N962WN

Service difficulty reports · 194

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 = 'N962WN' 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 SWAA2023070554175Floor Panel · pulledFLOOR PANEL 241DF UPPER SKIN HAS PULLED STRANDS. THIS FAULT SHOULD BE FOR FLOOR PANEL 231DF NOT 241DF. THIS FAULT WAS GENERATED FROM A 231DF OPEN TASK AND UPPER SKIN PULLED STRANDS HAVE BEEN VERIFIED AS A VALID DISCREPANCY ON 231DF.<[01] IDENTIFIED FLOOR PANELMay 31, 2023 · N962WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023070554179Floor Panel · pulledFLOOR PANEL 241VF UPPER SKIN HAS PULLED STRANDS.<[01] DUE TO THE EXTENT OF ALL OF THE DAMAGE; DECIDED TO FABRICATE A NEW BOARD USING BMS4-17 TYPE VI LOT 1526676-1 AND BMS5-107 CLASS 1 RESIN LOT AK2KP8383K-1; CURED RESIN UNDER A HEAT LAMP USING THERMOMETER ID: May 31, 2023 · N962WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023070554684Intercostal · crackedCRACKED INTERCOSTAL AT FWD CABIN BS380+14 RBL10 WL208.<[01] REMOVED CRACKED INTERCOSTAL AT FWD CABIN BS 380-400 RBL 10 WL 208 IAW SRM 51-40-02;[02] OBTAINED NEW INTERCOSTAL AT FWD CABIN BS380 TO BS 400 BL10 WL208 ; LOCATED AND DRILLED IAW SRM 51-40-05 AND DWG May 31, 2023 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023070554689Stringer · crackedCRACKED STR CLIP AT PASSENGER CABIN BS727B S-7L. MARKED. CORRECTION TO FAULT DETAILS: CRACKED STR CLIP AT BS727E S-7L.<[01] CORRECTION TO FAULT DETAILS: CRACKED STR CLIP AT BS727E S-7L;[02] REMOVED STRINGER CLIP AT BS 727E; STR 7L PER SRM 51-40-02;[03] ALLOWABMay 31, 2023 · N962WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2023070554483Intercostal · crackedCRACKED INTERCOSTAL AT FWD CABIN BS295.5 S-16L WL216.<[01] REMOVED CRACKED INTERCOSTAL AT FWD CABIN BS295.5 S-16L WL216 IAW SRM 51-40-02;[02] LOCATED AND DRILLED NEW INTERCOSTAL P/N 141A8181U51 LOT# 1530110-1 AT FWD CABIN BS 295.5 S-16L WL 216 PER SRM 51-40-05May 31, 2023 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023070565023Floor Panel · pulledFWD FLOOR PANEL 222CF UPPER SKIN HAS PULLED STRANDS.<[01] IDENTIFIED FLOOR PANEL 222CF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 6 TABLE 6.<BR><BR>DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.F. <BR><BR>DAMAGE IS REPAIRABLE IAW SRM 53-0May 31, 2023 · N962WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023070565025Floor Panel · pulledFLOOR PANEL 231GF UPPER SKIN HAS PULLED STRANDS.<[01] IDENTIFIED 231GF PANEL IAW SRM 53-00-50-0I-1 PARA FIGURE 3; TABLE 3.<BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.F. DUE TO THE EXTENT OF DAMAGE A NEW BOARD WILL BE FABRICATED.May 31, 2023 · N962WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023070565021Floor Panel · pulledFLOOR PANEL 231KF UPPER SKIN HAS PULLED STRANDS.<[01] DUE TO AMOUNT OF DAMAGE; FLOOR PANEL 231KF WILL BE REPLACED WITH NEWLY FABRICATED FLOOR PANEL IAW SRM 53-00-50-2R-0.PARA 1.A.NOTE.