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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR UIEA200800351Skin · dentedNR 10 VC FLAP BULLNOSE HAS DENT. REPAIRED AS PER SRM 57-43-02.SDR FDEA200812235266Pressure Switch · frozenLOW SPEED REJECTED T/O AT 75KT DUE TO LEVEL 2 ENGINE OIL FILTER 3 ALERT. COMPLETED RTO AND OIL FILTER CHECK LISTS. OIL TEMPS WERE ALL AT 65 DEGREES. ACFT COLD SOAKED FROM SITTING IN VERY COLD AIR FOR 2 DAYS. CONTACTED MX AND AGREED THAT PROBLEM WAS MOST LIKESDR FDEA200812125132Relay · failedDURING T.O. ROLL NR 1 ENG N1 AND N2 SURGED AFTER TOGA, DROPPED 2 % 3 TIMES. NOTED EGT AND F.F. GAGES MIRRORED N1 AND N2. REJECTED TO AT 85 KTS. FOLLOWED QRH PROCEDURE. RETRIEVED FAULT CODE 351-18, 28 VDC POWER DISCONNECT FAULT. PER TSM REMOVED AND REPLACEDSDR DL764081654Pseu · damagedLOW SPEED ABORT FOR TAKEOFF WARNING EICAS FLAPS FOUND DURING TROUBLESHOOTING WENT TO RERACK PSEU AND FOUND ALIGNMENT KEY BROKEN. REMOVED KEY RESEATED PSEU. FAULT REMOVED BITE CHECK OF FSEU AND PSEU, NO FAULTS NOTED.SDR UIEA2008341Skin · puncturedAT DEPARTURE FOUND TAIL PUNCTURED THRU FUSELAGE EXTERNAL SKIN JUST FWD OF STA 2598 AT 6 O'CLOCK POSITION APPROX 11.5 FT BY 16 INCHES. CUTOUT FUSELAGE SKIN DAMAGE AND LOWER CHORD AT STA 2598 AS PER SRM 53-00-01 AND 51-70-12. REPAIR NOT COMPLETED AT THIS TIME.SDR FDEA200811114854Hmu · failedENGINE NR 3 FLAMED OUT DURING DESCENT AT APPROX HIGH 20'S. ON DEBRIEF CREW REPORTED RESTART WAS NORMAL AND ENGINE OPERATED NORMAL REMAINDER OF FLIGHT. T/S NOW IN PROGRESS. REMOVED AND REPLACED NR 3 HMU PER MM 73-21-01-4, ALL LEAK CHECKS ON. FUEL AND OIL CHSDR 08FDEA04074Actuator · brokenFOUND NR 1 LT T/R DAMAGED. FOUND LT LWR SCREWJACK BROKE OFF AND DAMAGED THE TRANSLATING COWL, DAMAGED PARTS FOUND AT RUNWAY TOUCH DOWN AREA. VISUALLY INSPECTED LT WING, FLAP, AFT FUSELAGE, STAB SURFACE AND NO DAMAGE FOUND. MANUAL DEPLOY AND STOW NR 1 RT REVSDR CA080926005Connector · damaged(CAN) DURING STATION TRANSIT, CABIN CREW REPORTED SMOKE COMING FROM AFT GALLEY, WITH SMOKE WARNING, WHEN GALLEY ELECTRICAL PWR WAS PUT ON. GALLEY POWER WAS REMOVED FROM THE AFT GALLEY. DURING MX INVESTIGATION, THE GALLEY CONNECTOR 38 MC WAS FOUND DAMAGED WITSDR P5CA0801575Shutoff Valve · defectiveNR 1 ENGINE AUTO START FAILED. TROUBLESHOT AND FOUND NR 1 PRSOV DEFECTIVE AMM36-11-04. (K)SDR 08FDEA03645Ecu · failedDURING CLIMB NR 2 ENG N1, FF, EGT BECAME UNSTABLE, ASSOCIATED WITH ENGINE SURGING. FOLLOWING NR 2 ENG FADEC BITE DISPLAY: BITE CHA CHB 270 84120 84120 271 99080 99080 272 20000 20000 273 274 ON 350-354. FADEC GROUND TEST: FOUND FAULT CODE 