDR 0301731232](https://openairdocs.org/sdr/0301731232.md): Autothrottle Sys · malfunctioned · Sep 10, 2003 · N232NW · Doug DC1030 · Auto Flight System > DURING TAKE-OFF ROLL THE CREW OBSERVED THE NR 1 ENGINE EXCEED LIMITS FOR N1, N2 AND EGT. THE NR 3 ENGINE ALSO EXCEEDED THE N2 LIMIT. THE TAKE-OFF WAS ABORTED AT 115KTS AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED THE NR 1 AND 3 ENGINES PER THE - [SDR 0101551211](https://openairdocs.org/sdr/0101551211.md): Gearbox · leaking · Apr 28, 2001 · N211NW · Doug DC1030 · Turbine Engine Accessory Drive > DURING CRUISE, THE NR 3 ENGINE OIL QUANTITY DECREASED TO ZERO AND OIL PRESSURE DROPPED INTO THE RED WITH THE LOW OIL PRESSURE WARNING LIGHT ILLUMINATED. THE ENGINE WAS SHUT DOWN AND THE FLIGHT DIVERTED TO MNL. THE LANDING WAS WITHOUT INCIDENT. MAINTENANCE R - [SDR 0002101235](https://openairdocs.org/sdr/0002101235.md): Fuel Filter · clogged · Jun 2, 2000 · N235NW · Doug DC1030 · Aircraft Fuel Filter/Strainer > DURING THE TAKEOFF ROLL, THE NR 3 ENGINE FUEL FILTER PRESSURE DROP LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AT 100 KTS AND AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE FUEL FILTER PER TAFI AND MAINTENANCE MANUALS. - [SDR CALA9900582](https://openairdocs.org/sdr/CALA9900582.md): Seal · leaking · May 26, 1999 · N12080 · Doug DC1030 · Turbine Engine Accessory Drive > F/A REPORTED SMOKE WITH AN OILY SMELL IN THE CABIN APPROX 30 MIN AFTER TAKEOFF. THE SMOKE CHECKLIST WAS ACCOMPLISHED WITH THE SMOKE AND ODOR DISSIPATING AFTER THE NR 2 ENGINE BLEED WAS SHUTOFF AND THE NR 2 PACK WAS SUPPLIED BY THE 1-2 ISOL VALVE. THE FLT WAS - [SDR 9807241227](https://openairdocs.org/sdr/9807241227.md): Packing · failed · Apr 24, 1998 · N227NW · Doug DC1030 · Turbine Engine Accessory Drive > WHILD CLIMBING THROUGH FL200 (TPE), THE NR 2 ENGINE OIL QUANTITY INDICATION DROPPED TO ZERO WITH THE INDICATED OIL PRESSURE DOWN TO 10 PSI. THE LOW OIL PRESSURE WARNING LIGHT ILLUMINATED ONE MINUTE LATER. THE CREW THEN FOLLOWED COM PROCEDURES AND SHUT DOWN T - [SDR 9806331228](https://openairdocs.org/sdr/9806331228.md): Compressor · stalled · Apr 6, 1998 · N228NW · Doug DC1030 · Turbine Engine Compressor Section > DURING TAKEOFF AT ROTATION, THE NR 3 ENGINE COMPRESSOR STALLED SEVERAL TIMES WITH VISIBLE FIRE REPORTED BY THE TOWER AND FLIGHT ATTENDANT. NOTICEABLE FUEL FLOW DECREASE AND POWER LOSS OCCURRED. BOTH FIRE BOTTLES FOR THE NR 3 ENGINE WERE DISCHARGED AND THE EN - [SDR 98FDEA00201](https://openairdocs.org/sdr/98FDEA00201.md): Engine · failed · Mar 15, 1998 · Doug DC1010F · Engine (Turbine/Turboprop) > IN LEVEL CRUISE AT FL350 AND APPROX M.83 NR 3 ENG APPEARED TO FLAMEOUT. ENG INDICATORS STABILIZED AT APPROX N1 33 PERCENT, EGT 530, NR 65 PERCENT, F/F 600. RED TAB CK LIST ACCOMPLISHED AND ENG RESTARTED AT FL 280. INSP INT AND EXH BOTH CK'D GOOD. FOUND VSV - [SDR 9804001221](https://openairdocs.org/sdr/9804001221.md): By Pass Switch · failed · Mar 8, 1998 · N221NW · Doug DC1030 · Engine Oil Indicating System > WHILE AT CRUISE, THE NR 3 ENGINE OIL FILTER CLOG LIGHT ILLUMINATED. THE CREW FOLLOWED THE COM 2.72.72 AND SHUT DOWN THE ENGINE. THERE WERE NO OTHER ABNORMAL INDICATIONS. THE AIRCRAFT RETURNED TO HNL AND LANDED WITHOUT DIFFICULTY. MAINTENANCE REPLACED THE O - [SDR 9701271234](https://openairdocs.org/sdr/9701271234.md): Duct · cracked · Jan 19, 1998 · N234NW · Doug DC1030 · Pneumatic Distribution System > DURING TAKEOFF ROLL, THE NR 1 ENGINE FIRE WARNING ILLUMINATED. THE TAKEOFF WAS ABORTED AT 120 KNOTS AND THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE FOUND A 14TH STAGE BLEED AIR DUCT CRACKED. THE DUCT WAS REPLACED AND ENGINE RUN AT HIGH POWER WAS NORMAL. - [SDR 9801221234](https://openairdocs.org/sdr/9801221234.md): Duct · damaged · Jan 18, 1998 · N234NW · Doug DC1030 · Pneumatic Distribution System > ON INITIAL CLIMB-OUT (BOM), THE NR 1 ENGINE FIRE WARNING LOOP A LIGHT ILLUMINATED. THREE MINUTES LATER