N952WN

Service difficulty reports · 222

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 = 'N952WN' 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 SWAA2024101440848Floor Panel · delaminatedCABIN FLOOR PANEL 241BF TOP SURFACE IS DELAMINATED.<[01] DUE TO EXTENT OF THE DAMAGE; FABRICATED NEW 241BF FLOOR PANEL FROM BMS4-23 TYPE 2 LOT#1553922-1; INSERTS INSTALLED USING BMS5-107 LOT#AK4BA2601A/A THEN CURED UNDER HEAT LAMP MONITORED WITH THERMOMETER ATSep 23, 2024 · N952WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024101440849Floor Panel · delaminatedCABIN FLOOR PANEL 242AF TOP SURFACE IS DELAMINATED.<[01] DUE TO EXTENT OF THE DAMAGE; FABRICATED NEW 242AF FLOOR PANEL FROM BMS4-23 TYPE 2 LOT#1553922-1; INSERTS INSTALLED USING BMS5-107 LOT#AK4BA2601A/A THEN CURED UNDER HEAT LAMP MONITORED WITH THERMOMETER ATSep 23, 2024 · N952WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024101440850Floor Panel · delaminatedCABIN FLOOR PANEL 242BF TOP SURFACE IS DELAMINATED.<[01] CABIN FLOOR PANEL 242BF WAS REPLACED BY FABRICATION IAW SRM 53-00-50-2R-0 AND DRAWING 144A5810 SHEET 122.;[02] JOB COMPLETE.Sep 23, 2024 · N952WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2024101439848Vapor Barrier · crackedR/H BS663 VAPOR BARRIER HAS A 10 INCH CRACK- FWD OF THE GROUND HYD SERVICE PUMP<[01] R/H BS663 VAPOR BARRIER HAD A 10 INCH CRACK- FWD OF THE GROUND HYD SERVICE PUMP REPAIRED IAW SRM 51-70-04-2R-10;[02] VERIFIED CORRECTIVE ACTION ITEM 1.Sep 20, 2024 · N952WN · Boeing 7377H4 · Fuselage Main, BulkheadSDR SWAA2024060597718Battery Pack · inoperativeMULTIPLE EMERGENCY LIGHTS INOP THROUGHOUT AIRCRAFT<[01] REMOVED AND REPLACED 1 FORWARD ENTRY AND 2 AFT CEILING EMERGENCY LIGHT BATTERY PACKS IN ACCORDANCE WITH AMM 33-51-06. OPS CHECK GOOD.Jun 3, 2024 · N952WN · Boeing 7377H4 · Emergency LightingSDR SWAA2022100554074Lens · missingRH EMERGENCY EXIT DOOR INTERIOR EMERGENCY EXIT LIGHT LENS MISSING / [01] INSTALLED NEW LIGHT LENS AT R/H FWD OVER WING EXIT LIGHT IAW AMM 33-51-01-960-801 VERIFIED GOOD OPS CHECK OF R/H FWD OVER WING EXIT HATCH LIGHT;[02] VERIFIED CORRECTIVE ACTIONS STEP 1.Oct 4, 2022 · N952WN · Boeing 7377H4 · Emergency LightingSDR SWAA2022100649497None · crackedELECTRICAL GROUND POWER RECEPTACLE CRACKED ON THE LOWER CUTOUT DOUBLER LIP / TRIMMED OUT DAMAGE AREA ALONG EDGE L=3.5' AND PERFORMED DVI. NO ADDITTIONAL DAMAGE NOTED PER SRM 53-10-15-2R-4 PARAGRAPH 4.; FABRICATED; LOCATED AND DRILLED REPAIR PARTS (ZONE 2) -3 FSep 30, 2022 · N952WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2022100550538Fitting · damagedFWD COIN MAT IS DAMAGED BETWEEN FSD THRESHOLD PLATE AND AFT GIRT BAR FITTING / [01] DISPLACED COIN MAT IAW 25-27-21-000-801. NOTED DAMAGE TO MOISTURE BARRIER. NOTED DAMAGE TO FLOOR BOARDS 222BF AND 222DF.;[02] REMOVED DAMAGED FWD COIN MAT IAW AMM 25-27-21-000-Sep 30, 2022 · N952WN · Boeing 7377H4 · Emergency EquipmentSDR SWAA2022100538811Scuff Plate · crackedAFT CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED / [01] WELDED CRACK ON AFT CARGO FWD CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-60-15-2R-1 