N489WN

Service difficulty reports · 401

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 = 'N489WN' 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 SWAA2022092243746Seat Track · corrodedCORROSION ON PASSENGER CABIN SEAT TRACK RBL45 BS562; BS683 - BS691. MARKED. / BLEND AREA AT BS 682-687; RBL 45 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A-1;[06] REMOVED PASSENGER CABIN SEAT TRACK RBL45 BS562 BS683- BS691 IAW SOPM 20-50-01.;[07] COMPLETED COAug 19, 2022 · N489WN · Boeing 737 · Fuselage Miscellaneous StructureSDR SWAA2022092243360None · corrodedCORROSION ON FWD ENTRY DOOR THRESHOLD SUPPORT ANGLE FROM STA 303.9+13 TO STA 328+12; WL 209; LBL 60 TO LBL 65. / [01] REMOVED CORROSION IAW SRM 53-10-15-1A-1. 2'X.65X.015 BS 341.5-343.5. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15-1A-1.;[02] TOOL ID: ATS401<BR>Aug 19, 2022 · N489WN · Boeing 737 · Fuselage Miscellaneous StructureSDR SWAA2022092243363None · corrodedSTA 344 FLOOR BEAM UPPER FLANGE HAS CORROSION COMMON TO FASTENER HOLES AT LBL 11 AND BL 0; WL 208.1. / FOUND OUT OF LIMITS FABRICATED REPAIR TIE FROM AND10136 EXTRUSSION LOT# 1415860-1; 2 STRAP FROM 7075T6;0.125 LOT # 1369715-1 AND 2 ANGLES FROM 7075T6;0.125 LAug 19, 2022 · N489WN · Boeing 737 · Fuselage Main, Floor BeamSDR SWAA2022092243362None · corrodedCORROSION ON FWD ENTRY DOOR MOP SILL FROM STA 294.5+7 TO STA 348.2+6; WL 208 TO WL 209; LBL 54 TO LBL 62. / REMOVED CORROSION FROM FWD ENTRY DOOR MOP SILL AT STA 335 LBL 59 WL 208 WITH ORIGINAL THICKNESS 0.090' AND WITH MEASUREMENTS OF THE REWORKED AREA OF L= Aug 19, 2022 · N489WN · Boeing 737 · Fuselage Miscellaneous StructureSDR SWAA2022092243353Intercostal · crackedCRACKED INTERCOSTAL AT STA 312+5 & STA 312+11; WL 208; RBL 31. / [01] NO ALLOWABLE LIMITS FOUND ON SRM REPLACEMENT OF THE PART IS APPLICABLE I.A.W SRM 51-10-02-0G-0 PAR.9.C;[02] REMOVED INTERCOSTAL LOCATED BS312-BS328 RBL31 WL208 I.A.W SRM 51-40-02-0G-0;[03] LAug 19, 2022 · N489WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022092243354Intercostal · corrodedCORROSION ON INTERCOSTAL AT STA 294 TO STA 312; WL 208; LBL 10 TO LBL 12. / [01] VERIFIED APPLICABILITY FOR SRM 53-10-51-1A-1<BR>NO DAMAGE IS PERMITTED AT FLOOR BEAM UPPER CHORD UNDER INTERCOSTAL FOR GALLEY HARD MOUNT/ATTACHMENT IAW SRM 53-10-51-1A-1 PARAGRAPHAug 19, 2022 · N489WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022092243357Intercostal · corrodedCORROSION ON INTERCOSTAL FROM STA 312 TO 328; WL 208; LBL 12. / [01] REMOVED PANEL BREAK AT STA 312 TO 328 WL 208 LBL 12 IAW SRM 51-40-02<BR><BR>REMOVED CORROSION ON PANEL BREAK BS 