<BR><BR>STARTED FABRICATING FLOOR PANEL FROM BMS 4-23 TY 2 LOT#1525675-1; LOMay 31, 2023 · N962WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023070554177Floor Panel · pulledFLOOR PANEL 241RF UPPER SKIN HAS PULLED STRANDS.<[01] IDENTIFIED FLOOR PANEL 241RF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 5 TABLE 5.<BR><BR>DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.F. <BR><BR>DAMAGE TO FLOOR PANEL IS BEYOND ECONOMay 31, 2023 · N962WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023070554178Floor Panel · pulledFLOOR PANEL 241UF UPPER SKIN HAS PULLED STRANDS.<[01] IDENTIFIED FLOOR PANEL 241UF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 5 TABLE 5.<BR><BR>DAMAGE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.F. <BR><BR>DAMAGE TO FLOOR PANEL IS BEYOND ECONOMay 31, 2023 · N962WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023070565029Intercostal · crackedCRACKED INTERCOSTAL AT FWD CABIN BS344+5 BL0 WL208.<[01] VERIFIED APPLICABILITY OF SRM 53-10-51-1A-1 ALLOWABLE DAMAGE 1 - SECTION 41 FLOOR STRUCTURE;[02] ACCOMPLISHED EVALUATION ON INTERCOSTAL AT FWD CABIN STA-344+5'' BL-0 WL208 AND FOUND TO BE OUT OF LIMITS IMay 31, 2023 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023070554482Intercostal · crackedCRACKED INTERCOSTAL AT FWD CABIN BS344+9 RBL12 WL208.<[01] CRACKED INTERCOSTAL AT FWD. CABIN BS344+9 RBL12 WL208 WITH NEXT DIMENSION L=0.600' TOOL USED CALIPER ID: ATS2739; S/N: A22004232; DATE: 11/2022; DUE:11/2023 P/N 141A5410-24; VERIFIED APPLICABILITY OF SMay 31, 2023 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023070554486Intercostal · crackedCRACKED INTERCOSTAL AT FWD CABIN BS344+5 RBL50 WL208.<[01] VERIFIED APPLICABILITY OF SRM 53-10-51-1A-1 ALLOWABLE DAMAGE 1 - SECTION 41 FLOOR STRUCTURE;[02] ACCOMPLISHED EVALUATION ON INTERCOSTAL AT FWD CABIN STA-344+5'' RBL50 WL208 AND FOUND TO BE OUT OF LIMITMay 31, 2023 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023070565049Intercostal · crackedCRACKED INTERCOSTAL AT FWD CABIN BS380+14 BL0 WL208.<[01] REMOVED CRACKED INTERCOSTAL AT FWD CABIN BS380+14 BL0 WL208 IAW SRM 51-40-02;[02] OBTAINED NEW INTERCOSTAL AT FWD CABIN BS380 TO BS 400 BL0 WL208 ; LOCATED AND DRILLED IAW SRM 51-40-05 AND DWG #143A5410May 31, 2023 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023070554686Angle · crackedCRACKED INTERCOSTAL AT FWD CABIN BS380+14 LBL13 WL208.<[01] REMOVED ANGLE INTERCOSTAL;FOUND PART HAS NOT SRM LIMITS AND SO PART IS REPAIRABLE BY REPLACEMENT; IAW SRM 51-10-02 PARAG 9;[02] LOCATED AND DRILLED NEW ANGLE OF INTERCOSTAL<BR>WITH P/N 143A54190-174 LMay 31, 2023 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023070565030Gusset · crackedGUSSET IS CRACKED AT STR 19R; BS 500D<[01] VERIFY APPLICABILITY PER SRM 53-30-08-0I-1. NOT ALLOWABLE DAMAGE PARTS THAT DO NOT HAVE ENTRIES ARE CALLED REPAIRABNLE BY REPLACEMENT IAW SRM 51-10-02 STEP 9C;[02] REMOVED GUSSET AT STR 19R BS 500D IAW SRM 51-40-02;[0May 31, 2023 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023070565031Gusset · crackedGUSSET IS CRACKED AT STR 19L; BS 500D<[01] VERIFY APPLICABILITY PER SRM 53-30-08-0I-1. NOT ALLOWABLE DAMAGE PARTS THAT DO NOT HAVE ENTRIES ARE CALLED REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02 STEP 9C;[02] REMOVED GUSSET AT STR 19L BS 500D IAW SRM 51-40-02;[03May 31, 2023 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023070565032Sidewall Support · corrodedFLOOR TO SIDE WALL SUPPORT HAS CORROSION AT BS 787+7; LBL 22; WL 156<[01] REMOVED CORROSION FROM AFT CARGO BAY FLOOR TO SIDE WALL SUPPORT ANGLE BS 787+7; LBL 22; WL 156; IN AREA OF 1.5' X 1.5' X 0.006' DEEP ORIGINAL MATERIAL THICKNESS 0.040' FOUND TO BE OUT OFMay 31, 2023 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023070565033Sidewall Support · corrodedFLOOR TO SIDE WALL SUPPORT HAS CORROSION AT BS 767-787; LBL 22; WL 156<[01] REMOVED CORROSION FROM AFT CARGO BAY FLOOR TO SIDE WALL SUPPORT ANGLE BS 767-787; LBL 22; WL 156; IN AREA OF 17' X 2.5' X 0.0075' DEEP ORIGINAL MATERIAL THICKNESS 0.040' FOUND TO BE OUMay 31, 2023 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023070565034Sidewall Support · corrodedFLOOR TO SIDE WALL SUPPORT HAS CORROSION AT BS 747-747+16; LBL 22; WL 156<[01] REMOVED CORROSION FROM AFT CARGO BAY FLOOR TO SIDE WALL SUPPORT ANGLE BS 747-747+16; LBL 22; WL 156; IN AREA OF 14' X 2' X 0.008' DEEP ORIGINAL MATERIAL THICKNESS 0.040' FOUND TO BEMay 31, 2023 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023070565035Sidewall Support · corrodedFLOOR TO SIDE WALL SUPPORT HAS CORROSION AT BS 747-747+16; RBL 22; WL 156<[01] REMOVED CORROSION FROM AFT CARGO BAY FLOOR TO SIDE WALL SUPPORT ANGLE BS 747-747+16; RBL 22; WL 156; IN AREA OF 14' X 1.5' X 0.08' DEEP ORIGINAL MATERIAL THICKNESS 0.040' FOUND TO BMay 31, 2023 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023070565036Sidewall Support · corrodedFLOOR TO SIDE WALL SUPPORT HAS CORROSION AT BS 727E+14; LBL 22; WL 156<[01] REMOVED CORROSION FROM AFT CARGO BAY FLOOR TO SIDE WALL SUPPORT ANGLE BS 727E+14; LBL 22; WL 156; IN AREA OF 1' X 1' X 0.006' DEEP ORIGINAL MATERIAL THICKNESS 0.040' FOUND TO BE OUT OFMay 31, 2023 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023070554681Sidewall Support · corrodedFLOOR TO SIDE WALL SUPPORT HAS CORROSION AT BS 727E+2; LBL 22; WL 156<[01] REMOVED CORROSION FROM AFT CARGO BAY FLOOR TO SIDE WALL SUPPORT ANGLE BS 727E+2; LBL 22; WL 156; IN AREA OF 2' X 1' X 0.006' DEEP ORIGINAL MATERIAL THICKNESS 0.040' FOUND TO BE OUT OF LMay 31, 2023 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023070565037Sidewall Support · corrodedFLOOR TO SIDE WALL SUPPORT HAS CORROSION AT BS 727E-747; RBL 22; WL 156<[01] REMOVED CORROSION FROM AFT CARGO BAY FLOOR TO SIDE WALL SUPPORT ANGLE BS 727E-747; RBL 22; WL 156; IN AREA OF 17' X 2' X 0.009' DEEP ORIGINAL MATERIAL THICKNESS 0.040' FOUND TO BE OUTMay 31, 2023 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023070565038Sidewall