GE CF6-80 series

Service difficulty reports · 1,092

Newest first. General aviation reporting is voluntary.

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 engine_model_key = 'CF680'
  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 07FDEA00353Thrust Reverser · malfunctionedNR 1 T/R PRESSURIZED AS POWER INCREASED THROUGH 75-80 PERCENT N1. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A CATEGORY: C EXPIRATION: 16FEB07 "MEL 78-30-01-A: ENGINE NR 1 TSI OPENED FOR T/S.Feb 6, 2007 · N681FE · Airbus A300F4605R · Engine Thrust ReverserSDR 07FDEA00325Bleed Valve · leakingREPORT OF NR 1 FIRE INDICATION ON LANDING ROLLOUT AT KROC. AML LOGPAGE FROM FLIGHT CREW TO FOLLOW REFER TO WRI 72-00-9550 FOR ACTION TAKEN ON THIS ITEM. BLEED AIR TO NR 1 ENG DUCTING. FOUND BLEED VALVE VENT FITTING LEAKING EXCESSIVELY, VERIFIED THIS TO BEFeb 5, 2007 · N664FE · Airbus A300F4605R · Compressor Bleed ValveSDR 07FDEA00229Unknown · unknownNR 2 ENG REVERSER PRESSURIZED LIGHT ON ECAM ILLUMINATED AT GEAR RETRACTION ON TAKEOFF COMPLIED WITH E-CAM AND QRH ATB. R&R DIR. PILOT VALVE, HARNESS FOR T/R, PRESS REG. S/O VALVE,DIODE UNIT 20KM,MOD BLOCK 204VT, RELAYS 6KM&16KM, AWAITING FINAL OPS CHECK & EJan 31, 2007 · N665FE · Airbus A300F4605R · Engine Thrust ReverserSDR BB07008Filter · cloggedFLIGHT 1565, MXP-PHL: AFTER TAKEOFF, CREW RECEIVED A LEFT ENGINE FUEL FILTER MESSAGE. RETURNED TO MXP. MAINTENANCE REPLACED THE LEFT ENGINE FUEL FILTER. NO FURTHER DIFFICULTIES.Jan 16, 2007 · N248AY · Boeing 767201 · Engine Fuel DistributionSDR DL76G070023Turbine · making metalAPU AUTO SHUTDOWN AT GATE. FOUND METAL ON CHIP DETECTOR. REPLACED APU.Jan 6, 2007 · N1602 · Boeing 767332 · APU Core EngineSDR USAABB06085Filter · cloggedFLIGHT 1411, MAD-PHL: AFTER TAKEOFF, CREW RECEIVED A RIGHT ENGINE FUEL FILTER CLOG MESSAGE. FLIGHT RETURNED TO MAD AND LANDED WITH NO FURTHER DIFFICULTIES. MAINTENANCE REPLACED THE RIGHT ENGINE FUEL FILTER.Nov 17, 2006 · N248AY · Boeing 767201 · Engine Fuel DistributionSDR UIEA200600285Rail · crackedAFT CARGO SIDE RAIL DAMAGED.Nov 8, 2006 · N409MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR UIEA200600286Rail · crackedAFT CARGO SIDE RAIL CRACKED.Nov 8, 2006 · N409MC · Boeing 74747UF · Fuselage Miscellaneous StructureSDR 06FDEA03800Magnetic Seal · leakingAPPROX 1 HOUR OF FLIGHT NR 1 OIL QUANTITY STARTED TO DECREASE. ALL OTHER INDICATIONS NORMAL. AFTER APPROX 2 HOURS OF FLIGHT THE OIL PRESSURE STARTED TO FLUCTUATE PLUS OR MINUS 15 PSI. PER QRH THIS COULD BE ABNORMAL, DIVERTED TO KDEN. ENGINE NR 1 LEFT AT