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 SWAA2024042665548Support Angle · crackedCRACK ANGLE - SUPPORT LOCATED BS 947.5 AND S-26L AFT CARGO COMPARTMENT 2024-195835<[01] REPLACED SUPPORT ANGLE LOCATED BS 947.5 AND S-26L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9. AND DRAWING # 149A8103 REV: -. SEE INDIVIDUAL SIGN OFF BELOW.;[02]Mar 19, 2024 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024042665552Floorbeam · crackedCRACK ANGLE - SUPPORT LOCATED BS 727 BETWEEN S-27R TO S-27L AFT CARGO COMPARTMENT 2024-195840<[01] REPLACE ANGLE - SUPPORT LOCATED BS 727 BETWEEN S-27R TO S-27L AFT CARGO COMPARTMENT IAW. B737-700 SRM 51-40-02-0G-0 AND DRAWING 144A2600 REV B;[02] CORRECTE STEPMar 19, 2024 · N468WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2024042665549Intercostal · corrodedCORROSION WEB - INTERCOSTAL LOCATED BS 767 TO BS787 ND S-25R WL 156 AFT CARGO COMPARTMENT 2024-195841<[01] REPLACE WEB-INTERCOSTAL LOCATED : BS 767 TO BS787 ND S-25R WL 156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 AND DRAWING #146A0081 REV A.;[02] Mar 19, 2024 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024042665026Pressure Deck · crackedCRACK INDICATION FOUND ON HORIZONTAL PRESSURE DECK WEB LBL 30 AT MAIN WHEEL WELL COMPARTMENT. CRACK LENGTH:0.328 INCH APPROX. 2024-195800 EXACTLY LOCATION OF DAMAGE: HORIZONTAL PRESSURE DECK BS-663 TO BS-675 WEB LBL 30 AT MAIN WHEEL WELL COMPARTMENT. CRACK LENMar 18, 2024 · N468WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2024042665161Frame · crackedCRACK FRAME LOCATED STA747 BETWEEN STR8R TO STR9R AT PASSENGER CABIN 2024-195816<[01] REPAIRED FRAME LOC. STA747 BTW S-8R TO -9R AT PASSENGER COMPARTMENT I.A.W EA 1-A53-12114.SE INDIVIDUAL SIGN OFFS BEOW;[02] CORRECTED STEP 1 <BR>PERFORMED PERMANENT REPAIR ON Mar 18, 2024 · N468WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2024042665164Frame · crackedCRACK FRAME LOCATED STA827 BETWEEN STR8R TO STR9R AT PASSENGER CABIN 2024-195818<[01] PERFORMED PERMANENT REPAIR ON FRAME LOC. STA827 BETWEEN STR8R TO STR9R AT PASSENGER CABIN I.A.W EA 1-A53-12114. SEE INDIVIDUAL SIGN OFF BELOW;[02] PERFORMED PERMANENT REPAIR Mar 18, 2024 · N468WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2024042665029Web · crackedCRACK WEB FLOOR STRUCTURE LOCATED BETWEEN STA500D TO STA520 AT LEVEL STR28R AT FWD CARGO COMPARTMENT 2024-195808<[01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 22-JAN-25; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: Mar 18, 2024 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024042665027Stringer · crackedCRACK STRINGER 23R LOCATED BS 540 FWD CARGO COMPARTMENT 2024-195759<[01] ULTRASONIC EQUIPMENT USED P/N: 45MG; S/N: 232017609 AND DUE DATE: 22-SEP-24.;[02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES500000; S/N: 142811020; DUE DATE: 23-JAN-25 AND TEMPERATMar 18, 2024 · N468WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2024042665028Stringer · crackedCRACK STRINGER 26L LOCATED STA540 FWD CARGO COMPARTMENT 2024-195762<[01] ULTRASONIC EQUIPMENT USED P/N: 45MG; S/N: 232017609 AND DUE DATE: 22-SEP-24.;[02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES500000; S/N: 142811020; DUE DATE: 23-JAN-25 AND TEMPERATMar 18, 2024 · N468WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2024042665030Stringer · crackedCRACK STRINGER 25L LOCATED STA 540 FWD