GE CF6-80C2B6F
Service difficulty reports · 1,456
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 = 'CF680C2B6F' 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 = 'CF680C2B6F' 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 UIEA2020092202047Indicator · malfunctionedSTANDBY ENGINE INDICATOR INOP. SYSTEM BITE GOOD, PER AMM 77-41-00. NO OTHER FAULTS, OPS CHECK GOOD.SDR UIEA2020091502003Tube · damagedEICAS MESSAGE RT ENG HPSOV AT 03.57Z AT FL250 N1 106.5 DURING CLIMB OUT. MESSAGE APPEARED AND SELF CORRECTED BEFORE WE RAN QRH. TRANSFER TO DMI NR 134451, IAW MEL 36-11-02-02, CAT C, DUE DATE 25SEP20. PLACARD INSTALLED. ACTIVATED HPSOV, CHECKED FOR LOOSE LSDR UIEA2020091862009Blade · nickedNR 1 ENG HAS FOUR EACH NICKED BLADES WITHIN LIMITS, PER AMM 72-31-02-308-045-H00 FIG 801 NR 5 .93 X.062 NR 16 .062X.062 NR 28 .187X.062 NR 30 .156X.125, IAW AMM 72-31-02-308 FIG 801 NICKS ARE WITHIN LIMITS. TRANSFERRED TO NON MEL MDDR 134433.SDR UIEA2020091542000Indication Sys · malfunctionedRECEIVED NO ENGINE VALVE LIGHT WHEN MOVING THE FUEL CONTROL VALVE TO RUN ON ENGINE START. LIGHT WORK PRIOR TO ENGINE START, AS WELL AS, AFTER. PERFORMED ENGINE FUEL SHUTOFF VALVE ACTUATOR TEST ON LT AND RT ENG, IAW B767 AMM 28-22-11-801. OPS TEST GOOD.SDR UIEA2020091401988Acoustic Panel · damagedAS PER AMM 72-00-00-206-167-H00,TABLE 642, FIGURE 628 CONDITION: DAMAGED ACOUSTICAL PANELS AFT OF THE FAN BLADES, CONTINUE IN-OPERATION LIMIT 10 FLIGHT CYCLES OR 100 FLIGHT HOURS. OPENED NON-MEL 134014. APPLIED RTV SEALANT TO ACOUSTIC PANEL DAMAGE AT 4 O'CLOSDR UIEA2020090801966Warning Message · false activationRIGHT ENGINE FUEL FLOW INDICATOR INOPERABLE, QUANTITY INDICATORS ALL INDICATE NORMALLY. PERFORMED FUEL FLOW TRANSMITTER INSPECTION IAW AMM 73-31-00, NO LEAKS FOUND. TRANSMITTER CONNECTOR PLUG IS RIGHT, NO DEFECTS FOUND. PERFORMED OPERATIONS CHECK IAW AMM 71SDR UIEA2020090801968Engine · stalledDURING CLIMBOUT AT APPROX PASSING 1300 FEET, RIGHT ENGINE COMPRESSOR STALLED SEVERAL TIMES. ENGINE DAMAGE INDICATOR, MAX EGT 995. REMOVED AND REPLACED NR 2 ENGINE, IAW ATLAS WC A-71-999-04-02, OPS CHECKED NORMAL.SDR UIEA2020091081967Indication Sys · intermittentRT ENGINE FUEL FLOW IS INTERMITTENT. TRANSFERRED TO MEL 73-31-01-02, MDDR 133972, CAT C.SDR UIEA2020090101907Intake · corrodedON WALKAROUND FOUND LEFT ENGINE INLET COWL INSIDE AFT 12 O'CLOCK POSITION HAS CORROSION(<P>ACCOMPLISHED PERMANENT HOT BOND COMPOSITE REPAIR ON LEFT ENGINE IAW SRM 51-21-01, 54-12-01-1A-1 AND 54-12-01 REPAIR 6, BY AVENIR FAA CRS #8AVR479B W.O # W14997 FEAM R.O SDR 