N965WN

Service difficulty reports · 175

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 = 'N965WN' 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 SWAA2023080975579Floor Panel · pulledFLOOR PANEL 231HF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATED NEW FLOOR PANEL 231HF IAW SRM 53-00-50-2R-0.;[02] ATTACHED CURE SHEET TO THIS FAULT RECORD.;[03] VERIFIED CORRECTIVE ACTION 1; 2; CURE SHEETS AND MEASUREMENTSJul 6, 2023 · N965WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023080975580Floor Panel · pulledFLOOR PANEL 231KF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] IDENTIFIED FLOOR PANEL 231KF MATERIALS IAW SRM 53-00-50-0I-1 FIG 3 TABLE 3.<BR><BR>DUE TO EXTENT OF THE DAMAGE FABRICATED NEW 231KF FLOOR PANEL FROM BMS4-23 TYPE 2 LOT#1531001-1; INSTALLED INSERTS Jul 6, 2023 · N965WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023080975572Floor Panel · pulledFLOOR PANEL 231LF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] UPLOADED CURE SHEET AND VERIFIED COMPLETION OF PANEL 231LF FABRICATION IAW SRM 53-00-50-2R-0 AND BOEING DWG: 143A5810 ID: 0579.;[02] FINAL INSPECTION. JOB COMPLETE.Jul 6, 2023 · N965WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023080975582Floor Panel · pulledFLOOR PANEL 231UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATED NEW FLOOR PANEL 231UF IAW SRM 53-00-50-2R-0.;[02] ATTACHED CURE SHEET TO THIS FAULT RECORD.;[03] VERIFIED CORRECTIVE ACTION 1; 2; CURE SHEETS AND MEASUREMENTSJul 6, 2023 · N965WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023080975574Floor Panel · pulledFLOOR PANEL 231ZF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATED NEW FLOOR PANEL 231ZF IAW SRM 53-00-50-2R-0.;[02] ATTACHED CURE SHEET TO THIS FAULT RECORD.;[03] VERIFIED CORRECTIVE ACTION 1; 2; CURE SHEETS AND MEASUREMENTSJul 6, 2023 · N965WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023080975575Floor Panel · pulledFLOOR PANEL 242NF UPPER SKIN HAS PULLED STRANDS.<[01] FLOOR PANEL 242NF UPPER SKIN WITH PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0 PARA 1. A. NOTE. AND ATTACHED CURE SHEET TO THIS FAULT RECORD.;[02] JOB COMPLETE.Jul 6, 2023 · N965WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023080975583Floor Panel · pulledFALOOR PANEL 241KF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241KF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE PER SRM 53-00-50-2R-0 PARA 1. A. NOTE AND DWG 146A5810 SHEET Jul 6, 2023 · N965WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023080975584Floor Panel · pulledFLOOR PANEL 241NF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241NF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE PER SRM 53-00-50-2R-0 PARA 1. A. NOTE AND DWG 146A5810 SHEET 4Jul 6, 2023 · N965WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023080975585Floor Panel · pulledFLOOR PANEL 241RF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241RF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE PER SRM 53-00-50-2R-0 PARA 1. A. NOTE AND DWG 146A5810 SHEET 4Jul 6, 2023 · N965WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023080975586Floor Panel · pulledFLOOR PANEL 241TF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] UPLOADED CURE SHEET AND VERIFIED FABRICATION OF PANEL 241TF IAW SRM 53-00-50-2R-0 AND DWG 146A5810 SHEET 467;[02] FINAL INSPECTION. JOB COMPLETE.Jul 6, 2023 · N965WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023080975576Floor Panel · pulledFLOOR PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] UPLOADED CURE SHEET AND VERIFIED FABRICATION OF PANEL 241UF IAW SRM 53-00-50-2R-0 AND BOEING DWG:146A5810 ID:0470.;[02] VERIFIED CORRECTIVE ACTION 1Jul 6, 2023 · N965WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023080975587Floor Panel · pulledFLOOR PANEL 241VF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] UPLOADED CURE SHEET AND VERIFIED FABRICATION OF PANEL 241VF IAW SRM 53-00-50-2R-0 PAR. 5. S. (1) (A) - (D) AND BOEING DWG: 146A5810 ID: 0469.;[02] FINAL INSPECTION. JOB COMPLETE.<BR><BR>VERIFIED MEJul 6, 2023 · N965WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023080975588Floor Panel · pulledFLOOR PANEL 241WF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] UPLOADED CURE SHEET AND VERIFIED FABRICATION OF PANEL 241WF IAW SRM 53-00-50-2R-0 AND DWG 146A5810 SHEET 471;[02] FINAL INSPECTION. JOB COMPLETE.Jul 6, 2023 · N965WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023080976089Tension Tie · corrodedCORROSION ON TENSION STRAP AT AFT CABIN BS1016+12 RBL18 WL208.<[01] REMOVED TENSION STRAP AT AFT CABIN BS1016+12 RBL18 WL208 PER SRM 51-40-02-0G-0.;[02] UPDATED MEASUREMENTS TABLE.;[03] SRM DOES NOT HAVE ALLOWABLE DAMAGE FOR CORROSION ON TENSION STRAP. OUT OF Jul 6, 2023 · N965WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023080976090Floorbeam · corrodedCORROSION ON FLOOR BEAM AT AFT CABIN BS986 LBL43 WL208.<[01] VERIFIED SRM 53-70-51-1A-1 IS APPLICABLE FOR ALLOWABLE DAMAGE TO SECT. 47 FLOOR STRUCTURE.;[02] CONCUR WITH APPLICABILITY OF SRM 53-70-51-1A-1.;[03] REMOVED CORROSION FROM UPPER FLANGE OF BS 986.5 FLJul 6, 2023 · N965WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2023080976100Sill Drain · corrodedCORROSION ON FED MOP SILL BS294+9; BS317 - BS342 LBL56 WL208.<[01] VERIFIED APPLICABILITY FOR SRM 53-10-15-1A-1;[02] REMOVED CORROSION ALONG FED MOP SILL<BR>AT LBL56; WL208; BS294.5 + 10'; L: 2 X W:1'<BR>BS312 + 5'; L: 2.5' X W:1'<BR>BS312 + 9'; L: 1.5' X W:1'Jul 6, 2023 · N965WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023080976098Sill Drain · corrodedCORROSION ON FSD MOP SILL BS294+7; BS326 - BS346 RBL56 WL208.<[01] VERIFIED APPLICABILITY OF SRM 53-10-15-1A-2;[02] REMOVED CORROSION ALONG FSD MOP SILL <BR>AT RBL56; WL208 BS 291.5 + 11' - BS312 + 10' L:20' X W:1'; REMOVED CORROSION ALONG FSD MOP SILL AT RBL5Jul 6, 2023 · N965WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023080976099Support Angle · corrodedCORROSION ON FSD MOP SILL THRESHOLD SUPPORT ANGLE BS305 - BS323 RBL57 WL209.<REMOVED CORROSION ALONG FSD MOP SILL THRESHOLD SUPPORT ANGLE AT RBL57; WL209 BS 291.5 + 12' L:1.5' X W:1';<BR>BS312 L1:5' X W:1'; <BR>BS312 +5' L1:5' X W:1'; <BR>BS312 +8' L1:5' X W:1Jul 6, 2023 · N965WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023080975569Floor Panel · damagedFWD CABIN FLOOR PANEL 221BF AFT O/B CORNER (TANG) IS BROKEN<[01] FWD CABIN FLOOR PANEL 221BF WITH AFT O/B CORNER (TANG) BROKEN WAS REPAIRED PER SRM 53-00-50-2R-1. ATTACHED CURE SHEETS TO THIS FAULT RECORD.;[02] VERIFIED CORRECTIVE ACTION 1;[03] VERIFIED CORRECJul 5, 2023 · N965WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023080975570Floor Panel · damagedFWD CABIN FLOOR PANEL 221GF FORWARD O/B CORNER (TANG) BROKEN<[01] COMPLETED STEPS 11 AND 12.;[02] FWD CABIN FLOOR PANEL 221GF O/B