N966WN

Service difficulty reports · 254

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 = 'N966WN' 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 SWAA2021091312131Nut Plate · corrodedNUT PLATE STRIP HAS CORROSION. COMMON TO ACB DOOR SURROUND STRUCTURE. BS787+3.75; RBL20; WL153. ; / [01] REMOVED AND REPLACED NUT PLATE STRIP ACB DOOR SURROUND STRUCTURE BS787+3.75' RBL 20; WL 153. PER DWG#146A0081 REV: A AND SRM 51-40-02.; [02] VERIFIED ACTIOAug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2021091312130Strap · corrodedACB DOOR SURROUND STRUCTURE STRAP CORROSION BS807+2; RBL19.25; WL154. ; / [01] REMOVED AND EVALUATED CORROSION AT BS807+2 RBL19 WL154. DAMAGE MEASURES 1.3LX1.1WX0.025D. DAMAGE FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1. PART TO BE REPAIRED BY REPLACEMENT.Aug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312241Web · corrodedACB DOOR SURROUND; SUB THRESHOLD WEB CORROSION. BS827+2.2; RBL27; WL153. REMOVED CORROSION ON AFT CARGO BAY SUB THRESHOLD WEB AT BS 827+2.2' RBL 27 WL 153. MEASURED L 1' X W .5' AND 0.006' DEEP. ORIGINAL THICKNESS .050'; REMAINING THICKNESS .049'. FOUND TO Aug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312240Web · corrodedACB DOOR SURROUND; SUB THRESHOLD WEB CORROSION. BS827+2.5; RBL27; WL153 ; / [01] REMOVED CORROSION ON AFT CARGO BAY SUB THRESHOLD WEB AT BS 827+2.5' RBL 27 WL 153<BR>MEASURED L 1' X W 1' AND 0.006' DEEP. ORIGINAL THICKNESS .050'; REMAINING THICKNESS .049'<BR>FAug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312132Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS787+10.25; LBL22; WL153 ; / [01] REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 787 + 10.25 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF Aug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312189Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION; LOWER SURFACE. BS767+18.5; LBL22; WL151 ; / [01] REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 767 +18.5 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TAug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312188Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS767+10.5; LBL22; WL151 ; / [01] REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 767=10.5 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMIAug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312197Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS747+16.25; RBL20; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+16.25'; RBL 20; WL 151 ; WORK AREA 1.0'X 1.0' X 0.011' ; REMAINING THICKNESS IS 0.029 ; ORIGINAL THICKNESS IS 0.040; FOUND Aug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312153Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION; LOWER SURFACE. BS767+5.5; LBL22; WL151 ; / [01] REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 767 + 5.5' LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TAug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312154Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION; LOWER SURFACE. BS767+14.5; LBL22; WL151 ; / [01] REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 767+14.5 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TOAug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312152Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS767+14.5; LBL22; WL151 ; / [01] REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 767 + 14.5 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIAug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312167Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS767; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 767; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.012' ; REMAINING THICKNESS IS 0.028; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF LAug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312158Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS747+18.5; LBL22; WL151 ; / [01] REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 747+18.5 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMIAug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312160Cargo Track · corrodedACB RAIL UPPER SURFACE CORROSION BS767+4.5 TO BS767+6.5; RBL3; WL151 ; / REMOVED CORROSION ON AFT CARGO BAY R/H ACB RAIL UPPER SURFACE BS767+4.5 TO BS767+6.5 IN L: 2.150IN W: 0.900IN D: 0.012; FROM ORIGINAL THICKNESS OF 0.075IN. FOUND TO BE OUT OF LIMITS IAW SAug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2021091312156Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS747+10.5; LBL22; WL151 ; / [01] REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 747+10.5 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMIAug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312157Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS747+14.5; LBL22; WL151 ; / [01] REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 747 +14.5 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMAug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312155Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS747+6.5; LBL22; WL151 ; / [01] REMOVED CORROSION FROM FLOOR TO SIDEWALL SUPPORT BS 747+6.5 LBL 22 ACB IN AREA OF L=.5' X W=.5' D=.006' REMAINING THICKNESS =.034' FROM ORIGINAL THICKNESS .040' FOUND TO BE OUT OF LIMITSAug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312200Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS747+19; RBL21; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+19'; RBL 21; WL 151 ; WORK AREA 1.0'X 1.0' X 0.015' ; REMAINING THICKNESS IS 0.025 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE Aug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312198Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION; LOWER SURFACE. BS747+16; RBL21; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+16'; RBL 21; WL 151 ; WORK AREA 1.0'X 1.0' X 0.012' ; REMAINING THICKNESS IS 0.028 ; ORIGINAL THICKNESS IS 0.04Aug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312199Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS747+18.5; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+18.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.015' ; REMAINING THICKNESS IS 0.025 ; ORIGINAL THICKNESS IS 0.040; FOUND TOAug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312196Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS747+15.75; RBL21; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+15.75'; RBL 21; WL 151 ; WORK AREA 1.0'X 1.0' X 0.011' ; REMAINING THICKNESS IS 0.029; ORIGINAL THICKNESS IS 0.040; FOUND TAug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312163Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS747+2; RBL21; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+2'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.035' ; REMAINING THICKNESS IS 0.005 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUAug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312194Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS747+10.5; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+10.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.013' ; REMAINING THICKNESS IS 0.027 ; ORIGINAL THICKNESS IS 0.040; FOUND TOAug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312192Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS747+6.5; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+6.