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 CA130906003Irs · failed(CAN) ON TAKEOFF WE GOT A CENTER IRS ON DC EICAS MESSAGE, DURING THE CLIMB THE ALIGN ILLUMINATE ON THE CENTER IRS. CONTACTED MOC AND WAS ADVISED TO RETURN TO BS. CTR IRS CHANGED IAW AMM 34-21-01-PB401.SDR UIEA2013080200423Unknown · odorELECTRICAL ODOR IN COCKPIT, CYCLED COCKPIT DOOR MASTER AND ODOR CEASED. VISUAL INSPECTION CARRIED OUT IAW AMM 05-51-56/201, NO EVIDENCE FOUND. FLIGHT COMPARTMENT DOOR INSPECTION CHECK CARRIED OUT IAW AMM 52-51-05/601, OPS CHECKED GOOD. OK FOR SERVICE.SDR CA130805017Gasket · leaking(CAN) DURING THE FLIGHT THE CREW REPORTED AN INCREASING FUEL IMBALANCE IN THE WING TANKS THAT ULTIMATELY REACHED APPROXIMATELY 1900KG. ON ARRIVAL MAINTENANCE FOUND A LEAKING FUEL FEED LINE ON THE RT ENGINE. FOUND FWD GASKET LEAKING ON LINE, PN 9378M19G07 TO HSDR NOCA201308090004Glowstrip · inoperativeTHREE INCH STRIP OF PHOTO ILLUMINESCENT STRIP, JUST FWD OF THE L3 DOOR. REPLACED MISSING PIECE OF PHOTO ILLUMINSCENT STRIP IAW AMM 33-51-00.SDR CA130731002Actuator · failed(CAN) SOON AFTER DEPARTURE, THE ACFT LOST NR 2 PACK. UNABLE TO CONTINUE TO DESTINATION. ACFT LANDED OVERWEIGHT AND EMERGENCY EQUIPMENT WAS CALLED OUT. RT PACK CONTROLLER BITE TEST C/OUT. FOUND FAULTY RT PACK EXHAUST ACTUATOR. RT RAM AIR EXHAUST ACTUATOR RESDR CA131125012Support Fitting · cracked(CAN) RT PYLON FAN COWL BEAM SUPPORT FITTING INBD LUG CRACK FOUND IN RADIUS. R & R RT PYLON SUPPORT FITTING, IAW SRM 51-40-02 AND DWG 311T2110. ACCOMPLISHED GOOD OPS CHECK OF DISTURBED PNEUMATIC DUCTS IN NR 2 PYLON IAW AMM 36-11-00-795-148, STEPS 3.F, 9. NO SDR CA130621002Hose · loose(CAN) FIRE TRUCKS WERE CALLED TO INVESTIGATE FUEL LEAKING FROM ACFT. MAY HAVE BEEN REPORTED AS A FUEL LEAK BY SOMEONE AT THE STATION BUT IT WAS A HYDRAULIC FLUID LEAK FROM THE TAIL OF THE ACFT. MOC SUSPECTS A COLD SOAKED YAW DAMPER ACTUATOR SEAL FAILURE. PUDSDR CA130502006Actuator · failed(CAN) RUDDER TRIM NOT RESPONDING TO INPUTS. NO MOVEMENT ON FLIGHT CONTROL PAGE OR RUDDER TRIM POSITION ON PEDESTAL. RUDDER TRM RESET C/B NO FIX CLEANED RUDDER TRIM SW IAW AMM 27-21-23-102-017: NO FIX FIM 27-21-00-990-806 ACCOMPLIHED UP TO ITEM 54 POWER CHECSDR CA130426002Pca · leaking(CAN) WHILE TAXIING FOR DEPARTURE THE ACFT DEVELOPED A LEAK FROM THE LT HYD SYS AND RETURNED TO THE GATE. CTR, LT HYD SYS, RUDDER PCA REPLACED IAW J/C B767-27-21-02-422-038-8A98. INDEPENDENT CHECK CARRIED OUT.SDR UIEA2013041300200Rod · wornENG 1 COOLING DUCT POSITION ROD ON RT SIDE WORN OUT. R & R POSITION ROD FOR COOLING DUCT ON NR 1 ENG RT SIDE.SDR UIEA2013041300201Bracket · wornHARDWARE HAS WEAR ON ENG NR 