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 IPXA2016040101497Eec · inoperativeEGT INDICATES BLANK OR ABNORMAL OTHER ENGINE INDICATIONS NORMAL. R & R NR 2 ELECTRONIC ENGINE CONTROL IAW AMM 73-21-15-401. OPS CHECKS GOOD IAW AMM 71-00-00-725-268-H03.SDR UIEA2016031000147Compressor Blade · deformedENGINE 2 FAN BLADE LE HAS BETWEEN 3" - 4" DEFORMATION BELOW MID SPAN SHROUD. R & R ENG 2 FAN BLADE, NR 16 OLD MOMENT, .174 NEW MOMENT, .174 IAW 72-31-02-804-076-1400. VIBRATION SURVEY TUBE DONE ON TASK CARD A72-999-01-02.SDR UIEA2016031000152Compressor Blade · out of limitsNUMBER 2 ENG FAN BLADE NR 17 REQUIRES REPLACEMENT FOR BEING OUT OF LIMITS. REF NR00246, PAO NRI 3238. R & R ENG 2 FAN BLADE 17 OLD MOMENT, 155, NEW MOMENT .155 IAW AMM 72-31-02-404-076-H00. VIBRATION SURVEY TO BE DONE ON TASK A-72-999-01-02.SDR P5CA2016022900053Transmitter · no testENGINE NR 2 FUEL TRANSMITTER FAILED IN TEST. REPLACED FUEL TRANSMITTER IAW AMM 73-31-01, REV 116.SDR CA160223005Fan · malfunctioned(CAN) IN PREPARATION FOR DEPARTURE IT WAS REPORTED BY GROOMERS THERE WAS A BURNING ODOR IN THE CABIN OF THE ACFT. MAINTENANCE WAS ADVISED AND INVESTIGATION RESULTED IN THE AFT GALLEY EQUIPMENT FAN MALFUNCTIONING AND AN MEL WAS APPLIED. FLIGHT WAS DELAYED APPRSDR IPXA2016021699491Pawl · brokenCREW ENTRY DOOR HANDLE DIFFICULT TO MOVE, OPEN AND CLOSE, DOOR CLOSED IMPROPERLY, OUT OF SEQUENCE.REPOSITIONED UPPER PAWL AND UPPER CEILING PANEL. OPERATIONALLY CHECKED DOOR INSIDE AND OUT IAW AMM 52-12-00-201. OK FOR SERVICE.SDR CNMA201601150002Fuel Filter · cloggedDURING FLIGHT, STATUS MESSAGE, RT ENGINE FUEL FILTER. DURING POWER REDUCTION AT TOP OF DECENT, EICAS MESSAGE WENT AWAY. R & R RT ENGINE FUEL FILTER LEAK AND OPS CK IAW AMM 73-11. OPS CK GOOD. PREFORMED ENGINE RUN IAW AMM 71-00. OPS CK GOOD. MSG'S CLEAREDSDR UIEA2016011400017Shutoff Valve · failedSTATUS MSG, LT IDG VALVE. VALVE LOCKED OPEN IAW AMM 75-00-00-901. REPLACED LT IDG AIR & OIL HEAT EXCHANGER AIR SOV IAW AMM 24-11-07. TESTED IDG SYS OK, IAW AMM 24-11-00 501. ACFT RESTORED TO NORMAL CONFIG IAW 75-00-00 905.SDR CA151229011Filter · contaminated(CAN) DUE TO A MAINTENANCE ISSUE WITH A FUEL FILTER, THE ACFT WAS BROUGHT BACK TO AIRPORT. NO FUEL DUMP WAS CARRIED OUT. THE FLIGHT LANDED OVERWEIGHT AND THE CAPTAIN DECLARED A PAN PAN TO HAVE THE EMERGENCY VEHICLES STANDING BY IN CASE OF HOT BRAKES. RESOLUTSDR UIEA2015122200789Module · failedRIGHT FUEL CONTROL ENG VALVE LIGHT IS INOPERATIVE. R & R FUSE DIODE MODULE ASSEMBLY IAW SWPM 20-84-10. OPS CHECKED GOOD AT