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 CA110621005Fitting · leakingTHE CREW EXPERIENCED A LOW HYD SYS PRESSURE AND DECLARED AN EMERGENCY PRIOR TO LANDING. EICAS C HYD QTY MESSAGE 4 HRS AFTER T/O. C HYD QTY SHOWED 0.46 TURNED OFF C HYD PRESS TO SAVE FLUID. QTY SLOWLY DROPPED TO 0.35. FRM 29-11-15-00 HYD LEAK FOUND AT C2 PUMSDR CA110704010Union · leakingEICAS C HYD QTY MESSAGE 4 HRS AFTER T/O. C HYD QTY SHOWED 0.46 TURNED OFF C HYD PRESS TO SAVE FLUID. QTY SLOWLY DROPPED TO 0.35. FRM 29-11-15-00. HYD LEAK FOUND AT C2 PUMP PRESSURE LINE. SEAL REPLACED AT PUMP UNION IAW AMM 29-11-02, PB401. LEAK CHECK OK. SDR CA110609006Brake · overheated(CAN) AS THE ACFT PULLED INTO THE GATE THE LEAD REPORTED HOT BRAKES AND SIGHTING OF FLAMES. AIRPORT FIRE AND RESCUE ATTENDED THE ACFT. THERE WAS NO FIRE. NO MORE INFO IS AVAILABLE, NO OTHER SYS ENTRIES FOUND (AUG 24 2011).SDR CA110607014Contactor · looseRELAY FAILED IN FLIGHT CAUSING SEVERAL SYS FAILURES. PART WAS REPLACED ON SPEC. IT WAS NOTED THAT SEVERAL OF THE CONNECTING POSTS WERE LOOSE, ALMOST IF THE BONDING MATERIAL OR SOLDER HAD FAILED.SDR IPXA11665996Panel · delaminatedVERTICAL STAB PANEL DELAMINATED, AREA MEASURING 11.5 BY 6.5" 18" FROM FWD EDG E PF PANEL AND 39" UP FROM THE BOTTOM. REPAIRED REF EO B767-5530-41998-B.SDR CNMA20110016Stringer Clip · corrodedANGLE CORRODED AFT OF FRAME RT FS 1285 AT FLOOR LINE. REMOVED CORRODED ANGLE FOR REPLACEMENT-FABRICATED NEW STRINGER CLIP IAW DWG 146T1510. INSTALLED NEW STRINGER CLIP IAW SRM 51-40-02, PAR 7.SDR CA110324004Receptacle · contaminated(CAN) AFTER DEPARTURE, THE AIRCRAFT BEGAN EXPERIENCING PROBLEMS WITH THE RIGHT SIDE EGT INDICATION IN NORMAL AND STANDBY. RIGHT HAND EGT ON UPPER EICAS AND STANDBY ENGINE INDICATOR WENT BLANK ON CLIMB OUT. OCCASIONALLY EGT WOULD INDICATE BUT ERRONEOUSLY. CREW SDR CA110323004Rvdt · misrigged(CAN) ON APPROACH THE CREW HAD A LE ASYMMETRY FAULT. PERFORMED A GO AROUND. QRH PROCEDURE WAS CARRIED OUT & THE FLIGHT THEN LANDED, FLAP & SLAT UNIT MSG M48. OTBD SLAT PDU RVDT MIS-RIG, SLAT & FLAPS ALTERNATE CYCLED. FLAP & SLATS OPERATED SEVERAL CYCLES ONSDR NOCA01511Turbine Blades · damagedFOUND NR 2 ENGINE LOWER PRESSURE TURBINE BLADE DAMAGED ON WALK AROUND. REPLACED NR 2 ENGINE AS PER JOB CARD 767-71-R07.SDR CA110222001Transfer Valve · failedON T/O AT APPROX 100 KTS EICAS WARNING L FWD PUMP & LT FWD LOW PRESS LIGHT ILLUM . REJECTED T/O. AFTER REJECT TO, PRESS LIGHT EXTINGUISHED. MAX BRAKE TEMP 5 ACFT HAD DEPARTED UNDER MEL 28-22-01 L/H AFT BOOST PUMP INOP. LT DEFUEL VALVE ACTUATOR REPLACED IAW SDR CA110105007Buss · failedAS A RESULT OF A MALFUNCTION OF THE ELECTRICAL BUSES, THE FLIGHT ELECTED TO RETURN WITH SUBSEQUENT OVERWEIGHT LANDING. REPEAT SNAG, L/R UTILITY BUSS OFF LIGHTS, EICAS MESSAGE, L/R RECIRC FANS OFF LIGHTS WITH LOSS OF GALLEY POWER AND PAX