314 IN L=2' X W=2' X D=0.40' FROM ORIGINAL TICKNESS OF 0.80' FOUND TO BE OUT OFAug 19, 2022 · N489WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022092243358Intercostal · corrodedCORROSION ON INTERCOSTAL AT STA 312+8; LBL 45; WL 208. / [01] VERIFIED APPLICABILITY FOR SRM 53-10-51-1A-1<BR>REMOVED CORROSION FROM THE INTERCOSTAL OF THE FLOOR STRUCTURE AT STA 312+8 LBL 45 WL 208; WITH ORIGINAL THICKNESS 0.040' AND MEASUREMENTS OF THE REWORAug 19, 2022 · N489WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022092243359Intercostal · crackedCRACKED INTERCOSTAL AT STA 328+8; WL 208; LBL 45. / [01] LOCATED AND DRILLED NEW INTERCOSTAL BS 328 TO 344 WL 208 LBL 45 IAW SRM 51-40-05-0G-0; AND OK TO INTALL;[02] REMOVED INTERCOSTAL BS 328 TO 344 WL 208 LBL 45 IAW SRM 51-40-02-0G-0;[03] UPDATED MEASUREMENTAug 19, 2022 · N489WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022092765167None · corrodedCORROSION; AFT LH MOP SILL; BS 947 TO BS 995 / [01] UPDATED MEASUREMENTS CHART;[02] REMOVED CORROSION ON AFT LH MOP SILL BETWEEN BS 947 TO 995. L=10' X W=3' X D=0.012' FOUND TO BE OUT OF LIMITS WITH A REMAINING THICKNESS OF 0.068' OF ORIGINAL THICKNESS OF 0.08Aug 18, 2022 · N489WN · Boeing 737 · Fuselage Miscellaneous StructureSDR SWAA2022092765172None · corrodedCORROSION; AFT RH MOP SILL; BS 947 TO BS 995 / [01] VERIFIED APPLICABILITY PER SRM 53-70-15-1A-1;[02] REMOVED CORROSION ON ASD R/H MOPSILL BETWEEN BS 947 TO 995. L=10' X W=2' X D=0.014' FOUND TO BE OUT OF LIMITS WITH A REMAINING THICKNESS OF 0.066' OF ORIGINALAug 18, 2022 · N489WN · Boeing 737 · Fuselage Miscellaneous StructureSDR SWAA2022092765124Web · corrodedCORROSION ON PRESSURE DECK STIFFENER; 706+12; RBL 68; WL 202. / [01] CLEANED; INSPECTED; AND REMOVED CORROSION ON PRESSURE DECK STIFFENER AT STA 706+12; RBL 68; WL 202 PER SRM 51-10-02-0G-0 STEP 15. NO SRM DAMAGE LIMITS.;[02] VERIFIED;[03] CERTIFIED MEASUREMENAug 18, 2022 · N489WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2022092765138Panel · pulledFLOOR PANEL 241UF HAS AN PULLED INSERT. (MARKED) / [01] IDENTIFIED PANEL 241UF IAW SRM 53-00-50-0I-1 SHEET 1; FIGURE 5; TABLE 5. PANEL IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PAR. 4.C. OK TO FAB NEW PANEL IAW SRM 53-00-50-2R-0 PAR. 1.A.<BR><BR>Aug 18, 2022 · N489WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2022092765146Floor Panel · frayedCABIN FLOOR PANEL 242TF HAS FRAYED UPPER SURFACE PLIES / [01] IDENTIFIED MATERIAL IAW SRM 53-00-50-0I-1 TABLE 6 FIG 6.