PARA 4.B (2) (4)<BR>EQUIPMENT USED: WELDING MACHINE; E10583. CAL DUE 12/22;[02] VERIFIED COSep 27, 2022 · N952WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022100694387Splice Strap · corrodedAFT CARGO BAY FLOOR PANEL SPLICE STRAP IS CORRODED AT BS887 / [01] REMOVED CORROSION ON FLOOR PANEL SPLICE STRAP ACB AT BS 887 REWORKED AREA; L: 2' W: 1' D: 0.025' FOUND TO BE OUT LIMIT DUE NOT LIMIT IN SRM PART WILL BE REPAIRABLE BY REPLACEMENT; IAW SRM 51-10Sep 20, 2022 · N952WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022100694386None · crackedLT HORIZONTAL STAB FRONT SPAR UPPER SLIDE SEAL IS SRACKED. / [01] REMOVED AND REPLACED LT HORIZONTAL STAB FRONT SPAR UPPER SLIDE SEAL IAW AMM 53-31-31-000-802 AND AMM 53-31-31-400-802. OPERATED STAB FULL CYCLE NO DEFECTS NOTED. CHECKED GOOD.;[02] VERIFIED CORRSep 20, 2022 · N952WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous StructureSDR SWAA2022101052780Panel · elongatedPANEL 193D HAS ELONGATED FASTENER HOLES 'MARKED' (TRANSFERRED FROM FAULT TTG8Q009AWK9) / [01] IDENTIFIED PANEL 193D MATERIAL ACCORDING TO SRM 53-40-70-0I-1; FIG. 2; ITEM 12; TABLE 2.<BR><BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-40-70-1A-1; PARASep 13, 2022 · N952WN · Boeing 7377H4 · Aerodynamic FairingsSDR SWAA2022101052781Panel · elongatedPANEL 194E HAS ELONGATED FASTENER HOLES 'MARKED' (TRANSFERRED FROM FAULT TTG8Q009AWK9) / [01] IDENTIFIED PANEL 194E MATERIAL ACCORDING TO SRM 53-60-70-0I-4; FIG. 2; ITEM 8; TABLE 2. <BR><BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-60-70-1A-1; PARASep 13, 2022 · N952WN · Boeing 7377H4 · Aerodynamic FairingsSDR SWAA2022100545374Floor Panel · pulledFLOOR PANEL 242HF HAS PULLED INSERT LOCATED AT O.B EDGE. (MARKED) / [01] DAMAGE TO PANEL 242GF IS OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.E AND NEW PANEL WILL BE FABRICATED FROM NEW STOCK.<BR><BR>ROUGH CUT NEW FLOOR PANEL IAW SRM 53-00-50-2R-0 ANDSep 7, 2022 · N952WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022100550717Floor Panel · pulledFLOOR PANEL 242HF HAS PULLED INSERT LOCATED AT O.B EDGE. (MARKED) / [01] DAMAGE TO PANEL 242GF IS OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PARA 4.E AND NEW PANEL WILL BE FABRICATED FROM NEW STOCK.<BR><BR>ROUGH CUT NEW FLOOR PANEL IAW SRM 53-00-50-2R-0 ANDSep 7, 2022 · N952WN · Boeing 7377H4 · Fuselage Floor PanelSDR SWAA2022101050434None · bulgedL/W I/B AFT FLAP HAS A BULGE ON THE UPPER SURFACE SKIN 23.5' FROM I/B END; 1.5' FROM T/E / REMOVED AREA OF UPPER SURFACE SKIN AND FULL DEPTH HONEYCOMB CORE FABRICATED REPLACEMENT CORE SECTION FROM BMS 4-4; TY 4-25; NPA HONEYCOMB CORE (LOT# 1095039); SOLVENT CLSep 5, 2022 · N952WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2022101045356None · bulgedL/W I/B AFT FLAP HAS A BULGE ON THE UPPER SURFACE SKIN 23.5' FROM I/B END; 1.5' FROM T/E / [01] IDENTIFIED FLAP T/E WEDGE MATERIAL IAW SRM 57-53-01-0I-2; FIG. 2; ITEMS 1; 3; AND 4; AND TABLE 2. <BR><BR>FOUND DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW SRM 57-53-0Sep 5, 2022 · N952WN · Boeing 