IOct 27, 2006 · N680FE · Airbus A300F4605R · Turbine Engine Oil SystemSDR HALA0600818Intercostal · crackedINTERCOSTAL AT BS 287-303 RBL 37 CRACKED AT LOWER FASTENER ROW ON WEB AND ANGLE. REMOVED INTERCOSTAL WEB AND ANGLE. FABRICATED NEW INTERCOSTAL AND WEB. REPAIR PARTS AND INSTALLED IAW SRM 51-40-02, SRM 51-40-05, AND 51-70-13/101 FIG 1.Oct 6, 2006 · N598HA · Boeing 767332 · Fuselage Miscellaneous StructureSDR HALA0600817Channel · damagedDURING REMOVAL OF RT HORIZONTAL STAB OB TE WEDGE, FOUND U-COMMON TO WEDGE AND STAB WITH LIGHTING STRIKE DAMAGE. REMOVED AND REPLACED RT HORIZONTAL STAB OB T/E WEDGE U-CHANNEL IAW SRM 51-40-02 AND DWG 183T1140.Oct 4, 2006 · N598HA · Boeing 767332 · Horizontal Stabilizer StructureSDR DL764060709Circuit Card · malfunctionedIDLE DISAGREE MSG, FWD TO MCO AND PLACARD RT ENG IN MIN GND IDLE INOP PER MEL 73-21-08A. REPLACED NR 2 HMU PER MM, NO HELP. REPLACED K433 AND K1026R, NO HELP. FOUND K433 NOT ENGAGING. REPLACED EEC DISCREETS GE CARD ENG, OPS CHECKS OK.Sep 2, 2006 · N831MH · Boeing 767424ER · Engine Fuel System WiringSDR 06FDEA03140Unknown · malfunctionedAFTER TAKEOFF, NR 1 OIL QTY WENT TO 3 QTS ON THE OIL QTY GAGE AND ON THE ECAM. DID AN AIR TURNBACK AND OIL QUANTITY BEGAN TO RISE BACK TO NORMAL AFTER TURNING BASE LEG. SERVICED 1 QT, PRESS AND OIL TEMP OK, MEL/CDL: 79-31-01-A CATEGORY: B EXPIRATION: 01SEP06Aug 29, 2006 · N414FE · Airbus A310203 · Engine Oil QuantitySDR HALA0600815Sill · corrodedCORROSION ON R-4 DOOR CUT OUT LWR SILL PLATE FOR FWD GIRT BAR FITTING STA 1487 RBL 90 WL 200. REMOVED R-4 DOOR CUTOUT LWR SILL PLATE FOR FWD GIRT FITTING AT BS 1487, RBL90, WL 200. REMOVED CORROSION DAMAGE, DETERMINED OUT OF LIMITS. FABRICATED NEW LWR SILL Jul 10, 2006 · N598HA · Boeing 767332 · Fuselage Miscellaneous StructureSDR HALA0600813Stringer · gougedSTRINGER GOUGED IN RADIUS STA 589 STR 8R. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03 PAGE 101 AND 103 DETAIL 2, CUT OUT DAMAGED ON STR. 8R BS 578 - 600 IAW SRM 53-00-03 REPAIR 201 STEP 1 SHEET 1,FOUND MAX ID IAW SRM FIG 201 SHEET 3 TABLE 2 AND MFG BWG Jun 28, 2006 · N598HA · Boeing 767332 · Fuselage Main, Longeron/StringerSDR HALA0600812Intercostal · crackedCRACKED INTERCOSTAL STA 742-764 RBL 73 WL 199. REMOVED AND INSTALLED NEW INTERCOSTAL AT STA 742- STA 764 RBL 73, WL 199.Jun 27, 2006 · N598HA · Boeing 767332 · Fuselage Miscellaneous StructureSDR HALA0600809Support Angle · crackedVERTICAL SUPPORT ANGLE CRACKED STA 347 RBL WL 199. REMOVED VERTICAL SUPPORT AT RT STA 347 RBL, WL 199 IAW SRM 51-40-02-06-0, PG.2 