CORNER (TANG) REPAIRED IAW SRM 53-00-50-2R-6;[03] VERIFIED CORRECTIVE ACTION 2;[04] VERIFIED CORRECTIVE ACTION 2Jul 5, 2023 · N965WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023081074776Support · corrodedFLOOR TO SIDEWALL SUPPORT HAS CORROSION BS 727A+5 - 727E+3 LBL 20 WL 156<[01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS OF ACB FLOOR TO SIDEWALL SUPPORT; BS727A+5 727E+3 LBL 20 WL 156 IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2.;[05] FABRIACATED LOCATED Jul 4, 2023 · N965WN · Boeing 7377H4 · Fuselage Structure (General)SDR SWAA2023080974772Intercostal · crackedCRACKED INTERCOSTAL IN UPPER AFT RADIUS BS 947 RBL 17 WL 179<[01] VERIFIED APPLICABILITY OF SRM 53-70-53-01-2 IDENTIFICATION 2 - SECTION 47 AND SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2.;[02] VERIFIED ITEM 1 CORRECTIVE ACTIONS.;[03] MEASURED CRACK ON INTERCOSTAL ISJul 4, 2023 · N965WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023080974778Shield · corrodedFWD SHIELD IS CORRODED FROM BS 767-767+16 RBL 20 WL 157<[01] UPDATED MEASUREMENTS TABLE;[02] NOT FOUND ALLOWABLE ON SRM; PART WILL BE REPLACE PER SRM 51-10-02-0G-0; STEP 9;[03] REMOVED FWD SHIELD FROM AFT CARGO COMPARTMENT FROM BS 767 TO BS 794.25 IAW SRM 51-4Jul 4, 2023 · N965WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023080974779Support · corrodedFLOOR TO SIDEWALL SUPPORT HAS CORROSION BS 727E+13 - 787+19 RBL 20 WL 156<[01] UPDATED MEASUREMENTS TABLE;[02] FOUND UNDER INVESTIGATION LOCATION IS BS 727E+13 TO BS 747+19; RBL 20; WL 156;[03] SRM 53-00-53-1A-2 IS APPLICABLE FOR THIS;[04] BLENDED CORROSION ONJul 4, 2023 · N965WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023080974773Stringer · corrodedAREA AFT OF FWD CARGO BAY HAS A CRACKED STRINGER AT THE AFT FASTENER; STR. 23R BS 520-540 WL 156<[01] EVALUATED CRACK AT FCB STRINGER 23R/H BS 539 DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53-00-03-1A FIG 103 DETAIL A;[02] VERIFIED APPLICABILITY FOR STR 23R/H AT FJul 4, 2023 · N965WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2023080974774Stringer · crackedAREA AFT OF FWD CARGO BAY HAS A CRACKED STRINGER AT THE AFT FASTENER; STR. 24R BS 520-540 WL 156<[01] EVALUATED CRACK AT FCB STRINGER 24R/H BS 539 DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53-00-03-1A FIG 103 DETAIL A.;[02] VERIFIED APPLICABILITY FOR STR 24R/H AT Jul 4, 2023 · N965WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2023080974775Stringer · crackedAREA AFT OF FWD CARGO BAY HAS A CRACKED STRINGER AT THE AFT FASTENER; STR. 26L BS 520-540 WL 156<[01] EVALUATED CRACK AT FCB STRINGER 26L;BS 539 DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53-00-03-1A FIG 103 DETAIL A.;CUTOUT AND REMOVED DAMAGE AT STRINGER SECTION 2Jul 4, 2023 · N965WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2023080974768Stringer · crackedAREA AFT OF FWD CARGO BAY HAS A CRACKED STRINGER AT THE AFT FASTENER; STR. 23L BS 520-540 WL 156<[01] EVALUATED CRACKAT FCB STRINGER 23L;BS 539 DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53-00-03-1A FIG 103 DETAIL A.;[02] EVALUATED CRACK AT FCB STRINGER 23L;BS 539 Jul 4, 2023 · N965WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2023080974771Strap · corrodedCORROSION ON THRESHOLD TIE STRAP AT FASTENER HOLES BS 787+8 - 807+13 RBL 20 WL 159<[01] VERIFIED APPLICABILITY IAW SRM 53-60-15-01-1 AND SRM 53-60-15-1A-1;[09] OK TO INSTALL