GE CF6-80C2D1F
Service difficulty reports · 536
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 = 'CF680C2D1F' 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 = 'CF680C2D1F' 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 FDEA201105191883Engine · malfunctionedTAKING OFF ON 30R AT APPROXIMATELY 1000FT EXPERIENCED A NR 2 ENGINE EGT OVERHEAT 966 DEGREES AND LARGE BANGING SOUND (COMPRESSOR STALL). PULLED NR 2 THROTTLE TO IDLE IMMEDIATELY. EGT CAMEBACK TO NORMAL (740-760 ) AND COMPRESSOR STALL STOPPED. AFTER THROSDR FDEA201102020453Anti-Ice System · malfunctionedLEFT WINDSHIELD HEAT FAILED IN ICING CONDITION, ASSOCIATED WITH SPARKS IN CAPTAIN'S FLOOR PAN. PERFORMED OPS CHECK OF LT WINDSHIELD ANTI-ICE IAW MM 30-41-01-4. OPS CHECKED GOOD.SDR FDEA201101060019Shoulder Belt · malfunctionedCAPTAINS SHOULDER HARNESS VERY DIFFICULT TO UNLOCK. OPS CHECKED THE CAPTAINS SHOULDER HARNESS WITH CAPTAIN WATCHING AND SHOULDER HARNESS, OPS CHECKED NORMAL. ACFT OK TO CONTINUE.SDR FDEA201101060047Engine · failedREJECTED TAKEOFF AT APPROX 120-130 KTS DUE TO COMPRESSOR STALL/ LOUD BANG. ENG 3 EXCEEDANCE REPORT, SHOWED PS3 OVER LIMIT. ALL OTHER PARAMETERS NORMAL, EGT NORMAL. STILL IN WORK. IAW AMM 72-00-05-6 FOR ENG NR 3 STALL INSP, FAN BLADE SHINGLING INSP CHECKED NSDR FDEA201101060020Vane · delaminatedRT WING INBD T/E FLAP VANE LOWER SURFACE DELAMINATED BETWEEN VANE CTR AND OTBD TRACK. VANE REMOVED AND REPLACED AS PER AMM 27-50-22-4 REVISION 69.0. FLAP VANE ADJUSTMENT AND TEST CARRIED OUT AS PER AMM 27-50-22-5 REVISION 69.0 FOUND SATISFACTORY.SDR FDEA201012244746Wire · burnedRT SIDE TURN OFF LIGHT INOP - SCAN LIGHT SEEMS OK. RELEASED FOR SERVICE IAW MEL: 33-43-01 CATEGORY: C EXPIRATION: 31DEC10 "MEL 33-43-01: RT RUNWAY TURNOFF LIGHT - INOP." C/B CHECKS NORMAL , QUICK TURN NO TIME TO WORK THIS TURN. FOUND BOTH ELEC WIRES BURSDR IPXA10M63885Bottle · low pressureL1 DOOR SLIDE BOTTLE PRESS LOW. SERVICED BOTTLE IAW MM 12 25 04.SDR FDEA201012204729Cargo Track · corrodedMAIN DECK CARGO TRACK AT STATION 1665, 'X' = -27.5 FOUND CORRODED. REPAIRED BY SECTIONAL CARGO TRACK REPLACEMENT FROM STA 1631 TO STA 1671, 'X' = -27.5 IAW SRM 53-00-52, FIG 201 REPAIR 1, REV 45. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 111.SDR FDEA201012144671Wire Harness · chafedNR 1 ENGINE GENERATOR LEADS T2 AND GRD CHAFED AND ARCHED TO COOLING AIRDUCT BRACKET NEAR FWD ENGINE MOUNT. NO RESTRICTION NR1 ENGINE GENERATOR FEEDER CABLE IS DAMAGE DUE TO CHAFE CONDITIONS. INSTRUCTIONS TO MX FOR WRAPPING DAMAGE FEEDER CABLE IAW EA1-2420-SDR FDEA201012104629Fire Detector · malfunctionedFIRE DET 2 FAULT