Support · corrodedFLOOR TO SIDE WALL SUPPORT HAS CORROSION AT BS 727D-727E; LBL 22; WL 156<[01] REMOVED CORROSION FROM AFT CARGO BAY FLOOR TO SIDE WALL SUPPORT ANGLE BS 727D-727E; LBL 22; WL 156; IN AREA OF 17' X 1.5' X 0.008' DEEP ORIGINAL MATERIAL THICKNESS 0.040' FOUND TO BEMay 31, 2023 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023070565040Sidewall Support · corrodedFLOOR TO SIDE WALL SUPPORT HAS CORROSION AT BS 727D-727E; RBL 22; WL 156<[01] REMOVED CORROSION FROM AFT CARGO BAY FLOOR TO SIDE WALL SUPPORT ANGLE BS 727D-727E; RBL 22; WL 156; IN AREA OF 15' X 1.5' X 0.0065' DEEP ORIGINAL MATERIAL THICKNESS 0.040' FOUND TO BMay 31, 2023 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023070565041Sidewall Support · corrodedFLOOR TO SIDE WALL SUPPORT HAS CORROSION AT BS 727C-727C+12; LBL 22; WL 156<[01] REMOVED CORROSION FROM AFT CARGO BAY FLOOR TO SIDE WALL SUPPORT ANGLE BS 727C-727C+12; LBL 22; WL 156; IN AREA OF 11' X 1.5' X 0.008' DEEP ORIGINAL MATERIAL THICKNESS 0.040' FOUNDMay 31, 2023 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023070565042Sidewall Support · corrodedFLOOR TO SIDE WALL SUPPORT HAS CORROSION AT BS 727C-727C+12; RBL 22; WL 156<[01] REMOVED CORROSION FROM AFT CARGO BAY FLOOR TO SIDE WALL SUPPORT ANGLE BS 727C-727C+12; RBL 22; WL 156; IN AREA OF .5' X 1' X 0.007' DEEP ORIGINAL MATERIAL THICKNESS 0.040' FOUND TMay 31, 2023 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023070565045Sidewall Support · corrodedFLOOR TO SIDE WALL SUPPORT HAS CORROSION AT BS 727B-727C; RBL 22; WL 156<[01] REMOVED CORROSION FROM AFT CARGO BAY FLOOR TO SIDE WALL SUPPORT ANGLE BS 727B-727C; RBL 22; WL 156; IN AREA OF 17' X 1' X 0.008' DEEP ORIGINAL MATERIAL THICKNESS 0.040' FOUND TO BE OMay 31, 2023 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023070554673Web · corrodedSUB THRESHOLD IS CORRODED AT BS 847-787+11; RBL 26; WL 162<[01] VERIFIED APPLICABILITY PER REF SRM 53-60-15-0I-1 AND SRM 53-60-15-1A-1 <BR><BR>REMOVED CORROSION ON SUB THRESHOLD AT BS 847-787+11; RBL 26; WL 162 L=1 W=1 . ORIGINAL MATERIAL THICKNESS IS .050'' AMay 31, 2023 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023070554690Support · corrodedFLOOR TO SIDE WALL SUPPORT HAS CORROSION AT BS 727B+10-727B+16; LBL 22; WL 156<[01] REMOVED CORROSION FROM AFT CARGO BAY FLOOR TO SIDE WALL SUPPORT ANGLE BS 727B+10-727B+16; LBL 22; WL 156; IN AREA OF 6' X 1.5' X 0.0075' DEEP ORIGINAL MATERIAL THICKNESS 0.040'May 31, 2023 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023070565016Floorbeam · corrodedBS 986 FLOOR BEAM UPPER CHORD HAS CORROSION AROUND THE NUT PLATE HOLE AT LBL 45<[01] SRM 53-70-51-1A-1 ALLOWABLE DAMAGE 1 AND SRM 53-70-51-2R-6 REPAIR 6 ARE APPLICABLE TO THIS A/C;[02] CORROSION AROUND THE NUTPLATE HOLE AT LBL45 OF BS 986 FLOOR BEAM UPPER CHORMay 30, 2023 · N962WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2023070553604Panel · pulledR/W T/E PANEL 661CB HAS SEVERAL PULLED FASTENER HOLE ON AFT END (MARKED)<[01] PART/MATERIAL IDENTIFIED PER SRM 57-51-01-0I-1 FIGURE 3 TABLE 3 ITEM 10.