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 FDEA201208052850Cargo Track · corrodedMAIN CARGO TRACK 2L HAS 4 INCH LONG AREA OF CORROSION BETWEEN FR 51 AND FR 52. REMOVED CORROSION 52 IAW SRM 51-74-10, FOUND AREA TO BE OUT OF LIMITS IAW SRM 53-10-16, FIG 102. REMOVED CARGO TRACK FROM FR 50 TO FR 54 AND FABRICATED REPAIR ANGLES IAW SRM 53-10Aug 5, 2012 · N658FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201208052851Cargo Track · corrodedMAIN DECK CARGO BETWEEN FR 72 & FR 75 CARGO TRACK 2L HAS 4 SPOTS OF CORROSION 2 SQUARE INCHES. AFTER REMOVAL OF CORROSION, FOUND AREA TO BE OUT OF LIMITS IAW SRM 53-10-16 FIG. 102. REMOVED CARGO TRACK, FABRICATED REPLACEMENT AND REPAIR SPLICES, AND INSTALLEAug 5, 2012 · N658FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201208052852Seat Track · corrodedSEAT TRACK NR 5 LT CORRODED AFT OF FR 54.3 RT FLANGE. REMOVED CORROSION IAW SRM 51-74-10, FOUND AREA TO BE OUT OF LIMITS IAW SRM 53-10-16, FIG 102. R & R SEAT TRACK IAW SRM 53-10-16, FIG 102. REPROTECTED AREA IAW SRM 51-75-10.Aug 5, 2012 · N658FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201208052856Adapter · gougedFR 63 CLEVIS ADAPTER BETWEEN SEAT TRACK 4L & 5L GOUGED. R & R CLEVIS ADAPTER IAW SRM 51-72-10.Aug 5, 2012 · N658FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201208022815Seat Track · gougedSEAT TRACK 4L GOUGED AT SCALLOP AND INSIDE SCALLOP BETWEEN FR 56 - FR 58. SMOOTHED AND BLENDED GOUGES IAW SRM 51-74-10. FOUND ALL BLENDED AREAS TO BE OUT OF LIMITS IAW SRM 53-10-16, FIG 102, PG 105. R & R SECTION OF SEAT TRACK 4L FROM 54.2 AND FR 58 IAW SRMAug 2, 2012 · N658FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201208022825Adapter · corrodedCLEVIS ADAPTER FR 42 BETWEEN SEAT TRACKS 4L & 5L HAS A 1SQ" AREA OF CORROSION AT UPPER AFT FLANGE. REMOVED CORROSION ON CLEVIS ADAPTER AT FR 42 BETWEEN TRACKS 4L & 5L IAW FSRM 51-74-10, PARA 5. VERIFIED OUT OF TOLERANCE IAW DWG A53813019. R & R CLEVIS ADAPAug 2, 2012 · N658FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201208022817Cargo Track · gougedMAIN DECK CARGO TRACK 2R GOUGED AT FR 54 REF AMM 53-10-06. R & R CARGO TRACK IAW FSRM 51-72-10.Aug 2, 2012 · N658FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201208022824Seat Track · corrodedSEAT TRACK 5L INBD FLANGE HAS 3EA AREAS OF CORROSION FR 28-29 APPROX TWO SQUARE INCHES. REMOVED CORROSION IAW SRM 51-74- 10. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16 FIG. 102 PG. 105. REMOVED, FABRICATED, AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-Aug 2, 2012 · N658FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201208012797Adapter · corrodedMAIN DECK CARGO , CLEVIS ADAPTER BETWEEN SEAT TRACKS 4L & 5L FR 37 HAS 3 SQUARE INCHES OF CORROSION UPPER & LWR SURFACE. AROUND FASTENER HOLES. AFTER REMOVAL OF CORROSION OF CLEVIS ADAPTER WAS FOUND TO BE OUT OF TOLERANCE IAW DWG 53781936. ORIGINAL THICKNESAug 1, 2012 · N658FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201208012804Floorboard · damagedMAIN DECK CARGO, FLOORBOARD 231KG HAS A 1 SQUARE INCH AREA WITH DAMAGED FIBERGLASS, BROKEN INSERT, & BALL BEARINGS EMBEDDED AT UPPER SURFACE. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Aug 1, 2012 · N658FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201208012805Floorboard · damagedMAIN DECK CARGO FLOORBOARD 242RT BROKEN. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Aug 1, 2012 · N658FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201208012806Floorboard · damagedFLOORBOARD 242BF HAS 8 INCH AREA OF IMPACT DAMAGE, WITH CRACK, ON FORWARD EDGE. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Aug 1, 2012 · N658FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201208012813Adapter · corrodedMAIN DECK CARGO, FR 74 CLEVIS ADAPTER BETWEEN SEAT TRACKS 4 & 5R TWO FASTENER HOLES UPPER & LOWER SURFACE CORRODED .5 SQUARE INCH. R & R CORRODED CLEVIS ADAPTER IAW SRM 51-40-21, PARA 7.Aug 1, 2012 · N658FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201208012802Adapter · gougedMAIN DECK CARGO AT FR65 CLEVIS ADAPTER BETWEEN SEAT TRACK 4L AND 5L CROWN HAS MULTIPLE GOUGES. R & R CLEVIS ADAPTER IAW SRM 51-72-10.Aug 1, 2012 · N658FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201208012803Cargo Track · corrodedMAIN DECK CARGO TRACK BETWEEN FR 76 AND FR 77 CORRODED, AFTER REMOVAL OF CORROSION, SEAT TRACK NR 1 WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. R & R CARGO TRACK IAW SRM 53-10-16, FIG 201 AND SRM 51-40-21, PARA 7.Aug 1, 2012 · N658FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201208012807Skin · misrepairedSKIN AT BS 1900, L52L MISREPAIRED. FABRICATED NEW DOUBLER & TRIPLER IAW SRM 53-20-00. INSTALLED NEW DOUBLER & TRIPLER IAW SRM 51-31-01. MAJOR REPAIR.Aug 1, 2012 · N303FE · Doug MD1030F · Fuselage Main, Plate/SkinSDR FDEA201207312776Adapter · corrodedMAIN DECK CARGO FR63 CLEVIS ADAPTER BETWEEN SEAT TRACK 2R AND 3R, ONE FASTNER HOLE UPPER SURFACE CORRODED APX .5 SQUARE INCHES. AFTER REMOVAL OF CORROSION, FOUND TO BE OUT OF TOLERANCE IAW DWG A53275404. R & R CLEVIS ADAPTER IAW SRM 51-40-21, PARA 7.Jul 31, 2012 · N658FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201207312778Cargo Track · gougedMAIN DECK CARGO, CARGO TRACK 2L SCALLOPS GOUGED SIX SQUARE INCHES. LOCATED BETWEEN FR58 AND FR59. BLENDED AREA IAW SRM 51-73-10 P208. FOUND OUT OF LIMITS IAW SRM 53-10-16 P105. R & R CARGO TRACK SECTION IAW SRM 51-72-10.Jul 31, 2012 · N658FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201207312785Adapter · gougedFR 64 CLEVIS ADAPTER BETWEEN SEAT TRACK 3R & 4R CROWN & CHANNEL GOUGED. R & R CLEVIS ADAPTER IAW FSRM 51-72-10.Jul 31, 2012 · N658FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201207312786Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL 231HG HAS TEN INCHES OF EDGE FILLER MISSING AND FWD CORNER BROKEN OFF. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Jul 31, 2012 · N658FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201207312787Floorboard · puncturedFLOORBOARD 231VG, HAS A .75 PUNCTURE AT UPPER SURFACE. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Jul 31, 2012 · N658FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201207312788Floorboard · damagedBULK CARGO FLOORBOARD 161GF, BACKING HAS SEPARATED IN SEVERAL PLACES. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Jul 31, 2012 · N658FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201207312789Floorboard · damagedAFT CARGO FLOORBOARD 161AF BACKING SEPARATED AND CORRODED APPROX 10 SQUARE INCHES. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Jul 31, 2012 · N658FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201207312790Floorboard · crackedMAIN CARGO DECK FLOORBOARD 231FF CRACKED AND HAS FOUR LOOSE INSERTS AND 30 INCHES OF EDGE FILLER MISSING. FABRICATED FLOORBOARD IAW DWG SRZ 25-005, REV J.Jul 31, 2012 · N658FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201207312791Floorboard · damagedFLOORBOARD 232UG HAS MISSING EDGE FILLER ON AFT EDGE (3 INCHES) AND AROUND CLEVIS CUTOUT (10 INCHES) ALSO SMALL PUNCTURED AREA LOCATED 0.5 INCH FROM AFT EDGE. FABRICATED FLOORBOARD IAW DWG SRZ 25-005, REV J.Jul 31, 2012 · N658FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201207312769Seat Track · gougedSEAT TRACK 2R GOUGED AT FR58 ABOUT 10 SQUARE INCHES. BLENDED