CYCLES ON/OFF ENROUTE ON STATUS PAGE. RECEIVED ALSO FIRE DET 2, FAIL ENROUTE NUMEROUS TIMES ON STATUS PAGE FOLLOWED BY FIRE WARNINGS FOR NR 2 ENGINE WHICH LASTED A FEW SECONDS ONLY. NO OTHER WARNINGS OCCURED BUT THE FIRE DET 2 FAULT REMAINSSDR FDEA201012034557Switch · malfunctionedCAN OPEN R L1 PASSENGER DOOR CAN NOT OPEN ELECTRICALLY , UNLESS MANUALLY HOLD THE ARM HANDLE AT DISARM POSITION. MEL 03DEC10 19:03, CAN R RELEASED FOR SERVICE IAW MEL: 52-10-01. R & R DOOR CONTROL INTERLOCK SWITCH S1-1090, AND GIRT BAR ARMED WARNING SWITCSDR FDEA201011154375Fan Blade · bentDURING TAKEOFF GOT "ICE DETECTED" FOLLOWED BY EVM COMP NR 3 ENG 5.6 WITH AMBER BOX. CREW FELT THE EXCESSIVE VIBRATION. ON ARRIVAL INSPECT FAN AREA AND FOUND 2 FAN BLADE BENT. FOUND ALSO SLIGHT REMAIN OF BLOOD AROUND THE ICE DECTECTOR AND NEAR THE OUTER FAN ASDR FDEA201010294192Engine · failedCLIMBING OUT OF 7000, NR1 ENG FAILED WITH A FIRE INDICATION. QRH PROCEDURES, SHOT BOTH BOTTLES, FIRE INDICATION REMAINED. N1, N2, NEAR ZERO. R&R NR 1 ENG IAW WORK CARDS. REF WORK CARDS, OK FOR SERVICE.SDR FDEA201010294193Battery Pack · out of positionTEST LIGHT ON L1 DOOR DOES NOT ILLUMINATE DURING TEST. REPOSITIONED BATTERIES IAW AMM 25-61-04-4-0. OPS WAS NORMAL. ACFT OK FOR CONTINUED SERVICE.SDR CLCA10212010.5Warning Light · illuminatedDURING CRUISE FL 310, LEVEL 2 ALERT ENGINE. FOLLOWED QRH PROCEDURE AND RETURNED TO MIA. LANDING AND TAXI TO RAMP NORMAL.SDR IPXA10M63170Sign · failedEXIT SIGN OVER R1 DOOR CAME OFF. R & R R1 DOOR EXIT SIGN IAW AMM 33-27-05-4.SDR IPXA10M63095Light · inoperativeFWD LOWER MAIN ENTRY DOOR EMERGENCY LIGHT AT THE LOWER POSITION, INOP. R & R DOOR LIGHT IAW AMM 33-051-1. OPS CK NORMAL. ACFT OK FOR CONTINUED SERVICE.SDR FDEA201010073971Control Panel · odorPROIR TO STARTUP F/O AND CAPT HEARD WHAT SOUNDED LIKE ELECTRICAL ARCING AND SPARKING. THEN SMELLED ELECTRICAL SMOKE IN THE COCKPIT. OVERHEAD SWITCH ONLY LIGHTING / CIRCUIT BREAKER WAS POPPED. RESET OVERHEAD PANEL LIGHTING CIRCUIT BREAKER. NO FAULTS NOTED OSDR IPXA10M62998Lamp · inoperativeCABIN EMERGENCY LIGHT INOP AT L1 DOOR CEILING PANEL. RELAMPED EMERGENCY LIGHTS. REF AMM 33-52-04-2. OPS CK NORMAL.SDR IPXA10M62922Structure · damagedRT NR1 SLAT OTBD AFT CORNER DAMAGED. REPAIRED IAW MD11-5750-39569-B.SDR FDEA201009293790O-Ring · missingNOTICED NR 2 ENGINE OIL AT 7 QTS. LOSING APPROX 1 QT IN 20 MINUTES. DIVERTED. ENROUTE OIL QTY DECREASED TO 2 QTS & OIL PRESS STARTED TO DECREASE. ENGINE SHUTDOWN. EMERGENCY DECLARED. LANDING UNEVENTFUL. ISOLATED LEAK TO NR 2 ENG LOWER INBD HYD PUMP DRISDR IPXA10M63020Longeron · corrodedINSPECTION TYPE:1C