N455WN

Service difficulty reports · 354

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 = 'N455WN' 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 SWAA2024011629375Support Plate · corrodedCORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 LBL22 WL156<[01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 747+12' REMOVED 0.015' IN AN AREA OF 1'X1' ORIGINAL THICDec 7, 2023 · N455WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024011629374Support Plate · damagedCORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 RBL22 WL156<[01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 727D-9' REMOVED 0.020' IN AN AREA OF 1'X1' ORIGINAL Dec 7, 2023 · N455WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024011629377Shield · corrodedCORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS767+3 TO BS794 RBL22 WL156<[01] CORROSION ON AFT CARGO BAY SHIELD FWD OF CARGO DOOR FOUND OUT OF LIMITS. REMOVED; REPLACED AND INSTALLED NEW SHIELD AT BS767 TO BS794 RBL22 WL156Dec 7, 2023 · N455WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024011629376Intercostal · corrodedCORROSION AFT CARGO BAY ON INTERCOSTAL BS787 TO BS807 WL150 RBL6 S-27R<[01] CORROSION ON AFT CARGO BAY INTERCOSTAL BS787 TO BS807 WL150 RBL6 S-27R WAS FOUND OUT LIMITS. REMOVED; REPLACED AND INSTALLED NEW AFT CARGO BAY INTERCOSTAL AT BS 787 TO BS 807 WL150 RBLDec 7, 2023 · N455WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024011628827Skin · crackedHORIZONTAL STABILIZER LOWER SKIN - FOUND .7' CRACK 17.5' FROM FWD EDGE AT STA 193.90<[01] CRACK IS ON THE LEFT HORIZONTAL STABILIZER;[02] VERIFIED APPLICABILITY OF SRM 55-10-01-2R-11 REPAIR 11.;[03] REPAIRED HORIZONTAL STABILIZER LOWER SKIN STA 193.90 IAW SRM Dec 6, 2023 · N455WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/SkinSDR SWAA2024011628814Seat Track · corrodedCABIN SEAT TRACK HAS CORROSION IN WELL AND ON TOP OF CROWN AT BS 663; BS 706+18; LBL 25; WL 208<[01] COMPLETED STEPS 1-3;[02] PARTIALLY UPDATED STEP 4;[03] VERIFIED PARTIAL ON MAINTENANCE STEP 4.;[04] UPDATED STEP 5;[05] UPDATED PARTS USAGE TABLE.;[06] UPDATEDDec 6, 2023 · N455WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2024011628806Seat Track · corrodedCABIN SEAT TRACK HAS CORROSION IN WELL AND ON TOP OF CROWN AT BS 500A+5; BS 500B+15; LBL 45; WL 208<[01] COMPLETED STEP 1; UPDATED TABLE;[02] PASSENGER CABIN SEAT TRACK STA 480-520; LBL 45; WL 208 WENT OUT OF LIMITS ON CUSTOMER CARD# TTG8Q00Q3RA0. MEASURED WITDec 6, 2023 · N455WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2024011628810Seat Track · corrodedCABIN SEAT TRACK HAS CORROSION IN WELL AND ON TOP OF CROWN AT BS 578+2; BS 639+11; BS 727+14; RBL 45; WL 208<[01] COMPLETED STEP 1; UPDATED TABLE;[02] COMPLETED STEPS 1-7.;[03] PARTIAL STEP 8; OK TO INSTALL NEW PASSENGER CABIN SEAT TRACK STA 540-727B; RBL 45; Dec 6, 2023 · N455WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2024011628811Seat Track · corrodedCABIN SEAT TRACK HAS CORROSION IN WELL AND ON TOP OF CROWN AT BS 727E+10; RBL 45; WL 208<[01] UPDATED TABLE;[02] COMPLETED STEP 1;[03] PASSENGER CABIN SEAT TRACK STA 727B-887; RBL 45 WAS FOUND TO BE OUT OF LIMITS AND WILL BE REPLACED ON CUSTOMER CARD# TTG8Q00QDec 6, 2023 · N455WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2024011628825Seat Track · corrodedCABIN SEAT TRACK HAS CORROSION IN WELL OF CROWN AT BS 597+18; RBL 45; WL 208<[01] COMPLETED STEP 1; SEAT TRACK STA 540-727B; RBL 45; WL 208 WENT OUT OF LIMITS AND WILL BE REPLACED ON CUSTOMER CARD# TTG8Q00Q3RDG.;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENDec 6, 2023 · N455WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2024011628823Seat Track · corrodedCABIN SEAT TRACK HAS CORROSION IN WELL OF CROWN AT BS 827+2; RBL 45; WL 208<[01] PASSENGER CABIN SEAT TRACK STA 727B-887; RBL 45 WAS FOUND TO BE OUT OF LIMITS AND WILL BE REPLACED ON CUSTOMER CARD# TTG8Q00Q3S6G.;[02] VERIFIED MEASUREMENTS.Dec 6, 2023 · N455WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2024011628824Seat Track · corrodedCABIN SEAT TRACK HAS CORROSION ON TOP OF CROWN AT BS 787+11; RBL 45; WL 208<[01] COMPLETED STEPS 1-2; UPDATED TABLE.;[02] EDITED TABLE;[03] VERIFIED;[04] UPDATED STEP 5;[05] ACCOMPLISHED PARTIAL MAINTENANCE STEP 4.;[06] UPDATED STEP 7.;[07] UPDATED STEP 3.;[08Dec 6, 2023 · N455WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach FittingsSDR SWAA2024011628027Stringer · crackedCRACKED STRINGER AT AREA AFT OF FCB BS535 S-25R WL155. MARKED<[01] VERIFIED STEPS 3;4;6; COMPLETE.;[02] DAMAGE WAS FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE AND INSTALLED REPAIR AS PER EA 23-153-03563.;[03] VERIFIED CORRECTIVE ACTION COMPLETE.<BR>VERIFIED MEASDec 5, 2023 · N455WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2024011628028Stringer · crackedCRACKED STRINGER AT AREA AFT OF FCB BS535 S-25L WL155. MARKED<[01] CRACK WAS FOUND TO BE OUT OF LIMITS; REMOVED DAMAGED STRINGER SECTION AND INSTALLED REPAIR AS PER SRM 53-00-03-2R-1.Dec 5, 2023 · N455WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2024011628025Stringer · crackedCRACKED STRINGER AT AREA AFT OF FCB BS535 S-23R WL164. MARKED<[01] CRACKED STRINGER WAS FOUND TO BE OUT OF LIMITS. THE DAMAGE WAS REPAIRED AS PER 737-700 SRM 53-00-03-2R-1 (REPAIR 1) AND EA 23-153-03573. UPDATED MEASUREMENT TABLE.;[02] VERIFIED JOB COMPLETEDec 5, 2023 · N455WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2024011628029Stringer · crackedCRACKED STRINGER AT AREA AFT OF FCB BS535 S-23L WL164. MARKED<[01] CRACK ON STRINGER FOUND TO BE OUT OF LIMIT; REMOVED DAMAGED STRINGER SECTION. THE DAMAGE WAS REPAIRED PER 737-700 SRM 53-00-03-2R-1 (REPAIR 1) AND EA 23-153-03569.;[02] VERIFIED MEASUREMENT TABDec 5, 2023 · N455WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2024011628026Stringer · crackedCRACKED STRINGER AT AREA AFT OF FCB BS535 S-26R WL153. MARKED<[01] CRACK WAS FOUND TO BE OUT OF LIMITS; REMOVED DAMAGED STRINGER SECTION AND INSTALLED REPAIR AS PER SRM 53-00-03-2R-1.Dec 5, 2023 · N455WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2024011628030Stringer · crackedCRACKED STRINGER AT AREA AFT OF FCB BS535 S-26L WL153. MARKED<[01] CRACK WAS FOUND TO BE OUT OF LIMITS; REMOVED DAMAGED STRINGER SECTION AND INSTALLED REPAIR AS PER SRM 53-00-03-2R-1.Dec 5, 2023 · N455WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2024011628031Stringer · crackedCRACKED STRINGER AT AREA AFT OF FCB BS535 S-27R WL150. MARKED<[01] CRACK WAS FOUND TO BE OUT OF LIMITS; REMOVED DAMAGED STRINGER SECTION AND INSTALLED REPAIR AS PER SRM 53-00-03-2R-1.Dec 5, 2023 · N455WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2024011628032Stringer · crackedCRACKED STRINGER AT AREA AFT OF FCB BS535 S-27L WL150. MARKED<[01] CRACK WAS FOUND TO BE OUT OF LIMITS; REMOVED DAMAGED STRINGER SECTION AND INSTALLED REPAIR AS PER SRM 53-00-03-2R-1.;[02] VERIFIED CORRECTIVE ACTION COMPLETED THROUGH STEPS 1-11.Dec 5, 2023 · N455WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2024011627868Threshold · crackedFORWARD CARGO BAY FORWARD CORNER THRESHOLD IS CRACKED<[01] VERIFIED MEASUREMENTS.;[02] UPDATED CORRECTIVE ACTION STEP 1. CRACK ON SCUFF PLATE WAS FOUND TO BE OUT OF LIMITS AS PER SRM 53-30-15-1A-1.;[03] CORRECTION TO STEP 2 SHOULD STATE ' CRACK ON SCUFF PLATE Dec 5, 2023 · N455WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024011627852Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 241DF HAS DELAMINATION<[01] IDENTIFIED FLOORBOARD 241DF IAW SRM 53-00-50-0I-1 FIG. 4 SHEET 1 TABLE 4 AND FOUND DAMAGE TO BE OUT OF ECONOMICAL REPAIR. NEW PANEL TO BE FABRICATED IAW SRM 53-00-50-2R-0 PARA 1.A NOTE. <BR>CUT NEW PANEL Dec 4, 2023 · N455WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024011627860Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 241AF HAS DELAMINATION<[01] IDENTIFIED FLOORBOARD 241AF IAW SRM 53-00-50-0I-1 FIG. 4 SHEET 1 TABLE 4 AND FOUND DAMAGE TO BE OUT OF ECONOMICAL REPAIR. NEW PANEL TO BE FABRICATED IAW SRM 53-00-50-2R-0 PARA 1.A NOTE. <BR>CUT NEW PANEL Dec 4, 2023 · N455WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024011627865Floor Panel · delaminatedPASSENGER CABIN FLOOR PANEL 231XF HAS DELAMINATION<[01] IDENTIFIED FLOORBOARD 231XF IAW SRM 53-00-50-0I-1 FIG. 4 SHEET 1 TABLE 4 AND FOUND DAMAGE TO BE OUT OF ECONOMICAL REPAIR. NEW PANEL TO BE FABRICATED IAW SRM 53-00-50-2R-0 PARA 1.A NOTE. <BR>CUT NEW PANEL Dec 4, 2023 · N455WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2023042029393Strip · looseFWD GALLEY EGRESS FLOOR LIGHT STRIP NOT SECURE<[01] RE SECURED FWD GALLEY EGRESS FLOOR LIGHT STRIP REF AMM 33-51-15.Apr 20, 2023 · N455WN · Boeing 7377H4 · Emergency LightingSDR SWAA2022071127481Separator · contaminatedPER TELCON WITH MOC CAPTAINS REPORT CHEMICAL SMELL IN CABIN. / [01] ACCOMPLISHED SMOKE OR FUMES IN CABIN CONDITIONAL INSPECTION PER AMM 05-51-56. NO DISCREPANCIES NOTED AND FIM 21-00 TASK 806. AS PRECAUTIONARY R&R LT AND RT A/C WATER SEPARATORS PER AMM21-51-05Jul 10, 2022 · N455WN · Boeing 7377H4 · Cabin Cooling SystemSDR SWAA2022061316994Light · brokenFWD SERVICE DOOR EMER LT BROKE OFF.