GE CF6-80C2A5F

Service difficulty reports · 263

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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 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 PanelSDR FDEA201208223111Floor Panel · debondedCARGO BAY 16HF FLOOR PANEL EDGE AREA DEBONDED. FABRICATED NEW FLOOR PANEL IAW SRM 53-10-20 & DWG A53279961. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Aug 22, 2012 · N661FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201208223107Floor Panel · corrodedCARGO BAY 162HF FLOOR PANEL INNER SURFACE CORRODED. REMOVED FLOOR PANEL IAW AMM 53-10-35-04. FABRICATE A NEW FLOOR PANEL IAW SRM 53-10-20 & DWR.A53279962. INSTALLED FLOOR PANEL IAW AMM 53-10-35-04. PER GMM 6-2-100 REPAIR CLASSIFIED AS MAJOR.Aug 22, 2012 · N661FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201208213088Cargo Track · corrodedMAIN DECK CARGO SEAT TRACK 1 HAS 2 AREAS 1 SQ" CORROSION: 1) AT FR44 12" AND 1) AT FR46 10" IN THROUGH (CENTER) AND ON SCALLOPS (UPPER CENTER).Aug 21, 2012 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201208203085Link · crackedMAIN DECK CARGO LOWER SUPPORT LEG AT FR49 SEAT TRACK L4 FITTING CRACKED. R & R LINK IAW SRM 51-40-21, PAR 5, PAGE 7.Aug 20, 2012 · N663FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201208203087Frame · gougedMAIN DECK CARGO LT SIDEWALL FR 73 GOUGES BETWEEN STGR 12 AND STGR 22 LT AT 12 PLACES. BLENDED GOUGES IAW SRM 51-73-10, PG 209. REPAIRED AREA 1 BY CUTTING OUT FRAME DAMAGE & INSTALLING REPAIR IAW SRM 53-10-13 F 202. SMOOTHED AREAS 2 THRU 12 IAW FSRM 51-73-10Aug 20, 2012 · N658FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201208203083Cargo Track · corrodedMAIN DECK CARGO TRACK 1 AT FR54 HAS ONE SQUARE INCH OF CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16 FIG 102. REMOVED AND REPLACED SEAT TRACK AT FR52 12" TO FR54 IAW SRM 53-10-16 PGS 227-232.Aug 20, 2012 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201208203084Cargo Track · corrodedMAIN DECK CARGO TRACK 2R AT FR47 12 INCHES AREA OF COROSSION. FOUND TO BE OUT OF LIMITS IAW A300-600 SRM 53-10-16 FIG 102. REMOVED AND REPLACED SEATTRACK 2R BETWEEN FR 44 TO 48 IAW SRM 53-10-16 PG. 231/232 FIG. 205 AND SRM 51-40-21 PG. 19 FIG. 5 AND PG 26Aug 20, 2012 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201208193078Floor Support · corrodedMAIN DECK CARGO FLOOR SUPPORT TEE CAP UNDER LAVATORY COMPOSITE DRAIN HAS CORROSION AROUND THE SCREW HOLE, APPROX 1 INCH. REMOVED CORRODED FLOOR SUPPORT IAW SRM 51-40-21 PAR 6 & 7. FABRICATED NEW FLOOR SUPPORT IAW DRAWING A53612213. INSTALLED FLOOR SUPPORT IAAug 19, 2012 · N663FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201208193075Cargo Track · corrodedMAIN DECK CARGO TRACK HAS TWO AREAS CORROSION AT FRAME 41. FOUND TO BE OUT OF LIMITS IAW SRM 51-74-10 PGS 205-206. REMOVED SEAT TRACK, FABRICATED NEW TRACK IAW SRM DWG A53820202. INSTALLED IAW SRM 51-72-10.Aug 19, 2012 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201208193076Cargo Track · corrodedMAIN DECK CARGO TRACK 5L HAS 12 INCHES OF CORROSION BETWEEN FR 41 AND FR 43. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16 FIG 102. REMOVED AND REPLACED CARGO TRACK. FABRICATED NEW CARGO TRACK IAW DWG A53820202 AND INSTALLED IAW SRM 51-72-10.Aug 19, 2012 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201208173057Floorboard · damagedAFT CARGO BAY FLOORBOARD 152UF CUTOUT EDGE HAS IMPACT DAMAGE & LOWER SURFACE HAS PUNCTURED (3 SQ IN) FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Aug 17, 2012 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201208173058Floorboard · damagedAFT CARGO BAY FLOORBOARD 152PF HAS A 25 SQUARE INCH BROKEN SECTION. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Aug 17, 2012 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201208173060Floorboard · damagedAFT CARGO BAY FLOORBOARD 152QF BROKEN IN HALF. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Aug 17, 2012 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201208173059Floor Panel · gougedAFT CARGO BAY FLOOR PANEL 152TF GOUGED 80 SQUARE INCHES. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Aug 17, 2012 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201208163024Web · crackedMAIN DECK CARGO LT SIDE FR 79 FLOOR LEVEL WEB CRACKED 4" IN LENGTH. R & R WEB AT FR 79 LT SIDE AT STR 27L IAW FSM 51-72-10.Aug 16, 2012 · N663FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201208163025Web · crackedMAIN DECK CARGO RT WEB BETWEEN FR 79 AND 80, STR 26 HAS A .50" CRACK. R & R WEB IAW SRM 51-72-10.Aug 16, 2012 · N663FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201208163027Floorboard · crackedMAIN DECK CARGO FLOORBOARD 242UJ HAS 5 AREAS OF CRACKS AT CLEVIS ADAPTER CUTOUT, CRACKRANGE FROM 1" TO 5" LONG. FABRICATED FLOORBOARD IAW DWG SRZ 25-005, REV J.Aug 16, 2012 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201208163028Floorboard · damagedAFT CARGO BAY FLOORBOARD 152XF GOUGED 50 SQ IN ON BOTTOM. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Aug 16, 2012 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201208163029Floorboard · damagedAFT CARGO BAY FLOORBOARD 152VF HAS 3 SQ IN BROKEN SECTION. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Aug 16, 2012 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201208163030Floorboard · damagedAFT CARGO PIT FLOORBOARD 152RF GOUGED 100 SQ IN AND 10 INSERTS BROKEN. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Aug 16, 2012 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201208163035Floorboard · damagedFWD CARGO BAY FLOORBOARD 132QG HAS 8 SQUARE INCHES OF DELAMINATION ON ONE CORNER , AND HAS 20 PUNTURES DOWN ONE SIDE ON LOWER SURFACE, ( .7500" X .7500" MEASUREMENTS). FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Aug 16, 2012 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201208163036Floorboard · damagedAFT CARGO BAY FLOORBOARD 151QF CORNER EDGE HAS IMPACT DAMAGE. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Aug 16, 2012 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201208163037Floorboard · delaminatedFWD CARGO BAY FLOORBOARD 132SG HAS 8 FEET OF DELAMINATION AROUND EDGES ON LOWER SURFACE. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Aug 16, 2012 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201208163038Floorboard · crackedMAIN DECK CARGO FLOORBOARD 242ZJ HAS 10 LOCATIONS AT EDGES OF CLEVIS ADAPTER CUTOUTS WITH CRACKS 1- 3 INCHES. FABRICATED FLOORBOARD IAW DWG NR SRZ 25-005, REV J.Aug 16, 2012 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201208163039Floorboard · crackedMAIN DECK CARGO FLOORBOARD 242ZJ HAS 10 LOCATIONS AT EDGES OF CLEVIS ADAPTER CUTOUTS WITH CRACKS 1- 3 INCHES. FABRICATED FLOORBOARD IAW DWG NR SRZ 25-005, REV J.Aug 16, 2012 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201208153016Floorboard · damagedFWD CARGO BAY FLOORBOARD 132KG CRUSHED AT THE FWD AND AFT EDGES (ABOUT 4 FT. LONG). FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Aug 15, 2012 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201208142995Floor Panel · crackedFLOOR PANEL 232G HAS TWO 9 INCH CRACKS, FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Aug 14, 2012 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201208142996Floor Panel · damagedFLOOR PANEL 251WG BROKEN IN HALF. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Aug 14, 2012 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201208142997Floorboard · damagedFLOORBOARD 241DF HAS FOUR AREAS 1INCH X 5 INCHES CRUSHED FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Aug 14, 2012 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201208142998Floorboard · delaminatedMAIN DECK CARGO FLOORBOARD 242SF, DELAMIATED ALL AROUND THE CLEVIS ADAPTERS MOUNTING AREA. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Aug 14, 2012 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201208142999Floorboard · damagedMAIN DECK CARGO, FLOORBOARD 251XH BROKEN IN HALF. FABRICATED FLOORBOARD IAW DWG SRZ 25-005, REV J.Aug 14, 2012 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201208143000Floorboard · damagedMAIN DECK CARGO FLOORBOARD 231TG HAS 10 INCHES OF CRUSHED HONEYCOMB NEAR CLEVIS CUTOUT, TWO MISSING INSERTS, AND FOUR PUNCTURES IN UPPER SURFACE. (LARGEST .2500" DIA) FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Aug 14, 2012 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201208143001Floorboard · damagedMAIN DECK CARGO FLOORBOARD 231VG IS CRUSHED AT CLEVIS ADAPTER CUTOUT ABOUT 6 X 0.25 INCHES, AT FWD AFT EDGES ABOUT 6 SQUARE INCHES. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Aug 14, 2012 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201208142975Frame · crackedONE CRACK (2MM) WAS FOUND AT FRAME 44 RT HOLE "B" AREA INBD DIRECTION. REPAIRED IAW EO E6-5310-7-5006.Aug 14, 2012 · N661FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201208132970Floor Panel · crackedFLOOR PANEL 242QJ HAS TWO 10 INCH CRACKS. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Aug 13, 2012 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201208132971Floor Panel · crackedFLOOR PANEL 242GF HAS ONE 12 INCH CRACK. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Aug 13, 2012 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201208132972Floor Panel · crackedFLOOR PANEL 242EK HAS TWO 10 INCH CRACKS. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Aug 13, 2012 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201208132973Floor Panel · crackedFLOOR PANEL 242RG HAS TWO 9 INCH CRACKS. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Aug 13, 2012 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201208112946Floorboard · crackedFLOORBOARD 252UH HAS TWO 9.5 INCH CRACKS. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Aug 11, 2012 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201208112947Floor Panel · crackedFLOOR PANEL 232YG HAS A 9 INCH CRACK & TWO 4 INCH CRACKS. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Aug 11, 2012 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201208112948Floor Panel · crackedFLOOR PANEL 242VG HAS ONE 9.5 INCH CRACK. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Aug 11, 2012 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201208112949Floor Panel · crackedFLOOR PANEL 252VF HAS TWO 9.5 INCH CRACKS. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Aug 11, 2012 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201208112953Pressure Switch · failedNR 1 ENGINE OIL FILTER CLOG ECAM & WARNING LIGHT CAME ON DURING TAKEOFF ROLL. STANDARD POWER HAD BEEN SET & ACFT WAS AT APPROX 100 KTS. REJECTED & COMPLIED WITH CHECK LIST. R & R NR 1 ENGINE OIL FILTER DIFFERENTIAL SWITCH IAW AMM 79-35-11-04. IDLE RUN, LAug 11, 2012 · N690FE · Airbus A300F4605R · Engine Oil Indicating SystemSDR FDEA201208102938Plug · leakingYELLOW HYD SYSTEM FAILED IN FLT. HYD QTY LOW. FOUND TWO PLUGS ON ACTUATOR BODY LEAKING AND NOT SAFETIED. TORQUED BOTH PLUGS REF. AMM 20-21-12-00 AND SAFETIED. SERVICED YELLOW SYSTEM REF. AMM 12-12-29-00. PRESSURIZED ALL THREE SYSTEMS WITH ELECTRIC PUMPS Aug 10, 2012 · N676FE · Airbus A300F4605R · Hydraulic System, MainSDR FDEA201208092909Seat Track · corrodedSEAT TRACK 3R CORROSION ON THE FLANGE AND THE SCALLOP BETWEEN FR 45 AND FR 50. AFFECTED AREA ABOUT 20 SQUARE INCHES. AFTER REMOVAL OF CORROSION, SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. R & R SEAT TRACK IAW SRM 51-40-21 AND 51-72-10.Aug 9, 2012 · N658FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201208092926Adapter · corrodedMAIN DECK CARGO AT FR74, CLEVIS ADAPTER BETWEEN SEAT TRACKS 4L & 5L AFT FLANGE 4EA FASTENER HOLES, UPPER AND LOWER SURFACE CORRODED, 2 SQ IN, REF AMM 53-10-16-6. REMOVED LEVEL 1 ON CLEVIS ADAPTER FLANGE AT FR 74 BETWEEN SEAT TRACKS 4L & 5L IAW FRSM 51-74-10 PAug 9, 2012 · N658FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201208082896Floorboard · damagedFOUND FLOORBOARD 241XG BROKE IN CENTER OF PANEL. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Aug 8, 2012 · N658FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201208072868Cargo Track · gougedMAIN DECK CARGO TRACK 5L HAS ONE SCREW HOLE GOUGED AT FR 52 RT FLANGE. SMOOTHED AND BLENDED GOUGE IAW SRM 51-74-10. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. REMOVED CARGO TRACK IAW SRM 51-40-21. FABRICATED CARGO TRACK IAW SRM 51-40-44. INSTALLED CARGO TAug 7, 2012 · N658FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201208062863Thrust Plate · corrodedTHRUST PLATE AT STRINGER 26, FR 30-31 HAS TWO AREAS OF CORROSION BETWEEN SEAT TRACK 5-6 LT. DEFECT MEASURES 2.5 SQ". AFTER REMOVAL OF CORROSION, THRUST PLATE WAS FOUND TO BE OUT OF TOLERANCE IAW DWG A53781984 AND SRM 51-73-11, PG 1. R & R THRUST PLATE IAW Aug 6, 2012 · N658FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
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