N469WN

Service difficulty reports · 322

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 = 'N469WN' 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 SWAA2022030769131Support · corrodedCORROSION ON FLOOR SUPPORT STA 986-1006; LBL 8-LBL 17; WL 208. / [01] NO ALLOWABLE LIMITS FOUND ON SRM FOR FLOOR SUPPORT BS986-1006 LBL8-LBL17 WL208 PART TO BE REMOVED AND REPLACED I.A.W.SRM 51-10-02-0G-0 PAR 9.C;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] REFeb 4, 2022 · N469WN · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022030369294Stringer · crackedCRACK ON STRINGER TIE STA 277; AT STR 9R; RBL 46; WL 261; FWD SIDE OF FRAME. / [01] REMOVED DAMAGED STRINGER TIE STA 277; AT STR 9R; RBL 46; WL 261 ON FWD SIDE OF FRAME PER SRM 51-40-02-0G-0.;[02] HFEC INSPECTED DAMAGED STRINGER TIE IAW 737 NDTM PART 6 51-00-0Feb 4, 2022 · N469WN · Boeing 737* · Fuselage Main, StructureSDR SWAA2022030369142None · crackedCRACK ON 294 FLOORBEAM UPPER CHORD RBL 52; WL 208 COMMON TO FSD MOPSILL. / [01] NO ALLOWABLE LIMIT FOR CRACK ON SPECIFIC LOCATION DAMAGE TO BE REMOVED AND REPAIRED I.A.W SRM 51-10-02-0G-0 AND SRM 53-10-51-2R-16 REPAIR 1609] HFEC INSPECTED CUT EDGE AREA IAW 737Feb 4, 2022 · N469WN · Boeing 737* · Fuselage Main, Floor BeamSDR SWAA2022030368949Floor Panel · damagedFWD PASSENGER CABIN FLOOR PANEL 221BF HAS DAMAGED INSERTS. / [01] IDENTIFIED PANEL 221BF IAW SRM 53-00-50-0I-1 FIG 2; TABLE 2. <BR><BR>CLEANED PANEL IAW SRM 53-00-50-2R-0 PARA 5. A. (1). <BR><BR>REMOVED (1) EACH CORRODED BLIND INSERTS AND (19) EACH CORRODED THFeb 4, 2022 · N469WN · Boeing 737* · Fuselage Floor PanelSDR SWAA2022030368950Floor Panel · pulledFWD PASSENGER CABIN FLOOR PANEL 221DF UPPER SKIN HAS AREAS OF PULLED STRANDS. / [01] DUE TO THE EXTENT OF DAMAGE; REPLACED FLOOR PANEL 221DF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-50D ITEM 158.;[02] VERIFIED CORRECTIVE ACTION 1Feb 4, 2022 · N469WN · Boeing 737* · Fuselage Floor PanelSDR SWAA2022030368944Floor Panel · pulledFWD PASSENGER CABIN FLOOR PANEL 222BF UPPER SKIN HAS AREAS OF PULLED STRANDS. / [01] DUE TO THE EXTENT OF DAMAGE; REPLACED FLOOR PANEL 222BF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-50D ITEM 96.;[02] VERIFIED CORRECTIVE ACTION 1Feb 4, 2022 · N469WN · Boeing 737* · Fuselage Floor PanelSDR SWAA2022030368947Floor Panel · pulledPASSENGER CABIN FLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS. / [01] IDENTIFIED PANEL MATERIAL IAW SRM 53-00-50-0I-1 FIG 4 TABLE 4.<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4F.<BR>DUE TO THE EXTENT OF DAMAGE CUT NEW Feb 4, 2022 · N469WN · Boeing 737* · Fuselage Floor PanelSDR SWAA2022030368958Floor Panel · pulledAFT PASSENGER CABIN FLOOR PANEL 241XF UPPER SKIN HAS AREAS OF PULLED STRANDS. / [01] IDENTIFIED PART AND MATERIAL ID PER SRM 53-00-50-0I-1 FIG.6; SHT.1; AN TABLE 6. FOUND DAMAGE TO BE OUT OF ALLOWABLE DAMAGE LIMITS PER SRM 53-00-50-1A-1 PAR.4B STEP 2. A REPAIRFeb 4, 2022 · N469WN · Boeing 737* · Fuselage Floor PanelSDR SWAA2022030368960Floor Panel · crackedAFT PASSENGER CABIN FLOOR PANEL 242XF UPPER SKIN IS CRACKED. / [01] AFT PASSENGER CABIN FLOOR PANEL 242XF WITH UPPER SKIN CRACK WAS REPLACED DUE TO THE EXTENT OF ALL DAMAGE IAW SRM 51-10-02-0G-0 PARA 9.A.