READING LIGHTS U/S. ISDR CA110103006Wire · brokenFLIGHT RETURNED TO DUE RED EICAS FLAP/SLAT ALERT T/O CONFIG, LANDING NORMAL. FINDINGS LISTED SEQ 2 DIODE BLOCK R608 PIN LOCK BROKEN AND LOOSE WIRE. DIODE BLK R608 REPLACED. ALSO L FSPM REPLACED AND TESTED IAW AMM 27-58-01-904-001. WEU PCC REPLACED AND TESTESDR DALA1100031706Skin · dentedDURING PSV 10, FOUND A DENT AT STA 1373 AND STR 29. THE DENT IS 6.5 LONG, 3.4 WIDE, .141 DEEP. REF NRC 29 AND ERA 488494-14, REV A. TRIMMED OUT DENT, ACCOMPLISHED HFEC INSP ALONG EDGE OF TRIM OUT. ACCOMPLISHED .040 INSURANCE CUT. BHEC INSPECTED ALL EXISTISDR IPXA10663910Altimeter · inoperativeSTBY ALTIMETER INOP, DIVERTED. T/S C/O IAW FIM 34-13-06, FIG 104, STEP 1,2,3, AND 23. CYCLED CB'S 11B7 11P2, 11A8. STBY ALTIMETER OPERATES OK. NO FURTHER PROBLEMS AND MALFUNCTIONS FOUND.SDR IPXA0663696Panel · damagedREF D439829, POSITION 4, DAMAGE 5" FROM RT SIDE PANEL AND 5' FROM A FT EDGE. FABRICATED AND REPLACED PANEL IAW EO B767-5320-9693-G.SDR CNMA20100033Skin · dentedBIRD STRIKE ON RT WING OTBD FLAP LOWER SURFACE OTBD OF INBD FLAP VORTELON BY 42" AND 10" FROM T/E WITH SURFACE CRACK 9" PARALEL TO SEAM. DENT AREA 5" RND. R & R RT OTBD FLAP IAW MM 27-11 & SB 767-27A0155.SDR IPXA0663686Floor Panel · damagedMAIN DECK FLOOR PANEL, PN 145T5876-68 IS DAMAGED. FABRICATED NEW FLOOR PANEL ON NRC 355114 IAW EO B767-5320-9693-G.SDR IPXA0663704Floor Panel · damagedMAIN CARGO FLOOR PANEL REQUIRES FABRICATION IAW EO B767-5320-9693E. THIS IS A MAJOR REPAIR. ACCOMPLISHED FABRICATION OF MAIN CARGO FLOOR PANEL ON NRC 355114 IAW EO B767-5320-9693E.SDR IPXA10663560Floor Panel · damagedREF D-4344202 POSITION 2L HAS 1 X 1 HOLE IN FLOORBOARD. REMOVED FLOOR PANEL AND MFG NEW PANEL IAW EO B767-5320-9693 AND INSTALLED IAW AMM 51-01-01.SDR CA101108008Printer · odor(CAN) ON GROUND, MAINTENANCE NOTICED A VERY STRONG BURNING SMELL IN FLT DECK. ACARS PRINTER FOUND TO BE AT FAULT. PRINTER REPLACED.SDR IPXA10663448Floor Panel · damagedMAIN CARGO DECK POSITON 10L FLOOR PANEL HAS SMALL HOLE 2" X 1". FABRICATIED NEW FLOOR PANEL PN 146T5869-107 IAW EO B767-5320-9693G.SDR CA101027012Module · failed(CAN) ON DEPARTURE, CREW RECEIVED 2 MOMENTARY EICAS STAB TRIM FAULTS, THEY ALSO REPORTED NO STAB MOVEMENT. FOUND R STCM FIM BALL YELLOW IN VIEW AT R SAM RESET OK, MCDP NO LAST FAULT. MCDP 65 GRD TEST COMPLETED MAN & A/P STAB OPERATION CHECKED OK. REF FIM 2SDR IPXA10663317Floorboard · dentedREF DMI D429161, MAIN CARGO DECK POS NR 2 RT FLOORBOARD - 2ND BOARD IN FROM OTBD HAS A 1-INCH BY 1-INCH DENT. REPLACED FLOORBOARD WORKING WITH EO B767-5320-9693 AND M/M 53-01-06.SDR CA101025005Wire · burnedWHILE IN CRUISE, THERE WAS A ELECTRICAL ODOR AROUND ROW 7. THE ENTERTAINMENT SYS AND LIGHTS WERE TURNED OFF AND THE ODOR DISSAPATED. SEAT 5-9AF SEAT CONTROL BOXES ALL CHECKED. ALL OPS NORMAL. NO DAMAGED OR BURN