2LCF2020090100001Warning Message · false activationDURING TAKEOFF, A MOMENTARY MESSAGE WAS PRESENTED ON THE EICAS FOR THE BULK CARGO DOOR. THE CREW RETURNED TO THE POSITION FOR TECHNICAL ASSISTANCE AND MANAGE THE REPORT OF SAID FAILURE. THE TECHNICAL STAFF APPLIED TASK 5-51-14-212-189 TO CONFIRM THAT THERE WSDR UIEA2020082601873Anti-Ice Valve · failedR ENG ANTI-ICE MSG. QRH COMPLETE, MSG REMAINS. REMOVED AND REPLACED RT ENG ANTI-ICE VALVE REF: AMM 30-21-03. OPS CHECK REQUIRED. ENG RUN OPS CHECK NORMAL IAW AMM 30-21-03 AND 71-00-00SDR UIEA2020082481806Valve · malfunctionedLT IDG VALVE STATUS. REMOVED AND REPLACED IDG AIR COOLING VALVE IAW AMM 24-11-07. GROUND RAN #1 ENG IAW AMM 71-00-00. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.SDR UIEA2020081411754Oil System · leakingDURING WALK AROUND FOUND EXCESSIVE OIL LEAK ON RH ENGINE (<P>REF ISSUED WO 19313 FOR NR 2 ENGINE UER. WORK ORDER C/W IAW ASSOCIATED JOB CARDS, NR 2 ENGINE REMOVED AND REPLACED (AMM 71-00-02/401).</P>)SDR P5CA202008120277Igniter · inoperativeRH ENGINE IGNITION 1 INOPERATIVE. EXCEPT ER OPERATIONS. PERFORMED AUDIBLE TEST OF THE RH ENGINE IAW AMM 71-00-00, NR 1 IGNITER INOPERATIVE, NR 2 IGNITER OPERATIONAL IAW AMM LIMITS.SDR UIEA2020081201743Eec · inoperativeLEFT ENGINE EEC C1 INOP (ELECTRONIC ENGINE CONTROL (EEC) SYSTEMS, EEC C1 FAULTS (CF6 FADEC))(<P>DEFERRED TO DMI 132560 IAW MEL 73-21-01-05, CAT "A" DUE 300HRS, NO PROCEDURES REQ'D, PLACARDS APPLIED. MX CTRL EDGAR DISPATCH TS 2018.</P><P>LP 1296659: ACCOMPLISHESDR P5CA2020080760276Igniter · unknownRT ENGINE NR 1 IGNITER INOPERATIVE (IGNITION SYSTEMS, EXCEPT ER OPERATIONS. ACCOMPLISHED NR 2 ENGINE IDLE RUN ON SINGLE IGNITION SYSTEM 1 & 2 IAW AMM 71-00-00, STARTED NORMAL.SDR IPXA2020080128740Indicator · inoperativeDIVERSION - EMERGENCY DECLARED**AFTER LEVELOFF R FUEL GAUGE STARTED TO DECREASE EXCESSIVELY -APPROX 5000 IMBAL- WITH FUEL CONFIG LIGHT - ACCOMPLISHED CHECKLIST AND SHUTDOWN ENGINE.PER FIM 28-41-00-990-854 TELEMETRY SHOWS CROSSFEED VALVES OPEN ENTIRE FLIGHT. NOSDR UIEA2020080401697Blade · nickedDURING WALK AROUND FOUND NICKS ON NR 2 ENG FAN BLADES, 5 BLADES WITH NICKS. PERFORMED FAN ROTOR BLADE INSPECTION IAW AMM 72-31-02. REPAIRED THE ROTOR FAN BLADES IAW AMM 72-31-02.SDR UIEA2020080431669Anti-Ice Valve · unsecureAFTER ENGINE START, RT ENGINE BLEED OFF LIGHT ILLUMINATED. RT ENG BLEED OFF EICAS MESSAGE. ON GVI OF PNEUMATIC VALVES ON RT ENG FOUND ANTI-ICE VALVE TO BE LOOSE. SECURED THE ANTI-ICE VALVE. RAN NR 2 ENG. PERFORMED RT ENG BLEED VALVE OPS CHECK. CHECKED GOOD SDR UIEA2020072201597Fuel