N683FE

Service difficulty reports · 289

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 = 'N683FE' 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 FDEA201604271387Floor Panel · damagedMDCC FLOOR PANEL 231YG DENTED & BROKEN INSERT. FABRICATED FLOOR PANEL 231YG ON T16 1204990 IAW SRZ 25-005. THIS REPAIR IS CLASSIFIED AS A CATEGORY A MAJOR REPAIR.Apr 27, 2016 · N683FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201604271386Floor Panel · puncturedMDCC FLOOR PANEL 232UG PUNCTURED. FABRICATED FLOOR PANEL 232UG ON T16 1205112 IAW SRZ 25-005. THIS REPAIR IS CLASSIFIED AS A CATEGORY A MAJOR REPAIR.Apr 27, 2016 · N683FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201604271385Floor Panel · damagedMDCC FLOOR PANEL 231DH PUNCTURED & DAMAGED. FABRICATED FLOOR PANEL 231DHF ON T16 1205162 IAW SRZ 25-005. THIS REPAIR IS CLASSIFIED AS A CATEGORY A MAJOR REPAIR.Apr 27, 2016 · N683FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201604271384Floor Panel · crackedMDCC FLOOR PANEL 252BF DENTED & CRACKED. FABRICATED FLOOR PANEL 252BF ON T16 1205228 IAW SRZ 25-005. THIS REPAIR IS CLASSIFIED AS A CATEGORY A MAJOR REPAIR.Apr 27, 2016 · N683FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201604271383Floor Panel · crackedPANEL 241UF HAS CRACKED AREA, MARKED FABRICATED FLOOR PANEL 241UF ON T16 1204825 IAW SRZ 25-005. THIS REPAIR IS CLASSIFIED AS A CATEGORY A MAJOR REPAIR.Apr 27, 2016 · N683FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201604271382Floor Panel · crackedMDCC FLOOR PANEL 242GF DENTED & CRACKED. FABRICATED FLOOR PANEL 242GF ON T16 1205252 IAW SRZ 25-005. THIS REPAIR IS CLASSIFIED AS A CATEGORY A MAJOR REPAIR.Apr 27, 2016 · N683FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201604271381Floor Panel · crackedMDCC FLOOR PANEL 252VF PUNCTURED & CRACKED. FABRICATED FLOOR PANEL 252VF ON T16 1205225 IAW SRZ 25-005. THIS REPAIR IS CLASSIFIED AS A CATEGORY A MAJOR REPAIR.Apr 27, 2016 · N683FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201604271380Floor Panel · crackedMDCC FLOOR PANEL 252GF DENTED & CRACKED. FABRICATED FLOOR PANEL 252GF ON T16 1205236 IAW SRZ 25-005. THIS REPAIR IS CLASSIFIED AS A CATEGORY A, MAJOR REPAIR.Apr 27, 2016 · N683FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201604261377Seat Track · corrodedMCD SEAT TRACK GOUGED BETWEEN FRAME 38 & 38.1, Y 0. REMOVED GOUGE & FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. CUT OUT SEAT TRACK SECTION Y 0, FRAME 38 - 38.2 IAW SRM 53-10-16 FIG 208. FABRICATED NEW SEAT TRACK SECTION PN 53274005-SFS-DAP. INSTALLED SEAT Apr 26, 2016 · N683FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201604261376Seat Track · corrodedMCD SEAT TRACK, BETWEEN FRAME 26 & 27, -Y1456 CORRODED. BLENDED AREA CORRODED & FOUND TO BE OUT OF LIMITS IAW SRM 53-10-13 FIG 102. REMOVED SECTION OF SEAT TRACK & FIVE EACH SPLICES IAW SRM 51-40-21. FABRICATED NEW SECTION OF SEAT TRACK PN A53274005-SFS-DAPApr 26, 2016 · N683FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201604231362Floor Support · corrodedMDC COURIER FLOOR SUPPORT FRAME 13A, Y730 CORRODED. REMOVED DAMAGE IAW SRM 51-74-10 CHECKED DIMENSIONS L=8.50', W=1.50', D=0.020', NO ESTABLISHED DAMAGE LIMITS FOUND IN SRM. R & R FLOOR SUPPORT IAW SRM 51-40-21. FABRICATED FLOOR SUPPORT ON T16 1204159.Apr 23, 2016 · N683FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201604231361Floor Panel · puncturedMAIN CABIN FLOOR PANEL 252MG HAS A PUNCTURE. FABRICATED FLOOR PANEL 252MG ON T16 1203466 IAW SRZ 25-005, CLASSIFIED CAT A MAJOR REPAIR.Apr 23, 2016 · N683FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201604231360Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 251 UH IS DELAMINATED. FABRICATED FLOOR PANEL 251UH ON T16 1203469 IAW SRZ 25-005, CLASSIFIED CAT A MAJOR REPAIR.Apr 23, 2016 · N683FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201604231359Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 251PH IS DELAMINATED. FABRICATED FLOOR PANEL 251PH ON T16 1203467 IAW SRZ 25-005, CLASSIFIED CAT A MAJOR REPAIR.Apr 23, 2016 · N683FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201604231358Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 251GF IS DELAMINATED. FABRICATED FLOOR PANEL 251GF ON T16 1203464 IAW SRZ 25-005, CLASSIFIED CAT A MAJOR REPAIR.Apr 23, 2016 · N683FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201604231357Floor Panel · puncturedMAIN CABIN FLOOR PANEL 251 RG HAS SEVERAL PUNCTURES. FABRICATED FLOOR PANEL 251RG ON T16 1203465 IAW SRZ 25-005, CLASSIFIED CAT A MAJOR REPAIR.Apr 23, 2016 · N683FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201604231356Floor Panel · puncturedMAIN CABIN FLOOR PANEL 251BH HAS A PUNCTURE. FABRICATED FLOOR PANEL 251BH ON T16 1203571 IAW SRZ 25-005, CLASSIFIED CAT A MAJOR REPAIR.Apr 23, 2016 · N683FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201604231355Floor Panel · puncturedMAIN CABIN FLOOR PANEL 251WH HAS SEVERAL PUNCTURES. FABRICATED FLOOR PANEL 251WH ON T16 1203468 IAW SRZ 25-005, CLASSIFIED CAT A MAJOR REPAIR.Apr 23, 2016 · N683FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201604231354Floor Panel · puncturedMAIN CABIN FLOOR PANEL 251RH HAS SEVERAL PUNCTURES. FABRICATED FLOOR PANEL 251RH ON T16 1203470 IAW SRZ 25-005, CLASSIFIED CAT A MAJOR REPAIR.Apr 23, 2016 · N683FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201604221353Floor Panel · puncturedMAIN CABIN FLOOR PANEL 251 NG HAS A PUNCTURE MARK. FABRICATED FLOOR PANEL 251NG ON T16 1203572 IAW SRZ 25-005, CLASSIFIED CAT A MAJOR REPAIR.Apr 22, 2016 · N683FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201411293980Rib · corrodedLEFT MLG RIB 5 FWD LUG HAS CORROSION IN BORE, FWD & AFT FACES. REPAIR COMPLETE, COMPLIED WITH EA 6-5710-T0313591 REV NO PS P1 WINGS BASIC STRUCTURE TERMINATING ACTION OF RIB 5 FWD LUG LT WING. MAJOR REPAIR.Nov 29, 2014 · N683FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA201411293979Rib · corrodedRIGHT MLG RIB 5 FWD LUG HAS CORROSION IN BORE, FWD & AFT FACES. COMPLIED WITH EA 6-5710-T0313592 P1 WING BASIC STRUCTURE TERMINATING ACTION OF RIB 5 FWD LUG RT WING. MAJOR REPAIR.Nov 29, 2014 · N683FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA201406121415Skin · damagedFUSELAGE SKIN EXTERNAL SURFACE DAMAGED BETWEEN FRAMES 64 - 65, STRINGERS 38 - 40R. SMOOTHED CHAFED AREA IAW SRM 51-73-10, CHECKED FOR CRACKS IAW NTM51-10-04, NO CRACKS FOUND. PERFORM ROTO TEST INSPECTION TO ALL OPEN HOLES IAW NTM 51-10-01, NO CRACKS FOUND. Jun 12, 2014 · N683FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201406051317Skin · damagedFUSELAGE SKIN EXTERNAL SURFACE DAMAGED BETWEEN FRAMES 63 - 64, STRINGERS 38 - 40R. REPAIRED IAW TD-K4-S1-46479-2014 & EA 6-5330-T0308681 P1.Jun 5, 2014 · N683FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201405211106Fitting · crackedFUSELAGE CTR WING BOX REAR SPAR & BOTTOM PANEL RT SIDE HOLE C FOUND CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0308679 PT1. MAJOR REPAIR IAW GMM 6-2-100.May 21, 2014 · N683FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201405211105Fitting · crackedFUSELAGE CTR WING BOX