<BR>DAMAGE TO UPPER SURFACE SKIN PLIES IS OUT OF ALLOWALBE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARA 4B<BR>REPAIR TO BE ACCOMPLISHED IAW SRM 53Aug 18, 2022 · N489WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022092765149Floor Panel · frayedCABIN FLOOR PANEL 242RF UPPER SURFACE PLIES FRAYED / [01] IDENTIFIED MATERIAL IAW SRM 53-00-50-0I-1 TABLE 6 FIG 6.<BR>FOUND 2 PUNCTURES TO UPPER SURFACE SKIN PLIES AND 2 AREAS ON LOWER SURFACE WITH CRACKED SKIN PLIES AND DAMAGED CORE.<BR>DAMAGE NOTED IS OUT OFAug 18, 2022 · N489WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022092765175None · corrodedCORROSION; FLOOR BEAM UPPER CHORD; BS 986.5; LBL 45 TO RBL 45; WL 208 / [01] UPDATED MEASUREMENTS CHART;[02] REMOVED CORROSION ON FLOOR BEAM UPPER CHORD; BS 986.5; LBL 43 L=1.6'XW=0.9'XD=.025; BS 986.5 LBL 41 L=.9XW=.9'XD=.020'; BS 986.5 LBL 38 L=1'XW=.8'XD=.0Aug 18, 2022 · N489WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2022092765168Web · corrodedCORROSION; FLOOR AFT SHEAR WEB; BS 1016 TO BS 1016 + 15'; LBL 4 TO LBL 25; WL 208 / [01] REMOVED SURFACE CORROSION ON 1016 SHEAR WEB IN TWO AREAS IAW SRM 51-10-02-0G-0. <BR>AREA 1) 3'X16'<BR>AREA 2) 2' 2.5'<BR>SRM DOES NOT HAVE ALLOWABLE LIMITS FOR CORROSION RAug 18, 2022 · N489WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022092765169Web · corrodedCORROSION; FLOOR AFT SHEAR WEB UPPER STRAP; BS 1016 TO BS 1016 + 6'; LBL 3 WL 208 / [01] REMOVED CORROSION ON STRAP IN A 2'X2.5'X.011 AREA IAW SRM 51-10-02-0G-0. ORIGINAL THICKNESS .080' SRM DOES NOT HAVE LIMTS FOR CORROSION ON STRAPS AT BS 1016. OUT OF LIMITSAug 18, 2022 · N489WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022092765152Strap · corrodedCORROSION ON AFT CARGO BAY TENSION STRAP AT RBL 19 BS 787+6; BS 787+13; BS 807+9. / [01] REMOVED CORROSION ON ACB ON TENSION STRAP AT RBL 19 BS 787+6' IN L=2' X W=2' X D=0.027' FROM ORIGINAL TICKNESS OF .100' FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1 PARAug 18, 2022 · N489WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022092765154Strap · corrodedCORROSION ON AFT CARGO BAY LOWER NUT PLATE BRACKET AT RBL 19 BS 787+13. / [01] REMOVED STRAP ON ACB LOWER STRAP AT RBL 19 BS 787+13' IAW SRM 51-40-02;[02] STRAP IT IS OUT OF LIMITS DUE TO NO LIMITS GIVEN IN THE SRM WILL BY REPAIRED BY REPLACEMENT OF PART IAW SAug 18, 2022 · N489WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022092765155Tie Down · corrodedCORROSION ON AFT CARGO BAY TIE DOWN AT LBL 17 BS 727D; BS 787. / [01] SRM 53-00-53-1A-2 IS FOUND TO BE APPLICABLE;[02] REMOVED CORROSION ON ACB TIE DOWN LBL 17 BS 727D L=1.4'XW=.5'XD=.055' FOUND TO BE OUT OF LIMITS WITH REMAINING THICKNESS OF .090' OF ORIGINALAug 18, 2022 · N489WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022092765156Shield · corrodedCORROSION ON AFT CARGO BAY FWD DOOR SHIELD AT RBL 22 BS 767+3; BS 767+19. / [01] NO ALLOWABLE DAMAGE LIMITS IN SRM REPAIR BY REPACEMENT IAW SRM 51-10-02-0G-0 PARAGRAPH # 9;[02] REMOVED ON AFT CARGO BAY FWD DOOR SHIELD AT RBL 22 BS 767; TO BS 787+6 WL 156 IAW SAug 18, 2022 · N489WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022092765159Support · crackedCORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 727B+2; BS 727B+14; BS 727B+18; BS 727C+5; BS 727C+15; BS 727D; BS 727D+7; 727D+16; BS 727D+19. / [01] ENTERED MEASUREMENTS.;[02] SRM 53-00-53-1A-2 IS EFFECTIVE FOR THIS EVALUATION.<BR>REMOVED CAug 18, 2022 · N489WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022092765157Support · corrodedCORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 727E; BS 727E+10; BS 727E+18; BS 747+2; BS 747+6; BS 747+14. / [01] ENTERED MEASUREMENTS.;[02] SRM 53-00-53-1A-2 IS EFFECTIVE FOR THIS EVALUATION.<BR>REMOVED CORROSION IAW SRM 51-10-02-0G-0.<BR>Aug 18, 2022 · N489WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022092242828Floor Panel · pulledFLOOR PANEL 241UF HAS AN PULLED INSERT. (MARKED) / [01] IDENTIFIED PANEL 241UF IAW SRM 53-00-50-0I-1 SHEET 1; FIGURE 5; TABLE 5. PANEL IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PAR. 4.C. OK TO FAB NEW PANEL IAW SRM 53-00-50-2R-0 PAR. 1.A.<BR><BR>Aug 18, 2022 · N489WN · Boeing 737 · Fuselage Floor PanelSDR SWAA2022092243320Floor Panel · frayedCABIN FLOOR PANEL 242TF HAS FRAYED UPPER SURFACE PLIES / [01] IDENTIFIED MATERIAL IAW SRM 53-00-50-0I-1 TABLE 6 FIG 6.<BR>DAMAGE TO UPPER SURFACE SKIN PLIES IS OUT OF ALLOWALBE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARA 4B<BR>REPAIR TO BE ACCOMPLISHED IAW SRM 53Aug 18, 2022 · N489WN · Boeing 737 · Fuselage Floor PanelSDR SWAA2022092243323Floor Panel · crackedCABIN FLOOR PANEL 242RF UPPER SURFACE PLIES FRAYED / CRACKED SKIN PLIES AND DAMAGED CORE.<BR>DAMAGE NOTED IS OUT OF ALLOWALBE DAMAGE LIMITS REMOVED DAMAGE AND CLEANED REPAIR AREAS; OK TO POT EXPOSED CORE IAW SRM 53-00-50-2R-1 PARA 4C-F;[02] VALIDATED APPLICABIAug 18, 2022 · N489WN · Boeing 737 · Fuselage Floor PanelSDR SWAA2022092243346None · corrodedCORROSION; AFT RH MOP SILL; BS 947 TO BS 995 / [01] VERIFIED APPLICABILITY PER SRM 53-70-15-1A-1;[02] REMOVED CORROSION ON ASD R/H MOPSILL BETWEEN BS 947 TO 995. L=10' X W=2' X D=0.014' FOUND TO BE OUT OF LIMITS WITH A REMAINING THICKNESS OF 0.066' OF ORIGINALAug 18, 2022 · N489WN · Boeing 737 · Fuselage Miscellaneous StructureSDR SWAA2022092243341None · corrodedCORROSION; AFT LH MOP SILL; BS 947 TO BS 995 / FOUND TO BE OUT OF LIMITS WITH A REMAINING THICKNESS OF 0.068' OF ORIGINAL THICKNESS OF 0.080'<BR>CORROSION REMOVED IAW SRM 53-70-15-0I-1 AND SRM 53-70-15-1A-1.