THIS TIME.SDR UIEA2015122100788Anti-Ice Valve · malfunctionedRIGHT ENG ANTI-ICE EICAS MESSAGE WITH ENGINE AT LOW POWER SETTINGS. REPLACED & OPERATIONS CHECKED RT NAC TAI VALVE IAW AMM 30-21-03 401.SDR CA151202007Module · leaking(CAN) ON APPROACH FLIGHT, EXPERIENCED A L/E SLAT ASYMMETRY. A MISSED APPROACH WAS CONDUCTED AND THE QRH WAS CARRIED OUT BEFORE RETURNING FOR LANDING. AN EMERGENCY WAS NOT DECLARED. REPLACED FLAP/SLAT SHUTOFF VALVE MODULE IAW AMM 27-51-48-022-001.SDR CA151109006Fan · failed(CAN) FLIGHT CREW ADVISED AFTER ARRIVAL THEY HAD SMOKE IN THE CABIN EN-ROUTE. RESOLUTION L RECIRCULATION FUN REPLACED IAW AMM TASK 21-25-01 PLUS FAN INSTALLATION TEST C/O IAW TASK 25-21-01-864-022, NO FAULT FOUND MEL CLEARED.SDR CA151109008Priority Valve · failed(CAN) FLIGHT DIVERTED BACK TO AIRPORT DUE GEAR PROBLEMS. NLG RETRACT ACTR REPALCED IAW AMM 32-34-01-PB401 NLG PRIORITY VALVE CHANGED IAW AMM 32-34-07-404-009. LEAK CHECK OPEN TESTED NLG IAW AMM 32-34-00-715-001. EXT/RETRACTION NIL FAULTS.SDR CA151105006Proximity Sensor · out of adjust(CAN) SECOND DEPARTURE ATTEMPT, ACFT RETURNED TO AIRPORT. ACCOUNT SAME EICAS MESSAGE LANDING GEAR MONITOR. RESOLUTION FOUND SENSOR 235 OUT OF LIMIT INTERMITTENTLY. SENSOR 235 RT NLG ADJUSTED IAW AMM 32-61-03-822-022 TEST OK ON PROXIMITY BOX.SDR CA151106003Computer · failed(CAN) FLIGHT CREW REPORTING ACFT OSCILLATING PITCH UP TO 200 FT. RESOLUTION ALL 3 FCC`S REPLACED IAW AMM TASK 22-11-01, PB 401. CHECK SERVICEABLE.SDR CA151103001Probe · failed(CAN) DUAL AUTO PILOT FAILURE SHORTLY AFTER DEPARTING. CAPTAIN PHONE PATCHED WITH MOC. UNABLE TO RESOLVE THE AUTO PILOT FAILURE. RETURNED TO DEPARTURE AIRPORT AND OVERWEIGHT LANDING CARRIED OUT. RESOLUTION REPLACED TAT PROBE REF AMM 34-12-02. CHECKS SERVICEASDR UIEA2015110100599Transmitter · brokenRIGHT ENG OIL TEMP BLANKED OUT IN FLIGHT. TROUBLE SHOT IAW FIM 79-34TR807. FOUND RT ENG TEMP TX BROKEN OFF, R & R. PERFORMED LEAK CHECK & OPERATIONS CHECK TEST 3 IAW AMM 79-34-001 & 71-00-00. OK FOR SERVICE.SDR CA151026003Windshield · cracked(CAN) APPROX 1 HR FROM TLV, THE FIRST OFFICERS OUTER WINDSCREEN CRACKED. ACFT DECLARED A PAN PAN WITH ATC. RESOLUTION REPLACED WINDOW ASSY RT.SDR IPXA2015100694467Anti-Ice Valve · malfunctionedEICAS MESSAGE, RT ENGINE ANTI-ICE DISPLAYED AND ENGINE ANTI-ICE VALVE LIGHT REMAINED ILLUMINATED WITH SWITCH ON. R & R RT ENG ANTI-ICE VALVE IAW MM 30-21-03-401. OPS TEST SATISFACTORY.SDR CA150929003Cover · damaged(CAN) ON DESCENT I/C REPORTED AN ELECTRICAL BURNING ODOR IN BACK GALLEY, THAT THAT