N468WN

Service difficulty reports · 309

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 = 'N468WN' 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 SWAA2022041182379Support · corrodedCORROSION ON UNDERSIDE OF FLOOR SUPPORT STA 955; RBL 24; WL 208. / [01] REMOVED CORROSION ON UNDERSIDE OF FLOOR SUPPORT STA 955; RBL 24; WL 208. MAX MATERIAL REMOVED WAS .014' 1' BY 1' FROM .075'. OUT OF LIMITS PER SRM 53-70-51-1A-1.MEASURED DEPTH WITH SPHERICMar 10, 2022 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022040882370Door Sill · crackedCRACK ON EDGE BS 312 FRAME AT FWD ENTRY DOOR UPPER SILL LBL 33 WL 298. / [01] ACCOMPLISHED HFEC INSPECTION OF CRACK MARKED END IAW 737 NDTM PART 6; 51-00-00 PROCEDURE 23 TOOL# IS000450;[02] REMOVED DAMAGED AREA ON BS312 FRAME AT FWD ENTRY DOOR UPPER SILL BETWEMar 10, 2022 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022040882373Hinge Box · crackedFWD SERVICE DOOR UPPER HINGE BOX AT FWD FRAME CRACKED RBL 52 WL 255 BS 294. / [01] REMOVED FSD HINGE TORQUE TUBE ACCESS PANEL 222AR; DISPLACED HINGE TORQUE TUBE AND UPPER PIN; AND REMOVED FSD UPPER HINGE FITTING PER AMM 52-41-41-000-801.[07] INSTALLED NEW FSD Mar 10, 2022 · N468WN · Boeing 7377H4 · Fuselage, Door HingeSDR SWAA2022040882007Floor Support · crackedCRACKED FLOOR SUPPORT BS 328-344 LBL 46 WL 208. / [01] FAULT WILL BE CORRECTED ON TTG8Q00BFOUF.;[02] CORRECTION ON CCN: TTG8Q00BF0UF.;[03] CORRECTED MEASUREMENT TABLE.;[04] VERIFIED CORRECTIVE ACTION 2.Mar 10, 2022 · N468WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2022040882003Floor Support · crackedCRACKED INTERCOSTAL BS 294-312 RBL 16 WL 208. / [01] CRACK ON INTERCOSTAL BS294-BS312 RBL16 WL208 IS OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS; SRM 51-10-02-0G-0; REPLACEMENT OF PART IS APPLICABLE;[02] REMOVED; LOCATED AND DRILLED NEW INTERCOSTAL BS294-BS312 RBMar 10, 2022 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022040882004Floor Support · crackedCRACKED INTERCOSTAL BS 344-360 RBL 33 WL 208. / [01] UPON FURTHER INVESTIGATION; THERE IS NO ALLOWABLE DAMAGE FOR CRACKED INTERCOSTAL BS 344-360 RBL 33 WL 208. PART WILL BE REPLACED IAW SRM 51-10-02-0G-0; STEP 9.;[02] LOCATED; DRILLED; AND DEBURRED NEW INTERCOMar 10, 2022 · N468WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2022040882005Floor Support · crackedCRACKED FLOOR SUPPORT BS 277-294 RBL 1 WL 208. / [01] REMOVED FLOOR SUPPORT BS 277-294 RBL 1 IAW SRM 51-40-02.;[02] RECIVED NEW INTERCOSTAL P/N 141A5410U3 LOT NO 240015 AND LOCATED AND DRILLED AT BS 277-294 RBL 1 IAW SRM 51-40-05 AND DWG: 141A5400 ID:0020 REV:Mar 10, 2022 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022040882006Floor Support · crackedCRACKED FLOOR SUPPORT BS 312-328 RBL 31 WL 208. / [01] NO ENTRIES FOUND ON SRM FOR CRACK ON FLOOR SUPPORT AT BS312-BS328 RBL 31;REPLACEMENT OF THE PART IS APPLICABLE I.A.W SRM 51-10-02-0G-0. PAR 9.C;[02] REMOVED;LOCATED AND DRILLED FLOOR SUPPORT BS312-BS328 RBMar 10, 2022 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022040882008Floor Support · crackedCRACKED FLOOR SUPPORT BS 380-400 LBL 1 WL 208. / [01] REMOVED FLOOR SUPPORT AT BS 380-400 LBL1 WL 208 PER SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW FLOOR SUPPORT AT BS 380-400 LBL1 PER SRM 51-40-05-0G-0 AND DWG #143A5400; OK TO INSTALL;[03] VERIFIED CORREMar 10, 2022 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022040882009Floor Support · crackedCRACKED