N429WN

Service difficulty reports · 350

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 = 'N429WN' 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 SWAA2023062053472Baffle · crackedFWD CARGO BAY BAFFLE IS CRACKED AT BS 500B-500C RBL 21 WL 156<[01] VERTIFY APPLICABILITY PER SRM 53-30-53-0I-2 IDENTIFICATION NOT ALLOWABLE DAMAGE PARTS THAT DO NOT HAVE ENTRIES ARE CALLED REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02 STEP 9C;[02] RECEIVED NEW BAMay 29, 2023 · N429WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062151970Skin · corrodedLITE SURFACE CORROSION ON UPPER CROWN SKIN UNDER VERTICAL STAB BETWEEN FUSELAGE STATION 1016 AND 1040 AND STRINGERS 2L AND 2R.<FOUND TO BE OUT OF LIMITS DUE TO MORE THAN THREE AREAS HAVING DAMAGED REMOVAL AROUND THREE FASTENERS OUT OF A GROUP OF TEN IAW SRM 53May 24, 2023 · N429WN · Boeing 7377H4 · Vertical StabilizerSDR SWAA2023062050618Scuff Plate · crackedAFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED<[01] WELDED CRACK ON AFT CARGO BAY AFT CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-60-15-2R-1 REPAIR 1 PARA 4.B. (2) AND (4)<BR>EQUIPMENT USED: WELDING MACHINE E10583; CALIBRATION DUEMay 21, 2023 · N429WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062649669Panel · crackedRT WING T/E PANEL 661BB AFT FASTENER HOLES ARE CRACKING AROUND EDGES<[01] IDENTIFIED PANEL 661BB IAW SRM 57-51-01-0I-1 FIGURE 3; TABLE 2; ITEM (9).<BR><BR>PANEL IS BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 57-51-01-1A-1 PARA 4 B (5)(A).<BR><BR>DAMAGE TO BE REPAIRMay 18, 2023 · N429WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2023062163446Panel · crackedRT WING T/E PANEL 661BB AFT FASTENER HOLES ARE CRACKING AROUND EDGES<DAMAGE TO BE REPAIRED IAW SRM 51-70-04-2R-9 AS DIRECTED BY SRM 57-51-01-2R-1 PARA 4 B (2) TABLE 202.<BR><BR>REMOVED DAMAGE TO (52EA) FASTENER HOLES ALL TO A MEASURE OF .5'DIA; CLEANED; WITH NMay 18, 2023 · N429WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2023062149667Flap · delaminatedLT WING O/B AFT FLAP HAS AREA OF DELAMINATION ON UPPER SURFACE NEAR I/B AFT CORNER.<[01] IDENTIFIED AFT FLAP IAW SRM 57-53-01-0I-4; FIG 2; TABLE 2; ITEM 2.<BR><BR>DAMAGE IS BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 57-53-01-1A-4 PARA 4.A (5).<BR><BR>DAMAGE IS REPMay 17, 2023 · N429WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2023062148969Intercostal · crackedINTERCOSTAL CRACKED AT BS 259.5; WL 207; LBL 5<[01] RECIVED FABRICATED INTERCOSTAL FROM OSS LOT # 1528128-1 CUSTOMER RO NO 920188-SWA; AND LOCATED AND DRILLED NEW PART IAW SRM 51-40-05-0G-0 DGW 141A5100; APPLIED CHEMICAL CONVERSION COATING IAW SRM 51-20-01-0G-May 16, 2023 · N429WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2023062049269Frame · crackedBS 312 FRAME CRACKED AT FED HEADER FRAME<[01] ACCOMPLISHED REPAIR PER EA#M-22-153-01244 ON FAULT#TTG8Q00L4U7D;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLEMay 16, 2023 · N429WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2023062048958Intercostal · crackedINTERCOSTAL AT AFT INNER RADIUS IS CRACKED BS 947; RBL 23; WL 165. (MARKED)<[01] REMOVED INTERCOSTAL FROM AFT CARGO BAY BS 927 TO BS 947 RBL 23 WL 165 IAW SRM 51-40-02-0G-0;[02] VERIFY APPLICABILITY PER SRM NOT ALLOWABLE DAMAGE DO NOT HAVE ENTRIES ARE CALLED RMay 15, 2023 · N429WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062048275Floor Panel · pulledFLOOR PANEL 242DF UPPER SURFACE HAS PULLED STRANDS.