(SIDEWALL) / [01] R&R LIGHT ASSY & COVER PER SIP.OPS CKS OK.Jun 9, 2022 · N455WN · Boeing 7377H4 · Emergency LightingSDR SWAA2021122753000Panel · damagedSUPPLEMENTAL INFORMATION: MATING SURFACE FOR PANEL 193AR HAS ABRASION DAMAGE AT BS 663 THROUGH BS 674 AT RBL 26 TO RBL 28. ; / [01] WING TO BODY FAIRING SUPPORT AT BS 663 - BS 674 ; RBL 26 - RBL 28 WL 140 FOUND TO BE OUT OF LIMITS DUE TO MATERIAL LOSS IS MORE Dec 14, 2021 · N455WN · Boeing 737 · Fuselage Main, Attach FittingsSDR SWAA2021122751776Clevis · crackedSUPPLEMENTAL INFORMATION: LH ACM ROD ATTACHMENT CLEVIS CRACKED AND BROKEN ; / [01] LH ACM REMOVED ON TTG8Q009GE9D; [02] MEASUREMENTS; [03] PREPARED SERVICABLE L/H ACM PER AMM 21-51-09-400-801 STEPS 3.A.-F.(1)(2)(A)-(D); (J)-(M) AND AMM 21-51-04-400-801-001 STEDec 9, 2021 · N455WN · Boeing 737 · Wing Miscellaneous StructureSDR SWAA2021122751006Seal Depressor · crackedCRACK FOUND ON FSD UPPER SEAL DEPRESSOR BS 294.5 + 3'; APPROX. WL 265 ; / [01] REMOVED FSD UPPER SEAL DEPRESSOR IAW SRM 51-40-02; [02] LOCATED AND DRILLED NEW FSD UPPER SEAL DEPRESSOR PN#141A8372U1 IAW SRM 51-40-05 AND IAW DWG#141A8370... OK TO INSTALL; [03] VDec 7, 2021 · N455WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021122750140Stiffener · corrodedSUPPLEMENTAL INFORMATION: CORROSION ON STIFFENER AT MID PASSENGER CABIN BS686 LBL70 WL203. ; / [01] REMOVED CORROSION ON DIFFERENTS AREAS OF STIFFENER AT MID PASSENGER CABIN PER REF SRM 51-10-01 L=1 W=.2 ;L=.250 W=.2 AND L=1 W=.2; [02] VERIFIED CORRECTIVE ACTIDec 3, 2021 · N455WN · Boeing 737 · Fuselage Miscellaneous StructureSDR SWAA2021122750139Stiffener · corrodedSUPPLEMENTAL INFORMATION: CORROSION ON STIFFENER AT MID PASSENGER CABIN BS708 LBL62; LBL65 WL203. ; / [01] REMOVED CORROSION ON DIFFERENTS AREAS OF STIFFENER AT MID PASSENGER CABIN PER REF SRM 51-10-01 L=.8 W=.2 ;L=.6 W=.2 AND L=.250 W=.2; [02] VERIFIED CORRECDec 3, 2021 · N455WN · Boeing 737 · Fuselage Main, FrameSDR SWAA2021122750138Angle · crackedSUPPLEMENTAL INFORMATION: CRACKED ATTACH ANGLE AT MID PASSENGER CABIN BS693 LBL1 WL203. ; / [01] REMOVED CRACKED ANGLE AT BS 693 RBL 24 WL 203 PER REF SRM 51-40-02; [02] CORRECTION ENTRY 1 : LBL1; [03] FORMED A MID PASSENGER CABIN REPLACEMENT ANGLE BS 691 LBL Dec 3, 2021 · N455WN · Boeing 737 · Fuselage Main, Attach FittingsSDR SWAA2021122750136Angle · crackedSUPPLEMENTAL INFORMATION: CRACKED ATTACH ANGLE AT MID PASSENGER CABIN BS691 RBL1 WL206. ; / [01] REMOVED CRACKED ANGLE AT BS 691 RBL 1 WL 206 