CARGO COMPARTMENT 2024-195806<[01] ULTRASONIC EQUIPMENT USED P/N: 45MG; S/N: 232017609 AND DUE DATE: 22-SEP-24.;[02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES500000; S/N: 142811020; DUE DATE: 23-JAN-25 AND TEMPERAMar 18, 2024 · N468WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2024042665160Frame · crackedCRACK FRAME LOCATED STA 747 BETWEEN STR 8L TO STR 9L AT PASSENGER CABIN 2024-195817<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 200053402; DUE DATE: 24-AUG-24.;[02] PERFORMED HFEC INSPECTION ON AREA AFTER REMOVED BRACKET AND NOT FOUND DMar 18, 2024 · N468WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2024042964847Crease Beam · corrodedCORROSION CREASE BEAM LOCATED STA639 RBL 64.5 WL 208.1 CENTER SECTION 2024-195751<[01] REPLACED CREASE BEAM LOCATED STA616 PLUS 10 IN TO STA639 PLUS 10IN RBL 64.5 WL 208.1 CENTER SECTION IAW B737-700 SRM 53-40-02. AND DWG-144A5901 REV: - SEE INDIVIDUAL SIGN OFMar 17, 2024 · N468WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2024042664841Stringer · crackedCRACK ON STRINGER 15L LOCATED BETWEEN STA294.5 TO STA303.9 AT FWD GALLEY AREA 2024-195741<[01] TOOL USED PN. 45MG; SN. 130061901 ; DUE DATE. 09-JUN-24;[02] TOOL USED STEP 7: EDDY CURRENT EQUIPMENT; P/N: NORTEC 500D; S/N: N500X12101U102020; DUE DATE: 07 SEP 24.Mar 17, 2024 · N468WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2024042664842Tie Clip · crackedCRACK TIE CLIP LOCATED STA277 AND STR10R AT PASSENGER CABIN 2024-195743<[01] INSTALLED TIE CLIP LOCATED STA277 AND STR10R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 141A1110 SHEET 18 REV -;[02] REPLECED TIE CLIP LOCATED STA277 AND STR10R AT PASSENGERMar 17, 2024 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024042664840Crease Beam · corrodedCORROSION CREASE BEAM LOCATED STA639 AND LBL64.5 WL208.1 CENTER SECTION 2024-195750<[01] REPLACED CREASE BEAM LOCATED STA616 PLUS 10 IN TO STA639 PLUS 10IN AND LBL64.5 WL208.1 CENTER SECTION IAW B737-700 SRM 51-40-02 AND DWG 144A5901 REV:- SEE INDIVIDUAL SIGN Mar 17, 2024 · N468WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2024042664844Floorbeam · crackedCRACK ANGLE FLOOR STRUCTURE LOCATED BS 540 LBL 1 CENTER SECTION 2024-195748<[01] REPLACE ANGLE FLOOR STRUCTURE LOCATED BS 540 LBL 1 CENTER SECTION IAW. B737-700 SRM 51-40-02-0G-0 AND DRAWING 143A0060;[02] INSTALLED NEW ANGLE FLOOR STRUCTURE; PERFORMED VISUAL IMar 17, 2024 · N468WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2024042664706Angle · crackedCRACK ANGLE LOCATED BS 695 RBL 24.75 AT CENTER WING BOX. REPLACED ANGLE LOC. BS 695 RBL 24.75 AT CENTER WING BOX IAW B737-700 SRM 51-40-02-0G-0 AND DWG #111A6000 AND DWG #273A9110.;[03] REPLACED ANGLE LOC. BS 695 RBL 24.75 AT CENTER WING BOX IAW B737-700 SRM Mar 17, 2024 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024042664843Floorbeam · crackedCRACK ANGLE FLOOR STRUCTURE LOCATED BS540 RBL 24.75 CENTER SECTION 2024-195746<[01] REPLACED ANGLE FLOOR STRUCTURE LOCATION BS540 RBL 24.75 CENTER SECTION IAW B737-700 SRM 51-40-02-0G-0 AND DRAWING #143A0060 REV: A.;[02] REPLACED ANGLE FLOOR STRUCTURE LOCATIONMar 17, 2024 · N468WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2024042664846Floorbeam · crackedCRACK ANGLE FLOOR STRUCTURE LOCATED STA540 BETWEEN RBL24.75 TO RBL45.5 CENTER SECTION 2024-195747<[01] REPLACE ANGLE FLOOR STRUCTURE LOCATED STA540 BETWEEN