RECEIVED NEW PART NR 284T0611-16 IAW MFG DWG 284T0301, FRAME 2 OF 3 AND MFG DWG 284T0611 FRAME 1 OF 1, DRILLED HOLES IAW SRM 51-Jun 26, 2006 · N598HA · Boeing 767332 · Fuselage Miscellaneous StructureSDR HALA0600811Floor Support · crackedCRACKED FLOOR SUPPORT ANGLE STA 325-347 LBL 40, WL 200. REMOVED FLOOR SUPPORT ANGLE AND INSTALLED NEW ANGLE IAW SRM 51-20-01-0G-0, SRM 51-21-10 AND SRM 51-40-02 AND SRM 51-40-05.Jun 26, 2006 · N598HA · Boeing 767332 · Fuselage Miscellaneous StructureSDR BB06051Engine · oil consumptionFLIGHT 893, FRA-PHL: LEFT ENGINE OIL CONSUMPTION HIGH. DIVERTED TO KEF. MAINTENANCE REPLACED GASKET AT D-SUMP SCAVENGE LINE. RAN ENGINE, NO LEAKS NOTED. AIRCRAFT WAS THEN MAINTENANCE FERRIED FROM KEF-PHL. DURING FERRY FLIGHT, LEFT ENGINE CONTINUED TO CONSJun 23, 2006 · N645US · Boeing 767201 · Engine (Turbine/Turboprop)SDR DL764060493Unknown · malfunctionedAPU AIR INOP FOR ENG START. RESTORED SHUT OFF VLV TO NORMAL. MANUALLY OPENED APU SHUT OF VLV, APU SHOT OFF VLV OPS NORMAL. PACK OPS NORMAL, DRY MOTOR ENGINES NO PROBLEMS. APU SHUT OFF WAS CYCLED APPROX 15 TIMES, NO DEFECTS NOTED. ASCTU BITE HAS NO CURRENTJun 15, 2006 · N826MH · Boeing 767432ER · APU Bleed Air SystemSDR DL764060489Turbine Blades · damagedPERFORM BORO OF NR 1 ENG DUE TO PRIOR EGT EXCEEDENCE. FOUND DAMAGE T1 BLADES AND END CAPS MISSING. REPLACED NR 1 ENG.Jun 10, 2006 · N839MH · Boeing 767432ER · Turbine SectionSDR 06FDEA2192Control Unit · malfunctionedDURING TAKEOFF ABOUT 90 KIAS ECAM FLASHING NAC HEAT WAS ABOVE 100 DEGS. COMPLETED ABORT. NO ABNORMAL ENGINE INDICATIONS NOTED. REPLACED NR 2 FIRE DETECTION CONTROL UNIT IAW A310 MM 26-12-11-04 AND EA 6-2610-72097. RAN NR 2 ENGINE IAW CHAPTER 5 AND 6-11 A31Jun 4, 2006 · N433FE · Airbus A310203 · Fire DetectionSDR FWT2006F00001Relay · malfunctionedAFTER 00:25 FLYING MINUTES, RETURNED TO GROUND DUE TO 1-30-32-03-01 EICAS MSG L AOA PROBE DISPLAYED. L AOA PROBE HEAT LIGHT ILLUM. 2-30-33-06-00 EICAS MSG TAT PROBE DISPLAYED, TAT PROBE HEAT LIGHT ILLUM. 3-30-31-09-00 EICAS MSG PROBE HEAT DISPLAYED 2 OR MORMay 25, 2006 · N316LA · Boeing 767* · Pitot/Static SystemSDR P5CA0601841Manifold · faultyON INITIAL CLIMB, AFTER FLAP RETRACTION, EICAS CAUTION MESSAGE OVHT ENG 1 NAC. COMPLIED WITH CHECKLIST AND MESSAGE CLEARED, TRIED TO CONTINUE WITH CLIMB, MESSAGE RETURNED. RETURN TO LAX. REMOVE AND REPLACE NR 1 ENGINE TWELVE SEGMENT LPT COOLING AIR MANIFOLDMay 16, 2006 · N450PA · Boeing 74746NF · Engine Cooling SystemSDR P5CA0601481Manifold · defectiveON INITIAL CLIMB, AFTER FLAP RETRACTION, EICAS