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 IPXA1664037Control Cable · damagedCREW REPORTED STAB FAULT INBOUND. MX INSP FOUND LARGE AMOUNT OF ICE WITH PULLEY AND CABLE DAMAGE IN TAIL OF ACFT. FOUND ICE IN STAB AND THE CABLE DRUMS FOR THE STAB INDICATION WERE BROKEN. (OPEN)SDR FDEA201101050014Rib · corrodedVERTICAL STABILIZER RIB 1 WEB TOP SURFACE HAS CORROSION ( ABOUT 4 - SQUARE INCHES) RT STRINGER 5R TO STRINGER 7R VERT STAB RT SIDE REMOVED CORRODED SECTION ON RIB1 WEB BETWEEN STR 5R AND 7R IAW SRM 55-31-19, PG 209 - 210 FIG 203. FABRICATED AND INSTALLED RESDR FDEA201101050016Plate · corrodedVERTICAL STABILIZER, RIB 1, STRINGER 2RT - 5RT REAR LOWER PLATE. LOWER SURFACE CORRODED APPROX 1IN WIDE X 2IN LENGTH JUST ABOVE RT AFT STABILIZER HINGE. R & R VERTICAL STAB RIB 1AFT LOWER PLATE IAW SRM 51-72-10, PGS 1-3.SDR FDEA201101050011Rib · crackedRT WING L/E INBD RIB NR16 CRACKED. RIB REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 45 AND DRAWING ARB7565 REVISION C. THIS REPAIR IS CLASSIFIED AS MINOR AS PER GMM 6-2-100 REVISION 111.SDR FDEA201101050012Slat Track · crackedRT WING SLAT TRACK NR8 CUT OUT OTBD AREA CRACKED. REPAIRED AS PER E.A. 1-5740-143499. THIS REPAIR IS CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.SDR FDEA201101050017Fitting · crackedRT MLG DOOR UPLATCH FITTING FOUND CRACKED. FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 45. FITTING FABRICATED AS PER DRAWING ANB7089 REVISION A. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.SDR FDEA201101050018Fitting · crackedLT MLG DOOR UPLATCH FITTING FOUND CRACKED. FITTING REMOVED AND REPLACED AS PER SRM 51-31-01 REVISION 45. FITTING FABRICATED AS PER DRAWING ANB7089 REVISION A. THIS REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REVISION 111.SDR HALA2011010400011Totalizer · failedETOPS SIGNIFICANT SYS - FMS PROG 2 LOST TOTALIZER FOR FUEL READINGS. T/S IAW FIM 34-61-00, FIG 106, PROGRESS PAGE 2/2 SHOWED TOTALIZER & CALCULATED QUANTITIES THE SAME AT 17.0 ON GROUND. ON BOTH DCU'S COULD NOT DUPLICATE PROBLEM. OK FOR CONTINUED SERVICE. FUSDR HALA2011010400012Engine · out of adjustETOPS SIGNIFICANT SYS - ENG GROUND IDLE PARAMETERS DO NOT MATCH. LT N1-20.9, RT N1 -22.5, LT EGT -468, RT EGT- 396. LT N2 61.8 - RT, N2 - 63.3. LT F/F 1.4 RT F/F - 1.4 FOUND NR 2 ENG IDLE ABOVE LIMITS ADJUSTED TEST NR3 STEP (D)2. ACCOMPOMPLISHED TEST NR3 IASDR HALA2011010300005Warning Light · illuminatedETOPS SIGNIFICANT SYS - AILERON LOCKOUT EICAS ILLUMINATED DURING DESCENT THRU 10000 FT, SPEED 240 