N588FE

Service difficulty reports · 346

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 = 'N588FE' 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 FDEA202009142196Spar · crackedDURING ULTRASONIC INSPECTION FOR VERTICAL CRACKS BEHIND SERVICE REPAIR SR10550013, PER DRAWING NUMBER SN10550000 ON RIGHT HAND SIDE OF THE LOWER VERTICAL STABILIZER FORWARD FLANGE OF UPPER REAR SPAR CAP, STATION Y=2164, CRACK INDICATION FOUND ON THIRD FASep 14, 2020 · N588FE · Doug MD11F · Vertical Stabilizer, Spar/RibSDR FDEA202009142207Skin · crackedHIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND WING FIXED LEADING EDGE SKIN ADJACENT TO ACCESS DOOR CORNER 5 FOUND CRACK APPROXIMATELY 2.2 INCHES AT XOS 490 . RIGHT HAND WING FIXED LEADING EDGE SKIN ADJACENT TO ACCESS DOOR CORNER 5 AT XOS 490 REPSep 14, 2020 · N588FE · Doug MD11F · Wing, Plate/SkinSDR FDEA202009142203Doubler · crackedRIGHT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER AT XOS 700 FOUND CRACK . RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT DOUBLER AT XOS 700 REPAIR CARRIED OUT AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15 . REPAIR CLASSIFIED AS MAJOR PER GMM Sep 14, 2020 · N588FE · Doug MD11F · Wing, Plate/SkinSDR FDEA202009142206Doubler · crackedLEFT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER AT XOS 682 FOUND CRACK. LEFT HAND WING FIXED LEADING EDGE COMPARTMENT DOUBLER AT XOS 682 REPAIR CARRIED OUT, AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100Sep 14, 2020 · N588FE · Doug MD11F · Wing, Plate/SkinSDR FDEA202009142205Doubler · crackedLEFT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER AT XOS 618 FOUND CRACK. LEFT HAND WING FIXED LEADING EDGE COMPARTMENT DOUBLER AT XOS 618 REPAIR CARRIED OUT, AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100Sep 14, 2020 · N588FE · Doug MD11F · Wing, Plate/SkinSDR FDEA202009142204Doubler · crackedLEFT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER AT XOS 614 FOUND CRACK. LEFT HAND WING FIXED LEADING EDGE COMPARTMENT DOUBLER AT XOS 614 REPAIR CARRIED OUT, AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100Sep 14, 2020 · N588FE · Doug MD11F · Wing, Plate/SkinSDR FDEA202009142202Doubler · crackedLEFT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER AT XOS 688 FOUND CRACK. LEFT HAND WING FIXED LEADING EDGE COMPARTMENT DOUBLER AT XOS 688 REPAIR CARRIED OUT, AS PER SRM 57-40-02-2R FIGURE 203 REPAIR 15. REPAIR CLASSIFIED AS MAJOR, PER GMM 6-2-100Sep 14, 2020 · N588FE · Doug MD11F · Wing, Plate/SkinSDR FDEA202009142201Skin · crackedLEFT HAND WING FIXED LEADING EDGE SLAT TRACK OUTBOARD AFT CUT OUT SKIN AT XOS 892 FOUND CRACK. LEFT HAND WING FIXED LEADING EDGE SLAT TRACK OUTBOARD AFT CUT OUT SKIN AT XOS 892 REPAIRED, AS PER SRM 57-40-02-2R FIGURE 201 REPAIR 7. REPAIR CLASSIFIED AS MAJOR Sep 14, 2020 · N588FE · Doug MD11F · Wing, Plate/SkinSDR FDEA202009142200Trunnion · crackedHIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON RIGHT HAND NOSE LANDING GEAR TRUNNION FITTING, STATION 583 EXISTING TRIMMED OUT AREA FOUND CRACK APPROXIMATELY 0.4 INCHES. CRACKED NOSE LANDING GEAR RIGHT HAND TRUNNION FITTING AT STATION Y=583 REPAIRED, ASep 14, 2020 · N588FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR FDEA202009142199Trunnion · crackedHIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON LEFT HAND NOSE LANDING GEAR TRUNNION FITTING, STATION 583 EXISTING TRIMMED OUT AREA FOUND CRACK APPROXIMATELY 0.45 INCHES. CRACKED NOSE LANDING GEAR LEFT HAND TRUNNION FITTING AT STATION Y=583 REPAIRED, ASSep 14, 