352-21 SDR 08FDEA03646Hmu · failedNR 1 ENGINE N1 INDICATION BECAME UNSTABLE DURING CLIMB. REPEAT WRITE-UP. THEN EGT EXCEEDED LIMITS AT 952 DEG. THEN FUEL FLOW INDICATION BECAME UNSTABLE WITH SURGING AND YAW. PULLED TO IDLE N-1 AND FF INDICATION REMAINED UNSTABLE BUT SURGING STOPPED. PERFORSDR 08FDEA03093Hmu · failedAPPROACHING CRUISE ALTITUDE GOT A LEVEL 2 'ENG 2 N2 LOW' FOLLOWED BY A ROLL BACK ON ENG 2. ALL INDICATIONS INDICATED FLAME OUT. ACCOMPLISHED QRH PROCEDURES AND LANDED WITHOUT INCIDENT. DID NOT ATTEMPT A RESTART. PERFORMED ENGINE POST-WINDMILLING INSPECTIONSDR AIEA200800260Engine · oil consumptionENGINE NR 3 OIL QTY WENT TO 0 (3 HOURS AFTER TAKEOFF). ENGINE SHUT DOWN PRECAUTIONARY. FIM 79-00-00 FOLLOWED. INSPECTED FOR OIL LEAK. NO WETTING FOUND. REPLENISHED 22 QTS OIL AND LEAK AND OPS CHECK PERFORMED. NO LEAK FOUND. IDG AND STARTER DRAIN LINE CASDR UPS08M52620Switch · sparksSPARKS/SMOKE FROM WING & RUNWAY TURNOFF LIGHT SWITCHES. OPENSDR UPS08652624Module · malfunctionedRUDDER TRIM STUCK AT 4 UNITS. T/S IAW FIM 27-21-00 FIG 106 FOUND RUDDER TRIM CONTROL PANEL FAULT. R/R AILERON AND RUDDER TRIM CONTROL MODULE IAW MM 27-21-23-2. OPS GOOD.SDR UIE2008F00010Engine · power lossON TAKEOFF ROLL POWER WAS ADVANCED TO 70 PERCENT. N1 ENGINE 1,3, AND 4 ADVANCED NR 2 LAGGED SIGNIFICANTLY BEHIND, TAKEOFF ROLL ABORTED AT 40 KNOTS, AIRCRAFT TAXIED TO RUNUP AREA WHERE ENGINE RUN UP WAS PERFORMED AND NR 2 WAS NOW NORMAL. (K)SDR P5CA0801569Engine · failedAT DESCENT, ENGINE NR 4 SHUT DOWN AND RESTARTED 6 TIMES. AFTER THE 6TH RESTART ENGINE SHUTDOWN AND LEFT OFF. AIRCRAFT LANDED SAFELY AND WITHOUT DECLARING EMERGENCY. FOUND NR 4 ENGINE OUT OF BOROSCOPE LIMITS PER AMM. REMOVED AND REPLACED NR 4 ENGINE. (A)SDR DL764080769Cover · missingLEFT ENG SHUTDOWN AT 15000 FT DUE TO LOW OIL PRESSURE AND QUNTITY DURING CLIMBOUT. INFO DURING CHECKLIST AND SUBSEQUENT SHUTDOWN ENG WAS RUN AT 8 PSI FOR LESS THAN 30 SEC AT CRUISE POWER AND APPROX 3-4 MIN AT IDLE, PLS CHECK FOR TIME ACCURACY. OPENED LT ENG SDR TAMF20080022OCircuit Card · burnedAFTER TAKEOFF WHEN LANDING GEAR LEVER WAS MOVED TO UP A SMOKE FUME APPEARED IN THE COCKPIT (P3-1) WITH NO VISUAL EVIDENCE OF FIRE. AC RETURNED TO DEPARTURE. AFTER MAINT, INSP ON PANEL LIGHT DOOR MODULE KIT (P3-1) 2 DIODES FOUND BURN. NO ADDITIONAL DAMAGES WESDR TAMF20080015SSill · corrodedDURING C2 CHECK WAS FOUND CORROSION ON LOWER SILL OF LARGE CARGO DOOR CUTOUT BETWEEN STA 500-522. DAMAGED AREA WAS REPAIRED IAW EWO 767 53-074 AND MFG SERVICE REQUEST 1-791518899. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FAA FORM 8100-9 WAS ISSUED APPROVING THISDR TAMF20080021SSkin · corrodedDURING (C2) CHECK WAS FOUND SKIN PN 146T3240 WITH CORROSION. STA 1417, STRINGER 36 RT. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-075 AND SR 1-79124788. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR.SDR TAMF20080018SRib · corrodedCORROSION ON LT WING OB L/E RIB LOWER OUTER SHROUD AT STA 933.73 AND 938.73. (2) RIBS WERE FABRICATED AND INSTALLED IAW MFG AUTHORIZATION PO214294 AND PO214297, DRAWINGS 117T2224 AND 114T2223 AND SRM 51-40-02/1-3 AND 7.SDR TAMF20080019SRib · corrodedCORROSION ON LT WING OB L/E RIB LOWER OUTER CHORD AT STA 441.60. CORRECTIVE ACTION: RIB WAS FABRICATED AND INSTALLED IAW MFG AUTHORIZATION PO214240, DRAWING 114T2200 AND SRM 51-40-02 PG 1-7.SDR TAMF20080014SSpar · corrodedDURING C2 CHECK INSPECTION WAS FOUND CORROSION ON THE CENTER WING REAR SPAR WEB NEAR RBBL 75 AT THE REAR SPAR BULKHEAD FITTINGS. DAMAGED AREA WAS BLENDED TO A MINIMUM WEB THICKNESS OF 0.288 INCHES AND NDT (EDDY CURRENT) INSPECTION DID NOT REVEAL ANY REMAINING SDR TAMF20080013SDoor · corrodedDURING C2 CHECK INSPECTION WAS FOUND CORROSION ON MAIN FUEL TANK ACCESS DOORS 541LB AND 541GB PN: 112N6101-3. DAMAGED AREA WAS BLENDED TO A MINIMUM DOOR THICKNESS OF 0.120 INCHES (541LB) AND 0.106” INCHES (541GB). NDT (EDDY CURRENT) INSPECTION WAS PERFORMED ASDR TAMF20080020SFitting · crackedDURING C CHECK INSPECTION WAS FOUND A CRACK ON CF6-80C2, THRUST REVERSER FITTING P/N 3114M90-001 AT 2 O’CLOCK. DAMAGED AREA WAS REPAIRED IAW EWO 767 54-036 AND TAC-080316. THIS REPAIR IS CLASSIFIED AS TEMPORARY REPAIR AND THE AFFECTED FITTING MUST BE CHANGED ASDR UIEA200800029Gearbox · crackedNR 4 ENGINE GEAR BOX WAS FOUND WITH A 3.0 INCH CRACK ON INBOARD SIDE OF FUEL PUMP DRIVE PAD AREA. ENGINE CHANGE IS CURRENTLY IN PROGRESS.SDR 07FDEA05139Valve · failedON TAKEOFF ROLL AS POWER WAS ADVANCED TO FLEX POWER LEFT ECAM SHOWED "ENG 1 REV PRESSURIZED", W/MASTER CAUTION. REJECTED TAKEOFF AT 60KTS. AS THROTTLES REDUCED TO IDLE, LEFT ECAM AND MASTER CAUTION CLEARED. RELEASED FOR SERVICE. FOUND FAULTY DPV. REMOVED ASDR 07FDEA05065Unknown · malfunctionedNR 2 ENG RPM LO ON CLIMB-OUT (FLAMEOUT). CREW REPORTED DURING CLIMB-OUT NR 2 ENG N1 WENT TO 11 PERCENT WITH N2 ALMOST 0 PERCENT, LOW EGT, AND FF APPROX 600 PPM. INSP NR 2 ENG INLET AND EXH FOR METAL PARTICLES AND FOD. NO DEFECTS NOTED. CHKD NR 2 ECU, NO SDR 07FDEA04922Pressure Switch · malfunctionedDURING CRUISE FLIGHT, GOT A LEVEL 2 ALERT "ENG 2 OIL FILTER". THIS ALERT DID NOT GO AWAY, EVEN WITH THROTTLE IDLE. ENGINE SHUT DOWN IAW QRH NO OTHER ABNORMAL