KTS, WENT OUT PASSING 4300 FT. T/S IAW FIM 21-11-00, FIG 104, RT SAM FAULTED RT ADC, RESET IAW BLOCK 25, FAULT CLEARED IAW BLOCK 57, SYS CKS OK, OK FOR SERVICE.SDR DALA1100521815Light · inoperativeEMERGENCY PATH LIGHTS AT GALLEY L2 DOOR ARE INOPERATIVE. MX REPLACED THE LIGHT ASSY. SYS OPS IS NORMAL.SDR UIEA2010123100249Skin · dentedDURING WALKAROUND INSP, MX REPORTED DENT DAMAGE FOUND ON THE LT OTBD FORE FLAP - WBL745 UPPER EXTERNAL SKIN PANEL. MEASURING 5.0 IN LENGTH X 3.125 IN. WIDTH & AMP; 0.625 IN. (REF FIG 1). THE DAMAGED AREA EXCEEDS THE SRM 57-53-01, FIG 101, ALLOWABLE DAMAGE 1 SDR FDEA201012304784Switch · inoperativeECAM, FWD CARGO DOOR NOT CLOSED CAME ON AT FL 220 ON DEPARTURE, RAN QRH, CABIN ALT OK, RETURNED TO DEPARTURE, FWD CARGO SWITCH FAULT ECAM CAME ON LATER. R & R FWD CARGO DOOR SWITCH (16WS) IAW MM 52-71-11-04.SDR FDEA201012304786Engine · malfunctionedON INITIAL TAKEOFF, WITH ENGINES STABLE AT 40 PERCENT, UPON SELECTION OF TO GA, NR 1 ENGINE DID NOT ADVANCE. NR 2 ENGINE ADVANCED NORMALY. ACCOMPLISHED LOW SPEED REJECT. SUBSEQUENT TAKEOFF NORMAL. ACCOMPLISHED QRH PROCEDURES AND ENSURED TRP RESET PRIOR TSDR SAJFCALS099042Blades · damaged(B-18310) TOOKOFF AT 0831L, DURING CLIMB AT 0844L AT FLIGHT LEVEL 28000FT, ECAM WARNINGS APPEARED: "ENG 1 EGT OVER LIMIT, ENG 1 FAIL, ENG1 N1 VIBRATION, ENG 1 EGT EXCEEDED DURING AIR START, ENG1 N2 VIBRATION, ENG 1 START FAULT, ENG 1 SHUT DOWN." AT 0855L, CRESDR DALA1052811817Unknown · odorELECTRICAL ODOR COMING FROM THE EYEBALL VENT MID GALLEY, TURNED OFF GASPER FAN SWITCH AND ODOR STOPPED, PULLED CIRCUIT BREAKER R17 AS DIRECTED BY MX CONTROL. MX INSPECTED AREA NO TROUBLE FOUND. CIRCUIT BREAKER RESET. SYS OPS IS NORMAL. ETOPS CATEGORY 'E'SDR FDEA201012234745Slat System · malfunctionedON APPROACH SPEED 230KTS, SLAT SYS 1 & 2 FAULT WHEN SLATS EXTENDED. MOMENTARY WENT OUT. UNTIL FLAP 15 SELECTED, THEN CAME BACK ON. PERFORMED GO-AROUND THEN PERFORMED CYCLE. SLATS EXTENDED OK WITHOUT FAULT. FOUND SFCC1 AND SFCC2 WITH THE SAME 4 FAULT BALLS SDR FDEA201012224739Frame · crackedENG 1 RT THRUST REVERSER COWL FWD RING FLANGE GOT CRACK AT UPPER EDGE, ABOUT 1.5 INCH. REPAIR THE DAMAGE AREA WITH DOUBLER AND FASTENERS IAW DWG NR: SRZ-78-002. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR UIEA2010122200197Skin · damagedDURING WALK-AROUND INSP BEING PERFORMED, DAMAGE WAS FOUND TO THE FUSELAGE SKIN BS 2596 ABOVE STR- 46R (TAIL JACK AREA) CONSISTING OF DENT L:1.5 IN. W:0.750 IN. D:0.0625 (REF FIG 1). THE DAMAGE IS OUT OF THE SRM 53-00-01, FIG 101. ALLOWABLE DAMAGE 1, DETAIL ISDR DALA1052321521Wire Harness · disconnectedEMERGENCY EGRESS AISLE LIGHTING IS INOPERATIVE AT ROW 34. MX RECONNECTED THE HARNESS AND SYS NOW CHECKS OK.SDR DALA1052751701Lamp · inoperativeEMERGENCY EGRESS SLIDE ILLUMINATION LIGHTS INOP AT DOORS 1L AND 1R. RELAMPED 1L & 1R SLIDE LIGHTS, CHECKS OK.SDR FDEA201012204721Frame · deformedMAIN DECK CARGO FRAME AT STA 1661, LONGERON 12 LT FOUND DEFORMED. MAIN DECK CARGO - DEFORMED FRAME AT STA 1661, LONG 12 LT REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2 REV 45. REPETITIVE INSP REQUIRED, INITIAL AT 14,500 CYCLES AND REPETITIVE AT 9,500 CYCLES,SDR FDEA201012204722Longeron Splice · crackedMAIN DECK - DURING HFEC INSP, LONGERON 3, RT SPLICE FITTING AT STA 6-100, FOUND 02 EACH CRACKED APPROX 0.5 INCH. CRACKED SPLICE FITTING AT STA 6-100. R & R IAW SRM 51-31-01, REV 45. NEW LONGERON SPLICE FITTING FABRICATED IAW DOUG DWG A6A7112 REV A. REPAIR CSDR FDEA201012204723Access Panel · crackedLT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN XORS 683.4 AND XORS 713.6. FOUND 04 EACH FASTENER HOLES WITH CRACKED INDICATION DURING HFEC OPEN HOLE INSP. REPAIR CARRIED OUT IAW DWG SG11570004, REV A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 111.SDR FDEA201012204724Access Panel · crackedRT WING LOWER SKIN ACCESS DOOR CUT OUT BETWEEN XORS 683.4 AND XORS 713.6. FOUND 12 EA FASTENER HOLES WITH CRACKED INDICATION DURING HFEC OPEN HOLE INSP. REPAIR CARRIED OUT IAW DWG SG11570004 REV A. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 111.SDR FDEA201012204725Skin · crackedLT WING FIXED L/E SLAT TRACK NR12 CUT OUT FOUND CRACKED. REPAIRED IAW SRM 57-40-02, FIG 201, REV 45. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 111.SDR FDEA201012194717Cover Plate · corrodedAT STA 40951, FR75A AFT CREW DOOR AFT FRAME TOP ON WEB CORROSION ABOUT 3 INCHES AROUND LT SIDE. REPAIRED UPPER WEB OF L-2 DOOR CUT OUT AT FR 75A IAW SRM 53-18-18 PAR 7, FIG 202, SHEET 5 AND DWG A53980302.SDR FDEA201012194718Seat Track · gouged4 GOUGES ON SEAT TRACK SCALLOP ON NR 3R SEAT TRACK FRAME 54 PLUS 12" ABOUT .2500" X .5" EACH. DAMAGE TO SEAT TRACK AT 3R FR 54.2 TO 55/58 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, FIG 101. REMOVED SEAT TRACK IAW SRM 51-72-10, PG1. FABBED NEW SEAT TRACKSDR FDEA201012174714Vane · delaminatedLT WING INBD FLAP VANE LOWER SURFACE FOUND DELAMINATED. R & R IAW AMM 27-50-22-4 REV 69.0. ADJUSTMENT AND TEST CARRIED OUT IAW AMM 27-50-22-5, REV 69.0 FOUND SATISFACTORY.SDR