RBL24.75 TO RBL45.5 CENTER SECTION IAW. B737-700 SRM 51-40-02-0G-0 AND DRAWING 143A0060;[02] INSTALLED NMar 17, 2024 · N468WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2024042664845Floorbeam · crackedCRACK ANGLE FLOOR STRUCTURE LOCATED STA540 BETWEEN LBL24.75 TO LBL45.5 CENTER SECTION 2024-195749<[01] REPLACE ANGLE FLOOR STRUCTURE LOCATED STA 540 BETWEEN LBL24.75 TO LBL45.5 CENTER SECTION IAW B737-700 SRM 51-40-02-0G-0 AND DRAWING 143A0060;[02] INSTALLED NMar 17, 2024 · N468WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2024042664037Support Angle · crackedCRACK ANGLE - SUPPORT LOCATED BS 727D CEILING AREA AFT CARGO COMPARTMENT 2024-195702 CRACK ANGLE - SUPPORT LOCATED BS727A TO BS747 CEILING AREA AFT CARGO COMPARTMENT<[01] PERFORMED DETAILED VISUAL INSPECTION ON ANGLE - SUPPORT LOC. AT BS727A TO BS747 CEILING AMar 15, 2024 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2024042663458Frame · crackedCRACK ON FRAME LOCATED BS 259.5 AT LEVEL STR 9L AT PASSENGER CABIN 2024-195616<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60007161486; DUE DATE: 28-JUL-24.;[02] PERFORMED PERMANENT REPAIR LOCATED ON FRAME LOCATED BS 259.5 AT LEVEL STR Mar 14, 2024 · N468WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2024042663456Rib · crackedCRACK INSPAR RIB 120.30 AT 36 INCHES OF FRONT SPAR AT RT HORIZONTAL STABILIZER 2024-195612<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE DATE: 11-MAR-25.;[02] TOOL UED: EDDY CUREENT EQUIPMENT; PN: NORTEC 600D; SN: 6000716Mar 14, 2024 · N468WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2023101209759Sign · out of adjustAFT GALLEY AREA O/H EXIT SIGN IS LOSE AND HANGING DOWN<[01] REMOVE AND REPLACED AFT CABIN O/H EMER EXIT SIGN ASSY PER M/M 33-51-01; OPS CHK GOOD.Oct 10, 2023 · N468WN · Boeing 7377H4 · Emergency LightingSDR SWAA2023072882896Cover · looseFO SIDE OVER WING EXIT DOOR HANDLE COVER LOOSE<[01] REESE URGED COVER IAW M/M 52-22-51Jul 27, 2023 · N468WN · Boeing 7377H4 · Emergency ExitsSDR SWAA2023041024041Seal · cracked-LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED.<[01] R&R LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL REF AMM 53-31-31.;[02] R&R LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL REF AMM 53-31-31.Apr 6, 2023 · N468WN · Boeing 7377H4 · Horizontal Stabilizer, Tab StructureSDR SWAA2023041024042Seal · cracked-RIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED.<[01] R&R RIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL. IAW AMM 53-31-31Apr 6, 2023 · N468WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/SkinSDR SWAA2023040724044Battery Pack · failed5 EMERGENCY BATTERY PACKS FAILED CAPACITY CHECK<[01] REMOVED AND REPLACED BATTERY PACKS AT LOCATIONS: M1668; M1672; M1673; M1669; M1675 PER AMM 33-51-06. OPS CHECK GOOD.Apr 6, 2023 · N468WN · Boeing 7377H4 · Emergency LightingSDR SWAA2022121380961Light · inoperativeLEFT OVERWING EMERGENCY EXIT LIGHT (EXTERIOR) INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-04, OPS CHECKED GOOD.Dec 13, 2022 · N468WN · Boeing 7377H4 · Emergency LightingSDR SWAA2022090750921None · missingEMERGENCY EXIT SIGN MISSING AT FWD ENTRY LEFT SIDE / [01] INSTALLED NEW LENS IAW AMM 33-51-01 OPS CHECK GOODSep 7, 2022 · N468WN · Boeing 7377H4 · Emergency LightingSDR SWAA2022081842449Panel · elongatedPANEL 193B HAS NUMEROUS ELONGATED FASTENER HOLES AND