INDICATIONS. REPLACED OIL FILTER DIFFERENTIAL PRESSURE SWITCH PER MM 79-35-01-4. REFLUSH NR 2 ENG SDR 07FDEA04889Thermocouple · malfunctionedDURING CLIMB, NR 2 EGT (POINTER/DIGITAL) WERE FLUCTUATING +/- 50C. ALL OTHER ENGINE PARMS NML. NO YAW NOTED. PULL NR 2 THROTTLE BACK TO ABOUT 10 PERCENT, NO CHANGE. HIGHEST EGT WAS APPROX 860C. AFTER ABOUT 10 MINS EGT STAB AT ABOUT 800C AND NML REST OF FLSDR NOCA16307Warning System · activatedRIGHT ENG HPSOV EICAS MESSAGE. CREW FOLLOWED QRH AND TURNED OFF BLEED SWITCH. CREW STATED THAT THE RIGHT PACK WAS INOP AFTER TURNING BLEED SWITCH OFF. WITH BLEED ISSUE AND INOP PACK THE A/C CANNOT CONTINUE ETOPS A/C DIVERTING TO GANDER. SDR REMAINS OPEN.SDR TAMF20070037SStrap · corrodedDURING INSPECTION OF (C2) CHECK WAS FOUND A CORROSION ON CARGO DOOR SURROUND STRUCTURE, SAFE FAIL STRAP P/N 146T8048-3. REMOVED, FABRICATED AND INSTALLED A NEW FAIL SAFE STRAP P/N 146T8048-3 IAW EWO 767-53-057 AND SERVICE REQUEST 1-557292575. THIS REPAIR CONSDR TAMF20070034SSill · corrodedDURING INSPECTION OF (C2) CHECK WAS FOUND A CORROSION ON CARGO DOOR SURROUND STRUCTURE, MAIN SILL, OUTER CHORD STA 632 RT. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-059 AND SERVICE REQUEST 1-533874348. THIS REPAIR CONSTITUTES A MAJOR REPAIR, FORM 8100-9 WAS ISSDR TAMF20070035SSill · corrodedDURING INSPECTION OF (C2) CHECK WAS FOUND A CORROSION ON CARGO DOOR SURROUND STRUCTURE, MAIN SILL, OUTER CHORD STA 569.65 RT. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-056 AND SERVICE REQUEST 1-527218048. THIS REPAIR CONSTITUTES A MAJOR REPAIR, FORM 8100-9 WASDR TAMF20070036SSkin · corrodedDURING INSPECTION OF (C2) CHECK WAS FOUND A CORROSION ON PRESSURE SKIN STA 582 BETWEEN STRINGER 34-35 RT. DAMAGED AREA WAS REPAIRED IAW EWO 767-53-058 AND SERVICE REQUEST 1-526668594. THIS REPAIR CONSTITUTES A MAJOR REPAIR, FORM 8100-9 WAS ISSUED APPROVING THSDR DL764070440Engine · failedNR 1 ENG FAILED HPC BORO OP 5039. REPLACED NR 1 ENG PER TRANS 14T103.SDR HALA0700166Trim System · malfunctionedETOPS SIGNIFICANT SYSTEM - STAB TRIM LEVERS SPLIT IN CLIMB AND IN CRUISE .5 INCH./RIGGED STAB TRIM LEVERS IAW AMM 27-41-00 5639. C/W STAB TRIM CONTROL OPS TEST IAW MM 27-41-00-715-251.SDR TAMF20070002SWeb · crackedDURING INSPECTION CHECK WAS FOUND A CRACK AT AFT WING FAIRING WEB STA 1080 BL 62-70-LT. DAMAGED AREA WAS REPAIRED IAW EWO 767 53-035 AND MFG SERVICE REQUEST 1-311853573. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR.SDR BB07032Transmitter · failedFLIGHT 1015, PHL-STT: ABOUT 20 MINUTES AFTER DEPARTURE, RIGHT ENGINE OIL QUANTITY INDICATION DROPPED TO ZERO. OIL PRESSURE REMAINED NORMAL. FLIGHT RETURNED TO PHL. MAINTENANCE REPLACED THE RIGHT OIL QUANTITY TRANSMITTER. NO FURTHER FAULTS.SDR DL76G070234Door · malfunctionedAFTER APU SHUTDOWN GOT STATUS MSG AND APU DOOR MSG ON EICAS. FWD TO MCO AND PLAC PER MEL 49-15-01B. APU DOOR LOCKED IN FULLY OPEN POSITION.SDR TAMF20070001SFairing · crackedDURING INSPECTION, FOUND A CRACK AT AFT WING FAIRING WEB STA 1080, BL 62-70, LT. DAMAGED AREA WAS REPAIRED IAW MFG SERVICE REQUEST 1-303353670 AND EWO 767-53-031. THIS REPAIR CONSTITUTES A MAJOR REPAIR. FAA FORM 8100-9 WAS ISSUED APPROVING THIS REPAIR.SDR 07FDEA00601Pilot Valve · unknownAFTER APPLYING TAKEOFF POWER ON RUNWAY, ECAM ALERT NR 2 ENG REVERSER PRESSURIZED. REJECTED TAKEOFF ABOUT 70 KTS. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A CATEGORY: C EXPIRATION: 09MAR07. INSPECTED T/R ON NR 2 ENGINE NO DEFECTS FOUND. REMOVED AND REPSDR UIEA200700088Fairing · crackedENGINE NR 2 RT T/REV AFT UPPER BEAVER TAIL FAIRING ASSY INNER SKIN FOUND CRACKED. REPAIRED ACCOMPLISHED AS PER EO NR 4778A094 AND FAA FORM 8110-3.SDR UIEA200700085Access Door · damagedNR 3 ENGINE RT FAN T/REV ACCESS DOOR ASSY SKIN DAMAGED. REPAIRED ACCOMPLISHED AS PER EO NR 4778A095 AND FAA FORM 8110-3.SDR DL764070149B-Nut · looseAPU BLEED UNAVAILABLE AFTER PUSHBACK RTB. FOUND B-NUT ON PNEUMATIC SENSE LINE AT TOP OF APU COMPLETELY BACKED OFF OF THREADS. RETORQUED, MOTORED ENGS 30.1 N2. 40P DURING ROTATION. APU AIR CKS GOOD.SDR UIEA200700078Blowout Door · chafedENGINE NR 1 AND NR 2, RT C-DUCT BLOW OUT DOOR ASSEMBLY HAS MISSING MATERIAL AND CHAFE MARKED. REPAIRED ACCOMPLISHED AS PER EO NR 4778A093 AND FAA FORM 8110-3.SDR 07FDEA00466Unknown · unknownON TAKEOFF ROLL, ECAM MESSAGE ENG NR 2 REV PRESSURIZED APPEARED, STOPPED TAKEOFF AND RETURNED GATE. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A CATEGORY: C EXPIRATION: 23FEB07 "MEL 78-30-01-A: ENGINE (IDENTIFY 1 OR 2) 2 THRUST REVERSER, INOP. THRUST REVSDR 07FDEA00379Unknown · unknownON T/O ROLL ECAM SHOWED NR 2 ENGINE REVERSER PRESSURIZED. CYCLED REVERSER WITH NO HELP. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A CATEGORY: C EXPIRATION: 18FEB07 "MEL 78-30-01-A: ENGINE NR 2 THRUST REVERSER INOP. THRUST REVERSER IS DEACTIVATED ISDR 07FDEA00352Unknown · unknownON PUSHING POWER UP FOR TAKEOFF, AFTER SELECTING TOGA, GOT NR 1 ENGINE REVERSER PRESSURIZED AT 50 KIAS. TAXIED BACK TO RAMP. ACN RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-A CATEGORY: C EXPIRATION: 16FEB07 "MEL 78-30-01-A: ENGINE NR 1 THRUST REVERSER INOP
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