DALA1051671821Fan · failedLT RECIRCULATION FAN IS INOPERATIVE, SMOKE/BURNING ODOR IN THE CABIN. MX REPLACED THE RECIRCULATION FAN. SYS OPS IS NORMAL.SDR FDEA201012164700Gcu · malfunctionedACFT RETURNED TO DEPARTURE WITH NR1 ENGINE GEN FAULTED AND NR 1 AC BUSS FAILURE. INSPECTED AND PERFORMED GPCU BITE. TROUBLE SHOOTING INDICATED NO RESPONSE FROM NR 1 GCU. PULLED NR 1 GCU FROM RACK SMELLED STRONG BURN ODOR. SWAPPED APU GCU INTO NR 1 POSITIOSDR FDEA201012164701Skin · dentedON POST FLIGHT OF ACFT DISCOVERED DENT ON LT SIDE OF ACFT JUST FWD OF NOSE WHEEL AREA. REMOVED DAMAGED AREA BY PERFORMING CUT OUT OF DENT. CUT WAS 3.25 IN LONG X 1.8 IN WIDE. INSTALLED EXTERNAL DOUBLER WITH INTERNAL FILLER IAW SRM 53-12-12, FIG 201, PAGESSDR FDEA201012164709Spar Cap · corrodedLEFT WING REAR SPAR LOWER CAP, ACCESS THROUGH PANEL NR541FB, 8 IN OTBD OF JACK POINT FOUND CORROSION. REMOVED IAW SRM 51-31-01, REV 45 AND REPLACED WITH A FABRICATED STRAP IAW SRM 51-34-01, REV 45. STRAP FABRICATED IAW DWG ARB2615 REV D. FUEL LEAK CHECK SDR DALA1051991814Wire · brokenEMERGENCY LIGHTS AT L4 AND R4 ARE INOPERATIVE. MX REPAIRED THE BROKEN WIRES FOR POWER SUPPLY PLUG D110722. SYS OPS IS NORMAL.SDR FDEA201012144659Carriage · misalignedRT WING NR5 FLAP TRACK FWD CARRIAGE UPPER BRIDGE INBD SIDE SHIM MIGRATION. EA6-2750-141650 REPAIR ACCOMPLISHED. IAW GMM 6-2-100, REPAIR CLASSIFIED AS MINOR.SDR FDEA201012144665Seat Track · corrodedCABIN SEAT TRACK 4 LT HAS CORROSION AT 5 IN AFT OF FR 45. REMOVED LEVEL 1 CORROSION. REMOVED DAMAGED SECTION OF TRACK 4 LT BETWEEN FR 45 TO FR 49 AND INSTALLED SEAT TRACK REPAIR, CTR SECTION FLOORBEAM RAIL SPLICING METHOD IAW SRM 53-10-16, FIG 205, PAGE 231/SDR FDEA201012144663Gearbox · failedON TAKEOFF, FLAP SYS 1 AND SYS 2. FLAPS STUCK BETWEEN 15 AND 20. OCCURRED AT TEMP -4 MX UPDATE FOUND TORQUE LIMITER POPPED IN LT WHEEL WELL. WOULD NOT RESET. FOUND BOTH SFCC'S INDICATING A JAM.SDR FDEA201012134648Light · damagedEMERGENCY LIGHT DAMAGED AT DOOR L1 DROP CEILING. R & R LT DOOR HANDLE EMERGENCY LIGHT ASSY AND OPS CHECK CARRIED OUT IAW MM 33-52-02-2, REV 66.0. SATIFACTORY. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION.SDR DALA1051201814Battery Pack · inoperativeEMERGENCY LIGHTS AROUND L4 AND R4 DOORS ARE INOPERATIVE. MX REPLACED THE BATTERY PACK AT M1210. SYS OPS IS NORMAL.SDR FDEA201012124642Switch · damagedAFTER TAKEOFF, GOT CAC DOOR LEVEL 1 ALERT. RETURNED AND LANDED WITHOUT INCIDENT. MX REPLACED CAC DOOR SWITCH IAW AMM 52-70-02.SDR UIEA2010121100189Skin · damagedDURING