7377H4 · Trailing Edge FlapsSDR SWAA2022100645341None · crackedCRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS535 S-26L WL153. MARKED / [01] VERIFIED THE APPLICABILITY OF SRM 53-00-03-2R-1 REPAIR 1;[02] CUT AND REMOVED THE DAMAGED PART OF STRINGER 26L BETWEEN BS 500D +11 TO BS 540 IAW SRM 53-00-03-2R-1 REPAIR 1 . AND UPDSep 3, 2022 · N952WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2022100645342None · crackedCRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS535 S-26R WL153. MARKED / CUT AND REMOVED THE DAMAGED PART OF STRINGER 26R BETWEEN BS 500D+11' AND BS 540. AND UPDATED STEPS 2 AND 3 RECEIVED NEW REPLACEMENT STRINGER SECTION FROM O.S.S AFTER BEING FORMED AND FABSep 3, 2022 · N952WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2022100649921None · crackedCRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS535 S-26L WL153. MARKED / [01] VERIFIED THE APPLICABILITY OF SRM 53-00-03-2R-1 REPAIR 1;[02] CUT AND REMOVED THE DAMAGED PART OF STRINGER 26L BETWEEN BS 500D +11 TO BS 540 IAW SRM 53-00-03-2R-1 REPAIR 1 . AND UPDSep 3, 2022 · N952WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2022100649922None · crackedCRACKED STRINGER AT AREA AFT OF FWD CARGO BAY BS535 S-26R WL153. MARKED / CUT AND REMOVED THE DAMAGED PART OF STRINGER 26R BETWEEN BS 500D+11' AND BS 540. AND UPDATED STEPS 2 AND 3; RECEIVED NEW REPLACEMENT STRINGER SECTION FROM O.S.S AFTER BEING FORMED AND FASep 3, 2022 · N952WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2022101049660Stub Frame · crackedFWD CABIN SERVICE DOOR SURROUND LOWER STUB FRAME CRACKED BS294 RBL55 WL209. / [01] CRACKED ON FWD CABIN SERVICE DOOR SURROUND LOWER STUB FRAME BS294 RBL55 WL209 P/N 141A8370-12 ; WITH NEXT DIMENSION L=1.100' ; TOOL USED CALIPER ID:ATS2738 ;S/N:A22004095;DATE:0Sep 2, 2022 · N952WN · Boeing 7377H4 · Fuselage Main, FrameSDR SWAA2022100649664Stringer Clip · crackedCRACKED STRINGER CLIP AT PASSENGER CABIN BS360 S-4R. MARKED. / [01] REMOVED STRINGER CLIP AT PASSENGER CABIN BS360 S-4R PER REF SRM 51-40-02;[02] FABRICATED AND DRILLED NEW STRINGER CLIP AT PASSENGER CABIN P/N 141A1250-23 BS360 S-4R WITH NEXT MATERIAL BAC1493-Sep 2, 2022 · N952WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2022100645335Stringer Clip · crackedCRACKED STRINGER CLIP AT PASSENGER CABIN BS807 S-3R. MARKED. / [01] REMOVED STRINGER CLIP AT PASSENGER CABIN BS807 S-3R I.A.W SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW STRINGER CLIP AT PASSENGER CABIN BS807 S-3R PER REF SRM 51-40-05<BR><BR>OK TO INSTALL;Sep 2, 2022 · N952WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2022100649666Stringer Clip · crackedCRACKED STRINGER CLIP AT PASSENGER CABIN BS807 S-3R. MARKED. / [01] REMOVED STRINGER CLIP AT PASSENGER CABIN BS807 S-3R I.A.W SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW STRINGER CLIP AT PASSENGER CABIN BS807 S-3R PER REF SRM 51-40-05<BR><BR>OK TO INSTALL;Sep 2, 2022 · N952WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2022100545333Attach Angle · crackedFWD PASSENGER CABIN ATTACH ANGLE IS CRACKED BS293 RBL55 