N234WN

Service difficulty reports · 288

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 = 'N234WN' 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 SWAA2023110703295Access Panel · delaminatedRIGHT WING LOWER LEADING EDGE ACCESS PANEL 621UB DELAMINATED AT FLANGE TIP.<[01] REPAIRED RIGHT WING LOWER LEADING-EDGE ACCESS PANEL 621UB AS PER SRM 51-70-04-2R-13-A00757 MATERIAL USED PO.1791128 AND PO.1473815. PAINTED PANEL #621UB PER B737 AMM 51-21-99-300-Sep 22, 2023 · N234WN · Boeing 7377H4 · Wing, Plate/SkinSDR SWAA2023110703449Door · out of adjustL1 DOOR REQUIRES ADJUSTMENT<[01] ACCOMPLISHED ADJUSTMENT OF L1 DOOR AS PER AMM 52-11-00-820-801; LINER INSTALLATION WILL BE ACCOMPLISHED ON TTG8Q00NL1PQ TOOLING USED: CALIPER: B/C: 175909 DUE 25-MAY-24; SLIDE SIM.: B/C: 174714 NO CALIBRATION DUE DATE;[02] VERISep 22, 2023 · N234WN · Boeing 7377H4 · Passenger/Crew DoorsSDR SWAA2023110703446Bracket · elongatedFLIGHT DECK ENTRY DOOR R/H POST UPPER BRACKET HAS ELONGATED HOLES.<[01] REMOVED AND INSTALLED NEW BRACKET PART#141A9402U6 PO#2028887 AT FLIGHT DECK ENTRY DOOR RH POST UPPER AS PER SRM 51-40-02-0G-0 AND DWG# 141A9402.;[02] VERIFIED STEP:1 INSTALLATION NEW BRACKSep 22, 2023 · N234WN · Boeing 7377H4 · Fixed Inner DoorsSDR SWAA2023110703447Strap · out of limitsAFT WET AREA STA.1006 LBL 3 STRAP CORRODED.<[01] REMOVED CORROSION ON CORRODED STRAP AND WAS FOUND OUT OF LIMITS; LOCATED AND DRILLED NEW PART REPLACEMENT HOLES; AND INSTALLED PART 100% COMPLETED PER REF ATTACHED ON PREVIOUS STEPS SRM 51-40-02-0G-0.;[02] VERIFSep 22, 2023 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2023110704637Skin · crackedEXT PWR RECEPTACLE LWR SKIN CRACKED<[01] ACCOMPLISHED REPAIR AT EXT PWR RECEPTACLE LWR SKIN AS PER SRM 53-10-15-2R-4.;[02] VERIFIED REPAIR ACCOMPLISHED.Sep 19, 2023 · N234WN · Boeing 7377H4 · Fuselage Main, Plate/SkinSDR SWAA2023110701991Skin · crackedCRACK FOUND AT RH HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 193.90; 16.5' FROM FRONT SPAR ; I/B ROW. CRACK LENGTH : 0.593' CRACK FOUND AT RH HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 193.90 16.5' FROM FRONT SPAR I/B ROW. CRACK LENGTH : 0.593'<[01] ACOMPLSep 19, 2023 · N234WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/SkinSDR SWAA2023110701992Skin · crackedCRACK FOUND AT LH HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 193.90 ; 17.25' FROM FRONT SPAR ; I/B ROW. CRACK LENGTH : 0.468' CRACK FOUND AT LH HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 193.90 17.25' FROM FRONT SPAR I/B ROW. CRACK LENGTH : 0.468'<[01] ACCSep 19, 2023 · N234WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/SkinSDR SWAA2023011791173Attach Bracket · damagedRT WING /L/E AT FSS150 DUCT BRAKET ATTACH HOLES ELONGATED<[01] REMOVED AND REPLACED BRACKET PER SOPM 20-50-01;[02] REMOVED AND REPLACED