COUNTERSINKS. / [01] R&R PANEL 193B PER SRM 51-40-02Aug 17, 2022 · N468WN · Boeing 7377H4 · Aerodynamic FairingsSDR SWAA2022080839181Bracket · brokenLT MLG AREA; LANDING GEAR ELECTRICAL BUNDLE GUIDE; LOWER BRACKET BROKEN LT MLG AREA LANDING GEAR ELECTRICAL BUNDLE GUIDE LOWER BRACKET BROKEN / [01] REMOVED AND REPLACED BRACKET PER. SRM REF. 51-40-02.Aug 6, 2022 · N468WN · Boeing 7377H4 · Wing Miscellaneous StructureSDR SWAA2022041191003Light · inoperativeEMERGENCY EXIT SIGN FWD OF L/H OWE HATCH INOP. / [01] CONNECTED CONNECTORS D3670 AND 3672 AND PERFORMED GOOD OPS TEST OF EMERGENCY EXIT SIGN FWD OF L/H OWE HATCH PER AMM 33-51-01-960-801 STEP 2.C.(2).;[02] VERIFIED CORRECTIVE ACTIONS STEP 1.Apr 5, 2022 · N468WN · Boeing 7377H4 · Emergency LightingSDR SWAA2022040790169Floor Panel · damagedCABIN FLOOR PANEL 231DF POPS WHEN WALKED ON. / [01] REMOVED FLOOR PANEL 231DF IAW AMM 53-21-00-000-801<BR>REMOVED AND REPLACED FOAM TAPE PER AMM 53-21-00-400-801 OK TO CLOSE FLOOR PANEL;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] OK TO CLOSE GIVEN PANEL 231DFMar 31, 2022 · N468WN · Boeing 737* · Fuselage Floor PanelSDR SWAA2022040888503Seal Depressor · crackedUPON REMOVING SEAL DEPRESSOR FROM FSD SURROUND STUB FRAME; NOTICED SEAL DEPRESSOR IS CRACKED AT BS294 RBL55 WL255. UPON REMOVING SEAL DEPRESSOR FROM FSD SURROUND STUB FRAME NOTICED SEAL DEPRESSOR IS CRACKED AT BS294 RBL55 WL255. / [01] UPON INVESTIGATION; THERMar 27, 2022 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022040886965Stub Frame · crackedUPON REMOVING FSD UPPER HINGE FITTING; FSD SURROUND STUB FRAME IS CRACKED AT BS294 RBL55 WL255. / [01] LOCATED AND DRILLED NEW FSD SURROUND STUB FRAME AT BS 294 RBL 55 WL 255 IAW SRM 51-40-05-0G-0 AND DWG 141A8370;[02] VERIFIED CORRECTIVE ACTION 1;[03] OK TO IMar 23, 2022 · N468WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2022040886047Floor Support · crackedCRACKED FLOOR SUPPORT BS 312-344 LBL 46 WL 208. / [01] UPON FURTHER INVESTIGATION FOUND CRACKED FLOOR SUPPORT TO BE LOCATED AT BS 312-328; LBL46 WL 208. REMOVED CRACKED FLOOR SUPPORT BS 312-328 LBL 46 WL 208 IAW SRM 51-40-02 0G-0.;[02] LOCATED AND DRILLED NEW Mar 21, 2022 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022040786048Lens · crackedAFT SERVICE DOOR EMERGENCY LIGHT LENS IS CRACKED. / [01] FAULT TO BE CORRECTED ON TTG8Q00BFOV2.;[02] REMOVED & REPLACED AFT SERVICE DOOR (ASD) EMERGENCY LIGHT LENS IAW AMM 33-51-01-960-802;[03] INSPECTED & VERIFIED CORRECTIVE ACTION ITEM 2.Mar 21, 2022 · N468WN · Boeing 7377H4 · Emergency LightingSDR SWAA2022041183741Web · corrodedCORROSION ON BS 348 FRAME CLOSE OUT WEB LBL 62 WL 209. / [01] REMOVED CORROSION ON 348 FRAME CLOSEOUT WEB; LBL 62; WL 209. MAX MATERIAL REMOVED WAS .019' 1' BY 2' FROM .071'. OUT OF LIMITS PER SRM 53-10-15-1A-1; SRM 51-10-02-0G-0.;[02] VERIFIED CORRECTIVE ACTIMar 14, 2022 · N468WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2022041183070Panel · debondedPANEL 193CR HAS SMALL DISBOND ON INNER SURFACE OVER CORE; MARKED / [01] IDENTIFIED PANEL MATERIAL IAW SRM 53-40-70-0I-1; TABLE 2; FIG. 2; ITEM 9. <BR><BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-40-70-1A-1; PARA. 4.B.