N613FE

Service difficulty reports · 422

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 = 'N613FE' 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 04FDEA02270Skin Panel · corrodedLEFT HAND WING UPPER SURFACE TRAILING EDGE PANEL FORWARD EDGE FOUND BULGING AT OUTBOARD OF NR 5 SPOILER XORS 827. REMOVED AS PER SRM 51-21-01, VOLUME II, MATERIAL THICKNESS=0.270, MATERIAL REMAINED=0.231, MATERIAL REMOVED=0.039 FOUND WITHIN LIMIT (0.054) ASJul 28, 2004 · N613FE · Doug MD11 · Wing, Plate/SkinSDR 04FDEA02269Barrel Nut · corrodedLEFT HAND NR 27 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79810, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 27L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EJul 28, 2004 · N613FE · Doug MD11 · FastenersSDR 04FDEA02268Barrel Nut · corrodedLEFT HAND NR 29 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79809, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 29L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EJul 28, 2004 · N613FE · Doug MD11 · FastenersSDR 04FDEA02267Barrel Nut · corrodedLEFT HAND NR 1 BARREL NUT CORROSION REMOVED ON BORE AREA FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79820, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 1L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO Jul 28, 2004 · N613FE · Doug MD11 · Horizontal Stabilizer StructureSDR 04FDEA02208Structure · corrodedLEFT HAND HORIZONTAL STABILIZER NR 28L BARREL NUT BORE FOUND WITH CORROSION. CLEANED UP CORROSION AND FOUND EXCEEDED LIMIT PER MD11 SB. REPAIRED AS PER FEDEX EA NR 1-5510-80302, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 28L - CORROSION RJul 28, 2004 · N613FE · Doug MD11 · Horizontal Stabilizer StructureSDR 04FDEA02207Structure · corrodedLEFT HAND HORIZONTAL STABILIZER NR 24L BARREL NUT BORE FOUND WITH CORROSION. CLEANED UP CORROSION AND FOUND EXCEEDED LIMIT PER MD11 SB. REPAIRED AS PER FEDEX EA NR 1-5510-80303, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 24L - CORROSION RJul 28, 2004 · N613FE · Doug MD11 · Horizontal Stabilizer StructureSDR 04FDEA02206Structure · corrodedRIGHT HAND NR 1 BARREL NUT CORROSION REMOVED ON BORE AREA, FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79824, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 1R - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EJul 28, 2004 · N613FE · Doug MD11 · Horizontal Stabilizer StructureSDR 04FDEA02205Structure · corrodedLEFT HAND NR 20 BARREL NUT CORROSION REMOVED ON BORE AREA, FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79833, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 20L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX Jul 28, 2004 · N613FE · Doug MD11 · Horizontal Stabilizer StructureSDR 04FDEA02204Structure · corrodedLEFT HAND NR 18 BARREL NUT CORROSION REMOVED ON BORE AREA, FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79803, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 18L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX Jul 28, 2004 · N613FE · Doug MD11 · Horizontal Stabilizer StructureSDR 04FDEA02203Structure · corrodedLEFT HAND NR 16 BARREL NUT CORROSION REMOVED ON BORE AREA, FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79823, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 16L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEJul 28, 2004 · N613FE · Doug MD11 · Horizontal Stabilizer StructureSDR 04FDEA02202Structure · corrodedLEFT HAND NR 6 BARREL NUT CORROSION REMOVED ON BORE AREA, FOUND EXCEEDED LIMITS. REPAIRED AS PER FEDEX EA NR 1-5510-79827, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 6L - CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EOJul 28, 2004 · N613FE · Doug MD11 · Horizontal Stabilizer StructureSDR 04FDEA02201Structure · corrodedLEFT HAND NR 2 BARREL NUT CORROSION REMOVED ON BORE AREA, FOUND EXCEEDED LIMITS. CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7-5000.Jul 28, 2004 · N613FE · Doug MD11 · Horizontal Stabilizer StructureSDR 04FDEA02200Structure · corrodedRIGHT HAND HORIZONTAL STABILIZER NR 5R BARREL NUT BORE FOUND WITH CORROSION. CLEANED UP CORROSION AND FOUND EXCEEDED LIMIT PER MD11 SB. CORROSION REPAIR PER BOEING S/B MD-11 55-023 REVISION 2 AND FEDEX EO 1-5510-7- 5000.Jul 28, 2004 · N613FE · Doug MD11 · Horizontal Stabilizer StructureSDR 04FDEA02199Structure · corrodedRT HORIZONTAL STABILIZER NR 13R BARREL NUT BORE FOUND WITH CORROSION. CLEANED UP CORROSION AND FOUND EXCEEDED LIMIT PER MD11 SB. REPAIRED AS PER FEDEX EA NR 1-5510-79830, TITLE: STABILIZERS - HORIZONTAL STABILIZER - BARREL NUT BORE NR 13R - CORROSION REPAIR Jul 28, 2004 · N613FE · Doug MD11 · Horizontal Stabilizer StructureSDR 04FDEA02195Structure · corrodedLEFT HAND HORIZONTAL STABILIZER NR 14L BARREL NUT BORE FOUND WITH CORROSION. CLEANED UP CORROSION AND FOUND EXCEEDED LIMIT PER MD11 SB. REMOVED AND REPLACED AS PER SRM 51-33-01, VOLUME II.Jul 27, 2004 · N613FE · Doug MD11 · Horizontal Stabilizer StructureSDR 04FDEA02194Structure · corrodedLEFT HAND HORIZONTAL STABILIZER 26L BARREL NUT BORE FOUND WITH CORROSION. REMOVED AND REPLACED AS PER SRM 51-33-01, VOLUME II.Jul 27, 2004 · N613FE · Doug MD11 · Horizontal Stabilizer StructureSDR 04FDEA02160Fitting · crackedAFT FUSELAGE COMPT STA 2007 RIGHT HAND X=-10 VERTICAL SUPPORT FITTING MOST END SUSPECT CRACKED. CUT AND REMOVED AS PER SRM 53-00-01, FIGURE 8, VOLUME I. REPAIR ANGLES FABRICATED AS PER SRM 53-00-01, FIGURE 8, VOLUME I, T-SECTION MACHINED AS PER FEDEX E.Jul 22, 2004 · N613FE · Doug MD11 · Fuselage Main, Attach FittingsSDR 04FDEA02146Seat Track · corrodedMAIN DECK, RIGHT HAND MOST OUTBOARD SEAT TRACK CORRODED AT R1 DOORWAY. REMOVED LAVATORY ON MAIN DECK AS PER AMM 25-41-06-4. REMOVED AND REPLACED RIGHT HAND MOST OUTBOARD SEAT TRACK AT R1 DOORWAY AS PER SRM 51-35-01, VOLUME II. REINSTALLED LAVATORY MODULE ASJul 21, 2004 · N613FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02147Seat Track · corrodedMAIN DECK, LEFT HAND MOST OUTBOARD SEAT TRACK CORRODED AT L1 DOORWAY. CORRODED SEAT TRACK AT MAIN DECK, LEFT HAND MOST OUTBOARD AT L1 DOORWAY REMOVED AS PER SRM 51-31-01, VOLUME II AND REPLACED AS PER SRM 51-31-01, VOLUME II.Jul 21, 2004 · N613FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02145Seat Track · wornMAIN DECK, SEAT TRACK LBL 47 FOUND WITH DEEP SCRATCHES AT STA 1100. NEW TRACK AND SPLICE REWORKED AS PER SRM 53-70-00, FIGURE 1, VOLUME I AND INSTALLED AS PER SRM 53-70-00, FIGURE 1, VOLUME I.Jul 21, 2004 · N613FE · Doug MD11 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA02140Stringer · crackedRIGHT HAND UPPER NR 9 STRINGER END FOUND CRACK AT INSIDE ACCESS PANEL 638AB. REPAIR ANGLES FABRICATED AS PER SRM 57-20-00, FIGURE 10, VOLUME I AND INSTALLED AS PER SRM 57-20-00, FIGURE 10, SHEET 6, VOLUME I.Jul 20, 2004 · N613FE · Doug MD11 · Wing, Longeron/StringerSDR 04FDEA02139Stringer · crackedLEFT HAND UPPER NR 9 STRINGER END FOUND CRACK AT INSIDE ACCESS PANEL 538AB. REPAIR SPLICE ANGLE FABRICATED AS PER SRM 57-20-00, VOLUME I; NEW STRINGER AND SPLICE ANGLES INSTALLED AS PER SRM 57-20-00, VOLUME I.Jul 20, 2004 · N613FE · Doug MD11 · Wing, Longeron/StringerSDR 04FDEA02137Stop Fitting · corrodedLEFT HAND WING OUTBOARD FLAP STOP FITTING FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01, VOLUME II.Jul 19, 2004 · N613FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02136Stop Fitting · crackedRIGHT HAND WING OUTBOARD FLAP STOP FITTING FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-33-01, VOLUME II.Jul 19, 2004 · N613FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02135Hinge · corrodedLT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.403, MATERIAL REMOVED=0.005, REMAINING THICKNESS=0.398 AND REPAIRED AS PER FEDEXJul 19, 2004 · N613FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02134Hinge · corrodedLT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.400, MATERIAL REMOVED=0.006, REMAINING THICKNESS=0.394 AND REPAIRED AS PER FEDEX EAJul 19, 2004 · N613FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02133Hinge · corrodedLT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT HOLE OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.190 AND REPAIRED AS PER EA NR 1-5750-77942. TITLE: WINGS - TJul 19, 2004 · N613FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02132Hinge · corrodedLEFT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT HOLE INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Jul 19, 2004 · N613FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02131Hinge · corrodedLT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.506, MATERIAL REMOVED=0.002, REMAINING THICKNESS=0.504, AND REPAIRED AS PER FEDEX EA NR 1-5Jul 19, 2004 · N613FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02130Hinge · corrodedLEFT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.503, MATERIAL REMOVED=0.004, REMAINING THICKNESS=0.499 AND REPAIRED AS PER FEDEX EA NJul 19, 2004 · N613FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02129Hinge · corrodedLEFT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Jul 19, 2004 · N613FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02128Hinge · corrodedLEFT HAND WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.095 AND REPAIRED AS PER EA NR 1-5750-77942. TITLE: WINGS - TRAILING Jul 19, 2004 · N613FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02127Hinge · corrodedLT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT HOLE INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.190 AND REPAIRED AS PER FEDEX EA NR 1-5750-77940. TITLE: WINJul 19, 2004 · N613FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02126Hinge · corrodedLEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.405", MATERIAL REMOVED = 0.005, REMAINING THICKNESS=0.400, AND REPAIRED AS Jul 19, 2004 · N613FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02125Hinge · corrodedLEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT HOLE OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED ASPER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER 1.062, FINAL DIAMETER 1.207, AND REPAIRED AS PER FEDEX EA NR 1-5750-77940. TITLE: Jul 19, 2004 · N613FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02124Hinge · corrodedLEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Jul 19, 2004 · N613FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02123Hinge · corrodedLEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD BORE FOUND CORRODED.Jul 19, 2004 · N613FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02122Hinge · corrodedLEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.505, MATERIAL REMOVED=0.004, REMAINING THICKNESS=0.501, AND REPAIRED AS PER FEDEX EAJul 19, 2004 · N613FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02121Hinge · corrodedLEFT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Jul 19, 2004 · N613FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02120Hinge · corrodedLT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.510, MATERIAL REMOVED=0.003, REMAINING THICKNESS=0.507, AND REPAIRED AS PER FEDEX EA NR 1-Jul 19, 2004 · N613FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02119Hinge · corrodedRT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT HOLE INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.190 AND REPAIRED AS PER EA NO. 1-5750-77941. TITLE: WINGS - Jul 19, 2004 · N613FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02118Hinge · corrodedRT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.406, MATERIAL REMOVED=0.008, REMAINING THICKNESS=0.398 AND REPAIRED AS PER FEDEX EJul 19, 2004 · N613FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02117Hinge · corrodedRT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT HOLE OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.190 AND REPAIRED AS PER EA NR 1-5750-77941. TITLE: WINGS - Jul 19, 2004 · N613FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02116Hinge · corrodedRT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT OUTBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.404, MATERIAL REMOVED=0.007, REMAINING THICKNESS=0.397 AND REPAIRED AS PER FEDEX EJul 19, 2004 · N613FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02115Hinge · corrodedRT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER = 1.093, FINAL DIAMETER = 1.196 AND REPAIRED AS PER EA NR 1-5750-77941. TITLE: WINGS - TRAILING EDGE ANJul 19, 2004 · N613FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02114Hinge · corrodedRT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE INBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.506, MATERIAL REMOVED=0.005, REMAINING THICKNESS=0.501 AND REPAIRED AS PER FEDEX EA NR 1-5Jul 19, 2004 · N613FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02113Hinge · corrodedRT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.193 AND REPAIRED AS PER EA NR 1-5750-77941. TITLE: WINGS - TRAILING EDJul 19, 2004 · N613FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02112Hinge · corrodedRT WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), PIVOT HOLE OUTBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL THICKNESS=0.506, MATERIAL REMOVED=0.004, REMAINING THICKNESS=0.502 AND REPAIRED AS PER FEDEX EA NR 1-5Jul 19, 2004 · N613FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02111Hinge · corrodedRT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT HOLE INBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4, ORIGINAL DIA.=1.062, FINAL DIAMETER = 1.218 AND REPAIRED AS PER EA NR 1-5750-77943. TRAILING EDGE DEVICES -Jul 19, 2004 · N613FE · Doug MD11 · Trailing Edge FlapsSDR 04FDEA02110Hinge · corrodedRT WING OUTBOARD FLAP INBOARD HINGE (FLAP SIDE), ACTUATOR ATTACHMENT INBOARD LUG SPOTFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02.Jul 19, 2004 · N613FE · Doug MD11 · Trailing Edge Flaps
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