FLOOR SUPPORT BS 380-400 RBL 7 WL 208. / [01] REMOVED FLOOR SUPPORT AT BS 380-400 RBL7 WL 208 PER SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW FLOOR SUPPORT AT BS 380-400 RBL7 WL 208 PER SRM 51-40-05-0G-0 AND DWG #143A5400. OK TO INSTALL;[03] VERIFIEMar 10, 2022 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022040882010Floor Support · crackedCRACKED FLOOR SUPPORT BS 380-400 RBL 40 WL 208. / [01] FLOOR SUPPORT BS380-BS400 RBL40 WL 208 IS OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS; SRM 51-10-02-0G-0; REPLACEMENT OF PART IS APPLICABLE;[02] REMOVED ;LOCATED AND DRILLED NEW FLOOR SUPPORT BS380-BS400 RBL4Mar 10, 2022 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022040882381Strap · corrodedCORROSION ON STRAP STA 1029; RBL 17.5; WL 208. / [01] STRAP STA 1029; LBL 17.5; WL 208 IS OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS; SRM 51-10-02-0G-0; REPLACEMENT OF PART IS APPLICABLE;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] REMOVED;LOCATED AND DRILLED NEMar 10, 2022 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022040882382Channel · corrodedCORROSION ON AFT ENTRY MOPSILL STA 900-988; L/H; WL 208. / [01] EVALUATED CORROSION ON AFT ENTRY MOPSILL STA 900-988; L/H; WL 208. FOUND TO HAVE 100 PERCENT MATERIAL LOSS. OUT OF LIMITS PER SRM 53-70-15-1A-1. REPLACEMENT OF PART IS APPLICABLE SRM 51-10-02-0G-0Mar 10, 2022 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022041181998Floorbeam · corrodedCORROSION ON FLOOR BEAM BS 294 RBL 11 WL 208. / FORMED ITEM 2 ANGLES (2EA) MADE OUT 7075-T0 0.080' C LOT 1001382 ALL I.A.W SRM 51-30-01-0G-0 FIG 3 TABLE 1; REMOVED CORROSION ON FLOOR BEAM BS294 RBL11 WL208 UPPER CHORD 1.2'X1.0' AREA ORIGINAL MATERIAL THICKNESSMar 9, 2022 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022041181576Stiffener · crackedRT HORIZONTAL STAB AT RIB 120.3; #3 STIFFENER IS CRACKED AT THE LOWER END RT STAB L/E @ STAB STA 120.3. / [01] REMOVED RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB AT STAB STA 120.30 TO ACCESS RIB REPAIRS IAW SRM 51-40-02-0G-0.;[02] APPLICABLE REPAIR FOR THIS CMar 9, 2022 · N468WN · Boeing 737 · Horizontal Stabilizer, Spar/RibSDR SWAA2022041181577Stiffener · crackedRT HORIZONTAL STAB AT RIB 129.5; #4 STIFFENER IS CRACKED AT THE LOWER END RT STAB L/E @ STAB STA 129.5 / [01] REMOVED RIGHT HAND HORIZONTAL STABILIZER RIB AT STAB STA 129.50 TO ACCESS RIB REPAIRS IAW SRM 51-40-02-0G-0.;[02] APPLICABLE REPAIR FOR THIS CRACKED HMar 9, 2022 · N468WN · Boeing 737 · Horizontal Stabilizer, Spar/RibSDR SWAA2022041181587Support · corrodedCORROSION ON ACB FLOOR TO SIDEWALL SUPPORT FROM STA 727B+10 TO STA 767; WL 156; RBL 22 / [01] EVALUATED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE BS 727E+10 RBL 22 WL 156; FOUND 0.015 REMOVED FROM ORIG 0.040 IN 1'X1'Mar 9, 2022 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022041181593Support · corrodedCORROSION ON ACB FLOOR TO SIDEWALL SUPPORT FROM STA 727 TO STA 787; WL 156; LBL 22. / [01] EVALUATED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE BS 747+10 LBL 22 WL 156; FOUND 0.015 REMOVED FROM ORIG 0.040 IN 1'X1' AREMar 9, 2022 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022041181595Shield · corrodedCORROSION ON ACB DOOR CUTOUT FWD SHIELD FROM STA 767+2; TO STA 767+16; WL 156; RBL 23. / [01] EVALUATED CORROSION ON SHIELD BS 767+16 WL 157 RBL 23; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0;[02] VERIFMar 