(1).;[02] VERIFIED CORRECTIVE ACTION ITEM 1.Feb 4, 2022 · N469WN · Boeing 737* · Fuselage Floor PanelSDR SWAA2022030369128None · corrodedCORROSION ON 986 FLOORBEAM UPPER CHORD AT LBL 44 AND AT RBL 44; WL 208. / [01] VERIFY APPLICABILITY PER SRM 53-70-51-1A-1; NSTALLED L/H BS986 RBL1-LBL55 T-CHORD REPAIR I.A.W SRM 53-70-51-2R-4 REPAIR 4 ALTERNATIVE 2 PAR.4.N-O.;INSTALLED R/H BS986 RBL22-RBL55 T-Feb 4, 2022 · N469WN · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022030369130None · corrodedCORROSION ON AFT SERVICE MOPSILL STA 953-992.8; RBL 45-54; WL 208. / [01] VERIFY APPLICABILITY PER SRM 53-70-15-1A-1 ALLOWABLE DAMAGE 1;[02] REMOVED CORROSION ON ASD MOPSILL 40'X 2' BS953-BS993 RBL45-RBL54 WL 208 ORIGINAL MATERIAL THICKNESS IS 0.080 LOWEST MATFeb 4, 2022 · N469WN · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022030369133Strap · corrodedCORROSION ON SHEARWEB STRAP STA 1006-1028; LBL 3-LBL 8; WL 208. / [01] NO ALLOWABLE LIMITS FOUND ON SRM FOR SHEAR WEB STRAP BS1006-1028 LBL3-LBL8 WL208 PART TO BE REMOVED AND REPLACED I.A.W.SRM 51-10-02-0G-0 PAR 9.C;[02] VERIFIED CORRECTIVE ACTION STEP 1;[03] Feb 4, 2022 · N469WN · Boeing 737* · Fuselage Main, StructureSDR SWAA2022030369134Strap · corrodedCORROSION ON AFT SHEARWEB STRAP STA 1016-1018; RBL 3; WL 208. / [01] NO ALLOWABLE LIMITS FOUND ON SRM FOR SHEAR WEB STRAP BS1016-1018 RBL3 WL208 PART TO BE REMOVED AND REPLACED I.A.W.SRM 51-10-02-0G-0 PAR 9.C;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] REMOVEFeb 4, 2022 · N469WN · Boeing 737* · Fuselage Main, StructureSDR SWAA2022030766911Skin · crackedRT HORIZONTAL STAB LOWER IN-SPAR SKIN, CRACKED INBOARD OF RIB AT HSS 193.90, CRACK IS .200' LONG & 17.2' FROM FRONT SPAR. REMOVED DAMAGED SECTION IAW SRM 55-10-01-2R-11 PARA 4A; 4B(2) AND 4C. NO INITIAL REPAIR OR MULTIPLE SITE DAMAGE NOTED. HFEC INSPECTEDFeb 3, 2022 · N469WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/SkinSDR SWAA2022030368927Intercostal · crackedCRACKED INTERCOSTAL STA 277-294; RBL 1; WL 208. / [01] REMOVED DAMAGED INTERCOSTAL STA 277-294; RBL 1; WL 208 PER SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW INTERCOSTAL STA 277-294; RBL 1; WL 208 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG# 141A5400;. OFeb 3, 2022 · N469WN · Boeing 737* · Fuselage Main, StructureSDR SWAA2022030368938Attach Angle · crackedCRACKED INTERCOSTAL ATTACH ANGLE STA 500D-520; BL0; WL 208. / [01] REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE AT BS 500D-520 BL0 WL208 IAW SRM 51-40-05; SRM 51-40-02 BOEING DWG 143A5400;[02] VERIFIED CORRECTIVE ACTION 1. PART REPLACED.;[03] VERIFIED ALL WORFeb 3, 2022 · N469WN · Boeing 737* · Fuselage Main, StructureSDR SWAA2022030368937Attach