GE CF6-80C2A5F

Service difficulty reports · 263

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 = '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 FDEA201004061064Floor Panel · damagedMAIN CABIN FLOOR PANEL 242 RJ IS DAMAGED. FABRICATED NEW FLOOR PANEL 242 RJ IAW DWG SRZ 25-005, REV "H".Apr 6, 2010 · N658FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201004061070Floor Panel · damagedMAIN CABIN FLOOR PANEL 232 TG IS DAMAGED. FABRICATED NEW FLOOR PANEL 232 TG IAW DWG SRZ 25-005, REV "H".Apr 6, 2010 · N658FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201004051053Support Bracket · crackedAFT MAIN CABIN SUPPORT BRACKET IS CRACKED AT STRINGER 25 LT; FRAME 79 TO FRAME 80. REMOVED CRACKED SUPPORT BRACKET IAW SRM 51-72-10. LOCATED AND DRILLED HOLES IN NEW BRACKET PN A539111320051, PO 631621.2 IAW SRM 51-72-10. INSTALLED SUPPORT BRACKET IAW SRMApr 5, 2010 · N658FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201004051054Seat Track · corrodedCORROSION ON SEAT TRACK FWD END AT FRAME 14; RBL 16.Apr 5, 2010 · N658FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201004051055Seat Track · corrodedSEAT TRACK FLANGE HAS SOME FLAKED PAINT AND CORROSION AT FRAME 51; RBL 16. CLEANED AREA TO EVALUATE IAW AMM 51-23-10-00. NO CORROSION FOUND.Apr 5, 2010 · N658FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201003301028Support Bracket · crackedFWD CARGO COMPARTMENT AFT BAY HAS A CRACKED SUPPORT BRACKET AT FRAME 38.2, LT SIDE ON AFT SIDE OF THE BULKHEAD WALL UPPER MOUNT TRIM. REMOVED CRACKED BRACKET IAW SRM 51-72-10, PARA A, PG 2. FABRICATED NEW BRACKET IAW DWG A25370669. ALODINED BRACKET IAW SRMar 30, 2010 · N658FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201003301029Support Bracket · crackedFWD CARGO COMPARTMENT AFT BAY HAS A CRACKED SUPPORT BRACKET AT FRAME 38.2, LT SIDE ON AFT SIDE OF THE BULKHEAD WALL UPPER MOUNT TRIM, 36 IN. TO THE LT OF THE CTR POST. REMOVED CRACKED BRACKET IAW A300-600 SRM 51-72-10, PARA A, PG 2. FABRICATED NEW BRACKET IAMar 30, 2010 · N658FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201003281022Skin · bentFWD CARGO DOOR EXTERIOR SKIN AT FWD CORNER HAS 3" AREA OF SKIN BENT INTO WIND DAMAGE CLASSIFIED OUT OF LIMITS IAW SRM 52-30-00. REPAIRED DOOR SKINS IAW SRM 52-31-00, FIG 203 BY INSTALLING DOUBLER AND FILLER TO TOP SKIN.Mar 28, 2010 · N684FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA201003261015Skin · crackedCRACK IN THE RT WING LOWER SKIN INBD OF RIB 9 (FASTENER THROUGH JOGGLE SECTION) SHOWN ON FIG 3. (VERIFIED WITH EDDY CURRENT) COMPLIED WITH EA 6-5710-139432 "WINGS - AD 2008-06-17- RT WING LWR SKIN PANEL INBD OF RIB 9".Mar 26, 2010 · N658FE · Airbus A300F4605R · Wing, Plate/SkinSDR FDEA201003190936Anti-Ice Valve · malfunctionedNR 2 ENG ECAM ENG 2 N, AC VALVE NOT OPEN ENG NR 2 ANTI ICE INOP MEL 19MAR10 23:05 MEM U RELEASED FOR SERVICE IAW MEL: 30-21-01-B CATEGORY: C EXPIRATION: 29MAR10 "MEL 30-21-01-B: ENGINE (IDENTIFY 1 AND/OR 2) NR 2 ANTI-ICE VALVE- INOP. ENGINE NACELLE VALVMar 19, 2010 · N659FE · Airbus A300F4605R · Engine Anti-Icing SystemSDR FDEA200808293645Ecu · failedDURING CLIMB NR 2 ENG N1, FF, EGT BECAME UNSTABLE, ASSOCIATED WITH ENGINE SURGING. FADEC GRD TEST, FOUND FAULT CODE 352-21 ON CH A. N1 SPEED SENSOR PERFORMED TSM PROCEDURE 73-21-30 352-21 FIG 102 SHEET 28. CHECKED BOTH CH A AND B SYS GOOD. SPEED SENSOR IS Aug 29, 2008 · N681FE · Airbus A300F4605R · Fuel Controlling SystemSDR FDEA200804151417Crossbeam · crackedCROSSBEAM AT FR 60 HAS 1 IN CRACK ON VERTICLE FLANGE, OTBD OF SEAT TRACK 3 RT, - Y1456, ON AFT FACE REMOVED CRACK AND ACCOMPLISHED FLOORBEAM REPAIR IAW SRM 53-10-15, FIG 211.Apr 15, 2008 · N658FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA200804151418Floorbeam · crackedFLOORBEAM AT FR 60 HAS 1 IN CRACK ON VERTICLE FLANGE, OTBD OF SEAT TRACK 3 RT, - Y1456, ON AFT FACE, REMOVED CRACK AND ACCOMPLISHED FLOORBEAM REPAIR IAW SRM 53-10-15, FIG 211.Apr 15, 2008 · N658FE · Airbus A300F4605R · Fuselage Main, Floor Beam
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