<BR>MULTIPLE PULLED FASTENER HOLES EXCEED THE ALLOWABLE LIMITS AS GIVEN IN SRM 57-51-01-1A-1 PARA 4. B. (4). RMay 29, 2023 · N962WN · Boeing 7377H4 · Wing, Control SurfacesSDR SWAA2023070553605Panel · pulledR/W T/E PANEL 661BB HAS SEVERAL PULLED FASTENER HOLE (MARKED)<[01] PART/MATERIAL IDENTIFIED PER SRM57-51-01-0I-1 FIGURE 3 TABLE 3 ITEM 9<BR>MULTIPLE PULLED FATTENER HOLES EXCEED THE ALLOWABLE LIMITS AS GIVEN IN SRM 57-51-01-1A-1 PARA 4. B. (4). REPAIR TO BE PEMay 29, 2023 · N962WN · Boeing 7377H4 · Wing, Control SurfacesSDR SWAA2023070553606Panel · pulledR/W T/E PANEL 661AB HAS SEVERAL PULLED FASTENER HOLE (MARKED)<[01] PART/MATERIAL IDENTIFIED PER SRM 57-51-01-0I-1 FIGURE 3 TABLE 3 ITEM 5.<BR>MULTIPLE PULLED FASTENER HOLES EXCEED THE ALLOWABLE LIMITS AS GIVEN IN SRM 57-51-01-1A-1 PARA 4. B. (4). REPAIR TO BE May 29, 2023 · N962WN · Boeing 7377H4 · Wing, Control SurfacesSDR SWAA2023070552659Attach Angle · crackedB.S. 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT R.B.L. 45; W.L. 165.<[01] PARTIALLY COMPLETED STEPS 1 & 2;[02] REMOVED BS 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE FROM RBL 6 TO RBL 63; WL 165 IAW SRM 51-40-02-0G-0;[03] RECEIVED NEW ANMay 25, 2023 · N962WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2023010588281Connector · disconnectedFWD SERVICE DOOR EMERGENCY LIGHTING INOP. FOUND FWD SERVICE DOOR EMERGENCY EXIT DOOR WIRING CONNECTOR DISCONNECTED D40042P. RECONNECTED, OPS CHECK GOOD REF AMM 33-51-12 WDM.Jan 5, 2023 · N962WN · Boeing 7377H4 · Light System WiringSDR SWAA2023010588282Charger · inoperativeFWD L/H AISLE LIGHTS BS 379 & 480 INOP. R&R FWD LT BATTERY CHARGER AND BATTERY PACK IAW AMM 33-51-06. OPS GOOD.Jan 5, 2023 · N962WN · Boeing 7377H4 · Emergency LightingSDR SWAA2022082946758Handle · looseFWD SERVICE DOOR LOOSE / [01] RESECURED FWD SVC DOOR HANDLE PER AMM 52-41-11 OPS CHECK GOODAug 26, 2022 · N962WN · Boeing 737 · Service DoorsSDR SWAA2022052611502Battery Pack · failedALL EMERGENCY LIGHT BATTERY PACKS FAILED CAPACITY TEST. / [01] R&R ALL 7 BATTERY PACKS PER AMM 33-51-06.May 26, 2022 · N962WN · Boeing 7377H4 · Emergency LightingSDR SWAA2021080200645Battery Pack · failedEMERGENCY LIGHTS-AED; AFT GALLEY OVERHEAD LIGHT; AND BIN RAIL LIGHTS AT 16 FED AND 18 FED COME ON MOMENTARILY AND EXTINGUISH WITHIN 5 SECONDS. DUPLICATED SEVERAL TIMES / [01] REMOVED AND REPLACED BATTERY PACK M1672 AND PERFORMED INSTALLATION TEST PER AMM 33-51Jul 29, 2021 · N962WN · Boeing 7377H4 · Emergency LightingSDR SWAA2021080298508Battery Pack · inoperativeEMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1675 INOP ; / [01] REMOVED AND REPLACED M1675 POWER SUPPLY AND PERFORMED INSTALLATION TEST PER AMM 33-51-06-960-806 CHECKED GOOD; [02] VERIFIED REMOVAL AND REPLACEMENT OF M1675 POWER SUPPLY AND PERFORMED INSTALLATJul 25, 2021 · N962WN · Boeing 7377H4 · Emergency LightingSDR