<[01] PANEL DAMAGE TO MARKED AREA WITH PULLED STRANDS EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PAR. 4. F.<BR><BR>FABRICATING NEW FLOORBOARD IAW SRM 53-00-50-2R-0 PAR. 1. A. NOTE:<BR><BR>FABRICATEDMay 13, 2023 · N429WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023062048266Floor Panel · pulledFLOOR PANEL 241FF UPPER SURFACE HAS PULLED STRANDS.<[01] DUE TO EXTENT OF THE DAMAGE FABRICATED NEW FLOOR PANEL 241FF FROM BMS4-17 TYPE 6 LOT#1526676-1; LOCATED AND INSTALLED ALL INSERTS USING BMS5-107 LOT# AK2KP8383K-1; CURED INSERTS USING HEAT LAMP AND THERMMay 13, 2023 · N429WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023062048268Floor Panel · pulledFLOOR PANEL 242CF UPPER SURFACE HAS PULLED STRANDS.<[01] PART/MATERIAL IDENTIFIED PER SRM 53-00-50-0I-1 FIGURE 4 TABLE 4 SECTION 44. <BR>UPPER SURFACE DAMAGE EXCEEDS THE ALLOWABLE LIMITS AS GIVEN IN SRM 53-00-50-1A-1 PARA 4 SECTION. 44.<BR>DAMAGED FLOOR PANEL May 13, 2023 · N429WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023062048274Floor Panel · pulledFLOOR PANEL 241EF UPPER SURFACE HAS PULLED STRANDS.<[01] DUE TO EXTENT OF THE DAMAGE FABRICATED NEW FLOOR PANEL 241EF FROM BMS4-17 TYPE 6 LOT#1526676-1; LOCATED AND INSTALLED ALL INSERTS USING BMS5-107 LOT# AK2KP8383K-1; CURED INSERTS USING HEAT LAMP AND THERMMay 13, 2023 · N429WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023062048265Floor Panel · pulledFLOOR PANEL 241DF UPPER SURFACE HAS PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; FABRICATED NEW FLOOR PANEL 241DF USING BMS 4-17TY6 LOT#1526676-2; INSTALLED INSERTS USING BMS 5-107 LOT#AK2KP8383K; CURED WITH THERMOMETER ID:ATS2208 CAL DUE 10/2023; PART MAMay 13, 2023 · N429WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023062048267Floor Panel · pulledFLOOR PANEL 242AF UPPER SURFACE HAS PULLED STRANDS.<[01] IDENTIFIED PANEL MATERIAL IAW SRM 53-00-50-0I-1 SHEET 1; FIGURE 4; TABLE 4; AND DWG DOC: 144A5810 ID: 0189<BR><BR>PANEL UPPER SURFACE DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM <BR>53-00-50-1A-1 PAR.May 13, 2023 · N429WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023062048273Floor Panel · pulledFLOOR PANEL 241CF UPPER SURFACE HAS PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; FABRICATED NEW FLOOR PANEL 241CF USING BMS 4-17TY6 LOT#1526676-2; INSTALLED INSERTS USING BMS 5-107 LOT#AK2KP8383K; CURED WITH THERMOMETER ID:ATS2208 CAL DUE 10/2023 AND PARTMay 13, 2023 · N429WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023062048261Floor Panel · pulledFLOOR PANEL 241XF UPPER SURFACE HAS PULLED STRANDS. PANEL SHOULD BE 231XF DUE TO THE FAULT DETAILS ON THIS DEFECT MENTIONING THE OPEN OF PANEL 231XF.