GE CF6-80C2A5F

Service difficulty reports · 262

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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 = 'CF680C2A5F'
  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.

SDR FDEA202607030831Engine · damagedBURNED SMELL ON TAKEOFF. SUSPECT OIL LEAK IN HPC. EMERGENCY DECLARED. O2 USED. ENGINE R & R, COMPLETED RT ENG OPS CHECKS IN REF TO FEDEX WORKCARD 7100000-02-04. OK FOR SERVICE.Jul 3, 2026 · N168FE · Boeing 767300 · Engine Oil System (Airframe Furnished)SDR FDEA201708312443Line · chafedDURING PREFLIGHT, FOUND FLUID LEAKING OUT OF REAR OF THE NR 1 ENGINE. FOUND AN OIL SUPPLY LINE MOUNTING CLAMP BROKEN AND OIL LINE CHAFED THROUGH. REMOVED AND REPLACED THE AFFECTED ENGINE OIL LINE AND CLAMPS IAW AMM 70-00-00-02-0-F. RAN THE NR 1 ENGINE. ALAug 31, 2017 · N681FE · Airbus A300F4605R · Turbine Engine Oil SystemSDR FDEA201708082147Duct · separatedAPU BLEED PREASURE WAS 4 PSI ON ENGINE START. ACFT RETURNED TO GATE. COULD HEAR BLEED AIR LEAK ON THE NR 2 ENGINE COWL. GAINED ACCESS FOUND MAIN SUPPLY DUCT CLAMP TOP OF ENGINE BLOWN OFF , PIPE CONNECTION SEPORATED WITH SEVERAL WIRE BUNDLES NEAR IT MELTED.Aug 8, 2017 · N673FE · Airbus A300F4605R · Pneumatic Distribution SystemSDR FDEA201704111130Engine · failedFLYING FROM SJC TO IND AT LEVEL OFF THE OIL BUGS WERE SET AT 16QTS ON EACH GAGE TO MATCH THE CORRECT OIL QUANTITY READING. APPROXIMATELY 15-20 MINS LATER, NR 1 ENG OIL QUANTITY DECREASED TO 13 QTS, THEN 5-10MIN LATER WENT TO 12.5 QTS. FO WENT TO THE CABIN AREApr 11, 2017 · N651FE · Airbus A300F4605R · Engine (Turbine/Turboprop)SDR FDEA201703150881Eec · malfunctionedAT FL 200, THE NR 2 ENGINE ROLLED BACK SUDDENLY. WARNING LIGHTS BUT NO HORNS. STARTED A DESCENT, TURNED OFF AUTO THROTTLES AND SELECTED CONTINOUS RELIGHT AFTER CHECKING N1 AND N2. THE ENGINE RESPONDED, ELECTED TO LEAVE IT AT IDLE UNTIL THE THRUST REVERSMar 15, 2017 · N660FE · Airbus A300F4605R · Fuel Control/Turbine EnginesSDR FDEA201606041828Floor Panel · wornMAIN CABIN FLOOR PANEL 242FJ DAMAGED. FABRICATED AFT CARGO FLOOR PANEL 242FJ ON T16 1211786 IAW SRZ 25-005. CLASSIFIED AS A CAT A MAJOR REPAIR.Jun 4, 2016 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201512254078Hmu · malfunctionedAT TOP OF DESCENT, NR 1 ENG STARTED A SERIES OF 6 - 7 STALLS. FOLLOWED THE QRH & OPERATED AT IDLE. N1 STARTED TO DECREASE & EGT CLIMBED TO 622 AT SHUTDOWN. PARAMETERS AT SHUTDOWN N1 29.5, EGT 622, N2 66.6 WIND MILLING TIME WAS 10 MIN PERFORMED BORESCOPE INDec 25, 2015 · N652FE · Airbus A300F4605R · Fuel Control/Turbine EnginesSDR FDEA201506292123Thrust Reverser · damagedNUMBER 1 OTBD THRUST REVERSER AFT HINGE LUG DAMAGED EXHAUST SYS. THRUST REVERSER BLEND REPAIR OF HINGE BEAM REPAIRED IAW EA 6-7830-T0318435. THIS REPAIR IS CLASSIFIED AS A CATEGORY B MAJOR REPAIR.Jun 29, 2015 · N651FE · Airbus A300F4605R · Engine Thrust ReverserSDR FDEA201408072105Connector · unknownON TAKEOFF NR 2 THRUST REVERSER PRESSURIZED. FOUND LT DPV SOLENOID CONNECTOR NOT PROPERLY REMOVED IAW MEL 