Angle · crackedCRACKED INTERCOSTAL ATTACH ANGLE STA 380-400; RBL 41; WL 208. / [01] REMOVED DAMAGED INTERCOSTAL ATTACH ANGLE STA 380-400; RBL 41; WL 208 PER SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW INTERCOSTAL ATTACH ANGLE STA 380-400; RBL 41; WL 208 PER SRM 51-40-02-Feb 3, 2022 · N469WN · Boeing 737* · Fuselage Main, StructureSDR SWAA2022030368936Intercostal · crackedCRACKED INTERCOSTAL ATTACH ANGAL STA 380-400; RBL 9; WL 208. / [01] REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE AT BS 380-400 RBL9 WL208 IAW SRM 51-40-05;SRM 51-40-02 BOEING DWG 143A5400;[02] VERIFIED CORRECTIVE ACTION 1. PART REPLACED.;[03] VERIFIED ALL WORFeb 3, 2022 · N469WN · Boeing 737* · Fuselage Main, StructureSDR SWAA2022030368942Intercostal · crackedCRACKED INTERCOSTAL ATTACH ANGLE STA 380-400; BL0; WL 208. / [01] NO DAMAGE LIMITS GIVEN IN SRM PART REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0;[02] REMOVED CRACK DAMAGED INTERCOSTAL ATTACH ANGLE BETWEEN BS 380 AND 400 BL O WL 208 LOCATED AND DRILLED NEW Feb 3, 2022 · N469WN · Boeing 737* · Fuselage Main, StructureSDR SWAA2022030368941Intercostal · crackedCRACKED INTERCOSTAL STA 344-360; LBL 11; WL 208. / [01] REMOVED DAMAGED INTERCOSTAL STA 344-360; LBL 11; WL 200-208 PER SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW INTERCOSTAL STA 344-360; LBL 11; WL 208 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG#141A54Feb 3, 2022 · N469WN · Boeing 737* · Fuselage Main, StructureSDR SWAA2022030368935Intercostal · crackedCRACKED INTERCOSTAL STA 344-360; BL0; WL 208. / [01] REMOVED DAMAGED INTERCOSTAL STA 344-360; BL0; WL 200-208 PER SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW INTERCOSTAL STA 344-360; BL0; WL 208 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG#141A5400. OK TOFeb 3, 2022 · N469WN · Boeing 737* · Fuselage Main, StructureSDR SWAA2022030368932Intercostal · crackedCRACKED INTERCOSTAL STA 344-360; RBL 32; WL 208. / [01] UPDATED TABLE;[02] REMOVED DAMAGED INTERCOSTAL STA 344-360; RBL 32; WL 208 PER SRM 51-40-02-0G-0.;[03] LOCATED AND DRILLED NEW INTERCOSTAL STA 344-360; RBL 32; WL 208 PER SRM 51-40-02-0G-0; SRM 51-40-05-0Feb 3, 2022 · N469WN · Boeing 737* · Fuselage Main, StructureSDR SWAA2022030368931Intercostal · crackedCRACKED INTERCOSTAL STA 312-328; RBL 31; WL 208. / [01] REMOVED INTERCOSTAL AT BS312-328; RBL31; WL208; IAW SRM 51-40-02. LOCATED HOLES; DRILLED; AND DEBURRED NEW INTERCOSTAL PO#234228 IAW SRM 51-40-05-0G-0; FIGURE 4.; SHEET 2 AND BOEING DWG141A5400. OK TO INSFeb 3, 2022 · N469WN · Boeing 737* · Fuselage Main, StructureSDR SWAA2022030368929Intercostal · crackedCRACKED INTERCOSTAL STA 328-344; LBL 44; WL 208. / [01] UPDATE MEASUREMENTS;[02] REMOVED INTERCOSTAL ON STA 328-344; LBL 44; WL 208 IAW SRM 51-40-02-0G-0 TEM 7.D RECEIVE PO/LOT 234228/033194. OK TO INSTALL;[03] REMOVED INTERCOSTAL ON STA 328-344; LBL 44; WL 20Feb 3, 2022 · N469WN · Boeing 737* · Fuselage Main, StructureSDR