2020 · N588FE · Doug MD11F · Fuselage, Landing Gear Attach FittingsSDR FDEA202009132190Floor Panel · delaminatedFWD CABIN, FOUND FLOOR PANEL 232FF AT STATION 595 TO STA 675 DELAMINATED. DELAMNATED FLOOR PANEL 232FF AT FOWARD CABIN STATION 595 TO STATION 675 REMOVED, AS PER AMM 53-21-04-4. FLOOR PANEL 232FF FABRICATED, AS PER FEDEX DRAWING SRZ-25-005 REVISION R. FABRISep 13, 2020 · N588FE · Doug MD11F · Fuselage Floor PanelSDR FDEA202009122178Seat Track · wornMAIN DECK CARGO COMPARTMENT-CABIN, FOUND SEAT TRACK CROWN WORN AT STATION 1015 X=47.5. MAIN DECK CARGO COMPARTMENT-CABIN AT SEAT TRACK STATION 1015 X=47.5, WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CSep 12, 2020 · N588FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202009122177Seat Track · wornMAIN DECK CARGO COMPARTMENT-CABIN, FOUND SEAT TRACK CROWN WORN AT STATION 1015, X= -27.5 MAIN DECK CARGO COMPARTMENT-CABIN AT SEAT TRACK STATION 1015, X= -27.5, WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1Sep 12, 2020 · N588FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202009122176Seat Track · wornMAIN DECK CARGO COMPARTMENT CABIN, FOUND SEAT TRACK CROWN WORN AT STATION 6-10, X= -47.5. MAIN DECK CARGO COMPARTMENT-CABIN AT SEAT TRACK STATION 6-10, X= -47.5, WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101. ALLOWABLE DAMASep 12, 2020 · N588FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202009112169Seat Track · wornMAIN DECK CARGO COMPARTMENT, FOUND SEAT TRACK CROWN WORN AT STATION 879, X= -47.5. MAIN DECK CARGO COMPARTMENT-CABIN, AT SEAT TRACK STATION 879, X = -47.5 WORN CROWN EVALUATED AND FOUND EXCEEDED LIMIT, AS PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. CRSep 11, 2020 · N588FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2020061211186Tire · low pressureTIRE PRESS LO LEVEL ALERT AT LRMSE. PRES WENT DOWN TO 56 PSI NR 5 TIRE. REMOVED AND REPLACED NR 5 AND NR 6 TIRE DUE TO NR 5 TIRE LOW PRESSURE. NO DAMAGE NOTED TO LEFT MAIN LANDING GEAR. TIRES CHANGED IAW AMM 32-41-01-4. OK FOR SERVICE.Jun 11, 2020 · N588FE · Doug MD11F · TireSDR FDEA2018090512320Hinge Bracket · corrodedRT WING O/B FLAP ASSY I/B FWD HINGE (WING SIDE) LOWER MOUNT O/B BORE CORROSION. HINGE LOWER MOUNT O/B BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08, EXISTING HOLE DIA 0.705", FINAL HOLE DIA 0.722" MAXIMUM ALLOWABLE HOLE DIA 0.709". SHOULDER BUSHINAug 31, 2018 · N588FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018090512319Hinge Bracket · corrodedRT WING O/B FLAP ASSY I/B FWD HINGE (WING SIDE) UPPER MOUNT O/B BORE CORROSION. HINGE UPPER MOUNT O/B BORE (NR 2 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08, EXISTING HOLE DIA 0.944", FINAL HOLE DIA 0.950" MAXIMUM ALLOWABLE HOLE DIA 0.944". OVERAug 31, 2018 · N588FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018090512318Hinge Bracket · corrodedLT WING O/B FLAP ASSY I/B FWD HINGE (WING SIDE) PIVOT BORE CORROSION. HINGE PIVOT BORE(NR 4 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA: 2.309", FINAL HOLE DIA: 2.315", MAXIMUM ALLOWABLE DIA: 2.3135. OVERSIZE BUSHING FABRICATED ANAug 31, 2018 · N588FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018090512316Hinge Bracket · corrodedLT WING O/B FLAP ASSY I/B FWD HINGE (WING SIDE) UPPER MOUNT O/B BORE CORROSION. HINGE UPPER MOUNT O/B BORE (NR 2 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA: 0.943", FINAL HOLE DIA: 0.9465", MAXIMUM ALLOWABLE DIA: 0.944. OVERSIZE Aug 31, 2018 · N588FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018090512315Hinge Bracket · corrodedLT WING O/B FLAP ASSY I/B FWD HINGE (WING SIDE) LOWER MOUNT O/B BORE CORROSION. HINGE (WING SIDE) LOWER MOUNT O/B BORE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA: 0.709", FINAL HOLE DIA: 0.712", MAXIMUM ALLOWABLE DIA: 0.709Aug 31, 2018 · N588FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018090512314Hinge Bracket · corrodedLT WING O/B FLAP ASSY I/B FWD HINGE (WING SIDE) ACTUATOR ATTACH I/B BORE CORROSION. HINGE ACTUATOR ATTACH I/B BORE (NR 8 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA: 1.2105", FINAL HOLE DIA: 1.222", MAXIMUM ALLOWABLE DIA: 1.220. OAug 31, 2018 · N588FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018090512312Hinge Bracket · corrodedRT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) ACTUATOR ATTACH O/B BORE CORROSION. HINGE ACTUATOR ATTACHED OUTBD BORE (NR 8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09, EXISTING HOLE DIA 1.220", FINAL HOLE DIA 1.224" MAXIMUM ALLOWABLE HOLE DIA 1Aug 31, 2018 · N588FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018090512311Hinge Bracket · corrodedRT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) ACTUATOR ATTACH I/B BORE CORROSION. HINGE ACTUATOR ATTACHED INBD BORE (NR 8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09, EXISTING HOLE DIA 1.2205", FINAL HOLE DIA 1.224" MAXIMUM ALLOWABLE HOLE DIA 1Aug 31, 2018 · N588FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018090512309Hinge Bracket · corrodedRT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) BARREL NUT UPPER BOLT HOLE CORROSION. HINGE BARREL NUT UPPER BOLT HOLE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09, EXISTING HOLE DIA 0.327", FINAL HOLE DIA 0.406" MAXIMUM ALLOWABLE HOLE DIA Aug 31, 2018 · N588FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018090512308Hinge Bracket · corrodedRT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) LOWER MOUNT O/B BORE SURFACE CORROSION. HINGE LOWER MOUNT OUTBD BORE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09, EXISTING THICKNESS 0.408", MATERIAL REMOVED FWD FACE 0.004", AFT FACE 0.011", REMAug 31, 2018 · N588FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018090512307Hinge Bracket · corrodedRT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) LOWER MOUNT I/B BORE SURFACE CORROSION. HINGE LOWER MOUNT INBD BORE SURFACE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09, EXISTING THICKNESS 0.408", MATERIAL REMOVED FWD FACE 0.004", AFT FACE 0.014", REMAIAug 31, 2018 · N588FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018090512305Hinge Bracket · corrodedRT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) LOWER MOUNT O/B BORE CORROSION. HINGE LOWER MOUNT OUTBD BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09, EXISTING HOLE DIA 0.596", FINAL HOLE DIA 0.612" MAXIMUM ALLOWABLE HOLE DIA 0.584", SHAug 31, 2018 · N588FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018090502293Hinge Bracket · corrodedRT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) LOWER MOUNT I/B BORE CORROSION. HINGE LOWER MOUNT INBD BORE REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09, EXISTING HOLE DIA 0.596", FINAL HOLE DIA 0.599" MAXIMUM ALLOWABLE HOLE DIA 0.584", SHOULDER BUSHIAug 30, 2018 · N588FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018090502292Hinge Bracket · corrodedLT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) ACTUATOR ATTACH I/B BORE CORROSION. HINGE (WING SIDE) ACTUATOR ATTACH I/B BORE (NR 8 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA: 1.231", FINAL HOLE