CAUTION MESSAGE OVHT ENG 1 NAC. COMPLIED WITH CHECKLIST AND MESSAGE CLEARED, TRIED TO CONTINUE WITH CLIMB, MESSAGE RETURNED. RETURN TO LAX. REMOVE AND REPLACE NR 1 ENGINE TWELVE SEGMENT LPT COOLING AIR MANIFOLDMay 16, 2006 · N450PA · Boeing 74746NF · Engine Cooling SystemSDR 06FDEA1927Pressure Switch · malfunctionedRECEIVED "ENG 1 OIL FILTER". PROCEEDED VIA QRH PROCEDURES, SHUT DOWN ENGINE AND DESCENDED TO 300 (FROM 360). ALL ENGINE PARAMETERS NORMAL OTHER THAN THE ALERT. DECLARED EMERGENCY AND LANDED AT PANC. INSPECTED MASTER CHIP DETECTOR AND SCAVANGE FILTER ELEMEMay 15, 2006 · N615FE · Doug MD11F · Engine Oil PressureSDR 2006FA0000428Actuator · crackedNLG RETRACT ACTUATOR WAS RECEIVED WITH THE PISTON ROD CRACKED. 3 CRACKS RUN AROUND THE CIRCUMFERENCE OF THE ROD AT THE THREADED END. CRACKS RUN ABOUT 95 PERCENT AROUND ROD BUT DO NOT CONNECT (RUN IN A SPIRAL) CORROSION FOUND ON INTERIOR THREADS. CORROSION AApr 21, 2006 · N325OP · Rolsch LS3A · Landing Gear ActuatorSDR 06FDEA1438Throttle · obstructedDESCENDING FROM 380 13000 AT YYC, NR 2 THROTTLE WOULDN'T RETARD TO IDLE. COMPLIED WITH QRH "THROTTLE LEVER JAMMED" NR 2 THROTTLE WOULD ADVANCE BUT NOT RETARD TO IDLE. IT WOULD ONLY GO AS LOW AS 10-15 DEGREES ON THE QUADRANT. ENGINE SHUT DOWN AS PER QRH. WIApr 11, 2006 · N434FE · Airbus A310203 · Power LeverSDR 06FDEA1357Pressure Switch · malfunctionedNR 1 FUEL FILTER CLOG CAME ON ON T/O ROLL. RELEASED FOR SERVICE PER MEL/CDL: 73-36-03-01. NR 1 FUEL CLOG LIGHT(S) INOP. VERIFY AND RECORD IN AML/EAML THAT FILTER HAS BEEN CHECKED FOR CONTAMINATION ONCE EACH FLIGHT DAY. CHECKED FILTER PER A310 AMM CH 73-12-Apr 10, 2006 · N404FE · Airbus A310203 · Engine Fuel DistributionSDR DL76G060207Line · seizedDUE TO HOC HAD MSU TO REPLACE THE GEARBOX SHUTOFF VALVE AND SHUTTLE VALVE. MTC FOUND LINES TO TO SHUTOFF VALVE SHUTTLE VALVE SEIZED. REPLACED APU PER AMM.Mar 19, 2006 · N1611B · Boeing 767332 · APU Cowling/ContainmentSDR 06FDEA0803Stringer · damagedUPON REMOVAL OF LT WING UPPER STRINGER 13 STRINGER END FOUND TWO FASTENER HOLES ELONGATED AT XORS 562 AND XORS 550. REPAIR CARRIED OUT IAW FEDEX EA 1-5710-90767.Feb 22, 2006 · N615FE · Doug MD11 · Wing, Longeron/StringerSDR 06FDEA0802Hinge Fitting · crackedRT WING, OB FLAP IB HINGE FITTING AT MOST OB LOWER BOLT HOLE FOUND WITH CRACK INDICATION. REPLACED AS PER AMM 27-50-30-4. OTBD FLAP ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-00-5 FOUND SATISFACTORY.Feb 21, 2006 · N585FE · Doug MD11 · Trailing Edge FlapsSDR DL76G060142Apu · making metalAPU AUTO SHUTDOWN. BITE CHECK OF ECU SHOW APU STARTER REPLACED SAME, NO HELP. FOUND CHIP DETECTOR FULL OF METAL SHAVINGS. REMOVED AND REPLACED APU ASSY PER AMM. GROUND RUNUP LEAK CHECK GOOD.Feb 20, 2006 · N152DL · Boeing 7673P6 · APU Core EngineSDR 06FDEA0715Valve · unknownWHILE APPLYING POWER FOR T/O, ECAM ALERT NR 1 REVERSER PRESSURIZE DEACTIVATING T/R MEL. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A CATEGORY: C EXPIRATION: "MEL 78-30-01-A: ENGINE 1 THRUST REVERSER INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POFeb 17, 2006 · N664FE · Airbus A300F4605R · Engine Thrust ReverserSDR 06FDEA0702Indicator · malfunctionedDURING CLIMBOUT AFTER TAKEOFF NR 1 ENG EGT LIMIT WAS EXCEEDED. EGT POINTER PAST 1000 DEGREE MARK. ON FINAL EGT GAUGE WENT TO ZERO AND BLANK THEN CAME BACK UP TO ABOUT 400 DEGREES SIMILAR TO NR 2 ENG EGT INDICATOR. INSPECTED ENGINE EXHAUST AND INLET FOR FOD Feb 16, 2006 · N434FE · Airbus A310203 · Engine Temperature Indicating SystemSDR DL764060124Pump · leakingRIGHT ENG HYD RESERVIOR AND EICAS RIGHT HYD QTY AND A QUANTITY OF 4. FOUND NR 2 ENG HYD PUMP LEAKING. REPLACED PUMP PER MM. LEAK AND OPS CHECKS GOOD.Feb 12, 2006 · N834MH · Boeing 767432ER · Hydraulic Pump (Electric/Engine), MainSDR 06FDEA0703Line · failedSLOWING TO 250 KNTS FOR DESCENT, NOTICED AN INCREASED VIBRATION THAT FELT LIKE IT WAS ENGINE. FOUND T/R -Y- CHECK VALVE NR 1 ENGINE LOWER SUPPLY LINE BLOWN APART. REMOVED LINE AND ORDERED PARTS. UPON FURTHER INVESTIGATION ON WHY THE T/R V AIR TUBE CAME APARFeb 11, 2006 · N668FE · Airbus A300F4605R · Engine Thrust ReverserSDR 06FDEA0690Line · failedSLOWING TO 250 KNTS FOR DESCENT NOTICED AN INCREASED VIBRATION THAT FELT LIKE IT WAS ENGINE. NORMAL LANDING KMHT (NOT A DIVERSION). FOUND T/R -Y- CHK VALVE NR 1 ENGINE LOWER SUPPLY LINE BLOWN APART. REMOVED LINE AND ORDERED PARTS. UPON FURTHER INVESTIGATIOFeb 11, 2006 · N668FE · Airbus A300F4605R · Engine Thrust ReverserSDR DL764060099Actuator · leakingFUEL LEAK FROM APU DRAIN MAST. FORWARD TO FLIGHT CREW PLACARD PER MEL 49-11-01B. AIRCRAFT FLOWN TO HNL TO MTC REPAIR APU. REPLACE IGV ACTUATOR PER M/M.Feb 3, 2006 · N840MH · Boeing 767432ER · APU Core EngineSDR TAMF20060001ODuct · delaminatedDURING WEEKLY CHECK, FOUND DELAMINATION ON NR 1 ENGINE RT T/R (FAN COWL DUCT) INNER SKIN (DAMAGE MEASUREMENT IS 34 BY 13.5 INCH), CAUSED BY LIBERATION OF 2 OUTLET VANES ON IDG AIR/OIL COOLER ASSY P/N 35E38-5. FAN REVERSER P/N 683L136G08 WAS REMOVED AND TEMPORJan 16, 2006 · N770QT · Boeing 767200 · Nacelle/Pylon, Plate/SkinSDR FWT2006F00000Warning System · activatedFWD EQUIPMENT OVERHEAT DISPLAYED AND OVERHEAT LIGHT REMAINED EXTIN AFTER SELECTOR WAS POSITIONED TO STBY. ABORTED TAKEOFF AT 90KNTOS. PERFORMED FIM, OPS CHECK SYSTEM FOUND GOOD AND PERFORMED AIRCRAFT INSPECTION OF HIGH ENERGY STOP ABORTED TAKEOFF IAW AMM. AIJan 9, 2006 · N316LA · Boeing 767* · Central WarningSDR BB05107Engine · bird ingestionLGW FLT 15, EN ROUTE MUC TO PHL - A BIRD STRUCK THE LEFT ENGINE AT ROTATION DURING TAKEOFF. THE CREW INITIALLY HEARD AN ABNORMAL SOUND. ALL ENGINE PARAMETERS RETURNED TO NORMAL AFTER AN INITIAL DROP IN ENGINE READINGS. THE CREW DECIDED TO DIVERT TO LGW TO Dec 25, 2005 · N652US · Boeing 7672B7 · Engine (Turbine/Turboprop)SDR AU510001522Proximity Sensor · false indicationAFT CARGO DOOR OPEN INDICATION. INSPECTION FOUND THE DOOR SECURE. SUSPECT FAULTY SENSOR.Dec 12, 2005 · Airbus A330* · Door Warning SystemSDR AU510001537Proximity Sensor · faultyAFT CARGO DOOR WARNING. INVESTIGATION FOUND THE DOOR CLOSED AND LOCKING MECHANISM SERVICEABLE. SUSPECT CAUSED BY FAULTY SENSOR.Dec 12, 2005 · Airbus A330* · Door Warning SystemSDR AU510001562Computer · failedFLIGHT CONTROL PRIMARY COMPUTER (FCPC) FAILED. FCPC REMOVED AND SENT FOR TEST AND REPAIR. INVESTIGATION FOUND THE POWER SUPPLY FAULTY.Dec 12, 2005 · Airbus A330* · Flight Control SystemSDR AU510001666Tire · low pressureLEFT NOSE WHEEL TIRE LOW PRESSURE. NOSE SHIMMY ALSO EVIDENT.Dec 12, 2005 · Airbus A330* · TireSDR AU510001752Control Unit · faulty(AUS) CARGO COMPARTMENT SMOKE WARNINGS. FORWARD CARGO FIRE BOTTLES DISCHARGED. EMERGENCY LANDING CARRIED OUT. LOCAL AUTHORITIES REPORTED A (WHITE POWDER) IN THE WHEEL WELL AREA. DURING EMERGENCY EVACUATION, DOOR 1L ESCAPE SLIDE FAILED TO DEPLOY. ALL OTHER SLIDDec 12, 2005 · Airbus A330300 · Smoke DetectionSDR AU510001899Light · failedFO READING LIGHT FAILED. SMOKE AND FUMES IN COCKPIT. INVESTIGATION FOUND SWARF MATERIAL IN THE LENS ASSEMBLY FOLLOWING REMOVAL OF THE COVER.Dec 12, 2005 · Airbus A330* · Flight Compartment LightingSDR AU510001917Slide · failed(AUS) DURING EMER EVAC FOR FIRE WARNING, DOOR 1L SLIDE FAILED TO DEPLOY. DOOR OPENING HANDLE HAD BEEN MOVED TO FULL UP POSITION, DOOR WAS FOUND TO HAVE OPENED APPROX 3 INCHES, JAMMED IN THAT POSITION. DOOR ARMING HANDLE HAD BEEN MOVED FROM ARMED POSITION TO DDec 12, 2005 · Airbus A330* · Escape SlideSDR AU510001946Wire · failed(AUS) DOOR 3 EMERGENCY EXIT LIGHTS (2OFF) FAILED. SUSPECT WIRING DEFECT. (CASA NR 510001946)Dec 12, 2005 · Airbus A330300 · Light System Wiring
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