AFTER REMOVAL OF L3 DOOR SCUFF PLATE FOR NDT INSP FOUND CORROSION ON EXTERNAL LONGERON BELOW DOOR CUT OUT. REMOVED DAMAGE FROM LONGERON 28 AT STA 1305 BELOW L3 DOOR CUT OUT. FABRICATED REPAIR PARTS AND INSTALLED REF EA 011-5310-01-A2722 ANSDR IPXA10M63030Longeron · corrodedINSPECTION TYPE:1C, AFTER REMOVAL OF R3 DOOR SCUFF PLATE FOR NDT, FOUND CORROSSION ON EXTERNAL LONGERON BELOW DOOR CUT OUT. REMOVED LONGERON 28R BELOW R3 DOOR CUT OUT FROM STA 1159-1341. INSTALL ED REPLACEMENT LONGERON REF SRM 51-33-01 PG 30-31.SDR FDEA201009293779Doubler · corrodedLT WING UPPER WING SURFACE MLG SUPPORT UPPER DOUBLER AT XORS 288 FOUND CORROSION. CARRIED OUT RECTIFICATION AS PER EA 1-5710-143434. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.SDR IPXA10M62804Door Frame · damagedMCD AFT JAMB INNER SKIN DAMAGED. REPAIRED IAW MD11-5310-39632-B.SDR IPXA10M62945Doubler · crackedINSPECTION TYPE:1C, WHILE PERFORMING DVI OF THE REPAIRED AREA REF EA 011-5720-01-A2697 STEP E, FOUND 3 CRACKS ON BEADED DOUBLER AT INBD OF FORMER XOS 789.6. REMOVED DAMAGE ON RT WING FIXED L/E BEADED DOUBLER BETWEEN STA XOS 783. 2 TO XOS 789.6. FABRICATED SDR IPXA10M63019Skin · chafedINSPECTION TYPE:1C, LT WING FIXED L/E AT NR 3 SLAT ANTI-ICE DUCT CUT OUT DOUBLER HAS CHAFE DAMAGE 2 PLACES (INBD AND OTBD OF ANTI-ICE DUCT). REMOVED EXISTING REPAIR FROM LT WING FIXED L/E AT ANTI-ICE DUCT BETWEEN XOS464-XOS470, CUT OUT DAMAGE AT STA XOS470 WSDR IPXA10M63049Skin · delaminatedINSPECTION TYPE:1C, TAP TEST OF REPAIR AREAS ON LT INBD ELEVATOR HAS REVEALED 2 AREAS OF DELAMINATION: UPPER SURFACE, APPROS. 1.7500" DIA NEAR AFT INBD CORNER AND LOWER SURFACE AFT INBLD CORNER BETWEEN DRAIN HOLE AND IND EDGE. ACCOPLISHED REPAIR IAW STA-SA EASDR FDEA201009193544Landing Gear · malfunctionedAFTER T/O COULD NOT RAISE GEAR. RUN QRH AND RETURN. PULLED GEAR HANDLE UP TENSION FELT LOOSE, ALSO ALL 4 LIGHT BOTH PRI AND SECONDARY WERE EITHER ALL RED, WITH HANDLE UP OR ALL GREEN WITH HANDLE DOWN.SDR IPXA10M62925Skin · crackedINSPECTION TYPE:1C, RT WING FIXED L/E SLAT TRACK NR 14 DOOR WING CUT OUT FOUND WITH SUSPECTED CRACK AS MARKED. REMOVED DAMAGE ON RT WING FIXED L/E AT SLAT TRACK NR 14. FABRICATED DOUBLER AND FILLER AND INSTALLED REF SRM 57-40-02, FIG 201, REPAIR 7.SDR IPXA10M62966Stiffener · crackedINSPECTION TYPE:1C, RT WING FIXED L/E COMPT OTBD OF SLAT TRACK NR 12 FOUND STIFFENER CRACKED AS MARKED. REMOVED DAMAGE AND REWORKED RT WING FIXED L/E STRINGER INBD OF XOS 789.6. FABRICATED REPAIR STRAP AND FILLER AND INSTALLED REF EA 011-572 0-01-A2697 REV I/SDR IPXA10M62967Skin · chafedINSPECTION TYPE:1C, RT WING FIXED L/E SLAT NR3 WING