THE NR 1 ENGINE FIRE WARNING LOOP B LIGHT ALSO ILLUMINATED. POWER WAS REDUCED TO 60 PERCENT ON THE NR 1 ENGINE AND BOTH INDICATIONS EXTINGUISHED. ALL OTHE - [SDR 9724501234](https://openairdocs.org/sdr/9724501234.md): Duct · cracked · Dec 29, 1997 · N234NW · Doug DC1030 · Compressor Bleed Control > DURING CLIMB TO FL390, THE NR 1 ENGINE NACELLE TEMPERATURES WERE VERY HIGH AND THE NACELLE LOOP A LIGHT ILLUMINATED. CREW FOLLOWED COM ABNORMAL PROCEDURES AND DESCENDED TO FL350 TO KEEP TEMPERATURES WITHIN LIMITS. FLIGHT CONTINUED WITHOUT FURTHER PROBLEMS. - [SDR 9714131225](https://openairdocs.org/sdr/9714131225.md): Engine · failed · Jul 23, 1997 · N225NW · Doug DC1030 · Engine (Turbine/Turboprop) > WHILE CLIMBING THROUGH FL180, THE NR 2 ENGINE EGT AND FUEL FLOW SPIKED WITH AN ASSOCIATED VIBRATION. THE ENGINE STABILIZED ON ITS OWN. THIRTY MINUTES LATER THE EGT REACHED MAXIMUM AND THE VIBRATION RETURNED. THE ENGINE WAS SHUT DOWN AND THE FLIGHT RETURNED - [SDR 9712551224](https://openairdocs.org/sdr/9712551224.md): Tr Unit · malfunctioned · Jun 26, 1997 · N224NW · Doug DC1030 · Engine Thrust Reverser > AFTER LANDING, THE NR 3 ENGINE WOULD NOT COME OUT OF REVERSE THRUST. THE ENGINE WAS SHUT DOWN. MAINTENANCE OPERATED NR 3 REVERSER AND FOUND NO PROBLEMS. AIRCRAFT RETURNED TO SERVICE. - [SDR 9711431224](https://openairdocs.org/sdr/9711431224.md): Tr Unit · malfunctioned · Jun 13, 1997 · N224NW · Doug DC1030 · Engine Thrust Reverser > AFTER LANDING, THE NR 3 ENGINE THRUST REVERSER DID NOT COME OUT OF REVERSE THRUST. THE ENGINE WAS SHUT DOWN AFTER CLEARING THE RUNWAY. MAINTENANCE LOCKED OUT NR 3 THRUST REVERSER PER MEL 78-1A. EXACT PART CAUSING PROBLEM TO BE DETERMINED. - [SDR 9626301220](https://openairdocs.org/sdr/9626301220.md): Compressor · stalled · Dec 6, 1996 · N220NW · Doug DC1030 · Engine (Turbine/Turboprop) > IN CRUISE FLIGHT AT FL350, NR 2 ENGINE EXPERIENCED A COMPRESSOR STALL. THE ENGINE WAS SHUT DOWN AND THE FLIGHT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND METAL FRAGMENTS IN THE TAILPIPE. THE ENGINE WAS REPLACED WITH A SERVICEABLE UNIT. - [SDR 9621051223](https://openairdocs.org/sdr/9621051223.md): Compressor · stalled · Oct 3, 1996 · N223NW · Doug DC1030 · Turbine Engine Compressor Section > AFTER TAKEOFF AT 1,000 FEET, THE NR 3 ENGINE EXPERIENCED TWO COMPRESSOR STALLS. FLIGHT CREW SHUTDOWN NR 3 ENGINE, DUMPED FUEL AND PERFORMED AN UNEVENTFUL LANDING AT DEPARTURE AIRPORT. MAINTENANCE REPLACING THE NR 3 ENGINE. - [SDR 9615501211](https://openairdocs.org/sdr/9615501211.md): Compressor · stalled · Jul 17, 1996 · N211NW · Doug DC1030 · Turbine Engine Compressor Section > AFTER TAKEOFF AND DURING CLIMB, THE NR 1 ENGINE EXPERIENCED COMPRESSOR STALL AT 6,000 FEET. CREW FOLLOWED COCKPIT OPERATING PROCEDURE, SHUT DOWN THE ENGINE, DUMPED 12,000 LBS OF FUEL AND RETURNED TO SEA WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTION OF THE - [SDR 9602821221](https://openairdocs.org/sdr/9602821221.md): Compressor · stalled · Feb 2, 1996 · N221NW · Doug DC1030 · Turbine Engine Compressor Section > EN ROUTE, THE NR 1 ENGINE EXPERIENCED SEVERAL COMPRESSOR STALLS. EGT WAS CLIMBING TO MAX AND SUBSEQUENT VIBRATION, POWER LEVER WAS PULLED BACK FOR THE REMAINDER OF THE FLIGHT. FOUND METAL IN TAILPIPE OF NR 1 ENGINE. ENGINE IS SCHEDULED FOR CHANGE IN MSP. - [SDR 9515931221](https://openairdocs.org/sdr/9515931221.md): Fuel Filter · dirty · Oct 14, 1995 · N221NW · Doug DC1030 · Engine Fuel Distribution > DURING TAKEOFF ROLL AT 80 KTS, THE FUEL FILTER PRESSURE DROP LIGHT ILLUMINATED FOR THE NR 3 ENGINE AND THE TAKEOFF WAS ABORTED. THE LIGHT CAME ON AGAIN FOR ONE MINUTE DURING CLIMB WHILE PASSING THROUGH 1,000 FT AND THE REMAINDER OF THE FLIGHT WAS UNEVENTFUL. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 engine_model_key = 'CF650C' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/engine/ge-cf6-50c/reports --- 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.