EVIDENCE FOUND. PSU`S IN CEILING AT SAME SESDR IPXA10663210Skin · damagedRT OTBD FLAP T/E WEDGE SKIN DAMAGED. REPAIRED IAW EO B767-5750-39284-B.SDR CA101019007Valve · failedDURING THE APPROACH TO LAND, THE CREW ADVISED THEY HAD AN ANTI-SKID FAILURE AND WERE REQUESTING A LONGER RUNWAY FOR THE LANDING. THE LANDED WITHOUT USING THE ANTISKID AND WITHOUT INCIDENT. INBD ANTI-SKID BITE VALVE 7 FAULT ANTI-SKID NORMAL AND ALT TEST NO FASDR IPXA10663178Eec · inoperativeINSPECTION TYPE:ETOP, LT ENGINE SHUTDOWN DUE TO AN ENGINE VALVE LIGHT AT 300 FT, WHILE ON FINAL APPROACH. R & R EEC DUE TO STORED PIMU MESSAGE.SDR IPXA10663155Compressor · stalledINSPECTION TYPE:ETOP, RT ENGINE HAD 4 COMPRESSOR STALLS AT 200 FT, NO HIGH EGT OR ENGINE EXCEEDENCE. CHECKLIST WAS ACCOMPLISHED, TRIED ONE MORE RECOVERY, HOWEVER ENGINE STALLED AGAIN. ENGINE WAS SHUTDOWN, LANDING WEIGHT WAS 320.00. R & R ENGINE.SDR CA101015001Pseu · failedAFTER TAKEOFF AND IN CLIMB THE CREW REPORTED FLAP/SLATS ASSYMETRY. DISCUSSIONS WITH MX TO RECTIFY THE PROBLEM WERE UNSUCCESSFUL AND THE FLIGHT RETURNED TO DEPARTURE, APPROX 25,000K OVERWEIGHT FSEU LAST LEG CODES 27-81021 & 27-81042. PSEU BIT FAULTS NR 10 & S3SDR IPXA10663056Floorboard · damagedHOLE IN MCD FLOORBOARD POSITION 4 CTR FS.635, LBL3. REPAIRED IAW SRM 53-00-50-2R PARA 6.SDR DALA1025911703Light · inoperativeDURING DRC MX, FOUND EMERGENCY ESCAPE PATH MARKING LIGHT OUT AT SEAT 22AB AND FORWARDED IAW MEL 33-51-03A.SDR DALA1025571609Light · inoperativeTHE COCKPIT EMERGENCY LIGHT ABOVE DOOR DOES NOT ILLUMINATE WITH TEST SWITCH OR LIGHT ON SWITCH. MX REPLACED THE LIGHT ASSY. SYS OPS IS NORMAL.SDR DALA1025581706Fuse · inoperativeEMERGENCY LIGHTS SEATS 14AB THROUGH 21AB ARE INOPERATIVE. MX REPLACED BAD FUSE AT POWER SUPPLY M1209. SYS OPS IS NORMAL.SDR IPXA10662910Floor Panel · damagedPOS 4 RT MAIN CARGO DECK FLOOR PANEL 3 RD FROM RT HAS DAMAGE. REMOVED AND MANFACTURED NEW PANEL IAW EO B767-5310-9693-G.SDR IPXA10662886Pressure Switch · inoperativeE-TOP DIVERSION LT ENGINE ANTI-ICE DISPLAYED AND ENGINE ANTI ICE VALVE REMAINED ILLUMINATED WITH SWITCH ON. REPLACED LT ENG ANTI ICE VALVE IAW MM 30-21-03-4 AND THERM A/I PRESS SWITCH IAW MM 30-21-04-4. OPS CHECK NORMAL.SDR DALA1025111701Connector · damagedEMERGENCY LIGHTS AT SEAT 26G AND 33B ARE INOPERATIVE. MX RE-PINNED THE CONNECTOR AT LIGHTS. SYS OPS IS NORMAL.SDR DALA1025091606Connector · looseEMERGENCY LIGHTS AT SEATS 32FG-34FG ARE INOPERATIVE. MX SECURED LOOSE CONNECTOR AT 34FG. SYS OPS IS NORMAL.SDR IPXA10663042Attach Fitting · crackedINSPECTION TYPE:C, BS 955 REAR SPAR BULKHEAD ATTACH FITTING FOUND 1EA FASTENER HOLE CRACKED APPROX 0.020" RUNNING DOWN. AND FOUND 2 EA FASTENER HOLES SHORT EDGE MARGIN ARE 1.33" AND 1.664". ATTACH FITTING REPLACED IAW EO B767-5350-17922G APP C & REPAIRED IAWSDR IPXA10663051Skin · damagedINSPECTION