NEW THRESHOLD TIE STRAP.;[10] OKAY TO INSTALL GIVEN.;[11] STARTED INSTALLATION OF THREJul 4, 2023 · N965WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023080974777Support · corrodedFLOOR TO SIDEWALL SUPPORT CORROSION BS 727A+9 - 767 RBL 20 WL 156<[01] UPDATE MEASUREMENTS TABLE;[02] SRM 53-00-53-1A-2 IS APPLICABLE FOR THIS;[03] BLENDED CORROSION ON FLOOR TO SIDEWALL SUPPORT CORROSION BS 727A+9 - 767 RBL 20 WL 156;<BR>WORK AREA <BR>BS 727AJul 4, 2023 · N965WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023080974520Shield · corrodedCORROSION ON AFT SHIELD AT BS 500-500A RBL 25 WL 156<[01] ENTERED MEASUREMENTS;[02] SRM 53-00-53-1A-2 IS APPLICABLE FOR THIS DAMAGE EVALUATION.<BR>NO ALLOWABLE DAMAGE FOUND IN 737-700 SRM FOR THIS PART.<BR>REPAIR BY REPLACEMENT SRM 51-10-02-0G-0 STEP 9;[03] VEJul 3, 2023 · N965WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023080974522Support · chafedCHAFING DAMAGE ON FWD BULKHEAD SUPPORT BS400 LBL24 WL156<[01] REMOVED DAMAGE IAW SRM 51-10-02.<BR>DAMAGED AREA MEASURES 0.30' X 0.80';[02] VERIFIED CORRECTIVE ACTION #1;[03] NOT FOUND ALLOWABLE DAMAGE ON THE SRM REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0 PARAJul 3, 2023 · N965WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023080974763Stringer · corrodedAREA AFT OF FWD CARGO BAY HAS A CORRODED STR. R25 BS500-540; WL 156<[01] EVALUATED CORROSION AT FCB STRINGER 25R/H BS 539 DAMAGE FOUND TO BE OUT LIMITS IAW SRM 53-00-03-1A FIG 103 DETAIL B;[02] VERIFIED APPLICABILITY FOR STR 25R/H AT FCB IAW SRM 53-00-03-2R-1 Jul 3, 2023 · N965WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2023080973920Scuff Plate · crackedFWD CARGO BAY AFT CORNER SCUFF PLATE CRACKED<[01] WELDED CRACK ON FCB; AFT CORNER SCUFF PLATE USING ER4043 ALUMINUM FILLER ROD LOT NUMBER 1131216 PER SRM 53-30-15-2R-1 PARAGRAPH 4.B.(2) AND (4). REPAIR AREA STILL REQUIRES A DYE PENETRANT INSPECTION.<BR>EQUIPMEJul 1, 2023 · N965WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023052450815Fuse · inoperativeEMERGENCY AISLE LIGHT AT ROW 7ABC INOP.<[01] REMOVED AND REPLACED EMERGENCY LIGHTS POWER SUPPLY FUSE REF: AMM 33-51-06. OPS CHECK GOOD.May 22, 2023 · N965WN · Boeing 7377H4 · Emergency LightingSDR SWAA2023052450814Battery Pack · inoperativeEMERGENCY AISLE LIGHTS AT ROW 11CB AND 9ABC INOP.<[01] REMOVED AND REPLACED BATTERY PACK AT LH STATION 727C IAW AMM 33-51-06. OP CHECK GOOD.May 22, 2023 · N965WN · Boeing 7377H4 · Emergency LightingSDR SWAA2023042630408Light · inoperativeAFT R/H SERVICE DOOR EMER EXTERIOR LIGHT INOP<[01] REMOVED AND REPLACED AFT SERVICE DOOR EXTERIOR EMER LIGHT BULB PER AMM 33-51-04. OPS TEST GOOD.Apr 23, 2023 · N965WN · Boeing 7377H4 · Emergency LightingSDR SWAA2023011090191Slide · detachedFORWARD GALLEY SERVICE DOOR PARTIALLY OPENED WITH GIRT BAR ARMED<[01] INSPECTED DOOR SLIDE FOUND TO BE PULLED FROM COVER WAS NOT DEPLOYED REPACKED SLIDE REF AMM25-66-01 AC OK FOR SERVICEJan 9, 2023 · N965WN · Boeing 7377H4 · Escape SlideSDR SWAA2022110968099Skin · crackedFOUND .5 CRACK AT LOCATION IDENTIFIED AS FIRST DENT LOCATED AT WS 271; AT APPROXIMATELY 21 FROM TRAILING EDGE. PERFORMED HFEC AS REQUIRED PER NDT MANUAL PART 6 51-00-00 PROC 23. AT BOTH DENTS IDENTIFIED IN DISCREPANCY. FOUND .5 CRACK AT LOCATION AT IDENTIFIED Nov 5, 2022 · N965WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2022092824668Light · inoperativeFWD LEFT STOWBIN BULLNOSE