DISSIPATED AFTER 15 MINUTES AND THEN RETURNED AFTER LANDING AND MOC ADVISED. AFT LAV DOME LIGHT FOUND LOOSE TERMINAL TOUCHING PLASTIC ISOLATION COVER MELTED PLASTIC CAUSING ELESDR IPXA2015092393866Blades · damagedINSPECTION TYPE:ETOP, ON T/O, APPROXIMATELY 400 FT AGL WE FLEW INTO SEVERAL BIRDS ON RT SIDE OF ACFT AND RT ENG VIBRATION WAS 5.0 ON INSTRUMENT AND NOTICEABLE IN THE COCKPIT. RT ENGINE FAN BLADE SET REPLACED IAW AMM 72-31-02-404-084-H00, REV AUG 15. FAN ROTSDR IPXA2015091893676Frame · crackedINSPECTION TYPE:C, DURING MAJOR MAINTENANCE VISIT NR 6779, FOUND CRACK POS 1 ENGINE LT T/R INNER FAN AIR DUCT SUPPORT FRAME CRACK TRANSFERRED TO EGAT NRC DCU05021 AND REPLACED DAMAGED PARTS WITH NEW PARTS IAW EO B767-7830-14712-N AND B767-7830-52256-B.SDR IPXA2015091893677Ring · chafedINSPECTION TYPE:C, DURING MAJOR MAINTENANCE VISIT 6779 FOUND CHAFING - POS 1 ENGINE RT T/R CASCADE AFT SUPPORT RING UPPER, NEAR AGB ACTUATOR CHAFING MARK TRANSFERRED TO EGAT NRC DCU05038 AND ACCOMPLISHED EO B767-7830-14712-N AND B767-7830-52256-B. REPLACED DASDR CA150908002Sensor · contaminated(CAN) EMERGENCY DECLARED WITH ATC DUE TO FLIGHT CONTROL PROBLEMS. FLIGHT LANDED. IN FLT: L/E SLAT ASSYM EICAS MESSAGE. QRH CHECKLIST COMPLETED. OPERATED SLATS/FLAPS FULL CYCLE NUMEROUS TIMES. NO SLAT ASSYMETRY, NO MSGS, NORM OPS. PSEU BITE SHOWED "294". PSSDR UIEA2015081900436Liner · missingLEFT ENG OTBD THRUST REVERSER, INTERIOR LINER MISSING AT 10 O CLOCK POSITION. IAW EO 6778A019 COMPLIED WITH PART 1 INTERIM REPAIR. PART 2 DVI REQUIRED EVERY 5 FC. PART 3 PERMANENT REPAIR DUE AT NEXT A CHECK. PLACED ON NON-MEL 59424.SDR CA150923011Transcowl · out of position(CAN) LT INBD T/R NR 1 ENGINE, TRANSLATING COWL FOUND ASKEW ON WALKAROUND AND DIFFICULTY CLOSING THRUST REVERSER. THE UPPER ACTUATOR ROD END WAS FOUND DISLOGED FROM THE CLEVIS FITTING. LT ENGINE R/N POSITION T/R REPLACED IAW AMM 78-31-04, P 401.SDR CA150730010Flap System · malfunctioned(CAN) FLIGHT EXPERIENCED LEADING FLAP ASYMMETRY ON FINAL APPROACH. NORMAL LANDING WAS CARRIED OUT. MAINTENANCE CONTROL ADVISED. RESOLUTION FAULTS CLEARED. NO HISTORY. FIM TASK 27-81-00-815-809 CARRIED OUT UNABLE TO FAULT. SYS CONSIDERED SERVICEABLE.SDR CA150729003Anti-Ice Valve · failed(CAN) AIR RETURN DUE TO BLEED OVER HEAT, SUBSEQUENT OVER WEIGHT LANDING BY 15.0. PAN PAN DECLARED. NEW TAI VALVE ASSY INSTALLED IAW AMM 30-21-03-401. OPS CHECK AND LEAK CHECK C/OUT ON GND RUN, SERVICEABLE.SDR CA150714005Converter · failed(CAN) CREW REPORTED A DIRTY SOCK ODOR ON BOARD THE ACFT. RESOLUTION