SWAA2021080396491Skate Angle · chafedCHAFE DAMAGE ON R/H VERTICAL STAB TO FUSELAGE FWD SKATE BS1006-1016 ; / [01] REMOVED R/H SKATE ANGLE IAW SRM 51-40-02; [02] LOCATED; DRILLED AND COUNTERSINK NEW L/H SKATE ANGLE P/N 147A32OOU12 IAW SRM 51-40-05;SRM 51-40-08 AND DWG 147A0030 REV. 0; [03] NO ALLOJul 19, 2021 · N962WN · Boeing 7377H4 · Vertical StabilizerSDR SWAA2021080396493Skate Angle · chafedCHAFE DAMAGE ON L/H VERTICAL STAB TO FUSELAGE FWD SKATE BS1006-1016 ; / [01] REMOVED L/H SKATE ANGLE IAW SRM 51-40-02; [02] LOCATED; DRILLED AND COUNTERSINK NEW L/H SKATE ANGLE P/N 147A32OOU11 IAW SRM 51-40-05;SRM 51-40-08 AND DWG 147A0030 REV. 0; [03] NO ALLOJul 19, 2021 · N962WN · Boeing 7377H4 · Vertical StabilizerSDR SWAA2021080296003Shield · crackedAFT CARGO BAY AFT SHIELD CRACK ON INNER SURFACE. ; / [01] THERE IS NO ALLOWABLE LIMIT FOR ACB AFT SHILED CRACK. PART TO BE REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0; [02] REMOVED AFT CARGO BAY AFT SHILED IAW SRM 51-40-02-0G-0; [03] VERIFIED SHIELD IS OUT LIMJul 17, 2021 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021080295989Seat Track · corrodedCORROSION ON SEAT TRACK AT PASSENGER CABIN BS766 RBL45 WL208. ; / [01] REMOVED DAMAGE IN SEAT TRACK WELL AT BS 766 RBL45 WL208 IAW SRM 51-10-02. BLENDED AN AREA 2.2' X .7'; WITH THE DEEPEST POINT BEING .041' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A-1 FIG Jul 17, 2021 · N962WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2021080295712Gusset · crackedGUSSET FOUND CRACKED AT BS500D LBL64 STR19L ; / [01] UPON FURTHER INVESTIGATION FOUND GUSSET IS AT STR21L IAW DWG 143A7902 SH 259 REV-; [02] ALL REF ARE IN MAINTENIX/TASK INFO/ATTACHMENTS; [03] REMOVED GUSSET BS 500D; STR 19L PER SRM 51-40-02.; [04] RECEIVED; Jul 16, 2021 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021080295714Gusset · crackedGUSSET FOUND CRACKED AT BS500D STR-19R RBL64 ; / [01] UPON FURTHER INVESTIGATION FOUND GUSSET IS AT STR21R IAW DWG 143A7902 SH 259 REV-; [02] ALL REF ARE IN MAINTENIX/TASK INFO/ATTACHMENTS; [03] REMOVED FCB GUSSET BS 500D; STR 19RH PER SRM 51-40-02.; [04] RECEJul 16, 2021 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021080295711Support · crackedFWD CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT IS CRACKED AT BS 500A W/L 156 LBL 24 ; / [01] REMOVED CRACKED LH FLOOR TO SIDEWALL SUPPORT FCB BS 500A W/L 156 LBL 24 IAW SRM<BR>51-40-02-0G-0 STEP 4; E; FIGURE 8; [02] FABRICATED NEW FLOOR TO SIDEWALL<BR>SUPPORT ANDJul 15, 2021 · N962WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021080295693Doubler · crackedBS 663 VAPOR BARRIER DBLR IS CRACKED LBL 24 W/L 148 P/N 111A1151-27 ; / [01] FORMED NEW BS 663 VAPOR BARRIER DOUBLER FROM 2024TO 0.040' CLAD SHEET LOT# 1430186-1; PER DWG 111A1511 SH25.; [02] VERIFIED FORMED NEW BS 663 VAPOR BARRIER DOUBLER FROM 2024TO 0.040' Jul 14, 2021 · N962WN · Boeing 7377H4 · Fuselage Main, Bulkhead
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