N583FE

Service difficulty reports · 461

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 = 'N583FE' 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 FDEA201901100074Seat Track · corrodedMAIN DECK FLOOR SEAT TRACK AT STATION 1311 X= 75.25 FOUND CORROSION AS MARKED. MAIN DECK FLOOR SEAT TRACK AT STATION 1311 X = 75.25 CORROSION REMOVED AND FOUND EXCEEDED LIMITED AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. SEAT TRACK REPAIR CARRIED OJan 10, 2019 · N583FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201901100073Seat Track · crackedMAIN DECK FLOOR SEAT TRACK AT STATION 635 X= -8.5 FOUND CRACKED AS MARKED. MAIN DECK FLOOR CRACKED SEAT TRACK AT STATION 635 X = - 8.5 CARRIED OUT REPAIR AS PER STRUCTURE REPAIR MANUAL 53-00-52-2R FIGURE 201 REPAIR 1 FROM STATION 625 TO STATION 705 X= -8.5. RJan 10, 2019 · N583FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201901100072Seat Track · crackedMAIN DECK FLOOR SEAT TRACK AT STATION 695 X= -8.5 FOUND CRACKED AS MARKED. MAIN DECK FLOOR CRACKED SEAT TRACK AT STATION 695 X = -8.5 CARRIED OUT REPAIR AS PER STRUCTURE REPAIR MANUAL 53-00-52-2R FIGURE 201 REPAIR 1 FROM STATION 625 TO STATION 705 X= -8.5. REJan 10, 2019 · N583FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201901090064Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT STATION 635 X = 8.5 FOUND CROWN DAMAGED MAIN DECK FLOOR SEAT TRACK AT STATION 635 X= 8.5 DAMAGED CROWN MEASURED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. SEAT TRACK CARRIED OUT REPAIR AT STATJan 9, 2019 · N583FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201901090063Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT STATION 755 X = 8.5 FOUND CROWN ELONGATED AS MARKED. MAIN DECK FLOOR SEAT TRACK AT STATION 755 X= 8.5 ELONGATED CROWN AREA CARRIED OUT REPAIR FROM STATION 745 TO 788 X= 8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSJan 9, 2019 · N583FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201901090062Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT STATION 770 X = 75.25 FOUND CROWN ELONGATED. MAIN DECK FLOOR SEAT TRACK AT STATION 770 X= 75.25 ELONGATED CROWN AREA CARRIED OUT REPAIR FROM STATION 769 TO 788 X= 75.25 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIEDJan 9, 2019 · N583FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201901090061Seat Track · crackedMAIN DECK FLOOR SEAT TRACK AT STATION 635 X = -27.5 FOUND CRACKED MAIN DECK FLOOR SEAT TRACK AT STATION 625 TO STATION 665 X=-27.5 CARRIED OUT REPAIR AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jan 9, 2019 · N583FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201901090060Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT STATION 1531 X = - 47.5 FOUND CROWN DAMAGED MAIN DECK FLOOR SEAT TRACK AT STATION 1531 X =-47.5 DAMAGED CROWN AREA MEASURED AND FOUND EXCEEDED LIMIT PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. SEAT TRACK REPAIR CARRIED OUT Jan 9, 2019 · N583FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201901090059Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT STATION 1531 X = 8.5 FOUND CROWN DAMAGED MAIIN DECK FLOOR SEAT TRACK AT STATION 1531 X= 8.5 DAMAGED CROWN MEASURED AND FOUND EXCEEDED LIMIT PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE1. SEAT TRACK REPAIR CARRIED OUT FROM STATIJan 9, 2019 · N583FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201901090058Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT STATION 1282 X = - 