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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FDEA201809252688Hinge Bracket · corrodedLEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) LOWER MOUNT INBD HOLE BORE FOUND CORROSION. HOLE BORE NR 3 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-09. NEW SHOULDER BUSHING FABRICATED PER EA 1-5750-T0342336 PT 1 STEP 2A AND INSTALLED PER CMM57-44SDR FDEA201809252687Hinge Bracket · corrodedLEFT WING OUTBD FLAP OUTBD HINGE (WING SIDE) PIVOT HOLE BORE FOUND CORROSION. HOLE BORE NR 4 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-09. NEW OVERSIZED BUSHING FABRICATED AND INSTALLED PER CMM57-44-09 & EA 1-5750-T0342336 PT 1 STEPS 2 & 2B. EO SDR FDEA201809252686Hinge Bracket · corrodedLEFT WING OUTBD FLAP INBD HINGE (WING SIDE) ACTUATOR ATTACHED OUTBD LUG HOLE FOUND CORROSION. LUG HOLE NR 8 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-08. NEW OVERSIZED BUSHING FABRICATED AND INSTALLED PER CMM57-44-08 & EA 1-5750-T0342352 PT 1 STSDR FDEA201809252685Hinge Bracket · corrodedLEFT WING OUTBD FLAP INBD HINGE (WING SIDE) ACTUATOR ATTACHED INBD LUG HOLE FOUND CORROSION. LUG HOLE NR 8 CORROSION REWORKED AND FOUND EXCEEDED LIMIT PER CMM57-44-08. NEW OVERSIZED BUSHING FABRICATED AND INSTALLED PER CMM57-44-08 & EA 1-5750-T0342352 PT 1 STESDR FDEA201809142544Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD (WING SIDE) HINGE BARREL NUT HOLE SURFACE CORROSION. HINGE BARREL NUT HOLE SURFACE REWORKED AS PER CMM 57-44-09, REPAIR SHIM FABRICATED AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-T0342161 P1 STEP 2. REPAIR CLASSIFIED AS MINOR PER SDR FDEA201809142543Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD (WING SIDE) HINGE LOWER BARREL NUT HOLE BORE CORROSION. HINGE LOWER BARREL NUT HOLE BORE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS EPR CMM 57-44-09, OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-T034SDR FDEA2018091432510Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD (WING SIDE) HINGE UPPER BARREL NUT HOLE BORE CORROSION. HINGE UPPER BARREL NUT HOLE BORE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-T034SDR FDEA2018091432509Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD (WING SIDE) HINGE LOWER MOUNT O/B HOLE BORE CORROSION. HINGE LOWER MOUNT O/B HOLE BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. SHOULDER BUSHING FABRICATED AS PER EA 1-5750-T0342161 P1 STEP 2A AND INSTALLED AS PSDR FDEA2018091432508Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD (WING SIDE) HINGE LOWER MOUNT I/B HOLE BORE CORROSION. HINGE LOWER MOUNT I/B HOLE BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS EPR CMM 57-44-09. SHOULDER BUSHING FABRICATED AS PER EA 1-5750-T0342161 P1 STEP 2A AND INSTALLED AS PSDR FDEA2018091432507Hinge Bracket · corrodedRT WING O/B FLAP O/B FWD (WING SIDE) HINGE LOWER MOUNT O/B HOLE BORE CORROSION. HINGE LOWER MOUNT O/B HOLE BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. SHOULDER BUSHING FABRICATED AS PER EA 1-5750-T0342163 P1 STEP 2A AND INSTALLED AS PSDR FDEA2018091432506Hinge Bracket · corrodedRT WING O/B FLAP O/B FWD (WING SIDE) HINGE LOWER MOUNT I/B HOLE BORE CORROSION. HINGE LOWER MOUNT I/B HOLE BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09. SHOULDER BUSHING FABRICATED AS PER EA 1-5750-T0342163 P1 STEP 2A AND INSTALLED AS PSDR FDEA2018091432505Hinge Bracket · corrodedRT WING O/B FLAP O/B FWD (WING SIDE) HINGE PIVOT HOLE BORE CORROSION. HINGE PIVOT HOLE BORE (NR 4 HOLE) REWORKED AND FOUND EXCEED LIMIT AS PER CMM 57-44-09, OVERSIZED BUSHING FABRICATED AND INSTALLED AS PER CMM 57-44-09 AND EA 1-5750-T0342163 P1 STEP 2B AND STSDR FDEA2018091172411Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD (WING SIDE) HINGE ACTUATOR I/B HOLE BORE CORROSION. HINGE ACTUATOR I/B HOLE BORE (HOLE 8) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA 1.2806", FINAL HOLE DIA 1.284", MAXIMUM ALLOWABLE HOLE