1, RT SIDE POSITION BRACKET. R & R HARDWARE.SDR UIEA2013040600174Gasket · tornFUEL LEAK AT NR 1 ENGINE. FOUND FUEL LINE BETWEEN HMU & TRANSMITTER GASKET TORN, R & R GASKET ON HMU TRANSMITTER LINE, LEAK CHECKED GOOD. REF AMM 73-33-00/001.SDR DALA1304221702Engine · failedRT ENGINE FAILED AT FL 360 0, OIL PRESSURE, 0 OIL QTY 18 QTS. ENGINE WIND MILLED 5-8 MINS BEFORW SHUTDOWN. WIND MILL PARAMETERS N1 20-25 PERCENT, N2 0.0 PERCENT. REPLACED ENGINE NR 2.SDR UIEA2013013100042Pressure Switch · malfunctionedSTATUS MESSAGE "NR 1 ANTI-ICE VALVE" DISPLAYED. R & R NR 1 ANTI ICE VALVE SWITCH, IAW AMM 30-21-01, OPS CHECKS GOOD, ENGINE RUN OPS CHECKS GOO, IAW AMM 72-00-00.SDR UIEA2013013000038Indicator · false indicationLEFT ENGINE OIL QTY DROPPED TO 7 AT 4+30 IN FLT, RECOVERED TO 10 OVER NEXT 2 HRS AC BLOCK IN 20 AT FLT TERMINATION. EICAS INDICATION AT BLOCK IN READS 19QTS CAP CHECK OIL INDICATION SHOWS FULL ADDED 1QT, IAW AMM 79-31-00 C/W ENGINE, INSPECTION FOR OIL LEAKAGSDR UIEA2013012800034Blade · nickedFAN BLADE NICKED NR 1 ENGINE. BLENDED AREA WITHIN LIMITS IAW AMM 72-31-02, FLORESCENT PARTICLE INSPECTION WITH NO ITEMS INDICATED.SDR CA130114010Skin · failed(CAN) ON APPROACH, CREW EXPERIENCE A LIGHTNING STRIKE. THE FLIGHT ALSO EXPERIENCED A L/E SLAT ASYMMETRY WHEN LOWERING FLAPS FROM 15 TO 20. MAINTENANCE CONTROL ADVISED LIGHTNING STRIKE CHECK DONE IAW AMM 05-51-19-22-001. NO FINDING THIS FMR IS NOW CONSIDEREDSDR IPXA13676609Skin · damagedRT OTBD ELEVATOR T/E HAS DAMAGE.SDR UIEA2013010200002Shutoff Valve · intermittentLEFT ENGINE HPSOV ILLUMINATED INTERMITTENTLY DURING ALL PHASES OF FLIGHT. R & R LT ENGINE HPSOV IAW AMM 36-11-07, SYS BITE, LEAK CHECKED GOOD.SDR UIEA2012122900569Oil Filter · warning lightSTATUS MESSAGE " RT OIL FILTER" DISPLAYED. R & R RT ENGINE OIL FILTER ELEMENT IAW 79-21-04. PERFORMED ENGINE RUN, NO LEAKS NOTED, MESSAGE CLEARED.SDR CA130114007Hose · failed(CAN) AFTER ENGINE START "LT HYD SYS PRESS" AND "LT HYD QTY" CAUTION ILLUMINATED. HYD PRESSURE AND QTY SHOWED ZERO. LEAK FROM VERTICAL TAIL CONFIRMED VISUALLY BY GROUND CREW. DURING INSPECTION CHECK FOUND HYD LEAK ON RUDDER RATIO CHANGER HOSE. RUDDER RATIOSDR CA130103006Ballast · failed(CAN) BURNING ODOR EMANATING FROM A3 LAVATORY, L2 BAR AREA. GALLEY POWER SHUTDOWN, VIDEO SCREENS POWER SHUTDOWN IAW ADVISE FROM MOC. MAINTENANCE TRAVELING ON THE FLIGHT PERFORMED AN INSPECTION RECOMMENDED SHUTTING DOWN LAVATORY LIGHTING CIRCUIT. FOUND AFT GSDR CA121217006Indicator · failed(CAN) WHILE ENROUTE, APPROXIMATELY 2 HRS AFTER TAKEOFF THE CREW ADVISED THEY HAS LOST THEIR NAVIGATION SYSTEMS. AFTER DISCUSSION WITH MAINTENANCE IT WAS DETERMINED THAT