N681FE

Service difficulty reports · 339

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 = 'N681FE' 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 FDEA201410173283Floor Panel · crackedMDC COMPARTMENT FLOOR PANEL 241KK CRACKED. FABRICATED NEW FLOOR PANEL 241KK ON T14 1098196 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.Oct 17, 2014 · N681FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201410173282Floor Panel · crackedMDC COMPARTMENT 241HK FLOOR PANEL CRACKED. FABRICATED NEW FLOOR PANEL 241HK ON T14 1097941 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.Oct 17, 2014 · N681FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201410173281Floor Panel · crackedMDC COMPARTMENT FLOOR PANEL 242 QJ CRACKED. FABRICATED NEW FLOOR PANEL 242 QJ ON T14 1097939 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.Oct 17, 2014 · N681FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201410173279Attach Fitting · wornRIGHT NR 5 DUMMY SEAT TRACK FRAME 54 TO 54.2 HAS WORN ATTACHMENT FITTING. REPAIRED IAW SRM-53-15-16 & SRM-51-40-21 & T14 10981. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.Oct 17, 2014 · N681FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201410173278Attach Fitting · wornLEFT NR 5 DUMMY SEAT TRACK FRAME 54 TO 54.2 HAS WORN ATTACHMENT FITTINGS. REPAIRED IAW SRM-53-15-16 FIG 201 T14 1098191 & SRM-51-40-21. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.Oct 17, 2014 · N681FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201410163219Floor Panel · crackedMDC COMPARTMENT FLOOR PANEL BETWEEN FRAME 54.2 - 54.3, RT SIDE BETWEEN BL -450 & -Y953 CRACKED AROUND FLOOR ADAPTER. REMOVED & INSTALLED NEW FABRICATED FLOOR PANEL IAW AMM-53-10-25-04-02. FABRICATED ON T14 1098263 PN FX-B5327026002200 DWG SRZ-25-005. CLASSIOct 16, 2014 · N681FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201410163217Floor Panel · crackedMDC COMPARTMENT FLOOR PANEL 241TH CRACKED. FABRICATED NEW FLOOR PANEL 241TH ON T14 1098194 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.Oct 16, 2014 · N681FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201410163216Floor Panel · crackedMDC COMPARTMENT FLOOR PANEL 241CK CRACKED. FABRICATED NEW FLOOR PANEL 241CK ON T14 1098200 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.Oct 16, 2014 · N681FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201410163215Floor Panel · crackedMDC COMPARTMENT FLOOR PANEL 241AJ CRACKED. MDC FLOOR PANEL 241AJ FABRICATED NEW ON T14 1097935 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS A CAT A MAJOR REPAIR.Oct 16, 2014 · N681FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201410163214Floor Panel · crackedMDC COMPARTMENT FLOOR PANEL 242LK CRACKED. FABRICATED NEW FLOOR PANEL 242LK ON T14 1098197 IAW DWG SRZ-25-005. REPAIR CLASSIFIED CAT A MAJOR REPAIR.Oct 16, 2014 · N681FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201410163213Floor Panel · crackedMDC COMPARTMENT FLOOR PANEL 241GK CRACKED. FABRICATED NEW FLOOR PANEL 241GK ON T14 1098199 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.Oct 16, 2014 · N681FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201410163212Floor Panel · crackedMDC COMPARTMENT FLOOR PANEL 242UF CRACKED. FABRICATED NEW FLOOR PANEL 242UF ON T14 1098261 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.Oct 16, 2014 · N681FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201410163183Floor Panel · crackedMDC COMPARTMENT FLOOR PANEL BETWEEN FRAME 58 - 60 LT SIDE BETWEEN BL Y1456 & Y1959 CRACKED. INSTALLED & SEALED NEW MDC COMPARTMENT FLOOR PANEL 251RH IAW AMM 51-24-00-00. FABRICATED FLOOR PANEL ON T141097708 PN FX B5327027602000 DWG SRZ-25-005. MAJOR REPAIR.Oct 16, 2014 · N681FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201410163180Floor Panel · crackedMDC COMPARTMENT FLOOR PANEL BETWEEN FRAME 62 - 65 RT SIDE BETWEEN BL -Y450 & -Y953 CRACKED AROUND FLOOR ADAPTORS. INSTALLED & SEALED NEW MDC COMPARTMENT FLOOR PANEL IAW AMM 51-24-00-00. FABRICATED FLOOR PANEL ON T141097703 PN FX B5327028000800 DWG SRZ-25-005Oct 16, 2014 · N681FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201410163176Floor Panel · puncturedMDC COMPARTMENT FLOOR PANEL BETWEEN FRAME 57.1 - 58 LT SIDE BETWEEN BL Y1456 - Y1959 PUNCTURED. INSTALLED & SEALED NEW MDC COMPARTMENT FLOOR PANEL 251RG IAW AMM 51024-00-00. FABRICATED FLOOR PANEL ON T14 1097710 PN FX B5327072300600 DWG SRZ-25-005. MAJOR REOct 16, 2014 · N681FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201410163173Floor Panel · crackedMDC COMPARTMENT FLOOR PANEL BETWEEN FRAME 62 - 65 RT SIDE BETWEEN BL -Y1456 & -Y1959 CRACKED AROUND FLOOR ADAPTOR. INSTALLED & SEALED NEW MDC COMPARTMENT FLOOR PANEL 252YG IAW 51-24-00-00. FABRICATED FLOOR PANEL ON T14 1097712 PN FX B5327028200000 DWG SRZ-25Oct 16, 2014 · N681FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201410163172Floor Panel · crackedMDC COMPARTMENT FLOOR PANEL BETWEEN FRAME 60 - 62 RT SIDE BETWEEN BL -Y1456 & -Y1459 CRACKED AROUND FLOOR ADAPTOR. INSTALLED & SEALED NEW MDC COMPARTMENT FLOOR PANEL 252WH IAW AMM 51-24-00-00. FABRICATED FLOOR PANEL ON T14 1097711 PN FX B5327027800400 DWG SROct 16, 2014 · N681FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201410153171Floor Panel · crackedMDC COMPARTMENT FLOOR PANEL BETWEEN FRAME 57.1 - 58 RT SIDE BETWEEN BL -Y450 & -Y953 CRACKED AROUND FLOOR ADAPTER. REMOVED FLOOR PANEL IAW AMM 53-10-25-04. FABRICATED NEW PANEL ON T14 1097713, PANEL 252GF. INSTALLED PANEL AT FRAME 57.1- 58 RT SIDE BETWEEN BOct 15, 2014 · N681FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201410063390Floor Panel · delaminatedMAIN DECK CARGO COMPARTMENT FLOOR PANEL 241UF DELAMINATED. FABRICATED NEW FLOOR PANEL 241UF ON T14 1097942 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.Oct 6, 2014 · N681FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201410063309Floor Panel · puncturedMDC COMPARTMENT FLOOR PANEL 242UH PUNCTURED. FABRICATED NEW FLOOR PANEL 242UH ON T14 1097936 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR.Oct 6, 2014 · N681FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201410063166Floor Panel · delaminatedMDC COMPARTMENT FLOOR PANEL 242ZJ CRACKED. FABRICATED NEW FLOOR PANEL 242ZJ ON T14 1097905 IAW DWG SRZ25-005. CLASSIFIED