ANTI-ICE TELESCOPIC DUCT DOOR CUT-OUT REPAIR DOUBLER FOUND CHAFED. REMOVED DAMAGED REPAIR FROM RT WING FIXED L/E SLAT NR3 WING ANTI-ICE TEL ESCOPIC DUCT DOOR CUT-OUT L/E SKIN. FABRICATED DOUBLER AND FILLER ASDR IPXA10M62969Stiffener · crackedINSPECTION TYPE:1C, RT WING FIXED L/E COMPT OUTBD OF SLAT TRACK NR10 FOUND STIFFENER WITH SU SPECTED CRACK AS MARKED. REMOVED DAMAGE AND REWORKED RT WING FIXED L/E STRINGER INBD OF STA XOS 667.6. FABRICATED REPAIR STRAP AND FILLER AND INSTALLED REF EA 011- 5SDR IPXA10M62504Panel · delaminatedRT SIDE FUSELAGE /PYLON ACCESS PANEL DELAMINATED ON INSIDE AND OUT SIDE SKIN. REPAIRED REF EO MD11-5430-39593-A.SDR FDEA201009093335Seat Track · corrodedMAIN DECK CARGO - SEAT TRACK AT STA 1717 X= -27 FOUND CORRODED. MAIN DECK CARGO SEAT TRACK CROWN AREA CORROSION REMOVED AS PER SRM 51-21-01 REVISION 44. ORIGINAL THICKNESS= 0.100"; MATERIAL REMOVED= 0.050"; MATERIAL REMAINED= 0.050" FOUND EXCEEDED LIMSDR FDEA201009093336Seat Track · corrodedMAIN DECK CARGO - SEAT TRACK AT STA 1281 X= 47.5 FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-21-01 REVISION 44. ORIGINAL THICKNESS= 0.100"; MATERIAL REMOVED= 0.050"; MATERIAL REMAINED= 0.050" FOUND EXCEEDED LIMIT AS PER SRM 53-00-52 FIGURE 101 REVISSDR WRNA20100004Cylinder · leakingAFTER TAKEOFF, LT MLG UNSAFE (RED) LIGHT ILLUMINATED BOTH PRIMARY AND SECONDARY. PERFORMED APPROPRIATE CHECK LIST. DUMPED FUEL,APPROX 20,380 GALLONS, RETURNED TO AIRFIELD WITH UNEVENTFUL LANDING. ACFT RETURNED TO GATE. MX PERFOMED INSP WHEN ACFT RETURNED TO GSDR IPXA10M62493Skin · crackedINSPECTION TYPE:1C, RT WING FIXED L/E OTBD OF SLAT TRACK DOOR NR1 CUT OUT. FOUND REPAIR DOUBLER CRACKED. REMOVED EXISTING REPAIR DOUBLER AT RT WING L/E OTBD OF SLAT TRACK DOOR NR 1 CUT OUT AREA. FABRICATED AND INSTALLED REPAIR DOUBLER REF SRM 5 7-40-02-2, R7SDR IPXA10M62523Strap · corrodedINSPECTION TYPE:1C, LT WING T/E UPPER SURFACE T/E JUST INBD AND FWD OF NR 2 SPOILER, XORS 480 APPROX, STRIP PANEL AND ADJACENT PANEL CORNERS ARE BULGING DUE TO EXFOLIATION CORROSION. REMOVED LT WING UPPER SURFACE T/E FILLER STRAP AT XORS 480 APPROX FABRICATEDSDR IPXA10M62494Skin · crackedINSPECTION TYPE:1C, LT WING L/E COMPT CEILING IS CRACKED AT FASTENERS AT XOS 767-762. REMOVED DAMAGED AREA OF LT WING L/E UPPER SURFACE AT XOS 762.5 TO 76 7.0. FABRICATED AND INSTALLED REPAIR REF SRM 57-40-02, REPAIR 9, FIG 203, REV 44.SDR IPXA10M62522Skin · dentedINSPECTION TYPE:1C, DEFERED ITEM D-368427 LT WING L/E INBD SKIN DENT HAS INTERIM REPAIR. REMOVED EXISTING REPAIR FROM LT WING FIXED L/E BETWEEN XIS 294.724 AND XIS 305.510. FABRICATED AND INSTALLED NEW REPAIR PARTS REF EO MD11-573 0-28618-C AND EA 011-5730-01SDR FDEA201008112920Skin · crackedCRACK INDICATION APPROX 1" LENGTH FOUND DURING X-RAY INSP AT STA 6-100, LONGERON -2L FWD SECTOR. REPAIRED AS PER SRM 53-00- 05 FIGURE 202 REPAIR 1 REVISION 44 AND E.A. 1-5310-140453. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 110.SDR FDEA201008112921Skin · crackedCRACK INDICATION APPROX 1" IN LENGTH FOUND DURING X-RAY AT STA 6-100, LONGERON -2R FWD SECTION EDGE. REPAIRED AS PER SRM 53- 00-05 FIGURE 202 REPAIR 1 REVISION 44 AND E.A. 1-5310-140453. REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 110.SDR FDEA201008112923Longeron · crackedCRACK INDICATION APPROX 0.5" IN LENGTH FOUND DURING X-RAY INSP AT STA 6-100, LONGERON -4R FWD SECTION EDGE. CRACKED LONGERON-4R AT FORWARD SECTION EDGE STATION 6-100, REPAIRED AS PER SRM 53-00-05 FIGURE 202 REPAIR 1 REVISION 44 AND E.A. 1-5310-140453. THIS RSDR FDEA201008112925Skin · cracked8 FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSP AT LT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=690 AND STA XORS=700. CARRIED OUT REPAIR AS PER EA 1-5710-132467. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV. 110.SDR FDEA201008112927Skin · cracked(10EA) FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSP AT RT WING LWR SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=690 AND STA XORS=700. CARRIED OUT REPAIR AS PER EA 1-5710-132468. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV 110.SDR FDEA201008102913Access Panel · crackedLT WING L/E LOWER ACCESS PANEL 519CB CUTOUT FWD INBD CORNER SUSPECTED CRACK. TRIMMED OFF AND REPAIR CARRIED OUT AS PER SRM 57-40-02 FIG. 201 REPAIR 7 REVISION 44. THIS REPAIR IS CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 110SDR FDEA201008092884Unknown · unknownFLT 5034/06, FLIGHT CREW STATED THE ACFT ENCOUTERED SEVERE TURBULENCE AT 10,000 FT MSL. THE CAPTAIN REPORTS LOOSING 700 FT AND EXPERIENCING MOMENTARY STICK SHAKER. COMPLY WITH MM 05-51-01-6 EXCESSIVE MANEUVER OR TURBULENCE - OVERLOAD CONDITON. COMPLY WITH ASDR IPXA10M61632Control Unit · inoperativeON DESCENT, ENCOUNTERED BUSS AC 1 OFF AND LEVEL 2 SELECT FADEC ALTERNATE. RAN FADEC CHECKLIST AND SELECTED ALTERNATE ON ALL 3 ENGINES. OTHER ALERT ON ELC SYNOPTIC WERE (AC T/E OFF, EMER PWR ON, AND GEN 1 OFF). EMERGENCY DECLARED. ON ELECT CONTROL PANEL MANUASDR IPXA10M61558Doubler · chafedINSPECTION TYPE:1C, LT TELESCOPIC DUCT CUTOUT DOUBLER CHAFED. REMOVED DOUBLER, CUT OUT SKIN, FABRICATED AND INSTALLED REPAIR FILER AND DOUBLER IAW SRM 57-40-01, REPAIR 10.
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