WL208. / [01] CRACKED ON FWD PASSENGER CABIN ATTACH ANGLE BS293 RBL55 WL208 WITH NEXT DIMENSIONS L=1.263' NEXT TOOL USED CALIPER ID:ATS2738;S/N:A22004095;DATE:04/2022;DUE:04/2023 FOUND TO BE OUT OF LIMITSSep 2, 2022 · N952WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2022100549662Door Frame · crackedPASSENGER CABIN FWD ENTRY DOOR STOP FITTING WEB CRACKED BS295 S-16L. MARKED. / [01] HFEC INSPECTED SUSPECTED CRACKED AREA IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23.<BR>CRACK WAS NOTED IN AREA MARKED.<BR>EQUIP USED:<BR>-NORTEC 600 ID: ATS2353 CAL DUE: 01/23;[02Sep 2, 2022 · N952WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2022100549661Attach Angle · crackedFWD PASSENGER CABIN ATTACH ANGLE IS CRACKED BS293 RBL55 WL208. / [01] CRACKED ON FWD PASSENGER CABIN ATTACH ANGLE BS293 RBL55 WL208 WITH NEXT DIMENSIONS L=1.263' NEXT TOOL USED CALIPER ID:ATS2738;S/N:A22004095;DATE:04/2022;DUE:04/2023 FOUND TO BE OUT OF LIMITSSep 2, 2022 · N952WN · Boeing 7377H4 · Fuselage Main, Attach FittingsSDR SWAA2022100545336Floor Support · crackedCRACKED INTERCOSTAL AT PASSENGER CABIN BS500D+3 BL0. CRACKED ON INTERCOSTAL AT PASSENGER CABIN BS500D+3 BL0 WL208 WITH NEXT DIMENSIONS L=0.320' . FOUND TO BE OUT OF LIMITS I.A.W SRM 53-30-51-1A-1 IT WILL BE REPAIRABLE BY REPLACEMENT I.A.W SRM 51-10-02-0G PARSep 2, 2022 · N952WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022100545337Intercostal · crackedCRACKED INTERCOSTAL AT PASSENGER CABIN BS380+14 BL0 WL208. / [01] REQUIRE NDI TO VERIFY FOR CRACK;[02] HFEC INSPECTED SUSPECTED CRACKED AREA IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23.<BR>CRACKS NOTED TO BE .4' AT AREA MARKED.<BR>EQUIP USED:<BR>-NORTEC 600 ID: Sep 2, 2022 · N952WN · Boeing 7377H4 · Fuselage Internal Mounting StructureSDR SWAA2022100545338Intercostal · crackedCRACKED INTERCOSTAL AT PASSENGER CABIN BS380+14 RBL9 WL208. / [01] REQUIRE NDI TO VERIFY FOR CRACK;[02] HFEC INSPECTED SUSPECTED CRACKED AREA IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23.<BR>CRACK NOTED TO BE .3' AT AREA MARKED.<BR>EQUIP USED:<BR>-NORTEC 600 ID: Sep 2, 2022 · N952WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022100545339Intercostal · crackedCRACKED INTERCOSTAL AT PASSENGER CABIN BS380+14 LBL13 WL208. / [01] REQUIRE NDI TO VERIFY FOR CRACK;[02] HFEC INSPECTED SUSPECTED CRACKED AREA IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23.<BR>CRACK NOTED TO BE .2' AT AREA MARKED.<BR>EQUIP USED:<BR>-NORTEC 600 ID:Sep 2, 2022 · N952WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022100549668Intercostal · crackedCRACKED INTERCOSTAL AT PASSENGER CABIN BS380+14 BL0 WL208. / [01] REQUIRE NDI TO VERIFY FOR CRACK;[02] HFEC INSPECTED SUSPECTED CRACKED AREA IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23.<BR>CRACKS NOTED TO BE .4' AT AREA MARKED.<BR>EQUIP USED:<BR>-NORTEC 600 ID: Sep 2, 2022 · N952WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022100549669Intercostal · crackedCRACKED INTERCOSTAL AT PASSENGER CABIN BS380+14 RBL9 WL208. / [01] REQUIRE NDI TO VERIFY FOR CRACK;[02] HFEC INSPECTED SUSPECTED CRACKED AREA IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23.