<BR>TOOL USED:<BR>DIAL DEPTH GAUGE ID: ATS2677; SN: UAug 18, 2022 · N489WN · Boeing 737 · Fuselage Miscellaneous StructureSDR SWAA2022092243349None · corrodedCORROSION; FLOOR BEAM UPPER CHORD; BS 986.5; LBL 45 TO RBL 45; WL 208 / FOUND TO BE OUT OF LIMITS WITH REMAINING THICKNESS OF .125' OF ORIGINAL THICKNESS .150' IAW SRM 53-70-51-0I-1; SRM 53-70-51-1A-1 AND BAC1518-1211FLAP PEENING CUT EDGES OF THE FLOOR BEAM BSAug 18, 2022 · N489WN · Boeing 737 · Fuselage Miscellaneous StructureSDR SWAA2022092243343Strap · corrodedCORROSION; FLOOR AFT SHEAR WEB UPPER STRAP; BS 1016 TO BS 1016 + 6'; LBL 3 WL 208 / [01] REMOVED CORROSION ON STRAP IN A 2'X2.5'X.011 AREA IAW SRM 51-10-02-0G-0. ORIGINAL THICKNESS .080' SRM DOES NOT HAVE LIMTS FOR CORROSION ON STRAPS AT BS 1016. OUT OF LIMITSAug 18, 2022 · N489WN · Boeing 737 · Fuselage Miscellaneous StructureSDR SWAA2022092243342Shear Web · corrodedCORROSION; FLOOR AFT SHEAR WEB; BS 1016 TO BS 1016 + 15'; LBL 4 TO LBL 25; WL 208 / [01] REMOVED SURFACE CORROSION ON 1016 SHEAR WEB IN TWO AREAS IAW SRM 51-10-02-0G-0. <BR>AREA 1) 3'X16'<BR>AREA 2) 2' 2.5'<BR>SRM DOES NOT HAVE ALLOWABLE LIMITS FOR CORROSION RAug 18, 2022 · N489WN · Boeing 737 · Fuselage Miscellaneous StructureSDR SWAA2022092243326None · corrodedCORROSION ON AFT CARGO BAY TENSION STRAP AT RBL 19 BS 787+6; BS 787+13; BS 807+9. / [01] REMOVED CORROSION ON ACB ON TENSION STRAP AT RBL 19 BS 787+6' IN L=2' X W=2' X D=0.027' FROM ORIGINAL TICKNESS OF .100' FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1 PARAug 18, 2022 · N489WN · Boeing 737 · Fuselage Miscellaneous StructureSDR SWAA2022092243328Bracket · corrodedCORROSION ON AFT CARGO BAY LOWER NUT PLATE BRACKET AT RBL 19 BS 787+13. / [01] REMOVED STRAP ON ACB LOWER STRAP AT RBL 19 BS 787+13' IAW SRM 51-40-02;[02] STRAP IT IS OUT OF LIMITS DUE TO NO LIMITS GIVEN IN THE SRM WILL BY REPAIRED BY REPLACEMENT OF PART IAW SAug 18, 2022 · N489WN · Boeing 737 · Fuselage Miscellaneous StructureSDR SWAA2022092243329Tie Down · corrodedCORROSION ON AFT CARGO BAY TIE DOWN AT LBL 17 BS 727D; BS 787. / [01] SRM 53-00-53-1A-2 IS FOUND TO BE APPLICABLE;[02] REMOVED CORROSION ON ACB TIE DOWN LBL 17 BS 727D L=1.4'XW=.5'XD=.055' FOUND TO BE OUT OF LIMITS WITH REMAINING THICKNESS OF .090' OF ORIGINALAug 18, 2022 · N489WN · Boeing 737 · Fuselage Miscellaneous StructureSDR SWAA2022092243330Shield · corrodedCORROSION