N679FE

Service difficulty reports · 176

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 = 'N679FE' 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 FDEA201404160740Skin Panel · gougedLEFT WING INBD FLAP UPPER SURFACE HAS SEVERAL GOUGES. WINGS FLIGHT SURFACES LT WING INBD FLAP UPPER SURFACE REPAIR ACCOMPLISHED EA 6-5750-T0307300 P1 CAT A MAJOR REPAIR.Apr 16, 2014 · N679FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201404120721Web · deformedEMPENNAGE, ACCESS THRU 312AR BETWEEN FRAME 86 & FRAME 87, STRINGER 33L, WEB FLANGE DEFORMED. REMOVED, FABRICATED, LOCATED & DRILLED & INSTALLED NEW WEB FLANGE IAW SRM 51-40-21, 51-40-44, 51-20-10, 51-75-10 & STAM TRAVELER T14 1059529, MAT 2024-T3 .032C BATCH Apr 12, 2014 · N679FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201404120720Web · deformedEMPENNAGE, ACCESS THRU 312AR BETWEEN FRAME 86 & FRAME 87, STRINGER 39R WEB FLANGE DEFORMED. REMOVED, FABRICATED, LOCATED & DRILLED & INSTALLED NEW WEB FLANGE IAW SRM 51-40-21, 51-40-44, 51-20-10, 51-75-10 & STAM TRAVELER T14 1059528, MAT 2024-T3 .032C BATCH 0Apr 12, 2014 · N679FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201404100711Mount · corrodedNR 1 ENG FWD MOUNT, PYRAMID, ATTACHMENT BOLT HOLES, FOUR EACH ARE PITTED. LOCALLY BLENDED THREE EACH HOLES, INBD FWD & AFT, ALSO OTBD FWD HOLE IAW-SRM-54-51-81 TO A MAX .942, WITHIN LIMITS. AFT OTBD HOLE REAMED HOLE TO .997 WITH CORROSION REMOVED, PROTECApr 10, 2014 · N679FE · Airbus A300F4605R · Nacelle/Pylon, Attach FittingsSDR FDEA201404100707Web · deformedEMPENNAGE, ACCESS THRU 312AR BETWEEN FRAME 86 & FRAME 87, STRINGER 33R, WEB FLANGE DEFORMED. REMOVED & INSTALLED WEB FLANGE FABRICATED BY STAM TRAVELER T14 1059600 FROM MATERIAL 2024-T3 032C IAW DWG A53986751 & SRM 51-40-21.Apr 10, 2014 · N679FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201404100706Web · deformedEMPENNAGE, ACCESS THRU 312AR BETWEEN FRAME 85 & FRAME 86, STRINGER 33R, WEB FLANGE DEFORMED. REMOVED & INSTALLED WEB FLANGE, STRAP, FABRICATED BY STAM TRAVELER T14 1059526 FROM MATERIAL 2024-T3 032C IAW DWG A53986751 & SRM 51-40-21.Apr 10, 2014 · N679FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201404060673Floor Panel · damagedMAIN DECK CARGO FLOOR PANEL 241TJ CORNER AREA BROKEN & MISSING PIECE. FABRICATED NEW FLOOR PANEL IAW SRZ 25-005.Apr 6, 2014 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201404060674Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 241AJ CRACKED. FABRICATED NEW FLOOR PANEL 241AJ PN R532B371500000 IAW SRZ 25-005 ON STAM TRAVELER T14 1059959.Apr 6, 2014 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201404060672Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 242EK CRACKED FABRICATED NEW FLOOR PANEL 242EK PN R532B373200100 IAW SRZ 25-005 ON STAM TRAVELER T14 1059955.Apr 6, 2014 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201404060671Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 241GK CRACKED. FABRICATED NEW FLOOR PANEL 241GK PN R532B372300000 IAW SRZ 25-005 ON STAM TRAVELER T14 1059956.Apr 6, 2014 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201404060670Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 242QJ CRACKED. FABRICATED NEW FLOOR PANEL 242QJ PN R532B372700100 IAW SRZ 25-005 ON STAM TRAVELER T14 1059953.Apr 6, 2014 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201404060669Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 242VJ CRACKED. FABRICATED NEW FLOOR PANEL 242VJ PN R532B370300000 IAW SRZ 25-005 ON STAM TRAVELER T14 1059957.Apr 6, 2014 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201404050668Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 241TH HAS