DIA 1.220". REPAIR BUSSDR FDEA2018091172410Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD (WING SIDE) HINGE ACTUATOR O/B HOLE BORE CORROSION. HINGE ACTUATOR O/B HOLE BORE (HOLE 8) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA 1.220", FINAL HOLE DIA 1.223", MAXIMUM ALLOWABLE HOLE DIA 1.220". REPAIR BUSHSDR FDEA2018091172409Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD (WING SIDE) HINGE LOWER MOUNT I/B HOLE BORE CORROSION. HINGE LOWER MOUNT I/B HOLE BORE (NR 7) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA 0.718". FINAL HOLE DIA 0.727", MAXIMUM HOLE DIA 0.709". REPAIR BUSHING FASDR FDEA2018091172408Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD (WING SIDE) HINGE LOWER MOUNT O/B HOLE BORE CORROSION. HINGE LOWER MOUNT O/B HOLE BORE (HOLE 7) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA 0.705", FINAL HOLE DIA 0.722", MAXIMUM ALLOWABLE HOLE DIA 0.709". REPAISDR FDEA2018091172407Hinge Bracket · corrodedRT WING O/B FLAP I/B FWD (WING SIDE) HINGE BARREL NUT HOLE SURFACE CORROSION. HINGE BARREL NUT HOLE SURFACE REWORKED PER CMM 57-44-08. EXISTING THK - UPPER 0.389", LOWER 0.373", MATERIAL REMOVED - UPPER & LOWER 0.005", REMAINING THK - UPPER 0.384", LOWER 0.368SDR FDEA2018091172406Hinge Bracket · corrodedLT WING O/B FLAP I/B FWD (WING SIDE) HINGE ACTUATOR O/B HOLE BORE CORROSION. HINGE ACTUATOR O/B HOLE BORE (HOLE 8) REWORKED & FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA 1.222", FINAL HOLE DIA 1.252", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZED BUSSDR FDEA2018091172405Hinge Bracket · corrodedLT WING O/B FLAP I/B FWD (WING SIDE) HINGE ACTUATOR I/B HOLE BORE CORROSION. HINGE ACTUATOR I/B HOLE BORE (HOLE 8) REWORKED & FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA 1.222", FINAL HOLE DIA 1.252", MAXIMUM ALLOWABLE HOLE DIA 1.220". OVERSIZED BUSSDR FDEA2018091172404Hinge Bracket · corrodedLT WING O/B FLAP I/B FWD (WING SIDE) HINGE LOWER MOUNT O/B HOLE SURFACE CORROSION. HINGE LOWER MOUNT O/B HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING THK 0.400", MATERIAL REMOVED 0.004", REMAINING THK 0.396", MINIMUM ALLOWABLE THK 0.SDR FDEA2018091172402Hinge Bracket · corrodedLT WING O/B FLAP I/B FWD (WING SIDE) HINGE LOWER MOUNT I/B HOLE SURFACE CORROSION. HINGE LOWER MOUNT I/B HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING THK 0.436", MATERIAL REMOVED - FWD FACE 0.004", AFT FACE 0.013", REMAINING THK 0.41SDR FDEA2018091172401Hinge Bracket · corrodedLT WING O/B FLAP I/B FWD (WING SIDE) HINGE LOWER MOUNT O/B HOLE BORE CORROSION. HINGE LOWER MOUNT O/B HOLE BORE (NR 7 HOLE) REWORKED & FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA 0.709", FINAL HOLE DIA 0.729", MAXIMUM ALLOWABLE HOLE DIA 0.709". OVERSDR FDEA2018091172400Hinge Bracket · corrodedLT WING O/B FLAP I/B FWD (WING SIDE) HINGE LOWER MOUNT I/B HOLE BORE CORROSION. HINGE LOWER MOUNT I/B HOLE BORE (NR 7 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM57-44-08. EXISTING HOLE DIA 0.708", FINAL HOLE DIA 0.728", MAXIMUM ALLOWABLE HOLE DIA 0.709". OVESDR FDEA2018091172399Hinge Bracket · corrodedLT WING O/B FLAP I/B FWD (WING SIDE) HINGE BARREL NUT HOLE SURFACE CORROSION. HINGE BARREL NUT HOLE SURFACE REWORKED AS PER CMM 57-44-08, EXISTING THK - UPPER 0.378", LOWER 0.348", MATERIAL REMOVED, UPPER & LOWER 0.005", REMAINING THK - UPPER 0.373", LOWER 0.3SDR FDEA2018091172397Hinge Bracket · corrodedLT WING O/B FLAP I/B FWD (WING SIDE) HINGE PIVOT HOLE BORE CORROSION. HINGE PIVOT HOLE BORE REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-08. EXISTING HOLE DIA 2.312", FINAL HOLE DIA 2.317", MAXIMUM ALLOWABLE DIA 2.3135". OVERSIZED BUSHING FABRICATED & INSTALLSDR FDEA2018091172396Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD (WING SIDE) HINGE ACTUATOR O/B HOLE BORE CORROSION. HINGE ACTUATOR O/B HOLE BORE (NR 8 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA 1.249", FINAL HOLE DIA 1.253", MAXIMUM ALLOWABLE HOLE