9, 2022 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022041181596Support · corrodedCORROSION ON ACB FLOOR TO SIDEWALL SUPPORT AT STA 867+15; WL176; RBL 22. / [01] EVALUATED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT BS 867+15 RBL 22 WL 167; FOUND 0.015 REMOVED FROM ORIG 0.040 IN 1'X1' AREAS; FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 USIMar 9, 2022 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022041181597Strap · corrodedCORROSION ON ACB TENSION STRAP UPPER SURFACE; STA 767+4 TO STA 767+5; RBL 20; WL 156 CORRECTION: CORROSION IS ON VERTICAL WEB UPPER SURFACE AT STA 767+4 TO STA 767+5 RBL 20 WL 156. / [01] DISCREPANCY WAS CORRECTED TO VERTICAL WEB UPPER SURFACE; EVALUATED CORROMar 9, 2022 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022041181965Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS420 - BS500D LBL24. / [01] EVALUATED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 460+10 LBL 24 WL 156; FOUND 0.015 REMOVED FROM ORIG 0.040 IN 1'X1' AREAS Mar 9, 2022 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022041181993Seat Track · corrodedCORROSION ON PASSENGER CABIN SEAT TRACK BS400 LBL45 WL208. / [01] BLENDED AND REMOVED CORROSION DAMAGE FROM SEAT TRACK AT BS 400 LBL 45 WL 208 IAW SRM 53-00-52-1A-1 STEP 2. A.;[02] VERIFIED CORRECTIVE ACTION 1.;[03] EVALUATED CORROSION REMOVAL FROM SEAT TRACK Mar 9, 2022 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022041181999Floorbeam · corrodedCORROSION ON FLOOR BEAM BS 328 RBL 42 AND 54 WL 208. / [01] REMOVED FLOOR SUPPORT ANGLE AT BS 312 TO 328 R/H FOR ACCESS PER SRM 51-40-02-0G-0;[18] INSTALLED REPAIR PARTS ITEM 1(1EA);2(2EA);3(2EA);4(9);5(1);6(2EA)AND BRACKETS COMMON TO THE REPAIR LISTED ON CORRMar 9, 2022 · N468WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2022041182000Chain Drive · corrodedCORROSION ON FWD SERVICE DOOR MOP SILL BS 320-336 RBL 58 WL 208. / [01] VERIFIED APPLICABILITY OF SRM 53-10-15-1A-2 ALLOWABLE DAMAGE FWD GALLEY DOOR SURROUND STRUCTURE;[02] REMOVED ALL FASTENERS COMMON TO FSD MOP SILL IAW SRM 51-40-02-0G-0;[03] EVALUATED DAMAGMar 9, 2022 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022041181578Stiffener · crackedLT HORIZONTAL STAB AT RIB 120.3; #1 STIFFENER IS CRACKED AT THE LOWER END LT STAB L/E @ STAB STA 120.3 / [01] REMOVED LEFT HORIZONTAL STABILIZER RIB AT STAB STA 120.30 TO ACCESS RIB REPAIR IAW SRM 51-40-02-0G-0.[08] FABRICATED REPAIR PARTS; T-SECTION 7075-T765Mar 9, 2022 · N468WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2022041181971Plate · brokenRT WING WIGGLE PLATE AT ORSS 261 IS BROKEN. / [01] REMOVED AND REPLACED R/H WING WIGGLE PLATE AT ORSS 261 IAW SRM 51-40-02-0G-0 PARA 4.;[02] VERIFIED CORRECTIVE ACTION 1.Mar 9, 2022 · N468WN · Boeing 7377H4 · Wing, Control SurfacesSDR SWAA2022040882002Frame · crackedFRAME CRACKED ON LOWER END AT BS 294.5 RBL 55 WL 208. / [01] EVALUATED DAMAGED; VERIFIED APPLICABILITY OF REPAIR AND DAMAGE REMOVED L 1.8'X W 0.85' AT END OF STUB FRAME BS 294-296 WL 208 RBL 53 IAW SRM 53-10-15-2R-7 REP 7.;[10] PERFORMED DVI ON REPARIR AREA ANMar 9, 2022 · N468WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2022040881983Seat Track · corrodedCORROSION ON PASSENGER CABIN SEAT TRACK BS500D+7 LBL45 WL208. / [01] BLENDED AND REMOVED CORROSION DAMAGE FROM SEAT TRACK AT BS 500D+7 LBL 45.5 WL 208 IAW SRM 53-00-52-1A-1 STEP 2. A.;[02] VERIFIED CORRECTIVE ACTION 1.;[03] EVALUATED