CRACK. FABRICATED NEW FLOOR PANEL 241TH PN R532B372500000 IAW SRZ 25-005 ON STAM TRAVELER T14 1059960.Apr 5, 2014 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201404050666Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 242ZJ HAS CRACK. FABRICATED NEW FLOOR PANEL 242ZJ PN R532B371700100 IAW SRZ 25-005 ON STAM TRAVELER T14 1059954.Apr 5, 2014 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201404050665Floor Panel · damagedMAIN DECK CARGO COMPARTMENT FLOOR PANEL 241ZH HAS PUNCTURED TOP SURFACE MID SIDE AREA. PANEL RACK, FABRICATED NEW PANEL 241ZH PN R532B371600000 IAW SRZ 25-005 ON STAM TRAVELER T14 1060136.Apr 5, 2014 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201404050664Floor Panel · crackedMAIN DECK CARGO FLOOR PANEL 241WH HAS CRACK. FABRICATED NEW FLOOR PANEL 241WH PN R532B370700000 IAW SRZ 25-005 ON STAM TRAVELER T14 1060028.Apr 5, 2014 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201404010679Floorboard · crackedMAIN CABIN FLOORBOARD 252ZF CRACKED. FABRICATED NEW PNL 252ZF PN R532B382800600 IAW SRZ 25-005 ON STAM TRAVELER T14 1060138.Apr 1, 2014 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109213990Skin · dentedRT WING INNER FLAP T/E LOWER SKIN WAS FOUND A PREVIOUS DENT ABOUT 3.5" X 1" BETWEEN RIB 27 AND RIB 28A. CUT OUT THE DENTED AREA AND MEASURED THE DIMENSION OF THE CUTOUT AREA & FABRICATED REPAIR EXTERNAL PLATE AND INSTALLED IAW SRM 57-50-00 FIG. 205. REPAIR CSep 21, 2011 · N679FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201109213991Floor Support · corrodedFWD MAIN DECK UTILITY AREA FOUND LONGITUDINAL FLOOR SUPPORT CORROSION AT FR 12A 4" AND Y 725 POS AFTER FLOOR PANEL REMOVAL. REPLACED THE DAMAGED FLOOR SUPPORT IAW. SRM 51-72-10 AND 51-40-21. THE REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Sep 21, 2011 · N679FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201109213989Bracket · crackedINSP OF APU OIL COOLER BRACKET FOUND CRACKED AT AFT OTBD CORNER ABOUT .7500". REPAIRED IAW EA 6-4910-155444. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Sep 21, 2011 · N679FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201109203972Floor Panel · damagedBULK CGO COMPT 161JF EDGE AND UPPER SKIN GOT IMPACT DAMAGE. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM, IRM 9701 AND DWG 17 A532 79960.Sep 20, 2011 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109183951Floor Panel · damagedM/D COMP'T AFT REMOVED 242EK FLOOR PANEL INSP CHECK FOUND UPPER SKIN AND EDGE AREA GOT IMPACT DAMAGED. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG 15 B532 70614.Sep 18, 2011 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109183950Floor Panel · damagedM/D COMP'T AFT REMOVED 242ZJ FLOOR PANEL INSP CHECK FOUND UPPER SKIN AND EDGE AREA GOT IMPACT DAMAGED. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG 15 B532 70609.Sep 18, 2011 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109183949Floor Panel · damagedMAIN DECK COMPARTMENT AFT REMOVED 242QJ FLOOR PANEL INSP CHECK, FOUND UPPER SKIN AND EDGE AREA GOT IMPACT DAMGED. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG NR 15 B532 70600.Sep 18, 2011 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109183948Floor Panel · damagedMAIN DECK COMPARTMENT AFT REMOVED 242GF FLOOR PANEL INSP CHECK FOUND UPPER SKIN AND EDGE AREA GOT IMPACT DAMAGED. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG 14 B532 70480.Sep 18, 2011 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109183947Floor Panel · damagedMAIN DECK COMPARTMENT AFT REMOVED 242MF FLOOR PANEL INSPECTION CHECK FOUND UPPER SKIN ADN EDGE AREA GOT IMPACT DAMAGED. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG 17 B532 70337.Sep 18, 2011 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109183946Floor Panel · damagedMAIN DECK COMPARTMENT AFT REMOVED 242RG FLOOR PANEL. INSPECTION CHECK FOUND UPPER SKIN AND EDGE AREA GOT IMPACT DAMAGED. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG 15 B532 70620.Sep 18, 2011 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109183945Floor Panel · damagedMAIN DECK COMPARTMENT AFT REMOVED 242VG FLOOR PANEL, INSP CHECK FOUND UPPER SKIN AND EDGE AREA GOT IMPACT DAMAGED. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG 16 B532 70260.Sep 18, 2011 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109183944Floor Panel · damagedMAIN DECK COMPARTMENT AFT REMOVED 241TH FLOOR PANEL AND INSP CHECK FOUND UPPER SKIN AND EDGE AREA GOT IMPACT DAMAGED. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG NR 15 B532 70600.Sep 18, 2011 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109183943Floor Panel · damagedMAIN DECK COMPARTMENT AFT REMOVED 241AJ FLOOR PANEL AND INSP CHECK FOUND UPPER SKIN AND EDGE AREA GOT IMPACT DAMAGED. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG 15 B532 70609.Sep 18, 2011 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109183942Floor Panel · damagedMAIN DECK COMPARTMENT AFT REMOVED 252UH FLOOR PANEL AND INSP CHECK FOUND UPPER SKIN AND EDGE AREA GOT IMPACT DAMAGED. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG 17 B532 70337.Sep 18, 2011 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109183941Floor Panel · damagedMAIN DECK COMPARTMENT AFT REMOVED 252PH FLOOR PANEL AND INSP CHECK FOUND UPPER SKIN AND EDGE AREA GOT IMPACT DAMAGED. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG 16 B532 70260.Sep 18, 2011 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109183940Floor Panel · damagedMAIN DECK COMPARTMENT AFT REMOVED 252BF FLOOR PANEL AND INSP CHECK FOUND UPPER SKIN AND EDGE AREA GOT IMPACT DAMAGED. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG 16 B532 70262.Sep 18, 2011 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109183939Floor Panel · damagedMAIN DECK COMPARTMENT AFT REMOVED 241GJ FLOOR PANEL AND INSP CHECK. FOUND UPPER SKIN AND EDGE AREA GOT IMPACT DAMAGED. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG 15 B532 70620.Sep 18, 2011 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109183938Floor Panel · damagedMAIN DECK COMPARTMENT AFT REMOVED 242SF FLOOR PANEL INSP CHECK FOUND UPPER SKIN AND EDGE AREA GOT IMPACT DAMAGED. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG 15 B532 70618.Sep 18, 2011 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109183937Floor Panel · damagedMAIN DECK COMPARTMENT AFT REMOVED 251PH FLOOR PANEL AND INSP CHECK. FOUND UPPER SKIN AND EDGE AREA GOT IMPACT DAMAGED. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG 17 B532 70276.Sep 18, 2011 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109183936Floor Panel · damagedMAIN DECK COMPARTMENT AFT REMOVED 252VF FLOOR PANEL AND INSP CHECK, FOUND UPPER SKIN AND EDGE AREA GOT IMPACT DAMAGED. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG 17 B532 70339.Sep 18, 2011 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109183935Floor Panel · damagedMAIN DECK COMPARTMENT AFT REMOVED 252WH FLOOR PANEL AND INSP CHECK FOUND UPPER SKIN AND EDGE AREA GOT IMPACT DAMAGED. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG NR 17 B532 70278.Sep 18, 2011 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109183934Floor Panel · damagedMAIN DECK COMPARTMENT AFT REMOVED 251BH FLOOR PANEL AND INSP CHECK, FOUND UPPER SKIN AND EDGE AREA GOT IMPACT DAMAGED. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG 17 B532 70287.Sep 18, 2011 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109183933Floor Panel · damagedMAIN DECK COMPARTMENT AFT REMOVED 251VF FLOOR PANEL AND INSPECTION CHECK FOUND UPPER SKIN AND EDGE AREA GOT IMPACT DAMAGED. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG 17 B532 70339.Sep 18, 2011 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109183932Floor Panel · damagedMAIN DECK COMPARTMENT AFT REMOVED 251YG FLOOR PANEL AND INSP CHECK FOUND UPPER SKIN AND EDGE AREA GOT IMPACT DAMAGED. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG NR 17 B532 70281.Sep 18, 2011 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109183931Floor Panel · damagedMAIN DECK COMPARTMENT AFT REMOVED 251WH FLOOR PANEL AND INSPECTED. FOUND UPPER SKIN AND EDGE AREA HAS IMPACT DAMAGE. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW FLOOR PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG 17 B532 70278.Sep 18, 2011 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109183930Floor Panel · damagedMAIN DECK COMPARTMENT AFT REMOVED 251UH FLOOR PANEL AND INSPECTED, FOUND UPPER SKIN AND EDGE AREA HAS IMPACT DAMAGE. THE DAMAGED AREA IS OVER ALLOWABLE LIMITS. FABRICATED A NEW FLOOR PANEL REF TO AB6F SRM 53-10-20, IRM 9701 AND DWG 17 B532 70337.Sep 18, 2011 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109173922Floor Panel · damagedM/D COMP'T AFT REMOVED 242BF FLOOR PANEL INSPECTION CHECK FOUND UPPER SKIN AND EDGE AREA IMPACT DAMAGED. THE DAMAGED AREA IS OVER THE ALLOWABLE DAMAGE LIMITS . FABRICATED A NEW PANEL REFER TO AB6F SRM 53-10-20, IRM 9701 AND DWG B532 70478. THE REPAIR CLASSIFSep 17, 2011 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109173921Floor Panel · damagedM/D COMP'T AFT REMOVED 241QH FLOOR PANEL AND INSPECTION CHECK FOUND UPPER SKIN AND EDGE AREA RECEIVED IMPACT DAMAGED. THE DAMAGED AREA IS NOT WITHIN ALLOWABLE DAMAGE LIMITS. FABRICATED A NEW PANEL REFER TO AB6F SRM 53-10-20, IRM 9701 AND DG 15 B532 70 618. Sep 17, 2011 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109173920Floor Panel · damagedM/D COMP'T AFT REMOVED 231AH FLOOR PANEL INSP CHECK FOUND UPPER SKIN AND EDGE AREA IMPACT DAMAGED. THE DAMAGED AREA IS NOT WITHIN THE ALLOWABLE DAMAGE LIMITS. FABRICATED A NEW PANEL REFER TO AB6F SRM 53-10-20, IRM 9701, AND DWG 14 B532 70476. THE REPAIR ESep 17, 2011 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109173919Floor Panel · damagedM/D COMP'T AFT REMOVED 242UJ FLOOR PANEL INSP CHECK FOUND UPPER SKIN AND EDGE AREA GOT IMPACT DAMAGED. THE DAMAGED AREA IS OVER THE ALLOWABLE DAMAGE LIMITS. FABRICATED A NEW PANEL REFER TO AB6F SRM 53-10-20, IRM 9701, AND DWG 15 B532 70604. THE REPAIR EVALUSep 17, 2011 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109173918Floor Panel · damagedM/D COMPARTMENT AFT REMOVED 232YG FLOOR PANEL INSP CHECK FOUND UPPER SKIN AND EDGE AREA IMPACT DAMAGED. THE DAMAGED AREA IS NOT WITHIN THE ALLOWABLE DAMAGE LIMITS. FABRICATED A NEW PANEL REFER TO AB6F SRM 53-10-20, AND DWG 14 B532 70506. THE REPAIR CLASSIFISep 17, 2011 · N679FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201109073732Skin · corrodedFWD CARGO COMPARTMENT BILGE AREA OF S45R SKIN CORRODED BETWEEN FR 38.2 AND FR 39 POSITION.Sep 7, 2011 · N679FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201109073734Floor Panel · damagedBULK CARGO COMPARTMENT 161GF FLOOR PANEL EDGE AREA GOT IMPACT DAMAGED. MEASURED THE DAMAGED AREA IS 15 1/2"X DIA. IS NOT WITHIN THE ALLOWABLE DAMAGED LIMITS. FABRICATED A NEW FLOOR PANEL WITH THE EDGE FILLER, INSERTS AND ADHESIVE IAW SRM 53-10-20, AND DWG 17ASep 7, 2011 · N679FE · Airbus A300F4605R · Fuselage Floor Panel
Back to N679FE