8.5 FOUND CROWN DAMAGED MAIN DECK FLOOR SEAT TRACK AT STATION 1282 X = -8.5 DAMAGED CROWN AREA REMOVED AND FOUND EXCEEDED LIMIT AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. SEAT TRACK REPAIR CARRIED OUTJan 9, 2019 · N583FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201901090057Seat Track · damagedMAIN DECK FLOOR SEAT TRACK AT STATION 1282 X = 8.5 FOUND CROWN DAMAGED MAIN DECK FLOOR SEAT TRACK AT STATION 1282 X = 8.5 DAMAGED CROWN AREA MEASURED AND FOUND EXCEEDED LIMITED AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. SEAT TRACK REPAIR AT STATIOJan 9, 2019 · N583FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201901090056Skin · crackedDURING HIGH FREQUENCY EDDY CURRENT INSPECTION AT RIGHT HAND WING FIXED LEADING EDGE SKIN ADJACENT TO CUTOUT, CRACK INDICATION FOUND APPROXIMATELY 0.4" IN LENGTH AS MARKED AT CORNER NR 11 FUEL ACCESS DOOR AT FORWARD INBOARD CORNER AT XOS 610. REPAIR CARRIED OUTJan 9, 2019 · N583FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201901090055Doubler · crackedLEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT XOS 632 FOUND CRACK. REPAIR CARRIED OUT ON LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 632 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jan 9, 2019 · N583FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201901090054Doubler · crackedLEFT WING - FIXED LEADING EDGE RIB DOUBLER AT XOS 789 FOUND CRACK RIB DOUBLER ON LEFT WING - FIXED LEADING EDGE AT STATION XOS 789 REMOVED AND REPLACED AS PER SRM 51-31-01-0G. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. DOUBLER FABRICATED AS PER DRAWING ARB395Jan 9, 2019 · N583FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201901090053Doubler · crackedRIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT XOS 792 FOUND CRACK REPAIR CARRIED OUT ON RIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 792 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jan 9, 2019 · N583FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201901090052Doubler · crackedRIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT XOS 640 FOUND CRACK REPAIR CARRIED OUT ON RIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 640 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jan 9, 2019 · N583FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201901090051Doubler · crackedRIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT XOS 785 FOUND CRACK REPAIR CARRIED OUT ON RIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 785 AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Jan 9, 2019 · N583FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201901090065Doubler · crackedRIGHT WING - LEADING EDGE LOWER SURFACE FORWARD DOUBLER AT XOS 891 FOUND CRACK REPAIR CARRIED OUT ON RIGHT WING LEADING EDGE LOWER SURFACE FORWARD DOUBLER AT STATION XOS 891 AS PER SRM 57-40-03-2R FIGURE 201 REPAIR 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100Jan 9, 2019 · N583FE · Doug MD11F · Wing, Plate/SkinSDR FDEA201803040583Power Supply · inoperativeDURING PREFLIGHT EMERGENCY LIGHT TEST, RECEIVED A LEVEL 1 EMERGENCY LIGHT BATTERY LOW ALERT. REPLACED THE POWER SUPPLY IAW AMM 33-51-01-4, OPS TESTED OK & NO FAULT MESSAGE.Mar 4, 2018 · N583FE · Doug MD11F · Emergency LightingSDR FDEA201801260244Battery Pack · no testAFTER EMER LT. TEST: LVL 1 ALERT EMERGENCY LIGHT BATTERY LOW. REPLACEMENT OF EMERGENCY LIGHT BATTERY, OPS CHECKED GOOD.Jan 26, 2018 · N583FE · Doug MD11F · Emergency LightingSDR