BRACKET PER SOPM 20-50-01Jan 13, 2023 · N234WN · Boeing 7377H4 · Wing, Attach FittingsSDR SWAA2022060916040Panel · elongatedPANEL 193B HAS NUMEROUS ELONGATED FASTENER HOLES / [01] REPLACED PANEL 193B PER SRM 51-40-02Jun 8, 2022 · N234WN · Boeing 7377H4 · Aerodynamic FairingsSDR SWAA2021123055529None · looseSUPPLEMENTAL INFORMATION: FWD ENTRY DOOR ASSIST HANDLE COMMON TO HINGES IS LOOSE. ; / [01] REMOVED FWD ENTRY DOOR LINER FOR ACCESS PER AMM 52-11-31-000-802; [02] TIGHTEN FWD UPPER ASSIST HANDLE BRACKET PER SOPM 20-50-01. OK TO CLOSE FED LINER; [03] VERIFIED CODec 22, 2021 · N234WN · Boeing 737 · Service DoorsSDR SWAA2022010452301Angle · crackedCRACKEDLOWER ATTACH ANGLE ON CABLE GUARD INTERCOSTAL STA 694 AT LBL 1; WL 204.(MARKED) ; / [01] DISPLACED CABLE GUARD PULLEY BRACKET INTERCOSTAL STA 694 BLO-LBL 25; WL 204-208 FOR ACCESS PER SRM 51-40-02-0G-0; SOPM 20-50-01.[10] INSTALLED NEW LOWER ATTACH ANGLDec 13, 2021 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022010451827Angle · crackedPANEL 323AL SKATE ANGLE CLIP IS CRACKED / [01] UPDATED MEASUREMENTS; [02] REMOVED AND REPLACED PANEL 323AL SKATE ANGLE CLIP IAW SRM 51-40-02-01-0G AND BAC DWG 172A6122; [03] VERIFIED CORRECTIVE ACTIONS STEP 2.Dec 10, 2021 · N234WN · Boeing 7377H4 · Vertical StabilizerSDR SWAA2022010450062Structure · corrodedSUPPLEMENTAL INFORMATION: CORRSION AFT OF AFT CARGO BAY DRAIN MAST BS 986.5+9 LBL 19 ; / [01] EVALUATED CORROSION ON AFT GREY WATER DRAIN MAST SUPPORT STRUCTURE AND FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02Dec 3, 2021 · N234WN · Boeing 737 · Fuselage Miscellaneous StructureSDR SWAA2021123050057Stringer · crackedSUPPLEMENTAL INFORMATION: CRACKED STRINGER AT AREA AFT OF FCB BS540 S-25R WL157. MARKED ; / [01] UPDATED STEPS 1& 2.; [02] VERIFIED CORRECTIVE ACTIONS 1 AND 2.; [03] RECEIVED STRINGER REPAIR SECTION; FOR STR 25R; APPROXIMATELY BS500D+10 - 540; PER P.O.#848376.Dec 3, 2021 · N234WN · Boeing 737 · Fuselage Main, Longeron/StringerSDR SWAA2021123050044Attach Angle · crackedSUPPLEMENTAL INFORMATION: FWD CARGO BAY INTERCOASTAL ATTACH ANGLE CRACKED BS 440 LBL 25 WL 156 ; / [01] EVALUATED INTERCOSTAL ATTACH ANGLE; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED EVALDec 3, 2021 · N234WN · Boeing 737 · Fuselage Miscellaneous StructureSDR SWAA2021123050040Attach Angle · crackedSUPPLEMENTAL INFORMATION: FWD CARGO BAY INTERCOASTAL ATTACH ANGLE CRACKED BS 500C LBL 25 WL 156 ; / [01] EVALUATED INTERCOSTAL ATTACH ANGLE; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED EVADec 3, 2021 · N234WN · Boeing 737 · Fuselage Miscellaneous StructureSDR SWAA2021123050039Gusset · crackedSUPPLEMENTAL INFORMATION: FWD CARGO BAY INTERCOASTAL ATTACH ANGLE CRACKED BS 400 LBL 25 WL 156 ; / [01] EVALUATED INTERCOSTAL ATTACH ANGLE; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED EVALDec 3, 2021 · N234WN · Boeing 737 · Fuselage Miscellaneous StructureSDR SWAA2022010449935Angle · crackedSUPPLEMENTAL INFORMATION: L/H BS663 VAPOR BARRIER UPPER ATTACH ANGLE CRACKED AT LBL8 WL167.68 ; / [01] UPDATED MEASUREMENT TABLE; [02] VALIDATED SRM 57-10-10-2R-5 REPAIR 5 TO BE CORRECT [05] CONFORMED-1 REPLACEMENT ANGLE AND -2 SPLICE ANGLE PER SRM 57-10-102R-Dec 3, 2021 · N234WN · Boeing 737 · Wing Main, Frame StructureSDR SWAA2021123049689Gusset · crackedSUPPLEMENTAL INFORMATION: FWD CARGO BAY GUSSET IS CRACKED AT BS500D COMMON TO STR 21R ; / [01] EVALUATED GUSSET; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED EVALUATED GUSSET; FOUND TO BE ODec 3, 2021 · N234WN · Boeing 737 · Fuselage Main, Plate/SkinSDR SWAA2021123049687Gusset · crackedSUPPLEMENTAL INFORMATION: FWD CARGO BAY GUSSET IS CRACKED AT BS 500D COMMON TO STR 23L ; / [01] CORRECT LOCATION OF CRACKED GUSSET IS BS 500D STRINGER 19 L/H; [02] EVALUATED GUSSET; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENTDec 3, 2021 · N234WN · Boeing 737 · Fuselage Main, Plate/SkinSDR SWAA2021123049686Gusset · crackedSUPPLEMENTAL INFORMATION: FWD CARGO BAY GUSSET IS CRACKED AT BS 500D COMMON TO STR 19R ; / [01] EVALUATED GUSSET; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED EVALUATED GUSSET; FOUND TO BE Dec 3, 2021 · N234WN · Boeing 737 · Fuselage Main, Plate/SkinSDR SWAA2021123050059Stringer · corrodedSUPPLEMENTAL INFORMATION: CRACKED STRINGER AT AREA AFT OF FCB BS540 S-23R WL164. MARKED ; / [01] UPDATED PARTIAL WORKS IN STEPS 1 & 2.; [02] UPDATED STEPS 1 AND 2.; [03] COMPLETED STEPS 1 AND 2; [04] COMPLETE; [05] THE DAMAGE WAS REPAIRED PER 737-700 SRM 53-00Dec 3, 2021 · N234WN · Boeing 737 · Fuselage Main, Longeron/StringerSDR SWAA2022010450055Support · corrodedCORROSION; AFT CARGO FLOOR TO SIDEWALL SUPPORT; BS 727A TO BS 727E + 10 REPAIR SPLICE; LBL 21 ; / [01] EVALUATED CORROSION ON ALL LOCATION OF FLOOR TO SIDEWALL SUPPORT; FOUND DEEPEST LOCATION TO BE 727E+10 LBL 21 WL 156; FOUND 0.015 REMOVED FROM ORIG 0.040 IN Dec 3, 2021 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022010450047Support · corrodedCORRSION FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT BS 500B+2; +10; +15; BS 500C+6; +10; +14 RBL 24 ; / [01] EVALUATED CORROSION AT ALL LOCATION; FOUND DEEPEST LOCATION TO BE AT BS 500B+2 RBL 24 WL 156. FOUND 0.015 REMOVED FROM ORIG 0.040 IN 1'X1' AREAS. FOUND TODec 3, 2021 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022010450041Support · corrodedCORRSION FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT BS 440+17; BS 460+7; BS 480+3;+12; BS 500+9; +14; BS 500A+10; BS 500B+14;+18 LBL 24 ; / [01] EVALUATED CORROSION AT ALL LOCATION; FOUND DEEPEST LOCATION TO BE AT BS 440+17 LBL 24 WL 156. FOUND 0.015 REMOVED FROMDec 3, 2021 