Filter · warning messageRIGHT ENGINE FUEL FILTER EICAS MESSAGE DISPLAYED TWICE DURING CLIMB. MESSAGE LASTED A FEW SECONDS THEN BECAME A STATUS MESSAGE. REMOVED AND REPLACED THE RT FUEL FILTER. NO FUEL FILTER STATUS, OPS AND LEAK CHECKED OK IAW AMM 73-11-02.SDR UIEA2020072101592Accelerometer · malfunctionedLEFT ENGINE VIB INDICATION INOPERATIVE. R & R THE NR 1 ENGINE ACCELEROMETER IAW 77-31-02, AND PERFORMED ENGINE RUNS IAW 71-00-00, OPS CHECKED GOOD.SDR UIEA2020072311587Transmitter · failedNR 2 ENGINE, NO FUEL FLOW INDICATION. PERFORMED FIM 73-31 TREE 806 ITEM 44, ACCOMPLISHED. REMOVED AND REPLACED THE FUEL FLOW TRANSMITTER FOR THE RT ENG, OPS CHECKED GOOD, FUEL FLOW TRANSMITTER TESTED GOOD.SDR UIEA2020062981427Anti-Ice Valve · failedLEFT ENG TAI VALVE EICAS MESSAGE. REMOVED AND REPLACED TAI VALVE ON LEFT ENGINE IAW AMM 30-21-03. OPS CHECK NORMAL.SDR UIEA2020100851400Bleed Valve · malfunctionedLEFT ENGINE FOUND FUEL LEAK DRAIN MAST FROM PORT "FUEL DIRECT", 8 DROPS PER MINUTE FOUND IN LIMITS, IAW AMM TASK 71-71-00-796-067-H00 TABLE 601. FUEL DRIP FROM DIRECT FUEL ON DRAIN MUST WITHIN LIMITS, PER AMM 71-71-00 TABLE 601. TRANSFER TO NON-MEL NR 130228SDR UIEA2020060801231Igniter · defectiveRT ENGINE FAILED TO START W/ SINGLE IGNITER. SECOND ATTEMPT IN BOTH SUCCESSFUL. R ENGINE BOTH IGNITER PLUGS IN POOR CONDITION, REPLACED BOTH PLUGS IAW AMM 74-21-02. TESTED SATISFACTORY.SDR UIEA2020060401206Blade · nickedRH ENG BLADE NR 33 SMALL NICK WITHIN LIMITS IAW AMM 72-31-02-2226-012-H00. BLADE BLEND OUT REPAIR ACCOMPLISHED. PERFORMED A FLUORESCENT PENETRANT INSPECTION IAW AMM 70-11-06-232-001-H00. NO DEFECTS NOTED.SDR 2LCF20200603531Pin · out of positionON THE MIA - GUA ROUTE, THE DISPLAY OF THE EADI INDICATION FOR THE FIRST OFFICER OF THE AIRCRAFT WAS LOST. ALTHOUGH THE AIRCRAFT COULD SAFELY CONTINUE THE FLIGHT TO GUA, FOR TECHNICAL CONVENIENCE THE DECISION IS MADE TO RETURN TO THE MIA BASE TO ADMINISTER THSDR FDEA2020060390981Hmu · failedOPEN U DURING CLIMB DEPT KORD APPROX 5000 LOUD BANGING NOISE FOLLOWED BY YAW, A/P ENGAGED, LE N1 30%, FUEL FLOW APPROX. 4000PPH, RT ENG NORMAL, LT ENG BACK TO NORMAL. SECOND OCCURRENCE BANGING LOW N1 & FF ON LT ENG EICAS "L ENG HPSOV" ( SOUNDED LIKE COMPRESSOSDR UIEA2020042700834Filter Element · faultedL. ENG FUEL FILTER ADVISORY AND STATUS MESSAGE DISPLAYED IN FLIGHT. NO ERRATIC ENGINE OPERATION NOTED.(<P>REMOVED AND REPLACED LEFT ENG FUEL FILTER ELEMENT PER AMM 73-11-02. LEAK AND OPS CK PERFORMED PER AMM 71-00-00-712-168-H03. ALL LEAK & OPS CK GOOD.