AS CAT A MAJOR REPAIR.Oct 6, 2014 · N681FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201410063165Floor Panel · crackedMDC COMPARTMENT FLOOR PANEL 242UJ CRACKED. FABRICATED NEW FLOOR PANEL 242UJ ON T14 1097934 IAW DWG SRZ 25-005. CLASSIFIED AS CAT A MAJOR REPAIR.Oct 6, 2014 · N681FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201410063164Floor Panel · crackedMDC COMPARTMENT FLOOR PANEL 242TH CRACKED. FABRICATED NEW FLOOR PANEL 242TH ON T14 1098195 IAW DWG SRZ 25-005. CLASSIFIED AS CAT A MAJOR REPAIR.Oct 6, 2014 · N681FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201410063163Floor Panel · crackedMDC COMPARTMENT FLOOR PANEL 241LK CRACKED. FABRICATED NEW FLOOR PANEL 241LK ON T14 1098198 IAW DWG SRZ25-005. CLASSIFIED AS CAT A MAJOR REPAIR.Oct 6, 2014 · N681FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201410053405Attach Fitting · wornRIGHT NR 2 DUMMY TRACK FRAME 38.2 TO FRAME 40 HAS WORN ATTACHMENT FITTINGS. REPAIRED IAW SRM 53-15-16 FIG 201. INSERT FABRICATED ON T14 1098137 IAW SRM 53-15-16 FIG 201.Oct 5, 2014 · N681FE · Airbus A300F4605R · Fuselage Main, Attach FittingsSDR FDEA201410053330Attach Fitting · wornRIGHT NR 3 DUMMY TRACK FRAME 38.2 TO 40 HAS WORN ATTACHMENT FITTINGS. REPAIRED RT NR 3 DUMMY TRACK FRAME 38.2 TO 40 IAW SRM 53-15-16 FIG 201. INSERT FABRICATED ON T14 1098139 IAW SRM 53-15-16 FIG 201. REPAIR CLASSIFIED AS CAT A MAJOR.Oct 5, 2014 · N681FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201410053315Seat Track · gougedMDC COMPARTMENT SEAT TRACK BETWEEN FRAME 54.2 - 54.3 AT BL Y450 IS GOUGED IN SCALLOP. BLENDED AREA IAW SRM 51-73-10 L=1.6 & D=.900 OUT OF LIMITS IAW SRM 53-10-16 FIG 101. FABRICATED NEW SEAT TRACK SECTION IAW SRM 53-10-16 FIG 208. INSTALLED NEW SEAT TRACK SOct 5, 2014 · N681FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201410053308Floor Panel · crackedMDC COMPARTMENT FLOOR PANEL BETWEEN FRAME 60 - 62 LT SIDE BETWEEN BL Y1456 & Y1959 CRACKED AROUND FLOOR ADAPTORS. REMOVED & INSTALLED NEW FLOOR PANEL IAW AMM 53-10-25-04-02. FABRICATED NEW FLOOR PANEL IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPOct 5, 2014 · N681FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201410053307Floor Panel · crackedMDC COMPARTMENT FLOOR PANEL BETWEEN FRAME 58 - 60 RT SIDE BETWEEN BL -Y450 & -Y953 CRACKED AROUND FLOOR ADAPTORS. REMOVED & INSTALLED NEW FLOOR PANEL IAW AMM 53-10-25-04-02. FABRICATED NEW FLOOR PANEL IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS CAT A MAJOR REPOct 5, 2014 · N681FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201410053306Floor Panel · crackedMDC COMPARTMENT FLOOR PANEL BETWEEN FRAME 62 - 65 LT SIDE BETWEEN BL Y1456 & Y1959 CRACKED AROUND FLOOR ADAPTORS. REMOVED & INSTALLED FLOOR PANEL 251YG IAW AMM 53-10-25-04-02. FABRICATED NEW FLOOR PANEL T14 1097903 IAW DWG SRZ-25-005. REPAIR CLASSIFIED AS Oct 5, 2014 · N681FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201410053169Floor Panel · crackedMDC COMPARTMENT FLOOR PANEL BETWEEN FRAME 62 - 65 LT SIDE BETWEEN BL Y450 & Y953 CRACKED AROUND FLOOR ADAPTORS. REMOVED & INSTALLED PANEL IAW AMM 53-10-25-04-02. FABRICATED