FDEA201711103238Warning System · false activationON PREFLIGHT DURING EMERGENCY LIGHT TEST GOT "EMER LT BAT 1 LO" DISPLAYED. PERFORMED OPERATIONAL TEST 4 TIMES, ALL OPS NORMAL. NO HISTORY IN 30 DAYS. REF AMM 33-51-01-5.Nov 10, 2017 · N583FE · Doug MD11F · Emergency LightingSDR FDEA201711103218Battery · faultedDURING PREFLIGHT, DURING AN EMERGENCY LIGHT TEST RECEIVED AN EMERGENCY LIGHT BATTERY 1 LOW DISPLAYED. PERFORMED AN OPERATIONAL TEST 4 TIMES, ALL OPS NORMAL. NO HISTORY IN 30 DAYS. IAW AMM 33-51-01-5Nov 10, 2017 · N583FE · Doug MD11F · Emergency LightingSDR FDEA201703070803Hinge Bracket · corrodedRT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR ATTACH INBOARD BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09 EXISTING HOLE DIA 1.218", FINAL HOLE DIA 1.226", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZED BUSHINGMar 7, 2017 · N583FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201703070802Hinge Bracket · corrodedRT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR ATTACH OUTBOARD BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 1.218", FINAL HOLE DIA 1.226" MAXIMUM ALLOWABLE HOLE DIA 1.220", OVERSIZED BUSHING Mar 7, 2017 · N583FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201703070801Hinge Bracket · corrodedRT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD BORE SURFACE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09. EXISTING THICKNESS 0.402" , MATERIAL REMOVED 0.008", REMAINING THICKNESS 0.394". MINIMUM ALLOWABLMar 7, 2017 · N583FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201703070800Hinge Bracket · corrodedRT WING OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) ACTUATOR ATTACH INBOARD BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIAMETER 1.220 INCH; FINAL HOLE DIAMETER 1.234 INCH; MAXIMUM ALLOWABLE DIAMETER 1.220 INCMar 7, 2017 · N583FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201703070799Hinge Bracket · corrodedRT WING OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) ACTUATOR ATTACH OUTBOARD BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIAMETER 1.220 INCH; FINAL HOLE DIAMETER 1.234 INCH; MAXIMUM ALLOWABLE DIAMETER 1.220 INMar 7, 2017 · N583FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201703070798Hinge Bracket · corrodedLT WING OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) ACTUATOR ATTACH OUTBOARD BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIAMETER 1.219 INCH; FINAL HOLE DIAMETER 1.226 INCH; MAXIMUM ALLOWABLE DIAMETER 1.220 INMar 7, 2017 · N583FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201703070797Hinge Bracket · corrodedLT WING OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) ACTUATOR ATTACHED INBOARD BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08. EXISTING HOLE DIAMETER 1.219 INCH; FINAL HOLE DIAMETER 1.226 INCH; MAXIMUM ALLOWABLE DIAMETER 1.220 IMar 7, 2017 · N583FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201703070796Hinge Bracket · corrodedLT WING OUTBOARD FLAP INBOARD FORWARD HINGE (WING SIDE) FORWARD MOUNT OUTBOARD LUG SURFACE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-08. EXISTING THICKNESS: 0.380" MATERIAL REMOVED: 0.003" REMAINING THICKNESS: 0.377" MINIMUM ALLOWABLEMar 7, 2017 · N583FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201703070795Hinge Bracket · corrodedLT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR ATTACH OUTBOARD BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 1.218", FINAL