</P>)SDR IPXA2020052765828Engine · smokeINSPECTION TYPE:N/AWHILE STARTING THE LEFT ENGINE, THE MECHANIC CALLED FOR US TO SHUTDOWN THE LEFT ENGINE DUE TO EXCESSIVE FLUID AND SMOKE COMING FROM THE ENGINE. SHORTLY AFTER WE GOT THE L HYD QTY EICAS AND MASTER CAUTION LIGHT. SHUTDOWN LEFT ENGINE AND RANFOSDR UIEA2020041700761Status Message · false activationSTATUS MSG R ENG EEC C1 AFTER ENG START.(<P>COMPLIED WITH R PIMU BITE CK. SYSTEM PASS, OK FOR CONTINUED SERVICE AT THIS TIME, FIM 73-21-885-00, MSG CLEARED.</P>)SDR UIEA2020042000775Eec · failedRH ENG EEC C1 STATUS MESSAGE. REMOVED AND REPLACED THE RT EEC IAW AMM 73-21-15. PERFORMED TEST 12 GROUND TEST EEC IAW AMM 71-00-00. PERFORMED ENGINE RUN IAW AMM 71-00-00. OPS CHECK GOOD.SDR UIEA2020041700758Status Message · false activationR ENG EEC C1 STATUS MESSAGE.(<P>PERFORMED BITE PROCEDURE ON R PIMU IAW AMM/FIM 71-01-FT-810. MSG CLEARED, MCC NOTIFIED.</P>)SDR UIEA2020041400749Filter · faultyR ENG FUEL FILTER EICAS ON INITIAL CLIMBOUT(<P>REMOVED AND REPLACED R ENGINE FUEL FILTER PER AMM 73-11-03. PERFORMED ENGINE LEAK CHECK, FOUND OK.</P>)SDR UIEA2020041400752Fuel Filter · faultyL ENG FUEL FILT EICAS MSG DISPLAY ON AND OFF(<P>REMOVED AND REPLACED L ENG FUEL FILT PER FIM 73-11 FAULT TREE 803 AND AMM 73-11-02/401. OPS AND LEAK CHECK GOOD.</P>)SDR P5CA2020040800140Start Valve · failedLEFT ENG START VALVE FAILED(<P>TRANSFERRED TO MDDR 126765, MEL 80-00-02-01, CAT C, DUE DATE 17APR20.</P><P>LP 1232027 ITEM 2: REMOVED AND REPLACED LEFT ENG START VALVE IAW AMM 80-11-02. OPS CHECK GOOD. THIS CLEARS MDDR 126765. PLACARD REMOVED.</P>)SDR UIEA2020033100573Igniter · defectiveINFO ONLY #2 ENGINE 1ST START ATTEMPT UNSUCCESSFUL, 2ND START ATTEMPT SUCCESSFUL WITH IGNITER IN BOTH THEN BACK TO SINGLE AFTER #2 ENGINE STABILIZED.(<P>TRANSFERRED SINGLE IGNITION SYSTEM #2 ENGINE TO MDDR 126428, EXP 31MAR20, PER MEL 74-00-01A, CAT "A".</P><PSDR P5CA2020031900112Guide Vane · brokenBROKEN - METAL L/E, NO. 1 ENG O.G.V ON 11, 2~5 O'CLOCK.(<P>IAW AMM 72-33-00-308-043 REV. 129 REPAIRED METAL L/E NO. 1 ENG O.G.V ON 11, 2~5 O'CLOCK. CONDITION CHECK NORMAL.</P>)SDR P5CA2020031800103Acoustic Liner · debondedDISBOND - HONEYCOMB, NO. 1 ENG FWD ACOUSTIC LINER ON 6:00.(<P>IAW AMM 72-33-01-004-001 REV. 129 AND AMM 72-33-01-404-011 REV. 129 REPLACED THE NO. 1 ENG FWD ACOUSTICAL LINER WITH SERVICEABLE PARTS. COMPLETED THIS JOB AND CONDITION CHECK NORMAL.</P>)SDR P5CA2020031900102Packing · damagedFOUND #1 ENG A-SUMP OIL LEAK.(<P>IAW AMM 72-31-03-004-001 REV. 129 AND AMM 72-31-02-404-005 REV. 129 REPLACED THE PACKING WITH SERVICEABLE PARTS AT NO. 1 ENG A-SUMP. TRANSFER TO FORM T2031 ITEM #6.