GE CF6-80 series
Service difficulty reports · 1,092
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 = 'CF680' 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 = 'CF680' 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 FDEA201407241951Wire Harness · failedPASSING 1000 FT AFTER TAKEOFF, RECEIVED A NR 2 ENGINE THRUST REVERSER PRESSURIZED. REPLACED ECS CONTROL WIRE HARNESS AND THRURST REVERSER RETURNED TO NORMAL CONFIGURATION, PERFORMED OPS TEST OF HP VALVE AND THRUST REVERSER, ALL CHECKED GOOD.SDR UIEA2014071000324Ring · crackedNUMBER 2 ENG RT THRUST REVERSER AFT CASCADE SUPPORT RING FOUND CRACKED AT NR 6 CASCADE. LOWER SUPPORT RING REPLACED IAW E0 1978A084.SDR FDEA201406151459O-Ring · leakingDURING FLIGHT, NR 2 ENGINE OIL QTY STARTED TO SLOWLY DROP TO ZERO. SHUT ENGINE DOWN IAW QRH. LOWEST PRESSURE 36PSI, TEMP 110 DEG. CREW STATED WINDMILL TIME WAS 45 MINS. NR 2 ENGINE LOST OIL QTY. REMOVED AND REPLACED STARTER GEARBOX CARBON RING ASSY. INSDR IPXA2014052383020Clamp · looseRT ENGINE BLEED DUCT LEAK. TIGHTENED NR 2 BLEED INTERCONNECT DUCT CLAMPS IAW AMM 36-11-01-401, TASK 424-019-001, PAR F, SUB PAR 4. PERFORMED ENGINE GRAD RUN, N1=50 PERCENT, N2=88.4 PERCENT. NO DUCT LEAK INDICATION, LIGHT AND EICAS, OK FOR SERVICE.SDR IPXA2014051282932Cap · openPERFORMED AN AIR TURN BACK DUE TO RT ENGINE OIL PRESSURE LOW ON CLIMBOUT. ENGINE WAS NOT SHUTDOWN. FOUND RT ENGINE OIL CAP OPEN. SERVICED RT ENGINE WITH TWO QUARTS OF OIL IAW AMM 12-13-01-613. OK FOR SERVICE.SDR AALA20140501007Probe · faultyJFK CREW REPORTED LT ENG EGT INCREASED UNTIL JUST BELOW MINIMUM LIMIT. EMER DECLARED FLIGHT RETURNED JFK LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. FOUND LT ENG EGT FOUND TO BE IN LIMITS BUT RT ENG EGT WAS LOWER THAN REQUIRED. REPLACED RT ENG 1 THSDR UIEA2014031700110Mount Fitting · crackedNR 2 ENG LT THRUST REVERSER COWL FWD BULKHEAD LOWER THRUST REVERSER ACTUATOR MOUNTING FITTING FOUND CRACKED. CRACK AREA REPAIRED IAW CMM 78-32-02 REPAIR 016.SDR UIEA2013121300598Hmu · faultyNUMBER 1 ENG PRECAUTIONARY SHUTDOWN. BY MCC REQUEST PERFORMED WIND WILL INSPECTION IAW MM 72-00-00-206-0059-J00, NO FAULTS NOTED AT THIS TIME. ECM 2013P-148 ASSIGNED WHICH INCLUDED BORE SCOPE INSPECTIONS & HMU REPLACEMENT THESE ITEMS WERE WORKED ON LP 540652SDR IPXA2013102800712Lamp · inoperativeEXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LAMP, OPS GOOD IAW AMM 33-51-16-201.SDR SAJF201310080029Starter · failedB-18358. NR 1 ENGINE LOW OIL QTY & LOW OIL PRESSURE, PERFORMED QRH , NR 1 ENGINE SHUTDOWN INFLT . ACFT DIVERTED. GROUND CHECK & FOUND STARTER FAILED LEADING TO LOSS OF ENGINE OIL.SDR HALA2013081200100Idg · failedAIR DIVERSION - RT GEN DRIVE EICAS DISCONNECTED GEN DRIVE. R & R NR 2 IDG IAW AMM 24-11-01. LEAK AND OPS CHECKED GOOD. OK FOR