GOUGES ON SEAT TRACK 2R AT FR 58 IAW SRM 51-73-10, PG 208. FOUND TO BE OUT OF LIMITS IAW FSRM 53-10-16, PG 103. REMOVED, CUT-OUT SEAT TRACK SECTION BETWEEN FR57.3 AND FR 58 SEAT TRACK 2R IAW FSRM 5Jul 31, 2012 · N658FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201207312773Adapter · gougedCLEVIS ADAPTER SCALLOPS GOUGED 4 SQUARE INCHES LOCATED FR61 BETWEEN SEAT TRACKS 4L AND 5L. R & R CLEVIS ADAPTER IAW FSRM 53-40-21, PG 23-31.Jul 31, 2012 · N658FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201207312795Floorbeam · crackedFLOORBEAM, FWD CARGO BAY AT FR 27 RT SIDE BETWEEN CARGO TRACKS 2 & 3 CRACKED .1250". PERFORMED CUT OUT OF CRACK AND REWORKED FLANGES AND STIFFENER FLUSH IAW SRM 53-10-15 FIG 212, FABRICATED ANGLE IAW SRM 53-10-15 AND INSTALLED ANGLE AT FR 27 BETWEEN SEAT TRAJul 31, 2012 · N658FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201207312770Seat Track · gougedSEAT TRACK 2R HAS BARE METAL ABOUT FIVE SQUARE INCHES AND GOUGED AT FASTENER HOLES, 5 PLACES, BETWEEN FR40 AND FR44. REMOVED GOUGES IAW SRM 51-73-10 PG 207, FOUND FIVE AREAS TO BE OUT OF LIMITS IAW SRM 53-10-16 PG 105. REMOVED SEAT TRACK SECTION IAW SRM 51-4Jul 31, 2012 · N658FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201207312793Floorbeam · crackedMAIN DECK CARGO FLOORBEAM AT FR 30 LT SIDE BETWEEN SEAT TRACKS 4 & 5 CRACKED .1250" CUT OUT DAMAGED AREA IAW SRM 53-10-15, FIG 212. VERIFIED CRACK REMOVAL IAW NTM 51-10-08 NO CRACK FOUND AFTER CUT OUT. REPAIRED FLOORBEAM IAW SRM 53-10-15, FIG 212.Jul 31, 2012 · N658FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201207312794Floorbeam · crackedMAIN DECK CARGO FLOORBEAM AT FR 32, LT SIDE BETWEEN SEAT TRACK 4 & 5 CRACKED. CUT OUT DAMAGED AREA IAW SRM 53-10-15, FIG 212. VERIFIED CRACK REMOVAL, FOUND NO CRACK INDICATION AFTER CUT OUT IAW NTM 51-10-08. REPAIRED FLOORBEAM IAW SRM 53-10-15, FIG 212. PROJul 31, 2012 · N658FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201207302762Floor Panel · damagedMAIN CARGO DECK FLOOR PANEL 241YJ HAS CORNER BROKEN OFF APPROXIMATELY FOUR SQUARE INCHES. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Jul 30, 2012 · N658FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201207302763Floorboard · damagedMAIN DECK CARGO FLOORBOARD 242QJ CRUSHED AROUND THE CLEVIS ADAPTER CUT OUT AT THE EDGE, FOUR PLACES. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV. JJul 30, 2012 · N658FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201207302764Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL 231AH HAS ONE INSERT PULLED THRU PANEL & 10 INCHES OF EDGE FILLER MISSING. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Jul 30, 2012 · N658FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201207302765Floorboard · crackedFLOORBOARD 232VH, BROKEN ACROSS ENTIRE MIDDLE SECTION. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Jul 30, 2012 · N658FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201207302767Floorboard · damagedMAIN DECK CARGO FLOORBOARD 241DF HAS SEVEN INCHES OF IMPACT DAMAGE. FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.Jul 30, 2012 · N658FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201207302750Cargo Track · gougedMAIN DECK CARGO TRACK 1 SCALLOPS GOUGED 4 SQUARE INCHES. LOCATED BETWEEN FR 58 AND FR 59. BLENDED DAMAGED AREA IAW SRM 51-73-10 PG 208, AND FOUND AREA TO BE OUT OF LIMITS IAW SRM 53-10-16 PG 105. REMOVED DAMAGED CARGO TRACK IAW SRM 51-40-21 PG 46. FABRICATEDJul 30, 2012 · N658FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201207302766Cargo Track · corrodedMAIN DECK CARGO AT FR 76 - 77 CARGO TRACK 4L FLANGE HAS THREE SPOTS OF CORROSION, 