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022010450053Intercostal · corrodedCORROSION; AFT CARGO DOORWAY SUB THRESHOLD IB INTERCOSTAL UPPER FLANGE; BS 794.5 + 1 TO BS 840; RBL 19 ; / [01] EVALUATED CORROSION AT ALL LOCATIONS ON AFT CARGO BAY VERTICAL WEB UPPER FLANGE; FOUND DEEPEST LOCATION TO BE AT BS 794.5+1 RBL 19 WL 156 IN 1'X1' ADec 3, 2021 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022010450066Support Angle · corrodedCORROSION; AFT CARGO FLOOR PANEL SUPPORT T-ANGLE UPPER FLANGE; BS 794.5; RBL 18. FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT IAW SRM 51-10-02-0G-0. REMOVED FLOOR PANEL SUPPORT T-ANGLE IAW SRM 51-40-02-0G-0. LOCATED AND DDec 3, 2021 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022010450052Retainer · corrodedCORROSION; AFT CARGO DOORWAY SUB THRESHOLD IB CHORD LWR NUTPLATE RETAINER STRIP BS 847 + 4; RBL 18. FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT IAW SRM 51-10-02-0G-0. REMOVED SUB THRESHOLD IB LOWER NUTPLATE RETAINER STRIP Dec 3, 2021 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022010450050Retainer · corrodedCORROSION; AFT CARGO DOORWAY SUB THRESHOLD IB CHORD; LWR NUTPLATE RETAINER STRIP BS 794.5 + 1 RBL 19. EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT IAW SRM 51-10-02-0G-0. REMOVED SUB THRESHOLD IB CHORD; LDec 3, 2021 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022010450049Web · corrodedCORROSION; AFT CARGO DOORWAY SUB THRESHOLD WEB UPPER SURFACE; BS 794.5 + 3 TO BS 827 + 17; RBL 23 TO RBL 27 ; / [01] EVALUATED CORROSION ON SUBTHRESHOLD WEB BS 794.5+3 TO 827+17 RBL 23-27; FOUND 0.015 REMOVED FROM ORIG 0.045 FOUND TO BE OUT OF LIMITS PER SRM 5Dec 3, 2021 · N234WN · Boeing 7377H4 · Fuselage Main, StructureSDR SWAA2022010450042Shield · corrodedCORRSION FWD CARGO BAY AFT SHIELD BS 500+6; +14 RBL 24 ; / [01] EVALUATED SHIELD; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED EVALUATED SHIELD; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IDec 3, 2021 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022010450067Strip · corrodedCORROSION; AFT CARGO FLOOR PANEL SPLICE STRIP; BS 767 + 4; RBL 18 TO LBL 18 ; / [01] EVALUATED CORROSION ON SPLICE STRIP; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED CORRECTIVE ACTIONS STEDec 3, 2021 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022010450043Web · corrodedCORRSION FWD CARGO BAY THRESHOLD SUBWEB BS 440+10-BS 500 RBL 29 ; / [01] EVALUATED CORROSION AT ALL LOCATIONS; FOUND DEEPEST LOCATION TO BE AT BS 440+10 RBL 29 WL 156. FOUND 0.015 REMOVED FROM ORIG 0.045 IN 1'X1' AREAS FOUND TO BE OUT OF LIMITS PER SRM 53-30-1Dec 3, 2021 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022010450063Shield · corrodedCORROSION; AFT CARGO FLOOR TO SIDEWALL SUPPORT SHIELD; BS 767 + 3 TO BS 767 + 12; RBL 21 ; / [01] EVALUATED CORROSION ON