WALKAROUND INSP, MX FOUND DAMAGE TO THE OTBD RT WS1585 - L/E NOSE EXTERNAL SKIN MEASURING 2.5 IN. L X 1.5 IN. W AND 0.125 IN. DEPTH (REF. FIG 1). DAMAGED AREA FOUND BEYOND THE SRM 57-41-01, FIG 101, DETAIL III ALLOWABLE DAMAGE (GENERAL) LIMITS. (DISPOSSDR FDEA201012114641Stringer · corrodedREAR FUSELAGE FRAME 84 TO 85 STR 27RT CORRODED ON AFT END APROX 4 IN. REPAIRED STR 27R BETWEEN FR 84 AND FR85 IAW SRM 53-19-14, FIG 202. GENERAL REPAIR SCHEME.SDR DALA1051211814Battery Pack · inoperativeEMERGENCY LIGHT AT L4 AND R4 DOOR ARE INOPERATIVE. MX REPLACED THE BATTERY PACK AT R4 F/A SEAT. SYS IS NORMAL.SDR FDEA201012104634Float Switch · malfunctionedAT FL340 "TANK 3 LOW" & "TANK TIP TRAPPED" NR 3. FUEL IN AUTO TRANSFERRED FROM TANK2 TO TANK3. TOTAL FUEL ONBOARD 18.0. ALERT TANK 2 LOW ILLUMINATED. "TANK 3 TIP TRAPPED ALERT" CAME ON A SECOND TIME AT FL280. DECLARED EMERGENCY AND LANDED MEM WITHOUT INCSDR DALA1051181503Connector · unsecureEMERGENCY LIGHT AT SEAT 21GF ARE INOPERATIVE. MX SECURED THE CONNECTOR AT SIDEWALL. SYS OPS IS NORMAL.SDR FDEA201012064595Seat Track · wornAFT CARGO FR54 TO 54.2 DUMMY TRACK LT NR4 EXCEEDS MINIMUM GAP VALUE (0.048) IAW EO6-5310-7-3322B, PART 1, PG5 STEP 11I. REMOVED DUMMY TRACK 4L AFT CARGO FR54 TO 54.2 IAW SRM51-40-21, PAR 7. ROUTED TO BACK SHOP FOR REPAIR. REPAIRED IAW SRM 53-15-16, PGS 203-SDR FDEA201012064596Seat Track · wornFWD CARGO FR 38.2 TO 40 DUMMY TRACK LT NR3 EXCEEDS MINIMUM GAP VALUE (0.0235) IAW EO6-5310-7-3322B, PART 1, PG 5, STEP 11I. REMOVED DUMMY TRACK 3L AT FR38.2 TO 40 IAW SRM51-40-21, PAR 5. INSTALLED NEW DUMMY TRACK IAW SRM 51-40-21, PAR 5.SDR FDEA201012064597Seat Track · wornAFT CARGO FR54 TO 54.2 DUMMY TRACK LT NR2 EXCEEDS MINIMUM GAP VALUE (0.0240) IAW EO6-5310-7-3322B, PART 1, PG 5, STEP 11I. REMOVED DUMMY 2L AFT CARGO FR54 TO 54.2 IAW SRM51-40-21, PAR 5 ROUTED TO BACKSHOP FOR REPAIR. REPAIRED AND REINSTALLED DUMMY TRACK 2L ATSDR FDEA201012054581Skin · damagedAFT CARGO DOOR CUT OUT LOWER FWD EDGE IS DAMAGED APPROX 6 IN LONG AND 0.25 IN WIDE. REPAIRED AFT CARGO DOOR CUT OUT FWD EDGE SKIN IAW SRM 53-17-12, FIG 201, SHEET 1. USING DOUBLER REPAIR SCHEME. COMPLIED WITH EA 6-5310-145512.SDR FDEA201012054582Mount · gougedNR1 PYLON FWD ENGINE MOUNT FITTING CTR GUIDE PIN HOLE HAS A GOUGE ON INNER DIAMETER. (SPIGOT GUIDE HOLE). REMOVED NR1 PYLON FWD MOUNT FITTING IAW SRM 51-40-21, PG 7 AND SRM 54-51-81, FIG 1, PG 202. REPAIRED NR1 PYLON FWD MOUNT FITTING (SPIGOT GUIDE HOLE BY
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