ON AFT CARGO BAY FWD DOOR SHIELD AT RBL 22 BS 767+3; BS 767+19. / [01] NO ALLOWABLE DAMAGE LIMITS IN SRM REPAIR BY REPACEMENT IAW SRM 51-10-02-0G-0 PARAGRAPH # 9;[02] REMOVED ON AFT CARGO BAY FWD DOOR SHIELD AT RBL 22 BS 767; TO BS 787+6 WL 156 IAW SAug 18, 2022 · N489WN · Boeing 737 · Fuselage Miscellaneous StructureSDR SWAA2022092243331None · corrodedCORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 727E; BS 727E+10; BS 727E+18; BS 747+2; BS 747+6; BS 747+14. / REMOVED CORROSION IAW SRM 51-10-02-0G-0.<BR>AREAS MEASURE: 727E; 1.00'L X 1.00'W X 0.007'D 727E+10; 1.20'L X 1.00'W X 0.008'D 727E+Aug 18, 2022 · N489WN · Boeing 737 · Fuselage Miscellaneous StructureSDR SWAA2022092242814Stiffener · corrodedCORROSION ON PRESSURE DECK STIFFENER; 706+12; RBL 68; WL 202. / [01] CLEANED; INSPECTED; AND REMOVED CORROSION ON PRESSURE DECK STIFFENER AT STA 706+12; RBL 68; WL 202 PER SRM 51-10-02-0G-0 STEP 15. NO SRM DAMAGE LIMITS.;[02] VERIFIED;[03] CERTIFIED MEASUREMENAug 18, 2022 · N489WN · Boeing 737 · Fuselage Main, FrameSDR SWAA2022092243333Sidewall Support · corrodedCORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21 BS 727B+2; BS 727B+14; BS 727B+18; BS 727C+5; BS 727C+15; BS 727D; BS 727D+7; 727D+16; BS 727D+19. / [01] ENTERED MEASUREMENTS.;[02] SRM 53-00-53-1A-2 IS EFFECTIVE FOR THIS EVALUATION.<BR>REMOVED CAug 18, 2022 · N489WN · Boeing 737 · Fuselage Miscellaneous StructureSDR SWAA2022092765118Bear Strap · crackedFORWARD GALLEY DOOR BEAR STRAP HAS A 2 INCH LONG CRACK 3 INCHES BELOW STRINGER 8R / [01] REPAIRED BY 737-700 SRM 53-10-01-2R-6 AND EA M-21-153-03542;[02] UPDATED MEASUREMENT TABLE;[03] VERIFIED MEASUREMENT TABLE COMPLETED.;[04] VERIFIED CORRECTIVE ACTION ITEM Aug 17, 2022 · N489WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2022092242808Bear Strap · crackedFORWARD GALLEY DOOR BEAR STRAP HAS A 2 INCH LONG CRACK 3 INCHES BELOW STRINGER 8R / [01] REPAIRED BY 737-700 SRM 53-10-01-2R-6 AND EA M-21-153-03542;[02] UPDATED MEASUREMENT TABLE;[03] VERIFIED MEASUREMENT TABLE COMPLETED.;[04] VERIFIED CORRECTIVE ACTION ITEM Aug 17, 2022 · N489WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2022092765106Fitting · crackedCROSS OVER DUCT SUPPORT FITTING CRACKED; BS541; LBL8; FWD LEG / [01] REMOVED AND REPLACED SUPPORT FITTING P/N 121A1116-1AAR LOT.# WO-45631100 AT BS 541 LBL 8 IAW SRM 51-40-02-0G-0;[02] VERIFIED CORRECTIVE ACTIONS STEP 1.Aug 16, 2022 · N489WN · Boeing 7377H4 · Wing, Attach FittingsSDR SWAA2022092342425Fitting · crackedCROSS OVER DUCT SUPPORT FITTING CRACKED; BS541; LBL8; FWD LEG / [01] REMOVED AND REPLACED SUPPORT FITTING P/N 121A1116-1AAR LOT.