<[01] IDENTIFIED FLOOR PANEL 231XF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 4 TABLE 4 AND BAC DWG 144A5810 ID: 012May 13, 2023 · N429WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023062048262Floor Panel · pulledFLOOR PANEL 231ZF UPPER SURFACE HAS PULLED STRANDS.<[01] IDENTIFIED FLOOR PANEL 231ZF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 4 TABLE 4 AND BAC DWG 144A5810 ID: 0160. DAMAGE TO UPPER SURFACE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.F. FLMay 13, 2023 · N429WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023062048271Floor Panel · pulledFLOOR PANEL 232RF UPPER SURFACE HAS PULLED STRANDS.<[01] IDENTIFIED FLOOR PANEL 232RF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 4 TABLE 4. DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.F. DAMAGE TO FLOOR PANEL IS BEYOND ECONOMICAL REPAIRMay 13, 2023 · N429WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023062048263Floor Panel · pulledFLOOR PANEL 232SF UPPER SURFACE HAS PULLED STRANDS.<[01] IDENTIFIED FLOOR PANEL 232SF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 4 TABLE 4. DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.F. DAMAGE TO FLOOR PANEL IS BEYOND ECONOMICAL REPAIRMay 13, 2023 · N429WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023062048264Floor Panel · pulledFLOOR PANEL 241AF UPPER SURFACE HAS PULLED STRANDS.<[01] IDENTIFIED PANEL 241AF MATERIAL IAW SRM 53-00-50-0I-1 FIG 4 AND TABLE 4.<BR><BR>DAMAGE TO PANEL 241BF IS OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4. F. AND BEYOND ECONOMICAL REPAIR.<BR><BR>NEW May 13, 2023 · N429WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023062048272Floor Panel · pulledFLOOR PANEL 241BF UPPER SURFACE HAS PULLED STRANDS.<[01] IDENTIFIED PANEL 241BF MATERIAL IAW SRM 53-00-50-0I-1 FIG 4 AND TABLE 4.<BR><BR>DAMAGE TO PANEL 241BF IS OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4. F. AND BEYOND ECONOMICAL REPAIR.<BR><BR>NEW May 13, 2023 · N429WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023062163434Track · crackedCRACKED TRACK AT ACB BS767 RBL13 WL156.<[01] CRACKED TRACK AT ACB BS767 RBL13 WL156 FOUND TO BE OUT OF LIMITS DUE TO CRACKS ARE NOT PERMITTED PER SRM 53-00-53-1A-2;[02] VERIFIED CORRECTIVE ACTION 1;[03] REMOVED TRACK AT ACB FROM BS 727 TO BS 887 RBL13 WL 156 IMay 12, 2023 · N429WN · Boeing 7377H4 · Fuselage Internal Mounting StructureSDR SWAA2023062148256Attach Angle · crackedCRACKED BULKHEAD PANEL SUPPORT ATTACH ANGLE AT ACB BS847+19 LBL10 WL167.<[01] RECIVED NEW ATTACH ANGLE ITEM P/N 149A8109-114 LOCATED AND DRILLED NEW ATTACH ANGLE AT ACB BS 847+19 LBL10 WL167; IAW B 737-700 SRM 51-40-05-0G-0 DWG 149A8102 REV:A;[02] VERIFIED CORMay 12, 2023 · N429WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062148232Track · crackedCRACKED TRACK AT ACB BS767 RBL13 WL156.<[01] CRACKED TRACK AT ACB BS767 RBL13 WL156 FOUND TO BE OUT OF LIMITS DUE TO CRACKS ARE NOT PERMITTED PER SRM 53-00-53-1A-2;[02] VERIFIED CORRECTIVE ACTION 1;[03] REMOVED TRACK AT ACB FROM BS 727 TO BS 887 RBL13 WL 156 IMay 12, 2023 · N429WN · Boeing 7377H4 · Fuselage Internal Mounting StructureSDR SWAA2023062163437Frame · corrodedCORROSION ON FRAME AT ACB BS947 LBL9 WL180..