HOLE DIA 1.222", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZED BUSHINGMar 7, 2017 · N583FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201703070794Hinge Bracket · corrodedLT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) ACTUATOR ATTACH INBOARD BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44--09 EXISTING HOLE DIA 1.281", FINAL HOLE DIA 1.285", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZED BUSHING Mar 7, 2017 · N583FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201703070793Hinge Bracket · corrodedLT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) BARREL NUT LOWER BOLT H0LE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIAMETER 0.406 INCH; FINAL HOLE DIAMETER 0.422 INCH; MAXIMUM ALLOWABLE DIAMETER 0.391 INCHMar 7, 2017 · N583FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201703070792Hinge Bracket · corrodedLT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) BARREL NUT UPPER BOLT HOLE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44--09 EXISTING HOLE DIA 0.405", FINAL HOLE DIA 0.422", MAXIMUM ALLOWABLE HOLE DIA 0.391". OVERSIZED BUSHING FAMar 7, 2017 · N583FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201703070791Hinge Bracket · corrodedLT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT INBOARD BORE SURFACE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09. EXISTING THICKNESS 0.410", MATERIAL REMOVED 0.005", REMAINING THICKNESS 0.405". MINIMUM ALLOWABLE Mar 7, 2017 · N583FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201703070790Hinge Bracket · corrodedLT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) PIVOT BORE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09. EXISTING HOLE DIA 2.316", FINAL HOLE DIA 2.320", MAXIMUM ALLOWABLE HOLE DIA 2.3135". OVERSIZED BUSHING FABRICATED AND IMar 7, 2017 · N583FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201703060782Hinge Bracket · corrodedLT WING OUTBOARD FLAP OUTBOARD FORWARD HINGE (WING SIDE) LOWER MOUNT OUTBOARD BORE SURFACE CORROSION. HINGE REWORKED AND FOUND EXCEEDED LIMIT AS PER CMM 57-44-09. EXISTING THICKNESS 0.405", MATERIAL REMOVED 0.005", REMAINING THICKNESS 0.400". MINIMUM ALLOWABLEMar 6, 2017 · N583FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201703030755Seat Track · crackedMAIN DECK CARGO COMPT FLOOR SEAT TRACK AT STA 6-96, X=-8.5 FOUND CRACKED. MAIN DECK CRACKED FLOOR SEAT AT STA 6-96, X=-8.5 REPAIRED BY SECTIONAL SEAT TRACK REPLACEMENT FROM STA 6-60 TO STA 6-100, X=-8.5 AS PER SRM 53-00-52-2R FIGURE 201 REPAIR 1. REPAIR CLASSMar 3, 2017 · N583FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201703030756Seat Track · corrodedMAIN DECK CARGO COMPT FLOOR SEAT TRACK AT STA 1139, X=- 8.5 FOUND CORROSION AS MARKED. MAIN DECK CORRODED FLOOR SEAT TRACK AT STA 1139, X=- 8.5 REPAIRED BY SECTIONAL REPLACEMENT FROM STA 6-100 TO STA 1149, X= - 8.5 AS PER SRM 53-00-02-2R FIG 201 REPAIR 1. REPMar 3, 2017 · N583FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201702280686Panel · corrodedUPON MAIN DECK RIGID CARGO BARRIER REMOVAL, FOUND RCB FLOOR SUPPORT PANEL P/N: WSP0785-501 AT STA 488, X= -27.5 TO X= -36 WITH CORROSION. MAIN DECK RIGID CARGO BARRIER CORRODED FLOOR SUPPORT PANEL P/N: WSP0785-501 AT STA 488, X= -27.5 TO X= -36 REMOVED PER AMMFeb 28, 2017 · N583FE · Doug MD11F · Fuselage Floor PanelSDR FDEA201702280683Panel · corrodedUPON MAIN DECK RIGID CARGO BARRIER REMOVAL, FOUND RCB FLOOR SUPPORT PANEL P/N: WSP0785-502 AT STA 