REAR SPAR & BOTTOM PANEL RT SIDE HOLE Q FOUND WITH A CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0308679 PT1. MAJOR REPAIR IAW GMM 6-2-100.May 21, 2014 · N683FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201405211104Skin · crackedFUSELAGE CTR WING BOX REAR SPAR & BOTTOM PANEL RT SIDE HOLE P FOUND CRACK SIGNAL. COMPLIED WITH EA 6-5710-T0308679 PT1. MAJOR REPAIR IAW GMM 6-2-100.May 21, 2014 · N683FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201405211103Fitting · crackedFUSELAGE CTR WING BOX REAR SPAR & BOTTOM PANEL LT SIDE HOLE P FOUND CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0308679 PT1. MAJOR REPAIR IAW GMM 6-2-100.May 21, 2014 · N683FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201405211102Frame · crackedJUNCTION BETWEEN CENTER WING BOX & CRUCIFORM FITTING BETWEEN FRAMES 40 - 44. RT FRAME 41+6 INCHES OTBD ONE FASTENER HOLE WITH CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0308784 PT1. MAJOR REPAIR IAW GMM 6-2-100.May 21, 2014 · N683FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201405211101Frame · crackedJUNCTION BETWEEN CTR WING BOX & CRUCIFORM FITTING BETWEEN FRAME 40 - 44. LT FRAME 43+8 INCHES OTBD ONE FASTENER HOLE HAS A CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0308784 PT1. MAJOR REPAIR IAW GMM 6-2-100.May 21, 2014 · N683FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201405211100Frame · crackedJUNCTION BETWEEN CTR WING BOX & CRUCIFORM FITTING BETWEEN FRAME 40 - 44. LT FRAME 44 7.5 INCHES OTBD ONE FASTENER HOLE WITH CRACK SIGNAL. REPAIRED IAW EA 6-5710-T0308784 PT1. MAJOR REPAIR IAW GMM 6-2-100.May 21, 2014 · N683FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201405171052Skin · crackedFRAME 40 SKIN FOUND CRACKED. REPAIRED IAW EA 6-5710-T0308785 PT1. MAJOR REPAIR IAW GMM 6-2-100.May 17, 2014 · N683FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201405171051Skin · crackedFRAME 40 SKIN CRACKED. REPAIRED IAW EA 6-5710-T0308785 PT1. MAJOR REPAIR IAW GMM 6-2-100.May 17, 2014 · N683FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201405171050Skin · crackedFRAME 40 SKIN CRACKED. REPAIRED IAW EA 6-5710-T0308785 PT1. MAJOR REPAIR IAW GMM 6-2-100.May 17, 2014 · N683FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201405171049Floorbeam · crackedMDCC CROSSBEAM CRACKED BETWEEN FRAME 42, Y-450 - Y-953. REMOVED AND REPLACED THE FLOORBEAM IAW AMM 20-21-12-00.May 17, 2014 · N683FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201310032382Jackscrew · inoperativeSLAT SYS 1 & 2 FAULTED ON SLAT EXTENSION, NO SLAT LIGHT ON SFP PANEL. WOULD NOT RESET WITH CYCLE PROCEDURE. EMERGENCY DECLARED. REPLACED NR 3 RIGHT L/E JACKSCREW PER MM 27-84-22-04. CYCLED SEVERAL TIMES WITH NO PROBLEMS, OPS CHECKED NORMAL. OK FOR SERVICOct 3, 2013 · N683FE · Airbus A300F4605R · Leading Edge Slat Control SystemSDR FDEA201203010710Line · chafedAT FL280 ECAM INDICATED LOSS OF GREEN HYD SYS QTY. OVERHEAD INDICATIONS WERE THE SAME. COMPLIED WITH ECAM AND QRH HYD SYS LOW LEVEL. DURING ROLLOUT, GREEN SYS QTY RETURNED TO NORMAL. EMERGENCY DECLARED. FOUND GREEN HYD PRESSURE LINE CHAFFED THRU. R & R LEMar 1, 2012 · N683FE · Airbus A300F4605R · Hydraulic System, MainSDR FDEA201201110092Web · corrodedFLOOR PRESSURE WEB BETWEEN SEAT TRACK 2L - 3L AT FR 26 HAS SURFACE CORROSION AT 3 LOCATIONS. REMOVED CORROSION FROM FLOOR PRESSURE WEB BETWEEN SEAT TRACK 2L - 3L AT FR 26, ORIGINAL THICKNESS OF MAT. IS .071", MAX MATERIAL REMOVED .018" ; FOUND TO BE OUT OF LIJan 11, 2012 · N683FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201201110087Bracket · corrodedFLOOR PRESSURE WEB BETWEEN SEAT TRACK 3L-4L AND FR 25 -FR 26 HAS SURFACE CORROSION AT 4 LOCATIONS. REMOVED CORROSION FROM FLOOR PRESSURE WEB BETWEEN SEAT TRACK 3L - 4L AT FR 25-26 AT 4 EA LOCATIONS. AREAS WHERE MATERIAL REMOVED FOUND TO BE OUT OF LIMITS. Jan 11, 2012 · N683FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201201100074Floorbeam · chafedMAIN DECK CARGO COMPARTMENT FROM FR 38.2 TO FR 39 BETWEEN SEAT TRACKS 5 RT AND 6 RT CROSSBEAM HAS CHAFE MARK. R & R DAMAGED CROSSBEAM WITH NEW PART IAW SRM 53-15-15, FIG 11 AND SRM 51-40-21.Jan 10, 2012 · N683FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201201060037Frame · damagedFRAME 21 HAS A .25 DRILL START BETWEEN STRINGERS 8R & 9R. CUTOUT DAMAGED SECTION OF FRAME AND SPLICED IN NEW SECTION IAW EA 6-5310-156080.Jan 6, 2012 · N683FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201201060034Floorbeam · crackedMAIN DECK FLOORBEAM CRACKED BETWEEN SEAT TRACK 2R & 3R UNDER CLEVIS ADAPTOR. REPAIRED FLOORBEAM IAW SRM 53-10-15.Jan 6, 2012 · N683FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201201060032Seat Track · corrodedMAIN DECK SEAT TRACK 5L, AT FRAME 27, HAS CORROSION ON FLANGE. CORROSION WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16, FIG 102, PG 105. REPAIRED SEAT TRACK IAW SRM 53-10-16, FIG 201A.Jan 6, 2012 · N683FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201201050028Skin · dentedRIGHT SIDE FRAME 65, HAS 2 DENTS IN SKIN. 1 DENT 4.0" L X 4.0" W X 0.05" DEEP. NR 2 DENT 7.0"L X 7.0" W X 0.05" DEEP. REPAIRED IAW SRM 53-10-12.Jan 5, 2012 · N683FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201201040017Lug · gougedLEFT MLG RIB 5 AFT LUG FWD FACE HAS .5" LONG GOUGE. BLENDED LT MLG RIB 5 FWD FACE EDGE IAW FSRM 51-73-00. NDT PERFORMED WITH NO CRACK INDICATIONS IAW NTM 51-10-108. COMPLETED EA 6-5710-156082 AND VERIFIED NO PREVIOUS WORK WAS PERFORMED TO LUG. REF EA6-5710-1Jan 4, 2012 · N683FE · Airbus A300F4605R · Wing, Landing Gear Attach FittingsSDR FDEA201201020003Floor Support · crackedFLOOR STRUCTURE, FR 38.1 TO 38.2 RT SIDE, OTBD OF SEAT TRACK 6R, FRAME TO FRAME TIE-IN GUSSET HAS A 2 INCH CRACK. REMOVED AND REPLACED DAMAGE SUPPORT WITH NEW PART IAW SRM 51-40-21 AND 51-72-10.Jan 2, 2012 · N683FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201112315463Door Frame · dentedFUSELAGE FWD CARGO DOOR CUTOUT, FR 20, STR 39, 4.5" X 1.5 X .090 DENT IN FRAME. PERFORMED REPAIR IAW EA 6-5310-156072.Dec 31, 2011 · N683FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201112315465Floor Support · crackedMAIN CABIN FLOOR STRUCTURE FR 38, FR TO 38.2 LT SIDE OTBD OF SEAT TRACK 6L FRAME TO FRAME TIE IN GUSSET HAS 2" CRACK. REMOVED GUSSET TIE IN/SUPPORT IAW SRM 51-40-21, LOCATED AND DRILLED SUPPORT IAW SRM 51-72-10. INSTALLED SUPPORT IAW SRM 51-40-21 AND 51-72Dec 31, 2011 · N683FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201112315464Floor Support · crackedMAIN CABIN FLOOR STRUCTURE FR 38 TO FR 38.1 RT SIDE OTBD OF SEAT TRACK 6R FR TO FR TIE IN GUSSET HAS 2" CRACK. REMOVED GUSSET TIE-IN/SUPPORT IAW SRM 51-40-21, LOCATED AND DRILLED SUPPORT IAW SRM 51-72-10. INSTALLED SUPPORT IAW SRM 51-40-21 AND 51-72-10.Dec 31, 2011 · N683FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201112295457Web · corrodedFLOOR PRESSURE WEB BETWEEN SEAT TRACK 4L AND 5L AND BETWEEN FR'S 26 AND 27 HAS SURFACE CORROSION AT 5 LOCATIONS. R & R WEB IAW SRM 51-72-10.Dec 29, 2011 · N683FE · Airbus A300F4605R · Fuselage Miscellaneous Structure
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