<[01] VERIFIED APPLICABILITY OF SRM 53-70-07-01-1 FOR IDENTIFICATION AND SRM 53-00-07-1A-1 FOR ALLOWABLE LIMIT;[02] REMOVED CORROSION FROM AFT CARGO BAY FRAME INNER CHORD BS 947 LBL9 WL 180 IN AREA OF 5' X 1.25' ORIGMay 12, 2023 · N429WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2023062163435Shield · corrodedCORROSION ON FWD SHIELD AT ACB BS767 - BS787 RBL21 WL158.<[01] CORROSION ON FWD SHIELD AT AFT CARGO BAY; LOCATED BETWEEN BS767 - BS 787; FOUND TO BE OUT OF LIMIT DUE TO NO ALLOWABLE DAMAGE ON SRM; PART WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR-May 12, 2023 · N429WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062148259Frame · corrodedCORROSION ON FRAME AT ACB BS947 LBL9 WL180..<[01] VERIFIED APPLICABILITY OF SRM 53-70-07-01-1 FOR IDENTIFICATION AND SRM 53-00-07-1A-1 FOR ALLOWABLE LIMIT;[02] REMOVED CORROSION FROM AFT CARGO BAY FRAME INNER CHORD BS 947 LBL9 WL 180 IN AREA OF 5' X 1.25' ORIGMay 12, 2023 · N429WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2023062148245Shield · corrodedCORROSION ON FWD SHIELD AT ACB BS767 - BS787 RBL21 WL158.<[01] CORROSION ON FWD SHIELD AT AFT CARGO BAY; LOCATED BETWEEN BS767 - BS 787; FOUND TO BE OUT OF LIMIT DUE TO NO ALLOWABLE DAMAGE ON SRM; PART WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR-May 12, 2023 · N429WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062048260Support Angle · crackedCRACKED SUPPORT ANGLE AT ACB BEHIND WATER SERVICE PANEL BS914 RBL11 WL171.<[01] REMOVED SUPPORT ANGLE AT ACB BS 914 RBL 11 WL 171 IAW SRM 51-40-02-0G-0. NO ALLOWABLE DAMAGE ; PART WILL BE REPAIRABLE BY REPLACEMENT IAW 51-10-02-0G-0 STEP 9.;[02] LOCATED AND DRIMay 12, 2023 · N429WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062048269Support Angle · crackedCRACKED SUPPORT ANGLE AT ACB BEHIND WATER SERVICE PANEL BS918 RBL11 WL171.<[01] REMOVED SUPPORT ANGLE AT ACB BS 918 RBL 11 WL 171 IAW SRM 51-10-02-0G-0. NO ALLOWABLE DAMAGE; PART WILL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0.;[02] LOCATED AND DRILLEDMay 12, 2023 · N429WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062048257Intercostal · corrodedCORROSION ON INTERCOSTAL AT ACB BS867+2 LBL10 WL162.<[01] CORROSION ON INTERCOSTAL AT AFT CARGO BAY; LOCATED BETWEEN BS.867+2' - LBL10; WL.162 FOUND TO BE OUT OF LIMIT DUE TO NOT HAS ENTRIES ALLOWABLE DAMAGE IN SRM; PART WILL BE REPAIRED BY REPLACEMENT IAW SRMMay 12, 2023 · N429WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2023062048254Stringer Clip · corrodedCORROSION ON STRINGER CLIP AT ACB BS847 S-27L LBL6.<[01] EVALUATED CORROSION DAMAGE ON STRINGER CLIP AT ACB BS 847 S-27L LBL6 FOUND TO BE OUT OF LIMITS DUE NOT LIMITS IN SRM PARTS WILL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0;[02] REMOVED STRINGER CLMay 12, 2023 · N429WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062048238Stringer Clip · corrodedCORROSION ON STRINGER CLIP AT ACB BS827 S-27L LBL6.