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 IPXA10658763Floor Panel · damagedINSP TYPE:C -MCD POS 11R FLOOR DAMAGE 28.5 INCHES, RT BS LINE 79 INCHES FROM FWD PANEL. FLOOR PANEL FABRICATED IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR DL76G100517Battery Pack · inoperativeEMERGENCY LIGHT ABOVE COCKPIT DOOR INOP. REPLACED BATTERYS. OP CKS GOOD.SDR IPXA10658556Support · crackedINSP TYPE:6C, BULK CARGO LT STA 1417 LBL 14" FLOOR SUPPORT RIVET HOLE FOUND CRACKED. BULK CARGO LT STA 1417 LBL 14" FLOOR SUPPORT REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02, REV 46.SDR IPXA10658559Floorbeam · crackedINSPECTION TYPE:6C, BULK CARGO LT STA 1417 LBL 8" FLOOR SUPPORT RIVET HOLE FOUND CRACK. BULK CARGO LT STA 1417 LBL 8" FLOOR SUPPORT REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02 REV 46.SDR IPXA10658627Stiffener · deformedINSPECTION TYPE:C, BULK CARGO RT STA 1502 BELOW FLOOR RBL 8" STIFFENER FOUND DEFORMED. BULK CARGO RT STA1502 BELOW FLOOR RBL8" STIFFENER REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02, REV 46.SDR IPXA10658628Stiffener · deformedINSPECTION TYPE:C, BULK CARGO LT STA1480 BELOW FLOOR LBL8" STIFFENER FOUND DEFORMED. BULK CARGO LT STA1480 BELOW FLOOR LBL8" STIFFENER REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02 REV 46.SDR IPXA10658629Stiffener · deformedINSPECTION TYPE:C, BULK CARGO RT STA 1502 BELOW FLOOR RBL 14" STIFFENER FOUND DEFORMED. BULK CARGO RT STA1502 BELOW FLOOR RBL14" STIFFENER REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02 REV 46.SDR IPXA10658583Fairing · delaminatedINSPECTION TYPE:C, RT WING OTBD T/E FLAP MID L/E FAIRING DELAMINATED AT OTEF STA210. COMPOSITE HOT BOND REPAIR CARRIED OUT IAW SRM 51-70-05 PAR 5A (1) FIG 5, REV 46.SDR IPXA10658584Fairing · delaminatedINSPECTION TYPE:C, RT WING OTBD T/E FLAP MID L/E FAIRING DELAMINATED AT OTEF STA230.5 COMPOSITE HOT BOND REPAIR CARRIED OUT IAW SRM 51-70-05 PAR 5A (1) FIG 5 REV 46.SDR IPXA10658538Skin · crackedINSPECTION TYPE:6C, LT WING - NR 4 SLAT INBD NOSE SKIN RIVET HOLE FOUND CRACKED. LT WING NR 4 SLAT INBD NOSE SKIN REPAIRED IAW SRM 57-43-01-2R2, FIG 201, REV 46 JUST AT OSS572.5, ORIGINAL MATERIAL IS 7075T6-0063IN, CRACK LENGTH IS 0.07", DAMAGED CUTOUT SIZE ISDR IPXA10658553Stiffener · crackedINSP TYPE:6C, FWD CARGO WING CENTER SECTION FRONT SPAR VERTICAL STIFFENER UPPER AREA FOUND CRACKED JUST AT STA 785.9 LBL 32.94. STIFFENER REPAIRED IAW HX RS. R57-10-36618 REV A & EO NR B767-5710-36713-A. ORIN. MAT'L 1518-749-2024T3511, CRK LENGTH 3.25", CUTOSDR IPXA10658558Floorbeam · crackedINSPECTION TYPE:6C, MEC CABIN FLOOR SUPPORT BEAM STA246 LBL50" AFT CLIP FOUND CRACKED. MEC CABIN FLOOR SUPPORT BEAM STA 246 LBL 50" AFT CLIP REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02 REV.46.SDR IPXA10658616Floorbeam · crackedINSPECTION TYPE:C, MEC CABIN FLOOR SUPPORT BEAM STA246 RBL10" FWD CLIP FOUND CRACKED. MEC