N678FE

Service difficulty reports · 220

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N678FE' AND registry_match = 'registration'
  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 FDEA201109123834Floor Panel · delaminatedFORWARD CARGO BAY FLOOR PANEL 131PG FOUND DELAMINATED. FLOOR PANEL REMOVED PER AMM 53-10-29-04, REV 52. NEW FLOOR PANEL FABRICATED PER DWG SRZ-25-005, REV J AND INSTALLED PER AMM 53-10-29-04, REV 52. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REV 112.Sep 12, 2011 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109123833Floor Panel · delaminatedFORWARD CARGO BAY FLOOR PANEL 131QG AFOUND DELAMINATED. FLOOR PANEL REMOVED PER AMM 53-10-29-04, REV 52. NEW FLOOR PANEL FABRICATED PER DWG SRZ-25-005, REV J AND INSTALLED PER AMM 53-10-29-04, REV 52. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REV 112.Sep 12, 2011 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109123832Floor Panel · delaminatedFORWARD CARGO BAY FLOOR PANEL 131PG FOUND DELAMINATED. FLOOR PANEL REMOVED PER AMM 53-10-29-04, REV 52. NEW FLOOR PANEL FABRICATED PER DWG SRZ-25-005, REV J AND INSTALLED PER AMM 53-10-29-04, REV 52. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REV 112.Sep 12, 2011 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109123831Floor Panel · delaminatedFORWARD CARGO BAY FLOOR PANEL 131NG FOUND DELAMINATED. REMOVED PER AMM 53-10-29-04, REV 52. NEW FLOOR PANEL FABRICATED PER DWG SRZ-25-005, REV J. INSTALLED PER AMM 53-10-29-04, REV 52. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REV 112.Sep 12, 2011 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109123830Floor Panel · delaminatedAFT CARGO BAY FLOOR PANEL 151SF FOUND DELAMINATED. FLOOR PANEL REMOVED AND REPLACED BY FABRICATION PER DWG SRZ-25-005, REV J. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REV 112.Sep 12, 2011 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109123829Floor Panel · delaminatedAFT CARGO BAY FLOOR PANEL 151VF FOUND DELAMINATED. FLOOR PANEL REMOVED REMOVED PER AMM 53-10-33-04, REV 52. NEW FLOOR PANEL FABRICATED PER DWG SRZ-25-005 AND INSTALLED PER AMM 53-10-33-04, REV 52. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100, REV 112.Sep 12, 2011 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109013611Seat Track · wornMAIN DECK SEAT TRACK AND DUMMY SEAT TRACK ATTACHMENT FITTING GAP CHECK AT FRAME 38.2 LEFT NR 4 WORN OUT OF LIMITS. REWORKED AS PER SRM 53-15-16 REV 20, FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.Sep 1, 2011 · N678FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201109013610Seat Track · wornMAIN DECK SEAT TRACK ATTACHMENT FITTING GAP CHECK AT FRAME 38.2, NR 2 LT WORN OUT OF LIMIT. REWORKED AS PER SRM 53-15-16 REV 20, FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.Sep 1, 2011 · N678FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201109013609Seat Track · wornSEAT TRACK AT FRAME 38.2 WORN OUT OF LIMITS. SEAT TRACK REWORKED AS PER SRM 53-15-16 REV 20, FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.Sep 1, 2011 · N678FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201109013608Seat Track · wornDECK SEAT TRACK AT FRAME 38.2 WORN OUT OF LIMITS. REWORKED AS PER SRM 53-15-16 REV 20, FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.Sep 1, 2011 · N678FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201109013605Seat Track · wornSEAT TRACK AT FRAME 38.2 NR 4 FOUND WORN OUT OF LIMITS. SEAT TRACK REWORKED AS PER SRM 53-15-16 REV 20, FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.Sep 1, 2011 · N678FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201109013604Seat Track · wornMAIN DECK SEAT TRACK ATTACHMENT FITTING GAP CHECK AT FRAME 38.2 NR 5 RIGHT WORN OUT OF LIMITS. SEAT TRACK ATTACHMENT FITTING REWORKED AS PER SRM 53-15-16 REV 20, FIGURE 201. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. REV 112.Sep 1, 2011 · N678FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201108293560Floor Panel · damagedMAIN DECK FLOOR PANEL RT AT FRAME 37 TO 38.2, X = -57 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 52. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J. PAINTED IAW SRM 53-10-20, REV 20 AND INSTALLED IAW AMM 53-10-25, REV 52. REPAIR CLASSAug 29, 2011 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201108293554Floor Panel · damagedMAIN DECK FLOOR PANEL RT AT FRAME 37 TO 38.2, X = -57 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 52. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J. PAINTED IAW SRM 53-10-20, REV 20 AND INSTALLED IAW AMM 53-10-25, REV 52. REPAIR CLASSIAug 29, 2011 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201108293562Floor Panel · damagedMAIN DECK FLOOR PANEL LT AT FRAME 30 TO 34, X = 17 TO 34 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 52. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J. PAINTED IAW SRM 53-10-20, REV 20 AND INSTALLED IAW AMM 53-10-25, REV 52. REPAIR CLAAug 29, 2011 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201108293561Floor Panel · damagedMAIN DECK FLOOR PANEL AT FRAME 28 TO 30, X = 17 TO 37 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 52. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J. PAINTED IAW SRM 53-10-20, REV 20 AND INSTALLED IAW AMM 53-10-25, REV 52. REPAIR CLASSIAug 29, 2011 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201108293559Floor Panel · damagedMAIN DECK FLOOR PANEL LT AT FRAME 40 TO 43, X = 57 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 52. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005 REV J. PAINTED IAW SRM 53-10-20, REV 20 AND INSTALLED IAW AMM 53-10-25, REV 52. REPAIR CLASSIFIAug 29, 2011 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201108293558Floor Panel · damagedMAIN DECK FLOOR PANEL LT AT FRAME 38.2 TO 40, X = 57 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 52. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J. PAINTED IAW SRM 53-10-20, REV 20 AND INSTALLED IAW AMM 53-10-25, REV 52. REPAIR CLASSIFAug 29, 2011 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201108293557Floor Panel · damagedMAIN DECK FLOOR PANEL, RT AT FRAME 28 TO 30, X = -57 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 52. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J. PAINTED IAW SRM 53-10-20, REV 20 AND INSTALLED IAW AMM 53-10-25, REV 52. REPAIR CLASSAug 29, 2011 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201108293556Floor Panel · damagedMAIN DECK FLOOR PANEL RT AT FRAME 30 TO 34, X = -57 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 52. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J. PAINTED IAW SRM 53-10-20, REV 20 AND INSTALLED IAW AMM 53-10-25, REV 52. REPAIR CLASSIFIAug 29, 2011 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201108293555Floor Panel · damagedMAIN DECK FLOOR PANEL RT AT FRAME 34 TO 37, X = -57 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 52. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J. PAINTED IAW SRM 53-10-20, REV 20 AND INSTALLED IAW AMM 53-10-25, REV 52. REPAIR CLASSIFAug 29, 2011 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201108293553Floor Panel · damagedMAIN DECK FLOOR PANEL RT AT FRAME 38.2 TO 40, X = -57 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 52. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J. PAINTED IAW SRM 53-10-20, REV 20 AND INSTALLED IAW AMM 53-10-25, REV 52. REPAIR CLASAug 29, 2011 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201108293552Floor Panel · damagedFLIGHT COMPARTMENT FLOOR PANEL NR 211HP FOUND DAMAGED. R & R BY FABRICATION IAW DWG SR30-53-005. PAINTED IAW SRM 53-10-20, REV 20. REPAIR CLASSIFIED AS MJOR IAW GMM 6-2-100, REV 112.Aug 29, 2011 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201108293551Floor Panel · damagedMAIN DECK FLOOR PANEL LT AT FRAME 43 TO 47 X = 57 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 52. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J. PAINTED IAW SRM 53-10-20 REV 20 AND INSTALLED IAW AMM 53-10-25, REV 52. REPAIR CLASSIFIED AAug 29, 2011 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201108293550Floor Panel · damagedMAIN DECK FLOOR PANEL RT AT FRAME 40 TO 43, X = -57 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 52. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J. PAINTED IAW SRM 53-10-20, REV 20 AND INSTALLED IAW AMM 53-10-25, REV 52. REPAIR CLASSIFIEAug 29, 2011 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201108293549Floor Panel · damagedMAIN DECK FLOOR PANEL RT AT FRAME 43 TO 47, X = -57 FOUND DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 52. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J. PAINTED IAW SRM 53-10-20, REV 20 AND INSTALLED IAW AMM 53-10-25, REV 52. REPAIR CLASSIFIEAug 29, 2011 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201108263508Floorbeam · crackedFWD CARGO COMPARTMENT- MAIN DECK FLOORBEAM AT FRAME 31, RBL 27 CRACKED. REPAIR CARRIED OUT AS PER SRM 53-10-15 REV 20, FIGURE 212. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.Aug 26, 2011 · N678FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201108263510Floor Support · corrodedMAIN DECK FWD LAVATORY ENTRY AREA FLOOR SUPPORT AT FRAME 11 TO FRAME 13, X= 17.5 FOUND CORRODED. R & R FLOOR SUPPORT IAW SRM 51-40-21, REV 20. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 26, 2011 · N678FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201108263509Floorbeam · crackedFWD MAIN DECK CARGO FLOORBEAM AT FRAME 34, RBL 27 SUSPECTED CRACKED. REPAIR CARRIED OUT IAW SRM 53-10-15, REV 20, FIG 212. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Aug 26, 2011 · N678FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201108263507Floorbeam · crackedFWD MAIN DECK CARGO FLOORBEAM AT FRAME 31, RBL 27 SUSPECTED CRACKED. REPAIR CARRIED OUT IAW SRM 53-10-15, REV 20, FIG 212. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Aug 26, 2011 · N678FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201108263506Floorbeam · crackedFWD CARGO MAIN DECK FLOORBEAM AT FRAME 28, RBL 27 SUSPECTED CRACKED. REPAIR CARRIED OUT IAW SRM 53-10-15, REV 20, FIG 212. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.Aug 26, 2011 · N678FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201108263505Floor Panel · damagedMAIN DECK FLOOR PANEL DAMAGED, AT FRAME 58 TO FRAME 60, X = 37. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 52. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J. PAINTED IAW SRM 53-10-20, REV 20 AND INSTALLED IAW AMM 53-10-25, REV 52. REPAIR CLASSIFIED AAug 26, 2011 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201108263504Floor Panel · damagedMAIN DECK FLOOR PANEL DAMAGED, AT FRAME 60 TO FRAME 62, X = 57. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 52. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J. PAINTED IAW SRM 53-10-20, REV 20 AND INSTALLED IAW AMM 53-10-25, REV 52. REPAIR CLASSIFIED AAug 26, 2011 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201108263503Floor Panel · damagedMAIN DECK FLOOR PANEL DAMAGED, AT FRAME 54 TO FRAME 54.2, X = 57. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 52. NEW FLOOR PANEL FABRICATED DWG SRZ-25-005 REV J, PAINTED IAW SRM 53-10-20, REV 20 AND INSTALLED IAW AMM 53-10-25, REV 52. REPAIR CLASSIFIED AS MAAug 26, 2011 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201108263502Floor Panel · damagedMAIN DECK FLOOR PANEL DAMAGED, AT FRAME 52 TO FRAME 54, X = 57. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 52. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J, PAINTED IAW SRM 53-10-20, REV 20 AND INSTALLED IAW AMM 53-10-25, REV 52. REPAIR CLASSIFIED ASAug 26, 2011 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201108263501Floor Panel · damagedMAIN DECK FLOOR PANEL DAMAGED, AT FRAME 47 TO FRAME 51, X = -57. LOOR PANEL REMOVED IAW AMM 53-10-25, REV 52. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J, PAINTED IAW SRM 53-10-20, REV 20 AND INSTALLED IAW AMM 53-10-25, REV 52. REPAIR CLASSIFIED ASAug 26, 2011 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201108263500Floor Panel · damagedMAIN DECK FLOOR PANEL DAMAGED, AT FRAME 51 TO FRAME 54, X = -57. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 52. NEW FLOOR PANEL FABRICATED DWG SRZ-25-005, REV J, PAINTED IAW SRM 53-10-20, REV 20 AND INSTALLED IAW AMM 53-10-25, REV 52. REPAIR CLASSIFIED AS Aug 26, 2011 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201108263499Floor Panel · damagedMAIN DECK FLOOR PANEL DAMAGED, AT FRAME 54.0 TO FRAME 54.2, X = -57. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 52. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J, PAINTED IAW SRM 53-10-20, REV 20 AND INSTALLED IAW AMM 53-10-25, REV 52. REPAIR CLASSIFAug 26, 2011 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201108263498Floor Panel · damagedMAIN DECK FLOOR PANEL DAMAGED, AT FRAME 54.2 TO FRAME 55, X = -57. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 52. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J. PAINTED IAW SRM 53-10-20, REV 20 AND INSTALLED IAW AMM 53-10-25, REV 52. REPAIR CLASSIFAug 26, 2011 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201108263497Floor Panel · damagedMAIN DECK FLOOR PANEL DAMAGED, RT AT FRAME 55 TO FRAME 57.1, X = -57. DAMAGED FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 52. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J. PAINTED IAW SRM 53-10-20, REV 20 AND INSTALLED IAW AMM 53-10-25, REV 52. REPAAug 26, 2011 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201108263496Floor Panel · damagedMAIN DECK FLOOR PANEL RT AT FRAME 57.1 TO FRAME 58, X = -57 DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 52. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J, PAINTED IAW SRM 53-10-20, REV 20. NEW FLOOR PANEL INSTALLED IAW AMM 53-10-25, REV 52. Aug 26, 2011 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201108263495Floor Panel · damagedMAIN DECK FLOOR PANEL RT AT FRAME 58 TO FRAME 60, X = -57 DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 52. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J. FLOOR PANEL PAINTED IAW SRM 53-10-20, REV 20 AND INSTALLED IAW AMM 53-10-25, REV 52. RAug 26, 2011 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201108263494Floor Panel · damagedMAIN DECK FLOOR PANEL RT AT FRAME 60 TO FRAME 62, X = -57 DAMAGED. FLOOR PANEL REMOVED IAW AMM 53-10-25, REV 52. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J, FLOOR PANEL PAINTED IAW SRM 53-10-20, REV 20 AND INSTALLED IAW AMM 53-10-25 REV 52. REPAIRAug 26, 2011 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201108263493Floor Panel · damagedMAIN DECK FLOOR PANEL, RT AT FRAME 62 TO FRAME 65, X = -57 DAMAGED. REMOVED IAW AMM 53-10-25, REV 52. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J. INSTALLED FLOOR PANEL IAW AMM 53-10-25, REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 11Aug 26, 2011 · N678FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201108233408Skin · dentedSKIN DENT LOCATED 6 INCHES AFT OF FRAME 72 AND 0.30 INCH FROM STRINGER 29 R FASTENER LOCATION ANG 6.75 INCHES AFT OF FRAME 72 FROM STRINGER 29R FASTENER LOCATION IAW WRI 55-30/9975 (EA 6-5330-151155, PART 2). REPAIRED IAW EA 6-5310-155801.Aug 23, 2011 · N678FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201108233409Skin · dentedDENT LOCATED FORWARD OF FRAME 76, 1.0" FROM S30R IAW EA 6-5330-151155, PART 2. REPAIRED IAW SRM 53-10-012, REV 20, FIG 208. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Aug 23, 2011 · N678FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201108233420Longeron · corrodedCABIN RT FUSELAGE INTERCOSTAL AT LONGERON 18R STA 1381 TO STA 1401 FOUND WITH CORROSION. CORROSION REMOVED AS PER SRM 51-21-01 REV 47. ORIGINAL THICKNESS = 0.080 INCH; MATERIAL REMOVED = 0.040 INCH; MATERIAL REMAINED = 0.040 INCH, AND FOUND EXCEEDED LIMITSAug 23, 2011 · N678FE · Airbus A300F4605R · Fuselage Main, Longeron/StringerSDR FDEA201108233418Intercostal · corrodedCABIN RT FUSELAGE INTERCOSTAL AT LONGERON 16R STA 1159 TO STA 1179. FOUND WITH CORROSION.Aug 23, 2011 · N678FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR 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.Aug 6, 2011 · N678FE · Airbus A300F4605R · Engine (Turbine/Turboprop)SDR FDEA201107222910Brake · overheatedNR 7 BRAKE TEMP INDICATED 600 DEGREES WITH BRAKE FAN ON, ALL OTHER BRAKES 100 DEGREE OR LESS. R & R NR7 BRAKE, OPS & LEAK CHECK GOOD IAW MM CH 32-42-27-04.Jul 22, 2011 · N678FE · Airbus A300F4605R · Brake
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