JASC 5744

Service difficulty reports · 2,721

Reports filed under 5744 · Wing, Control Surface Attach Fittings, 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 jasc_code = '5744'
  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 AALA201712059004Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE. RIGHT AILERON FAILED BACKLASH FUNCTIONAL TEST. REPLACED AILERON HINGE FITTING NR 2 PER AMM 57-61-00-000-81.Nov 27, 2017 · N956UW · Emb ERJ190100IGWSDR AALA201712059003Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE. RIGHT AILERON FAILED BACKLASH FUNCTIONAL TEST. REPLACED AILERON HINGE FITTING NR 1 PER AMM 57-61-00-000-801.Nov 27, 2017 · N956UW · Emb ERJ190100IGWSDR FDEA201711083191Hinge · corrodedRT WING I/B FLAP O/B FWD HINGE (WING SIDE) PIVOT BORE CORROSION. REPAIR BUSHING FABRICATED AND INSTALLED PER EA 1-5750-T0331058A P1 STEP F(1) AND STEP F (3). RT WING INBD FLAP - OUTBD FWD HINGE (WING SIDE) REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Nov 8, 2017 · N610FE · Doug MD11FSDR FDEA201711083190Hinge · corrodedLT WING INBD FLAP OUTBD FWD HINGE (WING SIDE) PIVOT BORE CORROSION. REPAIR BUSHING FABRICATED AND INSTALLED PER EA 1-5750-T0331052A P1 STEP F(1) AND STEP F (3). LT WING INBD FLAP - OUTBD FWD HINGE (WING SIDE) REPAIR. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100Nov 8, 2017 · N610FE · Doug MD11FSDR FDEA201710233025Hinge Bracket · wornLEFT FWD WING SIDE INBD FLAP FWD OTBD HINGE PIVOT BORE WORN. FOUND THE INDB & OTBD FACE OUT OF LIMITS IAW CMM 57-44-07. A BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-87635F, P2, STEP 1F (1) AND STEP 1F (3). THE REPAIR WAS CLASSIFIED AS MAJOR IAW GMMOct 23, 2017 · N574FE · Doug MD11FSDR V0XD20171009006Attach Bracket · crackedRIGHT SLAT TRACK CANISTER 1 - 3 HAS A CRACKED ATTACH BRACKET. FABRICATED AND INSTALLED THE ATTACH BRACKET IAW REO 67057-42-577.Oct 9, 2017 · N656CA · Cndair CL6002C10SDR FDEA201710052859Hinge Bracket · corrodedLEFT WING, OTBD FLAP, OTBD FWD HINGE (WING SIDE) BARREL NUT HOLE SURFACE CORRODED. REWORKED IAW CMM 57-44-09. OUT OF LIMITS, A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335621, PART 1, STEP 2.Oct 5, 2017 · N609FE · Doug MD11FSDR FDEA201709282772Hinge · corrodedRT WING O/B FLAP I/B FWD HINGE (WING SIDE) ACTUATOR ATTACH O/B BORE CORROSION. RH WING O/B FLAP I/B FWD HINGE (WING SIDE) ACTUATOR ATTACH O/B BORE (#8 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER MD-11 CMM 57-44-08 EXISTING HOLE: 1.224", FINAL HOLE: 1.229Sep 28, 2017 · N609FE · Doug MD11FSDR FDEA201709282771Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD HINGE (WING SIDE) ACTUATOR ATTACH I/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 EXISTING HOLE: 1.2235", FINAL HOLE 1.229", MAXIMUM ALLOWABLE HOLE 1.220". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EO 1-Sep 28, 2017 · N609FE · Doug MD11FSDR FDEA201709282770Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD HINGE (WING SIDE) LOWER MOUNT O/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 EXISTING HOLE 0.708", FINAL HOLE 0.712", MAXIMUM ALLOWABLE HOLE 0.709". SHOULDER BUSHING FABRICATED AND INSTALLED AS PER EO 1-5750-T0Sep 28, 2017 · N609FE · Doug MD11FSDR FDEA201709282769Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD HINGE (WING SIDE) LOWER MOUNT I/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 EXISTING HOLE: 0.709", FINAL HOLE: 0.712", MAXIMUM ALLOWABLE HOLE: 0.709". SHOULDER BUSHING FABRICATED AND INSTALLED AS PER EO 1-5750Sep 28, 2017 · N609FE · Doug MD11FSDR FDEA201709282768Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD HINGE (WING SIDE) UPPER MOUNT O/B BORE SURFACE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 EXISTING THICKNESS: 760", MATERIAL REMOVED: 0.050", REMAINING THICKNESS: 