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.
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
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 FDEA201207262702Floor Panel · crackedMAIN CARGO DECK FLOOR PANEL NR 251 JF IS CRACKED IN HALF AT A44 CLEVIS AREA, FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.SDR FDEA201207262703Floorboard · damagedFLOORBOARD 252VF CRUSHED AT THE EDGE AND AROUND THE CLEVIS ADAPTOR CUT OUT. FABRICATED REPLACEMENT FLOORBOARD DWG SRZ 25-005, REV J.SDR FDEA201207262704Floorboard · crackedFLOORBOARD IDENTIFIED AS 232RG IS CRACKED DOWN THE WIDTH CENTER. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.SDR FDEA201207262705Floorboard · damagedFLOORBOARD 242EK, HAS IMPACT AT CLEVIS ADAPTOR CUT-OUT DEFECT MEASURES 10 INCHES LONG, UPPER SURFACE. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.SDR FDEA201207262706Floorboard · damagedFLOORBOARD 242ZJ, THREE AREAS AROUND THE CLEVIS OUTER PLY CRUSHED AND THREE BAD INSERTS. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-00, REV J.SDR FDEA201207262707Floorboard · damagedFLOORBOARD 252YG CRUSHED AT UPPER SURFACE AROUND CLEVIS ADAPTER CUTOUT. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.SDR FDEA201207262708Floorboard · damagedFLOORDBOARD 251BH, IMPACT DAMAGE 6" AT SURF AROUND CLEVIS CUT OUT. FABRICATED REPLACEMENT FLOORDBOARD IAW DWG SRZ 25-005, REV J.SDR FDEA201207252671Floorboard · crackedFLOORBOARD 232HG HAS IMPACT DAMAGED AND CRACK (5") AT AFT OTBD CORNER. FABRICATED FLOORBOARD IAW DWG SRZ25-005, REV J.SDR FDEA201207252672Floorboard · damagedFLOORBOARD 232JG HAS AREA OF IMPACT DAMAGE, 9", ON INBD SIDE, AND EDGE FILLER MISSING ALONG ENTIRE AFT EDGE. FABRICATED FLOORBOARD IAW DWG SRZ 25-005 REV J.SDR FDEA201207252673Floorboard · crackedFLOORBOARD 232YG HAS PUNCTURE AND CRACK ON FORWARD EDGE (5"), AND PUNCTURE AND CRACKED 8 INCHES AROUND CLEVIS ADAPTER CUTOUT. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-055, REV J.SDR FDEA201207252674Floorboard · damagedFLOORBOARD 252UH OUTER PLY AFT OF CUTOUT CRUSHED APPROX 6 INCHES. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.SDR FDEA201207252675Floorboard · damagedFWD CARGO BAY FLOORBOARD 131NG HAS PUNCTURED, CRACKED & EDGE DISBONDED. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.SDR FDEA201207252676Floorboard · damagedFLOORBOARD 131SG HAS 1 X 9 INCH PIECE TORN OFF & 6 INCHES OF DELAMINATED. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.SDR FDEA201207252677Floorboard · damagedFLOORBOARD 131QF HAS 45 INCHES OF EDGE DAMAGE. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.SDR FDEA201207252680Clevis · damagedCLEVIS ADAPTER AT FR61 BETWEEN SEAT TRACK 2R AND 3R SCALLOP IS BROKEN. R & R CLEVIS ADAPTER BETWEEN SEAT TRACK 2R AND 3R AT FR61 IAW SRM 51-72-10, PAGE 1-2.SDR FDEA201207252667Seat Track · corrodedNR 1 SEAT TRACK FROM FR71.4 TO FR73 HAS COROSSION AND GOUGE ON CROWN. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16 PG 105 FIG 102 , CUT AND REMOVED DAMAGED SECTION, SPLICE REPAIRED SEAT TRACK IAW SRM 53-10-16 PG 203 - 208 FIG 201.SDR FDEA201207252668Floorbeam · corrodedFWD CARGO COMPT AT FR34, FLOORBEAM LOWER SURFACE HAS CORROSION. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 51-24-10 PG 205. REMOVED DAMAGED SECTION FLOORBEAM, FABRICATED REPAIR ANGLES AND INSTALLED IAW WITH EA 6-5310-160164 AND DWG A53781959 AND SRM SDR FDEA201207242662Adapter · wornM/D FLOOR STRUCTURE OF ADAPTER CROWN BROKEN AT FR 31/ Y 1456, Y1959 POSITION REPLACED WITH NEW ADAPTER I.A.W. AB6F SRM 51-72-10. THE REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201207242660Adapter · wornM/D FLOOR STRUCTURE OF ADAPTER CROWN BROKEN AT FR32 / Y1456 , Y 1959 POSITION. REPLACED WITH NEW ADAPTER IAW AB6F SRM 51-72-10. THE REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.SDR FDEA201207222639Skin · dentedRT WING AILERON UPPER SURFACE T/E HAS 35 DENT FROM INBD EDGE TO OTBD EDGE LARGEST IS .5" L X .5" W X .011"D DENTS FOUND OUT OF LIMITS DUE TO DENTS BETWEEN REAR SPAR AND T/E AILERON IAW SRM 57-61-11, PG 108, PARA 6. R & R RT ASA IAW AMM 27-11-28-04. OPS CHECKESDR FDEA201207222641Floorboard · crackedMAIN DECK CARGO FLOORBOARD 251QH HAS AN 8 INCH CRACK AROUND CLEVIS CUT OUT. FABRICATED FLOORBOARD IAW DWG SRZ 25-005.SDR FDEA201207212632Sense Line · chafedCLIMBING OUT OF 260 TOWARD 330 RECEIVED A FIRE WARNING FOR NR 2 ENGINE ON ECAM. COMPLIED WITH PHASE 1. STILL HAD RED LIGHT. FIRED 1 BOTTLE (AGENT 1). LIGHT WENT OUT. LANDED WITHOUT MISHAP. MX FOUND HP SENSE LINE HAD BEEN RUBBING ON UPPER LOOP RAIL AND WORN HSDR FDEA201207172597Seat Track · corrodedMAIN DECK CARGO AT FR 69 AND FR 70 SEAT TRACK 1 HAS CORROSION ON TOP OF SEAT TRACK SCALLOPS, REMOVED TWO AREAS OF LEVEL 1 CORROSION IAW SRM 53-10-16, FIG 201.SDR FDEA201207162581Cargo Track · corrodedMAIN DECK CARGO AT FR73 TO FR77 SEAT TRACK 1 HAS CORROSION ON THE INSIDE OF SEAT TRACK AND ON TOP OF SCALLOPS; 3 EA AREAS. AFTER REMOVAL OF LEVEL 1 CORROSION SEAT-TRACK 1 AT FR73 TO FR77 WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. CUT AND REMOVED SEAT SDR FDEA201207162589Floorboard · delaminatedFLOORBOARD 132LG HAS 32 SQUARE INCHES OF DELAMINATION & FIVE, ONE INCH PUNCTURES. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 055, REV J.SDR FDEA201207162588Frame Splice · damagedEO E6-5310-7-5017B, PT2 FUSELAGE FRAME 47 SPLICE FITTING BETWEEN STR 24 AND 26 LT/RT FOUND INITIAL HOLE "N" IS OVERSIZED. REPAIRED IAW EA 6-5315-157934SDR FDEA201207132565Floor Panel · damagedFLOOR PANEL 152XF BROKEN IN TWO PLACES, AT EDGE. FABRICATED FLOOR PANEL IAW DWG SRZ25-005, REV J.SDR FDEA201207132567Floor Panel · damagedFLOOR PANEL 152VF BROKEN AT EDGES UPPER AND LOWER SURFACES. FABRICATED FLOOR PANEL IAW DWG SRZ25-005 REV J.SDR FDEA201207132568Floor Panel · damagedFLOOR PANEL 152UF HAS 60 INCHES OF EDGE DAMAGE. FABRICATED FLOOR PANEL IAW DWG SRZ25-005, REV J.SDR FDEA201207132570Floor Panel · damagedFLOOR PANEL 242LK BROKEN. FABRICATED FLOOR PANEL IAW DWG SRZ25-005 REV. JSDR FDEA201207132571Floor Panel · damagedFLOOR PANEL 152MF BROKEN AT EDGES IN 3 PLACES. FABRICATED FLOOR PANEL IAW DWG SRZ25-005 REV J.SDR FDEA201207132572Floor Panel · damagedFLOOR PANEL 151PF BROKEN AT THE EDGE AND LOWER SURFACE. FABRICATED FLOOR PANEL IAW DWG SRZ25-005, REV J.SDR FDEA201207132566Floor Panel · crackedFLOOR PANEL 132RF HAS 3 AREAS OF EDGE DAMAGE, A PUNCTURE, AND A 9 INCH CRACK, A 5 INCH CRACK AND A 3 INCH CRACK. FABRICATED FLOOR PANEL IAW DWG SRZ25-005, REV J.SDR FDEA201207132569Floor Panel · crackedFLOOR PANEL 251BH HAS TWO, SIX INCH CRACKS AROUND CLEVIS ADAPTORS, FABRICATED FLOOR PANEL IAW DWG SRZ25-005, REV J.SDR FDEA201202150586Manifold · leakingDURING PREFLIGHT, OIL QUANTITY 18 QUARTS. AT LEVEL FLIGHT OIL QUANTITY NR 2 WAS 13 QUARTS. OIL QUANTITY DECREASED TO 7 QUARTS IN CRUISE. AT BLOCK-IN OIL QUANTITY INDICATED 13 QUARTS. FOUND OIL PUDDLING UNDER NR 2 ENGINE FAN BLADES AT BOTTOM OF FAN COWL. OILSDR FDEA201112215413Indicator · malfunctionedNR 1 N1 ANALOG NEEDLE WOULD NOT INCREASE ABOVE 45 PERCENT