<[01] EVALUATED CORROSION DAMAGE ON STRINGER CLIP AT ACB BS 827 S-27L LBL6 FOUND TO BE OUT OF LIMITS DUE NOT LIMITS IN SRM PARTS WILL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0;[02] REMOVED STRINGER CLMay 12, 2023 · N429WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2023062048253Stringer Clip · corrodedCORROSION ON CLIP AT ACB BS807 LBL7 WL154.<[01] EVALUATED CORROSION DAMAGE ON CLIP AT ACB BS 807; LBL7 WL 154 FOUND TO BE OUT OF LIMITS DUE NOT LIMITS IN SRM PARTS WILL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0;[02] REMOVED CLIP AT ACB BS 807 LBL7 WL May 12, 2023 · N429WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2023062048237Stringer Clip · corrodedCORROSION ON STRINGER CLIP AT ACB BS807 S-26L LBL14. MARKED.<[01] EVALUATED CORROSION DAMAGE ON STRINGER CLIP AT ACB BS 807 S-26L LBL14 FOUND TO BE OUT OF LIMITS DUE NOT LIMITS IN SRM PARTS WILL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0;[02] REMOVED SMay 12, 2023 · N429WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2023062048246Stringer Clip · corrodedCORROSION ON STRINGER CLIP AT ACB BS787 S-26R RBL15.<[01] EVALUATED CORROSION DAMAGE ON STRINGER CLIP AT ACB BS 787; S-26R RBL15 FOUND TO BE OUT OF LIMITS DUE NOT LIMITS IN SRM PARTS WILL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0;[02] REMOVED STRINGERMay 12, 2023 · N429WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2023062048224Sidewall Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB BS796 - BS727D LBL21 WL158.<[01] VERIFIED SRM 53-60-53-0I-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE.<BR><BR>REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT BS 727E+10 LBL 21 WL 158 IAW SRM 5May 12, 2023 · N429WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062048229Stringer Clip · corrodedCORROSION ON CLIP AT ACB BS787;767; 747; 727E; 727D; 727C; 727B LBL7 WL152. MARKED<[01] EVALUATED CORROSION DAMAGE ON CLIP AT BS 787; 767; 747; 727E; 727D; 727C; 727B; LBL7 WL 152 FOUND TO BE OUT OF LIMITS DUE NOT LIMITS IN SRM PARTS WILL BE REPAIRABLE BY REPLMay 12, 2023 · N429WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062048225Sidewall Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB BS767 - BS727A RBL21 WL158.<[01] VERIFY APPLICABILITY PER SRM 53-60-53-0I-2 AND SRM 53-00-53-1A-2<BR>REMOVED CORROSION ON DISCREPANCY AREA L=3.5'; W=1.7'; D=0.007'. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 SMay 12, 2023 · N429WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062048249Stringer Clip · corrodedCORROSION ON CLIP AT ACB BS727D+5 LBL5 WL152.<[01] EVALUATED CORROSION DAMAGE ON CLIP AT ACB BS 727D+5; LBL5 WL 152 FOUND TO BE OUT OF LIMITS DUE NOT LIMITS IN SRM PARTS WILL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0;[02] REMOVED CLIP ACB AT BS 727D+5May 12, 2023 · N429WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062048250Stringer Clip · corrodedCORROSION ON CLIP AT ACB BS727D+10 LBL7 WL152.<[01] EVALUATED CORROSION DAMAGE ON CLIP AT ACB BS 727D+10; LBL7 WL 152 FOUND TO BE OUT OF LIMITS DUE NOT LIMITS IN SRM PARTS WILL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0;[02] REMOVED CLIP AT ACB BS 727DMay 12, 2023 · N429WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062048248Stringer Clip · corrodedCORROSION ON CLIP AT ACB BS727D+8 LBL5 WL152.