488, X= 27.5 TO X= 36 WITH CORROSION. MAIN DECK RIGID CARGO BARRIER CORRODED FLOOR SUPPORT PANEL P/N: WSP0785-502 AT STA 488, X= 27.5 TO X= 36. REMOVED AS PER AMMFeb 28, 2017 · N583FE · Doug MD11F · Fuselage Floor PanelSDR FDEA201702280682Panel · corrodedUPON MAIN DECK RIGID CARGO BARRIER REMOVAL, FOUND RCB FLOOR SUPPORT PANEL P/N: WSP0785-501 AT STA 488, X= 19 TO X= 27.5 WITH CORROSION. MAIN DECK RIGID CARGO BARRIER CORRODED FLOOR SUPPORT PANEL P/N: WSP0785-501 AT STA 488, X= 19 TO X= 27.5. REMOVED AS PER AMMFeb 28, 2017 · N583FE · Doug MD11F · Fuselage Floor PanelSDR FDEA201702280681Panel · corrodedUPON MAIN DECK RIGID CARGO BARRIER REMOVAL, FOUND RCB FLOOR SUPPORT PANEL P/N: WSP0786-501 AT STA 488, X=8.5 TO X= 19 WITH CORROSION. MAIN DECK RIGID CARGO BARRIER CORRODED FLOOR SUPPORT PANEL P/N: WSP0786-501 AT STA 488, X= 8.5 TO X= 19. REMOVED AS PER AMM 53Feb 28, 2017 · N583FE · Doug MD11F · Fuselage Floor PanelSDR FDEA201702280680Panel · corrodedUPON MAIN DECK RIGID CARGO BARRIER REMOVAL, FOUND RCB FLOOR SUPPORT PANEL P/N: WSP0785-501 AT STA 488, X= 0.0 TO X= 8.5 WITH CORROSION. MAIN DECK RIGID CARGO BARRIER CORRODED FLOOR SUPPORT PANEL P/N: WSP0785-501 AT STA 488, X= 0.0 TO X= 8.5 REMOVED AS PER AMM Feb 28, 2017 · N583FE · Doug MD11F · Fuselage Floor PanelSDR FDEA201702280679Panel · corrodedUPON MAIN DECK RIGID CARGO BARRIER REMOVAL, FOUND RCB FLOOR SUPPORT PANEL P/N: WSP0785-502 AT STA 488, X= 0.0 TO X= -8.5 WITH CORROSION. MAIN DECK RIGID CARGO BARRIER CORRODED FLOOR SUPPORT PANEL P/N: WSP0785-502 AT STA 488, X= 0.0 TO X= -8.5 REMOVED AS PER AMFeb 28, 2017 · N583FE · Doug MD11F · Fuselage Floor PanelSDR FDEA201702280678Panel · corrodedUPON MAIN DECK RIGID CARGO BARRIER REMOVAL, FOUND RCB FLOOR SUPPORT PANEL P/N: WSP0785-501 AT STA 488, X= -8.5 TO X= -17 WITH CORROSION. MAIN DECK RIGID CARGO BARRIER CORRODED FLOOR SUPPORT PANEL P/N: WSP0785-501 AT STA 488, X= -8.5 TO X= -17 REMOVED PER AMM 5Feb 28, 2017 · N583FE · Doug MD11F · Fuselage Floor PanelSDR FDEA201702280677Panel · corrodedUPON MAIN DECK RIGID CARGO BARRIER REMOVAL, FOUND RCB FLOOR SUPPORT PANEL P/N: WSP0786-501 AT STA 488, X= -17 TO X= -27.5 WITH CORROSION. MAIN DECK RIGID CARGO BARRIER CORRODED FLOOR SUPPORT PANEL PN: WSP0786-501 AT STA 488, X= -17 TO X= -27.5 REMOVED PER AMM Feb 28, 2017 · N583FE · Doug MD11F · Fuselage Floor PanelSDR FDEA201702280676Panel · corrodedUPON MAIN DECK RIGID CARGO BARRIER REMOVAL, FOUND RCB FLOOR SUPPORT PANEL P/N: WSP0790-502 AT STA 488, X= -75.25 TO X= -86.25 WITH CORROSION. MAIN DECK RIGID CARGO BARRIER CORRODED FLOOR SUPPORT PANEL P/N: WSP0790-502 AT STA 488, X= -75.25 TO X= -86.25 REMOVEFeb 28, 2017 · N583FE · Doug MD11F · Fuselage Floor PanelSDR FDEA201702280685Floor Panel · corrodedMAIN DECK RIGID CARGO BARRIER FLOOR SUPPORT PANEL AT STA 485, X=-36 TO X=-47.5 CORRODED AS MARKED. REMOVED AND REPLACED WITH NEW FLOOR SUPPORT PANEL AS PER AMM 53-21-10-2. REPAIR CLASSIFIED MAJOR PER GMM 6-2-100. CORROSION ON FLOOR SUPPORT PANEL EXCEEDED LIMITFeb 28, 2017 · N583FE · Doug MD11F · Fuselage Floor PanelSDR FDEA201702280684Floor Panel · corrodedMAIN DECK RIGID CARGO BARRIER FLOOR SUPPORT PANEL AT STA 485, X=86.25 TO X= 107.25 CORROSION AS MARKED. REMOVED AND REPLACED WITH NEW FLOOR SUPPORT PANEL AS PER AMM 53-21-10-2. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100. CORROSION ON FLOOR SUPPORT PANEL EXCEEDFeb 28, 2017 · N583FE · Doug MD11F · Fuselage Floor Panel
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