0.710", MINIMUM ALLOWABLE THICKNESS: 0.720", REPAIR Sep 28, 2017 · N609FE · Doug MD11FSDR FDEA201709282767Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD HINGE (WING SIDE) UPPER MOUNT I/B BORE SURFACE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 EXISTING THICKNESS: 0.729", MATERIAL REMOVED: 0.026" REMAINING THICKNESS: 0.703". REPAIR SHIM FABRICATED AND INSTALLED AS PERSep 28, 2017 · N609FE · Doug MD11FSDR FDEA201709282766Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD HINGE (WING SIDE) UPPER MOUNT O/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 EXISTING HOLE: 0.948", FINAL HOLE: 0.951", MAXIMUM ALLOWABLE HOLE: 0.944". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EO 1-575Sep 28, 2017 · N609FE · Doug MD11FSDR FDEA201709282765Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD HINGE (WING SIDE) UPPER MOUNT I/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 EXISTING HOLE: 0.9535", FINAL HOLE: 0.957", MAXIMUM ALLOWABLE HOLE: 0.944". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EO 1-57Sep 28, 2017 · N609FE · Doug MD11FSDR FDEA201709282764Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD HINGE (WING SIDE) PIVOT BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08 EXISTING HOLE: 2.317", FINAL HOLE: 2.321", MAXIMUM ALLOWABLE HOLE: 2.3135". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EO 1-5750-T033562Sep 28, 2017 · N609FE · Doug MD11FSDR FDEA201709282763Hinge Bracket · corrodedRIGHT WING, OTBD FLAP, OTBD FWD HINGE (WING SIDE) LOWER MOUNT, OTBD BORE SURFACE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335603, PT 1, STEP 1.Sep 28, 2017 · N609FE · Doug MD11FSDR FDEA201709282762Hinge Bracket · corrodedRIGHT WING OTBD FLAP, OTBD FWD HINGE (WING SIDE) FWD MOUNT, OTBD LUG SURFACE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. REPAIRED IAW EA 1-5750-T0335603, PART 1, STEP 1.Sep 28, 2017 · N609FE · Doug MD11FSDR FDEA201709282761Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE (WING SIDE) ACTUATOR ATTACH OTBD BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335603, PART 1, STEP 1E.Sep 28, 2017 · N609FE · Doug MD11FSDR FDEA201709282760Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE (WING SIDE) ACTUATOR ATTACH INBD BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335603, PART 1, STEP 1E.Sep 28, 2017 · N609FE · Doug MD11FSDR FDEA201709282759Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE (WING SIDE) BARREL NUT HOLE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335603, PART 1, STEP 1F.Sep 28, 2017 · N609FE · Doug MD11FSDR FDEA201709282758Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE (WING SIDE) LOWER MOUNT OTBD BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335603, PART 1, STEP 1B, AND STEP 1.Sep 28, 2017 · N609FE · Doug MD11FSDR FDEA201709282757Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE (WING SIDE) LOWER MOUNT INBD BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. A SHOULDER BUSHING FABRICATED BY MACHINING AND INSTALLED IAW EA 1-5750-T0335603, PART 1, STEP 1B, AND STEP 1.Sep 28, 2017 · N609FE · Doug MD11FSDR FDEA201709282756Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE (WING SIDE) UPPER MOUNT INBD BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335603, PART 1, STEP 1A.Sep 28, 2017 · N609FE · Doug MD11FSDR FDEA201709272750Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE (WING SIDE) UPPER MOUNT OTBD BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335603, PART 1, STEP 1A.Sep 27, 2017 · N609FE · Doug MD11FSDR FDEA201709272749Hinge Bracket · corrodedRIGHT WING OTBD FLAP OTBD FWD HINGE (WING SIDE) PIVOT BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-09. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335603, PART 1, STEP 1C.Sep 27, 2017 · N609FE · Doug MD11FSDR FDEA201709272748Hinge Bracket · corrodedLT WING O/B FLAP I/B FWD HINGE (WING SIDE) ACTUATOR ATTACH O/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE: DIA: 1.222", FINAL HOLE: DIA: 1.228", MAXIMUM ALLOWABLE HOLE: DIA: 1.220". OVERSIZED BUSHING FABRICATED AND INSTASep 27, 2017 · N609FE · Doug MD11FSDR FDEA201709272747Hinge Arm · corrodedLT WING O/B FLAP I/B FWD HINGE (WING SIDE) ACTUATOR ATTACH I/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-08. EXISTING HOLE: DIA: 1.224", FINAL HOLE: DIA: 1.228", MAXIMUM ALLOWABLE HOLE: DIA: 1.220". OVERSIZED BUSHING FABRICATED AND INSTASep 27, 2017 · N609FE · Doug MD11FSDR FDEA201709272746Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD FWD HINGE (WING SIDE) LOWER MOUNT OTBD BORE CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. A SHOULDER BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335583, PART 1, STEP 1B, AND STEP 1.Sep 27, 2017 · N609FE · Doug MD11FSDR FDEA201709272745Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD FWD HINGE (WING SIDE) LOWER MOUNT INBD BORE CORRODED. THE BORE CORROSION WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. FABRICATED AND INSTALLED A REPAIR IAW 1-5750-T0335583, PART 1, STEP 1B, AND STEP 1.Sep 27, 2017 · N609FE · Doug MD11FSDR FDEA201709272744Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD FWD HINGE (WING SIDE) BARREL NUT HOLE SURFACE CORRODED. CORROSION WAS WORKED IAW CMM 57-44-08. A REPAIR SHIM WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335583, PART 1, STEP 1.Sep 27, 2017 · N609FE · Doug MD11FSDR FDEA201709272743Hinge Bracket · corrodedLEFT WING OTBD FLAP INBD FWD HINGE (WING SIDE) PIVOT BORE CORRODED. CORROSION FOUND OUT OF LIMITS IAW CMM 57-44-08. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0335583, PART 1, STEP 1A.Sep 27, 2017 · N609FE · Doug MD11FSDR FDEA201709272742Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD HINGE (WING SIDE) ACTUATOR ATTACH O/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 EXISTING HOLE: 1.253", FINAL HOLE: 1.259", MAXIMUM ALLOWABLE HOLE; 1.220". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1Sep 27, 2017 · N609FE · Doug MD11FSDR FDEA201709272741Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD HINGE (WING SIDE) ACTUATOR ATTACH I/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 EXISTING HOLE: 1.252", FINAL HOLE: 1.259", MAXIMUM ALLOWABLE HOLE: 1.220". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1Sep 27, 2017 · N609FE · Doug MD11FSDR FDEA201709272740Hinge Arm · corrodedLT WING O/B FLAP O/B FWD HINGE (WING SIDE) BARREL NUT HOLE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 EXISTING HOLE: 0.692", FINAL HOLE: 0.702", MAXIMUM ALLOWABLE HOLE: 0.667". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T03Sep 27, 2017 · N609FE · Doug MD11FSDR FDEA201709272739Hinge · corrodedLT WING O/B FLAP O/B FWD HINGE (WING SIDE) BARREL NUT LOWER BOLT HOLE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 EXISTING HOLE: 0.3255", FINAL HOLE: 0.408", MAXIMUM ALLOWABLE HOLE: 0.391". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER ESep 27, 2017 · N609FE · Doug MD11FSDR FDEA201709272738Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD HINGE (WING SIDE) BARREL NUT UPPER BOLT HOLE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 EXISTING HOLE: 0.390", FINAL HOLE: 0.408", MAXIMUM ALLOWABLE HOLE: 0.391". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EASep 27, 2017 · N609FE · Doug MD11FSDR FDEA201709272737Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD HINGE (WING SIDE) LOWER MOUNT O/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 EXISTING HOLE: 0.586", FINAL HOLE: 0.597", MAXIMUM ALLOWABLE HOLE: 0.584". SHOULDER BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750Sep 27, 2017 · N609FE · Doug MD11FSDR FDEA201709272736Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD HINGE (WING SIDE) LOWER MOUNT I/B BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 EXISTING HOLE: 0.586", FINAL HOLE: 0.597", MAXIMUM ALLOWABLE HOLE: 0.584". SHOULDER BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750Sep 27, 2017 · N609FE · Doug MD11FSDR FDEA201709272735Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD HINGE (WING SIDE) PIVOT BORE CORROSION. REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09 EXISTING HOLE: 2.3165", FINAL HOLE: 2.322", MAXIMUM ALLOWABLE HOLE: 2.3135". OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER EA 1-5750-T03356Sep 27, 2017 · N609FE · Doug MD11FSDR AALA20170926006Hinge Fitting · corrodedCORROSION ON LEFT WING OUBOARD FLAP LOWER INBD SIDE OF CENTER HINGE FITTING AT STUD. REMOVED AND REPLACED THE HINGE FITTING IAW AMM 57-40-01-201.Sep 26, 2017 · N971TW · Doug MD83SDR FDEA201709252710Hinge Bracket · corrodedRIGHT WING INBD FLAP OTBD FWD HINGE (WING SIDE) PIVOT BORE CORRODED. A REPAIR BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T033099 A, PART 1, STEP 1F. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Sep 25, 2017 · N609FE · Doug MD11FSDR FDEA201709252709Hinge Bracket · corrodedRIGHT WING INBD FLAP OTBD AFT HINGE (FLAP SIDE) PIVOT OTBD BORE CORRODED. WORKED AND FOUND OUT OF LIMITS IAW CMM 57-52-03. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-137533C-PT5, STEP 2B, AND 2A. . REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2Sep 25, 2017 · N609FE · Doug MD11FSDR FDEA201709252705Hinge Bracket · corrodedLEFT WING INBD FLAP OTBD FWD HINGE (WING SIDE) ACTUATOR ATTACH OTBD BORE CORRDED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-07. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0330993 A, PART 1, STEP 1F. REPAIR CLASSIFEID AS MAJOR IAW Sep 25, 2017 · N609FE · Doug MD11FSDR FDEA201709252704Hinge Bracket · corrodedLEFT WING INBD FLAP, OTBD HINGE (WING SIDE) ACTUATOR ATTACH INBD BORE CORRODED. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-07. AN OVERSIZED BUSHING WAS FABRICATED AND INSTALLED IAW EA 1-5750-T0330993, PART 1, STEP 1F. REPAIR CLASSIFEID AS MAJOR IAW GMSep 25, 2017 · N609FE · Doug MD11FSDR FDEA201709122508Hinge Bracket · corrodedRIGHT WING OTBD FLAP INBD HINGE (WING SIDE) ACTUATOR OTBD LUG HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. THE FLAP INBD HINGE WAS REMOVED AND REPLACED IAW AMM 57-53-01-4.Sep 12, 2017 · N586FE · Doug MD11FSDR FDEA201709122507Hinge Bracket · corrodedRIGHT WING OTBD FLAP INBD HINGE (WING SIDE) ACTUATOR INBD LUG HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. THE FLAP INBD HINGE WAS REMOVED AND REPLACED IAW AMM 57-53-01-4.Sep 12, 2017 · N586FE · Doug MD11FSDR FDEA201709122506Hinge Bracket · corrodedRIGHT WING OTBD FLAP INBD HINGE (WING SIDE) LOWER MOUNT OTBD HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED, AND FOUND OUT OF LIMIT IAW CMM 57-44-08. THE OTBD FLAP INBD HINGE WAS REMOVED AND REPLACED IAW AMM 57-53-01-4.Sep 12, 2017 · N586FE · Doug MD11FSDR FDEA201709122505Hinge Bracket · corrodedRIGHT WING OTBD FLAP INBD HINGE (WING SIDE) LOWER MOUNT INBD HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. THE FLAP INBD HINGE WAS REMOVED AND REPLACED IAW AMM 57-53-01-4.Sep 12, 2017 · N586FE · Doug MD11FSDR FDEA201709122503Hinge Bracket · corrodedRIGHT WING OTBD FLAP INBD HINGE (WING SIDE) PIVOT HOLE BORE FOUND CORRODED. THE BORE WAS REWORKED AND FOUND OUT OF LIMITS IAW CMM 57-44-08. THE RIGHT WING OTBD FLAP INBD HINGE WAS REMOVED AND REPLACED IAW AMM 57-53-01-4.Sep 12, 2017 · N586FE · Doug MD11F
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