78-30-01-A. REMOVED CONNECTOR & CONTINUED ON WITH MX PROCEDURES TO END. OK TO CONTINUE ON MEL.Aug 7, 2014 · N674FE · Airbus A300F4605R · Engine Exhaust System WiringSDR FDEA201403210541Ecu · failedNR 1 ENGINE ROLLED BACK PASSING FL 315, N1 & N2 DECREASED IGNITION TURNED ON. ONE MINUTE LATER ENGINE REGAINED POWER. RETURNED & LANDED. NR 1 ENGINE FADEC FAULT LIGHT ILLUMINATED ON LANDING & APU AUTO SHUTDOWN. NO ECAM ALERTS ACCOMPANIED NR 1 ENGINE ROLLBMar 21, 2014 · N677FE · Airbus A300F4605R · Fuel Controlling SystemSDR FDEA201401160118Engine · leakingPRIOR TO DECENT, COURIERS NOTIFIED COCKPIT OF SMOKE IN CABIN. NO SMOKE DETECTORS OR ECAM WARNINGS IN COCKPIT OR ODOR OF SMOKE. RAN AIR CONDITIONING SMOKE CHECK LIST. DECLARED EMERGENCY LANDED. ON GROUND HAD ODOR IN COCKPIT. NR 1 ENGINE HAS DEBRIS IN SCRJan 16, 2014 · N667FE · Airbus A300F4605R · Engine (Turbine/Turboprop)SDR FDEA201311272884Engine · failedPDIS 664 79-310005832 27NOV13 IND OPEN U LOG PAGES 02343904. ENG ADVISORY FOR NR 2 ENG OIL QTY ZERO & FLUCTUATING OIL PRESS ON ECAM & ENG INSTRUMENTS. ADVISORY OCCURRED AT FL 370 EGT REMAINED NORMAL. OIL QTY & PRESS RETURNED TO NORMAL ON FINAL APPROACH. WNov 27, 2013 · N664FE · Airbus A300F4605R · Engine (Turbine/Turboprop)SDR FDEA201303210639Engine · inoperativePER FLIGHT CREW DEBRIEF, THE NR 1 ENGINE ON TAXI OUT HAD ECAM ENGINE FAILURE AND ASSOCIATED PARAMETERS WINDING DOWN. IAW CAPTAIN, AFTER BEING NOTIFIED BY MEM TOWER OF SMOKE FROM NR 1 ENG THEY PULLED FIRE HANDLE BUT DIDN'T DISCHARGE BOTTLE AND THEN DEPARTED ACMar 21, 2013 · N672FE · Airbus A300F4605R · Engine (Turbine/Turboprop)SDR FDEA201209223396Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL 242QJ CRUSHED AT CLEVIS ADAPTOR CUTOUT. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Sep 22, 2012 · N660FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209153331Link Assy · crackedMAIN DECK CARGO FRAME 48L BELOW SEAT TRACK 4L SUPPORT STRUCTURE ATTACHMENT LUG CRACKED ONE INCH LONG, STR 27-28. R & R DAMAGED LINK ASSY IAW SRM 51-40-21, PG 7, PARA 5.Sep 15, 2012 · N686FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201209113283Web · crackedMAIN DECK CARGO FLOOR WEB AT FR 79 RT OTBD OF FLOOR RAIL HAS .25" CRACK EXTENDING FROM LIGHTENING HOLE. R & R WEB IAW SRM 51-72-10, P1.Sep 11, 2012 · N686FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201209113287Floorboard · crackedMAIN DECK CARGO FLOORBOARD 242UJ CRACKED. FABRICATED FLOORBOARD IAW DWG SRZ 25-005, REV J.Sep 11, 2012 · N686FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209103275Floorboard · damagedFLOORBOARD 131NG CRACKED ON LOWER SURFACE. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Sep 10, 2012 · N686FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209073251Floorboard · damagedFLOORBOARD 151TF HAS TWO AREAS DAMAGED UPPER AND LOWER SKIN PLYS WITH CRUSHED CORE. THE LARGEST AREA IS 8" BY 3". FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Sep 7, 2012 · N686FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209073253Floorboard · gougedFLOORBOARD 252UH UPPER SURFACE GOUGED. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Sep 7, 2012 · N686FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209073254Floorboard · crackedMAIN DECK CARGO FLOORBOARD 251DF CRACKED, FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Sep 7, 2012 · N686FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201209073256Floorbeam · damagedFORWARD SIDE OF FLOORBEAM AT FR 17 Y1456 WEB IS DRILLED THROUGH AND HAS A RIVET IN THE HOLE THAT HAS NOT BEEN BUCKED. FABRICATED AND INSTALLED PICKUP FITTING IAW DWG A53611735 AND FSRM 51-40-21, PARA 7.Sep 7, 2012 · N663FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201209073255Skin · chafedLEFT WING OUTER FLAP INBD SIDE L/E CHAFED MARK APPROX LENGTH IS 1 INCH AND WIDTH IS 0.50 REF AMM 27-00-00-06, ZONE 580. REPAIRED WING OUTER FLAP IAW A300-600 FSRM 57-50-00 PARA 4.H. PG 231 THRU 233 AND FIG 208 AND EA 6-5750-160186 PT. 1.Sep 7, 2012 · N686FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201209063248Skin · damagedLEFT INBD FLAP LOWER SURFACE HAS 22 DENTS AND 12 GOUGES LOCATED FROM STGR 2.10 TO T/E AND RIB 3A TO RIB19A, COMPLIED WITH EA 6-5730160178.Sep 6, 2012 · N663FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201209063245Spring · brokenAVIONICS DOOR CAME OPEN IN FLIGHT (121BL). DOOR DID NOT OPEN BUT CREW GOT LIGHT IN COCKPIT. FOUND SPRING BROKEN. R & R THE DOOR HANDLE TENSION SPRINGS IAW MM 52-41-14-04. OPS TESTED GOOD. DOOR CLOSES SECURLY AND INDICATES ON ECAM.Sep 6, 2012 · N688FE · Airbus A300F4605R · Door Warning SystemSDR FDEA201209063247Floorbeam · crackedMAIN CARGO DECK FLOORBEAM AT FR 61 BETWEEN SEAT TRACK 4R AND 5R CRACKED ABOUT 0.125" ON THE AFT FACE EXTRUSION REF AMM 53-10-15-06-02, ZONE 250. BLENDED FLOORBEAM IAW SRM 53- 10-15- PG 14. CUT OUT CRACKED AREA OF FLOORBEAM IAW SRM 53-10-15 FIG 211 PG 386. Sep 6, 2012 · N686FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201209043220Skin · damagedLT ELEVATOR TIP LOWER SURFACE HAS A LIGHTNING STRIKE. REPAIRED IAW EA 6-5520-157869, AND RAS 70566303/003/2012, ISSUE A.Sep 4, 2012 · N663FE · Airbus A300F4605R · Elevator, Plate/SkinSDR FDEA201209043221Skin · damagedLT ELEVATOR TIP PANEL UPPER SURFACE HAS 2 EA LIGHTNING STRIKES. REPAIRED IAW EA 6-5520-157869 PART 1 AND RAS, ISSUE A.Sep 4, 2012 · N663FE · Airbus A300F4605R · Elevator, Plate/SkinSDR FDEA201209043218Floor Support · corrodedAFT HOLD FLOOR SUPPORT BETWEEN FR63 AND FR64 SECOND FROM LT SIDE FOUND CORRODED AT ANCHOR NUT LOCATIONS. AFT HOLD SUPPORT BEAM AT FR63 AND FR64 SECOND FROM LT SIDE, REPLACED IAW SRM 51-40-21.Sep 4, 2012 · N718FD · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201209043217Seat Track · corrodedCENTER MAIN DECK, FOUND RT 5TH SEAT TRACK CORROSION AREA FROM FR45 TO 54 AT -Y1959 POSITION. FABRICATE AND R & R THE SEAT TRACK IAW DWG NR A53813618 AND AB6F SRM 51-40-21. REINSTALLED THE CROSSBEAMS OF FR45-FR54 -Y1959 WITH CHECK OK FOR SERVICE IAW AMM 20-21Sep 4, 2012 · N661FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201209043215Floorbeam · crackedFWD CARGO COMPT CEILING AREA OF M/D FLOORBEAM RT SIDE EDGE AREA GOT CRACK AT FR29 POSITION. REPAIRED IAW EA 6-5310-149065 WITH AB6F SRM 53-10-15. THE REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Sep 4, 2012 · N661FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201208273183Floor Support · corrodedMAIN DECK CARGO FRAME 11A THRU 13A, Y1456 HAS SURFACE CORROSION ON TOP AND BOTTOM AROUND THE MOUNTING SCREWS ON TEE PROFILE. AFTER REMOVAL OF LEVEL 1 CORROSION FOUND CORROSION BEYOND ECONOMICAL REPAIR, R & R IAW SRM 51-72 10, PG 1-3 AND DWG A536-12519.Aug 27, 2012 · N663FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA2012082631710Floor Panel · damagedCENTER MAIN DECK FLOOR PANEL 242EJ HAS INSERT DAMAGE.Aug 26, 2012 · N661FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201208263177Cargo Track · corrodedMAIN DECK CARGO TRACK L4 BETWEEN FR 46 & 47 HAS 2EA AREAS OF CORROSION APPROXIMATELY 8" LONG. REPAIRED SEAT TRACK IAW SRM 53-10-16, FIG 205.Aug 26, 2012 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201208263172Floor Panel · damagedFWD CARGO FLOOR PANEL 131QG EDGE AREA HAS IMPACT DAMAGE. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Aug 26, 2012 · N661FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201208263168Cover · crackedLT WING T/E FOUND 1EA COVER CRACKED POSITION NEAR LT MAIN LT MLG AFT TRUNNION INBD SIDE. REMOVED COVER FOR FABRICATION IAW DWG A57240775 THEN REPLACED IAW SRM 51-72-10 & 51-40-21. INSTALLED COVER AND CONDITION CHECKED GOOD. REPAIR CLASSIFIED AS MINOR PER GMAug 26, 2012 · N661FE · Airbus A300F4605R · Wing Miscellaneous StructureSDR FDEA201208253164Seat Track · corrodedMAIN DECK CARGO BETWEEN FR 53 AND 54 SEAT TRACK 3R HAS CORROSION APPROX 2" IN THE CENTER OF THE TRACKS IN BET SCALLOPS. AFTER REMOVAL OF LEVEL 1 CORROSION, AREA FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, FIG 102. REMOVED SEAT TRACK 3R BET. FR50 AND 54 IAW SRAug 25, 2012 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201208243154Skin · gougedLT WING NR 2 SLAT LWR SURFACE GOUGED 1 SQUARE INCH, LOCATED 3 INCHES FROM INBD EDGE AND 6 INCHES FWD OF T/E SMOOTHED AND BLENDED GOUGE IAW FSRM 51-73-10 MATERIAL LOSS IS .007, BEFORE .047 AFTER .040 FOUND TO OUT OF LIMITS IAW SRM 57-40-00 PARA 4B, PG 104. Aug 24, 2012 · N663FE · Airbus A300F4605R · Leading Edge DevicesSDR FDEA201208243155Floorboard · damagedFWD CARGO BAY FLOORBOARD 131RG BROKEN AT 2 CORNERS AND CRUSHED BY TOOL ON THE EDGE. FABRICATED REPLACEMENT FLOORBOARD IAW DWGSRZ 25-005 REV J.Aug 24, 2012 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201208243157Adapter · damagedMAIN DECK CARGO FLOOR CLEVIS ADAPTER AT FR38.1 BTWN SEAT TRACKS 2R AND 3R HAS BROKEN SCALLOPS, .5 AREA R & R CLEVIS ADAPTER AT FR 38.1 BETWEEN SEAT TRACKS 2R AND 3R IAW SRM 51-72-10.Aug 24, 2012 · N663FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201208243160Adapter · crackedMAIN DECK CARGO ZONE 250, CLS ADAPTER HAS A 8.5 INCH LONG CRACK IN UPPER RADIUS AT FR61 BTWN SEAT TRACKS 