SHIELD; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; [02] VERIFIED CORRECTIVE ACTIDec 3, 2021 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022010450054Support · corrodedCORROSION; AFT CARGO FLOOR TO SIDEWALL SUPPORT; BS 727A TO BS 767 RBL 21 ; / [01] EVALUATED CORROSION ON FLOOR TO SIDEWALL SUPPORT FROM 727A-767 RBL 21 WL 156; FOUND DEEPEST MATERIAL REMOVED OF 0.015 FROM ORIG 0.040 FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1Dec 3, 2021 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022010450065Shield · corrodedCORROSION; 2 EA FASTENERS ON AFT CARGO FLOOR TO SIDEWALL SUPPORT SHIELD; BS 787; RBL 25 AND RBL 26 ; / [01] NO ALLOWABLE LIMITS IN THE SRM FOR CORROSION ON FASTENERS. THE FASTENERS ARE COMMON TO SHIELD BS 767-792 RBL 25 WL 157 AND IS OUT OF LIMITS AND TO BE REDec 3, 2021 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022010450058Support · corrodedCORROSION; AFT CARGO FLOOR TO SIDEWALL SUPPORT; BS 787 + 9; LBL 21 ; / [01] EVALUATED CORROSION ON FLOOR TO SIDEWALL SUPPORT; AT BS 787+9 LBL 21 WL 156; 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 USING DEDec 3, 2021 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022010450056Support · corrodedCORROSION; AFT CARGO FLOOR TO SIDEWALL SUPPORT; BS 787 + 6; LBL 21 ; / [01] EVALUATED CORROSION ON FLOOR TO SIDEWALL SUPPORT; AT BS 787+6 LBL 21 WL 156; 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 USING DEDec 3, 2021 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022010450064Intercostal · corrodedCORROSION; AFT CARGO FLOOR TO SIDEWALL SUPPORT INTERCOSTAL; BS 747 TO BS 767; RBL 21 ; / [01] EVALUATED CORROSION ON INTERCOSTAL; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G-0; INTERCOSTAL WILL BE REPLACEDDec 3, 2021 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2021123050060Stringer · crackedCRACKED STRINGER 26R, BS 540. REMOVED DAMAGED SECTION AND PERFORMED VISUAL INSPECTION IAW SRM 53-00-03-2R-1 REP 1, STEPS 4 A-B. ACCOMPLISHED HFEC INSPECTION OF CUTOUT EDGE, NO CRACK NOTED IAW NDTM PART 6, 51-00-00, PROCEDURE 23. EVALUATED CRACK AND FOUNDec 3, 2021 · N234WN · Boeing 7377H4 · Fuselage Main, Longeron/StringerSDR SWAA2022010349540None · corrodedSUPPLEMENTAL INFORMATION: CORROSION ON LATERAL BEAM AT FLIGHT DECK BS270 LBL10 TO RBL9 WL207.5. MARKED. ; / [01] REMOVED CORROSION ON LATERAL BEAM BS270 LBL10-RBL10 WL207.5 20'X1' AREA I.A.W SRM 53-10-51-1A-1 ALLOWABLE DAMAGE 1 PAR 4.C(2)(A) FIG 105/ALLOWABLE Dec 2, 2021 · N234WN · Boeing 737 · Fuselage Main, Floor BeamSDR SWAA2021123049319None · crackedSUPPLEMENTAL INFORMATION: CRACK IN HORIZONTAL PRESSURE DECK BS 672; RBL 41; WL 202. 