NEW PANEL ON T14 1097707 IAW DWG SRZ-25-005. CLASSIFIED AS CAT A MAJOR REPAIR.Oct 5, 2014 · N681FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201410053168Floor Panel · crackedMDC COMPARTMENT FLOOR PANEL BETWEEN FRAME 65 - 69 LT SIDE BETWEEN BL Y1456 & Y1959 CRACKED AROUND FLOOR ADAPTOR. REMOVED & INSTALLED PANEL IAW AMM 53-10-25-04-02. FABRICATED NEW PANEL ON T14 1098262 IAW DWG SRZ-25-005. CLASSIFIED AS CAT A MAJOR REPAIR.Oct 5, 2014 · N681FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201410053161Floor Panel · crackedMDC COMPARTMENT FLOOR PANEL BETWEEN FRAME 60 - 62 LT SIDE BETWEEN BL Y450 & Y953 CRACKED AROUND FLOOR ADAPTOR. REMOVED & INSTALLED PANEL IAW AMM 53-10-25-04-02. FABRICATED NEW PANEL ON T14 1097705 IAW DWG SRZ-25-005. CLASSIFIED AS CAT A MAJOR REPAIR.Oct 5, 2014 · N681FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201410053160Floor Panel · crackedMDC COMPARTMENT FLOOR PANEL BETWEEN FRAME 58 - 60 LT SIDE BETWEEN BL Y450 & Y953 CRACKED AROUND FLOOR ADAPTOR. REMOVED & INSTALLED PANEL IAW AMM 53-10-25-04-02. FABRICATED NEW PANEL ON T14 1097704 IAW DWG SRZ-25-005. CLASSIFIED AS CAT A MAJOR REPAIR.Oct 5, 2014 · N681FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201406171480Transformer · malfunctionedJUST AFTER GEAR RETRACTION, RECEIVED MULTIPLE AVIONIC FAILURES. AP 1 WOULD NOT ENGAGE, AP 2 ALREADY DEFER RED, OFF FLAGS IN BOTH ALTIMETERS, AUTO THROTTLES WOULD NOT ENGAGE, ROLLED BACK ON CLIMB OUT. BOTH FLIGHT DIRECTORS FAILED, NAV ADC FAILURE ECAM. ECAMJun 17, 2014 · N681FE · Airbus A300F4605R · Navigation SystemSDR FDEA201402100296Rib · corrodedRIGHT MLG RIB 5, FWD LUG, BORE, FWD & AFT FACES HAVE CORROSION. REPAIRED IAW EA 6-5710-TO305974A.Feb 10, 2014 · N681FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA201402090290Rib · corrodedLEFT MLG RIB 5, FWD LUG, FWD & AFT FACE HAS CORROSION. COMPLIED WITH EA 6-5710-T0305976 .Feb 9, 2014 · N681FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA201308131847Uplock · failedNOSE GEAR DOOR UNSAFE AMBER LIGHT ON BOTH PANELS AND BOTH SYS 1 AND 2 AT GEAR RETRACTION ON DEPARTURE. RAN QRH CHECK LIST WHICH DIRECTED NOT TO CYCLE GEAR WITH INCREASED FUEL CONSUMPTION ELECTED TO RETURN TO DEPARTURE UNSAFE NOSE GEAR DOOR LIGHT REMAINED ONAug 13, 2013 · N681FE · Airbus A300F4605R · Landing Gear Position and WarningSDR FDEA201209133318Altimeter · failedAT CRUISE FL350, CAPTAIN'S ALTIMETER OFF FLAG. ADC SWITCH DID NOT SOLVE FAILURE. ALTIMETER RETURNED TO NORMAL. REPLACED ALTIMETER IAW MM 34-12-21-04 AND ALL CHECKED NORMAL IAW MM 34-10-00-05.Sep 13, 2012 · N681FE · Airbus A300F4605R · Altimeter, Barometric/EncoderSDR FDEA201206092173Skin · corrodedLT WING OTBD FLAP OTBD T/E TIP STATIC DISCHARGER HAS CORROSION IN AND AROUND FLAP SKIN UPPER SURFACE. DEFECT MEASURES 2 SQ" AFTER REMOVAL OF LEVEL 1 CORROSION IAW SRM 51-74-10, AREA WAS FOUND TO BE OUT OF LIMITS IAW SRM 57-50-00, PG 118, FIG 103. REPAIRED ARJun 9, 2012 · N681FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201206072134Seat Track · corrodedMDCC FR28 SEAT-TRACK RT 3 INBD UPPER FLANGE HAS 1S QIN OF CORROSION. AFTER REMOVAL OF LEVEL 