LT OZONE CONVERTER REPLACED IAW AMM 21-51-22-004-001. COCKPIT TRIM AIR VLV INSPECTION, NO FAULTS. HT EX LT INSPECTED WITH NO FAULTS.SDR CA150714004Wire · broken(CAN) RETURN DUE AILERON LOCKOUT FAULT & CTR AUTOPILOT. CTR AUTOPILOT ENGAGEMENT SWITCH IS CAUSING FLIGHT CONTROL COMPUTER TO FAIL. AILERON LOCKOUT WORKS & ONLY AN INDICATION FAULT. MEL APPLIED. RESOLUTION FOUND WIRE AT PIN 30 OF CONNECTOR D479 BROKEN. RESDR UIEA2015070400326Hmu · failedON FINAL APPROACH, NOTICED LT ENGINE APPROXIMATELY 21% N1, 52% N2. THROTTLE ADVANCE DID NOT INCREASE POWER, AUTO THROTTLE DISCONNECTED. MANUAL LANDING MADE WITH NO FURTHER ISSUES. LT ENGINE EGT INCREASED TO APPROXIMATELY 750 DEGREES, ENGINE SHUTDOWN, NO FSDR UIEA2015070700328Unknown · malfunctionedMAX THRUST AT TAKEOFF N1 109.1, LT ENG WOULD ONLY GENERATE 106.6 N1 WITH THROTTLE TO STOP. ASSUMED TEMP REQUIREMENT 106.1, TROUBLESHOOTING ENGINE. R & R NR 1 ENG FUEL PUMP, R & R NR 1 ENG HMU, R & R NR 1 ENGINE EEC, R & R NR 1 ENGINE N1 SPEED SENSOR, R &SDR IPXA2015061290089Sleeve · dentedINSPECTION TYPE: C, DURING MAJOR MAINTENANCE VISIT ,FOUND A DENT ON NR 2 ENG EXHAUST SLEEVE AT NAC STA 336.6, MID 9 O'CLOCK AREA REF EGAT NRC CQU05082 EVALUATED DAMAGE IAW SRM 54-42-30-1A-1, REV 62.00 INFORMATION SUBMITTED FOR ADM DENT WITHIN ALLOWABLE DAMAGE.SDR CA150609002Actuator · failed(CAN) FLIGHT DEPARTED AND SOON AFTER TAKEOFF HAD AN AILERON LOCKOUT MESSAGE, IT WAS DECIDED TO RETURN AND HAVE MAINTENANCE THERE LOOKED INTO FAULT, NO OVERWEIGHT LANDING. RESOLUTION CARRIED OUT TROUBLESHOOTING IAW FIM 27-11-00-815-804 FOUND SYSTEM OK. MOC RSDR CA150610002Schrader Valve · leaking(CAN) APPROXIMATELY 2HRS INTO FLIGHT CREW CONTACTED MOC THROUGH DISPATCH TO DISCUSS MIGRATION OF HYD FLUID FROM RT SIDE TO CENTER. AFTER DISCUSSION IT WAS DECIDED NOT TO CROSS THE OCEAN & DIVERT BACK FOR MX TO INVESTIGATE FURTHER. RESOLUTION FOUND SCHRADER VSDR UIEA2015060600296Eec · malfunctionedLEFT ENG EEC C1 STATUS MSG. REPLACED LT ENG EEC.SDR UIEA2015051100269Packing · damagedNUMBER 1 ENG, NR 1 BEARING MANIFOLD LEAKING OIL. R & R 1 BEARING MANIFOLD PACKING SEAL IAW AMM 72-31-00. NO LEAKS NOTED.SDR CA151002009Cover · cracked(CAN) FOLLOWING INSPECTION AS REQUIRED BY AD 2014-22-09 AND SB 767-27A0229, OUT OF 4 ACFT INSPECTED, 1 AIRCRAFT WAS FOUND WITH A CRACKED COVER ASSY ON THE ACTUATOR FOUND IN POSITION NR 3. THE CONDITION IS NOT SOMETHING THAT THE SB IS LOOKING FOR AS THE SB IS SDR UIEA2015041600234Status Message · false activationSTATUS MSG, L ENG EEC C1. ACCOMPLISHED PIMU BITE