4R(-Y1456) AND 5R (-Y1959). R & R CLEVIS ADAPTER AT FR 61 BETWEEN SEAT TRACKS 4R & 5R IAW FRSM 51-72-10.Aug 24, 2012 · N663FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201208243161Adapter · crackedMAIN DECK CARGO ZONE 250, CLEVIS ADAPTER HAS A 9.5" LONG CRACK IN UPPER RADIUS AT FR62 BETWEEN SEAT TRACKS 4R(-Y1456) AND 5R (-Y1959). R & R CLEVIS ADAPTER AT FR 62 BETWEEN SEAT TRACKS 4R & 5R IAW FRSM 51-72-10.Aug 24, 2012 · N663FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201208243158Web · damagedFR11 TO FR12 WEB DAMAGED. REMOVED DAMAGED WEB IAW SRM 51-40-21 PARA 6. FABRICATED NEW WEB IAW DWG A53612536. INSTALLED NEW WEB AT FR 12A TO FR 14 STA Y953 IAW SRM 51-40-21 PARA 7. REPROTECTED ALL PARTS IAW SRM 51-21-10 AND 51-75-10.Aug 24, 2012 · N663FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201208243159Floor Support · corrodedMAIN DECK CARGO SURFACE CORROSION ON TOP AND BOTTOM AROUND MOUNTING SCREWS ON FLOOR SUPPORT. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-40-21 PARA 7.Aug 24, 2012 · N663FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201208233140Seat Track · corrodedSEAT TRACK L4 BETWEEN FR 42 AND 44 HAS 2 AREAS OF CORROSION APPROX 8 INCHES LONG, REF AMM 53-10-16-6 CORROSION AT TRACK 4L FR 42 TO 44 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, FIG 102. REMOVED 4L TRACK FR 40 TO 44.5 REDUCTION SPLICE IAW SRM 51-40-21, PARA Aug 23, 2012 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201208233145Adapter · corrodedFLOOR CLEVIS ADAPTER UPPER SURFACE CORRODED 10 SQUARE INCHES LOCATED FR 25 BTWN 2R & 3R SEAT TRACKS AFTER REMOVAL OF LEVEL 1 CORROSION IAW FRSM 51-74-10, PARA 5 FOUND NO LIMITS FOR CLEVIS ADAPTER AT FR25. R & R CLEVIS ADAPTER IAW SRM 51-40-21, PARA 6-7. REPAug 23, 2012 · N663FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201208223112Seat Track · corrodedSEAT TRACK 5R AT FR58 HAS 1 SQUARE INCH OF CORROSION ON INBD FLANGE AROUND NUT PLATE HOLE. AFTER REMOVAL OF LEVEL 1 CORROSION SEAT TRACK 5R WAS FOUND TO BE OUT OF LIMITS IAW SRM 51-74-10 AND 53-10-16 FIG 102. R & R SEAT TRACK 5R AT FR 57.3 TO FR 58 IAW SRM 5Aug 22, 2012 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201208223108Floor Panel · dentedCARGO BAY 162EF FLOOR PANEL UPPER SURFACE HAS SEVERAL SMALL DENTS. FABRICATED A NEW FLOOR PANEL IAW SRM 53-10-20 & DWG A53279966. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Aug 22, 2012 · N661FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201208223109Floor Panel · debondedCARGO BAY 161AF FLOOR PANEL EDGE AREA DEBONDED. FABRICATED NEW FLOOR PANEL IAW SRM 53-10-20 & DWG A53279966. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Aug 22, 2012 · N661FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201208223110Floor Panel · damagedCARGO BAY 162DF FLOOR PANEL EDGE AREA HAS IMPACT DAMAGE. FABRICATED NEW FLOOR PANEL IAW SRM 53-10-20. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Aug 22, 2012 · N661FE · Airbus A300F4605R · Fuselage Floor Panel
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