ON TAKEOFF. R& R NR1 ENG N1 GAUGE REF MM 77-11-21-04; OPS CHECKS GOOD. OK FOR SERVICE.SDR FDEA201110074352Ecu · failedNR 1 ENGINE POSSIBLE COMPRESSOR STALL WHILE DESCENDING. HEARD A POP ON LT SIDE AND NOTICED NR1 N1 RPM AT 20 PERCENT, EGT AT 700 DEG, AT N2 58 PERCENT ENGINE WOULD NOT RESPOND TO THROTTLE INPUTS. ENGINE APPEARED TO RECOVER TO NORMAL AFTER LANDED & TAXIED CLEASDR FDEA201108173323Check Valve · malfunctionedON FINAL APPROACH, NR 1 ENG STARTED TO VIBRATE AFTER A BANG. EGT WENT TO 700 DEG. ENGINE WAS AT FLIGHT IDLE. ENGINE APPEARED TO COME BACK AND OPERATE FINE. ON LANDING ROLLOUT, THE EGT CLIMBED TO 710 DEG. AND INCREASING. SHUTDOWN ENGINE. N1 & N2 LOOKED NORMASDR FDEA201108063123Engine · failedNR 2 ENGINE FAILURE ON TAKEOFF. WINDMILLING OIL PRESSURE, TIME 19 MIN, ECAM WARNING ENG OVER LIMIT. POWERPLANT ENGINEER HAS APPROVED THE ENGINE FOR REMOVAL. R & R NR 2 ENGINE, OPS AND LEAK CHECKED GOOD, OK FOR SERVICE.SDR FDEA201107283006Fitting · gougedNR 2 ENG OTBD THRUST REVERSER FWD LWR BUMPER FITTING GOUGED IN 2 EA AREAS. MEASUREMENTS ARE APROX .4 X .3 X .10D AND .35 X .15 X .050D. R & R BUMPER FITTING AT NR2 ENG OTBD THRUST REVERSER FWD LWR IAW MRA CMM 78-32-11 AND 78-32-00.SDR FDEA201107283007Bracket · chafed1 ENG INBD THRUST REVERSER LOWER HARD MOUNTED PANEL ON L/E HAS PANEL LAND FOR T/R. LATCH PANEL CHAFED ON AFT END. R & R PART IAW SRM 51-40-21.SDR FDEA201106042117Seat Track · corrodedSEAT TRACK 2R HAS CORROSION ON FLANGE BETWEEN FRAME 30 -32. AFTER REMOVAL OF LEVEL 1 CORROSION SEAT TRACK 2R WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, FIG 101. R & R SEAT TRACK SECTION IAW SRM 53-10-16, FIG 201.SDR FDEA201101260361Support Angle · crackedNR 2 ENG, LT THRUST REVERSER HINGE COVER SUPPORT ANGLE CRACKED. ACCOMPLISHED REPAIR IAW EA 6-7830-141662.SDR FDEA201012224738Skin · crackedCLOSE R LT WING SPOILER SHROUD SUPPORT SKIN CRACK ABOUT 0.75 IN BELOW NR3 SPOILER INBD EDGE. FABRICATE A NEW SUPPORT SKIN IAW DWG NR A57240194 AND INSTALL WITH FASTENERS. REF AB6F SRM 51-40-21. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201012214735Wheel · damagedEXCESSIVE TIRE VIBRATION ON T/O, ROLL-CONTINUED T/O FOR AIR TURN BACK. EXCESSIVE VIBRATION ON LANDING. AFTER TURN OFF RUNWAY FIRE MEM CONFIRMED, BLOWN TIRE ON RT LDG GEAR MAYBE NR 7 WITH HYD FLUID LEAKING. R & R NR 7 MAIN TIRE TEMPORALLY TO REMOVE SAID ACFSDR FDEA201012104628Carriage · misalignedLT WING T/E FLAP NR6 FRONT CARRIAGE UPPER BRIDGE OTBD SHIM EXTRUDED. EA6-2750-141650 REPAIR ACCOMPLISHED. IAW GMM 6-2-100 REPAIR CLASSIFIED AS MINOR.SDR FDEA201010134065Floorbeam · damagedAFT CARGO COMPARTMENT, UPPER DOOR CUTOUT AT FRAME 61 RT SIDE, HAS A DOUBLE DRILLED HOLE IN THE FLOORBEAM. THE HOLE IS FOR THE INSTALLATION OF THE UPPER PROFILE. REPAIRED IAW EA 6-5310-136713; "FUSELAGE - FRAME FITTING AT FRAME 61 AND STRINGER 26".SDR FDEA201010124007Shim · misalignedLT WING T/E NR 5 TRACK CARRIAGE UPPER BRIDGE INBD SHIM GOT MIGRATION. EA 6-2750-141636 REPAIR ACCOMPLISHED. THE REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201010124008Carriage · misalignedLT WING T/E NR 3 TRACK CARRIAGE UPPER BRIDGE INBD SHIM GOT MIGRATION. EA 6-2750-141636 REPAIR ACCOMPLISHED. THE REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.SDR FDEA201010124009Carriage · misalignedRT WING T/E FLAP NR6 REAR CARRIAGE LEVER MOUNTING YOKE INBD SHIM MIGRATED. EA 6-2750-414636 REPAIR ACCOMPLISHED. THE REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.
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