PROCEDURES IAW FIM 71-01-00 101, MSG ERASED. OK FOR SERVICE.SDR CA150327004Ballast · burned(CAN) AFTER ARRIVAL OF THE ACFT AT THE GATE, A HAZE AND ELECTRICAL SMOKE WAS OBSERVED BY THE CREW AND PASSENGERS AHEAD OF THE MID GALLEY. MAINTENANCE HAD MET THE FLIGHT AND WERE ABLE TO ISOLATE THE CAUSE TO AN ELECTRICAL BALLAST LOCATED ABOVE SEAT 5A. THE BASDR UIEA2015032500190Start Valve · slowLEFT START VLV SLOW TO OPEN. R & R STARTER & START VLV.SDR CA150324002Flap System · failed(CAN) THE ACFT ENCOUNTERED A FLAP DISAGREE ON FINAL APPROACH. THE FLIGHT CREW COMMENCED A MISSED APPROACH. THE SECOND APPROACH WAS OTHERWISE ROUTINE. NO ADVERSE PASSENGER REACTION WAS REPORTED. RESOLUTION NO MSG FOUND AND FLAP/SLAT OPERATIONAL TEST CARRIEDSDR CA150319004Elevator System · abnormal(CAN) CREW REPORTED THE FOLLOWING PERFORMANCE ASPECTS REGARDING THE FLIGHT: -40LBS BACK PRESSURE NEEDED TO ROTATE-ON APPROACH, 13.5 UNITS OF AFT STABILIZER TRIM WAS REQUIRED. ACFT WAS SERVICEABLE. OPS WAS VERIFYING WEIGHTS AND LOCATION OF CARGO, SO FAR ALL WSDR CA150318012Ballast · burned(CAN) AS REPORTED BY CABIN CREW, ODOR OF BURNING WIRES VERY STRONG AROUND ROW 20 AND 21. FOUND BALLAST AT 21AC WITH BLOWN FUSE AND BURNED ELECTRICAL ODOR. REPLACED BALLAST AND CHECKED SERVICE.SDR UIEA2015031100177Valve · faultyLEFT ENG LOW PRESS TURBINE CASE COOLING VLV INOPERATIVE. R&R LT ENGINE LPTCCV IAW AMM 75-24-01, ALSO REPLACED LT EEC HARNESS DUE TO DAMAGE FOUND AT P115 CONNECTOR OF P11 HARNESS(YELLOW), PERFORMED TASK AMM 71-00-00 CONF 3 TEST 12 EEC ACTUATORS TEST. FOUND EESDR UIEA2015021400118Starter · inoperativeNUMBER 2 STARTER INOPERATIVE ON DEPARTURE START-UP. R & R IAW AMM 80-11-01. OPERATIONS CHECKED SATISFACTORY.SDR UIEA2015021300116Liner · delaminatedNR 2 ENGINE LINER SEGMENTS BETWEEN THE FAN & INLET GUIDE VANES HAVE MINOR DELAMINATION AT 02:00, 03:00 & 06:30 POSITIONS, WITHIN LIMITS IAW AMM 72-00-00-206-167. ALL LOOSE MATERIAL REMOVED. R & R THE ACOUSTIC LINER IAW 72-33-01.SDR UIEA2015021300117Liner · delaminatedNR 1 ENGINE LINER SEGMENTS BETWEEN THE FAN & INLET GUIDE VANE HAVE MINOR DELAMINATION AT 01:00 & 03:00 POSITION, WITHIN LIMITS IAW AMM 72-00-00-206-167. ALL LOOSE MATERIAL REMOVED. R & R LINERS.SDR UIEA2015020200062Acoustic Panel · damagedDURING WALK AROUND INSPECTION FOUND LT ENG FAN MID OUTER LINER ACOUSTIC PANEL PEELING & MISSING EXPOSING HONEYCOMB. DIMENSION 31 INCHES LONG X 1.2 INCHES WIDE, FOUND WITHIN LIMITS FOR CONTINUING SERVICE IAW AMM 72-00-00-206-167-H00 TABLE 640 & 642. LIMIT 10
Back to GE CF6-80C2B6F