<BR>CRACK NOTED TO BE .3' AT AREA MARKED.<BR>EQUIP USED:<BR>-NORTEC 600 ID: Sep 2, 2022 · N952WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022100549670Intercostal · crackedCRACKED INTERCOSTAL AT PASSENGER CABIN BS380+14 LBL13 WL208. / [01] REQUIRE NDI TO VERIFY FOR CRACK;[02] HFEC INSPECTED SUSPECTED CRACKED AREA IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23.<BR>CRACK NOTED TO BE .2' AT AREA MARKED.<BR>EQUIP USED:<BR>-NORTEC 600 ID:Sep 2, 2022 · N952WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022100549667Intercostal · crackedCRACKED INTERCOSTAL AT PASSENGER CABIN BS500D+3 BL0. / [01] CRACKED ON INTERCOSTAL AT PASSENGER CABIN BS500D+3 BL0 WL208 WITH NEXT DIMENSIONS L=0.320' NEXT TOOL USED CALIPER ID:ATS2738;S/N:A22004095;DATE:04/2022;DUE:04/2023 FOUND TO BE OUT OF LIMITS I.A.W SRM Sep 2, 2022 · N952WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022101045295Support Angle · corrodedCORROSION ON FCB AFT BULKHEAD TO FLOOR SUPPORT ANGLE BS500D LBL23 - RBL20. / [01] VERIFIED APPLICABILITY SRM 53-30-08-01-1 FOR IDENTIFICATION AND SRM 53-30-08-1A-1 FOR ALLOWABLE DAMAGE.<BR><BR>REMOVED CORROSION ON FCB AFT BULKHEAD TO FLOOR SUPPORT ANGLE BS500DSep 1, 2022 · N952WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022101049099Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS500+10 - BS500B LBL23. / [01] REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT CARGO BAY BS 500+10 AND BS 500B LBL32 AT DISCREPANCY AREA BS.500+10 L=1.500' W=0.700' D=0.011 ORIGINAL THICKNESS 0.040 REMSep 1, 2022 · N952WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022101045305Web · corrodedCORROSION ON SUBTHRESHOLD WEB AT FWD CARGO BAY BS448- BS490 RBL24. / [01] VERIFIED APLICABILITY SRM 51-30-15-01-1 FOR IDENTIFICATION<BR>AND SRM 53-30-15-1A-1 FOR ALLOWABLE DAMAGE;[02] REMOVED CORROSION ON SUBTHRESHOLD WEB AT FCB BS460+5 RBL 24 IAW. SRM 51-10-0Sep 1, 2022 · N952WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2022101045315None · corrodedCORROSION ON BS986 FLOOR BEAM AT LBL42. / [01] CORROSION ON BS 986 FLOOR BEAM AT LBL 42 FOUND 100% OUT OF LIMITS DUE TO NO SRM ALLOWABLE DAMAGE ON THE PREVIOUS REPAIR. THE STRUCTURAL ITEM WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02 PAR 9C;13] FABRICATED -Sep 1, 2022 · N952WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2022101049114Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS727B - BS807 LBL20. / [01] VERIFIED APPLICABILITY SRM 53-60-53-01-2 FOR IDENTIFICATION<BR>AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE.<BR><BR>REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BSep 1, 2022 · N952WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022101049112None · corrodedCORROSION ON BS986 FLOOR BEAM AT LBL42. / [01] CORROSION ON BS 986 FLOOR BEAM AT LBL 42 FOUND 100% OUT OF LIMITS DUE TO NO SRM ALLOWABLE DAMAGE ON THE PREVIOUS REPAIR. THE STRUCTURAL ITEM WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02 PAR 9C12] INSPECTED ACTSep 1, 2022 · N952WN · Boeing 7377H4 · Fuselage Main, Floor BeamSDR SWAA2022100645294Attach Angle · crackedCRACKED INTERCOSTAL ATTACH ANGLE AT FCB BS500B LBL25. MARKED. / [01] PRIOR TO REMOVAL;FOUND PART TO HAVE NO SRM LIMITS AND SO PART IS REPAIRABLE BY REPLACEMENT;PER SRM 51-10-02-OG-0 STEP #9.;[02] REMOVED CRACKED ANGLE AT FWD CARGO BAY BS500B FWD SIDE LBL 25;IASep 1, 2022 · N952WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2022100645297Gusset · crackedFWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19L WL193. MARKED / [01] NO FOUND ALLOWABLE DAMAGE LIMITS ON SRM FOR THIS PART MUST BE REPLACED IAW SRM 51-10-02 PARAGRAPH 9;[02] REMOVED FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET AT BS 500D S-19L WSep 1, 2022 · N952WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2022100645307Gusset · crackedFWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19R WL193. MARKED / [01] NO FOUND ALLOWABLE DAMAGE LIMITS ON SRM FOR THIS PART MUST BE REPLACED IAW SRM 51-10-02 PARAGRAPH 9;[02] REMOVED FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET AT BS 500D S-19R WSep 1, 2022 · N952WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2022100649083Attach Angle · crackedCRACKED INTERCOSTAL ATTACH ANGLE AT FCB BS500B LBL25. MARKED. / [01] PRIOR TO REMOVAL;FOUND PART TO HAVE NO SRM LIMITS AND SO PART IS REPAIRABLE BY REPLACEMENT;PER SRM 51-10-02-OG-0 STEP #9.;[02] REMOVED CRACKED ANGLE AT FWD CARGO BAY BS500B FWD SIDE LBL 25;IASep 1, 2022 · N952WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2022100649086Gusset · crackedFWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19L WL193. MARKED / [01] NO FOUND ALLOWABLE DAMAGE LIMITS ON SRM FOR THIS PART MUST BE REPLACED IAW SRM 51-10-02 PARAGRAPH 9;[02] REMOVED FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET AT BS 500D S-19L WSep 1, 2022 · N952WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2022100649101Gusset · crackedFWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19R WL193. MARKED / [01] NO FOUND ALLOWABLE DAMAGE LIMITS ON SRM FOR THIS PART MUST BE REPLACED IAW SRM 51-10-02 PARAGRAPH 9;[02] REMOVED FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET AT BS 500D S-19R WSep 1, 2022 · N952WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2022100649115Track · crackedCRACKED TRACK AT AFT CARGO BAY BS767 RBL13. / FOUND TO BE OUT OF LIMITS I.A.W SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE AND SRM 53-60-53-0L-2 FOR IDENTIFICATION; IT WILL BE REPAIRABLE BY REPLACEMENT I.A.W SRM 51-10-02-0G PAR 9C .;[02] REMOVED TRACK AT AFT CARGO BSep 1, 2022 · N952WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022100645326Sidewall Support · crackedAFT CARGO BAY FLOOR TO SIDEWALL SUPPORT HAS CRACK BS927+13 RBL20. / [01] VERIFIED SRM 53-00-53-1A-2 IS APPLICABLE FOR REPAIR.<BR><BR>SIDEWALL SUPPORT AT BS887 TO BS947 RH;FOUND TO BE OUT LIMITS FOR CRACK;IAW SRM 53-00-53-1A-2;PARAG. 4(1) DETAIL C;D FIG.103.IDESep 1, 2022 · N952WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
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