PER REF SRM 51-40-02; [02] FORMED A MID PASSENGER CABIN REPLACEMENT ANGLE BS 691 RBL 1 WL 206 ; FROM 7075-T0 ; 0.050' Dec 3, 2021 · N455WN · Boeing 737 · Fuselage Main, Attach FittingsSDR SWAA2021122750135Stiffener · corrodedSUPPLEMENTAL INFORMATION: CORROSION ON STIFFENER AT MID PASSENGER CABIN BS692 LBL66; LBL70 WL203. ; / [01] REMOVED CORROSION ON DIFFERENTS AREAS OF STIFFENER AT MID PASSENGER CABIN PER REF SRM 51-10-01 L=1.8 W=.5 ;L=2.1 W=.2 AND L=1.5 W=.2; [02] VERIFIED CORREDec 3, 2021 · N455WN · Boeing 737 · Fuselage Miscellaneous StructureSDR SWAA2021122749750Support · crackedCRACKED FLOOR SUPPORT AT STA 344+9; LBL 1; WL 208. ; / [01] REMOVED INTERCOSTAL SUPPORT AT FLOOR STRUCTURE BETWEEN BS 344 TO BS 360 WL 208 LBL 1 SRM 51-40-02; [02] LOCATED AND DRILLED NEW FLOOR SUPPORT INTERCOSTAL P/N 141A5410U23 LOT #1472062-1 BETWEEN BS 344 Dec 3, 2021 · N455WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021122749747Floorbeam · corrodedCORROSION ON TOP OF FLOOR BEAM AT STA 312; LBL10. REMOVED CORROSION. MATERIAL ORIGINAL THICKNESS .125' MATERIAL REMAINING .095' FOUND TO BE OUT OF LIMITS IAW SRM 53-10-51-1A-1. SHOT PEENED THE BLENDED AREA IAW SRM 53-1-51-2R-15, REPAIR 15. PERFORMED A DVIDec 3, 2021 · N455WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021122750141Attach Angle · crackedCRACKED ATTACH ANGLE BS 693, RBL 24, WL 203. REMOVED CRACKED ANGLE IAW SRM 51-40-02. FABRICATED, LOCATED, DRILLED, AND TREATED THE NEW ANGLE IAW SRM 51-40-05, AND DWG 273A9112 REV-. APPLIED PRIMER TO NEW ANGLE IAW SOPM 20-41-02, AND DWG 273A9112 REV-. Dec 3, 2021 · N455WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021122750137Angle · crackedCRACKED ATTACH ANGLE AT MID PASSENGER CABIN BS693 LBL24 WL203. REMOVED ANGLE IAW SRM 51-40-02. FABRICATED, LOCATED, DRILLED, AND TREATED NEW ANGLE IAW SRM 51-40-05, AND DWG 273A9112. APPLIED PRIMER IAW SOPM 20-41-02 AND DWG 273A9112. INSTALLED NEW ANGLE IDec 3, 2021 · N455WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2021122749965Strap · crackedAFT CARGO BAY STRAP IS CRACKED BS 807; RBL 23; WL 156 ; / [01] REMOVED AFT CARGO BAY STRAP CRACKED BS.807 RBL23 WL156 IAW SRM 51-40-02; [02] RECIVED NEW STRAP ITEM 146A8128U14 LOT 1476381-1 PO 848206/1 LOCATED AND DRILLED NEW STRAP AT BS 787 TO 847 RBL 23 WL15Dec 3, 2021 · N455WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2021122750142Floor Panel · delaminatedCABIN FLOOR PANEL 242UF HAS LARGE DELAMINATED AREA IN CENTER OF PANEL ; / [01] DUE TO THE EXTENT OF DAMAGE; REPLACED CABIN FLOOR PANEL 242UF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-26 ITEM 116.; [02] PANEL REPLACED. JOB COMPLETE PER SRM 51-10-02-0G-0 PADec 3, 2021 · N455WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021122749358Panel · damagedDURING POST REPAIR UT INSPECTION FOUND DISBONDED SECTION IN REPAIRED AREA. FOUND ARE OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-40-70-1A-1 