SWAA2022030368940Intercostal · crackedCRACKED INTERCOSTAL STA 312-328; LBL 44; WL 208. / [01] UPDATED MEASUREMENTS.;[02] REMOVED INTERCOSTAL ON STA 312-328; LBL 44; WL 44; WL 208 IAW SRM 51-40-02-0G-0 ITEM 7.D AND RECEIVE PO/LOT 233222/033530. OK TO INSTALL;[03] REMOVED INTERCOSTAL ON STA 312-328;Feb 3, 2022 · N469WN · Boeing 737* · Fuselage Main, StructureSDR SWAA2022030368924Channel · crackedFWD ENTRY DOOR MOPSILL IS CRACKED COMMON TO 303 FRAME; LBL 59; WL 209. / [01] VERIFY APPLICABILITY PER SRM 53-10-15-1A-1 PAR.4.C(1)(A);[02] NO ALLOWABLE TYPICAL FIGURE LIMIT FOUND ON SRM 53-10-15-1A-1 PAR.4.C(1)(A) FOR SPECIFIC CRACK ON BS303 LBL 59 WL209 PARTFeb 3, 2022 · N469WN · Boeing 737* · Fuselage Main, StructureSDR SWAA2022030367085Support · corrodedCORROSION ON FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S. 480+14; 480+18; 500+4; 500+5; 500+10; 500+18; 500A+6; 500A+10; 500A+14 AND 500A+18; L.B.L. 25. / [01] EVALUATED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO Feb 3, 2022 · N469WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022030367086Support · corrodedCORROSION ON FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S. 500B+6; 500B+14; 500C+2 AND 500C+13 L.B.L. 25. / [01] EVALUATED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 500B+6 RBL 25 WL 156 FOUND 0.015 REMOVEFeb 3, 2022 · N469WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022030367083Support · corrodedCORROSION ON FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S. 500A+2; 500A+6; 500A+10; 500A+14; 500B+10 AND 500C+10; R.B.L. 25. / [01] EVALUATED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 500A+6 RBL 25 WL 156Feb 3, 2022 · N469WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022030368926Intercostal · corrodedCORROSION ON INTERCOSTAL UPPER SURFACE STA 294-312; LBL 10; WL 208. / [01] UPDATE MEASUREMENTS;[02] REMOVED INBTERCOSTAL ON UPPER SURFACE STA 294-312; LBL 10; WL 208 IAW. SRM 51-40-02-0G-0 ITEM 7.D;[03] DISPLACED INTERCOSTAL BETWEEN BS 294-312; BL0 WL 208 IAW Feb 3, 2022 · N469WN · Boeing 737* · Fuselage Main, StructureSDR SWAA2022030367082Shield · corrodedCORROSION ON FORWARD CARGO BAY SHIELD AT B.S. 420+16; R.B.L. 24. / [01] EVALUATED CORROSION ON SHIELD BS 420+16 RBL 24 WL 156; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;[02] VERIFIED CORRECTIVE ACTION Feb 3, 2022 · N469WN · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022030368925Support Angle · corrodedCORROSION ON FWD ENTRY SCUFFPLATE SUPPORT ANGLE COMMON TO FWD ENTRY MOPSILL STA 317-323; 337-341; LBL 59-60; WL 209. / [01] NO ALLOWABLE LIMITS FOUND ON SRM PART TO BE REMOVED AND REPLACED I.A.W.SRM 51-10-02-0G-O PAR 9.C;[02] VERIFIED CORRECTIVE ACTION 1;[03] Feb 3, 2022 · N469WN · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022030368928None · corrodedCORRODED BS 312 FLOORBEAM LBL 36-LBL 42; WL 208. NO ALLOWABLE LIMITS IN SRM. REMOVED CORROSION IAW SRM 51-10-02-0G-0. NDI UT INSPECTION, FOUND REPAIRABLE IAW SRM 53-10-51-2R-15 