DIA: 1.252", MAXIMUM ALLOWABLE DIAug 30, 2018 · N588FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018090502291Hinge Bracket · corrodedLT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) BARREL NUT HOLE CORROSION. HINGE BARREL NUT HOLE (NR 10 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA: 0.678", FINAL HOLE DIA: 0.707", MAXIMUM ALLOWABLE DIA: 0.667. OVERSIZE BUSHING FAAug 30, 2018 · N588FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018083102290Hinge Bracket · corrodedLT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) BARREL NUT HOLE SURFACE CORROSION. HINGE BARREL NUT HOLE SURFACE REWORKED AS PER CMM 57-44-09. EXISTING THICKNESS UPPER: 0.408"; LOWER: 0.408", MATERIAL REMOVED: UPPER: 0.012"; LOWER: 0.012", REMAINING THICKNESAug 30, 2018 · N588FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018083102289Hinge Bracket · corrodedLT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) BARREL NUT LOWER BOLT HOLE CORROSION. HINGE BARREL NUT LOWER BOLT (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09, EXISTING HOLE DIA 0.390", FINAL HOLE DIA 0.410" MAXIMUM ALLOWABLE HOLE DIA 0.39Aug 30, 2018 · N588FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018083102288Hinge Bracket · corrodedLT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) BARREL NUT UPPER BOLT HOLE CORROSION. HINGE BARREL NUT UPPER BOLT HOLE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA: 0.390", FINAL HOLE DIA: 0.410", MAXIMUM ALLOWABLE DIA: 0.391Aug 30, 2018 · N588FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018083102287Hinge Bracket · corrodedLT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) LOWER MOUNT O/B BORE CORROSION. HINGE LOWER MOUNT O/B BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA: 0.595", FINAL HOLE DIA: 0.611", MAXIMUM ALLOWABLE DIA: 0.584. SHOULDER BAug 30, 2018 · N588FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018083102286Hinge Bracket · corrodedLT WING O/B FLAP ASSY O/B FWD HINGE (WING SIDE) LOWER MOUNT I/B BORE CORROSION. HINGE LOWER MOUNT I/B BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA: 0.587", FINAL HOLE DIA: 0.611", MAXIMUM ALLOWABLE DIA: 0.584. SHOULDER BAug 30, 2018 · N588FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018083102285Skin · corrodedRT WING OUTBD ISLAND AREA UPPER T/E SURFACE STA XORS 1070 FOUND CORROSION. CORRODED SKIN REPAIRED AS PER EA 1-5730-T0341923 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Aug 30, 2018 · N588FE · Doug MD11F · Wing, Plate/SkinSDR FDEA2018083102284Skin · corrodedRT WING OUTBD AILERON AREA UPPER T/E SURFACE STA XORS 1040 FOUND CORROSION. CORRODED SKIN REPAIRED AS PER EA 1-5730-T0341923 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Aug 30, 2018 · N588FE · Doug MD11F · AileronsSDR FDEA2018083102282Skin · crackedLOWER VERTICAL STABILIZER LT SIDE IN FRONT OF NR 2 ENGINE FAN COWL DOOR JAMB UPPER AREA APPROX STA 2164 FOUND SKIN CRACK. CRACKED SKIN REPAIRED AS PER EA 1-5530-T0341902 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Aug 30, 2018 · N588FE · Doug MD11F · Vertical Stabilizer, Plate/SkinSDR FDEA2018083102281Skin · crackedLOWER VERTICAL STABILIZER RT SIDE IN FRONT OF NR 2 ENGINE FAN COWL DOOR JAMB UPPER AREA APPROX STA 2164 FOUND SKIN CRACK. CRACKED SKIN REPAIRED AS PER EA 1-5530-T0341903 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Aug 30, 2018 · N588FE · Doug MD11F · Vertical Stabilizer, Plate/SkinSDR FDEA2018083102280Hinge Bracket · corrodedLT WING I/B FLAP ASSY O/B FWD HINGE (WING SIDE) ACTUATOR ATTACH O/B BORE