<[01] EVALUATED CORROSION DAMAGE ON CLIP AT ACB BS 727D+8; LBL5 WL 152 FOUND TO BE OUT OF LIMITS DUE NOT LIMITS IN SRM PARTS WILL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0;[02] REMOVED CLIP AT ACB BS 727D+8May 12, 2023 · N429WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062048235Stringer Clip · corrodedCORROSION ON CLIP AT ACB BS727D RBL7 WL151.<[01] EVALUATED CORROSION DAMAGE ON CLIP AT ACB BS 727D; RBL7 WL 151 FOUND TO BE OUT OF LIMITS DUE NOT LIMITS IN SRM PARTS WILL BE REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0;[02] REMOVED CLIP AT ACB BS 727D RBL7 May 12, 2023 · N429WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062048251Sidewall Support · corrodedFORWARD CARGO COMPARTMENT - MULTIPLE AREA OF CORROSION ON AFT BULKHEAD SIDE WALL SUPPORT BS500C+18.25 STRG 19L TO STR 25L. (MARKED)<[01] REMOVED CORROSION ON AFT BULKHEAD SIDE WALL SUPPORT BS500C+18.25 STRG 19L TO STR 25L. PER REF SRM 53-30-08-1A-1 L=1;W=1<BR>May 12, 2023 · N429WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062048252Sidewall Support · corrodedFORWARD CARGO COMPARTMENT - MULTIPLE AREA OF CORROSION ON AFT BULKHEAD SIDE WALL SUPPORT BS500C+18.25 STRG 19R TO STR 25R. (MARKED)<[01] REMOVED CORROSION ON AFT BULKHEAD SIDE WALL SUPPORT BS500C+18.25 STRG 19R TO STR 25R. PER REF SRM 53-30-08-1A-1<BR><BR>BLENMay 12, 2023 · N429WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062048234Floor Support · corrodedFORWARD CARGO COMPARTMENT - MULTIPLE AREA OF CORROSION ON MIDDLE FLOOR SUPPORT BS 500C+18.25 RBL 14; RBL 20. (MARKED)<[01] REMOVED CORROSION ON MIDDLE FLOOR SUPPORT BS 500C+18.25 RBL 14; RBL 20. PER REF SRM 53-30-08-1A-1 L=1;W=1<BR><BR>BLEND OUT EVALUATION ORIMay 12, 2023 · N429WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062048240Shield · corrodedFORWARD CARGO COMPARTMENT - MULTIPLE AREA OF CORROSION ON AFT DOOR SHIELD BS 480+12 TO BS 500D RBL 24.75<[01] THE STRUCTURAL ITEM DOES NOT HAVE ALLOWABLE DAMAGE ENTRIES. THEREFORE; MUST BE REPAIRED BY REPLACEMENT PER REF SRM 51-10-02-0G-0;[02] REPLACED ;LOCATEMay 12, 2023 · N429WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062048222Sidewall Support · corrodedMULTIPLE AREA OF CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 21 BS 500-500D<[01] VERIFIED APPLICABILITY SRM 53-30-53-0I-2 FOR IDENTIFICATION <BR>AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE.;[02] REMOVED CORROSION IAW SRM 51-10-02.<BR>ON FWD CARGMay 12, 2023 · N429WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023062048221Shield · corrodedFORWARD CARGO COMPARTMENT - MULTIPLE AREA OF CORROSION ON FWD DOOR SHIELD BS 420+12 TO BS 440 RBL 24.75<[01] THE STRUCTURAL ITEM DOES NOT HAVE ALLOWABLE DAMAGE ENTRIES. THEREFORE; MUST BE REPAIRED BY REPLACEMENT PER REF SRM 51-10-02-0G-0;[02] REPLACED;LOCATED May 12, 2023 · N429WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
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