TYPE:C, BS 955 REAR SPAR BULKHEAD SIDE FITTING FAILSAFE STRAP SKIN ATTACH AREA DAMAGE FOUND AFT FAILSAFE STRAP CUTOFF. DAMAGE SMOOTHED OUT & REPROTECTED IAW R53-50-36849 & EO B767-5330-40064. BLEND OUT AREA A 0.75" X 2.75" X 0.025", AREA B 2" X 2.SDR IPXA10662865Floor Panel · dentedINSPECTION TYPE:8C, M/D STA 540 TO 654+22, RBL 11" TO LBL 11" FLR PNL FND 8 DENTS & 4 DAMAGE. FLOOR PANLE FABRICATE IAW EO B767-5320-9693-G & INSTALLED IAW AMM 53 53-01-01.SDR IPXA10662864Floor Panel · dentedINSPECTION TYPE:8C, M/D STA 933 TO 970, LBL 11 TO RBL 11 FLR PNL FND 12 DENT MARKS & UPPER SURFACE FIBERGLASS DELAMINATED (1" WIDTH & 37" LONG). FLR PNL FABRICATED IAW EO B767-5320-9693-G & INSTALLED IAW AMM 53-01-01.SDR IPXA10662964Wedge · puncturedINSPECTION TYPE:C, RT WING OTBD FLAP T/E WEDGE UPPER SURFACE PUNCTURE. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07, PAR 5A (1) FIG 9, REV 48.SDR IPXA10662988Skin · delaminatedINSPECTION TYPE:C, LT WING OTBD FLAP LWR SURFACE INBD AFT PANEL INBD AREA FOUND DELAMINATED. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R, REPAIR 4, FIG 202, SHEET 3, REV 48.SDR IPXA10662991Failsafe · crackedINSPECTION TYPE:C, BS 955 REAR SPAR BULKHEAD FITTING AREA WAS FOUND CRACKED ON 2 O/C POSITION AT FAIL SAFE STRAP APPROX .1250" IN LENGTH. FUSELAGE BS955 REAR SPAR BULKHEAD SIDE FITTING FAIL SAFE STRAP REPAIRED IAW EO B767-5350-17922-G, APPENDIX C AT LT SIDE.SDR IPXA10662992Fitting · crackedINSPECTION TYPE:C, BS 955 REAR SPAR BULKHEAD FITTING AREA WAS FOUND CRACKED ON 4 O/C AND 10 O/C POSITION AT FAIL SAFE STRAP THROUGH THICKNESS & APPROX .12" IN LENGTH. FUSELAGE BS955 REAR SPAR BULKHEAD SIDE FITTING FAIL SAFE STRAP REPAIRED IAW EO B767-5350-179SDR IPXA10663010Wedge · puncturedINSPECTION TYPE:C, RT WING OTBD FLAP UPPER SURFACE T/E WEDGE PUNCH HOLE. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-07 PAR 5A (1) FIG 9, REV 48.SDR IPXA10663041Stiffener · crackedINSPECTION TYPE:C, LT MLG W/W CANTED PRESSURE DECK AT BS 977 LATERAL "Z" STIFFENER FOUND CRACKED AT FASTENER HOLE AREA BETWEEN LBL 20 AND LBL 55. CRACK LENGTH ARE 1.625" AT LBL 32.94 AND 1.6" AT LBL 54.69. STIFFENER REPAIRED IAW HX RS NR R53-58-36842 REV A &SDR IPXA10662962Fairing · delaminatedINSPECTION TYPE:C, LT WING INBD MAIN FLAP OTBD L/E FAIRING DELAMINATION FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-70-05 PAR 5A(1) FIG 5, REV 48.SDR IPXA10662963Fairing · delaminatedINSPECTION TYPE:C, LT WING OTBD T/E FLAP L/E FAIRING DELAMINATION. FIBERGLASS PREPREG LAY UP REPAIR CARRIED OUT IAW SRM 51-71-05, PAR 5A(1) FIG 5, REV 48.SDR IPXA10662989Skin · chafedINSPECTION TYPE:C, RT WING NR9 SLAT UPPER WEDGE OTBD OF 30" FOUND DEEP CHAFING ON LWR SURFACE. METAL HOT BOND REPAIR PERFORMED IAW SRM 51-70-10-2R. REPAIR 4, FIG 202, SHEET 8, REV 48.
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