1 CORROSION SEAT-TRACK 3 RT WAS FOUND TO BE OUT OF LIMITS IAW FSRM 53-10-16, FIG 102. R & R SEAT TRACK SECTION IAW FSRM 53-10-16, FIG 208A.Jun 7, 2012 · N681FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201206042085Seat Track · corrodedSEAT TRACK 5R CORRODED SEVEN PLACES BETWEEN FR 14 - FR 16 AT BOTH LT & RT FLANGES. R & R SEAT TRACK IAW SRM 51-40-21, PGS 6-45.Jun 4, 2012 · N681FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201206042083Floorbeam · dentedFLOORBEAM ABOVE DUMMY TRACK BETWEEN SEAT TRACK 2L-3L DENTED APPROX L=1.0"X W=1.0" AND TORN AT LOWER FLANGE APPROX L=0.5" AT FR 11 UNDER COCKPIT DOOR. REMOVED DAMAGED SECTION AND PERFORMED A FORMED SECTION REPAIR IAW SRM 51-71-40, PARA 3.Jun 4, 2012 · N681FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201206042082Floorbeam · dentedFLOORBEAM ABOVE DUMMY TRACK BETWEEN SEAT TRACK 2L-3L DENTED APPROX L=1.0"XW=1.0" AND TORN AT LOWER FLANGE APPROX L=0.5" AT FR 11 UNDER COCKPIT DOOR. REMOVED DAMAGED AND PERFORMED A FORMED SECTION REPAIR IAW SRM 51-71-40, PARA 3.Jun 4, 2012 · N681FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201206012052Seat Track · corrodedMDCC FR26 SEAT TRACK 6R INBD UPPER FLANGE HAS 1.5 SQUARE INCHES OF CORROSION. AFTER REMOVAL OF LEVEL 1 CORROSION WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. REMOVED SEAT TRACK SECTION IAW SRM 53-10-16 PG. 250.Jun 1, 2012 · N681FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201205312035Bracket · corrodedMAIN DECK CARGO FR 27 BETWEEN SEAT TRACKS 3 L AND 4 L THRUST PLATE HAS AREA OF CORROSION APPOX 2 SQUARE INCHES. REMOVED CORRSION FROM THRUST PLATE AT FR 27 BETWEEN TRACK 3L AND 4L IAW SRM 51-74-10, PG 205. MATERIAL LOSS IS 0.30 BEFORE 0.079 AFTER .049. FOUNMay 31, 2012 · N681FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201205312034Floorboard · damagedMAIN DECK CARGO AT ZONE 230 FLOORBOARD 231 CF UPPER SURFACE HAS GOUGE & PUNCTURED (4 SQUARE INCHES) & TWO INSERT WASHERS WORN FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.May 31, 2012 · N681FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201205312033Seat Track · corrodedFR 27 SEAT TRACK 3R HAS 2 EA AREAS OF CORROSION. 1ST 1/2 SQUARE INCH AND 2ND 1/2 SQUARE INCH. REMOVED CORROSION IAW SRM 51-74-10, P 205 0.020. MATERIAL LOSS IS OUT OF LIMITS IAW FSRM 53-10-16 FIG 102. CUT OUT DAMAGED SECTION AND REPAIRED IAW SRM 53-10-16 FIG 2May 31, 2012 · N681FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201205312032Bracket · corrodedFR 26 TO FR 28 THRUST PLATE BETWEEN SEAT TRACK 4R AND 5 R HAS 7 EA AREAS OF CORROSION EA APPROX 1 SQUARE INCH. REMOVED CORROSION IAW SRM 51-74-10 P 205. MATERIAL LOSS 0.21 IS OUT OF DWG A53781984 TOLERANCE. REMOVED AND FABRICATED NEW THRUST BRACKET IAW DWD May 31, 2012 · N681FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201205312031Floorboard · damagedFLOORBOARD 232FG FWD, CUT & PUNCTURED (3 INCHES LONG) ONE INSERT WASHER MISSING & FIVE INSERTS WASHERS WORN FABRICATED REPLACEMENT FLOORBOARD IAW DWG SRZ 25-005, REV J.May 31, 2012 · N681FE · Airbus A300F4605R · Fuselage Floor Panel
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