SERVICE.SDR WRLA20130731598Skin · corrodedCORROSION WAS FOUND ON SKIN AJC7060, FROM STA Y:2140 TO 2163, L-33R TO L-35R. REPAIR CORROSION AREA IAW EI W2013A53B-1996, REV 1. COND CHECKED NORMAL.SDR WRLA201310020597Frame · corrodedCORROSION WAS FOUND ON FUSELAGE FRAME, AT STA Y 410, BETWEEN X 15 AND X -10. REPLACE DAMAGE FRAME WITH NEW FRAME IAW SRM 51-35-01 AND 51-33-01, REV 53 AND EI NR W2013A53B-2032, REV 1.SDR WRLA20130727599Skin · crackedCRACK ON LT WING FIXED L/E NOSE SKIN AT STA XOS 944. REPAIR THE DAMAGE AREA, IAW EI W2013A57B-1989, REV1. CONDITION CHECKED NORMAL.SDR WRLA201310020600Skin · crackedCRACK ON RT WING FIXED L/E NOSE SKIN AT STA XOS 776. REPAIR RT WING FIXED L/E NOSE SKIN IAW EI W2013A57B-1995, REV 1. CONDITION CHECKED NORMAL.SDR WRLA20130727601Wedge · debondedDISBOND WAS FOUND ON LT WING OTBD FLAP, NRC6753-503L, WEDGE UPPER SKIN AT STA X OF 614.25 TO 676.5. PERFORM THE LT WING OTBD FLAP WEDGE UPPER SKIN REPAIR IAW EI W2013A57B-2048, REV: 0. CHECK CONDITION SATISFACTORY.SDR HALA2013071200087Connector · disconnectedAFTER START RT ENGINE EGT FAILED (13DEG) (BTB). INSPECTED RT ENG THERMOCOUPLES, FOUND CONNECTOR DISCONNECTED ON THE FWD SIDE OF J-BOX. CONNECTED CONNECTOR, RAN ENGINE, EGT INDICATION NORMAL. ALL WORK PERORMED IAW AMM 77-21-02 AND 71-00-00.SDR DALA13028710129Bulkhead · crackedDURING HFEC OPEN HOLE INSPECTION AT BS 1809.5, LT BULKHEAD ON AREA WITH RUB STRIPS INSTALLED, CRACK INDICATION FOUND ON LWR FWD HOLE AT SECOND LAYER FROM INBD APPROX THREE O'CLOCK POSITION IAW CARD 5310-01376-1603, STEP 3, BS 1809.5 BULKHEAD OUTER CHORD, LT PESDR FDEA201305201038Seat Track · misrepairedMAIN DECK CARGO COMPARTMENT SEAT TRACK BETWEEN FRAME 33 AND FRAME 34, -Y953 MISREPAIRED. REPAIRED IAW SRM 53-10-16, FIG 202, REV 23. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.SDR FDEA201304020701Duct · tornAFTER TAKE OFF "ICE DET SINGLE" LEVEL 1 ALERT FOLLOWED BY "AIR SYS 1 OFF" LVL 1 AND LVL 3 MANIFOLD FAIL FOR SYS 1. NO ANTI ICE WING OR ENG WAS ON. LEVEL 3 MANIFOLD FAIL WENT OUT AS AS THROTTLE WAS RETARDED. REPLACED DUCT.SDR DALA1308371609Fairing · delaminatedLEFT WING INBD MAIN FLAP L/E OTBD FAIRING DELAMINATED. REPAIRED IAW SRM 57-53-01, REPAIR 1 AND SRM 51-70-05, PARA 5A (1).SDR WRLA20130308587Actuator · bypassingCREW REPORTED "AUTO PILOT 2 UNAVAILABLE IN FLIGHT. TURNING FINAL APPROACH AUTO PILOT 1 DISCONNECTED. ROLL CONTROL HAD RESISTANCE". DURING TROUBLESHOOTING MAINTENANCE FOUND, WITH ELECTRICAL POWER REMOVED FROM ACTUATOR AND WITH INPUT MECHANISM TO ACTUATOR DISCSDR WRLA20121210567Frame · crackedCRACK - DURING SPECIAL CHECK OF DATUM AIRCRAFT, EGAT MECHANIC FOUND CRACK ON FRAME (P/N: AGA0016-3) BETWEEN L-51R AND L-52, STATION 1853.SDR WRLA20121210568Frame · crackedCRACK - DURING SPECIAL CHECK OF DATUM AIRCRAFT, EGAT