4 SQUARE INCHES, REF AMM 53-10-16-06. REMOVED CORROSION IAW SRM 51-74-10 PG 205. FOUND AREA TO BE OUT OF LIMITS IAW SRM 53-10-16 FIG 102. REMOVED CARGO TRACK IAW SRM 51-40-Jul 30, 2012 · N658FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201207292741Stiffener · bentTAIL COMPARTMENT, BETWEEN FR 86 AND FR 87 AT STRINGER 35 RIGHT SUPPORT WEB UPPER STIFFINER IS BENT. FORMED UPPER SUPPORT STIFFENER IAW SRM 51-26-00 PG1, SUPPORT STIFFENER WOULD NOT RETAIN ORIGINAL SHAPE. R & R UPPER SUPPORT STIFFENER IAW SRM 51-72-10, PG 1-3Jul 29, 2012 · N658FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201207292742Adapter · gougedMAIN DECK CARGO FR 66 CLEVIS ADAPTER AT FR 66 BETWEEN SEAT TRACKS 4L & 5L CROWN & CHANNEL HAS GOUGE. REF AMM 53-10-16-6. REMOVED CORROSION AND GOUGES IAW AMM 12-21-13-03 AND SRM 51-73-10. OUT OF LIMITS IAW SRM 53-10-15, FIG 101. R & R CLEVIS ADAPTER IAW SRMJul 29, 2012 · N658FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201207282731Adapter · gougedMAIN DECK CARGO AT FR 71 CLEVIS ADAPTER BETWEEN SEAT TRACK 3R AND 4R CROWN GOUGED .5". R & R CLEVIS ADAPTER IAW SRM 51-72-10.Jul 28, 2012 · N658FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201207282733Adapter · gougedFR 64 BETWEEN SEAT TRACKS 1R AND 2R CLEVIS ADAPTER HAS GOUGE .5". R & R CLEVIS ADAPTER FR 64 SEAT TRACKS 1R AND 2R IAW FSRM 51-72-10.Jul 28, 2012 · N658FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201207282734Shear Plate · crackedFLOOR SHEAR WEB BETWEEN FR 79 AND FR 80 RT SIDE CRACKED. R & R SHEAR WEB IAW FSRM 51-72-10 PG2.Jul 28, 2012 · N658FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201207282735Adapter · gougedMAIN DECK CARGO AT FR. 64 CLEVIS ADAPTER BETWEEN SEAT TRACK 1L AND 2L CROWN HAS GOUGE 1.0". R & R CLEVIS ADAPTER IAW SRM 51-72-10.Jul 28, 2012 · N658FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201207282736Adapter · damagedMAIN DECK CARGO CLEVIS ADAPTER FR 51-52 BETWEEN SEAT TRACKS 2R AND 3R HAS ELONGATED FASTENER HOLES. R & R CLEVIS ADAPTER IAW SRM 51-72-10.Jul 28, 2012 · N658FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201207282737Floor Panel · crackedFLOOR PANEL 252PH HAS ONE 12 INCHE CRACK. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Jul 28, 2012 · N658FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201207282738Floor Panel · crackedFLOOR PANEL 252BF HAS TWO 12 INCH CRACKS. FABRICATED REPLACEMENT FLOOR PANEL IAW DWG SRZ 25-005, REV J.Jul 28, 2012 · N658FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201207282739Adapter · corrodedMAIN DECK CARGO AT FR 62 CLS ADAPTER BETWEEN SEAT TRACK 2R AND 3R FLANGE DEFORMED AND CROWN CORRODED (1" SQ IN). REMOVED LEVEL ONE CORROSION FROM CLEVIS ADAPTER AND FOUND THE CLEVIS ADAPTER OUT OF LIMITS IAW SRM 53-10-15, FIG 103. R & R CLEVIS ADAPTER IAW SJul 28, 2012 · N658FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201207282740Adapter · damagedMAIN DECK CARGO CLEVIS ADAPTER FR 31 HAS IMPACT DAMAGE (1" SQUARE INCH) ON UPPER SURFACE SCALLOP BETWEEN SEAT TRACK 4L AND 5L. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15 FIG 103. REMOVED AND REPLACED CLEVIS ADAPTER IAW SRM 51-40-21, PAR 7 AND 51-72-10.Jul 28, 2012 · N658FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201207272711Adapter · damagedCLEVIS ADAPTER SCALLOPS GOUGED 2 SQ". LOCATED FR 58 BETWEEN SEAT TRACKS 4L AND 5L. REMOVED CLEVIS ADAPTER ON FR 58 BETWEEN SEAT TRACK 4L AND 5L IAW SRM 51-72-10. LOCATED AND DRILLED ADAPTER IAW SRM 51-72-10. INSTALLED NEW ADAPTER SRM 51-72-10. REPROTECTEJul 27, 2012 · N658FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
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