</P>)SDR P5CA2020031900098Paint · peelingPEEL OFF - PAINT, NO. 2 ENG FAN ROTOR SPINNER CONE.(<P>CLEAN UP SURFACE AND APPLY THE COATING IAW GE CF6-80C2 ESM 72-21-10 REPAIR 004 AND REPAIR 006, REV. 89. CONDITION CHECK NORMAL.</P>)SDR P5CA2020031700097Paint · peelingPEEL OFF - PAIN, NO. 1 ENG SPINNER CONE PEEL OFF.(<P>CLEAN UP SURFACE AND APPLY THE COATING IAW GE CF6-80C2 ESM 72-21-10 REPAIR 004 AND REPAIR 006 REV. 89. CONDITION CHK NORMAL.</P>)SDR P5CA2020031100079Blade · dentedDURING WALK AROUND FOUND DENT ON LEADING EDGE OF #15 FAN BLADE.(<P>BLENDED AND DAMAGE REMOVED ON FAN BLADE #15 AROUND THE EDGE PER AMM 72-31-02. ON THE LEADING EDGE.</P><P><SPAN>(NOTE: OPENED MDDR 125624 FOR LEFT ENGINE FAN BLADE #15 BLENDED (REPAIR ACCOMPLISHSDR UIEA2020030300358Igniter · defectiveLP 822383-1 - STATUS MSG - LH ENG IGNITER NR 2 - (SEE DISCREPANCY ITEM NR 02) LP 822383-2 - INFO ONLY - LH ENGINE NO LIGHT OFF ON FIRST START ATTEMPT. PLACED ENG START SELECTOR IN BOTH. NORMAL START SECOND ATTEMPT.(SDR UIEA2020022420301Igniter · failedL ENGINE FAILED TO START 1ST ATTEMPT, STATUS MSG L ENG IGNITOR 2 , ENG START BOTH , 2ND ATTEMPT SUCCESSFUL.(<P>TRANSFERRED TO MDDR #124953 I.A.W MEL 74-00-01B CAT C </P><P>LOG PAGE 822355: TROUBLE SHOT IAW FIM 74-00 FAULT TREE 811. FOUND #2 IGNITOR TO BE AT FASDR UIEA2020022100299Eec · malfunctionedLEFT ENGINE CONTROL ON EICAS AND STATUS MESSAGE.(<P>PERFORMED FIM 73-21 FAULT TREE 878 AND 71-01 TASK 936. REMOVED AND REPLACED LEFT ENGINE EEC, TESTED AND FOUND OK AS PER AMM 73-21-15. PERFORMED ENGINE RUN UP AS PER AMM 71-00-00. NO FAULT FOUND AT THIS TIME.<SDR UIEA2020021900275Unknown · unknownDURING LEFT ENGINE START NO EGT RISE, NO FUEL FLOW RISE. FOLLOWED FCOM VOL 1 PROC. (WAIT 30 SECOND, SWITCH ENGINE START TO BOTH. TRY SECOND ATTEMPT) ENGINE START WAS SUCCESSFUL ON SECOND ATTEMPT. IGNITER WAS LEFT ON BOTH FOR REMINDER OF FLIGHT.(<P>PERFORMED LESDR UIEA2020021860257Anti-Ice Valve · malfunctionedRIGHT ENGINE ANTI-ICE VALVE DID NOT CLOSE AFTER IT WAS OPENED.(<P>ACTIVATED VALVE MANUALLY. PERFORMED SYSTEM TEST IAW B767 AMM 30-21-00. SYSTEM TESTS SATISFACTORY AT THIS TIME.<BR /></P>)SDR UIEA2020021900278Warning Light · false activationR ENG ANTI-ICE CAUTION MSG IN FLIGHT.(<P>PERFORMED SYSTEM TEST IAW B767 AMM 30-21-00. OPS CHECK GOOD. NO DEFECTS AT THIS TIME.</P>)SDR UIEA2020021430250Anti-Ice Valve · failedINFLIGHT AFTER TAKEOFF EICAS R ENG ANTI ICE.(<P>C/W FIM 30-21 FAULT TREE 805. FOUND THE R ENG ANTI ICE VALVE TO WORK NORMAL. OPS CHECK GOOD.<BR /></P>)
Back to GE CF6-80C2B6F