MECHANIC FOUND CRACK ON FRAME (P/N: AGA7351-31) BETWEEN L-51L AND L-52, STATION 1871.SDR WRLA20121210569Web · crackedCRACK - DURING SPECIAL CHECK OF DATUM AIRCRAFT, EGAT MECHANIC FOUND CRACK ON WEB (P/N: AGA7184-3) OF CARGO COMPARTMENT FLOOR AT STA 1921, X=5.SDR WRLA20121210570Frame · crackedCRACK - DURING SPECIAL CHECK OF DATUM AIRCRAFT, EGAT MECHANIC FOUND CRACK ON FRAME (P/N: AGA7125-3) BETWEEN L-49L AND L-49R, STATION 1841.SDR WRLA20121210571Support · crackedCRACK - DURING SPECIAL CHECK OF DATUM AIRCRAFT, EGAT MECHANIC FOUND CRACK ON SUPPORT (P/N: AGA7183-3) OF CARGO COMPARTMENT FLOOR AT STA 1942, L-49R.SDR WRLA20121210572Web · wrinkledWRINKLE - DURING SPECIAL CHECK OF DATUM AIRCRAFT, EGAT MECHANIC FOUND WRINKLE ON REPAIR WEB OF AFT BULKHEAD AT STA Y=2007, BETWEEN L-50L AND L-50R. REPAIRED PER EGAT EI: W2012A53B-2903, R00, R01. CONDITION CHECK NORMAL AND JOB COMPLETED.SDR WRLA20121210573Frame · crackedCRACK - DURING SPECIAL CHECK OF DATUM AIRCRAFT, EGAT MECHANIC FOUND CRACK ON FRAME (P/N: AGA7350-31) BETWEEN L-51R AND L-52, STATION 1887.SDR WRLA20121210574Skin · wrinkledWRINKLES - DURING SPECIAL CHECK OF DATUM AIRCRAFT, EGAT MECHANIC FOUND THREE LOCATIONS OF WRINKLES ON SKIN (P/N: AGA7381-1) AT STA 1841~1871, L-43L AND L-48L.SDR WRLA20121210575Frame · crackedCRACK - DURING SPECIAL CHECK OF DATUM AIRCRAFT, EGAT MECHANIC FOUND CRACK ON FRAME (P/N: AGA7129-3) BETWEEN L-51L AND L-52, STATION 1902.SDR WRLA20121210576Frame · crackedCRACK - DURING SPECIAL CHECK OF DATUM AIRCRAFT, EGAT MECHANIC FOUND CRACK ON FRAME (P/N: AGA7137-17) AT L-52, STATION 1975.SDR IPXA2676323Socket · inoperativeEXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT LAMP HOLDER ASSY IAW MM 33-51-16. OPS CHECKED GOOD.SDR FDEA201209273468Floorboard · damagedMAIN DECK CARGO FLOORBOARD 242ZJ CRUSHED AT UPPER SIDE. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.SDR UIEA2012092400442Cam · detachedPOST FLIGHT WALK AROUND INSPECTION, FOUND NR 4 T/E FLAP TRACK FAIRING DAMAGED BY FLAP DRIVE CRANK. FURTHER INSPECTION FOUND THE CAM DRIVE DETACHED FROM MID-FLAP. LT MID-FLAP ASSY AND NR 4 T/E FLAP TRACK FAIRING WAS REPLACED AND RIGGED IAW AMM 27-51-01 AND AMSDR 2012F00215Brake Assy · damagedLEFT MLG BRAKE LEAKING, ABNORMAL BRAKE PISTON DAMAGE, ONE MISSING BRAKE DISC 50 PARTS OF BRAKE DISC FOUND ON RWY. MX ENGINEER OBSERVED AFTER ARRIVAL OF THE ACFT ON STAND E27 A BROKEN BRAKE CYLINDER AND SOME HYD FLUID LEAKAGE.SDR UIEA2012090700382Tension Tie · crackedMAIN DECK RT BS 740 TENSION TIE AREA, ONE HOLE FOUND CRACKED AT FWD CHANNEL APPROX .040" RUNNING UPWARD. FWD CHANNEL REPAIRED IAW SRM 53-20-30-2R-1, REPAIR 1, FIG 201.SDR UIEA2012090700383Channel · crackedMAIN DECK LT BS 720 TENSION TIE AREA, FOUND ONE HOLE CRACK AT AFT CHANNEL APPROX .030". AFT CHANNEL REPAIRED