DIA 1.220". REPAIRSDR FDEA2018091172395Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD (WING SIDE) HINGE ACTUATOR I/B HOLE BORE CORROSION. HINGE ACTUATOR I/B HOLE BORE (NR 8 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA 1.249", FINAL HOLE DIA 1.253", MAXIMUM ALLOWABLE HOLE DIA 1.220". REPAIRSDR FDEA2018091172394Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD (WING SIDE) HINGE LOWER MOUNT O/B HOLE BORE CORROSION. HINGE LOWER MOUNT O/B HOLE BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA 0.584", FINAL HOLE DIA 0.596", MAXIMUM ALLOWABLE HOLE DIA 0.584". SHSDR FDEA2018091172393Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD (WING SIDE) HINGE LOWER MOUNT I/B HOLE BORE CORROSION. HINGE LOWER MOUNT I/B HOLE BORE (NR 3 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA 0.584", FINAL HOLE DIA 0.596", MAXIMUM ALLOWABLE HOLE DIA 0.584", SDR FDEA2018091172392Hinge Bracket · corrodedLT WING O/B FLAP O/B FWD (WING SIDE) HINGE UPPER MOUNT O/B HOLE BORE CORROSION. HINGE UPPER MOUNT O/B HOLE BORE (NR 2 HOLE) REWORKED AND FOUND EXCEED LIMIT PER CMM57-44-09. EXISTING HOLE DIA 0.880", FINAL HOLE DIA 0.948", MAXIMUM ALLOWABLE DIA 0.944". REPAIR BSDR FDEA2018091172391Hinge Bracket · corrodedRT WING O/B FLAP O/B FWD (WING SIDE) HINGE ACTUATOR O/B HOLE BORE CORROSION. HINGE ACTUATOR O/B HOLE BORE (HOLE 8) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA 1.280", FINAL HOLE DIA 1.1287", MAXIMUM ALLOWABLE HOLE DIA 1.220". REPAIR BUSSDR FDEA2018091172390Hinge Bracket · corrodedRT WING O/B FLAP O/B FWD (WING SIDE) HINGE ACTUATOR I/B HOLE BORE CORROSION. HINGE ACTUATOR I/B HOLE BORE (HOLE 8) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09, EXISTING HOLE DIA 1.220", FINAL HOLE DIA 1.248", MAXIMUM ALLOWABLE HOLE DIA 1.220". REPAIR BUSHSDR FDEA2018091172389Hinge Bracket · corrodedRT WING O/B FLAP O/B FWD (WING SIDE) HINGE BARREL NUT HOLE SURFACE CORROSION. HINGE BARREL NUT HOLE SURFACE REWORKED PER CMM 57-44-09. EXISTING THK - UPPER 0.381", LOWER 0.386", MATERIAL REMOVED - UPPER & LOWER 0.010", REMAINING THK - UPPER 0.371", LOWER 0.376SDR FDEA2018091172385Hinge Bracket · corrodedRT WING O/B FLAP O/B FWD (WING SIDE) HINGE UPPER MOUNT O/B HOLE SURFACE CORROSION. HINGE UPPER MOUNT HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT PER CMM57-44-09. EXISTING THK 0.715", MATERIAL REMOVED 0.004", REMAINING THK 0.711", MINIMUM ALLOWABLE THK 0.72". SDR FDEA2018091172384Hinge Bracket · corrodedRT WING O/B FLAP O/B FWD (WING SIDE) HINGE UPPER MOUNT HOLE SURFACE CORROSION. HINGE UPPER MOUNT O/B HOLE SURFACE REWORKED AND FOUND EXCEED LIMIT PER CMM57-44-09. EXISTING THK 0.715", MATERIAL REMOVED 0.004", REMAINING THK 0.711", MINIMUM ALLOWABLE THK 0.72". SDR FDEA2018091172383Hinge Bracket · corrodedRT WING O/B FLAP O/B FWD (WING SIDE) HINGE PIVOT HOLE BORE CORROSION. HINGE PIVOT HOLE BORE (HOLE 4) REWORKED AND FOUND EXCEED LIMIT PER CMM 57-44-09. EXISTING HOLE DIA 2.300", FINAL HOLE DIA 2.3185", MAXIMUM ALLOWABLE HOLE DIA 2.3135". REPAIR BUSHING FABRICATSDR 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 BUSHINSDR 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". OVERSDR 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 ANSDR 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 SDR 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: 0.709SDR 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. OSDR 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 1SDR 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 1SDR 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 SDR 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", REMSDR 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", REMAISDR 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", SHSDR 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 BUSHISDR 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 DI
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