A RE-SET ON THE GROUND WOULD BE REQUIRED. THE FLIGHT DIVERTED AND LANDED. OK FOR SERVICESDR CA121221008Skin · corroded(CAN) CORROSION FOUND ON FUSELAGE SKIN AT THE FORWARD LAVATORY BLOWER VENT OUTLET. EXFOLIATION CORROSION BETWEEN. LT FS SKIN BS 1540-1562, BETWEEN STR 24L-25L WAS TEMPORARY REPAIRED PENDING DTA.SDR UIEA2012121300547Sensor · malfunctionedRT ENGINE EEC C-2, RT PIMU MX MESSAGE DISPLAYED. R & R RT ENGINE T-12 SENSOR, IAW AMM 73-21-06, OPS CHECKED GOOD. GROUND OPS CHECKED GOOD.SDR CA121119007Track · fractured(CAN) THIS MORNING A FRACTURED OTBD DEFLECTION CONTROL TRACK WAS FOUND ON THE ACFT LT OTBD FLAP. A PRELIMINARY ENGINEERING INSPECTION FOUND DAMAGE TO THE WING T/E UPPER PANEL, PN 113T1346-113, FLAP L/E ACCESS PANEL AND AILERON CLOSURE CAP. NOTE: THIS IS A KNSDR IPXA2676105Alternator · inoperativeON TAKE OFF, LEFT ENGINE STARTED SURGING. NO EICAS INDICATIONS. STATUS MESSAGE LT ENGINE ANALOG N2 EICAS DISAGREE, LT ENGINE CONTROL HIGH OIL TEMP INDICATIONS AND LOW OIL PRESSURE. INFLIGHT SHUTDOWN OF ENGINE. FOUND BOTH A AND B CHANNEL DATA BUSS INOPERASDR UIEA2012102100488Filter Element · failedRT ENGINE FUEL FILTER MESSAGE, REPLACED RT ENGINE FUEL FILTER ELEMENT IAW AMM 73-11-02/401. DRY MOTORED AND WET MOTORED IAW AMM 71-00-00, OPS CHECKED GOOD.SDR CA121017002Stick Shaker · malfunctioned(CAN) ON DEPARTURE THE CREW EXPERIENCED A FALSE STICK SHAKER IN CLIMB. T/O SPEED AND ATTITUDE WAS NORMAL. MOC ADVISED. ASR TO FOLLOW. FIM 27-32-00-815-802 STALL WARNING MODULE, SWM, BITE PROCEDURE CARRIED OUT AND ALL TEST PASSED. SYSTEM OK AND SERVICEABLESDR CA121001001Filter · contaminated(CAN) APPROXIMATELY 1 HR AFTER DEPARTURE, IN CRUISE THE CREW ADVISED THERE WAS AN UNUSUAL ODOR IN THE CABIN. AFTER DISCUSSION WITH MAINTENANCE, THE CREW ADVISED THE ODOR WAS GROWING AND THE CREW ELECTED TO RETURN. THE FLIGHT WAS NOT EXPECTED TO BE OVERWEIGHTSDR UIEA2012092300441Warning Message · false activationRIGHT BLEED DUCT LEAK EICAS MESSAGE, QRH COMPLETED AFTER 20 MIN MESSAGE OUT, PERFORMED FIM PROCEDURE 26-18 FAULT TREE 804. THE SYS IS OK. NO FURTHER MAINT IS REQUIRED AT THIS TIME.SDR UIEA2012092200438Bleed Valve · failedDURING ENGINE START APU DIED TWICE, AFTER GOING TO BLEED OFF, KEPT BLEED ON ON APU TO START ENGINES. R & R SURGE BLEED VALVE, OPS AND LEAK CHECKS SATISFACTORY, OK FOR RETURN TO SERVICE, REF AMM 49-53-01.SDR UIEA2012092200440Warning Light · false activationDURING CRUISE FLIGHT, LEFT FORWARD FUEL BOOST PUMP LIGHT ILLUMINATED. TURNED PUMP OFF IAW QRH. OPS CHECK OF LT FORWARD BOOST PUMP SATISFACTORY. OK FOR SERVICE, REF AMM 28-22-00.SDR UIEA2012091700422Duct · damagedRT ACFT PACK HAS A DUCT LEAK. FOUND DUCT SEAL AT SLIP COUPLING BAD, DUCT DAMAGED, INSTALLED SERVICABLE LOANER DUCT. OPS & LEAK CHECK GOOD, IAW AMM 21-51-03; 21-51-00.SDR UIEA2012091700423Strut · leakingRIGHT GEAR STRUT LEAKING.SDR IPXA12675330Floor Panel · gougedMAIN CARGO DECK FLOOR PANEL 14L, SECOND PANEL FROM OTBD SIDE HAS A GOUGE. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693-H AND DWG 146T5869.SDR UIEA2012091200417Circuit Card · failedDURING CLIMBOUT EICAS MESSAGE FWD EQUIPMENT OVERHEAT DISPLAYED ALONG WITH OVERHEAT LIGHT ON OVERHEAD. FOLLOWED QRH PROCEDURE. LIGHTS REMAINED EXTINGUISHED. REPLACED M990 ECS FAN CONTROL CARD IAW AMM 21-26-05. OPS CHECKS GOOD.SDR UIEA2012091300419Skin · delaminatedRT REAR NOSE DOOR SHOWS SIGNS OF DELAMINATION. REPAIRED IAW EO 6752A007 PART 1.SDR UIEA2012091300420Pump · leakingRT ENGINE EDP IS LEAKING. R & R RT ENGINE DRIVEN PUMP IAW AMM 29-11-05. OPS & LEAK CHECKED OK.SDR UIEA2012091100412Indicator · inoperativeRT WING FUEL QUANITY INDICATOR INOPERATIVE.SDR UIEA2012091000393Fuel Filter · leakingSTATUS MESSAGE FOR LT ENG FUEL FILTER. R & R LT ENG FUEL FILTER ELEMENT WITH NEW UNIT IAW AMM 73-11-02. LEAK, OPS AND GROUND CHECKED GOOD.SDR UIEA2012091000394Warning Message · illuminatedSTATUS MESSAGE FOR LT ENGINE FIRE LP1.SDR IPXA2675215Skin · dentedRT OTBD T/E FLAP HAS DENT 1.5 X 4.2 CUTOUT. REPAIRED IAW EO B767-5750-48487-A.SDR IPXA2675216Floor Panel · dentedFLOOR PANEL AT POS 6R FWD HAS DENT WITH CRUSHED CORE. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693H.SDR IPXA2675217Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL AT POS 7R FWD HAS HOLE IN OTBD PANEL. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693H.SDR IPXA2675218Floor Panel · damagedMAIN CARGO DECK, FLOOR PANEL AT POS 8R AFT HAS HOLE IN OTBD PANEL. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693H.SDR IPXA2675219Floor Panel · dentedMAIN CARGO DECK FLOOR PANEL, POS 7R MID HAS A HOLE. FABRICATE NEW FLOOR PANEL IAW EO B767-5320-9693-H.SDR IPXA2675224Floor Panel · damagedMAIN CARGO DECK POS 7L FWD FLOOR PANEL HAS A HOLE, THIRD PANEL FROM OTBD. FABRICATED NEW FLOOR PANEL IAW EO B767-5320-9693H.SDR IPXA2675232Flap System · malfunctionedON APPROACH, T/E FLAP DISAGREE MESSAGE. RAN CHECKLIST. LANDED WITH FLAPS 27. EMERGENCY DECLARED, LANDED WITHOUT INCIDENT. T/E FLAP DISAGREE MESSAGE NO LONGER DISPLAYED. AFTER FIM TASK 27-51-00 FIG 114B C/O. FLAP FUNCTION CHECK C/O SATISFACTORY IAW AMM 27-51SDR UIEA2012090700379Cover · missingEXIT SIGN COVER MISSING AT FWD OVER WING ESCAPE DOOR RT SIDE. INSTALLED INDICATOR LIGHT IAW AMM 33-57-01. OPS CHECKED GOOD.
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