IAW SRM 53-20-30-2R-1, REPAIR 1, FIG 201.SDR P5CA2012072900030Oil System · lowSHUTDOWN NR 1 ENGINE AS A PRECAUTION DUE TO LOW OIL QUANTITY. TWO QUARTS REMAINED. SHUTDOWN TIME 16:40Z. FIRE SWITCH NOT PULLED. REMOVED AND REPLACED ENGINE 1 IDG BLANKING PLATE AND PLUG. SERVICED ENGINE IAW AMM 12-13-03. POST WINDMILL INSPECTION IAW 72-SDR UIEA2012061900272Blade · damagedDURING BIRD STRIKE INSPECTION IAW AMM 05-51-14, ENGINE 4, FAN BLADE; 8 WAS FOUND TO HAVE DAMAGE. (FAN BLADE 8 WAS INSPECTED IAW AMM 72-31-02 AND THE DAMAGE WAS FOUND TO BE OUT OF ALLOWABLE LIMITS. FAN BLADE 8 WAS REPLACED IAW AMM 72-31-00. VIBRATION SURVEY ASDR UIEA2012061900271Blade · damagedDURING BIRD STRIKE INSP IAW AMM 05-51-14, ENGINE 4, FAN BLADE 7 WAS FOUND TO HAVE DAMAGE. (FAN BLADE 7 WAS INSPECTED IAW AMM 72-31-02 AND THE DAMAGE WAS FOUND TO BE OUT OF ALLOWABLE LIMITS.; BLADE 7; REPLACED IAW AMM 72-31-00. VIBRATION SURVVEY ACCOMPLISHED SDR 2012F00107Engine · making metalEICAS MESSAGE FOR RT OIL FILTER. DISPLAY REMAINED WHEN THRUST REDUCED. RT ENGINE SHUTDOWN. ENGINE VIBRATION DURING CLIMB. DURING INSPECTION FOUND DEBRI IN ALL MAGNETIC CHIP DETECTORS. ENGINE REPLACED.SDR UIEA2012052700252Barrel · crackedENGINE 4 INLET COWL OUTER BARREL CRACKED AT 9 O'CLOCK. TIME LIMITED REPAIR ACCOMPLISHED IAW EO4471A094.SDR WRLA20120511538Seat Track · corrodedSTA 636, LBL, 10 CORROSION EXISTS ON LOWER FLANGES OF SEAT TRACK. REMOVED & REPLACED SEAT TRACK AT STA 635 LBL10 IAW SRM 53-00-52 REPAIR 1.SDR WRLA20120511539Seat Track · corrodedSTA 635, RBL 10 CRACKED FLANGE EXISTS ON SEAT TRACK AT CONNECTION TO FLOORBEAM. REMOVED & REPLACED SEAT TRACK SECTION IAW SRM 53-00-52 & 51-31-01.SDR WRLA20120511540Seat Track · corrodedSTA 635, LBL 20 CRACKED FLANGE EXISTS ON SEAT TRACK AT CONNECTION TO FLOORBEAM. REMOVED CRACKED FLANGE SEAT TRACK, FAB NEW IAW SRM 53-00-52. INSTALLED IAW SRM 51-30-01.SDR WRLA20120511541Seat Track · corrodedSTA 635, RBL 20 CRACKED FLANGE EXISTS ON SEAT TRACK AT CONNECTION TO FLOORBEAM. REPLACED CRACKED SECTION IAW SRM 51-10-02 & 51-31-01.SDR WRLA20120511542Seat Track · crackedSTA 635, LBL 40 CRACKED FLANGE EXISTS ON SEAT TRACK AT CONNECTION TO FLOORBEAM. REPLACE SEAT TRACK SECTION IAW SRM 51-31-01 & 53-00-52.SDR WRLA20120419543Beam · corrodedCORROSION FOUND ON BEAM ABOVE AVIONICS ACCESS DOOR FWD SIDE PRESSURE BULKHEAD STATION 475 LBL 18. REMOVED CORROSION AND IT IS OUT OF LIMITS IAW MD-11 SRM 53-00-00 PAGE 215 FIGURE 205. REPLACED SECTION IAW SRM 53-00-00 + 51-31-00. REMOVED CORROSION IAW SRM 5SDR HALA2012040900120Relay · failedETOPS SIGNIFICANT SYS - ON DECENT LT ENGINE WENT INTO GROUND IDLE & RT ENG INTO FLT IDLE, L N1 32.0 R 44.0. REPLACED RELAY K434 IAW WAM 73-21-19/ SSM73-21-02. GROUND RUN UP CHECKED OK.
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