CORROSION. HINGE (WING SIDE) ACTUATOR ATTACH O/B BORE REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-07. EXISTING HOLE DIA: 1.064", FINAL HOLE DIA: 1.1065", MAXIMUM ALLOWABLE DIA: 1.0935Aug 30, 2018 · N588FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA2018083102273Hinge Bracket · wornLT WING I/B FLAP ASSY O/B FWD HINGE (WING SIDE) PIVOT BUSHING WORN. WORN BUSHING AT FWD HINGE (WING SIDE) PIVOT BORE, REMOVED AND BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T0332025 A PART 1 STEP 1F (1) AND STEP 1F (3). REPAIR CLASSIFIED AS MAJOR PER GAug 30, 2018 · N588FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201808292261Hinge · wornRT WING I/B FLAP ASSY O/B FWD HINGE (WING SIDE) PIVOT BUSHING WORN. WORN BUSHING REMOVED AND BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-07 AND EA 1-5750-T0332026 A PART 1 STEP 1F(1) AND STEP 1F(3). REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Aug 29, 2018 · N588FE · Doug MD11F · Wing, Control Surface Attach FittingsSDR FDEA201808292260Hinge · corrodedLT WING I/B FLAP ASSY O/B AFT HINGE (FLAP SIDE) PIVOT O/B BORE CORROSION. HINGE PIVOT O/B BORE (HOLE A & B) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. EXISTING HOLE DIA: 1.255", FINAL HOLE DIA: 1.283", MAXIMUM ALLOWABLE DIA: 1.220. OVERSIZE BUSHING FABRAug 29, 2018 · N588FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201808292259Hinge Bracket · corrodedLT WING I/B FLAP ASSY O/B AFT HINGE (FLAP SIDE) PIVOT I/B BORE CORROSION. HINGE PIVOT INBD BORE (HOLE G & F) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. EXISTING HOLE DIA: 1.282", FINAL HOLE DIA: 1.326", MAXIMUM ALLOWABLE DIA: 1.220. OVERSIZE BUSHING FABAug 29, 2018 · N588FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201808292258Hinge Bracket · corrodedRT WING I/B FLAP ASSY O/B AFT HINGE (FLAP SIDE) PIVOT O/B BORE CORROSION. HINGE PIVOT OUTBD BORE (HOLE B & A) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. EXISTING HOLE DIA: 1.218", FINAL HOLE DIA: 1.251", MAXIMUM ALLOWABLE DIA: 1.220. OVERSIZE BUSHING Aug 29, 2018 · N588FE · Doug MD11F · Trailing Edge FlapsSDR FDEA201808292257Hinge Bracket · corrodedRT WING I/B FLAP ASSY O/B AFT HINGE (FLAP SIDE) PIVOT I/B BORE CORROSION. HINGE PIVOT INBD BORE (HOLE G & F) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-52-03. EXISTING HOLE DIA: 1.2565", FINAL HOLE DIA: 1.281", MAXIMUM ALLOWABLE DIA: 1.220Ï¿½. OVERSIZE BUSHIAug 29, 2018 · N588FE · Doug MD11F · Trailing Edge FlapsSDR FDEA2018082982211Skin · delaminatedRT WING NR 2 SPOILER PANEL UPPER SURFACE FOUND DELAMINATION, STA XOSP2 523 TO XOSP2 530. UPPER SURFACE REPAIRED AS PER EA 1-5750-T0341848 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Aug 28, 2018 · N588FE · Doug MD11F · SpoilersSDR FDEA2018082322152Seat Track · corrodedMAIN DECK RT AFT FLOOR CURVE SEAT TRACK AT STA 1901-2007 X=-107 FOUND CORROSION. CORROSION REMOVED AND EXCEEDED LIMIT PER SRM 53-00-52-1A FIGURE 101 ALLOWABLE DAMAGE 1. SEAT TRACK (CURVED) REPAIRED BY SECTIONAL REPLACEMENT FROM EXISTING SPLICE AT STA 1877 TOAug 22, 2018 · N588FE · Doug MD11F · Fuselage, Seat/Cargo Attach FittingsSDR FDEA2018082322163Seat Track · corrodedMAIN DECK SEAT TRACK AT BS 1791, LBL 8.5 WAS FOUND CORRODED. THE CORROSION WAS REMOVED AND FOUND EXCEEDED LIMITS IAW SRM 53-00-52-1A, FIGURE 101, ALLOWABLE DAMAGE 1. THE SEAT TRACK WAS REPAIRED BY A SECTIONAL REPLACEMENT FROM BS 1771 TO 1887, IAW SRM 53-00Aug 22, 2018 · N588FE · Doug MD11F · Fuselage, Seat/Cargo Attach Fittings
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