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.012' ; REMAINING THICKNESS IS 0.028 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BAug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312193Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS747+8.5; RBL21; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+8.5'; RBL 21; WL 151 ; WORK AREA 1.0'X 1.0' X 0.025' ; REMAINING THICKNESS IS 0.015 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BAug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312166Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS747+12; RBL21; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+12'; RBL 21; WL 151 ; WORK AREA 1.0'X 1.0' X 0.013' ; REMAINING THICKNESS IS 0.027 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE Aug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312165Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION; LOWER SURFACE. BS747+5.5; RBL21; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+5.5'; RBL 21; WL 151 ; WORK AREA 1.0'X 1.0' X 0.015' ; REMAINING THICKNESS IS 0.025 ; ORIGINAL THICKNESS IS 0.Aug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312164Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION; LOWER SURFACE. BS747+2; RBL21; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747+2'; RBL 21; WL 151 ; WORK AREA 1.0'X 1.0' X 0.006' ; REMAINING THICKNESS IS 0.034 ; ORIGINAL THICKNESS IS 0.040;Aug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312204Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION; LOWER SURFACE. BS727E+18.5; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+18.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.008' ; REMAINING THICKNESS IS 0.032 ; ORIGINAL THICKNESS IAug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312162Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS747; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.017' ; REMAINING THICKNESS IS 0.023 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF Aug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312161Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS747; RBL19; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 747; RBL 19; WL 151 ; WORK AREA 1.0'X 1.0' X 0.017' ; REMAINING THICKNESS IS 0.023 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OF Aug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312205Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION; LOWER SURFACE. BS727E+19; RBL21; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+19'; RBL 21; WL 151 ; WORK AREA 1.0'X 1.0' X 0.008' ; REMAINING THICKNESS IS 0.032 ; ORIGINAL THICKNESS IS 0.Aug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312201Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS727E+2; RBL21; WL151 ; / [01] FAULT RESOLVED ON OTHER CUSTOMER CARD NBR:TTG8Q006A3FD; [02] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+2'; RBL 21; WL 151 ; WORK AREA 1.0'X 1.0' X 0.012' ; REMAINING TAug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312203Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS727E+6.5; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+6.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.023' ; REMAINING THICKNESS IS 0.017 ; ORIGINAL THICKNESS IS 0.040; FOUND TOAug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312175Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS727E+19; RBL21; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+19'; RBL 21; WL 151 ; WORK AREA 1.0'X 1.0' X 0.014' ; REMAINING THICKNESS IS 0.026 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BAug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312202Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION; LOWER SURFACE. BS727E+2.5; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+2.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.009' ; REMAINING THICKNESS IS 0.031; ORIGINAL THICKNESS IS 0Aug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312174Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS727E+18.5; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+18.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.014' ; REMAINING THICKNESS IS 0.026 ; ORIGINAL THICKNESS IS 0.040; FOUND Aug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312172Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION; LOWER SURFACE. BS727E+14.5; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+14.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.007' ; REMAINING THICKNESS IS 0.033 ; ORIGINAL THICKNESS IAug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312173Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION; LOWER SURFACE. BS727E+15.5; RBL21; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+15.5'; RBL 21; WL 151 ; WORK AREA 1.0'X 1.0' X 0.007' ; REMAINING THICKNESS IS 0.033 ; ORIGINAL THICKNESS IAug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312171Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS727E+14.5; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+14.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.022' ; REMAINING THICKNESS IS 0.018 ; ORIGINAL THICKNESS IS 0.040; FOUND Aug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312169Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS727E+2.5; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+2.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.007' ; REMAINING THICKNESS IS 0.033; ORIGINAL THICKNESS IS 0.040; FOUND TO Aug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312170Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS727E+10.5; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E+10.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.035' ; REMAINING THICKNESS IS 0.005 ; ORIGINAL THICKNESS IS 0.040; FOUND Aug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312210Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS727D+18.5; RBL22; WL151 ; / [01] FAULT RESOLVED ON OTHER CUSTOMER CARD NBR:TTG8Q006A3FD; [02] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727D+18.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.011' ; REMAIAug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312168Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS727E; RBL19; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727E; RBL 19; WL 151 ; WORK AREA 1.0'X 1.0' X 0.008' ; REMAINING THICKNESS IS 0.032 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OUT OAug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312209Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS727D+16; RBL21; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727D+16'; RBL 21; WL 151 ; WORK AREA 1.0'X 1.0' X 0.022' ; REMAINING THICKNESS IS 0.018 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BAug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312207Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS727D+6; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727D+6'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.011' ; REMAINING THICKNESS IS 0.029 ; ORIGINAL THICKNESS IS 0.040; FOUND TO BE Aug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312208Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS727D+10.5; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727D+10.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.007' ; REMAINING THICKNESS IS 0.033 ; ORIGINAL THICKNESS IS 0.040; FOUND Aug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312183Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION; LOWER SURFACE. BS727D+15.5; RBL19; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727D+15.5'; RBL 19; WL 151 ; WORK AREA 1.0'X 1.0' X 0.006' ; REMAINING THICKNESS IS 0.034; ORIGINAL THICKNESS ISAug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312182Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS727D+14.5; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727D+14.5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.015' ; REMAINING THICKNESS IS 0.025; ORIGINAL THICKNESS IS 0.040; FOUND TAug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021091312181Support · corrodedACB FLOOR TO SIDEWALL SUPPORT CORROSION. BS727D+5; RBL22; WL151 ; / [01] REMOVED CORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT BS 727D+5'; RBL 22; WL 151 ; WORK AREA 1.0'X 1.0' X 0.011' ; REMAINING THICKNESS IS 0.029; ORIGINAL THICKNESS IS 0.040; FOUND TO BE OAug 26, 2021 · N966WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
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