REPAIR 15, FLAP PEEN BLENDED AREAS IAW SRM 53-10-51-2R-15 REPAIR 15 PAR.4.B(2Feb 3, 2022 · N469WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2022030368939Bracket · corrodedCORROSION ON FWD ENTRY GIRT BAR FITTING SUPPORT BRACKET STA 312; LBL 54; WL 209. / [01] NO LIMITS FOUND ON SRM FOR FED GIRT BAR FITTING SUPPORT BRACKET BS312 LBL54 WL209 PART TO BE REMOVED AND REPLACED I.A.W SRM 51-10-02-0G-0 PAR 9.C;[02] REMOVED FED GIRT BAR Feb 3, 2022 · N469WN · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022030368934None · corrodedCORROSION ON FWD SERVICE MOPSILL STA 296; RBL 55-56; STA 304; RBL 56-57; STA 323-335; RBL 57-58; WL 208. / [01] VERIFY APPLICABILITY PER SRM 53-10-15-1A-2;[02] REMOVED CORROSION ON FSD MOPSILL BS328 RBL 57 WL 208 ORIG.MATERIAL THICKNESS 0.080 LOWEST REMAINING Feb 3, 2022 · N469WN · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022030368933Bracket · corrodedCORROSION ON FWD ENTRY GIRT BAR FITTING SUPPORT BRACKET STA 344; LBL 58; WL 209. / [01] NO LIMITS FOUND ON SRM FOR FED GIRT BAR FITTING SUPPORT BRACKET BS344 LBL58 WL209 PART TO BE REMOVED AND REPLACED I.A.W SRM 51-10-02-0G-0 PAR 9.C;[02] REMOVED FED GIRT BAR Feb 3, 2022 · N469WN · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022030366889Scuff Plate · crackedAFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED / [01] UPDATED MEASUREMENT TABLE AND VERIFIED SRM 53-60-15-2R-1 TO BE CORRECT;[02] WELDED CRACKS ON ACB; AFT CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT # 1131216 PER SRM 53-60-15-2R-1 PARA 4.B.(2) AND (4)<BR>Feb 2, 2022 · N469WN · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022030366900Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 231EF IS DELAMINATED ON UPPER SURFACE. / [01] DUE TO THE EXTENT OF DAMAGE; REPLACED FLOOR PANEL 231EF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-51-81 ITEM 35.;[02] VERIFIED CORRECTIVE ACTION 1.Feb 2, 2022 · N469WN · Boeing 737* · Fuselage Floor PanelSDR SWAA2022030366905Stiffener · crackedCRACKED STIFFENER BEHIND WATER SERVICE PANEL AT ACB BS914 RBL11. / [01] EVALUATED STIFFENER BS 914 RBL 11 WL 169; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.;[03]Feb 2, 2022 · N469WN · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022030366909Stiffener · crackedCRACKED STIFFENER BEHIND WATER SERVICE PANEL AT ACB BS918 RBL11. / [01] EVALUATED CRACKED STIFFENER; BS 918 RBL 11 WL 170; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-0-2-0G-0;[02] UPDATED MEASUREMENT FIELD;[03]Feb 2, 2022 · N469WN · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022030366883Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS727A+18 - BS767 RBL21. / [01] EVALUATED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 727A+18 RBL 21 WL 156; FOUND 0.015 REMOVED FROM ORIG 0.040 IN 1'X1' ARFeb 2, 2022 · N469WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022030366884Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS767+10 - BS787; 749; 727E+2; 