CABIN FLOOR SUPPORT BEAM STA246 RBL10" FWD CLIP REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02, REV 46.SDR IPXA10663035Floor Panel · damagedMCD FLOOR PANEL DAMAGED AT POS 2R. FABRICATED NEW PANEL IAW EOB767-5320-9593G.SDR IPXA10663036Floor Panel · damagedMCD FLOOR PANEL DAMAGED AT POS 2L. MFG NEW PANEL IAW EO B767-5320-9693-G AND INSTALLED IAW AMM53-01-01.SDR IPXA10663037Floor Panel · damagedREF D418725 - MCD FLOOR PANEL DAMAGED AT POS 1. MFG NEW PANEL IAW EO B767-5320-9693-G AND INSTALLED IAW AMM 53-01-01.SDR IPXA10663038Floor Panel · damagedMCD FLOOR PANEL DAMAGED AT POS 4R. MFG NEW MCD FLOOR PANEL IAW EO B767-5320-9693-G AND INSTALLED IAW AMM53-01-01.SDR IPXA10663039Floor Panel · damagedMCD FLOOR PANEL DAMAGED AT POS 4L. MFG NEW FLOOR PANEL IAW EO B767-5320-9693-G AND INSTALLED IAW AMM53-01-01.SDR DL76G100148Circuit Card · malfunctionedDIVERT TO LT R DUE TO WRONG MEL APPLIED TO -L ENG ANALOG N2- STATUS MSG IN FRA. REPLACED L ENG N2 SPEED CARD IAW MM TASK 73-21-54-004-001- H00 MCO AND PLACARD REMOVED RAN ENG N2 INDICATION NOW, NORMAL. ETOPS CATEGORY 'B': DIVERSION OR TURNBACK.SDR DL76G092029Wire · brokenRT ENGINE HPSOV EICAS ALERT-RT PACK OFF- RT BLEED OFF. FOUND NR 2 WIRE TERMINAL BROKEN AT HPSOV CAPPED AND SECURED WIRE. FWD TO MCO/PLAC IAW MEL 36-11-02. ETOPS CATEGORY 'B': DIVERSION OR TURNBACK.SDR DL76G092030Blades · bentL ENG BIRDSTRIKE ON APPROACH - DEFLECTED OFF OF RADOME. MX IN PROGRESS- 2 FAN BLADES BENT AND OUT OF LIMITS. REPLACED NR 1 ENG FAN BLADE SET IAW MM ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.SDR DL76G091905Shutoff Valve · malfunctionedDURING INTITIAL T/O ROLL LT ENG BLEED AND MESSAGE ILLUMINATED FWD TO MCO PLACARDED HPSOV IAW MEL 36-11-02. DISP GRANTED. FWD TO MCO PLACARDED HPSOV IAW MEL 36-11-04 AND LT ENGINE THRUST REVERSER DEACTIVATED IAW MEL 36-11-02 DISP DISP GRANTED. ETOPS CATEGORY 'SDR DLM90091915Relay · shortedAFTER BLOCK IN IRS NR 1 BATTERY FAIL LIGHT ILLUMIN W/ ASSOCIATED CAUTION MSG APU DID NOT ST AND BATTERY VOLT READ 10 VOLTS ALSO NOTED ACRID ELECTRICAL ODOR IN COCKPIT AND FIRST CLASS CABIN. REPLACED BATTERY CHARGER BATTERY CHARGER RELAY R2-56 AND 3 SHIPS BATTSDR CA091125001Bearing · failed(CAN) NR 4 MAIN WHEEL INNER BEARING HAD A COMPLETE FAILURE. MAINTENANCE SPOTTED THE MAIN WHEEL SITTING AT AN ODD ANGLE ON THE GATE AND INVESTIGATED. OUTER BEARING AND THE PIECES LEFT FROM THE INNER BEARING HAVE BEEN HANDED OVER TO BOEING FOR FURTHER INVESTISDR DL76G091722Engine · oil consumptionREPLACING NR 1 ENG DUE TO HIGH HOC AND OIL IN RECOUP DUCTS.SDR DL76G091671Controller · malfunctionedDURING TAXI NO RT ENG BLEED AIR AVAILABLE, RTB. PRV CONTROLLER REPLACED BUT FOUND INOP ON FIT. LOAN ITEM OBTAINED FROM LUFTHANSA. FITTED IAW AMM 36-11-19-404-016-001, ENGINE RUN. PERFORMED AND OPS OK. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO SDR CNMA20090016Cover · missingOIL QTY AND PRESSURE LOSS ON RT ENG, NO TEMP OR ENG EXCEEDENCES, NO INFLIGHT SHUTDOWN. OIL PRESSURE DROPPED TO 10 PSI PRIOR TO RT ENG SHUTDOWN. FOUND CRANK PAD COVER NOT INSTALLED. INSTALLED CRANK PAD COVER IAW 72-00-00-982-007-H00. PERFORMED NO OIL PRESSUSDR DL76G091106Fuel Control · malfunctionedLEFT ENGINE WOULD NOT START - NO FUEL FLOW OR IGN - THE ENG VALVE LIGHT ILLUMINATED WITH THE FUEL CONTROL SWITCH IN RUN POSITION. NR 1 ENG HMU CHANGED IAW MM 73-21-14-404-030-H00. ALL INDICATIONS AND OPS NORMAL. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CSDR DL76L091107Vsi · inoperativeF/O VSI INDICATOR INOPERATIVE. R & R F/O VSI INDICATOR PER M/M CHECKS OK. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPSSDR CA090702001Duct · ruptured(CAN) AFTER TAKEOFF, F/A REPORTED EXCESSIVE HEAT IN AFT CABIN THAT COULD NOT BE CONTROLLED. ACFT RETURNED TO DEPARTURE WHERE MX FOUND THAT AFT CARGO HEAT DUCT RUPTURED BETWEEN THE SUPPLY AND THE SHUT-OFF VALVE. DUCT HAD A 4 INCH LONGITUDINAL CRACK. DUCT IS LSDR CA090702002Support Bracket · cracked(CAN) AFTER LANDING, CREW OBSERVED A LARGE SECTION OF INBD NR 1 ENG TRANSLATING SLEEVE MISSING. MX MEASURED DAMAGE AT 65 INCHES BY 13 INCHES. ACFT FERRIED BACK TO DEPARTURE WHERE MX OBSERVED INNER ACOUSTIC LINER SEGMENT AT 12 O`CLOCK POSITION, MISSING. SUPPSDR DL76G090868Mount · damagedDURING IFSD INSP FOUND THE FWD OTBD ENGINE MOUNT DAMAGED. REPLACED ENGINE MOUNT.SDR DL76G090815Wire Harness · damagedL ENG CONTROL EICAS MSG, RTB PERFORMED BITE ON L PIMU FOUND FAULT 155-23 A/B AND 353-14 CH A. SUSPECT HARNESS 012194. REMOVED AND REPLACED W7 HARNESS PER AMM. RAN ENGINE TWICE. MESSAGE DOES NOT COME. CONTACT MCC. NO FURTHER ACTION REQUIRES. A/C OK FOR SESDR DL76G090783Hmu · failedENGINE CONTROL STATUS MSG ON TAXI OUT. HMU CHANGE IN PROGRESS. C/W FIM FOUND J71 PIN 18 TO PIN 37 5.6 MEG WILL REQUIRE HMU. REPLACED HMU PER AMM P/N 442274 MALF-1T0 POS-01 CTL-498241001 SKILL-02.SDR DL76G090781Engine · stalledNR 1 ENG CHANGE FOR STAGGER INSTALLED ESN 706187.SDR DL76G090655Heat Exchanger · damagedDURING TAKEOFF ROLL AT APPROX 40 KTS FELT SHUTTER AND ACFT VEERED TO THE LEFT. THROTTLES PULLED BACK AND TAKEOFF ABORTED. LT ENG LEAKING FUEL FROM COWLING. LT ENG SHUT ITSELF DOWN. MAINTENANCE FOUND FOHE BAD. AFT SECTION OF HEAT EXCH WELD FAILED/5IN DIA DISDR DL76G090356Start Valve · inoperativeL START VALVE LIGHT REMAINS ILLUMINATED, NO AIR DROP NO ROTATION, RETURN TO GATE. START VALVE INOP FWD TO MCO AND PLACARD IAW MEL 80-00-02. REMOVED AND REPLACED LEFT ENG START VALVE PER AMM, OPS CHECK OK.SDR DL76G090323Sensor · contaminatedON CLIMB-OUT FROM JFK PASSING 8000 FT RT ENG STARTED SURGING. STATUS MSG R ENG CONTROL. DECLARED EMERGENCY AND RETURNED TO JFK. ENG WAS NOT S/D. OVERWEIGHT LANDING. R PIMU FAULTS T2.5 SNSR. (CIT) REPLACED SAME. REMOVED AND REPLACED N1 PROBE. BOROSCOPE SDR DL76G090324Sensor · malfunctionedON TAKEOFF RIGHT ENGINE SURGING N1 +/- 