EMEERGENCY EXIT LIGHTS ARE INOP. FOUND FUSE BLOWN ON EMERGENCY BATTERY POWER SUPPLY FOR FWD BULLNOSE LIGHTS; ALSO FOUND FWD BULLNOSE LIGHT ASSEMBLY BAD. REPLACED LIGHT ASSEMBLY IAW AMM 33-51-03-960-802 AND FUSE IAW AMM 33-51-06-960-8Sep 24, 2022 · N965WN · Boeing 7377H4 · Emergency LightingSDR SWAA2022080337728Sliding Sleeve · tornRT HORZ UPPER FWD SLIDING SEAL TORN / [01] R&R R/H UPPER SLIDER PER AMM 53-31-31Aug 3, 2022 · N965WN · Boeing 7377H4 · Horizontal Stabilizer StructureSDR SWAA2022071527801Slide · out of adjustUNABLE TO READ GAUGE ON FWD SERVICE DOOR SLIDE / [01] READJUSTED FWD SERVICE DOOR SLIDE IN REFERENCE TO AMM 25-66-01. GAUGE IS NOW VISIBLEJul 11, 2022 · N965WN · Boeing 7377H4 · Escape SlideSDR SWAA2022070124048Flashlight · brokenAFT INBOARD FLASHLIGHT BROKEN / [01] R&R AFT INBOARD FLASHLIGHT ASSY REF CMM 25-60-13Jun 29, 2022 · N965WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2022062721397Battery Pack · inoperativeEMERGENCY LIGHTS L733;L1223 AFT RIGHT SLIDE;AFT ENTRY INOP / [01] REPLACED M1672 POWER SUPPLY BATTERY PACK PER AMM 33-51-06Jun 22, 2022 · N965WN · Boeing 7377H4 · Emergency LightingSDR SWAA2021083112112Battery Pack · inoperativeEMERGENCY LIGHTS ASSOCIATED WITH BATTERY PACK M1675 ARE INOP ; / [01] REMOVED; REPLACED; AND PERFORMED GOOD INSTALLATION TEST OF EMERGENCY LIGHT BATTERY PACK AT M1675 PER AMM 33-51-06-960-805.; [02] VERIFIED CORRECTIVE ACTION 1 PER AMM 33-51-06-960-805.Aug 25, 2021 · N965WN · Boeing 7377H4 · Emergency LightingSDR SWAA2021083109722Gusset · crackedFCB GUSSET CRACKED BS 500D STR 19L WL 188 ; / [01] REMOVED GUSSET BS 500D STR-19L WL 188. IAW. SRM 51-40-02.; [02] LOCATED AND DRILLED FCB GUSSET AT B.S 500D STR 19L PER SRM51-40-05-0G-0;DWG 143A7902. O.K TO INSTALL.; [03] OKAY TO INSTALL FCB GUSSET; [04] INSTAug 20, 2021 · N965WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021083109729Gusset · crackedFCB R/H GUSSET CRACKED BS 500D STR 19R WL 188 ; / [01] REMOVED GUSSET BS 500D; STR 19R; WL 188 IAW SRM 51-40-02.; [02] LOCATED; DRILLED AND DEBURRED NEW FCB R/H GUSSET BS 500D; STR 19R; WL 188 IAW SRM 51-40-05-0G-0 AND DWG 143A7902; [03] VERIFIED; [04] LOCATEDAug 20, 2021 · N965WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021083108453Bulkhead Web · crackedRIGHT HAND B.S. 663 VAPOR BARRIER HAS A CRACKED FASTENER HOLE AT O/B EDGE ; / IDENTIFIED B.S. 663 RIGHT HAND VAPOR BARRIER MATERIAL IAW SRM 57-10-10-0I-2 TABLE 2 FIGURE 2 ITEM 4. DAMAGED FASTENER HOLE EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 57-10-10-1A-2 PARAGAug 17, 2021 · N965WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2021082308454Bulkhead Web · damagedRIGHT HAND B.S. 663 VAPOR BARRIER HAS MISALIGNED FASTENER HOLES AT I/B LOWER EDGE ; / [01] IDENTIFIED B.S. 663 RIGHT HAND VAPOR BARRIER MATERIAL IAW SRM 57-10-10-0I-2 TABLE 2 FIGURE 2 ITEM 4. DAMAGED FASTENER HOLES EXCEED ALLOWABLE DAMAGE LIMITS IAW SRM 57-10-Aug 17, 2021 · N965WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2021083107491Attach Angle · crackedR/H VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED; BS 663 RBL 8 W/L 164. ; / [01] VERIFIED APPLICABILITY IAW SRM 57-10-10-2R-5; [02] REMOVED 8 EA FASTENERS COMMON TO FUEL TANK AT BS 663 BETWEEN RBL 7 TO 20; WL 164 AND CUT OUT DAMAGE ANGLE IAW SRM 57-10-10-2R-5; Aug 12, 2021 · N965WN · Boeing 7377H4 · Fuselage Main, Bulkhead
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