# WO-45631100 AT BS 541 LBL 8 IAW SRM 51-40-02-0G-0;[02] VERIFIED CORRECTIVE ACTIONS STEP 1.Aug 16, 2022 · N489WN · Boeing 7377H4 · Wing, Center BoxSDR SWAA2022092765075Angle · crackedINDICATION OF CRACK AT VAPOR BARRIER PRESSURE WEB UPPER ATTACH ANGLE AT LBL 43 BS 663 WL 164. FWD SIDE / [01] REQUEST NDI FOR HFEC INSPECTION FOR CRACK FREE CONDITION;;[10] FABRICATED UPPER ANGLE IAW SRM 57-10-10-2R-5 FROM 2024 T3 0.063 LOT.# 1479101-1; LOCATEAug 15, 2022 · N489WN · Boeing 7377H4 · Wing Main, Frame StructureSDR SWAA2022092342032Angle · crackedINDICATION OF CRACK AT VAPOR BARRIER PRESSURE WEB UPPER ATTACH ANGLE AT LBL 43 BS 663 WL 164. FWD SIDE / [01] REQUEST NDI FOR HFEC INSPECTION FOR CRACK FREE CONDITION;;[34] INSTALLED AT L/H VAPOR BARRIER PRESSURE WEB UPPER ATTACH ANGLE AT LBL 6 TO LBL 65 BS 66Aug 15, 2022 · N489WN · Boeing 7377H4 · Fuselage Main, KeelSDR SWAA2022092765048Panel · delaminatedLEFT WING L/E PANEL 521DB HAS DELAM AT 3EA CORNERS AT FWD EDGE / [01] REMOVED 1EA BACKUP PLATE TO FACILITATE REPAIR IAW SRM 51-40-02-0G-0 PAR 4E.;[02] IDENTIFIED PANEL 521DB IAW SRM 57-41-01-0I-4 FIGURE 5 TABLE 5 ITEM 2.<BR>DAMAGE WAS FOUND OUT OF ALLOWABLE LIAug 13, 2022 · N489WN · Boeing 7377H4 · Wing, Attach FittingsSDR SWAA2022092341540Panel · delaminatedLEFT WING L/E PANEL 521DB HAS DELAM AT 3EA CORNERS AT FWD EDGE / [01] REMOVED 1EA BACKUP PLATE TO FACILITATE REPAIR IAW SRM 51-40-02-0G-0 PAR 4E.;[05] STARTED FABRICATING REPAIR PLIES USING BMS 5-129 TY2 LOT#1497184-1; BMS 8-79 ST120 LOT#1497818-1; AND BMS 8-7Aug 13, 2022 · N489WN · Boeing 7377H4 · Wing, Attach FittingsSDR SWAA2022021170446Battery Pack · failedBATTERY PACKS AT LOCATIONS M1669; M1670; M1674 & M1675 ; BATTERY PACKS AT LOCATIONS M1669; M1670; M1674 & M1675 FAILED CAPACITY TEST / [01] R&R BATTERY PACKS AT LOCATIONS M1669; M1670; M1674 & M1675 PER MM 33-51-06Feb 9, 2022 · N489WN · Boeing 737* · Emergency LightingSDR SWAA2021100123443Warning Light · illuminatedLE FLAPS TRANSIT ILLUMINATED DURING FLAP RETRACTION FLAPS INDICATED UP LE DEVICES 1;2;3;4;7 INDICATED TRANSIT ; / [01] TROUBLE SHOOT SYSTEM ; NOT ELECTRICAL BLEED SYSTEM AND OPERATE SYSTEM SEVERAL TIMES OPS CHECK GOOD PER FIM 27-81-812 & MM 27-81-00-201Sep 27, 2021 · N489WN · Boeing 7377H4 · Leading Edge Slat Position Indicating SystemSDR SWAA2021072396374Girt Bar · defectiveFWD ENTRY AND SVC DOORS GIRT BAR DIFFICULT TO REMOVE FROM SLIDE COVER HOOKS. ; / [01] ADJ. SLIDE COVER HOOKS PER AMM 20-00-00Jul 19, 2021 · N489WN · Boeing 7377H4 · Emergency Equipment
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