10 PERCENT. ALL OTHER ENGINE PARAMETERS ALSO FLUCTUATING. DECLARED AN EMERGENCY AND RETURNED TO JFK. LANDED OVERWEIGHT. MX IN PROGRESS. PIMU FAULT 352-15A/B AND EEC CONTROL MSG. REPLACING CIT SENSOR, N1 PROBE ANDSDR DL76G090202Module · malfunctionedLT REV ISLN VALVE EICAS MSG AT 10 TO 20 KTS DURING T/O MUC FWD LT T/R TO MCO/PLAC PER MEL 78-31-01. M PROCEDURE C/W, T/S PER FIM. NO TROUBLE FND. NO MSGS ON T/R RELAY MODULE. OPERATED T/R SEVERAL TIMES UNDER ENG PWR. OPS CKS NML. MCO/PLACARD REMOVED.SDR DL76G090209Relay · malfunctionedLEFT REVERSER ISOLATION VALVE MESSAGE CAME ON DURING START OF T/O ROLL. FWD LEFT THRUST REVERSER TO MCO AND PLACARD PER MEL 78-31-01 M PROC COMPLIED WITH TROUBLE SHOOTING PER FIM. NO TROUBLE FOUND. NO MESSAGES ON THRUST REVERSER RELAY MODULE. OPERATED THRSDR CA090212001Spar · failedON TAXI OUT, R RUDDER TEST FAILED. RUDDER PEDAL APPEARS TO BIND. UNABLE TO ACHIEVE MORE THAN HALF DEFLECTION. INITIAL INSPECTION FOUND CTR PCA (LT HYD SYS) FULLY RETRACTED IN THE LT RUDDER DEFLECTION POSITION, WITH ONLY LT HYD SYS PRESSURIZED, RUDDER APPROX SDR DL76G090183Pressure Sensor · inoperativeAFTER ENGINE START, LEFT ENGINE BLEED AIR INOP. MAINTENANCE IN WORK AIR SUPPLY BITE FAULTS PRSOV PRESS SENSE. REMOVED AND REPLACED PRSOV PRESS SEN PER M/M 451904 FOUND MUSCLE AIR LINE FITTING LOOSE REATTACH RAN ENG. OPS CKS OK PER M/M MFG 415G265-1.SDR DL76G090184Fuel Filter · unserviceableRIGHT ENGINE FUEL FILTER LIGHT AT 400. STAYED ON FOR 15 MINS IN TERM AND LEVEL OFF. FOUND FUEL FILTER DIRTY. REMOVED AND REPLACED FUEL FILTER IAW MM. OPS CHECK OK. SUMPED RT TANK. NO WATER OR DEBRIS FOUND.SDR DL76G090177Ignition Sys · warning lightRT ENG IGN 1 STATUS MSG. PERFORMED TWO GOOD STARTS NR 2 ENGINE. NO MSGS NOTED.SDR DL757090185Actuator · no testIRR AT FL 350 CABIN ALT WARNING FOLLOWED BY CABIN ALT AUTO 1 INOP. CABIN ALT REACHED APPROX 12.5-13.0. REPLACED NR 1 CABIN PRESS CONTROLLER. REPLACED OUTFLOW VALVE ACTUATOR PER MM OPN CKS GOOD BITE ON AUTO 1 AND AUTO 2 VERIFY NO FAULTS MANUAL, OPS NORMAL.SDR DL76G090091Relay · malfunctionedACFT RETURNED TO GATE, NR 1 ENG NO START AND EICAS MSG NR 1 AND NR 2 IGNITION. REPLACED LT ENG FUEL/IGN CONTROL RELAY K1251 AT P-36 PNL. RAN LT ENG HAD ONE SUCCESSFUL START IGN BOTH. GOT L ENG IGNITOR 2 AND L ENG IGNITOR 1 STATUS MSG 280809. TROUBLESHOT PESDR DL76L081565Connector · looseRTB - ON TAXI OUT RUDDER TRIM INOP. NO MEL RELIEF, MTC RESEATED CONNECTOR ON RUDDER TRIM MODULE SYSTEM. OPS CK OK.SDR DL76G081580Blades · damagedRIGHT ENGINE BIRD INGESTION, ENGINE VIBS, DIVERTED TO DKR 3 FAN BLADES ARE DAMAGED BORO WAS GOOD. REPLACED FANBLADE SETS.SDR DL76G081563Pressure Switch · failedINTERMITTENT RIGHT ENGINE FUEL FILTER LIGHT. REMOVED AND REPLACED RT ENG FILTER PER M/M. INSPECTED NTF REMOVED AND REPLACED FUEL FILTER PRESSURE SW PER M/M RAN ENG MSG DID NOT RETURN.
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