727D+10; BS727C. LBL21. / [01] EVALUATED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 727D+10 LBL 21 WL 156; FOUND 0.015 REMOVFeb 2, 2022 · N469WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022030366902Shield · corrodedCORROSION ON FWD SHIELD AT AFT CARGO BAY BS767+7 RBL22. / [01] EVALUATED CORROSION ON SHIELD BS 767+7 RBL 22 WL 156; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.;[Feb 2, 2022 · N469WN · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022030366898Intercostal · corrodedCORROSION ON INTERCOSTAL AT AFT CARGO BAY BS787+8 RBL6. / [01] EVALUATED CORROSION ON INTERCOSTAL BS 787+8 RBL 6 WL 153-154; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;[02] VERIFIED CORRECTIVE ACTION ENFeb 2, 2022 · N469WN · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022030366897Track · corrodedCORROSION ON TRACK AT ACB BS727A RBL13. MARKED. / [01] EVALUATED CORROSION AT BS 727A RBL 13 WL 156; FOUND 0.020 REMOVED FROM ORIG 0.071 IN 1'X1' AREAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DIAL DEPTH GAUGE ATS 2473; TRACK TO BE REPLACED ON CUSFeb 2, 2022 · N469WN · Boeing 737* · Fuselage Internal Mounting StructureSDR SWAA2022030366899Splice · corrodedCORROSION ON FLOOR SUPPORT SPLICE AT ACB BS887 BL0 TO RBL12. / [01] EVALUATED CORROSION ON FLOOR SUPPORT SPLICE BS 887 BL 0 TO RBL 12 WL 168; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;[02] VERIFIED CORFeb 2, 2022 · N469WN · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022030366904Support Angle · corrodedCORROSION ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT ACB BS947 LBL7 TO RBL17. / [01] EVALUATED CORROSION ON BULKHEAD SUPPORT BS 947 LBL 7 TO RBL 17 WL 179; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;[02]Feb 2, 2022 · N469WN · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022030366906Rail · corrodedCORROSION ON RAIL AT ACB BS927+18 RBL3. / [01] EVALUATED CORROSION ON RAIL AT BS 927+18 RBL 3 WL 179; FOUND 0.020 REMOVED FROM ORIG 0.063 IN 1'X1' AREAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USING DIAL DEPTH GAUGE ATS 2473;[02] VERIFIED CORRECTIVE ACFeb 2, 2022 · N469WN · Boeing 737* · Fuselage Miscellaneous StructureSDR SWAA2022030766376Angle · crackedCRACKED VERTICAL STIFFENER ANGLE ON B.S. 663 LOWER COMPOSITE BULKHEAD AT L.B.L. 27; W.L. 150; ON AFT SIDE. / [01] REMOVED VERTICAL STIFFENER ANGLE BS663 LBL27 WL150-WL163 ON AFT SIDE OF LOWER COMPOSITE BLKHD IAW SRM 51-40-02.;[02] LOCATED; DRILLED; AND DEBURREFeb 1, 2022 · N469WN · Boeing 737* · Wing Main, Frame StructureSDR SWAA2021082409245Floor Panel · puncturedCABIN FLOOR PANEL 231ZF HAS PUNCTURE AT INBD EDGE DOT A-21-02 ; / [01] EVALUATED PANEL 231ZF AND FOUND A DENT WITH PUNCTURE AT INBD/EDGE. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-2 PAR 1A REV74.; [02] BOND TEST IAW B737 NDT PART 4; 51-00-05. NO DEFAug 20, 2021 · N469WN · Boeing 7377H4 · Fuselage Floor Panel
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