1.3' LONG CRACK. MARKED IN BLACK INK. ; / [01] REMOVED FASTENER FROM THE DAMAGED WEB BS663-BS674 RBL32-RBL60 WL202 I.A.W SRM 53-40-51-SR-2 REPAIR 2 PAR 4(C)(2); [02] REMOVED DADec 2, 2021 · N234WN · Boeing 737 · Fuselage Main, StructureSDR SWAA2021123049584None · looseSUPPLEMENTAL INFORMATION: FWD ENTRY DOOR SLIDE COVER AFT GIRT BAR STORAGE CLIP IS LOOSE. ; / [01] REMOVED AND REPLACED FASTENER ON FWD ENTRY DOOR SLIDE COVER AFT GIRT BAR STORAGE CLIP PER SRM 51-40-02-0G-0; [02] VERIFIED REMOVED AND REPLACED FASTENER ON FWD ENDec 2, 2021 · N234WN · Boeing 737 · Escape SlideSDR SWAA2021123049530Scuff Plate · brokenSUPPLEMENTAL INFORMATION: AFT CARGO BAY AFT CORNER SCUFF PLATE IS BROKEN ; / [01] WELDED CRACK ON RADIUS OF ACB; AFT CORNER SCUFF PLATE USING ER4043 ALUMINUM FILLER ROD LOT # 1131216 PER SRM 53-60-15-2R-1 PARA 4.B. (2) AND (4)<BR>WELDING MACHINE CALIBRATION IDDec 2, 2021 · N234WN · Boeing 737 · Fuselage Miscellaneous StructureSDR SWAA2022010449673Intercostal · crackedCRACKED LOWER ATTACH ANGLE ON CABLE GUARD INTERCOSTAL BS 694 AT RBL 1; WL 204. REMOVED LOWER ATTACH ANGLE IAW SRAM 51-40-02-0G-0. INSTALLED NEW LOWER ATTACH ANGLE IAW SRM 51-40-02-0G-0; DWG 273A9110; REV A. INSTALLED INTERCOSTAL IAW SRM 51-40-02-0G-0; DWG 27Dec 2, 2021 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022010449674Intercostal · crackedCRACKED LOWER ATTACH ANGLE ON CABLE GUARD INTERCOSTAL STA 694 AT RBL 24; WL 204. (MARKED). ; / [01] REMOVED LOWER ATTACH ANGLE ON CABLE GUARD INTERCOSTAL STA 694 AT RBL 24 WL204 PER SRM 51-40-02-0G-0; [12] INSTALLED NEW LOWER ATTACH ANGLE ON CABLE GUARD INTERCDec 2, 2021 · N234WN · Boeing 7377H4 · Fuselage Miscellaneous StructureSDR SWAA2022010349528Beam · corrodedCORROSION ON LATERAL BEAM AT FLIGHT DECK BS259.5 LBL7 TO RBL8 WL207.5. MARKED. ; / [01] REMOVED CORROSION ON AFT FLANGE OF LATERAL BEAM BS259.5 WL207.5 LBL9 TO RBL9 IN AN AREA OF 1.2'X 18 IAW SRM 51-10-02-0G-0; [02] REQUEST HFEC ALL OPEN HOLES AND COUNTERSINK Dec 2, 2021 · N234WN · Boeing · Fuselage Main, StructureSDR SWAA2022010449301Vapor Barrier · crackedSUPPLEMENTAL INFORMATION: CRACKED LOWER R/H COMPOSITE BULKHEAD AT BS663 RBL50 WL164. ; / [01] PARTIAL ACCOMPLISHED FOR STEP 1.; [02] PARTIAL ACCOMPLISHED FOR STEP 2.; [03] PARTIAL ACCOMPLISHED FOR STEP 3.; [04] PARTIAL ACCOMPLISHED ON STEP 4.; [05] UPDATED MEADec 1, 2021 · N234WN · Boeing 737 · Wing Main, Frame StructureSDR SWAA2022010449296Angle · crackedSUPPLEMENTAL INFORMATION: B.S. 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT R.B.L. 42 W.L. 160. MARKED. ; / [01] UPDATE MEASUREMENT TABLE; [02] VALIDATED SRM 57-10-10-2R-5 REPAIR 5 TO BE CORRECT REPAIR; [16] INSTALLED REPAIR PARTS BS 663 RBL35-65 PER SRMDec 1, 2021 · N234WN · Boeing 737 · Wing Main, Frame StructureSDR SWAA2021113047791None · failedLEFT FRONT GIRT BARD HARD TO STOW AND REMOVE ; / [01] REPLACED FORWARD ENTRY DOOR SLIDER PER MT 725-61-06. OPS CHECKS OK.Nov 26, 2021 · N234WN · Boeing 7377H4 · Escape Slide
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