PAR 4A(6). REPAIRED IAW SRM 51-70-05-2R-1 IAW SRM 53-40-70-2R-1 PAR 4B(1).Dec 2, 2021 · N455WN · Boeing 7377H4 · Aerodynamic FairingsSDR SWAA2021122749590Panel · damagedPANEL 193CL HAS DISBOND OVER CORE ON INNER SURFACE NEAR I/B END. DAMAGE IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-40-70-1A-1 PAR 4A(6). REPAIRED IAW SRM 51-70-05-2R-1Dec 2, 2021 · N455WN · Boeing 7377H4 · Aerodynamic FairingsSDR SWAA2021122749217Flange · corrodedSUPPLEMENTAL INFORMATION: CORROSION ON APU CAVITY HORIZONTAL FLANGE OF CHORD AT B.S. 1088+13; R.B.L. 23. ACCESSED THROUGH APU INLET CAVITY. ; / [01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS AT APU CAVITY HORIZONTAL FLANGE OF CHORD AT B.S. 1088+13; R.Dec 1, 2021 · N455WN · Boeing 737 · Fuselage Miscellaneous StructureSDR SWAA2021122749219Beam · crackedFSD; HAS EVIDENCE OF CRACK ON TOP; FWD SIDE OF UPPER BEAM AT HANDLE BOX. ; / [01] REMOVED 2 BOLTS FROM FOWARD SIDE OF UPPER BEAM AT HANDLE BOX PER SOPM 20-50-01.; [02] VERIFY CRACK FREE CONDITON.; [03] HFEC INSPECTED #5 BEAM IAW 737 NDTM PART 6 51-00-00 PROCEDDec 1, 2021 · N455WN · Boeing 7377H4 · Galley DoorsSDR SWAA2021122748668Angle · crackedSUPPLEMENTAL INFORMATION: B.S. 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT L.B.L. 8 AND 42; W.L. 160. ; / [01] EVALUATED CRACK ON VAPOR BARRIER UPPER ATTACH ANGLE AND FOUND TO BE OUT OF LIMITS DUE TO EXCEEDS ALLOWED DAMAGE LIMITS; CRACK LENGTH L=1.0'' TNov 30, 2021 · N455WN · Boeing 737 · Fuselage Main, KeelSDR SWAA2021122748853Floor Panel · brokenPASSENGER CABIN FLOOR PANEL 221GF HAS BROKEN TANG. ALL DAMAGE WAS FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4F. REMOVED ALL DAMAGE, CLEANED REPAIR AREAS. FABRICATED CORE PLUG & UPPER SURFACE REPAIR PLIES FOR TANG REPAIR IAW SRM 53-00-50-Nov 30, 2021 · N455WN · Boeing 7377H4 · Passenger Compartment EquipmentSDR SWAA2021122748848Floor Panel · brokenCABIN FLOOR PANEL 221BF HAS BROKEN TANG. ALL DAMAGE WAS FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4F. DAMAGE REPAIRED IAW SRM 53-00-50-2R-6 AND SRM 53-00-50-2R-10.Nov 30, 2021 · N455WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2021122748843Fitting · corrodedCORROSION- BS867 RBL13.5 CARGO TRACK TIE DOWN FITTING CORRODED / [01] ACB TRACK BS 767-887 RBL 14 REPLACEMENT WILL ACCOMPLISH PER CUSTOMER CARD# TTG8Q009K6X6.; [02] UPDATED MEASUREMENTS; [03] VERIFIED CORRECTIVE ACTIONS 1 AND 2.Nov 30, 2021 · N455WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021122748670Angle · crackedBS 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT RBL 8, WL 160. EVALUATED CRACKED ATTACH ANGLE & FOUND TO BE OUT OF LIMITS. CRACK LENGTH 1.2'' IAW SRM 57-10-10-1A-2. ACCOMPLISHED CUT OUT OF ATTACH ANGLE IAW SRM 57-10-10-2R-5 REPAIR 5 PART 4B. HFEC INSNov 30, 2021 · N455WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
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