CORROSION REMOVAL FROM SEAMar 9, 2022 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022040882011Floorbeam · corrodedCORROSION ON FLOOR BEAM BS 312 LBL 50 WL 208. / [01] REMOVED CORROSION ON FLOOR BEAM BS 312 LBL 50 WL 208 IN A 2.9' X 2.2' AREA IAW SRM 51-10-02-0G-0[17] INSTALLED FLOOR PANEL 221DF AND 221BF USING NEW BACN11AF CLIPNUTS PER MM 51-40-02;[18] VERIFIED BACN11AF CMar 9, 2022 · N468WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2022040782013Channel · crackedFWD ENTRY DOOR MOP SILL CRACKED AT BS 309 LBL 56 WL 208. / [01] REMOVED FWD ENTRY DOOR MOP SILL AT BS 270 - BS 360 LBL 56 WL 208 IAW SRM 51-40-02-0G-0;[02] PRIOR TO REMOVING FWD ENTRY DOOR MOP SILL; FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15-1A-1 PARG 4;[03] VMar 9, 2022 · N468WN · Boeing 737* · Fuselage Main, StructureSDR SWAA2022041181187Rib · crackedCRACKED RIB FLANGE ON RT. HORIZ. STAB REMOVEABLE LEADING AT L/E STA.95.96 / [01] UPDATED PARTS SECTION;[02] REMOVED AND REPLACED RIB ON RT HORIZONTAL STAB L/E AT L/E STA 95.96 IAW SRM 51-40-02-0G-0 STEP 4; SRM 51-40-05-0G-0 AND BAC DWG 186A1001.;[03] VERIFIED Mar 8, 2022 · N468WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2022041181188Rib · crackedCRACKED RIB FLANGE ON RT. HORIZ. STAB. REMOVEABLE LEADING EDGE AT L/E STA. 105.26 CRACKED RIB FLANGE ON RT. HORIZ. STAB LEADING EDGE AT L/E STA.105.26 / [01] REMOVED RT HORIZ. STAB RIB ASSY. AT L/E STA 105.26 IAW SRM 51-40-02 AND DWG 186A1304.;[02] RT HORIZ. SMar 8, 2022 · N468WN · Boeing 737 · Horizontal Stabilizer, Spar/RibSDR SWAA2022041181571Angle · crackedR/H BS 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT RBL8 WL 167.68 / [01] UPDATED MEASUREMENT TABLE AND VALIDATED APPLICABILITY OF SRM 57-10-10-2R-5 TO BE CORRECT[11] INSTALLED REPAIR PARTS @ R/H BS663 VAPOR BARRIER UPPER ATTACH ANGLE RBL6-RBL14 WL167.68Mar 8, 2022 · N468WN · Boeing 7377H4 · Wing Main, Frame StructureSDR SWAA2022010657885Handle · brokenDOOR ASSIST HANDLE BROKEN R2 DOOR ; DOOR ASSIST HANDLE ROKEN R2 DOOR / [01] R&R DOOR ASSIST HANDLE R2 DOOR PER AMM 52-41-31Jan 4, 2022 · N468WN · Boeing 7377H4 · Galley DoorsSDR SWAA2021121452048None · brokenSUPPLEMENTAL INFORMATION: EMERGENCY EXIT SIGN RT OVERWING EXIT BROKEN ; / [01] R&R?D EXIT SIGN RT OVERWING EXIT AMM 33-51-01Dec 10, 2021 · N468WN · Boeing 737 · Emergency LightingSDR SWAA2020042043487Doubler · crackedEXTERNAL POWER DOOR CUTOUT DOUBLER IS CRACKED AT THE AFT LOWER CORNER / REMOVED DAMAGE AT EXTERNAL POWER DOOR CUTOUT DOUBLER AT THE AFT LOWER CORNER PER REF B737 SRM 53-10-15-1A-4Apr 19, 2020 · N468WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2021051336710Skate Angle · chafedCHAFED RH CROWN SKATE ANGLE AT BS1009 RBL14. / REMOVED AND REPLACED R/H CROWN SKATE ANGLE AT BS1006-BS1016 RBL14 IAW SRM 51-40-02-0G-0 AND DWG 147A3200Apr 7, 2020 · N468WN · Boeing 7377H4 · Vertical StabilizerSDR SWAA2020042036709Skate Angle · chafedCHAFED RH CROWN SKATE ANGLE AT BS1016 TO BS1121 RBL14. / REPAIRED CHAFED R/H CROWN SKATE ANGLE AT BS1016 TO BS1121 RBL14 IAW SRM 53-80-71-2R-6 REPAIR 6Apr 7, 2020 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2020042036708Stiffener · crackedCRACKED VERTICAL STIFFENER OF AFT SIDE OF B.S. 663 LOWER COMPOSITE BULKHEAD; L.B.L. 25; W.L. 150. / REMOVED AND REPLACED VERTICAL STIFFENER OF AFT SIDE OF BS 663 LOWER COMPOSITE BULKHEAD LBL 25 WL 150 IAW SRM 51-40-02-0G-0 AND DWG 111A1000Apr 7, 2020 