(5). <BR><BR>AREA IS TO BE REPMar 12, 2022 · N468WN · Boeing 7377H4 · Aerodynamic FairingsSDR SWAA2022041183073Panel · debondedPANEL 193CL HAS SMALL DISBOND ON INNER SURFACE OVER CORE; MARKED / [01] IDENTIFIED MATERIAL OF PANEL 193CL IAW SRM 53-40-70-0I-1 FIGURE 1-2; ITEM 9; TABLE 2<BR><BR>DAMAGE IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-40-70-1A-1 TABLE 101; PARA 4.A(5)<BR><BR>REPMar 12, 2022 · N468WN · Boeing 7377H4 · Aerodynamic FairingsSDR SWAA2022040883069Skin · debondedPANEL 193AL HAS DISBOND ON INNER SURFACE CORE AREA; MARKED / [01] IDENTIFIED PANEL IAW SRM 53-40-70-0I-1 FIG 2 TABLE 2 ITEM 7. <BR><BR>DAMAGE TO INNER SURFACE CORE AREA IS BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 53-40-70-1A-1 PARA 4.A (6). <BR><BR>DAMAGE TO (1EMar 12, 2022 · N468WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2022040883068Panel · debondedPANEL 193AR HAS SEVERAL DISBONDS TO INNER SURFACE OF PANEL CORE AREA; MARKED / [01] IDENTIFIED PART AND MATERIALS IAW SRM 53-40-70-0I-1 FIGURES 1-2; TABLE 2; ITEM[16] APPLIED BMS10-103 PRIMER & BMS10-60 ENAMEL IAW SRM 51-70-05-2R-2 PARA 4 STEP K.<BR>RE INSTALLMar 12, 2022 · N468WN · Boeing 7377H4 · Aerodynamic FairingsSDR SWAA2022041182636Stiffener · crackedRT HORIZ STAB RIB AT STAB STA 129.50 #3 VERT STIFFENER IS CRACKED. / [01] APPLICABLE REPAIR FOR THIS CRACKED HORIZONTAL STAB RIB STIFFENER LOWER END IS SRM 55-10-09-2R-4.05] ACCOMPLISHED HFEC INSPECTION OF DAMAGE CUTOUT AND HOLES IN REPAIR AREA NO CRACK NOTED Mar 11, 2022 · N468WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/RibSDR SWAA2022041182375Strap · corrodedCORROSION ON STRAP STA 1018; LBL 3; WL 208. / [01] STRAP STA 1018; LBL 3; 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 STRAP STA 1018; LBL3; WL 208Mar 10, 2022 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022041182376Strap · corrodedCORROSION ON STRAP STA 1016-1029; RBL 3; WL 208. / [01] STRAP STA 1016-1029; RBL 3; 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 STRAP STA 1016-10Mar 10, 2022 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022041182377Channel · corrodedCORROSION ON AFT SERVICE MOPSILL STA 927-1006; R/H; WL 208. / [01] EVALUATED CORROSION ON ASD MOPSILL STA 927-1006; R/H; WL 208. FOUND TO HAVE 100 PERCENT MATERIAL LOSS. OUT OF LIMITS PER SRM 53-53-70-15-01-1;[02] VERIFIED CORRECTIVE ACTION STEP 1.;[03] REMOVEMar 10, 2022 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022041182383Support · corrodedCORROSION ON FLOOR SUPPORT STA 954; RBL 8; WL 208. / [01] REMOVED CORROSION ON FLOOR SUPPORT STA 954; RBL 8; WL 208. MAX MATERIAL REMOVED WAS .018' 1' BY .5' FROM .075. OUT OF LIMITS PER SRM 53-70-51-1A-1.MEASURED DEPTH WITH SPHERICAL MICROMETER ID# IS000459; Mar 10, 2022 · N468WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022041182384Floorbeam · corrodedCORROSION ON 986 FLOORBEAM UPPER FLANGE LBL 2-LBL 45; WL 208. / [01] VERIFY APPLICABILITY PER SRM 53-70-51-1A-1 ALLOWABLE DAMAGE 1;[02] EVALUATED DAMAGE ON BS986 FLOOR BEAM AND FOUND TO BE OUT LIMITS AT LBL2 WL208 1.5'X1.5' ORIG. MAT. THICKNESS IS 0.150' REMAIMar 10, 2022 · N468WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2022041182378Floorbeam · corrodedCORROSION ON 986 FLOORBEAM UPPER FLANGE RBL 4-RBL 45; WL 208. / [01] VERIFY APPLICABILITY PER SRM 53-70-51-1A-1 ALLOWABLE DAMAGE 1;[02] EVALUATED DAMAGE ON BS986 FLOOR BEAM AND FOUND TO BE OUT LIMITS AT RBL4 WL208 1.5'X1.5' ORIG. MAT. THICKNESS IS 0.150' REMAIMar 10, 2022 · N468WN · Boeing 7377H4 · Fuselage Main, Floor Beam
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