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021051336442Skate Angle · chafedLH CROWN SKATE ANGLE FROM BS 1010_1017 IS CHAFED. / REMOVED AND REPLACED L/H CROWN SKATE ANGLE FROM BS1006-BS1017 IAW SRM 51-40-02-0G-0 AND DWG 147A3200Apr 6, 2020 · N468WN · Boeing 7377H4 · Vertical StabilizerSDR SWAA2021051336443Skate Angle · chafedLH CROWN SKATE ANGLE IS CHAFED AT BS 1109 AREA. NO VERIFICATION OF CHAFE REMOVED PRIOR TO APPLICATION OF TOP COAT. / WORK ACCOMPLISH WITH SAM 326 A1296390.Apr 6, 2020 · N468WN · Boeing 7377H4 · Vertical StabilizerSDR SWAA2020042236438Panel Support · corroded***CORROSION*** ON AFT CARGO BAY FLOOR PANEL SUPPORT AT B.S. 773; L.B.L. 21 -R.B.L. 21; W.L. 155. / REPLACED ACB FLOOR PANEL SUPPORT BS773; LBL21 - RBL21; WL155 P/N 3530573 PO# 777784 IAW SRM 51-10-02 STEP 9.C. 89008U 15APR20Apr 6, 2020 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2020042236437Support · corroded***CORROSION*** ON AFT CARGO BAY FLOOR PANEL SUPPORT AT B.S. 747; L.B.L. 21 -R.B.L. 21; W.L. 155. / AFT CARGO BAY FLOOR PANEL SUPPORT (P/N 146A9401-8) AT B.S 747; LBL 21 - RBL 21; W.L 155. WAS FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE DAMAGE PER SRM 51-10-Apr 6, 2020 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2020042236430Support · corroded***CORROSION*** ON AFT CARGO BAY AFT BULKHEAD CENTER PANEL LOWER SUPPORT AT B.S. 947; L.B.L. 21 - R.B.L. 21; W.L. 155. / REMOVED AND REPLACED AFT CARGO BAY AFT BULKHEAD CENTER PANEL LOWER SUPPORT AT BS 947; LBL21 RBL21 WL155 IAW SRM 51-40-02 AND DWG 149A8117 RApr 6, 2020 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2020042236431Support · corroded***CORROSION*** ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S. 887-947; R.B.L. 21; W.L. 155. / REMOVED CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT BS 887-BS947 WL 155 MAX. MAT. LOSS 3.'X2.'X.015 ORIGINAL THICKNESS .040 FOUND TO BE OUT OF LIMITS; RApr 6, 2020 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2020042236434Support · corroded***CORROSION*** ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S. 747-847; L.B.L. 21; W.L. 155. / REMOVED AND INSTALLED NEW ACB FLOOR TO SIDEWALL SUPPORT B.S. 727 TO B.S. 847. LBL 21; WL 155 ITEM #7532037; PO #779297 IAW SRM 51-40-02-0G-0; DWG #146A2500; DWG Apr 6, 2020 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2020042236435Support · corroded***CORROSION*** ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT B.S. 747-767; R.B.L. 21; W.L. 155. / REMOVED CORROSION FROM ACB FLOOR TO SIDEWALL SUPPORT B.S 747-767 RBL 21; WL 155 MAX MAT REMOVED 4'X2'X.012'; FOUND TO BE OUT OF LIMITS; REMOVED AND REPLACED R/H Apr 6, 2020 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2020042236441Intercostal · corroded***CORROSION*** ON AFT CARGO BAY INTERCOSTAL AT B.S. 787-807; R.B.L. 6; W.L. 150. / REMOVED AND REPLACED ACB INTERCOSTALL AT BS 787-807 RBL 6 WL 150 DUE TO MORE THAN 100% OF MATERIAL LOSS IN AN AREA OF 2'X2' IAW SRM 51-40-02-0G-0 AND DWG #146A1830Apr 6, 2020 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2020042036440Cargo Track · cocked***CORROSION*** ON AFT CARGO BAY CARGO TRACK AT B.S. 794-847; R.B.L. 14; W.L. 155. / REPAIRED AFT CARGO BAY TRACK BY REPLACING TRACK FROM BS 727 TO 747+10 AND FROM BS 757 TO BS 887 WITH A REPAIR CHANNEL SPLICE AT BS 747+10; RBL 14; WL 155 IAW EA #1-A53-4982; SApr 6, 2020 · N468WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
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